NACA
Digital Library - UK Mirror
7640 records
- Diederichs, H Upton, G
B; Mufflers for
aeronautic engines; naca-report-10; 1917
- Lucke, Charles Edward
Willhofft, Friederich Otto; Carburetor
design - a preliminary study of the state of the art; naca-report-11;
1917
- Marchis, L; Experimental
researches on the resistance of air; naca-report-12; 1917
- (Author(s) Not
Available); General
specifications covering requirements of aeronautic instruments;
naca-report-8; 1917
- Blair, William R; Meteorology and
aeronautics; naca-report-13; 1917
- Hunsaker, J C Wilson,
Edward Bidwell; Report on behavior
of aeroplanes in gusts; naca-report-1; 1917
- Sunderlang, C C Horn, H
J Green, D; Report on
investigations of aviation wires and cables, their fastenings and terminal
connections; naca-report-3; 1917
- (Author(s) Not
Available); Relative worth of
improvements of fabrics; naca-report-5; 1917
- Lucke, Charles E; Thermodynamic
efficiency of present types of internal combustion engines for aircraft;
naca-report-7; 1917
- Gorrell, E. S., Martin,
H. S.; Aerofoils and
Aerofoil Structural Combinations; naca-report-18; 1917
- Durand, William F; Experimental
research on air propellers; naca-report-14; 1918
- Haas, Rudolf Dietzius,
Alexander; The
stretching of the fabric and the deformation of the envelope in nonrigid
balloons; naca-report-16; 1918
- Klemin, Alexander
Warner, Edward P Denkinger, George M; An
investigation of the elements which contribute to statical and dynamical
stability, and of the effects of variation in those elements;
naca-report-17; 1918
- Gorrell, Edgar S
Martin, H S; Aerofoils and
aerofoil structural combinations; naca-report-18; 1918
- Ames, Joseph S; Aerodynamic
coefficients and transformation tables; naca-report-20; 1918
- Wilson, Edwin Bidwell;
Theory of an
airplane encountering gusts II; naca-report-21; 1918
- Walen, E D; Fabrics
for aeronautic construction; naca-report-22; 1918
- Dickinson, H C; Aeronautic power
plant investigations; naca-report-23; 1918
- ; Nomenclature
for aeronautics; naca-report-15; 1918
- Zahm, A. F.; Periodic
stresses in gyroscopic bodies, with applications to air screws;
naca-report-19; 1918
- Smith, W H; Airplane
dopes and doping; naca-report-38; 1919
- Wm Knight; Italian
and French experiments on wind tunnels; naca-tn-17; Nov 1920
- W. Stieber; The
dynamometer hub; naca-tn-18; Sep 1920
- W. Margoulis; The
steadiness factor in engine sets; naca-tn-19; Jan 1920
- George De Bothezat; Airplane
performance as influenced by the use of a supercharged engine; naca-tn-2;
May 1920
- S. W. Sparrow; High
thermal efficiency in airplane service; naca-tn-39; Dec 1920
- E. P. Warner; The
problem of the helicopter; naca-tn-4; May 1920
- A. Baumann; Progress
made in the construction of giant airplanes in Germany during the war;
naca-tn-29; Dec 1920
- A. Betz; Development
of the inflow theory of the propeller; naca-tn-24; Nov 1920
- Karl D. Wood; A
variable speed fan dynamometer; naca-tn-26; Dec 1920
- S. W. Sparrow; Instrument
for measuring engine clearance volumes; naca-tn-27; Dec 1920
- E. P. Warner; Notes
on the theory of the accelerometer; naca-tn-3; May 1920
- F. H. Norton; Design
of recording wind tunnel balances; naca-tn-30; Dec 1920
- A. Toussaint; Drag
or negative traction of geared-down supporting propellers in the downward
vertical glide of a helicopter; naca-tn-21; Sep 1920
- W. Margoulis; Notes
on specifications for French airplane competitions; naca-tn-20; Oct
1920
- F. H. Norton; The
photographic recording of small motions; naca-tn-22; Nov 1920
- A. F. Zahm; Relation
of rib spacing to stress in wing planes; naca-tn-5; May 1920
- E. P Warner; Static
testing and proposed standard specifications; naca-tn-6; Jul 1920
- A. F. Zahn; Horizontal
buoyancy in wind tunnels; naca-tn-23; Nov 1920
- L. Prandtl; Gottingen
Wind Tunnel for testing aircraft models; naca-tn-66; Nov 1920
- Schwager; Notes
on the design of supercharged and overdimensioned aircraft engines;
naca-tn-7; Jul 1920
- E. Unger, E. Schmidt;
Duralumin;
naca-tn-8; Jul 1920
- L. Prandtl; Theory
of lifting surfaces; naca-tn-9; Jul 1920
- K. Kutzbach; Experience
with geared propeller drives for aviation engines; naca-tn-16; Sep
1920
- Edward P. Warner; Notes on
longitudinal stability and balance; naca-tn-1; Apr 1920
- L. Prandtl; Theory
of lifting surfaces; naca-tn-10; Aug 1920
- Rene Devillers; The problem of
the turbo-compressor; naca-tn-11; Aug 1920
- Schwager; Recent
efforts and experiments in the construction of aviation engines;
naca-tn-12; Sept 1920
- P. Idrac; Soaring
flight in Guinea; naca-tn-13; Aug 1920
- S. W. Sparrow; Increase
in maximum pressures produced by preignition in internal combustion
engines; naca-tn-14; Aug 1920
- W. G. Noack; Tests
of the Daimler D-IVa engine at a high altitude test bench; naca-tn-15; Oct
1920
- Lewis, G W Nutting, E
M; Air flow
through poppet valves; naca-report-24; 1920
- Wilson, Edwin Bidwell;
The variation
of yawing moment due to rolling; naca-report-26; 1920
- Wilson, Edwin Bidwell;
Theory of an
airplane encountering gusts III; naca-report-27; 1920
- De Bothezat, George; An introduction
to the laws of air resistance of aerofoils; naca-report-28; 1920
- De Bothezat, George; The general
theory of blade screws including propellers, fans, helicopter screws,
helicoidal pumps, turbo-motors, and different kinds of helicoidal blades;
naca-report-29; 1920
- Durand, William F
Lesley, E P; Experimental
research on air propellers II; naca-report-30; 1920
- Zahm, A F; Development
of air speed nozzles; naca-report-31; 1920
- Larson, L J; The
airplane tensiometer; naca-report-32; 1920
- Dorsey, N E; Self-luminous
materials; naca-report-33; 1920
- Merica, Paul D; Aluminum and its
light alloys; naca-report-34; 1920
- Nelson, John H; The strength of
one-piece solid, build-up and laminated wood airplane wing beams;
naca-report-35; 1920
- Walen, E Dean; The
structure of airplane fabrics; naca-report-36; 1920
- Walen, E D Fisher, R T;
Fabric
fastenings; naca-report-37; 1920
- Edwards, Junius David
Moore, Irwin L; The
testing of balloon fabrics; naca-report-39; 1920
- Weaver, E R Berry, W M
Bohnson, V L Gordon, B D; The
ferrosilicon process for the generation of hydrogen; naca-report-40;
1920
- Edwards, Junius David;
Testing
balloon gas; naca-report-41; 1920
- Paris, Auguste Jean, Jr
Paris, W Francelyn; A
new process for the production of aircraft-engine fuels; naca-report-42;
1920
- Dickinson, H C
Kleinschmidt, R V; Synopsis
of aeronautic radiator investigations for years 1917 and 1918;
naca-report-43; 1920
- Dickinson, H C Boutell,
H G; The
altitude laboratory for the test of aircraft engines; naca-report-44;
1920
- Dickinson, H C
(National Bureau of Standards) James, W S Anderson, G V Brinkerhoff, V W; Effect of
compression ratio, pressure, temperature, and humidity on power;
naca-report-45; 1920
- Gage, Victor R; A study of
airplane engine tests; naca-report-46; 1920
- Dickinson, W S James, W
S Roberts, E W Gage, V R Harper, D R Iii; Power
characteristics of fuels for aircraft engines; naca-report-47; 1920
- Tice, Percival S; Carbureting
conditions characteristics of aircraft engines; naca-report-48;
1920
- Tice, Percival S
Dickinson, H C; Metering
characteristics of carburetors; naca-report-49; 1920
- Kemble, E C; Calculation
of low-pressure indicator diagrams; naca-report-50; 1920
- Gorton, W S; The
subsidiary gap as a means for improving ignition; naca-report-57;
1920
- Silsbee, F B; Characteristics
of high-tension magnetos; naca-report-58; 1920
- Dickinson, H C James, W
S Kleinschmidt, R V; General
analysis of airplane radiator problems; naca-report-59; 1920
- Dickinson, H C James, W
S Brown, W B; General
discussion of test methods for radiators; naca-report-60; 1920
- Kleinschmidt, R V
Parsons, S R; Head resistance
due to radiators; naca-report-61; 1920
- James, W S Parsons, S
R; Effect of
altitude on radiator performance; naca-report-62; 1920
- Dickinson, H C James, W
S Kleinschmidt, R V; Results
of tests on radiators for aircraft engines; naca-report-63; 1920
- Durand, W F Lesley, E
P; Experimental
research on air propellers III; naca-report-64; 1920
- Tiemann, Harry D; The kiln drying
of wood for airplanes; naca-report-65; 1920
- Allen, S W Truax, T R;
Glues used in
airplane parts; naca-report-66; 1920
- Sparhawk, W N; Supplies
and production of aircraft wood; naca-report-67; 1920
- Wilson, T R C; The
effect of kiln drying on the strength of airplane woods; naca-report-68;
1920
- Coffin, J G; A
study of airplane ranges and useful loads; naca-report-69; 1920
- Warner, E P Norton, F
H; Preliminary
report on free flight tests; naca-report-70; 1920
- Warner, Edward P; Slip-stream
corrections performance computation; naca-report-71; 1920
- Warner, Edward P
Norton, F H; Wind tunnel
balances; naca-report-72; 1920
- Warner, Edward P
Norton, F H Hebbert, C M; The
design of wind tunnels and wind tunnel propellers; naca-report-73;
1920
- Norton, F H; Construction
of models for tests in wind tunnels; naca-report-74; 1920
- Norton, F H; The
aerodynamic properties of thick aerofoils suitable for internal bracing;
naca-report-75; 1920
- Warner, Edward P
Miller, Roy G; Fuselage stress
analysis; naca-report-76; 1920
- Parker, H F; The
Parker variable camber wing; naca-report-77; 1920
- Wilson, Edwin Bidwell;
The limiting
velocity in falling from a great height; naca-report-78; 1920
- Wilson, Edwin Bidwell;
Bomb
trajectories; naca-report-79; 1920
- Froude, W; On
the elementary relation between pitch, slip, and propulsive efficiency;
naca-tm-1; July 1920
- (Author(s) Not
Available); Variable pitch
propellers; naca-tm-2; November 1920
- Woodward, R W (Bureau
of Standards); Recent
developments in light alloys; naca-tm-3; November 1920
- Gradenwitz, Arthur; Tests of
artificial flight at high altitudes; naca-tm-4; November 1920
- Silsbee, F. B., Loeb,
L. B., Sawyer, L. G., Fonseca, E. L, Dickinson, H. C., Agnew, P. G.; Spark
plug defects and tests; naca-report-51; 1920
- Cragoe, C. S.; Temperatures
in spark plugs having steel and brass shells; naca-report-52; 1920
- Silsbee, F. B.,
Honaman, R. K., Fonseca, E. L., Bleininger, A. V., Staley, H. F.; Properties
and preparation of ceramic insulators for spark plugs; naca-report-53;
1920
- Loeb, L. B., Silsbee,
F. B.; Effect
of temperature and pressure on the sparking voltage; naca-report-54;
1920
- Upton, G. B., Gage, V.
R.; Investigation of
the muffling problem for airplane engines; naca-report-55; 1920
- Silsbee, F. B., Loeb,
L. B., Fonseca, E. L.; Heat
energy of various ignition sparks; naca-report-56; 1920
- Zahm, A. F., Crook, L.
H.; Airplane
stress analysis; naca-report-82; 1920
- ; Nomenclature
for aeronautics; naca-report-25; 1920
- F. H. Norton; A
mechanical device for illustrating airplane stability; naca-tn-76;
December, 1921
- Ing Stelmachowski; Loads and
calculations of army airplanes; naca-tn-28; Feb 1921
- W. E. Davidson, D. L.
Bacon; The
determination of the effective resistance of a spindle supporting a model
airfoil; naca-tn-37; Jan 1921
- Ing V. Heidelberg; Measurements of
rudder moments on an airplane during flight; naca-tn-38; Jan 1921
- A. Toussaint; Note
on the resistance of polished cylinders (and cylindrical wires) with
generatrices perpendicular to the airstream; naca-tn-43; Feb 1921
- Fr. Natalis; Crippling
strength of axially loaded rods; naca-tn-31; Oct 1921
- Marsden Ware; Effect
of the reversal of air flow upon the discharge coefficient of Durley
Orifices; naca-tn-40; Feb 1921
- F. B. Silsbee; Causes
of cracking of ignition cable; naca-tn-32; Feb 1921
- Ing C. Wieselsberger;
The effect of
the nature of surfaces on resistance as tested on struts; naca-tn-33; Feb
1921
- A Betz; Influence
of span and load per square meter on the air forces of the supporting
surface; naca-tn-41; Mar 1921
- D. P. Riabouchinshy; On the
Resistance of spheres and ellipsoids in wind tunnels; naca-tn-44; Jan
1921
- A. Toussaint, Hayer; Extract from a
report on the resistance of spheres of small diameter in an airstream of high
velocity; naca-tn-45; Mar 1921
- Wilhelm Hoff; Theory
of the ideal windmill; naca-tn-46; Jul 1921
- Prof. Karman; Recent
European developments in helicopters; naca-tn-47; Apr 1921
- W. G. Noack; Airplane
superchargers; naca-tn-48; May 1921
- D. Riabouchinski; On the
resistance of the air at high speeds and on the automatic rotation of
projectiles; naca-tn-49; Apr 1921
- A. Heller; The
300 H.P. Benz aircraft engine; naca-tn-34; Jan 1921
- F. H. Norton, D. L.
Bacon; The
optical wing aligning device of the Langley Field tunnel; naca-tn-35; Jan
1921
- Walter S. Diehl; The
determination of downwash; naca-tn-42; Jan 1921
- F. H. Norton, D. L.
Bacon; N.A.C.A. Langley
field wind tunnel apparatus the tilting manometer; naca-tn-36; Jan
1921
- W. Margoulis; Gordon
Bennett Airplane Cup; naca-tn-50; Apr 1921
- L. Huguet; Airplane
balance; naca-tn-51; Jun 1921
- W. Margoulis; A
new method of testing in wind tunnels; naca-tn-52; Aug 1921
- D. L. Bacon; Similitude
tests on wind sections; naca-tn-53; Mar 1921
- F. H. Norton; The
factors that determine the minimum speed of an airplane; naca-tn-54; Mar
1921
- Stanwood W. sparrow; Airplane
crashes: engine troubles : a possible explanation; naca-tn-55; Mar
1921
- Wilhelm Hoff; The
development of German Army airplanes during the war; naca-tn-56; Jun
1921
- Max Munk; The
Caproni Seaplane; naca-tn-57; Jul 1921
- Max Munk; Absolute
coefficients and the graphical representation of airfoil characteristics;
naca-tn-58; Jun 1921
- O. Enoch; The
dynamometer hub for the testing propellers and engines during flight;
naca-tn-59; Jul 1921
- Max Munk; On
a new type of wind tunnel; naca-tn-60; May 1921
- R. H. Heald; Performance
of a vane driven-gear pump; naca-tn-61; Sep 1921
- W. S. James; The
problem of fuel for aviation engines; naca-tn-62; Jul 1921
- Umberto Nobile; The employment
of airships for the transport of passengers; naca-tn-63; Aug 1921
- F. H. Norton; N.A.C.A.
recording air speed meter; naca-tn-64; Oct 1921
- D. L. Bacon; Langley
Field wind tunnel apparatus; naca-tn-65; Oct 1921
- Arthur E. Raymond; Ground influence
on airfoils; naca-tn-67; Dec 1921
- A. Betz; Vortices
and the related principles of hydrodynamics; naca-tn-68; Nov 1921
- F. H. Norton; An
investigation on the effect of raked wing tips; naca-tn-69; Nov
1921
- F. H. Norton; The
effect of staggering a biplane; naca-tn-70; Sep 1921
- G. Lachmann; Experiments
with slotted wings; naca-tn-71; Nov 1921
- M. D. Hersey; Aneroid
investigations in Germany; naca-tn-72; Oct 1921
- Edward P. Warner; The choice of
wing sections for airplanes; naca-tn-73; Nov 1921
- L. Prandtl; Mutual
influence of wings and propeller; naca-tn-74; Dec 1921
- L. Prandtl; Effects
of varying the relative vertical position of wing and fuselage;
naca-tn-75; Dec 1921
- Norton, F H Warner,
Edward P; Accelerometer
design; naca-report-100; 1921
- Kemble, E C; The
calculated performance of airplanes equipped with supercharging engines;
naca-report-101; 1921
- Sparrow, S W White, H
S; Performance of a
Liberty 12 airplane engine; naca-report-102; 1921
- (Author(s) Not
Available); The law relating
to air currents; naca-tm-10; March 1921
- Sparrow, S W White, H
S; Performance of a
300-horsepower Hispano-Suiza airplane engine; naca-report-103; 1921
- Miller, Roy G; Torsion
of wing trusses at diving speeds; naca-report-104; 1921
- Warner, E P Norton, F
H; Angles of
attack and air speeds during maneuvers; naca-report-105; 1921
- Parsons, S R; Turbulence
in the air tubes of radiators for aircraft engines; naca-report-106;
1921
- Dickinson, H C Newell,
F B; A
high-speed engine pressure indicator of the balanced diaphragm type;
naca-report-107; 1921
- Gage, Victor R; Factors of
airplane engine performance; naca-report-108; 1921
- Durand, W F Lesley, E
P; Experimental
research on air propellers IV; naca-report-109; 1921
- Hersey, M D Hunt, F L
Eaton, H N; The altitude
effect on air speed indicators; naca-report-110; 1921
- (Author(s) Not
Available); Nomenclature for
aeronautics; naca-report-15; 1921
- Caldwell, F W Fales, E
N; Wind
tunnel studies in aerodynamic phenomena at high speed; naca-report-83;
1921
- Elmendorf, Armin; Data on the
design of plywood for aircraft; naca-report-84; 1921
- Dunlap, M E; Moisture
resistant finishes for airplane woods; naca-report-85; 1921
- Parsons, S R; Properties
of special types of radiators; naca-report-86; 1921
- Parsons, S R
Kleinschmidt, R V; Effects
of nature of cooling surface on radiator performance; naca-report-87;
1921
- Parsons, S R; Pressure
drop in radiator air tubes; naca-report-88; 1921
- Gage, V R Sparrow, S W
Harper, D R; Comparison of
alcogas aviation fuel with export aviation gasoline; naca-report-89;
1921
- Dickinson, H C Gage, V
R Sparrow, S W; Comparison
of hecter fuel with export aviation gasoline; naca-report-90; 1921
- Warner, E P Miller, R
G; Analysis
of wing truss stresses including the effect of redundancies;
naca-report-92; 1921
- (Author(s) Not
Available); Aerodynamic
characteristics of aerofoils I; naca-report-93; 1921
- Norton, F H; The
efficiency of small bearings in instruments of the type used in aircraft;
naca-report-94; 1921
- Batemen, H; Diagrams
of airplane stability; naca-report-95; 1921
- Warner, Edward P; Statical
longitudinal stability of airplanes; naca-report-96; 1921
- De Bothezat, George; General theory
of the steady motion of an airplane; naca-report-97; 1921
- Norton, F H Warner,
Edward P; Design of wind
tunnels and wind tunnel propellers II; naca-report-98; 1921
- Norton, F H Allen, E T;
Accelerations
in flight; naca-report-99; 1921
- (Author(s) Not
Available); The Goebel
rotary engine; naca-tm-11; March 1921
- Margoulis, W; Abacus
giving the variation of the mean pressure of an aviation engine as a function
of its speed of rotation; naca-tm-12; March 1921
- (Author(s) Not
Available); The Oehmichen
Peugeot helicopter; naca-tm-13; 1921
- Boccaccio, Paul; The coupling of
engines; naca-tm-14; April 1921
- Rateau, A; Resume
of the theory of naval and aerial propulsive propellers and of airplanes in
the rectilinear flight; naca-tm-17; April 1921
- (Author(s) Not
Available); Rates for
flights organized by the state; naca-tm-18; April 1921
- (Author(s) Not
Available); The technical
development of the transport airplane.Report of the Aero-Technical Conference
of the Scientific Association for Aeronautics, March 5, 1919; naca-tm-19;
April 1921
- (Author(s) Not
Available); Sixth meeting of
the members of the German Scientific Association for Aeronautics;
naca-tm-20; April 1921
- Rohbach, A K (Zeppelin
Works, Staaken, Germany); Transport
airplanes; naca-tm-22; April 1921
- (Author(s) Not
Available); British
certificates of airworthiness; naca-tm-23; May 1921
- Volterra, Vito; Observations on
the method of determining the velocity of airships; naca-tm-24; June
1921
- Everling, E (German
Aeronautical Laboratory); The
dynamometer hub and the flywheel of the engine; naca-tm-25; June
1921
- Kook, E; Simple
means for saving fuel on traffic flights; naca-tm-26; June 1921
- Proll, A; Flexibility
of bearing surfaces and stress on fabrics; naca-tm-27; June 1921
- Tenani, Mario; Abacus
for the reduction of English measures to the metric system and vice versa;
naca-tm-30; July 1921
- (Author(s) Not
Available); Flexible petrol
pipe; naca-tm-31; July 1921
- Pegna, G; High
efficiency of seaplanes; naca-tm-32; August 1921
- Ratzersdorfer, Julius;
Calculation
of wing spars; naca-tm-34; August 1921
- Muller-Breslau, H; Calculation of
wing spars; naca-tm-35; August 1921
- Sabatier, J; Large
German airship stations; naca-tm-36; August 1921
- Lewe, Victor; Shape
and strength of seaplane under-structures with special regard to
seaworthiness; naca-tm-37; August 1921
- Schwager, Otto; Preliminary
calculation of cylinder dimensions for aircraft engines; naca-tm-38;
September 1921
- (Author(s) Not
Available); Competition for
safety fuel tanks; naca-tm-39; September 1921
- Nicolson, David; Glossary of
terms used in flying boat hull construction; naca-tm-40; September
1921
- Frey, Ernst; The
small diesel engine as an automotive engine; naca-tm-43; September
1921
- Segre, Marco; A
new dynamometer brake; naca-tm-44; September 1921
- Heidelberg, V; Influence
of struts and stays on the speed of an airplane; naca-tm-46; October
1921
- Prandtl, L; Some
remarks concerning soaring flight; naca-tm-47; October 1921
- (Author(s) Not
Available); A
petrol-proof flexible tubing at last: an invention of the greatest importance
to aviation; naca-tm-48; October 1921
- Kempe, Erich; Establishment
of aviation schools; naca-tm-49; November 1921
- Wronsky, W; Commercial
aviation in Germany : past and future; naca-tm-5; February 1921
- (Author(s) Not
Available); Extracts from
the Belgian regulations for government assistance to air transport
companies; naca-tm-50; November 1921
- Bouche, Henri; Aeronautic
instruction in Germany; naca-tm-51; November 1921
- Hopf, L; The
danger of stalled flight and an analysis of the factors which govern it;
naca-tm-52; November 1921
- Leyensetter, Walther;
Traffic
airships with special reference to economy; naca-tm-53; November
1921
- Borck, Hermann; Dependence of
propeller efficiency on angle of attack of propeller blade; naca-tm-54;
1921
- Langsdorff, Werner V;
The Rumpler
passenger airplane; naca-tm-6; March 1921
- Norton, F H; The
art of writing scientific reports; naca-tm-7; March 1921
- (Author(s) Not
Available); Development of
aeronautical engines by the Army and Navy; naca-tm-9; March 03,
1921
- ; Nomenclature
for aeronautics; naca-report-91; 1921
- A. Betz; Theory
of the slotted wing; naca-tn-100; June, 1922
- Stanwood W. Sparrow,
Stephen M. Lee; Comparing
maximum pressures in internal combustion engines; naca-tn-101; June,
1922
- W. S. Diehl; Skin
frictional resistance of plane surfaces in air; naca-tn-102; July,
1922
- Walter S. Diehl; Simple formula
for estimating airplane ceilings; naca-tn-103; June, 1922
- Max M. Munk; Notes
on aerodynamic forces I : rectilinear motion; naca-tn-104; July,
1922
- Max M. Munk; Notes
on aerodynamic forces II : curvilinear motion; naca-tn-105; July,
1922
- Max M. Munk; Notes
on aerodynamic forces III : the aerodynamic forces on airships;
naca-tn-106; July, 1922
- Adolf Rohrbach; Structural
safety during curved flight; naca-tn-107; August, 1922
- Standwood S. Sparrow;
The use of
multiplied pressures for automatic altitude adjustments; naca-tn-108;
January, 1922
- Max M. Munk; The
twisted wing with elliptic plan form; naca-tn-109; August, 1922
- H. I. Hood, D. L.
Bacon; The
effect on rudder control of slip stream body, and ground interference;
naca-tn-110; September, 1922
- Max M. Munk; Stresses
produced on an airship flying through gusty air; naca-tn-111; September,
1922
- H. J. E. Reid; The
NACA three component accelerometer; naca-tn-112; October, 1922
- Edward P. Warner; Report on the
general design of commercial aircraft; naca-tn-113; September, 1922
- H. S. McDewell; Supplementary
report of oil scraper piston rings; naca-tn-114; September, 1922
- F. H. Norton, T.
Carroll; The
effect of longitudinal moment of inertia upon dynamic stability;
naca-tn-115; October, 1922
- W. S. Diehl; Comparative
performance with direct and geared engines; naca-tn-116; October,
1922
- W. G. Brown; The
synchronization of NACA flight records; naca-tn-117; October, 1922
- W. S. Diehl; F-5-L
Boat Seaplane : performance characteristics; naca-tn-118; October,
1922
- Thomas Carroll; The elimination
of dead center in the controls of airplanes with thick sections;
naca-tn-119; November, 1922
- F. H. Norton, W. G.
Brown; A
preliminary study of airplane performance; naca-tn-120; November,
1922
- C. Wieselsberger; Further
information on the laws of fluid resistance; naca-tn-121; December,
1922
- F. H. Norton; A
preliminary investigation of a new method for testing aerofoils in free
flight; naca-tn-77; January, 1922
- Bureau of Standards; Impact tests for
woods; naca-tn-78; February, 1922
- Walter S. Diehl; Effect of
aerofoil aspect ratio on the slope of the lift curve; naca-tn-79; January,
1922
- Colonel Crocco; The dead weight
of the airship and the number of passengers that can be carried;
naca-tn-80; January, 1922
- D. L. Bacon; Langley
Field wind tunnel apparatus; naca-tn-81; January, 1922
- Walter S. Diehl; Notes on the
construction and testing of model airplanes; naca-tn-82; January,
1922
- A. Betz; The
theory of the screw propeller; naca-tn-83; February, 1922
- C. Wieselsberger; New data on the
laws of fluid resistance; naca-tn-84; March, 1922
- Aeronautics Staff,
Construction Department, Navy Yard, Washington, D.C.; Air
force and three moments for F-5-L Seaplane; naca-tn-85; February,
1922
- W. S. Diehl; Surface
area coefficients for airship envelopes; naca-tn-86; February, 1922
- Aeronautics Staff,
Construction Department, Navy Yard, Washington, D. C.; Hydrostatic
tests of an airship model; naca-tn-87; March, 1922
- H. S. McDewell; Tests of oil
scraper piston ring and piston fitted with oil drain holes; naca-tn-88;
August, 1922
- Max M. Munk; The
choice of the speed of an airship; naca-tn-89; March, 1922
- H. N. Eaton, G. H.
Keulegan; Syphon
diaphragms : a method for predicting their performance for purposes of
instrument design; naca-tn-90; January, 1922
- Max M. Munk; Notes
on propeller design I : the energy losses of the propeller; naca-tn-91;
April, 1922
- Max M. Munk; Full
scale determination of the lift and drag of a seaplane; naca-tn-92; April,
1922
- Stanwood S. Sparrow; The background
of detonation; naca-tn-93; April, 1922
- Max M. Munk; Notes
on propeller design II: The Distribution of Thrust Over a Propeller;
naca-tn-94; April, 1922
- Max M. Munk; Notes
on propeller design III; naca-tn-95; May, 1922
- Max M. Munk; Notes
on propeller design IV : general proceeding in design; naca-tn-96; May,
1922
- F. H. Norton; N.A.C.A.
control position recorder; naca-tn-97; January, 1922
- Charles J. McCarthy; Notes on the
design of latticed columns subject to lateral loads; naca-tn-98; May,
1922
- Walter S. Diehl; Notes on the
standard atmosphere; naca-tn-99; June, 1922
- W. S. Diehl; Center
of pressure coefficients for airfoils at high speeds; naca-tn-25; Apr
1922
- Hoff, Wilhelm; Lecture
on the Rhon soaring flight competition, 1921; naca-tm-100; June
1922
- (Author(s) Not
Available); Fakir fuel
pump; naca-tm-101; June 1922
- Becker, G; Engine
pistons of light metal; naca-tm-102; June 1922
- (Author(s) Not
Available); Effect of
structure in middle part of leading edge of a thick wing : communication from
Rijks-Studiedienst voor de Luchtvaart of Amsterdam; naca-tm-103; June
1922
- Klemperer, W; Problem
of the slotted wing : a communication from the Aerodynamic Institute of the
Aachen Technical High School; naca-tm-104; June 1922
- Herrera, Emilio; The R-38
catastrophe and the mechanics of rigid airship construction; naca-tm-105;
June 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Comfort
in flight; naca-tm-106; June 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); The
prospects of the helicopter; naca-tm-107; June 1922
- (Author(s) Not
Available); The world's air
transportation services : data as to passengers, mail, and goods carried by
American and European transportation services; naca-tm-108; June
1922
- Ravennes, Jean; Maritime
aviation; naca-tm-109; July 1922
- Arnstein, Karl; The stresses in
columns under combined axial and side loads; naca-tm-110; July 1922
- Burzio, Filippo
(Aeronautical Laboratory, Royal Polytechnical Institute, Turin); Aerodynamics
and ballistics; naca-tm-111; July 1922
- Vivent, Jacques; Politics of
aviation fields; naca-tm-112; July 1922
- Van Crombrugge, A
(Belgium Air Service); Aviation
in the Belgian Congo; naca-tm-113; July 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); European
air travel in 1922; naca-tm-114; July 1922
- Rota, Augusto; Airplane
stability calculations and their verification by flight tests;
naca-tm-115; July 1922
- (Author(s) Not
Available); Resume of the
activities of the Aeronautical Experimental Institute, Rome, during the months
of May, June, July and August 1921; naca-tm-116; July 1922
- Maffert, Pierre; Aerial
navigation by dead reckoning; naca-tm-117; July 1922
- Richard, Maurice
Richard, Paul; General
problem of the airplane; naca-tm-118; July 1922
- Senouque, A; Propeller
tests on airplanes; naca-tm-120; July 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); The
future of the airship; naca-tm-121; July 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); This
summer's gliding meets; naca-tm-122; July 1922
- Miner, V S (U. S. Air
Service) Carroll, T; Laying
out of a practical air route; naca-tm-123; July 1922
- Stadthagen, Paul; Illumination of
airways and landing fields; naca-tm-124; August 1922
- (Author(s) Not
Available); Description of
the Klemperer wing strain meter (accelerometer); naca-tm-125; August
1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Commercial
aircraft in war; naca-tm-126; August 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Potentialities
of the parachute; naca-tm-127; August 1922
- De Guiche, A De
Gramont; Turn
indicator; naca-tm-128; August 1922
- (Author(s) Not
Available); Test of specimen
of wood of longerons of the S.E.5 airplane after seven years' service;
naca-tm-129; August 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Police
regulation of aircraft; naca-tm-130; August 1922
- DE MAROLLES; Utilization
conditions of different types of airplanes; naca-tm-131; August
1922
- SACADURA CABRAL; Coutinho-Sacadura
course corrector; naca-tm-132; August 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Safety
in flight; naca-tm-133; August 1922
- JUBERA; Aerodynamic
laboratory at Cuatro Vientos; naca-tm-134; September 1922
- (Author(s) Not
Available); Fatigue
resistance of duralumin; naca-tm-135; September 1922
- Lippisch, Espenlaub; Problem of
glider models; naca-tm-136; September 1922
- Constantin, M Louis; Wind vane with
various applications; naca-tm-137; September 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Giant
airplanes; naca-tm-138; September 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); International
aspects of air travel; naca-tm-139; September 1922
- Schrenk, M; Aerodynamic
computation of gliders; naca-tm-140; September 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Miniature
airplanes; naca-tm-141; September 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); The
disposal of military aircraft; naca-tm-142; September 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); What
retards air transport?; naca-tm-143; September 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); The
prevention of fire in the air; naca-tm-144; September 1922
- Katzmayr, R; Deflection
of propeller blades while running; naca-tm-145; October 1922
- Prondzynski, Stephan V;
The wing with
a pointed tip; naca-tm-146; October 1922
- Sonntag, R; Best
rectangular and I-shaped cross sections for airplane wing spars;
naca-tm-148; October 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Training
of aeronautical engineers; naca-tm-149; October 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Air
transport economics; naca-tm-150; October 1922
- Hoff, Wilhelm; Computative
examination of bending strength of girders originally curved and subjected to
longitudinal compression; naca-tm-151; October 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); The
development of the racing airplane; naca-tm-152; November 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Metal
construction of aircraft; naca-tm-153; November 1922
- Kapteyn, A; Principle
of the Boerner airship; naca-tm-154; November 1922
- Bacon, David L; The "Universal"
adjustable and reversible propeller built by Paragon Engineers, Inc.,
Baltimore, Md; naca-tm-155; November 1922
- Eiffel, G; Method
rendering it possible, in testing airplane wing models at the Eiffel
Laboratory, to obtain comparable polars, whether the supports are attached to
the upper or lower side of model; naca-tm-156; November 1922
- (Author(s) Not
Available); Commercial
aviation in France; naca-tm-157; November 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); The
organization of airways; naca-tm-158; November 1922
- Warner, Edward P; Selling air
transport; naca-tm-159; November 1922
- Hamel, M; Type
of engine to employ; naca-tm-160; November 1922
- Warner, Edward P; Aeronautical
museums; naca-tm-161; November 1922
- Warner, Edward P; The usefulness
of stunting; naca-tm-162; November 1922
- Stapfer,; Comparison
of nonrigid and semirigid airships; naca-tm-163; November 1922
- Black, Archibald; How to lay out
and build an airplane landing field : notes on shape and size of plot, runway
details, type and arrangement of buildings, drainage of field, best kind of
grass and proper marking to aid pilots; naca-tm-164; November 1922
- MISES; Location
of center of pressure of airplane wings; naca-tm-165; November 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Lessons
of the glider meets; naca-tm-166; November 1922
- Martinot, Lagarde; Definition of
terms used in connection with commercial aircraft engines; naca-tm-167;
November 1922
- Reed, S Albert; Air reactions to
objects moving at rates above the velocity of sound with application to the
air propeller; naca-tm-168; November 1922
- Wieselsberger, C; Effect of method
of suspending models in airstream on resulting measurements; naca-tm-169;
November 1922
- LEROY (Bureau des
Longitudes); Effect of
temperature and pressure on watches and chronometers; naca-tm-170;
November 1922
- Sonntag, R Hoff, W; Causes of
failure of airship sheds; naca-tm-171; November 1922
- Chollet, L (Technical
Section of Aeronautics (S.T.Ae.)); Balloon
fabrics made of Goldbeater's skins; naca-tm-172; December 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Airplane
performance, past and present; naca-tm-173; December 1922
- POINT (Hanriot Airplane
Factory); Commercial
airplanes and seaplanes : thick wings or thin wings - all metal or mixed
construction; naca-tm-174; December 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Depreciation
of aircraft; naca-tm-175; December 1922
- Black, Archibald
(American Society of Mechanical Engineers); Influence
of design on cost of operating airplanes; naca-tm-176; December
1922
- Pistolesi, E (War
Department Air Services, Engineering Division, McCook Field, Dayton, Ohio.);
The problem
of landing; naca-tm-33; February 1922
- Prandtl, L; Recent
progress in the theory of air flow as applied to aeronautics; naca-tm-55;
1922
- Lagarde, Martinot C; Vibrations of
aviation engines; naca-tm-56; 1922
- Loth, William; Aerial
navigation : on the problem of guiding aircraft in a fog or by night when
there is no visibility; naca-tm-57; 1922
- Proll, A; Pressure
measurements during flight; naca-tm-58; November 1922
- Katzmayr, R Kirste, L;
The
aerodynamical laboratory of the Vienna Technical High School; naca-tm-61;
February 1922
- James, P; Marking
airdromes; naca-tm-62; February 1922
- Wendt, FR; Deterioration
of airplane fabrics; naca-tm-63; February 1922
- PIERROT; Aerial
transportation; naca-tm-64; February 1922
- Miller, Wm H
(Massachusetts Institute of Technology); The
efficiency of a wind tunnel; naca-tm-65; February 1922
- Wieselsberger, C; Manometer for
recording air speed; naca-tm-66; February 1922
- Carleman, M T; Differential
equations in airplane mechanics; naca-tm-67; March 1922
- Duval, A; Maps
and navigation methods; naca-tm-68; March 1922
- Bacon, David L; The "Universal
propeller": built by Paragon Engineers, Inc., Baltimore, Md; naca-tm-70;
March 1922
- Aujames, P (Service
Radio Meteo de la Compagnie Franco-Roumaine de Navigation Aerienne); Some
principles governing the establishment of meteorological stations along air
routes; naca-tm-71; March 1922
- Easter, Ewing; Notes
on landing places for sea planes along the Atlantic coast; naca-tm-72;
March 1922
- Fiore, Amedeo; Bagnulo
heavy fuel internal combustion engine and its employment in aviation;
naca-tm-73; March 1922
- Carlier, Andre; Publicity by
airplane; naca-tm-74; March 1922
- Neal, Erik
(Ingenieur-Conseil pour l'Aeronautique); Aeronautic
insurance; naca-tm-75; March 1922
- Toussaint, A
(Aerotechnic Institute of Saint Cyr); Evolution
of modern aviation and experimental and technical researches in aerodynamic
laboratories; naca-tm-76; April 1922
- Margoulis, W; Joukowski
wings; naca-tm-78; April 1922
- Margoulis, W; Propeller
theory of Professor Joukowski and his pupils; naca-tm-79; April
1922
- DORAND (Interallied
Mission of Berlin); Influence
of elliptical distribution of lift on strength of airplane wings;
naca-tm-80; April 1922
- (Author(s) Not
Available); Distribution of
pressure on fuselage of airplane model: communication from Rijks-Studiedienst
voor de Luchtvaart of Amsterdam; naca-tm-81; April 1922
- (Author(s) Not
Available); Test flight of
the Handley Page torpedo-carrying airplane; naca-tm-82; April 1922
- Tete, Albert; Organization
and exploitation of regular aerial transportation lines; naca-tm-83; April
1922
- ROBERT; Applying
the results of experiments on small models in the wind tunnel to the
calculation of full-sized aircraft; naca-tm-84; April 1922
- Royer, Etienne; Commercial
airplanes and seaplanes; naca-tm-85; April 1922
- Senouque, A; Testing
airplanes in flight: determining position of resultant of action of air and
longitudinal stability of an airplane at different angles of attack;
naca-tm-86; April 1922
- PORQUET; Irresponsibility
clause in air traffic contracts; naca-tm-87; April 1922
- Verduzio, Rodolfo
(Instituto Sperimentale Verduzio); Metal
construction; naca-tm-88; April 1922
- Sudre, G; Air
traffic; naca-tm-89; May 1922
- Ripert, Georges (Paris
College of Law and the School of Political Science); Proposed
air traffic law; naca-tm-90; May 1922
- DEVALUEZ; Regulation
of air traffic; naca-tm-91; May 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Stability
of airplanes; naca-tm-92; May 1922
- Mayo, R H (Societe
Anonyme d'Ingenieurs, Conseils Ogilvie et Co); Aviation
and insurance; naca-tm-93; May 1922
- Roper,; Aerial
convention of October 13, 1919; naca-tm-94; May 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Technical
problems of commercial flying; naca-tm-95; May 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); The
choice of air routes; naca-tm-96; May 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Night
flying; naca-tm-97; May 1922
- Warner, Edward P
(Massachusetts Inst. of Tech); Mechanical
aids to flight; naca-tm-98; May 1922
- Blume, W.; The
glider; naca-tm-59; 1922
- Schwager, O.; Behavior
of aviation engines at different air densities; naca-tm-60; 1922
- Max M. Munk; The
determination of the angles of attack of zero lift and of zero moment,;
naca-tn-122; January, 1923
- John A. C. Warner; An optical
altitude indicator for night landing; naca-tn-123; January, 1923
- Max M. Munk, Gunther
Cairo; Downwash of
airplane wings; naca-tn-124; January, 1923
- K. Kutzbach; Results
of experimental flights at high altitudes with Daimler, Benz and;
naca-tn-125; January, 1923
- Werner Heisenberg; Absolute
dimensions of Karman vortex motion; naca-tn-126; January, 1923
- H. Dietsius; The
air propeller, its strength and correct shape; naca-tn-127; February,
1923
- Max M. Munk, Wilhelm
Molthan; Tests on an
airplane model, AEG D I of the Allgemeine Elektricitats Gesellschft, A-G,
airplane construction section conducted at the Gottingen Model Testing
Laboratory for Aerodynamics; naca-tn-128; February, 1923
- L. B. Tuckerman; Notes on
aerodynamic forces on airship hulls; naca-tn-129; March, 1923
- David L. Bacon; Model supports
and their effects on the results of wind tunnel tests; naca-tn-130;
February, 1923
- W. Achenbach; Variation
in the number of revolutions of air propellers; naca-tn-131; March,
1923
- E. Everling; The
increase in dimensions of airplanes - weight, area, and loading of wings;
naca-tn-132; March, 1923
- A. Riedler; Disturbing
effect of free hydrogen on fuel combustion in internal combustion engines;
naca-tn-133; March, 1923
- William Knight, L.
Prandtl, von Karman, G. Costanzi, W. Margoulis, R. Verduzio, R. Katzmayr, E.
B. Wolff, A. F. Zahm; Standardization
and aerodynamics; naca-tn-134; March, 1923
- W. G. Brown; Measuring
an airplane's true speed in flight testing; naca-tn-135; April,
1923
- P. Meyer, April, 1923;
Is there any
available source of heat energy lighter than gasoline?; naca-tn-136;
- A. Proell; Experiments
with fabrics for covering airplane wings; naca-tn-137; April, 1923
- Richard Baumann; Determination of
the value of wood for structural purposes; naca-tn-138; April, 1923
- L. Ballenstedt; Influence of
ribs on strength of spars; naca-tn-139; May, 1923
- W. Watters Pagon; General theory
of stresses in rigid airship, ZR-1; naca-tn-140; May, 1923
- C. Wiesselsberger; Experiments with
a built-in or fuselage radiator; naca-tn-141; May, 1923
- K. Kutzbach; Adaptation
of aeronautical engines to high altitude flying; naca-tn-142; May,
1923
- O. Blumenthal; Calculations
for a single-strut biplane with reference to the tensions in the wing
bracing; naca-tn-143; June, 1923
- W. S. Diehl; Notes
on the design of ailerons; naca-tn-144; June, 1923
- Kurt Bennewitz; Aeronautical
instruments; naca-tn-145; June, 1923
- Edward P. Warner; The faring of
airfoil contours; naca-tn-146; June, 1923
- V. Heidelberg, A.
Hoelzel; Speed
measurements made by Division A of the airplane director; naca-tn-147;
July, 1923
- K. Kutzbach; The
flexible mounting of an airplane engine; naca-tn-148; July, 1923
- Robertson Matthews; Influences in
the selection of a cycle for small high speed engines running on solid or
airless injection with compression ignition; naca-tn-149; July,
1923
- H. J. E. Reid; Notes
on the N.A.C.A. control force recorder; naca-tn-150; July, 1923
- T. A. Schwamb, C. S.
Smith; Tests
on built-up airplane struts having initial tension in outside fibers;
naca-tn-151; August, 1923
- George Koenig; Thrust
and power required in climbing; naca-tn-152; August, 1923
- Student; Flight
characteristics; naca-tn-153; August, 1923
- K. M. Ronan; An
instrument for recording the position of airplane control surfaces;
naca-tn-154; August, 1923
- (Author(s) Not
Available); Regulations
governing the issuance of certificates of airworthiness of aircraft in
France; naca-tn-155; August, 1923
- H. J. E. Reid; The
N.A.C.A. recording tachometer and angle of attack recorder; naca-tn-156;
August, 1923
- W. F. Joachim; An
impulse electric motor for driving recording instruments; naca-tn-157;
September, 1923
- Max M. Munks; Analysis
of Dr. Schaffran's propeller model tests; naca-tn-158; September,
1923
- Robertson Matthews, A.
W. Gardiner; The time lag and
interval of discharge with a spring actuated fuel injection pump;
naca-tn-159; September, 1923
- P. Eydam; Fittings
and other structural parts of airplanes; naca-tn-160; October, 1923
- James M. Shoemaker,
John G. Lee; Preliminary
study of the damping factor in roll; naca-tn-161; October, 1923
- Stanwood S. Sparrow; The arithmetic
of distribution in multi-cylinder engines; naca-tn-162; October,
1923
- Adolph Rohrbach, Edwin
Lupberger; Graphic method
for calculating the speed and climbing ability of airplanes; naca-tn-163;
October, 1923
- Max M. Munk; General
theory of windmills; naca-tn-164; October, 1923
- H. F. Rettew, G.
Thumin; Tests
on riveted joints in sheet duralumin; naca-tn-165; November, 1923
- H. Blasius; Determination
of climbing ability; naca-tn-166; February, 1923
- Edward P. Warner; Wind tunnel
tests of five strut sections in yaw; naca-tn-167; November, 1923
- A. Proll; Experiments
with fabrics for covering airplane wings, to determine effect of method of
installation; naca-tn-168; December, 1923
- C. Weiselsberger; Air resistance
measurements on actual airplane parts; naca-tn-169; November, 1923
- Max M. Munk; Reduction
in efficiency of propellers due to slipstream; naca-tn-170; December,
1923
- Viktor Lewe; Compressive
Strength of Tapered Airplane Struts; naca-tn-171; December, 1923
- James B. Ford; The
Nichols wing cutting equipment; naca-tn-172; December, 1923
- Diehl, Walter S; The variation of
aerofoil lift and drag coefficients with changes in size and speed;
naca-report-111; 1923
- Norton, F H Allen, E T;
Control in
circling flight; naca-report-112; 1923
- Durand, W F Lesley, E
P; Tests on
air propellers in yaw; naca-report-113; 1923
- Munk, Max M; Some
new aerodynamical relations; naca-report-114; 1923
- Burgess, C P; Bending
moments, envelope, and cable stresses in non-rigid airships;
naca-report-115; 1923
- Prandtl, L (Gottingen
Univ. (Germany, F. R.)); Applications
of modern hydrodynamics to aeronautics; naca-report-116; 1923
- Munk, Max M; The
drag of Zeppelin airships; naca-report-117; 1923
- Norton, F H; The
pressure distribution over the horizontal tail surfaces of an airplane I;
naca-report-118; 1923
- Norton, F H; Practical
stability and controllability of airplanes; naca-report-120; 1923
- Munk, Max M; The
minimum induced drag of aerofoils; naca-report-121; 1923
- Bacon, D L; Preliminary
experiments to determine scale and slip-stream effects on a 1/24th size model
of a JN4H biplane; naca-report-122; 1923
- Silsbee, F B; Simplified
theory of the magneto; naca-report-123; 1923
- (Author(s) Not
Available); Aerodynamic
characteristics of aerofoils II : continuation of report no. 93;
naca-report-124; 1923
- Hersey, Mayo D; Aeronautic
instruments. Section I : general classification of instruments and problems
including bibliography; naca-report-125; 1923
- Mears, A H Henrickson,
H B Brombacher, W G; Aeronautic
instruments. Section II : altitude instruments; naca-report-126;
1923
- Hunt, Franklin L
Stearns, H O; Aeronautic
instruments. Section III : aircraft speed instruments; naca-report-127;
1923
- Franklin, W S Stillman,
M H Sanford, R L Warner, John A C Sylvander, R C Rounds, E W; Aeronautic
instruments. Section IV : direction instruments; naca-report-128;
1923
- Hunt, F L; Aeronautic
instruments. Section VI : oxygen instruments; naca-report-130; 1923
- Eaton, H N; Aeronautic
instruments. Section VI : aerial navigation and navigating instruments;
naca-report-131; 1923
- Hunt, F L; Aeronautic
instruments. Section VIII : recent developments and outstanding problems;
naca-report-132; 1923
- Munk, Max M; The
tail plane; naca-report-133; 1923
- Sparrow, S W; Performance
of Maybach 300-horsepower airplane engine; naca-report-134; 1923
- Sparrow, S W; Performance
of B. M. W. 185-horsepower airplane engine; naca-report-135; 1923
- Chu, Lynn; Damping
coefficients due to tail surfaces in aircraft; naca-report-136;
1923
- Zahm, A F Smith, R H
Hill, G C; Point drag and
total drag of navy struts no. 1 modified; naca-report-137; 1923
- Zahm, A F Smith, R H
Hill, G C; The drag of C
class airship hull with varying length of cylindric midships;
naca-report-138; 1923
- Zahm, A F; Influence
of model surface and air flow texture on resistance of aerodynamic bodies;
naca-report-139; 1923
- Zahm, A F Bear, R M
Hill, G C; Lift and drag
effects of wing-tip rake; naca-report-140; 1923
- Durand, W F Lesley, E
P; Experimental
research on air propellers V; naca-report-141; 1923
- Munk, Max M; General
theory of thin wing sections; naca-report-142; 1923
- Hoff, Wilhelm; Analysis
of stresses in German airplanes; naca-report-143; 1923
- Bateman, H; The
decay of a simple eddy; naca-report-144; 1923
- Heim, A L Knauss, A C
Seutter, Louis; Internal
stresses in laminated construction; naca-report-145; 1923
- Zahm, A F; The
six-component wind balance; naca-report-146; 1923
- Gregg, Willis Ray; Standard
atmosphere; naca-report-147; 1923
- Norton, F H Brown, W G;
The pressure
distribution over the horizontal tail surfaces of an airplane III;
naca-report-148; 1923
- Norton, F H Brown, W G;
Pressure
distribution over the rudder and fin of an airplane in flight;
naca-report-149; 1923
- Norton, F H Bacon, D L;
Pressure
distribution over thick airfoils - model tests; naca-report-150;
1923
- Munk, Max M; General
biplane theory; naca-report-151; 1923
- Norton, F H Bacon, D L;
Aerodynamic
properties of thick airfoils II; naca-report-152; 1923
- Norton, F H Brown, W G;
Controllability
and maneuverability of airplanes; naca-report-153; 1923
- Carroll, T; A
study of taking off and landing an airplane; naca-report-154; 1923
- Reid, J E; A
study of airplane maneuvers with special reference to angular velocities;
naca-report-155; 1923
- Eaton, H N Macnair, W
A; The
altitude effect on air speed indicators II; naca-report-156; 1923
- Harper, R R Brown, W B;
Mathematical
equations for heat conduction in the fins of air-cooled engines;
naca-report-158; 1923
- Washburn, G E
Sylvander, R C Mueller, E F Wilhelm, R M Eaton, H N Warner, John A C; Aeronautic
instruments. Section V : power plant instruments; naca-report-129;
1923
- Norton, F H Bacon, D L;
The pressure
distribution over the horizontal tail surfaces of an airplane II;
naca-report-119; 1923
- (Author(s) Not
Available); List of
commercial aircraft belonging to the various French air navigation companies
as of August 31st, 1922; naca-tm-177; 1923
- Warner, Edward P
(Massachusetts Inst. of Tech); Airplane
speeds of the future; naca-tm-178; 1923
- Constantin, Louis; New lateral
stabilizing device for airplanes; naca-tm-179; 1923
- Delanghe, C; Marcel
Besson wing sections; naca-tm-180; 1923
- Hoff, Wilhelm; Soaring
flight and the Rhon contests; naca-tm-181; 1923
- Ziembinski, S (L.
Renault Automobile Company); Possible
improvements in gasoline engines; naca-tm-182; 1923
- Warner, Edward P; Soaring without
rising currents; naca-tm-183; February 1923
- (Author(s) Not
Available); Rules and
regulations of the 1922 Rhon Soaring Flight Contest; naca-tm-184; February
1923
- H. Von Sanden; Significance
of the expression C(sub L)(exp 3)/C(sub D)(exp 2); naca-tn-173; January,
1924
- Heinrich Kann; Airplanes
in horizontal curvilinear flight; naca-tn-174; January, 1924
- Wilhelm Molthan; Tests on a model
of the D.F.W. airplane T-29 of the Deutsche Flugzeug derke (German airplane
works); naca-tn-175; January, 1924
- E. Salkowski; Curvilinear
flight of airplanes; naca-tn-176; January, 1924
- Max M. Munk; Note
on the relative effect of the dihedral and the sweep back of airplane
wings; naca-tn-177; January, 1924
- C. Wieselsberger; Triplane
tests; naca-tn-178; February, 1924
- H. Hamburger; Practical
method for balancing airplane moments; naca-tn-179; February, 1924
- Robertson Mathews,
Arthur W. Gardiner; Increasing
the compression pressure in an engine by using a long intake pipe;
naca-tn-180; February, 1924
- H. Von Sanden; Interference
of multiplane wings having elliptical lift distribution; naca-tn-181;
February, 1924
- L. Prandtl; Induced
drag of multiplanes; naca-tn-182; February, 1924
- W. S. Diehl; Static
stability of seaplane floats and hulls; naca-tn-183; March, 1924
- Max M. Munk; Note
on vortices on their relation to the lift of airfoils; naca-tn-184; March,
1924
- Robertson Matthews,
Arthur W. Gardiner; The
influence of inlet air temperature and jacket water temperature on initiating
combustion in a high speed compression ignition engine; naca-tn-185;
March, 1924
- A. Proll; Testing
airplane fabrics; naca-tn-186; April, 1924
- Max M. Munk; The
induction factor used for computing the rolling moment due to the
ailerons; naca-tn-187; April, 1924
- R. Fuchs, L. Hopf; Longitudinal
oscillation of an airplane Part I : problem and method; naca-tn-188;
April, 1924
- N. S. Otey; Torsional
strength of nickel steel and duralumin tubing as affected by the ratio of
diameter to gage thickness; naca-tn-189; April, 1924
- Max M. Munk, Edward P.
Warner; Comparing the
performance of geometrically similar airplanes; naca-tn-190; April,
1924
- W. L. Lepage, J. T.
Nichols; The
effect of wind tunnel turbulence upon the forces measured on models;
naca-tn-191; May, 1924
- Max M. Munk; Note
on the pressure distribution over the hull of elongated airships with circular
cross section; naca-tn-192; May, 1924
- Paul B. King, Thomas
Carroll; High
altitude flying; naca-tn-193; May, 1924
- C. P. Burgess; A
method of determining the dimensions and horsepower of an airship for any
given performance; naca-tn-194; May, 1924
- Max M. Munk; On
the distribution of lift along the span of an airfoil with displaced
ailerons; naca-tn-195; June, 1924
- Max M. Munk; Remarks
on the pressure distribution over the surface of an ellipsoid, moving
translationally through a perfect fluid; naca-tn-196; June, 1924
- Max M. Munk; Some
tables of the factor of apparent additional mass; naca-tn-197; July,
1924
- F. W. Caldwell, N. S.
Clay; Micarta
propellers I : materials; naca-tn-198; August, 1924
- F. W. Caldwell, N. S.
Clay; Micarta
Propellers II : method of construction; naca-tn-199; August, 1924
- F. W. Caldwell, N. S.
Clay; Micarta
propellers III : general description of the design; naca-tn-200; August,
1924
- F. W. Caldwell, N. S.
Clay; Micarta
propellers IV : technical methods of design; naca-tn-201; Sep 1924
- Toussaint, Kerneis,
Girault; Experimental
investigation of the effect of an oscillating airstream (Katzmayr effect) on
the characteristics of airfoils; naca-tn-202; Sep 1924
- John E. Younger; A short method
of calculating torsional stresses in an airplane fuselage; naca-tn-203;
Sep 1924
- Frank Rizzo; A
study of static stability of airships; naca-tn-204; Sep 1924
- Val Cronstedt; The
logarithmic polar curve-it's theory and application to the predetermination of
airplane performance; naca-tn-205; Oct 1924
- Charles Ward Hall; Structural
weight of aircraft as affected by the system of design; naca-tn-206; Nov
1924
- Max M. Munk; The
simplifying assumptions, reducing the strict application of classical
hydrodynamics to practical aeronautical computations; naca-tn-207; Nov
1924
- John G. Lee; Tests
on duralumin columns for aircraft construction; naca-tn-208; Nov
1924
- Elliott G. Reid; Tests of
rotating cylinders; naca-tn-209; Dec 1924
- R. N. DuBois; The
testing of aviation engines; naca-tn-210; Dec 1924
- Buckingham, Edgar; Jet propulsion
for airplanes; naca-report-159; 1924
- Weaver, E R Pickering,
S F; An
airship slide rule; naca-report-160; 1924
- Bacon, David L; The distribution
of lift over wing tips and ailerons; naca-report-161; 1924
- Norton, F H Brown, W G;
Complete
study of longitudinal oscillation of a VE-7 airplane; naca-report-162;
1924
- Norton, F H Carroll, T;
The vertical,
longitudinal, and lateral accelerations experienced by an S. E. 5a airplane
while maneuvering; naca-report-163; 1924
- Bateman, H; The
inertial coefficients of an airship in a frictionless fluid;
naca-report-164; 1924
- Hersey, M D; Diaphragms
for aeronautic instruments; naca-report-165; 1924
- Zahm, A F; The
aerodynamic plane table; naca-report-166; 1924
- Norton, F H; The
measurement of the damping in roll on a JN4h in flight; naca-report-167;
1924
- Diehl, Walter S; The general
efficiency curve for air propellers; naca-report-168; 1924
- Hoot, H I; The
effect of airfoil thickness and plan form on lateral control;
naca-report-169; 1924
- Norton, F H; A
study of longitudinal dynamic stability in flight; naca-report-170;
1924
- Diehl, Walter S; Engine
performance and the determination of absolute ceiling; naca-report-171;
1924
- Wilson, Edwin B; Dynamic
stability as affected by the longitudinal moment of inertia;
naca-report-172; 1924
- Diehl, Walter S; Reliable
formulae for estimating airplane performance and the effects of changes in
weight, wing area, or power; naca-report-173; 1924
- Norton, F H; The
small angular oscillations of airplanes in steady flight; naca-report-174;
1924
- Munk, Max M; Analysis
of W. F. Durand's and E. P. Lesley's propeller tests; naca-report-175;
1924
- Stevens, F W; A
constant pressure bomb; naca-report-176; 1924
- Lesley, E P Woods, B M;
The effect of
slipstream obstructions on air propellers; naca-report-177; 1924
- Diehl, Walter S; Relative
efficiency of direct and geared drive propellers; naca-report-178;
1924
- Silsbee, F B; The
effect of electrode temperature on the sparking voltage of short spark
gaps; naca-report-179; 1924
- Newlin, J A Trayer, G
W; The
influence of the form of a wooden beam on its stiffness and strength I :
deflection of beams with special reference to shear deformations;
naca-report-180; 1924
- Newlin, J A Trayer, G
W; The
influence of the form of a wooden beam on its stiffness and strength II : form
factors of beams subjected to transverse loading only; naca-report-181;
1924
- (Author(s) Not
Available); Aerodynamic
characteristics of airfoils III : continuation of reports nos. 93 and 124;
naca-report-182; 1924
- Munk, Max M; The
analysis of free flight propeller tests and its application to design;
naca-report-183; 1924
- Munk, Max M; The
aerodynamic forces on airship hulls; naca-report-184; 1924
- Bacon, D L Reid, E G;
The
resistance of spheres in wind tunnels and in air; naca-report-185;
1924
- Fred E. Weick; Simplified
propeller design for low-powered airplanes; naca-tn-212; Jan 1925
- Robertson Mathews; Discharge
characteristics of a high speed fuel injection system; naca-tn-213; Feb
1925
- Shatswell Ober; Note on the
Katzmayr effect on airfoil drag; naca-tn-214; Feb 1925
- Edward P. Warner; The calculation
of wing float displacement in single-float seaplanes; naca-tn-215; Mar
1925
- Max M. Munk; The
velocity distribution caused by an airplane at the points of a vertical plane
containing the span; naca-tn-216; Mar 1925
- Max M. Munk; Note
on the air forces on a wing caused by pitching; naca-tn-217; Mar
1925
- Edward P. Warner; The estimation
of airplane performance from wind tunnel tests on conventional airplane
models; naca-tn-218; May 1925
- George J. Higgins; The comparison
of well-known and new wing sections tested in the variable density wind
tunnel; naca-tn-219; May 1925
- Edward P. Warner; The drift of an
aircraft guided towards it's destination by directional receiving of radio
signals transmitted from the ground; naca-tn-220; Jun 1925
- Max M. Munk; Model
tests on the economy and effectiveness of helicopter propellers;
naca-tn-221; Jan 1925
- R. G. Freeman; Air
flow investigation for location of angle of attack head on a JN4h
airplane; naca-tn-222; Aug 1925
- Fred E. Weick; Propeller
scale effect and body interference; naca-tn-225; Sep 1925
- Max M. Munk; Determination
and classification of the aerodynamic properties of wing sections;
naca-tn-227; Sep 1925
- Edward P. Warner; Wind tunnel
tests of fuselages and windshields; naca-tn-226; Sep 1925
- Frank Rizzo; The
Flettner rotor ship in the light of the Kutta-Joukowski theory and of
experimental results; naca-tn-228; Oct 1925
- J. E. Reid, Otto E.
Kirchner; An
altitude chamber for the study and calibration of aeronautical
instruments; naca-tn-229; Nov 1925
- E. E. Wilson; Aircraft
engine design; naca-tn-211; Jan 1925
- Diehl, Walter S; The application
of propeller test data to design and performance calculations;
naca-report-186; 1925
- Randolph, D W Silsbee,
F B; Flame
speed and spark intensity; naca-report-187; 1925
- Newlin, J A Trayer, G
W; The
influence of the form of a wooden beam on its stiffness and strength III :
stresses in wood members subjected to combined column and beam action;
naca-report-188; 1925
- Sparrow, Stanwood W; Relation of
fuel-air ratio to engine performance; naca-report-189; 1925
- Sparrow, Stanwood W; Correcting
horsepower measurements to a standard temperature; naca-report-190;
1925
- Munk, Max M; Elements
of the wing section theory and of the wing theory; naca-report-191;
1925
- Diehl, Walter S; Charts for
graphical estimation of airplane performance; naca-report-192; 1925
- Norton, F H; Pressure
distribution over the wings of an MB-3 airplane in flight;
naca-report-193; 1925
- Crowley, J W , Jr; Investigation of
slipstream velocity; naca-report-194; 1925
- Reid, Elliott G; Standardization
tests of NACA no. 1 wind tunnel; naca-report-195; 1925
- Durand, William F
Lesley, E P; Comparison of
model propeller tests with airfoil theory; naca-report-196; 1925
- Munk, Max M; A
new relation between the induced yawing moment and the rolling moment of an
airfoil in straight motion; naca-report-197; 1925
- Beij, K Hilding; Astronomical
methods in aerial navigation; naca-report-198; 1925
- Reid, Elliott G; Interference
tests on NACA pitot tubes; naca-report-199; 1925
- Scarborough, James B;
Some problems
on the lift and rolling moment of airplane wings; naca-report-200;
1925
- Reid, Elliott G; The effects of
shielding the tips of airfoils; naca-report-201; 1925
- Silsbee, F B; The
sparking voltage of spark plugs; naca-report-202; 1925
- Doolittle, J H; Accelerations in
flight; naca-report-203; 1925
- Burgess, C P; Forces
on airships in gusts; naca-report-204; 1925
- Sparrow, Stanwood W; The effect of
changes in compression ratio upon engine performance; naca-report-205;
1925
- Eaton, H N Buckingham,
C T; Nonmetallic
diaphragms for instruments; naca-report-206; 1925
- Briggs, L J Hull, G F
Dryden, H L; Aerodynamic
characteristics of airfoils at high speeds; naca-report-207; 1925
- Crowley, J W , Jr
Freeman, R G; Determination of
turning characteristics of an airship by means of a camera obscura;
naca-report-208; 1925
- Crowley, J W , Jr
Ronan, K M; Characteristics
of a single float seaplane during take-off; naca-report-209; 1925
- Green, Maurice W; Determination of
the lift and drag characteristics of an airplane in flight; naca-tn-223;
August 1925
- Fairbanks, Karl J; Pressure
distribution on the nose of an airship in circling flight; naca-tn-224;
August 1925
- Montgomery Knight; Wind tunnel
standardization disk drag; naca-tn-253; Dec 1926
- R. A. Castleman; The resistance
to the steady motion of small spheres in fluids; naca-tn-231; Feb
1926
- Stevens Bromley,
William H. Robison, Jr.; Lateral
failure of spars; naca-tn-232; Mar 1926
- W. F. Joachim; An
investigation of the characteristics of steel diaphragms for automatic
fuel-injection valves; naca-tn-234; Apr 1926
- Fred E. Weick; Propeller
design I : practical application of the blade element theory; naca-tn-235;
May 1926
- Fred E. Weick; Propeller
design: extension of test data on a family of model propellers by means of the
modified blade element theory II; naca-tn-236; May 1926
- Fred E. Weick; Propeller
design - a simple system based on model propeller test data III;
naca-tn-237; May 1926
- Fred E. Weick; Propeller
design IV : a simple method for determining the strength of propellers;
naca-tn-238; Jun 1926
- E. E. Wilson; Steam
power plants in aircraft; naca-tn-239; Jun 1926
- George J. Higgins; The NACA CYH
airfoil section; naca-tn-240; Jun 1926
- W. F. Joachin, Harold
W. Case; Tests of several
bearing materials lubricated by gasoline; naca-tn-241; Jul 1926
- George J. Higgins; The
characteristics of the NACA M-12 airfoil section; naca-tn-243; Aug
1926
- Fred E. Weick; Navy
propeller section characteristics as used in propeller design;
naca-tn-244; Aug 1926
- E. P. Lesley; Report
on tests of metal model propellers in combination with a model VE-7
airplane; naca-tn-245; Aug 1926
- E. P. Lesley; Test
of a model propeller with symmetrical blade sections; naca-tn-246; Sep
1926
- C. H. Havill; The
drag of airships; naca-tn-247; Jan 1926
- Clinton H. Havill; The drag of
airships : drag of bare hulls II; naca-tn-248; Oct 1926
- Eastman N. Jacobs; Effect of
protruding gasoline tanks upon the characteristics of an airfoil;
naca-tn-249; Oct 1926
- Paul E. Hemke; Influence
of the orifice on measured pressures; naca-tn-250; Nov 1926
- T. Carroll, R. E.
Mixon; The
effect of tube length upon the recorded pressures from a pair of static
orifices in a wing panel; naca-tn-251; Nov 1926
- James M. Shoemaker; Resistance of a
fifteen-centimeter disk; naca-tn-252; Dec 1926
- Max M. Munk; The
spacing of orifices for the measure of pressure distributions;
naca-tn-230; Jan 1926
- Kemper, Carlton; Improving the
performance of a compression ignition engine by directing flow of inlet
air; naca-tn-242; July 1926
- Tuckerman, L B; Inertia factors
of ellipsoids for use in airship design; naca-report-210; 1926
- Tuckerman, L B; Water model
tests for semirigid airships; naca-report-211; 1926
- Zahm, A F; Stability
equations for airship hulls; naca-report-212; 1926
- Ames, Joseph S; A resume of the
advances in theoretical aeronautics made by Max M. Munk; naca-report-213;
1926
- Warner, Edward P; Wing spar stress
charts and wing truss proportions; naca-report-214; 1926
- Zahm, A F Smith, R H
Louden, F A; Air forces,
moments and damping on model of fleet airship Shenandoah; naca-report-215;
1926
- Diehl, Walter S Lesley,
E P; The
reduction of airplane flight test data to standard atmosphere conditions;
naca-report-216; 1926
- Munk, Max M; Preliminary
wing model tests in the variable density wind tunnel of the National Advisory
Committee for Aeronautics; naca-report-217; 1926
- Diehl, Walter S; Standard
atmosphere - tables and data; naca-report-218; 1926
- Taylor, D W; Some
aspects of the comparison of model and full-scale tests; naca-report-219;
1926
- Durand, W F Lesley, E
P; Comparison
of tests on air propellers in flight with wind tunnel model tests on similar
forms; naca-report-220; 1926
- Munk, Max M Miller,
Elton W; Model tests with
a systematic series of 27 wing sections at full Reynolds number;
naca-report-221; 1926
- Miller, Harold E
Beardsley, Edward G; Spray
penetration with a simple fuel injection nozzle; naca-report-222;
1926
- Crowley, J W , Jr
Defrance, S J; Pressure
distribution on the C-7 airship; naca-report-223; 1926
- Joachim, W F; An
investigation of the coefficient of discharge of liquids through small round
orifices; naca-report-224; 1926
- Munk, Max M (Bureau Of
Aeronautics (Navy), Washington, DC) Diehl, Walter S; The
air forces on a model of the sperry messenger airplane without propeller;
naca-report-225; 1926
- Crowley, J W Ronan, K
M; Characteristics
of a boat type seaplane during take-off; naca-report-226; 1926
- Diehl, Walter S; A study of the
effect of a diving start on airplane speed; naca-report-228; 1926
- Reid, Elliott G; Pressure
distribution over thick tapered airfoils, NACA 81, USA 27c modified and USA
35; naca-report-229; 1926
- Ware, Marsden; Description
and laboratory tests of a Roots type aircraft engine supercharger;
naca-report-230; 1926
- Dryden, H L Heald, R H;
Investigation
of turbulence in wind tunnels by a study of the flow about cylinders;
naca-report-231; 1926
- Sparrow, Stanwood W; Fuels for
high-compression engines; naca-report-232; 1926
- Munk, Max M Miller,
Elton W; The
variable density wind tunnel of the National Advisory Committee for
Aeronautics; naca-report-227; 1926
- Donald A. Hall; Technical
preparation of the airplane - Spirit of St. Louis.; naca-tn-257; Jul
1927
- Elliott G. Reid, Thomas
Carroll; A
warning concerning the take-off with heavy load; naca-tn-258; Jul
1927
- E. H. Dix, Jr.; A L C L A D :
new corrosion resistant aluminum product; naca-tn-259; Aug 1927
- Fred E. Weick; Study
of open jet wind tunnel cones; naca-tn-260; Aug 1927
- M. F. Schoeffel; The installation
and correction of compasses in airplanes; naca-tn-262; Aug 1927
- Roy G. Miller; A
load factor formula; naca-tn-263; Aug 1927
- George J. Higgins; Tests of the
N.P.L. airship models in the variable density wind tunnel; naca-tn-264;
Sep 1927
- M. W. Green; Measurement
of the moments of inertia of full scale airplanes; naca-tn-265; Jan
1927
- Elliott G. Reid; Airfoil lift
with changing angle of attack; naca-tn-266; Sep 1927
- R. V. Rhode; Pressure
distribution on wing ribs of the VE-7 and TS airplanes in flight;
naca-tn-267; Oct 1927
- Max Scherberg, R. V.
Rhode; Mass
distribution and performance of free flight models; naca-tn-268; Oct
1927
- Richard M. Mock; The distribution
of loads between the wings of a biplane having decalage; naca-tn-269; Nov
1927
- George J. Higgins; The
characteristics of the N.A.C.A 97, Clark Y, and N.A.C.A. M6 airfoils with
particular reference to the angle of attack; naca-tn-270; Dec 1927
- Frank Rizzo; Precision
of wing sections and consequent aerodynamic effects; naca-tn-255; Jan
1927
- George J. Higgins; Wall
interference in closed type wind tunnels; naca-tn-256; Mar 1927
- R. H. Smith; Method
of correcting wind tunnel data for omitted parts of airplane models;
naca-tn-254; Jan 1927
- Munk, Max M Miller,
Elton W; The
aerodynamic characteristics of seven frequently used wing sections at full
Reynolds number; naca-report-233; 1927
- Diehl, Walter S; Three methods of
calculating range and endurance of airplanes; naca-report-234; 1927
- Durand, W F; Interaction
between air propellers and airplane structures; naca-report-235;
1927
- Diehl, Walter S; Tests on
airplane fuselages, floats and hulls; naca-report-236; 1927
- Durand, W F; Tests
on thirteen navy type model propellers; naca-report-237; 1927
- Diehl, Walter S; The effect of
flight path inclination on airplane velocity; naca-report-238; 1927
- Paton, C R Kemper,
Carlton; Power output and
air requirements of a two-stroke cycle engine for aeronautical use;
naca-report-239; 1927
- Brode, R B Randolph, D
W Silsbee, F B; Electrical
characteristics of spark generators for automotive ignition;
naca-report-241; 1927
- Crowley, John W , Jr
Ronan, K M; Characteristics
of a twin-float seaplane during take-off; naca-report-242; 1927
- Gardiner, Arthur W; A preliminary
study of fuel injection and compression ignition as applied to an aircraft
engine cylinder; naca-report-243; 1927
- (Author(s) Not
Available); Aerodynamic
characteristics of airfoils IV : continuation of reports nos. 93, 124, and
182; naca-report-244; 1927
- Gregg, W R; Meteorological
conditions along airways; naca-report-245; 1927
- Zahm, A F; Pressure
of air on coming to rest from various speeds; naca-report-247; 1927
- Boyer, J A; The
corrosion of magnesium and of the magnesium aluminum alloys containing
manganese; naca-report-248; 1927
- Carroll, Thomas; A comparison of
the take-off and landing characteristics of a number of service airplane;
naca-report-249; 1927
- Ware, Marsden; Description
of the NACA universal test engine and some test results; naca-report-250;
1927
- Warner, Edward P Short,
Mac; Approximations
for column effect in airplane wing spars; naca-report-251; 1927
- Gove, W D Green, M W;
The direct
measurement of engine power on an airplane in flight with a hub type
dynamometer; naca-report-252; 1927
- Zahm, A F; Flow
and drag formulas for simple quadrics; naca-report-253; 1927
- Fairbanks, A J; Distribution of
pressure over model of the upper wing and aileron of a Fokker D-VII
airplane; naca-report-254; 1927
- Briggs, L J Dryden, H
L; Pressure
distribution over airfoils at high speeds; naca-report-255; 1927
- Munk, Max M; The
air forces on a systematic series of biplane and triplane cellule models;
naca-report-256; 1927
- Brombacher, W G; Tables for
calibrating altimeters and computing altitudes based on the standard
atmosphere; naca-report-246; 1927
- Henrickson, H B (Bureau
of Standards); Tension
experiments on diaphragm metals; naca-tn-261; August 1927
- ; Nomenclature
for aeronautics; naca-report-240; 1927
- Fred E. Weick; Full
scale drag tests on various parts of Sperry Messenger airplane;
naca-tn-271; Jan 1928
- A. M. Heim; Special
propeller protractor; naca-tn-272; Jan 1928
- Thomas Carroll; The effect on
performance of a cutaway center section; naca-tn-273; Jan 1928
- Fred E. Weick; The
effect of the Sperry Messenger fuselage on the air flow at the propeller
plane; naca-tn-274; Jan 1928
- Fred E. Weick; Determination
of propeller deflection by means of static load tests on models;
naca-tn-275; Jan 1928
- Clinton H. Havill; Helium
tables; naca-tn-276; Jan 1928
- R. V. Rhode; Pressure
distribution on wing ribs of the VE-7 and TS airplanes in flight Part II:
pull-ups; naca-tn-277; Jan 1928
- A. F. Zahm; An
automatic speed control for wind tunnels; naca-tn-278; Feb 1928
- George L. DeFoe; Resistance of
streamline wires; naca-tn-279; Mar 1928
- Donald H. Wood; Drag of exposed
fittings and surface irregularities on airplane fuselages; naca-tn-280;
Mar 1928
- Fred E. Weick; A
comparison of propeller and centrifugal fans for circulating the air in a wind
tunnel; naca-tn-281; Mar 1928
- Henry S. Rawdon; Corrosion
embrittlement of duralumin I : practical aspects of the problem;
naca-tn-282; Apr 1928
- Henry S. Rawdon; Corrosion
embrittlement of duralumin II : accelerated corrosion tests and the behavior
of high-strength aluminum alloys of different compositions; naca-tn-283;
Apr 1928
- Henry S. Rawdon; Corrosion
embrittlement of duralumin III : effect of the previous treatment of sheet
material on the susceptibility to this type of corrosion; naca-tn-284; Apr
1928
- Henry S. Rawdon; Corrosion
embrittlement of duralumin IV : the use of protective coatings;
naca-tn-285; Apr 1928
- Thomas Carroll; A dangerous
seaplane landing condition; naca-tn-287; May 1928
- H. C. Richardson; The reaction on
a float bottom when making contact with water at high speeds; naca-tn-288;
May 1928
- James M. Shoemaker; Preliminary
biplane tests in the variable density wind tunnel; naca-tn-289; Jun
1928
- W. B. Miller; Welding
of high chromium steels; naca-tn-290; Jun 1928
- T. R. Truax; Gluing
practice at aircraft manufacturing plants; naca-tn-291; Jul 1928
- Fred E. Weick; The
drag of a J-5 radial air-cooled engine; naca-tn-292; Jul 1928
- Carroll, Thomas Mcavoy,
Wm H; The
formation of ice upon exposed parts of an airplane in flight; naca-tn-293;
July 1928
- Carl J. Wenzinger,
Thomas A. Harris; Wind
tunnel force tests in wing systems through large angles of attack;
naca-tn-294; Aug 1928
- Paul V. Dronin, Earl I.
Ramsden, George J. Higgins; The
effect of tip shields on a horizontal tail surface; naca-tn-295; Aug
1928
- G. W. Trayer; Bearing
strength of wood under steel aircraft bolts and washers and other factors
influencing fitting design; naca-tn-296; Oct 1928
- Montgomery Knight,
Millard J. Bamber; Preliminary
report on the flat-top lift curve as a factor in control at low speed;
naca-tn-297; Sep 1928
- Chester W. Hicks,
Charles S. Moore; The
determination of several spray characteristics of a high-speed oil engine
injection system with an oscilloscope; naca-tn-298; Sep 1928
- Thomas Carroll, Wm. H.
McAvoy; The
variation in pressures in the cockpit fan airplane in flight; naca-tn-300;
Nov 1928
- Fred E. Weick; Drag
and cooling with various forms of cowling for a Whirlwind engine in a cabin
fuselage; naca-tn-301; Nov 1928
- Reid, E G Bamber, M J;
Preliminary
investigation on boundary layer control by means of suction and pressure with
the U.S.A. 27 airfoil; naca-tn-286; May 1928
- Gough, Melvin N; The effect of
fillets between wings and fuselage on the drag and propulsive efficiency of an
airplane; naca-tn-299; October 1928
- Crowley, J W , Jr; Pressure
distribution over a wing and tail rib of a VE-7 and of a TS airplane in
flight; naca-report-257; 1928
- Beardsley, E G; Some factors
affecting the reproducibility of penetration and the cut-off of oil sprays for
fuel-injection engines; naca-report-258; 1928
- Jacobs, Eastman N; Characteristics
of propeller sections tested in the variable density wind tunnel;
naca-report-259; 1928
- Higgins, George J
Jacobs, Eastman N; The
effect of a flap and ailerons on the N.A.C.A. M-6 airfoil section;
naca-report-260; 1928
- Smith, R H; Resistance
and cooling power of various radiators; naca-report-261; 1928
- Sparrow, S W Thorne, M
A; Friction
of aviation engines; naca-report-262; 1928
- Gardiner, Arthur W
Reid, Elliott G; Preliminary
flight tests of the N.A.C.A. Roots type aircraft engine supercharger;
naca-report-263; 1928
- Bear, R M; Differential
pressures on a Pitot-Venturi and a Pitot-static nozzle over 360 degrees pitch
and yaw; naca-report-264; 1928
- Reid, Elliott G; A full-scale
investigation of ground effect; naca-report-265; 1928
- Smith, R H; Air
force and moment for N-20 wing with certain cut-outs; naca-report-266;
1928
- Hemke, Paul E; Drag
of wings with end plates; naca-report-267; 1928
- Joachim, W F Beardsley,
E G; Factors
in the design of centrifugal type injection valves for oil engines;
naca-report-268; 1928
- Shoemaker, James M; Air force tests
of sperry messenger model with six sets of wings; naca-report-269;
1928
- Hemke, Paul E; The
measurement of pressure through tubes in pressure distribution tests;
naca-report-270; 1928
- Fairbanks, A J; Pressure
distribution tests on PW-9 wing models showing effects of biplane
interference; naca-report-271; 1928
- Gardiner, Arthur W
Whedon, William E; The
relative performance obtained with several methods of control of an
overcompressed engine using gasoline; naca-report-272; 1928
- Knight, Montgomery; Wind tunnel
tests on autorotation and the "flat spin."; naca-report-273; 1928
- Beardsley, Edward G; The N.A.C.A.
photographic apparatus for studying fuel sprays from oil engine injection
valves and test results from several researches; naca-report-274;
1928
- Higgins, George J; The effect of
the walls in closed type wind tunnels; naca-report-275; 1928
- Marvin, Charles F , Jr;
Combustion
time in the engine cylinder and its effect on engine performance;
naca-report-276; 1928
- Gardiner, Arthur W
Schey, Oscar W; The
comparative performance of an aviation engine at normal and high inlet air
temperatures; naca-report-277; 1928
- Smith, R H; Lift,
drag, and elevator hinge moments of Handley Page control surfaces;
naca-report-278; 1928
- Higgins, George J
(Bureau Of Aeronautics (Navy), Washington, DC) Defoe, George L Diehl, W S; Tests on models
of three British airplanes in the variable density wind tunnel;
naca-report-279; 1928
- Stevens, F W; The
gaseous explosive reaction : the effect of inert gases; naca-report-280;
1928
- Joachim, W F Beardsley,
Edward G; The
effects of fuel and cylinder gas densities on the characteristics of fuel
sprays for oil engines; naca-report-281; 1928
- Joachim, William F
Kemper, Carlton; Performance
of several combustion chambers designed for aircraft oil engines;
naca-report-282; 1928
- E. P. Lesley, E. G.
Reid; A new
method for the prediction of airplane performance; naca-tn-302; Feb
1929
- C. S. Fliedner; Condensed data
on the aircraft engines of the world; naca-tn-303; Apr 1929
- Henry S. Rawdon; Corrosion
embrittlement of duralumin V : results of weather-exposure tests;
naca-tn-304; Feb 1929
- Henry S. Rawdon; Corrosion
embrittlement of duralumin VI : the effect of corrosion accompanied by stress
on the tensile properties of sheet duralumin; naca-tn-305;
- Orrin E. Ross; Curves
showing column strength of steel and duralumin tubing; naca-tn-306; May
1929
- L. B. Tuckerman, S. N.
Petrenko, C. D. Johnson; Strength
of tubing under combined axial and transverse loading; naca-tn-307; Jun
1929
- Eastman N. Jacobs; Pressure
distribution on a slotted R.A.F. 31 airfoil in the variable density wind
tunnel; naca-tn-308; Jun 1929
- Donald B. Brooks; Correcting
engine tests for humidity; naca-tn-309; Jun 1929
- Montgomery Knight,
Richard Noyes; Wind
tunnel pressure distribution tests on a series of biplane wing models;
naca-tn-310; Jul 1929
- Thomas Carroll, Smith
J. Defrance; The use of wheel
brakes on airplanes; naca-tn-311; Jul 1929
- Eastman N. Jacobs; Sphere drag
tests in the variable density wind tunnel; naca-tn-312; Aug 1929
- Thomas Carroll, William
H. McAvoy; The formation of
ice upon airplanes in flight; naca-tn-313; Aug 1929
- Thomas Carroll, William
H. McAvoy; Spiral tendency
in blind flying; naca-tn-314; Aug 1929
- Mayo D. Hersey; Viscosity of
diesel engine fuel oil under pressure; naca-tn-315; Sep 1929
- Montgomery Knight,
Millard J. Bamber; Wind
tunnel tests on a model of a monoplane wing with floating ailerons;
naca-tn-316; Sep 1929
- Fred E. Weick; Tests
of four racing type airfoils in the twenty-foot propeller research tunnel;
naca-tn-317; Sep 1929
- Fred E. Weick; Full
scale investigation of the drag of a wing radiator; naca-tn-318; Sep
1929
- Shatswell Ober; Some experiments
on autorotation of an airfoil; naca-tn-319; Sep 1929
- Th. Von Karman; The impact on
seaplane floats during landing; naca-tn-321; Oct 1929
- Fred E. Weick, Donald
H. Wood; The
effect of the wings of single engine airplanes on propulsive efficiency as
shown by full scale wind tunnel tests; naca-tn-322; Oct 1929
- Montgomery Knight,
Millard J. Bamber; Wind
tunnel tests on airfoil boundary control using a backward opening slot;
naca-tn-323; Oct 1929
- Millard J. Bamber; Wind tunnel
tests on an airfoil equipped with a split flap and a slot; naca-tn-324;
Oct 1929
- Montgomery Knight,
Richard W. Noyes; Wind
tunnel pressure distribution tests on a series of biplane wing models Part II
: effects of changes in decalage, dihedral, sweepback and overhang;
naca-tn-325; Oct 1929
- Carl J. Wenzinger,
Oscar Loeser; Wind tunnel
pressure distribution tests on an airfoil with trailing edge flap;
naca-tn-326; Oct 1929
- Shatswell Ober; Some studies on
the aerodynamic effect of the gap between airplane wings and fuselages;
naca-tn-327; Nov 1929
- Oscar W. Schey; The effect of
fuel consumption on cylinder temperatures and performance of a cowled Wright
J-5 engine; naca-tn-328; Nov 1929
- A. M. Rothrock, E. G.
Beardsley; Some effects of
air flow on the penetration and distribution of oil sprays; naca-tn-329;
Dec 1929
- Montgomery Knight,
Richard W. Noyes; Wind
tunnel pressure distribution tests on a series of biplane wing models Part III
: effects of charges in various combinations of stagger, gap, sweepback, and
decalage; naca-tn-330; Dec 1929
- Jacobs, Eastman N; The drag and
interference of a nacelle in the presence of a wing; naca-tn-320; October
1929
- Ware, Marsden Schey,
Oscar W; A
preliminary investigation of supercharging an air-cooled engine in flight;
naca-report-283; 1929
- Ware, Marsden Wilson,
Ernest E; The
comparative performance of Roots type aircraft engine superchargers as
affected by change in impeller speed and displacement; naca-report-284;
1929
- Zahm, A F Bear, R M; A study of wing
flutter; naca-report-285; 1929
- (Author(s) Not
Available); Aerodynamic
characteristics of airfoils V : continuation of reports nos. 93, 124, 182, and
244; naca-report-286; 1929
- Zahm, A F; Theories
of flow similitude; naca-report-287; 1929
- Knight, Montgomery
Loeser, Oscar, Jr; Pressure
distribution over a rectangular monoplane wing model up to 90 degree angle of
attack; naca-report-288; 1929
- Zahm, A F Smith, R H
Louden, F A; Forces on
elliptic cylinders in uniform air stream; naca-report-289; 1929
- Thompson, F L; Water-pressure
distribution on seaplane float; naca-report-290; 1929
- Zahm, A F Smith, R H
Louden, F A; Drag of C-class
airship hulls of various fineness ratios; naca-report-291; 1929
- Diehl, Walter S; Two practical
methods for the calculation of the horizontal tail area necessary for a
statically stable airplane; naca-report-293; 1929
- Hicks, Chester W; The measurement
of maximum cylinder pressures; naca-report-294; 1929
- Gove, W D; The
variation in engine power with altitude determined from measurements in flight
with a hub dynamometer; naca-report-295; 1929
- Loeser, Oscar E , Jr;
Pressure
distribution tests on PW-9 wing models from -18 degree through 90 degree angle
of attack; naca-report-296; 1929
- Diehl, Walter S; Reduction of
observed airplane performance to standard conditions; naca-report-297;
1929
- Heald, R H Strother, D
H; Effect of
variation of chord and span of ailerons on rolling and yawing moments in level
flight; naca-report-298; 1929
- Keulegan, G H; Investigation
of damping liquids for aircraft instruments; naca-report-299; 1929
- Weick, Fred E Wood,
Donald H; The
twenty-foot propeller research tunnel of the National Advisory Committee for
Aeronautics; naca-report-300; 1929
- Weick, Fred E; Full
scale tests of wood propellers on a VE-7 airplane in the propeller research
tunnel; naca-report-301; 1929
- Weick, Fred E; Full
scale tests on a thin metal propeller at various tip speeds;
naca-report-302; 1929
- Schey, Oscar W Wilson,
Ernest E; An
investigation of the use of discharge valves and an intake control for
improving the performance of N.A.C.A. Roots type supercharger;
naca-report-303; 1929
- Crowley, J W , Jr
Green, M W; An investigation
of the aerodynamic characteristics of an airplane equipped with several
different sets of wings; naca-report-304; 1929
- Stevens, F W; The
gaseous explosive reaction : a study of the kinetics of composite fuels;
naca-report-305; 1929
- Weick, Fred E; Full-scale
wind-tunnel tests of a series of metal propellers on a VE-7 airplane;
naca-report-306; 1929
- Rhode, R V; The
pressure distribution over the horizontal and vertical tail surfaces of the
F6C-4 pursuit airplane in violent maneuvers; naca-report-307; 1929
- Crowley, J W , Jr
Mixson, R E; Characteristics
of five propellers in flight; naca-report-292; 1929
- (Author(s) Not
Available); Aircraft
accidents.method of analysis; naca-report-308; 1929
- G. Fayette Taylor, A.
Rehbock; Rate
of heat transfer from finned metal surfaces; naca-tn-331; Jan 1930
- A. M. Rothrock; Injection labs
in a common-rail fuel injection system; naca-tn-332; Feb 1930
- E. P. Lesley; Test
of an adjustable pitch model propeller at four blade settings;
naca-tn-333; Feb 1930
- Oscar W. Schey, Ernest
Johnson, Melvin N. Gough; Comparative
performance obtained with XF7C-1 airplane using several different engine
cowlings; naca-tn-334; Feb 1930
- H. J. McNicholas, F.
Hedrick; The
structure and properties of parachute cloths; naca-tn-335; Mar 1930
- Montgomery Knight, Carl
J. Wenzinger; The effect of
wing tip floating ailerons on the autorotation of a monoplane wing model;
naca-tn-336; Mar 1930
- Richard V. Rhode; Pressure
distribution on the tail surfaces of a PW-9 pursuit airplane in flight;
naca-tn-337; Apr 1930
- A. G. Gelalles; Some effects of
air and fuel oil temperatures on spray penetration and dispersion;
naca-tn-338; May 1930
- Montgomery Knight,
William C. Clay; Refrigerated
wind tunnel tests on surface coatings for preventing ice formation;
naca-tn-339; May 1930
- William H. Hernstein,
Jr.; Full
scale drag tests on various parts of Fairchild (FC-2W2) cabin monoplane;
naca-tn-340; May 1930
- Robert M. Pinkerton; Calibration and
lag of a Friez type cup anemometer; naca-tn-341; Jun 1930
- Horace Knerr; Identification
of aircraft by Rockwell test; naca-tn-342; Jun 1930
- George Michael Smith;
Strength in
shear of the thin curved sheets of Alclad; naca-tn-343; Jun 1930
- J. A. Spanogle, H. H.
Foster; Performance of a
high-speed compression-ignition engine using multiple orifice fuel injection
nozzles; naca-tn-344; Jun 1930
- William C. Geer, Merit
Scott; The
prevention of the ice hazard on airplanes; naca-tn-345; Jul 1930
- Richard V. Rhode,
Eugene E. Lundquist; Pressure
distribution over a Douglas wing tip on a biplane in flight; naca-tn-347;
Aug 1930
- John H. Collins, Jr.;
Alterations
and tests of the - Farnboro - engine indicator; naca-tn-348; Sep
1930
- Kenneth F. Ridley; An investigation
of airplane landing speeds; naca-tn-349; Sep 1930
- W. H. Mutchler, R. W.
Buzzard; Methods for the
identification of aircraft tubing of plain carbon steel and
chromium-molybdenum steel; naca-tn-350; Oct 1930
- M. P. Miller; An
accurate method of measuring the moments of inertia of airplanes;
naca-tn-351; Oct 1930
- A. G. Gellales; Effect of
orifice length-diameter ratio on spray characteristics; naca-tn-352; Oct
1930
- Robert M. Pinkerton; Analytical
determination of the load on a trailing edge flap; naca-tn-353; Oct
1930
- John F. Parsons, Jarvis
A. Wallen; An
investigation of the phenomenon of separation in the air flow around simple
quadric cylinders; naca-tn-354; Nov 1930
- A. M. Rothrock, D. W.
Lee; Some
characteristics of fuel sprays from open nozzles; naca-tn-356; Nov
1930
- Ralph W. Mossman,
Russell G. Robinson; Bending
tests of metal monocoque fuselage construction; naca-tn-357; Nov
1930
- Eastman N. Jacobs, Ira
H. Abbott; Experiments with
a model water tunnel; naca-tn-358; Dec 1930
- J. A. Spanogle, John H.
Collins, Jr.; A balanced
diaphragm type of maximum cylinder pressure indicator; naca-tn-359; Dec
1930
- Knight, Montgomery
Noyes, Richard W; Span
load distribution on two monoplanes wing models as affected by twist and
sweepback; naca-tn-346; July 1930
- Gough, Melvin N; Effect of the
angular position of the section of a ring cowling on the high speed of an
XF7C-1 airplane; naca-tn-355; November 1930
- Wheatley, John B; Simplified
aerodynamic analysis of the cyclogiro rotating wing system; naca-tn-467;
August 1930
- Diehl, Walter S; Joint report on
standardization tests on N.P.L. R.A.F 15 airfoil model; naca-report-309;
1930
- Brombacher, W G
Cordero, F; Pressure element
of constant logarithmic stiffness for temperature compensated altimeter;
naca-report-310; 1930
- Smith, R H; Aerodynamic
theory and test of strut forms. Part I; naca-report-311; 1930
- Weick, Fred E; Drag
and cooling with various forms of cowling for a "whirlwind" radial air-cooled
engine I; naca-report-313; 1930
- Weick, Fred E; Drag
and cooling with various forms of cowling for a "Whirlwind" radial air-cooled
engine II; naca-report-314; 1930
- Zahm, A F Louden, F A;
Tables for
pressure of air on coming to rest from various speeds; naca-report-316;
1930
- Knight, Montgomery
Wenzinger, Carl J; Wind-tunnel
tests on a series of wing models through a large angle of attack range. Part I
: force tests; naca-report-317; 1930
- De France, S J (Bureau
Of Aeronautics (Navy), Washington, DC) Burgess, C P; Speed
and deceleration trials of U.S.S. Los Angeles; naca-report-318;
1930
- Brigg, L J Dryden, H L;
Aerodynamic
characteristics of twenty-four airfoils at high speeds; naca-report-319;
1930
- Dryden, H L Kuethe, A
M; The
measurement of fluctuations of air speed by the hot-wire anemometer;
naca-report-320; 1930
- Joachim, William F
Rothrock, A M; Fuel
vapor pressures and the relation of vapor pressure to the preparation of fuel
for combustion in fuel injection engines; naca-report-321; 1930
- Jacobs, Eastman N; Investigation of
air flow in open-throat wind tunnels; naca-report-322; 1930
- Zahm, A F; Flow
and force equations for a body revolving in a fluid; naca-report-323;
1930
- De France, S J; Flight tests on
U.S.S. Los Angeles. Part I : full scale pressure distribution
investigation; naca-report-324; 1930
- Burgess, C P; Flight
tests on U.S.S. Los Angeles. Part II : stress and strength determination;
naca-report-325; 1930
- Lesley, E P Reid,
Elliott G; Tests of five
metal model propellers with various pitch distributions in a free wind stream
and in combination with model VE-7 fuselage; naca-report-326; 1930
- Schey, O W Gove, W D;
The effect of
supercharger capacity on engine and airplane performance; naca-report-327;
1930
- Thompson, F L; Water
pressure distribution on a twin-float seaplane; naca-report-328;
1930
- Burgess, C P; The
torsional strength of wings; naca-report-329; 1930
- Gelalles, A G Rothrock,
A M; Experimental and
analytical determination of the motion of hydraulically operated valve stems
in oil engine injection systems; naca-report-330; 1930
- Louden, F A; Collection
of wind-tunnel data on commonly used wing sections; naca-report-331;
1930
- Schey, Oscar W
Biermann, Arnold E; The
effect of cowling on cylinder temperatures and performance of a Wright J-5
engine; naca-report-332; 1930
- Thompson, F L; Full-scale
turning characteristics of the U.S.S. Los Angeles; naca-report-333;
1930
- Trayer, George W March,
H W; The
torsion of members having sections common in aircraft construction;
naca-report-334; 1930
- Smith, R H; Aerodynamic
theory and tests of strut forms. Part II; naca-report-335; 1930
- Wood, Donald H; Tests of large
airfoils in the propeller research tunnel, including two with corrugated
surfaces; naca-report-336; 1930
- Higgins, George J; The prediction
of airfoil characteristics; naca-report-312; 1930
- (Author(s) Not
Available); Aerodynamic
characteristics of airfoils VI : continuation of reports nos. 93, 124, 182,
244, and 286; naca-report-315; 1930
- F. L. Thompson, P. H.
Keister; Lift
and drag characteristics of a cabin monoplane; naca-tn-362; Jan
1931
- Fred E. Weick; The
behavior of conventional airplanes in situations thought to lead to most
crashes; naca-tn-363; Feb 1931
- John Stack; Tests
in the variable density wind tunnel to investigate the effects of scale and
turbulence on airfoil characteristics; naca-tn-364; Feb 1931
- Kenneth E. Ward; Interference
effects and drag of struts on a monoplane wing; naca-tn-365; Feb
1931
- John B. Wheatley; Torsion in box
wings; naca-tn-366; Feb 1931
- Raymond F. Anderson; The aerodynamic
characteristics of three tapered airfoils tested in the variable density wind
tunnel; naca-tn-367; Feb 1931
- Melvin N. Gough; The variation in
pressure in the cabin of an airplane in flight; naca-tn-368; Mar
1931
- A. G. Gelalles, E. E.
March; Effect
of orifice length-diameter ratio on the coefficient of discharge of
fuel-injection nozzles; naca-tn-369; Mar 1931
- Richard V. Rhodes,
Eugene E. Lundquist; Strength
tests on paper cylinder in compression, bending and shear; naca-tn-370;
Apr 1931
- J. A. Spanogle, G. H.
Hemmeter; Development of
an impinging-jet fuel-injection valve nozzle; naca-tn-372; Apr 1931
- Harold C. Gerrish, Fred
Voss; Investigation of
the discharge rate of a fuel-injection system; naca-tn-373; Apr
1931
- Richard V. Rhode,
Eugene E. Lundquist; Preliminary
study of applied load factors in bumpy air; naca-tn-374; Apr 1931
- Marvel P. Miller,
Hartley A. Soule; Moments
of inertia of several airplanes; naca-tn-375; May 1931
- A. M. Rothrock; Effect of high
air velocities on the distribution and penetration of a fuel spray;
naca-tn-376; May 1931
- Richard W. Noyes; An integrating
manometer for use in wind tunnel pressure distribution measurements;
naca-tn-377; May 1931
- E. C. Hartmann; Comparison of
weights of 17ST and steel tubular structural members used in aircraft
construction; naca-tn-378; May 1931
- Richard V. Rhode,
Eugene E. Lungquist; The
pressure distribution over a semicircular wing tip on an airplane in
flight; naca-tn-379; May 1931
- Fayette C. Taylor; A suggested
method for measuring turbulence; naca-tn-380; Jun 1931
- H. W. Russell, W. A.
Welcker, Jr.; Endurance and
other properties at low temperatures of some alloys for aircraft use;
naca-tn-381; Jun 1931
- J. A. Spanogle, H. H.
Foster; Basic
requirements of fuel-injection nozzles for quiescent combustion chambers;
naca-tn-382; Jun 1931
- Andrew E. Swickard; Metal-truss wing
spars; naca-tn-383; Jul 1931
- A. M. Rothrock, E. T.
Marsh; The
effect of injection-valve opening pressure; naca-tn-384; Jul 1931
- Eastman N. Jacobs; Tests of six
symmetrical airfoils in the variable density wind tunnel; naca-tn-385; Jul
1931
- Eugene E. Lundquist,
Richard V. Rhode; The
pressure distribution over a modified elliptical wing tip on a biplane in
flight; naca-tn-387; Aug 1931
- A. M. Rothrock; The N.A.C.A.
apparatus for studying the formation and combustion of fuel sprays and the
results from preliminary tests; naca-tn-389; Sep 1931
- Oscar W. Schey, Alfred
W. Young; A
method for reducing the temperature of exhaust manifolds; naca-tn-390; Sep
1931
- Eastman N. Jacobs,
Robert M. Pinkerton; Tests
of N.A.C.A. airfoils in the variable-density wind tunnel Series 43 and 63;
naca-tn-391; Sep 1931
- Eastman N. Jacobs,
Robert M. Pinkerton; Tests
of N.A.C.A. airfoils in the variable-density wind tunnel Series 45 and 65;
naca-tn-392; Sep 1931
- Wm. D. Appel, R. K.
Worner; An
investigation of cotton for parachute cloth; naca-tn-393; Sep 1931
- Theodore Theodorsen,
William C. Clay; The
prevention of ice formation on gasoline tank vents; naca-tn-394; Oct
1931
- A. M. Rothrock, E. T.
Marsh; Penetration and
duration of fuel sprays from a pump injection system; naca-tn-395; Oct
1931
- J. A. Spanogle, C. S.
Moore; Performance of a
compression-ignition engine with a precombustion chamber having high-velocity
air flow; naca-tn-396; Oct 1931
- Raymond F. Anderson; The aerodynamic
characteristics of six commonly used Airfoils over a large range of positive
and negative angles of attack; naca-tn-397; Nov 1931
- Hartley A. Soule; The effect of
slots and flaps on the lift and drag of the McDonnell Airplanes determined in
flight; naca-tn-398; Nov 1931
- A. M. Rothrock, C. D.
Waldron; Some
characteristics of fuel sprays at low-injection pressures; naca-tn-399;
Nov 1931
- R. W. Buzzard, W. H.
Mutchler; Advantages of
oxide films as bases for aluminum pigmented surface coatings for aluminum
alloys; naca-tn-400; Nov 1931
- Eastman N. Jacobs,
Robert M. Pinkerton; Tests
of N.A.C.A. airfoils in the variable density wind tunnel Series 44 and 64;
naca-tn-401; Dec 1931
- J. A. Spanogle, E. G.
Whitney; The
effectiveness of a double-stem injection valve in controlling combustion in a
compression-ignition engine; naca-tn-402; Dec 1931
- Kenneth E. Ward; The interference
effects on an airfoil of a flat plate at mid-span position; naca-tn-403;
Dec 1931
- Richard V. Rhode,
Eugene E. Lundquist; The
pressure distribution over a square wing tip on a biplane in flight;
naca-tn-360; Jan 1931
- Stevens, F W; The
gaseous explosive reaction at constant pressure : the reaction order and
reaction rate; naca-report-337; 1931
- Weick, Fred E; The
effect of reduction gearing on propeller-body interference as shown by
full-scale wind-tunnel tests; naca-report-338; 1931
- Weick, Fred E; Full-scale
wind-tunnel tests with a series of propellers of different diameters on a
single fuselage; naca-report-339; 1931
- Weick, Fred E; Full-scale
wind-tunnel tests on several metal propellers having different blade
forms; naca-report-340; 1931
- Joachim, William F
Hicks, Chester W Foster, Hampton H; The
design and development of an automatic injection valve with an annular orifice
of varying area; naca-report-341; 1931
- Dryden, H L Kuethe, A
M; Effect of
turbulence in wind-tunnel measurements; naca-report-342; 1931
- Heald, R H Strother, D
H Monish, B H; Effect
of variation of chord and span of ailerons on rolling and yawing moments at
several angles of pitch; naca-report-343; 1931
- Trayer, George W; The design of
plywood webs for airplane wing beams; naca-report-344; 1931
- Newlin, J A Trayer,
George W; The
design of airplane wing ribs; naca-report-345; 1931
- Thompson, F L; Water
pressure distribution on a flying boat hull; naca-report-346; 1931
- Newlin, J A Trayer,
George W; A
method of calculating the ultimate strength of continuous beams;
naca-report-347; 1931
- Whittemore, H L
Brueggeman, W C; Strength
of welded joints in tubular members for aircraft; naca-report-348;
1931
- Durand, W F; A
proof of the theorem regarding the distribution of lift over the span for
minimum induced drag; naca-report-349; 1931
- Weick, Fred E; Working
charts for the selection of aluminum alloy propellers of a standard form to
operate with various aircraft engines and bodies; naca-report-350;
1931
- Wood, Donald H; Full-scale
wind-tunnel tests of a propeller with the diameter changed by cutting off the
blade tips; naca-report-351; 1931
- Jacobs, Eastman N
Anderson, Raymond F; Large-scale
aerodynamic characteristics of airfoils as tested in the variable density wind
tunnel; naca-report-352; 1931
- Jacobs, Eastman N
Stack, John Pinkerton, Robert M; Airfoil
pressure distribution investigation in the variable density wind tunnel;
naca-report-353; 1931
- Markwardt, L J; Aircraft woods:
their properties, selection, and characteristics; naca-report-354;
1931
- Schey, Oscar W Young,
Alfred W; Comparative
flight performance with an NACA Roots supercharger and a turbocentrifugal
supercharger; naca-report-355; 1931
- Schuman, Louis Back,
Goldie; Strength of
rectangular flat plates under edge compression; naca-report-356;
1931
- Committee on Aircraft
Accidents; Aircraft
accidents : method of analysis; naca-report-357; 1931
- Brombacher, W G Melton,
E R; Temperature
coefficient of the modulus of rigidity of aircraft instrument diaphragm and
spring materials; naca-report-358; 1931
- Peters, Melville F
Summerville, Wayne L; An
investigation of the effectiveness of ignition sparks; naca-report-359;
1931
- Jacobs, Eastman N
Pinkerton, Robert M; Pressure
distribution over a symmetrical airfoil section with trailing edge flap;
naca-report-360; 1931
- Knight, Montgomery
Harris, Thomas A; Experimental
determination of jet boundary corrections for airfoil tests in four open wind
tunnel jets of different shapes; naca-report-361; 1931
- Millikan, Clark B; An extended
theory of thin airfoils and its application to the biplane problem;
naca-report-362; 1931
- Rothrock, A M; Pressure
fluctuations in a common-rail fuel injection system; naca-report-363;
1931
- Rhode, Richard; The pressure
distribution over the wings and tail surfaces of a PW-9 pursuit airplane in
flight; naca-report-364; 1931
- Ward, Kenneth E; The effect of
small variations in profile of airfoils; naca-tn-361; 1931
- Pinkerton, Robert M; Effect of nose
shape on the characteristics of symmetrical airfoils; naca-tn-386; August
1931
- Defoe, George L; A comparison of
the aerodynamic characteristics of the normal and three reflexed airfoils in
the variable density wind tunnel; naca-tn-388; August 1931
- Abbott, I H; Experiments
with an airfoil model on which the boundary layers are controlled without the
use of supplementary equipment; naca-tn-371; April 1931
- Wenzinger, Carl J
Harris, Thomas A; The
vertical wind tunnel of the National Advisory Committee for Aeronautics;
naca-report-387; 1931
- Dryden, Hugh L; Reduction of
turbulence in wind tunnels; naca-report-392; 1931
- Fuchs, Richard,
Schmidt, Wilhelm; The
steady spin; naca-tm-630; 1931
- Eastman N. Jacobs,
Kenneth E. Ward; Tests
of N.A.C.A. airfoils in the variable-density wind tunnel Series;
naca-tn-404; Jan 1932
- Edward S. Taylor; Valve timing of
engines having intake pressures higher than exhaust; naca-tn-405; Feb
1932
- Oscar W. Schey, Alfred
W. Young; The
use of large valve overlap in scavenging a supercharged spark-ignition engine
using fuel injection; naca-tn-406; Apr 1932
- A. M. Rothrock, D. W.
Lee; Effect
of the reservoir volume on the discharge pressures in the injection system
of; naca-tn-407; Feb 1932
- A. M. Rothrock; Preliminary
tests on the vaporization of fuel sprays; naca-tn-408; Feb 1932
- H. B. Hendrickson, D.
H. Strother; Effect of aging
on taut rubber diaphragms; naca-tn-409; Feb 1932
- Dana W. Lee; Experiments
on the distribution of fuel in fuel sprays; naca-tn-410; Mar 1932
- John C. Redmond; Rapid chemical
test for the identification of chromium-molybdenum steel; naca-tn-411; Mar
1932
- Raymond F. Anderson; The aerodynamic
characteristics of airfoils at negative angles of attack; naca-tn-412; Mar
1932
- Eugene E. Lundquist; The compressive
strength of duralumin columns of equal angle section; naca-tn-413; Mar
1932
- J. A. Spanogle, C. S.
Moore; Considerations
of air flow in combustion chambers of high-speed compression-ignition
engines; naca-tn-414; Apr 1932
- Fred E. Weick, Carl J.
Wenzinger; Preliminary
investigation of rolling moments obtained with spoilers on both slotted and
plain wings; naca-tn-415; Apr 1932
- Eastman N. Jacobs; Characteristics
of two sharp-nosed airfoils having reduced spinning tendencies;
naca-tn-416; Apr 1932
- Fred E. Weick, Robert
Sanders; Wind-tunnel
tests of a Hall high-life wing; naca-tn-417; May 1932
- J. A. Spanogle; Compression-ignition
engine tests of several fuels; naca-tn-418; May 1932
- Ray Windler; The
effect of propellers and nacelles on the landing speeds of tractor
monoplanes; naca-tn-420; May 1932
- N. F. Scudder, M. P.
Miller; The
nature of air flow about the tail of an airplane in a spin; naca-tn-421;
May 1932
- Fred E. Weick, Thomas
E. Harris; The aerodynamic
characteristics of a model wing having a split flap deflected downward and
moved to the rear; naca-tn-422; May 1932
- Dana W. Lee, Robert C.
Spencer; Preliminary
photomicrographic studies of fuel sprays; naca-tn-424; Jul 1932
- Melvin N. Gough, Ernest
Johnson; Methods of
visually determining the air flow around airplanes; naca-tn-425; Jul
1932
- Oscar W. Schey, Herman
H. R. Ellerbrock; Comparative
performance of a Powerplus vane-type supercharger and an N.A.C.A. Roots-type
supercharger; naca-tn-426; Jul 1932
- Eugene E. Lundquist; Strength tests
on thin-walled duralumin cylinders in torsion; naca-tn-427; Aug
1932
- Kenneth E. Ward; Characteristics
of an airfoil as affected by fabric sag; naca-tn-428; Aug 1932
- Oscar W. Schey, Arnold
E. Biermann; Heat dissipation
from a finned cylinder at different fin-plane/air-stream angles;
naca-tn-429; Aug 1932
- A. M. Rothrock, C. D.
Waldron; Effect of engine
operating conditions on the vaporization of safety fuels; naca-tn-430; Aug
1932
- Eastman N. Jacobs,
James M. Shoemaker; Tests
on thrust augmenters for jet propulsion; naca-tn-431; Sep 1932
- Ray Windler; Drag
tests of 4/9-scale model engine nacelles with various cowlings;
naca-tn-432; Oct 1932
- Freeman, Hugh B; Comparison of
full-scale propellers having R.A.F.-6 and Clark Y airfoil sections;
naca-report-378; 1932
- Weick, Fred E
Wenzinger, Carl J; Effect
of length of Handley Page tip slots on the lateral-stability factor, damping
in roll; naca-tn-423; July 1932
- Weick, Fred E Platt,
Robert C; Wind-tunnel
tests of the Fowler variable-area wing; naca-tn-419; May 1932
- Rhode, Richard V; The pressure
distribution over a standard and a modified Navy elliptical wing tip on a
biplane in flight; naca-tn-433; October 1932
- Gerrish, Harold C Voss,
Fred; Influence of
several factors on ignition lag in a compression-ignition engine;
naca-tn-434; November 1932
- Moore, C S Collins, J H
, Jr; The
effect of clearance distribution on the performance of a compression-ignition
engine; naca-tn-435; November 1932
- Moore, C S Collins, J
H; The effect
of connecting-passage diameter on the performance of a compression-ignition
engine with a precombustion chamber; naca-tn-436; November 1932
- Rhode, Richard V; The pressure
distribution over a long elliptical wing tip on a biplane in flight;
naca-tn-437; December 1932
- Stevens, F W (Bureau of
Standards); The gaseous
explosive reaction at constant pressure : further data on the effect of inert
gases; naca-tn-438; December 1932
- Samuels, L T (Weather
Bureau); Meteorological
conditions during the formation of ice on aircraft; naca-tn-439; December
1932
- Soule, Hartley A; Flight tests to
determine the effect of a fixed auxiliary airfoil on the lift and drag of a
parasol monoplane; naca-tn-440; December 1932
- Briggs, L J Dryden, H
L; Aerodynamic
characteristics of circular-arc airfoils at high speeds; naca-report-365;
1932
- Peck, William C; Dynamic and
flight tests on rubber-cord and oleo-rubber-disk landing gears for an F6C-4
airplane; naca-report-366; 1932
- Wenzinger, Carl J; Pressure
distribution over a thick, tapered and twisted monoplane wing model-NACA
81-J; naca-report-367; 1932
- Diehl, Walter S; A new chart for
estimating the absolute ceiling of an airplane; naca-report-368;
1932
- Dearborn, C H
Kirschbaum, H W; Maneuverability
investigation of the F6C-3 airplane with special flight instruments;
naca-report-369; 1932
- Monish, B H; Effect
of variation of chord and span of ailerons on hinge moments at several angles
of pitch; naca-report-370; 1932
- (Author(s) Not
Available); Present status
of aircraft instruments; naca-report-371; 1932
- Stevens, F W; The
gaseous explosive reaction : the effect of pressure on the rate of propagation
of the reaction zone and upon the rate of molecular transformation;
naca-report-372; 1932
- Gelalles, A G; Coefficients
of discharge of fuel-injection nozzles for compression-ignition engines;
naca-report-373; 1932
- Darnell, T H; The
automotive ignition coil; naca-report-374; 1932
- Wood, Donald H; Full-scale tests
of metal propellers at high tip speeds; naca-report-375; 1932
- Diehl, Walter S; Some approximate
equations for the standard atmosphere; naca-report-376; 1932
- Soule, Hartley A
Scudder, Nathan F; A
method of flight measurement of spins; naca-report-377; 1932
- Knight, Montgomery
Wenzinger, Carl J; Rolling
moments due to rolling and yaw for four wing models in rotation;
naca-report-379; 1932
- Rhode, Richard V
Lundquist, Eugene E; Pressure
distribution over the fuselage of a PW-9 pursuit airplane in flight;
naca-report-380; 1932
- Peck, William C Beard,
Albert P; Static, drop,
and flight tests on Musselman type airwheels; naca-report-381; 1932
- Trayer, George W March,
H W; Elastic
instability of members having sections common in aircraft construction;
naca-report-382; 1932
- Theodorsen, Theodore;
On the theory
of wing sections with particular reference to the lift distribution;
naca-report-383; 1932
- Schey, Oscar W; The comparative
performance of superchargers; naca-report-384; 1932
- Bamber, Millard J; Wind-tunnel
tests on airfoil boundary layer control using a backward-opening slot;
naca-report-385; 1932
- Dearborn, C H
Kirschbaum, H W; Maneuverability
investigation of an F6C-4 fighting airplane; naca-report-386; 1932
- Theodorsen, Theodore;
Investigation
of the diaphragm-type pressure cell; naca-report-388; 1932
- Freeman, Hugh B; The effect of
small angles of yaw and pitch on the characteristics of airplane
propellers; naca-report-389; 1932
- Schey, Oscar W
Biermann, Arnold E; The
effect of valve timing upon the performance of a supercharged engine at
altitude and an unsupercharged engine at sea level; naca-report-390;
1932
- Jacobs, Eastman N; The aerodynamic
characteristics of eight very thick airfoils from tests in the variable
density wind tunnel; naca-report-391; 1932
- Knight, Montgomery
Noyes, Richard W; Span-load
distribution as a factor in stability in roll; naca-report-393;
1932
- Abbott, Ira H; Airship
model tests in the variable density wind tunnel; naca-report-394;
1932
- Theodorsen, Theodore;
A new
principle of sound frequency analysis; naca-report-395; 1932
- Rothrock, A M; Hydraulics
of fuel-injection pumps for compression-ignition engines; naca-report-396;
1932
- Thompson, F L
Kirschbaum, H W; The
drag characteristics of several airships determined by deceleration tests;
naca-report-397; 1932
- Houseman, M R Keulegan,
G H; Investigation
of damping liquids for aircraft instruments : II; naca-report-398;
1932
- Marvin, Charles F , Jr
Best, Robert D; Flame
movement and pressure development in an engine cylinder; naca-report-399;
1932
- Wenzinger, Carl J
Shortal, Joseph A; The
aerodynamic characteristics of a slotted Clark y wing as affected by the
auxiliary airfoil position; naca-report-400; 1932
- Wood, Donald H; Tests of
nacelle-propeller combinations in various positions with reference to wings II
: thick wing - various radial-engine cowlings - tractor propeller;
naca-report-436; May 12, 1932
- Weick, Fred E Scudder,
Nathan F; The effect on
lift, drag, and spinning characteristics of sharp leading edges on airplane
wings; naca-tn-447; February 1933
- Defrance, Smith J; The aerodynamic
effect of a retractable landing gear; naca-tn-456; March 1933
- Heald, R H (Bureau of
Standards); Rolling,
yawing, and hinge moments produced by rectangular ailerons; naca-tn-441;
1933
- Schubauer, G B (Bureau
of Standards); Jet
propulsion with special reference to thrust augmenters; naca-tn-442;
1933
- Weick, Fred E
Wenzinger, Carl J; Wind
tunnel research concerning lateral control devices, particularly at high
angles of attack VII : Handley Page tip and full-span slots with ailerons and
spoilers; naca-tn-443; 1933
- Burke, Walter F
(University of Michigan); Working
charts for the stress analysis of elliptic rings; naca-tn-444; 1933
- Weick, Fred E Shortal,
Joseph A; Wind tunnel
research comparing lateral control devices, particularly at high angles of
attack VIII : straight and skewed ailerons on wings with rounded tips;
naca-tn-445; February 1933
- Heald, R H (Bureau of
Standards); Effect of
aileron displacement on wing characteristics; naca-tn-448; February
1933
- Weick, Fred E
Wenzinger, Carl J; Wind-tunnel
research comparing lateral control devices, particularly at high angles of
attack IX : tapered wings with ordinary ailerons; naca-tn-449; February
1933
- Wilkie, J B (Bureau of
Standards); Mercerization
of cotton for strength with special reference to aircraft cloth;
naca-tn-450; February 1933
- Weick, Fred E Noyes,
Richard W; Wind tunnel
research comparing lateral control devices, particularly at high angles of
attack X : various control devices on a wing with a fixed auxiliary
airfoil; naca-tn-451; March 1933
- Lesley, E P (Stanford
University); Experiments
with a counter-propeller; naca-tn-453; March 1933
- Spanogle, J A Buckley,
E C; The
N.A.C.A. combustion chamber gas-sampling valve and some preliminary test
results; naca-tn-454; March 1933
- Lundquist, Eugene E; Comparison of
three methods for calculating the compressive strength of flat and slightly
curved sheet and stiffener combinations; naca-tn-455; March 1933
- HOCKER RAY W; The
aerodynamic characteristics of airfoils as affected by surface roughness;
naca-tn-457; April 1933
- Weick, Fred E Harris,
Thomas A; Wind tunnel
research comparing lateral control devices, particularly at high angles of
attack XI : various floating tip ailerons on both rectangular and tapered
wings; naca-tn-458; May 1933
- Weick, Fred E Platt,
Robert C; Wind-tunnel
tests on model wing with Fowler flap and specially developed leading-edge
slot; naca-tn-459; May 1933
- Hood, Manley J White,
James A; Full-scale
wind-tunnel research on tail buffeting and wing-fuselage interference of a
low-wing monoplane; naca-tn-460; May 1933
- Dearborn, Clinton H; The effect of
rivet heads on the characteristics of a 6 by 36 foot Clark Y metal
airfoil; naca-tn-461; May 1933
- Miller, Roy A
(Consolidated Aircraft Corporation) Wood, Karl D (Cornell University); Formulas for
the stress analysis of circular rings in a monocoque fuselage;
naca-tn-462; June 1933
- Weick, Fred E Sanders,
Robert; Aerodynamic
tests of a low aspect ratio tapered wing with various flaps, for use on
tailless airplanes; naca-tn-463; June 1933
- Shoemaker, James M
Parkinson, John B; A
complete tank test of a model of a flying-boat hull-N.A.C.A. Model No.11;
naca-tn-464; July 1933
- Marsh, E T Waldron, C
D; Some
characteristics of sprays obtained from pintle-type injection models;
naca-tn-465; July 1933
- Schey, Oscar W Young,
Alfred W; Engine
performance with a hydrogenated safety fuel; naca-tn-466; July 1933
- Scudder, Nathan F; A study of
factors affecting the steady spin of an airplane; naca-tn-468; August
1933
- Kuhn, Paul; A
summary of design formulas for beams having thin webs in diagonal tension;
naca-tn-469; August 1933
- Parkinson, John B; A complete tank
test of a model of a flying-boat Hull - N.A.C.A. model no.11-A;
naca-tn-470; September 1933
- Shoemaker, James H; A complete tank
test of a model of flying-boat Hull - N.A.C.A. Model 16; naca-tn-471;
September 1933
- Wenzinger, Carl J; The effect of
partial-span split flaps on the aerodynamic characteristics of a Clark Y
wing; naca-tn-472; September 1933
- Bell, Joe W; Tank
tests of two floats for high-speed seaplanes; naca-tn-473; November
1933
- Bamber, M J Zimmerman,
C H; Effect
of stabilizer location upon pitching and yawing moments in spins as shown by
tests with the spinning balance; naca-tn-474; November 1933
- Wallace, Rudolf, N; The effect of
split trailing-edge wing flaps on the aerodynamic characteristics of a parasol
monoplane; naca-tn-475; November 1933
- Garlock, E A (Bureau of
Standards) Ellis, Greer (Bureau of Standards); The
effect on engine performance of change in jacket-water outlet temperature;
naca-tn-476; November 1933
- Sanders, Robert; Aerodynamic
tests of a low aspect ratio tapered wing with an auxiliary airfoil for use on
tailless airplanes; naca-tn-477; November 1933
- Soule, Hartley A
Wetmore, J W; The
effects of slots and flaps on lateral control of a low-wing monoplane as
determined in flight; naca-tn-478; November 1933
- Lundquist, Eugene E; Strength tests
of thin-walled duralumin cylinders in pure bending; naca-tn-479; December
1933
- Jacobs, Eastman N; The drag of
streamline wires; naca-tn-480; December 1933
- Jacobs, Eastman N; The reduction
in drag of a forward-sloping windshield; naca-tn-481; December 1933
- Dawson, John R; The effect of
spray strips on a model of the P3M-1 flying boat hull; naca-tn-482;
December 1933
- Anderson, Raymond F; Charts for
determining the pitching moment of tapered wings with sweepback and twist;
naca-tn-483; December 1933
- Rothrock, A M; Combustion
in a high-speed compression-ignition engine; naca-report-401; 1933
- Gelalles, A G; Effect
of orifice length-diameter ratio on fuel sprays for compression-ignition
engines; naca-report-402; 1933
- Theodorsen, Theodore
Clay, William C; Ice
prevention on aircraft by means of engine exhaust heat and a technical study
of heat transmission from a Clark y airfoil; naca-report-403; 1933
- Schey, Oscar W Rollin,
Vern G; The
effect of increased carburetor pressure on engine performance at several
compression ratios; naca-report-404; 1933
- Upson, Ralph H Klikoff,
W A; Application of
practical hydrodynamics to airship design; naca-report-405; 1933
- Peck, W D Beard, A P;
Drop and
flight tests on NY-2 landing gears including measurements of vertical
velocities at landing; naca-report-406; 1933
- Weick, Fred E
Wenzinger, Carl J; The
characteristics of a Clark y wing model equipped with several forms of
low-drag fixed slots; naca-report-407; 1933
- Oswald, W Bailey; General
formulas and charts for the calculation of airplane performance;
naca-report-408; 1933
- Theodorsen, Theodore
Freeman, Ira M; The
elimination of fire hazard due to back fires; naca-report-409; 1933
- Theodorsen, Theodore;
The theory
of wind-tunnel wall interference; naca-report-410; 1933
- Theodorsen, Theodore;
Theory of
wing sections of arbitrary shape; naca-report-411; 1933
- Harris, Thomas A; The 7 by 10
foot wind tunnel of the National Advisory Committee for Aeronautics;
naca-report-412; 1933
- Rhode, Richard V
Pearson, Henry A; A
method for computing leading-edge loads; naca-report-413; 1933
- Mcavoy, William H
Schey, Oscar W Young, Alfred W; The
effect on airplane performance of the factors that must be considered in
applying low-drag cowling to radial engines; naca-report-414; 1933
- Wood, Donald H; Tests of
nacelle-propeller combinations in various positions with reference to wings.
Part I : thick wing-N.A.C.A. cowled nacelle-tractor propeller;
naca-report-415; 1933
- Jacobs, Eastman N
Abbott, Ira H; The
NACA variable-density wind tunnel; naca-report-416; 1933
- Noyes, Richard W; Pressure
distribution tests on a series of Clark y biplane cellules with special
reference to stability; naca-report-417; 1933
- Weick, Fred E; Preliminary
investigation of modifications to conventional airplanes to give nonstalling
and short-landing characteristics; naca-report-418; 1933
- Weick, Fred E
Wenzinger, Carl J; Wind-tunnel
research comparing lateral control devices, particularly at high angles of
attack I : ordinary ailerons on rectangular wings; naca-report-419;
1933
- Beij, K Hilding; Aircraft speed
instruments; naca-report-420; 1933
- Stickle, George W; Measurement of
the differential and total thrust and torque of six full-scale
adjustable-pitch propellers; naca-report-421; 1933
- Weick, Fred E Noyes,
Richard W; Wind-tunnel
research comparing lateral control devices, particularly at high angles of
attack II : slotted ailerons and frise ailerons; naca-report-422;
1933
- Weick, Fred E
Wenzinger, Carl J; Wind-tunnel
research comparing lateral control devices, particularly at high angles of
attack III : ordinary ailerons rigged up 10 degrees when neutral;
naca-report-423; 1933
- Weick, Fred E Harris,
Thomas A; Wind-tunnel
research comparing lateral control devices, particularly at high angles of
attack IV : floating tip ailerons on rectangular wings; naca-report-424;
1933
- Lee, Dana W; The
effect of nozzle design and operating conditions on the atomization and
distribution of fuel sprays; naca-report-425; 1933
- Brooks, D G Garlock, E
A; The
effect of humidity on engine power at altitude; naca-report-426;
1933
- Weick, Fred E Shortal,
Joseph A; The effect of
multiple fixed slots and a trailing-edge flap on the lift and drag of a Clark
Y airfoil; naca-report-427; 1933
- Weick, Fred E Bamber,
Millard J; Wind-tunnel
tests of a Clark Y wing with a narrow auxiliary airfoil in different
positions; naca-report-428; 1933
- Rothrock, A M; The
NACA apparatus for studying the formation and combustion of fuel sprays and
the results from preliminary tests; naca-report-429; 1933
- Freeman, Hugh B; Measurements of
flow in the boundary layer of a 1/40-scale model of the U. S. Airship
"Akron."; naca-report-430; 1933
- Zimmerman, C H; Characteristics
of Clark Y airfoils of small aspect ratios; naca-report-431; 1933
- Freeman, Hugh B; Force
measurements on a 1/40-scale model of the U. S. Airship "Akron.";
naca-report-432; 1933
- Gelalles, A G Marsh, E
T; Rates of
fuel discharge as affected by the design of fuel-injection systems for
internal-combustion engines; naca-report-433; 1933
- Wheatley, John B; Lift and drag
characteristics and gliding performance of an autogiro as determined in
flight; naca-report-434; 1933
- Rothrock, A M Waldron,
C D; Fuel
vaporization and its effect on combustion in a high-speed compression-ignition
engine; naca-report-435; 1933
- Dryden, Hugh L Monish,
B H; The
effect of area aspect ratio on the yawing moments of rudders at large angles
of pitch on three fuselages; naca-report-437; 1933
- Lee, Dana W; Experiments
on the distribution of fuel in fuel sprays; naca-report-438; 1933
- Weick, Fred E Shortal,
Joseph A; Wind-tunnel
research comparing lateral control devices, particularly at high angles of
attack V : spoilers and ailerons on rectangular wings; naca-report-439;
1933
- Castleman, R A , Jr; The mechanism
of atomization accompanying solid injection; naca-report-440; 1933
- Jacobs, Eastman N Ward,
Kenneth E Pinkerton, Robert M; The
characteristics of 78 related airfoil sections from tests in the
variable-density wind tunnel; naca-report-460; 1933
- Theodorsen, T Garrick,
I E; General
potential theory of arbitrary wing section; naca-report-452; 1934
- Bamber, Millard J; Aerodynamic
rolling and yawing moments produced by floating wing-tip ailerons, as measured
by spinning balance; naca-tn-493; March 1934
- Ober, Shatswell
(Massachusetts Institute of Technology, Cambridge, Mass); Calculation
of horsepower available : appendix to estimation of the variation of thrust
horsepower with air speed; naca-tn-446; July 1934
- Hartman, Edwin P; A method of
calculating the performance of controllable propellers with sample
computations; naca-tn-484; 1934
- Spanogle, J A; A
comparison of several methods of measuring ignition lag in a
compression-ignition engine; naca-tn-485; 1934
- Shoemaker, James M
Dawson, John R; The
effect of trim angle on the take-off performance; naca-tn-486; 1934
- Anderson, Raymond F; Tests of three
tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y
sections; naca-tn-487; 1934
- Shoemaker, James M; A complete tank
test of a flying-boat hull with a pointed step -N.A.C.A. Model No. 22;
naca-tn-488; February 1934
- Parkinson, John B; Tank tests of
auxiliary vanes as a substitute for planing area; naca-tn-490; February
1934
- Shoemaker, James M
Parkinson, John B; Tank
tests of a family of flying-boat hulls; naca-tn-491; February 1934
- Wheatley, John B; The aerodynamic
analysis of the gyroplane rotating-wing system; naca-tn-492; March
1934
- (Author(s) Not
Available); Hazards to
aircraft due to electrical phenomena; naca-tn-494; March 1934
- Defrance, S J; Effect
of the surface condition of a wing on the aerodynamic characteristics of an
airplane; naca-tn-495; April 1934
- Buckley, E C Waldron, C
D; A
preliminary motion-picture study of combustion in a compression-ignition
engine; naca-tn-496; April 1934
- Dearborn, C H; Full-scale
drag tests of landing lamps; naca-tn-497; May 1934
- Wenzinger, Carl J; Wind-tunnel
measurements of air loads on split flaps; naca-tn-498; May 1934
- Shortal, J A; Effect
of retractable-spoiler location on rolling- and yawing-moment
coefficients; naca-tn-499; July 1934
- Kuhn, Paul; The
torsional stiffness of thin duralumin shells subjected to large torques;
naca-tn-500; July 1934
- Brevoort, M J; Landing-shock
recorder; naca-tn-501; July 1934
- Hubbard, John D
(Department of Aero. Engineering, University of Detroit.) Brescoll, George P
(Department of Aero. Engineering, University of Detroit); Aerodynamic
investigation of a cup anemometer; naca-tn-502; July 1934
- Brombacher, W G (Bureau
of Standards); Measurement
of altitude in blind flying; naca-tn-503; August 1934
- Shoemaker, James M
Bell, Joe W; Complete tank
tests of two flying-boat hulls with pointed steps - N.A.C.A. Models 22-A and
35; naca-tn-504; September 1934
- Wenzinger, Carl J; The effects of
full-span and partial-span split flaps on the aerodynamic characteristics of a
tapered wing; naca-tn-505; September 1934
- Schliestett, George Van
(Daniel Guggenheim School of Aeronautics, Georgia School of Technology); Experimental
verification of Theodorsen's theoretical jet-boundary correction factors;
naca-tn-506; October 1934
- Peck, William C; Landing
characteristics of an autogiro; naca-tn-508; November 1934
- Shoemaker, James M; Tank tests of
flat and v-bottom planning surfaces; naca-tn-509; November 1934
- Parkinson, J E Bell, J
W; The
calculated effect of trailing-edge flaps on the take-off of flying boats;
naca-tn-510; November 1934
- Higgins, George J
(Aeronautical Engineering Department, University of Michigan); A
study of the pitching moments and the stability characteristics of
monoplanes; naca-tn-511; November 1934
- Dawson, John R; A complete tank
test of the hull of the Sikorsky S-40 flying boat - American Clipper
Class; naca-tn-512; December 1934
- Truscott, Starr; The wave
suppressor used in the N.A.C.A. tank; naca-tn-513; December 1934
- Moore, C S Collins, J H
, Jr; Effect
of combustion-chamber shape on the performance of a prechamber
compression-ignition engine; naca-tn-514; December 1934
- Bamber, M J; Aerodynamic
effects of a split flap on the spinning characteristics of a monoplane
model; naca-tn-515; December 1934
- Scudder, Nathan F; A flight
investigation of the spinning of the NY-1 airplane with varied mass
distribution and other modifications, and an analysis based on wind-tunnel
tests; naca-report-441; 1934
- Soule, Hartley A
Wheatley, John B; A
comparison between the theoretical and measured longitudinal stability
characteristics of an airplane; naca-report-442; 1934
- Freeman, Hugh B; Pressure-distribution
measurements on the hull and fins of scale model of the U. S. Airship
"Akron."; naca-report-443; 1934
- Weick, Fred E Harris,
Thomas A; Wind-tunnel
research comparing lateral control devices, particularly at high angles of
attack VI : skewed ailerons on rectangular wings; naca-report-444;
1934
- Kuhn, Paul; Working
charts for the determination of the lift distribution between biplane
wings; naca-report-445; 1934
- Jacobs, Eastman N; Airfoil section
characteristics as affected by protuberances; naca-report-446; 1934
- Diehl, Walter S; Static thrust
of airplane propellers; naca-report-447; 1934
- Mock, W C , Jr Dryden,
H L; Improved
apparatus for the measurement of fluctuations of air speed in turbulent
flow; naca-report-448; 1934
- Jacobs, Eastman N
Sherman, Albert; Wing
characteristics as affected by protuberances of short span;
naca-report-449; 1934
- Diehl, Walter S; The calculation
of take-off run; naca-report-450; 1934
- Abbott, Ira H; The
drag of two streamline bodies as affected by protuberances and appendages;
naca-report-451; 1934
- Diehl, Walter S; The estimation
of maximum load capacity of seaplanes and flying boats; naca-report-453;
1934
- Lee, Dana W Spencer,
Robert C; Photomicrographic
studies of fuel sprays; naca-report-454; 1934
- Rothrock, A M Marsh, E
T; Penetration and
duration of fuel sprays from a pump injection system; naca-report-455;
1934
- Bamber, M J Zimmerm, N,
C h; The
aerodynamic forces and moments exerted on a spinning model of the NY-1
airplane as measured by the spinning balance; naca-report-456; 1934
- Thompson, F L
Kirschbaum, H W; Maneuverability
investigation of an O3U-1 observation airplane; naca-report-457;
1934
- Diehl, Walter S; Relative
loading on biplane wings; naca-report-458; 1934
- Defrance, Smith J; The NACA
full-scale wind tunnel; naca-report-459; 1934
- Theodorsen, Theodore;
Interference
on an airfoil of finite span in an open wind tunnel; naca-report-461;
1934
- Stack, John; The
NACA high-speed wind tunnel and tests of six propeller sections;
naca-report-463; 1934
- Hartman, Edwin P; Negative thrust
and torque characteristics of an adjustable-pitch metal propeller;
naca-report-464; 1934
- Garrick, I E; Determination
of the theoretical pressure distribution for twenty airfoils;
naca-report-465; 1934
- Sontag, Harcourt
Brombacher, W G; Aircraft
power-plant instruments; naca-report-466; 1934
- Soule, Hartley A
Miller, Marvel P; The
experimental determination of the moments of inertia of airplanes;
naca-report-467; 1934
- Biermann, David
Herrnstein, William H , Jr; The
interference between struts in various combinations; naca-report-468;
1934
- Spanogle, J A Hicks, C
W Foster, H H; Increasing
the air charge and scavenging the clearance volume of a compression-ignition
engine; naca-report-469; 1934
- Truscott, Starr; The NACA tank :
a high-speed towing basin for testing models of seaplane floats;
naca-report-470; 1934
- Schey, Oscar W Young,
Alfred W; Performance of
a fuel-injection spark-ignition engine using a hydrogenated safety fuel;
naca-report-471; 1934
- Weick, Fred E Sanders,
Robert; Wind-tunnel
tests on combinations of a wing with fixed auxiliary airfoils having various
chords and profiles; naca-report-472; 1934
- Lundquist, Eugene E; Strength tests
of thin-walled duralumin cylinders in compression; naca-report-473;
1934
- Von Karman, TH
Millikan, C; On the theory
of laminar boundary layers involving separation; naca-report-504;
1934
- Wood, Donald H; Tests of
nacelle-propeller combinations in various positions with reference to wings
III : Clark y wing - various radial-engine cowlings - tractor propeller;
naca-report-462; 1934
- R. Schulz, W. Pleines;
Technical
Aspects of the 1934 International Touring Competition (Rundflug);
naca-tm-760; December 1934
- Biechteler, Curt.; Influence of
cut-outs in elevator on the static longitudinal stability and on the static
elevator effect; naca-tm-750; 1934
- Stuper, J.; Investigation
of boundary layers on an airplane wing in free flight; naca-tm-751;
1934
- Hubner, Walter.; Additional test
data on static longitudinal stability; naca-tm-752; 1934
- Stipa, Luigi.; Stipa
monoplane with Venturi fuselage; naca-tm-753; 1934
- Wieselsberger, C.; Contribution to
the mutual interference of wing and propeller; naca-tm-754; 1934
- Teichmann, Alfred.; Safety and
design in airplane construction; naca-tm-755; 1934
- Schussler, Karl.; The behavior
under shearing stress of duralumin strip with round, flanged holes;
naca-tm-756; 1934
- Wieselsberger, C.; The Aachen
wind-tunnel balance; naca-tm-757; 1934
- Lutz, O.; The
processes in spring-loaded injection valves of solid injection oil
engines; naca-tm-758; 1934
- Kosin, R.; The
effect of weight and drag on the sinking speed and lift/drag ratio of
gliders; naca-tm-759; 1934
- Dawson, John R; A general tank
test of NACA model 11-C flying-boat hull, including the effect of changing the
plan form of the step; naca-tn-538; August 1935
- Zimmerman, C H; Aerodynamic
characteristics of several airfoils of low aspect ratio; naca-tn-539;
August 1935
- Burke, Walter F; A deflection
formula for single-span beams of constant section subjected to combined axial
and transverse loads; naca-tn-540; September 1935
- Allison, John M; The effect of
the angle of afterbody on the water performance of a flying-boat hull
model; naca-tn-541; September 1935
- Kuhn, Paul; The
initial torsional stiffness of shells with interior webs; naca-tn-542;
September 1935
- Stack, John; The
compressibility bubble; naca-tn-543; October 1935
- Von Doenhoff, Albert E;
An
application of the von Karman-Millikan laminar boundary-layer theory and
comparison with experiment; naca-tn-544; October 1935
- Parkinson, J B; Tank tests of a
model of a flying-boat hull having a longitudinally concave planing
bottom; naca-tn-545; November 1935
- Weick, Fred E Shortal,
Joseph A; Development of
the NACA slot-lip aileron; naca-tn-547; November 1935
- Soule, H A; Flight
tests of a balanced split flap with particular reference to rapid
operation; naca-tn-548; December 1935
- Defrance, S J; Drag
of prestone and oil radiators on the YO-31A airplane; naca-tn-549;
December 1935
- Theodorsen, Theodore;
General
theory of aerodynamic instability and the mechanism of flutter;
naca-report-496; 1935
- Taylor, E S
(Massachusetts Institute of Technology, Cambridge, Mass); The
importance of auto-ignition lag in knocking; naca-tn-452; March
1935
- Theodorsen, T; Propeller
vibrations and the effect of the centrifugal force; naca-tn-516; February
1935
- Bamber, M J Zimmerman,
C H; The
aerodynamic forces and moments on a spinning model of the F4B-2 airplane as
measured by the spinning balance; naca-tn-517; February 1935
- Moore, C S Foster, H H;
Performance
tests of a single-cylinder compression-ignition engine with a displacer
piston; naca-tn-518; February 1935
- Stowell, E Z Deming, A
F; Vortex
noise from rotating cylindrical rods; naca-tn-519; February 1935
- Datwyler, G; Calculations
of the effect of wing twist on the air forces acting on a monoplane wing;
naca-tn-520; 1935
- Parsons, John F; Full-scale
force and pressure-distribution tests on a tapered U.S.A. 45 airfoil;
naca-tn-521; March 1935
- Dawson, John R; Tank tests of a
model of a flying-boat hull with a fluted bottom; naca-tn-522; March
1935
- Lundquiest, Eugene E;
Strength
tests of thin-walled duralumin cylinders in combined transverse shear and
bending; naca-tn-523; April 1935
- Noyes, Richard W; Wind-tunnel
tests of a wing with a trailing-edge auxiliary airfoil used as a flap;
naca-tn-524; 1935
- Hartman, Edwin P; The aerodynamic
drag of flying-boat hull model as measured in the NACA 20-foot wind tunnel
I.; naca-tn-525; April 1935
- Bamber, M J; Spinning
characteristics of wings II : rectangular Clark Y biplane cellule: 25 percent
stagger; 0 degree decalage; gap/chord 1.0; naca-tn-526; April 1935
- Lundquist, Eugene E
Burke, Walter F; Strength
tests of thin-walled duralumin cylinders of elliptic section; naca-tn-527;
May 1935
- Wheatley, John B
Windler, Ray; Wind-tunnel
tests of a cyclogiro rotor; naca-tn-528; May 1935
- Schwartz, A Murray
(Stanford University) Bogert, Reid (Stanford University); Analysis
of a strut with a single elastic support in the span, with applications to the
design of airplane jury-strut systems; naca-tn-529; May 1935
- Kuhn, Paul; Bending
stresses due to torsion in cantilever box beams; naca-tn-530; June
1935
- Parkinson, J B; Tank tests of
model 11-G flying-boat hull; naca-tn-531; June 1935
- Sontag, Harcourt
(National Bureau of Standards) Borlik, E L (National Bureau of Standards); Method of
testing oxygen regulators; naca-tn-532; June 1935
- Taylor, E S
(Massachusetts Institute of Technology); The
thermodynamics of combustion in the Otto cycle engine; naca-tn-533; June
1935
- James, Benjamin Wylie
(Stanford University); Principal
effects of axial load on moment-distribution analysis of rigid structures;
naca-tn-534; July 1935
- Bell, Joe W; The
effect of depth of step on the water performance of a flying-boat hull
model; naca-tn-535; July 1935
- Desmond, G L
(Aerodynamical Laboratory, U.S.N) Mccrary, J A (Aerodynamical Laboratory,
U.S.N); The
6-foot-4-inch wind tunnel at the Washington Navy Yard; naca-tn-536; August
1935
- Scudder, N F
Kirschbaum, H W; A
preliminary determination of normal accelerations on racing airplanes;
naca-tn-537; August 1935
- Wheatley, John B; Wing pressure
distribution and rotor-blade motion of an autogiro as determined in
flight; naca-report-475; 1935
- Gerrish, Harold C
Tessmann, Arthur M; Relation
of hydrogen and methane to carbon monoxide in exhaust gases from
internal-combustion engines; naca-report-476; 1935
- Rothrock, A M Marsh, E
T; Effect of
viscosity on fuel leakage between lapped plungers and sleeves and on the
discharge from a pump-injection system; naca-report-477; 1935
- Theodorsen, Theodore
Silverstein, Abe; Experimental
verification of the theory of wind-tunnel boundary interference;
naca-report-478; 1935
- Donnell, L H; Stability
of thin-walled tubes under torsion; naca-report-479; 1935
- Sherman, Albert; The aerodynamic
effects of wing cut-outs; naca-report-480; 1935
- Hartman, Edwin P; Working charts
for the determination of propeller thrust at various air speeds;
naca-report-481; 1935
- White, James A Hood,
Manley J; Wing-fuselage
interference, tail buffeting, and air flow about the tail of a low-wing
monoplane; naca-report-482; 1935
- Rothrock, A M Spencer,
R C; Effect
of moderate air flow on the distribution of fuel sprays after injection
cut-0ff; naca-report-483; 1935
- Scudder, N F; A
flight investigation of the effect of mass distribution and control setting on
the spinning of the XN2Y-1 airplane; naca-report-484; 1935
- Herrnstein, William H
Biermann, David; The
drag of airplane wheels, wheel fairings, and landing gears - I;
naca-report-485; 1935
- Marvin, Charles F , Jr
Caldwell, Frank R Steele, Sydney; Infrared
radiation from explosions in a spark-ignition engine; naca-report-486;
1935
- Wheatley, John B; An aerodynamic
analysis of the autogiro rotor with a comparison between calculated and
experimental results; naca-report-487; 1935
- Biermann, Arnold, E
Pinkel, Benjamin; Heat
transfer from finned metal cylinders in an air stream; naca-report-488;
1935
- Thompson, F L Peck, W C
Beard, A P; Air conditions
close to the ground and the effect on airplane landings; naca-report-489;
1935
- Theodorsen, Theodore
Gelalles, A G; Vibration
response of airplane structures; naca-report-491; 1935
- Stack, John Von
Doenhoff, Albert E; Tests
of 16 related airfoils at high speed; naca-report-492; 1935
- Draper, C S; The
physical effects of detonation in a closed cylindrical chamber;
naca-report-493; 1935
- Weick, Fred E Soule,
Hartley A Gough, Melvin N; A
flight investigation of the lateral control characteristics of short wide
ailerons and various spoilers with different amounts of wing dihedral;
naca-report-494; 1935
- Spanogle, J A Whitney,
E G; A
description and test results of a spark-ignition and a compression-ignition
2-stroke-cycle engine; naca-report-495; 1935
- Dryden, Hugh L; Computation of
the two-dimensional flow in a laminar boundary layer; naca-report-497;
1935
- Clay, William C; Improved
airplane windshields to provide vision in stormy weather; naca-report-498;
1935
- Weick, Fred E
Wenzinger, Carl J; Wind-tunnel
research comparing lateral control devices, particularly at high angles of
attack XII : upper-surface ailerons on wings with split flaps;
naca-report-499; 1935
- Mutchler, Willard; The weathering
of aluminum alloy sheet materials used in aircraft; naca-report-490;
1935
- Rhode, Richard V; The influence
of tip shape on the wing load distribution as determined by flight tests;
naca-report-500; 1935
- Diehl, Walter S; Relative
loading on biplane wings of unequal chords; naca-report-501; 1935
- Silverstein, Abe; Scale effect on
Clark Y airfoil characteristics from NACA full-scale wind-tunnel tests;
naca-report-502; 1935
- Truscott, Starr; The effect of
spray strips on the take-off performance of a model of a flying-boat hull;
naca-report-503; 1935
- Mchugh, James G; Tests of
nacelle-propeller combinations in various positions with reference to wings IV
: thick wing - various radial-engine cowlings - tandem propellers;
naca-report-505; 1935
- Valentine, E Floyd; Tests of
nacelle-propeller combinations in various positions with reference to wings V
: Clark Y biplane cellule - NACA cowled nacelle - tractor propeller;
naca-report-506; 1935
- Wood, Donald H
Bioletti, Carlton; Tests
of nacelle-propeller combinations in various positions with reference to wings
VI : wings and nacelles with pusher propeller; naca-report-507;
1935
- Oskar Schrenk; Experiments
with suction-type wings; naca-tm-773; August 1935
- Georgii, W.; Gliding
in convection currents; naca-tm-761; 1935
- Lippisch, A.; Effect
of aerodynamic design on glider performance; naca-tm-762; 1935
- Doetsch, Hans.; The heat
transfer of cooling fins on moving air; naca-tm-763; 1935
- Muttray, H.; The
aerodynamic aspect of wing-fuselage fillets; naca-tm-764; 1935
- Leglise, Pierre.; The 1934
contest for the Deutsch de la Meurthe trophy; naca-tm-765; 1935
- Malmer, Ivar.; The
aeronautical laboratory of the Stockholm Technical Institute; naca-tm-766;
1935
- Betz, A.; Modification
of wing-section shape to assure a predetermined change in pressure
distribution; naca-tm-767; 1935
- Muttray, H.; The
interdependence of profile drag and lift with Joukowski type and related
airfoils; naca-tm-768; 1935
- Cicala, Placido.; The bending of
beams with thin tension flanges; naca-tm-769; 1935
- Eula, Antonio.; Hydrodynamic
tests of models of seaplane floats; naca-tm-770; 1935
- Le Sueur, Maurice.; Ground effect
on the take-off and landing of airplanes; naca-tm-771; 1935
- ; The
Denis-Gruson six-component wind-tunnel balance; naca-tm-772; 1935
- Wagner, H.,
Ballerstedt, W.; Tension
fields in originally curved, thin sheets during shearing stresses;
naca-tm-774; 1935
- Kiel, G.; Total-head
meter with small sensitivity to yaw; naca-tm-775; 1935
- Venediger, Herbert J.;
A discussion
of the several types of two-stroke-cycle engines; naca-tm-776; 1935
- Hoerner, S.; Tests
of spheres with reference to Reynolds number, turbulence, and surface
roughness; naca-tm-777; 1935
- Lippisch, A.; Method
for the determination of the spanwise lift distribution; naca-tm-778;
1935
- Muller, J.; Weldability
of high-tensile steels from experience in airplane construction, with special
reference to welding crack susceptibility; naca-tm-779; 1935
- Shenstone, B. S.,
Scott-Hall, S.; Glider
development in Germany :a technical survey of progress in design in Germany
since 1922; naca-tm-780; 1935
- Herbert Wagner; Torsion and
Buckling of Open Sections; naca-tm-807; October 1936
- Dawson, John R; Tank tests of
three models of flying-boat hulls of the pointed-step type with different
angles of dead rise - NACA model 35 series; naca-tn-551; 1936
- Weick, Fred E; Wind-tunnel
tests of wing flaps suitable for direct control of glide-path angle;
naca-tn-552; 1936
- Gough, Melvin N; Notes on the
technique of landing airplanes equipped with wing flaps; naca-tn-553;
1936
- Kaplan, Carl; Circular
motion of bodies of revolution; naca-tn-554; February 1936
- Schey, Oscar W
Ellerbrock, Herman H , Jr; The
performance of a DePalma Roots-type supercharger; naca-tn-558; March
1936
- Brevoort, Maurice J; Combustion-engine
temperatures by the sodium line-reversal method; naca-tn-559; March
1936
- Sullivan, J E (Bureau
of Aeronautics, Navy Department); A
comparison of corrosion-resistant steel (18 percent chromium - 8 percent
nickel) and aluminum alloy (24st); naca-tn-560; March 1936
- Parsons, John F; Full-scale
wind-tunnel to determine a satisfactory location for a service Pitot-static
tube on a low-wing monoplane; naca-tn-561; March 1936
- Kuhn, Paul; Remarks
on the elastic axis of shell wings; naca-tn-562; April 1936
- Parkinson, J B; Tank tests of
models of floats for single-float seaplanes First series.; naca-tn-563;
April 1936
- Thompson, F L; Procedure
for determining speed and climbing performance of airships; naca-tn-564;
April 1936
- Gerrish, Harold C Ayer,
Bruce E; Influence of
fuel-oil temperature on the combustion in a prechamber compression-ignition
engine; naca-tn-565; 1936
- Bell, Joe W; Tank
tests of a model of the NC flying-boat hull - N.A.C.A. model 44;
naca-tn-566; May 1936
- Gough, M N Beard, A P;
Limitations
of the pilot in applying forces to airplane controls; naca-tn-550;
1936
- Jacobs, Eastman N
Pinkerton, Robert M; Tests
of N.A.C.A. airfoils in the variable-density wind tunnel Series 230.;
naca-tn-567; May 1936
- Wetmore, J W; Calculated
effect of various types of flap on take-off over obstacles; naca-tn-568;
May 1936
- Moore, Charles S
Foster, Hampton H; Boosted
performance of a compression-ignition engine with a displaced piston;
naca-tn-569; May 1936
- Zimmerman, C H; Effect of
changes in tail arrangement upon the spinning of a low-wing monoplane
model; naca-tn-570; June 1936
- Pearson, H A; A
method of estimating the aerodynamic effects of ordinary and split flaps of
airfoils similar to the Clark Y; naca-tn-571; June 1936
- Schey, Oscar W
Ellerbrock, Herman H , Jr; Performance
of air-cooled engine cylinders using blower cooling; naca-tn-572; July
1936
- Womack, S H J (National
Bureau of Standards) Peterson, J B (National Bureau of Standards); Carbon-monoxide
indicators for aircraft; naca-tn-573; July 1936
- Allison, John M Ward,
Kenneth E; Tank tests of
models of flying boat hulls having longitudinal steps; naca-tn-574; July
1936
- Kirschbaum, H W; Estimation of
moments of inertia of airplanes from design data; naca-tn-575; July
1936
- Allison, John M; Tanks test of a
model of the hull of the Navy PB-1 flying boat - N.A.C.A. Model 52;
naca-tn-576; August 1936
- Moore, Charles S
Collins, John H , Jr; Friction
of compression-ignition engines; naca-tn-577; August 1936
- Dearborn, C H Soule, H
A; Full-scale
wind-tunnel and flight tests of a Fairchild 22 airplane equipped with a Fowler
flap; naca-tn-578; August 1936
- White, Roland J
(California Institute of Technology) Martin, Victor J (California Institute of
Technology); Charts for
calculating the performance of airplanes having constant-speed propellers;
naca-tn-579; September 1936
- Dawson, John R
Truscott, Starr; A
general tank test of a model of the hull of the British Singapore IIC flying
boat; naca-tn-580; September 1936
- Wheatley, John B; A study of
autogiro rotor-blade oscillations in the plane of the rotor disk;
naca-tn-581; September 1936
- Wheatley, John B
Bioletti, Carlton; Analysis
and model tests of autogiro jump take-off; naca-tn-582; October
1936
- Gerrish, Harold C Voss,
Fred; Mixture
distribution in a single-row radial engine; naca-tn-583; October
1936
- Schey, Oscar W Pinkel,
Benjamin; Effect of
several factors on the cooling of a radial engine in flight; naca-tn-584;
November 1936
- Brueggeman, Wm C
(National Bureau of Standards); Mechanical
properties of aluminum-alloy rivets; naca-tn-585; November 1936
- Donely, Philip; The forces and
moments on airplane engine mounts; naca-tn-587; December 1936
- Kuhn, Paul; Analysis
of 2-spar cantilever wings with special reference to torsion and load
transference; naca-report-508; 1936
- Lundquist, Eugene E
Burke, Walter F; General
equations for the stress analysis of rings; naca-report-509; 1936
- Weick, Fred E Noyes,
Richard W; Wind-tunnel
research comparing lateral control devices particularly at high angles of
attack XIII : auxiliary airfoils used as external ailerons;
naca-report-510; 1936
- Schey, Oscar W Rollin,
Vern G; The
effect of baffles on the temperature distribution and heat-transfer
coefficients of finned cylinders; naca-report-511; 1936
- Rothrock, A M Cohn,
Mildred; Some factors
affecting combustion in an internal-combustion engine; naca-report-512;
1936
- Brevoort, M J Joyner, U
T; Experimental
investigation of the Robinson-type cup anemometer; naca-report-513;
1936
- Gough, Melvin N; The measurement
of the field of view from airplane cockpits; naca-report-514; 1936
- Wheatley, John B Hood,
Manley J; Full-scale
wind-tunnel tests of a PCA-2 autogiro rotor; naca-report-515; 1936
- Kaplan, Carl; Potential
flow about elongated bodies of revolution; naca-report-516; 1936
- Soule, H A Mcavoy, W H;
Flight
investigation of lateral control devices for use with full-span flaps;
naca-report-517; 1936
- Biermann, David
Herrnstein, William H , Jr; The
drag of airplane wheels, wheel fairings, and landing gears II : nonretractable
and partly retractable landing gears; naca-report-518; 1936
- Bamber, M J Zimmerman,
C H; Spinning
characteristics of wings I : rectangular Clark Y monoplane wing;
naca-report-519; 1936
- Lee, Dana W; A
comparison of fuel sprays from several types of injection nozzles;
naca-report-520; 1936
- Zimmerman, Charles H;
An analysis
of longitudinal stability in power-off flight with charts for use in
design; naca-report-521; 1936
- Herrnstein, William H ,
Jr Biermann, David; The
drag of airplane wheels, wheel fairings, and landing gears - III;
naca-report-522; 1936
- Wheatley, John B; The influence
of wing setting on the wing load and rotor speed of a PCA-2 autogiro as
determined in flight; naca-report-523; 1936
- Schubauer, G B; A turbulence
indicator utilizing the diffusion of heat; naca-report-524; 1936
- Rothrock, A M Waldron,
C D; Some
effects of injection advance angle, engine-jacket temperature, and speed on
combustion in a compression-ignition engine; naca-report-525; 1936
- Stowell, E Z Deming, A
F; Noise
from two-blade propellers; naca-report-526; 1936
- Schubauer, G B; Air flow in a
separating laminar boundary layer; naca-report-527; 1936
- Harris, Thomas A; Reduction of
hinge moments of airplane control surfaces by tabs; naca-report-528;
1936
- Scudder, N F Seidman,
Oscar; A
flight investigation of the spinning of the F4B-2 biplane with various loads
and tail surfaces; naca-report-529; 1936
- Jacobs, Eastman N Clay,
William C; Characteristics
of the NACA 23012 airfoil from tests in the full-scale and variable-density
tunnels; naca-report-530; 1936
- Fiock, Ernest F King, H
Kendall; The
effect of water vapor on flame velocity in equivalent carbon monoxide and
oxygen mixtures; naca-report-531; 1936
- Fiock, Ernest F Roeder,
Carl H; The
soap-bubble method of studying the combustion of mixtures of carbon monoxide
and oxygen; naca-report-532; 1936
- Rothrock, A M Marsh, E
T; Distribution
and regularity of injection from a multicylinder fuel-injection pump;
naca-report-533; 1936
- Platt, Robert C; Aerodynamic
characteristics of a wing with Fowler flaps including flap loads, downwash,
and calculated effect on take-off; naca-report-534; 1936
- Gerrish, Harold C
Foster, H; Hydrogen as an
auxiliary fuel in compression-ignition engines; naca-report-535;
1936
- Wheatley, John B
Bioletti, Carlton; Wind-tunnel
tests of a 10-foot-diameter gyroplane rotor; naca-report-536; 1936
- Jacobs, Eastman N
Pinkerton, Robert M; Tests
in the variable-density wind tunnel of related airfoils having the maximum
camber unusually far forward; naca-report-537; 1936
- Brombacher, W G; Altitude-pressure
tables based on the United States standard atmosphere; naca-report-538;
1936
- Wallace, Rudolf; Investigation
of full-scale split trailing-edge wing flaps with various chords and hinge
locations; naca-report-539; 1936
- Jacobs, Eastman N Ward,
Kenneth E; Interference of
wing and fuselage from tests of 209 combinations in the NACA variable-density
tunnel; naca-report-540; 1936
- Platt, Robert C; Aerodynamic
characteristics of wings with cambered external airfoil flaps, including
lateral control, with a full-span flap; naca-report-541; 1936
- Kussner, H. G.; Status of wing
flutter; naca-tm-782; 1936
- Liebers, F.; Analysis
of the three lowest bending frequencies of a rotating propeller;
naca-tm-783; 1936
- Wagner, H., Pretschner,
W.; Torsion
and buckling of open sections; naca-tm-784; 1936
- Heck, O. S., Ebner, H.;
Methods and
formulas for calculating the strength of plate and shell constructions as used
in airplane design; naca-tm-785; 1936
- Noth, H., Polte, W.; The formation
of ice on airplanes; naca-tm-786; 1936
- Kramer, M.; The
5- by 7-meter wind tunnel of the DVL; naca-tm-788; 1936
- Forthmann. E.; Turbulent
jet expansion; naca-tm-789; 1936
- Holfelder, Otto.; Ignition and
flame development in the case of diesel fuel injection; naca-tm-790;
1936
- Schmidbauer, Hans.; Behavior of
turbulent boundary layers on curved convex walls; naca-tm-791; 1936
- Tollmien, W.; General
instability criterion of laminar velocity distributions; naca-tm-792;
1936
- Huber, Maximilian T.;
Bending of
beams of thin sections; naca-tm-793; 1936
- Dufaure De Lajarte, A.;
Chief
characteristics and advantages of tailless airplanes; naca-tm-794;
1936
- Gruson, M. F.; Similitude
in hydrodynamic tests involving planing; naca-tm-795; 1936
- Stuper, J.; Contribution
to the problem of airfoils spanning a free jet; naca-tm-796; 1936
- Wentzel, W.; Ignition
process in Diesel engines; naca-tm-797; 1936
- Winter, H.; Flow
phenomena on plates and airfoils of short span; naca-tm-798; 1936
- Ferrari, C.; The
transport of vorticity through fluids in turbulent motion : in the light of
the Prandtl and Taylor theories; naca-tm-799; 1936
- Borkmann, K.; Charts
for checking the stability of compression members in trusses; naca-tm-800;
1936
- McAvoy, W. H.; Piloting
technique for recovery from spins; naca-tn-555; 1936
- Hartman, Edwin P.; Considerations
of the take-off problem; naca-tn-557; 1936
- Dawson, John R; Tank tests of
two models of flying-boat hulls to determine the effect of ventilating the
step; naca-tn-594; February 1937
- Buckwalter, John C
(Stanford University) Reed, Warren D (Stanford University) Niles, Alfred S
(Stanford University); Bending
tests of circular cylinders of corrugated aluminum-alloy sheet;
naca-tn-595; March 1937
- Dearborn, C H Soule, H
A; Full-scale
wind-tunnel and flight test of a Fairchild 22 airplane equipped with a Zap
flap and Zap ailerons; naca-tn-596; March 1937
- Soule, Hartley A; Notes on the
calculation of the minimum horizontal tail surface for airplanes equipped with
wing flaps; naca-tn-597; April 1937
- Gauvain, William E; Wind-tunnel
tests of a Clark Y wing with 'Maxwell' leading-edge slots; naca-tn-598;
April 1937
- Pearson, H A; Charts
expressing the time, velocity, and altitude relations for an airplane diving
in a standard atmosphere; naca-tn-599; April 1937
- Lee, Dana W Marsh, E T;
Discharge
characteristics of a double injection-valve single-pump injection system;
naca-tn-600; May 1937
- Dumont, C (Aluminum
Company of America, Aluminum Research Labs., New Kensington, Penn) Hill, H N
(Aluminum Company of America, Aluminum Research Labs., Kensington, Penn); The lateral
instability of deep rectangular beams; naca-tn-601; May 1937
- Biermann, Arnold E; Heat transfer
from cylinders having closely spaced fins; naca-tn-602; May 1937
- Rothrock, A M Spencer,
R C; A
preliminary study of flame propagation in a spark-ignition engine;
naca-tn-603; June 1937
- Pearson, H A; Empirical
corrections to the span load distribution at the tip; naca-tn-606; August
1937
- Pekelsma, Robert E
(Department of Aeronautical Engineering, University of Michigan); The
behavior of thin-will monocoque cylinders under torsional vibration;
naca-tn-607; August 1937
- Diehl, W S (Bureau of
Aeronautics, Navy Department); Considerations
affecting the additional weight required in mass balance of ailerons;
naca-tn-609; August 1937
- Earle, Sherod L Dutee,
Francis J; Effect of
air-entry angle on performance of a 2-stroke-cycle compression-ignition
engine; naca-tn-610; August 1937
- Klemin, Alexander (New
York University); Motion
of the two-control airplane in rectilinear flight after initial disturbances
with introduction of controls following an exponential law; naca-tn-615;
September 1937
- Bamber, M J House, R O;
Spinning
characteristics of wings IV : changes in stagger of rectangular Clark Y
cellules; naca-tn-625; December 1937
- Wenzinger, Carl J; Pressure
distribution over a Clark Y-H airfoil section with a split flap;
naca-tn-627; December 1937
- Kuhn, Paul; Strain
measurements on small duralumin box beams in bending; naca-tn-588;
1937
- Pearson, H A; Theoretical
span loading and moments of tapered wings produced by aileron deflection;
naca-tn-589; 1937
- Ward, Kenneth E; Hydrodynamic
tests in the N.A.C.A. tank of a model of the hull of the Short Calcutta flying
boat; naca-tn-590; 1937
- Parsons, John F
Silverstein, Abe; Full
scale span load distribution on a tapered wing with split flaps of various
spans; naca-tn-591; February 1937
- Biermann, David; A study of the
factors affecting the range of airplanes; naca-tn-592; February
1937
- Wildhack, W A; Pressure
drop in tubing in aircraft instrument installations; naca-tn-593;
1937
- Reed, Warren D Clay,
William C; Full-scale
wind-tunnel and flight tests of a Fairchild 22 airplane equipped with
external-airfoil flaps; naca-tn-604; July 1937
- Seidman, Oscar
Neihouse, A I; Free-spinning
wind-tunnel tests of a low-wing monoplane with systemic changes in wings and
tails; naca-tn-608; August 1937
- Draper, C S
(Massachusetts Institute of Technology, Cambridge , Mass); The
sonic altimeter for aircraft; naca-tn-611; August 1937
- Bamber, M J House, R O;
Spinning
characteristics of wings III : rectangular and tapered; naca-tn-612;
September 1937
- Clauser, Milton
(California Institute of Technology) Clauser, Francis (California Institute of
Technology); The effect of
curvature on the transition from laminar to turbulent boundary layer;
naca-tn-613; September 1937
- Abbott, Ira H; Fuselage-drag
tests in the variable-density wind tunnel: streamline bodies of revolution,
fineness ratio of 5; naca-tn-614; September 1937
- Thompson, F L; The
measurement of air speed in airplanes; naca-tn-616; 1937
- Lundquist, Eugene E; Stability of
structural members under axial load; naca-tn-617; 1937
- Holt, M (Aluminum
Research Laboratories) Hartman, E C (Aluminum Research Laboratories); Increasing
the strength of aluminum-alloy columns by prestressing; naca-tn-618;
1937
- Moore, Charles S
Collins, John H; Compression-ignition
engine performance at altitudes and at various air pressures and
temperatures; naca-tn-619; November 1937
- Brevoort, Maurice J; Energy loss,
velocity distribution, and temperature distribution for a baffled cylinder
model; naca-tn-620; October 1937
- Rollin, Vern G
Ellerbrock, Herman H; Pressure
drop across finned cylinders enclosed in a jacket; naca-tn-621; November
1937
- Soule, H A Hootman,
James A; Flight tests of
an airplane showing dependence of the maximum lift coefficient on the test
conditions; naca-tn-622; November 1937
- Mcavoy, William H; Maximum forces
applied by pilots to wheel-type controls; naca-tn-623; November
1937
- Sontag, Harcourt
(National Bureau of Standards) Johnson, Daniel P (National Bureau of
Standards); Performance
characteristics of venturi tubes used in aircraft for operating air-driven
gyroscopic instruments; naca-tn-624; November 1937
- Knight, Montgomery
(Georgia School of Technology) Hefner, Ralph A (Georgia School of Technology);
Static
thrust analysis of the lifting airscrew; naca-tn-626; December 1937
- Kline, G M (National
Bureau of Standards); Plastics
as structural materials for aircraft; naca-tn-628; December 1937
- Stowell, E Z; A
sound pressure-level meter without amplification; naca-tn-629; December
1937
- Seidman, Oscar
Neihouse, A I; Free
spinning wind-tunnel tests of a low-wing monoplane with systematic wings and
tails; naca-tn-630; December 1937
- Garrick, I E; Potential
flow about arbitrary biplane wing sections; naca-report-542; 1937
- Parkinson, John B
Dawson, John R; Tank
tests of NACA model 40 series of hulls for small flying boats and
amphibians; naca-report-543; 1937
- Cohn, Mildred Spencer,
Robert C; Combustion in a
bomb with a fuel-injection system; naca-report-544; 1937
- Rothrock, A M Waldron,
C D; Effects
of air-fuel spray and flame formation in a compression-ignition engine;
naca-report-545; 1937
- Schubauer, G B Dryden,
H L; The
effect of turbulence on the drag of flat plates; naca-report-546;
1937
- Silverstein, Abe White,
James A; Wind-tunnel
interference with particular reference to off-center positions of the wing and
to the downwash at the tail; naca-report-547; 1937
- Shortal, Joseph A; Effect of tip
shape and dihedral on lateral-stability characteristics; naca-report-548;
1937
- Wenzinger, Carl J; Wind-tunnel
investigation of the aerodynamic balancing of upper-surface ailerons and split
flaps; naca-report-549; 1937
- Schey, Oscar W Rollin,
Vern G; Cooling
characteristics of a 2-row radial engine; naca-report-550; 1937
- Peterson, John B Smith,
Clyde W; Aircraft
compass characteristics; naca-report-551; 1937
- Wheatley, John B
Bioletti, Carlton; Wind-tunnel
tests of 10-foot-diameter autogiro rotors; naca-report-552; 1937
- Fiock, Ernst F Roeder,
Carl H; Some
effects of argon and helium upon explosions of carbon monoxide and oxygen;
naca-report-553; 1937
- Wenzinger, Carl J; Wind-tunnel
investigation of ordinary and split flaps on airfoils of different
profile; naca-report-554; 1937
- Brevoort, M J Rollin,
Vern G; Air
flow around finned cylinders; naca-report-555; 1937
- Marvin, Charles F , Jr
Wharton, Armistead Roeder, Carl H; Further
studies of flame movement and pressure development in an engine cylinder;
naca-report-556; 1937
- Zimmerman, C H; Preliminary
tests in the NACA free-spinning wind tunnel; naca-report-557; 1937
- Platt, Robert C; Turbulence
factors of NACA wind tunnels as determined by sphere tests;
naca-report-558; 1937
- Scudder, N F; The
forces and moments acting on parts of the XN2Y-1 airplane during spins;
naca-report-559; 1937
- Jones, Robert T; A simplified
application of the method of operators to the calculation of disturbed motions
of an airplane; naca-report-560; 1937
- Rothrock, A M Waldron,
C D; Effect
of nozzle design on fuel spray and flame formation in a high-speed
compression-ignition engine; naca-report-561; 1937
- Dryden, Hugh L; Air flow in the
boundary layer near a plate; naca-report-562; 1937
- Pinkerton, Robert M; Calculated and
measured pressure distributions over the midspan section of the NACA 4412
airfoil; naca-report-563; 1937
- Windler, Ray; Tests
of a wing-nacelle-propeller combination at several pitch settings up to 42
degrees; naca-report-564; 1937
- Lee, Dana W; Measurements
of fuel distribution within sprays for fuel-injection engines;
naca-report-565; 1937
- Silverstein, Abe
Gulick, B G; Ground-handling
forces on a 1/40-scale model of the U. S. Airship "Akron.";
naca-report-566; 1937
- Garrick, I E; Propulsion
of a flapping and oscillating airfoil; naca-report-567; 1937
- Foster, H H; The
quiescent-chamber type compression-ignition engine; naca-report-568;
1937
- Robinson, Russell G
Herrnstein, William H , Jr; Wing-nacelle-propeller
interference for wings of various spans force and pressure-distribution
tests; naca-report-569; 1937
- Weick, Fred E Jones,
Robert T; The effect of
lateral controls in producing motion of an airplane as computed from
wind-tunnel data; naca-report-570; 1937
- Wenzinger, Carl J
Harris, Thomas A; Pressure
distribution over a rectangular airfoil with a partial-span split flap;
naca-report-571; 1937
- Anderson, Raymond F; Determination
of the characteristics of tapered wings; naca-report-572; 1937
- Platt, Robert C Abbott,
Ira H; Aerodynamic
characteristics of NACA 23012 and 23021 airfoils with 20-percent-chord
external-airfoil flaps of NACA 23012 section; naca-report-573; 1937
- Wenzinger, Carl J; Pressure
distribution over an airfoil section with a flap and tab; naca-report-574;
1937
- Sherman, Albert; Interference of
wing and fuselage from tests of 28 combinations in the NACA variable-density
tunnel; naca-report-575; 1937
- (Author(s) Not
Available); Aircraft
accidents.method of analysis; naca-report-576; 1937
- Soule, Hartley A; Flight
measurements of the dynamic longitudinal stability of several airplanes and a
correlation of the measurements with pilots' observations of handling
characteristics; naca-report-578; 1937
- Wetmore, J W; The
rolling friction of several airplane wheels and tires and the effect of
rolling friction on take-off; naca-report-583; 1937
- Brueggeman, W C; Strength of
welded aircraft joints; naca-report-584; 1937
- Pearson, H A; Span
load distribution for tapered wings with partial-span flaps;
naca-report-585; 1937
- Jacobs, Eastman N
Sherman, Albert; Airfoil
section characteristics as affected by variations of the Reynolds number;
naca-report-586; 1937
- Schey, Oscar W
Ellerbrock, Herman H , Jr; Blower
cooling of finned cylinders; naca-report-587; 1937
- Rothrock, A M Waldron,
C D; Fuel
spray and flame formation in a compression-ignition engine employing air
flow; naca-report-588; 1937
- Zimmerman, Charles H;
An analysis
of lateral stability in power-off flight with charts for use in design;
naca-report-589; 1937
- Pearson, H A; Pressure-distribution
measurements on O-2H airplane in flight; naca-report-590; 1937
- Wheatley, John B; An analytical
and experimental study of the effect of periodic blade twist on the thrust,
torque, and flapping motion of an autogiro rotor; naca-report-591;
1937
- Theodorsen, Theodore
Brevoort, M J Stickle, George W; Full-scale
tests of NACA cowlings; naca-report-592; 1937
- Theodorsen, Theodore
Brevoort, M J Stickle, George W; Cooling
of airplane engines at low air speeds; naca-report-593; 1937
- Theodorsen, Theodore
Stickle, George W Brevoort, M J; Characteristics
of six propellers including the high-speed range; naca-report-594;
1937
- Theodorsen, Theodore
Brevoort, M J Stickle, George W Gough, M N; Full-scale
tests of a new type NACA nose-slot cowling; naca-report-595; 1937
- Brevoort, M J Stickle,
George W Ellerbrock, Herman H , Jr; Cooling
tests of a single-row radial engine with several NACA cowlings;
naca-report-596; 1937
- Lesley, E P Worley,
George F Moy, Stanley; Air
propellers in yaw; naca-report-597; 1937
- Mock, W C , Jr; Alternating-current
equipment for the measurement of fluctuations of air speed in turbulent
flow; naca-report-598; 1937
- Rhode, Ricahrd V
Pearson, Henry A; Flight
tests of the drag and torque of the propeller in terminal-velocity dives;
naca-report-599; 1937
- Wheatley, John B; An analysis of
the factors that determine the periodic twist of an autogiro rotor blade, with
a comparison of predicted and measured results; naca-report-600;
1937
- Stang, Ambrose H
Ramberg, Walter Back, Goldie; Torsion
tests of tubes; naca-report-601; 1937
- Shortal, Joseph A; Wind-tunnel and
flight tests of slot-lip ailerons; naca-report-602; 1937
- Platt, Robert C
Shortal, Joseph A; Wind-tunnel
investigation of wings with ordinary ailerons and full-span external-airfoil
flaps; naca-report-603; 1937
- Mchugh, James G; Pressure-distribution
measurements at large angles of pitch on fins of different span-chord ratio on
a 1/40-scale model of the U. S. Airship "Akron."; naca-report-604;
1937
- Weick, Fred E Jones,
Robert T; Resume and
analysis of NACA lateral control research; naca-report-605; 1937
- Peterson, John B
Womack, S H J; Electrical
thermometers for aircraft; naca-report-606; 1937
- Bamber, M J House, R O;
Spinning
characteristics of the XN2Y-1 airplane obtained from the spinning balance and
compared with results from the spinning tunnel and from flight tests;
naca-report-607; 1937
- Kuhn, Paul; Stress
analysis of beams with shear deformation of the flanges; naca-report-608;
1937
- Silverstein, Abe
Katzoff, S; Experimental
investigation of wind-tunnel interference on the downwash behind an
airfoil; naca-report-609; 1937
- Jacobs, Eastman N
Pinkerton, Robert M Greenberg, Harry; Tests
of related forward-camber airfoils in the variable-density wind tunnel;
naca-report-610; 1937
- Wenzinger, Carl J; Wind-tunnel
investigation of tapered wings with ordinary ailerons and partial-span split
flaps; naca-report-611; 1937
- Sherman, Albert; Wing-fuselage
interference comparison of conventional and airfoil-type-fuselage
combinations; naca-wr-l-509; March 1937
- Deming, A. F.; Noise
from propellers with symmetrical sections at zero blade angle;
naca-tn-605; 1937
- Pinkerton, Robert M
Greenberg, Harry; Aerodynamic
characteristics of a large number of airfoils tested in the variable-density
wind tunnel; naca-report-628; 1938
- Pinkel, Benjamin; Heat-transfer
processes in air-cooled engine cylinders; naca-report-612; 1938
- Pinkerton, Robert M; The variation
with Reynolds number of pressure distribution over an airfoil section;
naca-report-613; 1938
- Wenzinger, Carl J; Pressure
distribution over an NACA 23012 airfoil with an NACA 23012 external-airfoil
flap; naca-report-614; 1938
- Osgood, William R; Column strength
of tubes elastically restrained against rotation at the ends;
naca-report-615; 1938
- Gerrish, Harold C Voss,
Fred; Interrelation
of exhaust-gas constituents; naca-report-616; 1938
- Selden, Robert F; Auto-ignition
and combustion of diesel fuel in a constant-volume bomb; naca-report-617;
1938
- Silverstein, Abe
Katzoff, S Hootman, James A; Comparative
flight and full-scale wind-tunnel measurements of the maximum lift of an
airplane; naca-report-618; 1938
- Lindsey, W F; Drag
of cylinders of simple shapes; naca-report-619; 1938
- Wenzinger, Carl J
Anderson, Walter B; Pressure
distribution over airfoils with Fowler flaps; naca-report-620; 1938
- Kaplan, Carl; Compressible
flow about symmetrical Joukowski profiles; naca-report-621; 1938
- Rothrock, A M Spencer,
R C; A
photographic study of combustion and knock in a spark-ignition engine;
naca-report-622; 1938
- Bailey, F J , Jr; A study of the
torque equilibrium of an autogiro rotor; naca-report-623; 1938
- Kaplan, Carl; Two-dimensional
subsonic compressible flow past elliptic cylinders; naca-report-624;
1938
- Diehl, Walter S; A discussion of
certain problems connected with the design of hulls of flying boats and the
use of general test data; naca-report-625; 1938
- Wetmore, J W; The
transition phase in the take-off of an airplane; naca-report-626;
1938
- Anderson, Raymond F; The
experimental and calculated characteristics of 22 tapered wings;
naca-report-627; 1938
- Garrick, I E; On
some reciprocal relations in the theory of nonstationary flows;
naca-report-629; 1938
- Soule, H A Gracey, W;
A flight
comparison of conventional ailerons on a rectangular wing and of conventional
and floating wing-tip ailerons on a tapered wing; naca-report-630;
1938
- Eastman N. Jacobs, R.
V. Rhode; Airfoil Section
Characteristics as Applied to the Prediction of Air Forces and Their
Distribution on Wings; naca-report-631; 1938
- Osgood, William R; The crinkling
strength and the bending strength of round aircraft tubing;
naca-report-632; 1938
- Wenzinger, Carl J
Delano, James B; Pressure
distribution over an NACA 23012 airfoil with a slotted and a plain flap;
naca-report-633; 1938
- Allen, H Julian; Calculation of
the chordwise load distribution over airfoil sections with plain, split, or
serially hinged trailing-edge flaps; naca-report-634; 1938
- Pearson, Henry A Jones,
Robert T; Theoretical
stability and control characteristics of wings with various amounts of taper
and twist; naca-report-635; 1938
- Kuhn, Paul; Approximate
stress analysis of multistringer beams with shear deformation of the
flanges; naca-report-636; 1938
- Silverstein, Abe
Becker, John V; Determination
of boundary-layer transition on three symmetrical airfoils in the NACA
full-scale wind tunnel; naca-report-637; 1938
- Jones, Robert T; The influence
of lateral stability on disturbed motions of an airplane with special
reference to the motions produced by gusts; naca-report-638; 1938
- Biermann, David
Hartman, Edwin P; The
effect of compressibility on eight full-scale propellers operating in the
take-off and climbing range; naca-report-639; 1938
- Hartman, Edwin P
Biermann, David; The
aerodynamic characteristics of full-scale propellers having 2, 3, and 4 blades
of Clark y and R.A.F. 6 airfoil sections; naca-report-640; 1938
- Hartman, Edwin P
Biermann, David; The
negative thrust and torque of several full-scale propellers and their
application to various flight problems; naca-report-641; 1938
- Biermann, David
Hartman, Edwin P; Tests
of five full-scale propellers in the presence of a radial and a liquid-cooled
engine nacelle, including tests of two spinners; naca-report-642;
1938
- Hartman, Edwin P
Biermann, David; The
aerodynamic characteristics of four full-scale propellers having different
plan forms; naca-report-643; 1938
- Hartman, Edwin P
Biermann, David; The
torsional and bending deflection of full-scale aluminum-alloy propeller blades
under normal operating conditions; naca-report-644; 1938
- Highley, Frank H; Wind-tunnel
tests of carburetor-intake rams; naca-tn-631; 1938
- Soule, H A Gracey, W;
Improvement
of aileron effectiveness by the prevention of air leakage through the hinge
gap as determined in flight; naca-tn-632; 1938
- Bamber, M J House, R O;
Spinning
characteristics of wings V : N.A.C.A. 0009, 23018, and 6718 monoplane
wings; naca-tn-633; 1938
- Tozier, Robert E; The N.A.C.A.
optical engine indicator; naca-tn-634; 1938
- Allison, John M; Tank tests of a
model of one hull of the Savoia S-55-X flying boat -N.A.C.A. Model 46;
naca-tn-635; February 1938
- Imlay, Frederick H; The estimation
of the rate of change of yawing moment with sideslip; naca-tn-636;
February 1938
- (Author(s) Not
Available); Preliminary
fatigue studies on aluminum alloy aircraft engines; naca-tn-637; February
1938
- Allison, John; Tank
tests of Model 36 flying boat hull; naca-tn-638; March 1938
- Von Doenhoff, Albert E;
A
preliminary investigation of boundary-layer transition along a flat plate with
adverse pressure gradient; naca-tn-639; March 1938
- Sherman, Albert; Interference of
wing and fuselage from tests of the 18 combinations in the N.A.C.A.
variable-density tunnel - combination with split flaps; naca-tn-640; March
1938
- Sherman, Albert; Interference of
wing and fuselage from tests of 17 combinations in the NACA variable-density
tunnel combination with special junctures; naca-tn-641; March 1938
- Sherman, Albert; Interference of
wing and fuselage from tests of eight combinations in the NACA
variable-density tunnelcombinations with tapered fillets and straight-side
junctures; naca-tn-642; March 1938
- Diehl, Walter S; A study of
flying-boat take-off; naca-tn-643; April 1938
- Donely, Philip Pearson,
Henry A; Flight and
wind-tunnel tests of an XBM-1 dive bomber; naca-tn-644; April 1938
- Soule, Hartley A GOUGH
MELVIN N; Some aspects of
the stalling of modern low-lying monoplanes; naca-tn-645; April
1938
- Hartman, Edwin P; Wind-tunnel
tests of a 2-engine airplane model as a preliminary study of flight conditions
arising on the failure of the engine; naca-tn-646; April 1938
- Rothbrock, A M
Biermann, Arnold E; Engine
performance and knock rating of fuels for high-output aircraft engines;
naca-tn-647; April 1938
- Truscott, Starr
Parkinson, J B; The
increase in frictional resistance caused by various types of rivet heads as
determined by tests of planing surfaces; naca-tn-648; May 1938
- Brevoort, Maurice J; The effect of
air-passage length on the optimum fin spacing for maximum cooling;
naca-tn-649; May 1938
- Wenzinger, Carl J; Wind-tunnel
tests of a Clark Y wing having split flaps with gaps; naca-tn-650; May
1938
- Biermann, Arnold E; Effect of
spark-timing regularity on the knock of engine performance; naca-tn-651;
May 1938
- Lundquist, Eugene E
Kroll, W D; Tables of
stiffness and carry-over factor for structural members under axial load;
naca-tn-652; June 1938
- Soule, H A Hootman,
James A; A
flight investigation of the reduction of aileron operating force by means of
fixed tabs and differential linkage, with notes on linkage design;
naca-tn-653; June 1938
- Schey, Oscar W Clark, J
Denny; Fuel
consumption of a carburetor engine at various speeds and torques;
naca-tn-654; June 1938
- Brevoort, M J; Principles
involved in the cooling of a finned and baffled cylinder; naca-tn-655;
June 1938
- Parkinson, J B; Tank tests to
show the effect rivet heads on the water performance of a seaplane-float;
naca-tn-657; July 1938
- Lundquist, Eugene E; Generalized
analysis of experimental observations in problems of elastic stability;
naca-tn-658; July 1938
- Wenzinger, Carl J
Bamber, Millard J; Wind-tunnel
of three lateral-control devices in combination with a full-span slotted flap
on an NACA 23012 airfoil; naca-tn-659; August 1938
- Bleakney, William M; Fatigue testing
of wing beam by the resonance method; naca-tn-660; August 1938
- Wenzinger, Carl J Ames,
Milton B , Jr; Wind-tunnel
investigation of rectangular and tapered NACA 23012 wings with plain ailerons
and full-span split flaps; naca-tn-661; August 1938
- Brombacher, W G Trent,
W C; Gyroscopic
instruments for instrument flying; naca-tn-662; September 1938
- House, R O; The
effects of partial-span plain flaps on the aerodynamic characteristics of a
rectangular and a tapered Clark Y wing; naca-tn-663; September 1938
- Seidman, Oscar NEIHOUSE
A I; Free-spinning
wind-tunnel tests of a low-wing monoplane with systematic changes in wings and
tails III : mass distributed along the wings; naca-tn-664; September
1938
- Stack, John Lindsey, W
F; Tests of
N-85, N-86 and N-87 airfoil sections in the 11-inch high speed wind
tunnel; naca-tn-665; September 1938
- Klemin, Alexander
Pepper, Perry A Wittner, Howard A; Longitudinal
stability in relation to the use of an automatic pilot; naca-tn-666;
September 1938
- Jones, Robert T; Operational
treatment of the nonuniform-lift theory in airplane dynamics; naca-tn-667;
October 1938
- Truscott, Starr
Parkinson, J B Ebert, John W , Jr Valentine, E Floyd; Hydrodynamic
and aerodynamic tests of models of flying-boat hulls designed flow aerodynamic
drag - NACA models 74, 74-A, and 75; naca-tn-668; October 1938
- Robinson, Russell G; The drag of
inflatable rubber de-icers; naca-tn-669; October 1938
- Thopmson, F L; NACA
stall-warning indicator; naca-tn-670; October 1938
- Von Doenhoff, Albert E;
A method of
rapidly estimating the position of the laminar separation point;
naca-tn-671; October 1938
- Abbott, Ira H Sherman,
Albert; Flow
observations with tufts and lampblack of the stalling of four typical airfoil
sections in the NACA variable-density tunnel; naca-tn-672; October
1938
- Stickle, George W
Joyner, Upshur T; The
pressure available for ground cooling in front of the cowling of air-cooled
airplane engines; naca-tn-673; November 1938
- Rogowski, A R
(Massachusetts Institute of Technology) Bouchard, C L (Massachusetts Institute
of Technology); Scavenging
a piston-ported two-stroke cylinder; naca-tn-674; November 1938
- Marsh, Edred T; Discharge
characteristics of a simulated unit injection system; naca-tn-676;
November 1938
- Benson, William M
(Stanford University); Tests
of a contra-propeller for aircraft; naca-tn-677; November 1938
- Dawson, John R Hartman,
Edwin P; Hydrodynamic
and aerodynamic tests of four models of outboard floats : (N.A.C.A. models
51-A, 51-B, 51-C, and 51-D); naca-tn-678; December 1938
- Deming, A F; Noise
from propellers with symmetrical sections at zero blade angle, II;
naca-tn-679; December 1938
- House, R O; The
aerodynamic drag of five models of side floats N.A.C.A. Models 51-E, 51-F,
51-G, 51-H, 51-J; naca-tn-680; December 1938
- Dawson, John R; A general tank
test of a model of the hull of the P3M-1 flying boat including a special
working chart for the determination of hull performance; naca-tn-681;
December 1938
- Moore, Charles S
Collins, John H , Jr; Prechamber
compression-ignition engine performance; naca-report-577; 1938
- Jones, Robert T; A study of the
two-control operation of an airplane; naca-report-579; 1938
- Selden, Robert F
Spencer, Robert C; Heat
transfer to fuel sprays injected into heated gases; naca-report-580;
1938
- Dryden, Hugh L
Schubauer, G B Mock, W C , Jr Skramstad, H K; Measurements
of intensity and scale of wind-tunnel turbulence and their relation to the
critical Reynolds number of spheres; naca-report-581; 1938
- Lundquist, Eugene E
Fligg, Claude M; A
theory for primary failure of straight centrally loaded columns;
naca-report-582; 1938
- Wilson, Herbert A , Jr;
Aerodynamic
characteristics of a 4-engine monoplane showing effects of enclosing the
engines in the wing and comparisons of tractor- and pusher-propeller
arrangements; naca-wr-l-456; April 1938
- Parkinson, J B HOUSE R
O; Hydrodynamic
and aerodynamic tests of models of floats for single-float seaplanes NACA
models 41-D, 41-E, 61-A, 73, and 73-A; naca-tn-656; July 1938
- Robert T. Jones; The unsteady
lift of a finite wing; naca-tn-682; January 1939
- Reynolds, Blake
(Massachusetts Institute of Technology) Schecter, Harry (Massachusetts
Institute of Technology) Taylor, E S (Massachusetts Institute of Technology);
The charging
process in a high-speed, single-cylinder, four-stroke engine; naca-tn-675;
February 1939
- Troller, TH (Daniel
Guggenheim Airship Institute, Akron, Ohio) Rokaus, F (Daniel Guggenheim
Airship Institute, Akron, Ohio); Pressure-distribution
measurements on a tapered wing with a full-span split flap in curved
flight; naca-tn-683; 1939
- Ramberg, Walter
(National Bureau of Standards) MCPHERSON ALBERT E (National Bureau of
Standards) Levy, Sam (National Bureau of Standards); Experimental
study of deformation and of effective width in axially loaded sheet-stringer
panels; naca-tn-684; February 1939
- Kuethe, Arnold (Daniel
Guggenheim Airship Institute, Akron, Ohio); Circulation
measurements about the tip of an airfoil during flight through a gust;
naca-tn-685; February 1939
- Lundquist, Eugene E; Local
instability of symmetrical rectangular tubes under axial compression;
naca-tn-686; February 1939
- Kuhn, Paul; Loads
imposed on intermediate frames of stiffened shells; naca-tn-687; February
1939
- Schey, Oscar W Clark, J
Denny; Comparative
performance of engines using a carburetor, manifold injection, and cylinder
injection; naca-tn-688; February 1939
- Lesley, E P (Daniel
Guggenheim Aero. Lab., Stanford, Univ); Tandem
air propellers; naca-tn-689; February 1939
- Wenzinger, Carl J
Rogallo, Francis M; Resume
of air-load data on slats and flaps; naca-tn-690; March 1939
- Kuhn, Paul; Some
elementary principles of shell stress analysis with notes on the use of the
shear center; naca-tn-691; March 1939
- Diehl, Walter S (Bureau
of Aeronautics, Navy Department); Some
fundamental considerations in regard to the use of power in landing an
airplane; naca-tn-692; March 1939
- Goett, Harry J
Bicknell, Joseph; Comparison
of profile-drag and boundary-layer measurements obtained in flight and in the
full-scale wind tunnel; naca-tn-693; March 1939
- Fishbein, Meyer
(Stanford University); Physical
properties of synthetic resin materials; naca-tn-694; March 1939
- Moore, R L (Aluminum
Company of America, New Kensington, Penn) Paul, D A (Aluminum Company of
America, New Kensington, Penn); Torsional
stability of aluminum alloy seamless tubing; naca-tn-696; March
1939
- Coleman, Robert; The frequency
of torsional vibration of a tapered beam; naca-tn-697; March 1939
- Lesley, E P (Daniel
Guggenheim Aero. Lab., Stanford University); Propeller
tests to determine the effect of number of blades at two typical
solidities; naca-tn-698; April 1939
- House, R O; Tests
of an N.A.C.A. 23012 Airfoil with a slotted deflector flap; naca-tn-699;
April 1939
- Weiss, Herbert K; Theory of
automatic control of airplanes; naca-tn-700; April 1939
- Waldron, C D; Intermittent-flow
coefficients of a poppet valve; naca-tn-701; April 1939
- Bamber, M J; Wind-tunnel
tests of several forms of fixed wing slot in combination with a slotted flap
on an N.A.C.A. 23012 airfoil; naca-tn-702; April 1939
- Bamber, M J House, R O;
Wind-tunnel
investigation of effect of yaw on lateral-stability characteristics I : four
N.A.C.A. 23012 wings of various plan forms with and without dihedral;
naca-tn-703; April 1939
- Kuhn, Paul; Some
notes on the numerical solution of shear-lag and mathematically related
problems; naca-tn-704; May 1939
- Recant, Isidore G; Wind-tunnel
investigation of ground effect on wings with flaps; naca-tn-705; May
1939
- Donely, Philip; An experimental
investigation of the normal acceleration of an airplane model in a gust;
naca-tn-706; May 1939
- Moore, Charles S
Foster, Hampton H; Compression-ignition
engine performance with undoped and doped fuel oils and alcohol mixtures;
naca-tn-707; August 1939
- Hill, H N (Aluminum
Company of America); A
semi-graphical method for analyzing strains measured on three or four gage
lines intersecting at 45 degrees; naca-tn-709; May 1939
- Selden, Robert F; A comparison of
ignition characteristics of diesel fuels as determined in engines and in a
constant-volume bomb; naca-tn-710; June 1939
- Seidman, Oscar Donlan,
Charles J; An approximate
spin design criterion for monoplanes; naca-tn-711; June 1939
- Rodert, Lewis A; A preliminary
study of the prevention of ice on aircraft by the use of engine-exhaust
heat; naca-tn-712; June 1939
- Anderson, Raymond F; A comparison of
several tapered wings designed to avoid tip stalling; naca-tn-713; June
1939
- Wetmore, J W; Flight
tests of retractable ailerons on a highly tapered wing; naca-tn-714; June
1939
- Harris, Thomas A; Wind-tunnel
investigation of an N.A.C.A. 23012 airfoil with two arrangements of a
wide-chord slotted flap; naca-tn-715; June 1939
- Parkinson, John B
Olson, Roland E House, Rufus O; Hydrodynamic
and aerodynamic tests of a family of models of seaplane floats with varying
angles of dead rise - N.A.C.A. Models 57-A, 57-B, and 57-C; naca-tn-716;
July 1939
- Lundquist, Eugene E; A method of
estimating the critical buckling load for structural members; naca-tn-717;
July 1939
- Axilrod, Benjamin M
(National Bureau of Standards) Kline, Gordon M (National Bureau of Standards);
Resistance
of transparent plastics to impact; naca-tn-718; July 1939
- House, Rufus O; The effects of
partial-span slotted flaps on the aerodynamic characteristics of a rectangular
and a tapered N.A.C.A. 23012 wing; naca-tn-719; July 1939
- Stickle, George W; Flight tests of
N.A.C.A. nose-slot cowlings on the BFC-1 airplane; naca-tn-720; August
1939
- Ramberg, Walter
(National Bureau of Standards) Mcpherson, Albert E (National Bureau of
Standards) Levy, Sam (National Bureau of Standards); Compressive
tests of a monocoque box; naca-tn-721; August 1939
- Lundquist, Eugene E; Local
instability of centrally loaded columns of channel section and Z-section;
naca-tn-722; August 1939
- Rothrick, A M Selden,
R; Adhesion
of ice in its relation to the de-icing of airplanes; naca-tn-723; August
1939
- Hood, Manley J; The effects of
surface waviness and of rib stitching on wing drag; naca-tn-724; August
1939
- Bell, Joe W Olson,
Roland E; Tank tests to
determine the effects of the chine flare of a flying-boat hull N.A.C.A. Model
Series 62 and 69; naca-tn-725; August 1939
- Gottlieb, R (University
of Maryland) Thompson, T M (University of Maryland) Witt, E C (University of
Maryland); Combined
beam-column stresses of aluminum-alloy channel sections; naca-tn-726;
September 1939
- Rodert, Lewis A; A flight
investigation of the distribution of ice-inhibiting fluids on a propeller
blade; naca-tn-727; September 1939
- Duschik, Frank; Wind-tunnel
investigation of an N.A.C.A. 23021 airfoil with two arrangements of a
40-percent-chord slotted flap; naca-tn-728; September 1939
- Kline, Gordon M
(National Bureau of Standards) Schiefer, Herbert F (National Bureau of
Standards); An instrument
for estimating tautness of doped fabrics on aircraft; naca-tn-729;
September 1939
- Bamber, M J House, R G;
Wind-tunnel
investigation of effect of yawing on lateral-stability characteristics II :
rectangular N.A.C.A. 23012 wing with a circular fuselage; naca-tn-730;
September 1939
- Donely, Philip
Shufflebarger, C C; Tests
in the gust tunnel of a model of the XBM-1 airplane; naca-tn-731; October
1939
- Sherman, Albert; A simple method
of obtaining span load distributors; naca-tn-732; October 1939
- Nile, Alfred S
(Stanford University); Experimental
study of torsional column failure; naca-tn-733; October 1939
- Street, William G Ames,
Milton B; Pressure-distribution
investigation of an N.A.C.A. 0009 airfoil with a 50-percent-chord plain flap
and three tabs; naca-tn-734; November 1939
- Troller, TH (Daniel
Guggenheim Airship Institute) Rokus, F (Daniel Guggenheim Airship Institute);
Pressure-distribution
measurements on a tapered wing with a partial-span split flap in curved
flight; naca-tn-735; November 1939
- Mutchler, Willard
(National Bureau of Standards) Galvin, W G (National Bureau of Standards); Tidewater and
weather-exposure tests on metals used in aircraft; naca-tn-736; November
1939
- Weller, R Bussey, J K;
Photoelastic
analysis of three-dimensional stress systems using scattered light;
naca-tn-737; November 1939
- Kuhn, Paul; A
recurrence formula for shear-lag problems; naca-tn-739; December
1939
- Dumont, C (Aluminum
Company of America); Stress
concentration around an open circular hole in a plate subjected to bending
normal to the plane of the plate; naca-tn-740; December 1939
- Bailey, F J , Jr
Gustafon, F B; Observations
in flight of the region of stalled flow over the blades of an autogiro
rotor; naca-tn-741; December 1939
- Rokus, Frank G (Daniel
Guggenheim Airship Institute); Pressure-distribution
measurements on a rectangular wing with a partial-span split flap in curved
flight; naca-tn-742; December 1939
- Stowell, Elbridge Z
Lundquist, Eugene E; Local
instability of columns with I-, Z-, channel, and rectangular-tube
sections; naca-tn-743; December 1939
- Wenzinger, Carl J
Harris , Thomas A; Wind-tunnel
investigation of an NACA 23012 airfoil with various arrangements of slotted
flaps; naca-report-664; 1939
- Schey, Oscar W Pinkel,
Benjamin Ellerbrock, Herman H , Jr; Correction
of temperatures of air-cooled engine cylinders for variation in engine and
cooling conditions; naca-report-645; 1939
- Stack, John Lindsey, W
F Littell, Robert E; The
compressibility burble and the effect of compressibility on pressures and
forces acting on a airfoil; naca-report-646; 1939
- Goett, Harry J
Bullivant, W Kenneth; Tests
of NACA 0009, 0012, and 0018 airfoils in the full-scale tunnel;
naca-report-647; 1939
- Silverstein, Abe
Katzoff, S; Design charts
for predicting downwash angles and wake characteristics behind plain and
flapped wings; naca-report-648; 1939
- Aitchison, C S
Tuckerman, L B; The
pack method for compressive tests of thin specimens of materials used in
thin-wall structures; naca-report-649; 1939
- Biermann, David
Hartman, Edwin P; The
aerodynamic characteristics of six full-scale propellers having different
airfoil sections; naca-report-650; 1939
- Silverstein, Abe
Katzoff, S Bullivant, W Kenneth; Downwash
and wake behind plain and flapped airfoils; naca-report-651; 1939
- Schubauer, G B; Air flow in the
boundary layer of an elliptic cylinder; naca-report-652; 1939
- Lee, Dana W; A
study of air flow in an engine cylinder; naca-report-653; 1939
- Rockfeller, W C; General
airplane performance; naca-report-654; 1939
- Rothrock, A M Biermann,
Arnold E; The knocking
characteristics of fuels in relation to maximum permissible performance of
aircraft engines; naca-report-655; 1939
- Osgood, William R Holt,
Marshall; The column
strength of two extruded aluminum-alloy h-sections; naca-report-656;
1939
- Rothrock, A M Spencer,
R C; The
influence of directed air flow on combustion in spark-ignition engine;
naca-report-657; 1939
- Biermann, David HARTMAN
EDWIN P; Tests of two
full-scale propellers with different pitch distributions, at blade angles up
to 60 degrees; naca-report-658; 1939
- Kies, J A Quick, G W;
Effect of
service stress on impact resistance, x-ray diffraction patterns, and
microstructure of 25s aluminum alloy; naca-report-659; 1939
- Goett, Harry J; Experimental
investigation of the momentum method for determining profile drag;
naca-report-660; 1939
- Abbott, Ira H
Greenberg, Harry; Tests
in the variable-density wind tunnel of the NACA 23012 airfoil with plain and
split flaps; naca-report-661; 1939
- Stickle, George W; Design of NACA
cowlings for radial air-cooled engines; naca-report-662; 1939
- Mutchler, Willard; The effect of
continuous weathering on light metal alloys used in aircraft;
naca-report-663; 1939
- Person, Henry A
Anderson, Raymond F; Calculation
of the aerodynamic characteristics of tapered wings with partial-span
flaps; naca-report-665; 1939
- Johnson, Daniel P; Aircraft
rate-of-climb indicators; naca-report-666; 1939
- Bicknell, Joseph; Determination
of the profile drag of an airplane wing in flight at high Reynolds
numbers; naca-report-667; 1939
- Wenzinger, Carl J
Harris, Thomas A; Wind-tunnel
investigation of NACA 23012, 23021, and 23030 airfoils with various sizes of
split flap; naca-report-668; 1939
- Jacobs, Eastman N
Abbott, Ira H; Airfoil
section data obtained in the NACA variable-density tunnel as affected by
support interference and other corrections; naca-report-669; 1939
- Mcadam, D J Mebs, R W;
Tensile
elastic properties of 18:8 chromium-nickel steel as affected by plastic
deformation; naca-report-670; 1939
- Kaplan, Carl; A
theoretical study of the moment on a body in a compressible fluid;
naca-report-671; 1939
- Seidman, Oscar
Neihouse, A I; Free-spinning
wind-tunnel tests of a low-wing monoplane with systematic changes in wings and
tails IV : effect of center-of-gravity location; naca-report-672;
1939
- Silverstein, Abe
Joyner, Upshur T; Experimental
verification of the theory of oscillating airfoils; naca-report-673;
1939
- Brevoort, M J Joyner, U
T; Cooling
on the front of an air-cooled engine cylinder in a conventional engine
cowling; naca-report-674; 1939
- Goett, Harry J Reeder,
J P; Effects
of elevator nose shape, gap, balance, and tabs on the aerodynamic
characteristics of a horizontal tail surface; naca-report-675; 1939
- Ellerbrock, Herman H ,
Jr Biermann, Arnold E; Surface
heat-transfer coefficients of finned cylinders; naca-report-676;
1939
- Wenzinger, Carl J
Harris, Thomas A; Wind-tunnel
investigation of NACA 23012 airfoil with various arrangements of slotted
flaps; naca-report-677; 1939
- Sherman, Albert; Interference of
tail surfaces and wing and fuselage from tests of 17 combinations in the NACA
variable-density tunnel; naca-report-678; 1939
- Wenzinger, Carl J
Gauvain, Willikam E; Wind-tunnel
investigation of an NACA 23012 airfoil with a slotted flap and three types of
auxiliary flap; naca-report-679; 1939
- Mchugh, James G
Derring, Eldridge H; The
effect of nacelle-propeller diameter ratio on body interference and on
propeller and cooling characteristics; naca-report-680; 1939
- Sherman, Albert; Preliminary
report on the characteristics of the NACA 4400R series airfoils;
naca-wr-l-451; March 1939
- Turner, L I , Jr; Ground-cooling
and flight tests of an airplane equipped with a nose-blower engine
cowling; naca-wr-l-478; October 1939
- Mchugh, James G; Tests of
several model nacelle-propeller arrangements in front of a wing;
naca-wr-l-510; September 1939
- Pearson, Henry A; Acceleration,
stress, and deflection measurements on the XB-15 bomber in gusty air;
naca-wr-l-540; June 1939
- Ellerbrock, Herman H ,
Jr; Heat-transfer
tests of a steel cylinder barrel with aluminum fins; naca-wr-e-194; August
1939
- G. Sissingh; Contribution
to the Aerodynamics of Rotating-Wing Aircraft; naca-tm-921; December
1939
- Losch, F., Kramer, K.
N., Bock, G., Nikodemus, R.; Calculation
of the induced efficiency of heavily loaded propellers having infinite number
of blades; naca-tm-884; 1939
- Findeisen, W.; Meteorological-physical
limitations of icing in the atmosphere; naca-tm-885; 1939
- Gebelein, H.; Theory
of two-dimensional potential flow about arbitrary wing sections;
naca-tm-886; 1939
- Cicala, P.; Comparison
of theory with experiment in the phenomenon of wing flutter; naca-tm-887;
1939
- Ritz, L.; Ice
formation on wings; naca-tm-888; 1939
- Kuchemann, D.; Investigation
of the lift distribution over the separate wings of a biplane;
naca-tm-889; 1939
- Ruden, P.; Experiments
on a slotted wing; naca-tm-890; 1939
- Schmidt, Fritz A. F.;
Theoretical
and experimental study of ignition lag and engine knock; naca-tm-891;
1939
- Cremona, C.; Investigations
and tests in the towing basin at Guidonia; naca-tm-892; 1939
- Winter, H.; Contribution
to the theory of the heated duct radiator; naca-tm-893; 1939
- Vohrer, Eugen.; The way to
increased airplane engine power; naca-tm-894; 1939
- Ragazzi, Paolo.; The power of
aircraft engines at altitude; naca-tm-895; 1939
- Gothert, B.; The
drag of airplane radiators with special reference to air heating :comparison
of theory and experiment; naca-tm-896; 1939
- Langweiler, Heinz.; The
hydrodynamic theory of detonation; naca-tm-899; 1939
- Schmidt, Rudolf.; The effect of
the masses of the controls on the longitudinal stability with free elevator.
Part I; naca-tm-900; 1939
- Ferri, Antonio.; Investigations
and experiments in the Guidonia wind tunnel; naca-tm-901; 1939
- Betz, A., Flugge-Lotz,
I.; Design
of centrifugal impeller blades; naca-tm-902; 1939
- Mayer, Edwin.; Effect
of transition in cross-sectional shape on the development of the velocity and
pressure distribution of turbulent flow in pipes; naca-tm-903; 1939
- Barbre, R.; Stability
of rectangular plates with longitudinal or transverse stiffeners under uniform
compression; naca-tm-904; 1939
- Penzig, F.; Temperature-indicating
paints; naca-tm-905; 1939
- Hoerner, Sighard.; Forces and
moments on a yawed airfoil; naca-tm-906; 1939
- Hohenemser, K.; Dynamic
stability of a helicopter with hinged rotor blades; naca-tm-907;
1939
- Zeman, J.; Two-stroke-cycle
engines with unsymmetrical control diagram : supercharged engines;
naca-tm-908; 1939
- Betz, Albert.; The
theory of contra-vanes applied to the propeller; naca-tm-909; 1939
- Weinhart, H.; Knocking
in the Otto-cycle engine; naca-tm-911; 1939
- Muller, J.; Increase
of the specific load under tension, compression, and buckling of welded steel
tubes in airplane construction by suitable treatment of structural steel and
by proper design; naca-tm-912; 1939
- Kiel, Georg.; Measurement
of the true dynamic and static pressures in flight; naca-tm-913;
1939
- Zinner, Karl.; Engine
knock and combustion chamber form; naca-tm-914; 1939
- Schapitz, E., Feller,
H., Koller, H.; Experimental
and analytical investigation of a monocoque wing model loaded in bending;
naca-tm-915; 1939
- Peschard, Marcel.; Activation of
hydrocarbons and the octane number; naca-tm-916; 1939
- Walchner, O.; The
effect of compressibility on the pressure reading of a Prandtl pitot tube at
subsonic flow velocity; naca-tm-917; 1939
- Truscott, Starr.; The enlarged
N.A.C.A. tank, and some of its work; naca-tm-918; 1939
- ; Report
on ice formation on aircraft; naca-tm-919; 1939
- Franke, A., Weinig, F.;
The effect
of the slipstream on an airplane wing; naca-tm-920; 1939
- Pittoni, Mario.; The Breda wind
tunnel; naca-tm-922; 1939
- Wenger, Hermann.; Measurement of
the air-flow velocity in the cylinder of an airplane engine; naca-tm-923;
1939
- Allen, H. Julian; A Simplified
Method for the Calculation of Airfoil Pressure Distribution; naca-tn-708;
1939
- Bader, W.; Measurements
on a low-wing model in the rotating jet and comparison with flight
measurements; naca-tm-910; 1939
- Jones, Robert T; The unsteady
lift of a wing of finite aspect ratio; naca-report-681; 1940
- Neihouse, A I; The
aileron as an aid to recovery from the spin; naca-tn-776; September
1940
- Coleman, Robert P; Damping
formulas and experimental values of damping in flutter models;
naca-tn-751; February 1940
- Recant, I G; Wind-tunnel
investigation of an NACA 23030 airfoil with various arrangements of slotted
flaps; naca-tn-755; March 1940
- Rogowski, A R
(Massachusetts Institute of Technology) Bouchard, C L (Massachusetts Institute
of Technology) Fayatte Taylor, C (Massachusetts Institute of Technology); The effects of
piston-head shape, cylinder-head shape, and exhaust restriction, on the
performance of a piston-ported two-stroke cylinder; naca-tn-756; March
1940
- Pearson, Henry A; A study of
unsymmetrical-loading conditions; naca-tn-757; April 1940
- Donely, Philip Pierce,
Harold B Pepoon, Philip W; Measurements
and analysis of the motion of a Canard airplane model in gusts;
naca-tn-758; April 1940
- Howard, Walter B , Jr;
A full-scale
investigation of the effect of several factors on the shimmy of cantering
wheels; naca-tn-760; April 1940
- Ames, Milton B , Jr
Sears, Richard I; Pressure-distribution
investigation of an NACA 0009 airfoil with an 80-percent-chord plain flap and
three tabs; naca-tn-761; May 1940
- Ames, Milton B , Jr; Wind-tunnel
investigation of two airfoils with 25-percent-chord Gwinn and plain flaps;
naca-tn-763; May 1940
- Bailey, F J , Jr; Flight
investigation of control-stick vibration of the YG-1B autogiro;
naca-tn-764; June 1940
- Pinkel, Benjamin
Mangniello, Eugene J; A
method of measuring piston temperatures; naca-tn-765; June 1940
- Lee, Dana W; The
effects of engine speed and mixture temperature on the knocking
characteristics of several fuels; naca-tn-767; July 1940
- Rothrock, A M Biermann,
Arnold E; Correlation of
knocking characteristics of fuels in an engine having a hemispherical
combustion chamber; naca-tn-768; July 1940
- Seidman, Oscar Mcavoy,
William H; Spin tests of a
low-lying monoplane in flight and in the free-spinning wind tunnel;
naca-tn-769; July 1940
- Dumont, C (Aluminum
Company of America) Hill, H N (Aluminum Company of America); The
lateral stability of equal-flanged aluminum-alloy I-beams subjected to pure
bending; naca-tn-770; August 1940
- Gerrish, Harold C Voss,
Fred; Analysis of
cylinder-pressure-indicator diagrams showing effects of mixture strength and
spark timing; naca-tn-772; August 1940
- Hill, H N (Aluminum
Company of America); Chart
for critical compressive stress of flat rectangular plates; naca-tn-773;
August 1940
- Hasting, Charles E; Ionization in
the knock zone of an internal-combustion engine; naca-tn-774; September
1940
- Gracey, William; Measured
moments of inertia of 32 airplanes; naca-tn-780; October 1940
- Swanson, Robert S
Harris, Thomas A; Wind
tunnel tests of an NACA 23021 airfoil equipped with a slotted extensible and a
plain extensible flap; naca-tn-782; November 1940
- Jones, Alun R Rodert,
Lewis A; A
flight investigation of exhaust-heat de-icing; naca-tn-783; November
1940
- Winter, George (Cornell
University); Stress
distribution in and equivalent width of flanges of wide, thin-wall steel
beams; naca-tn-784; 1940
- Hoggard, H Page, Jr; Wind tunnel
investigation of fuselage stability in yaw with various arrangements of
fins; naca-tn-785; November 1940
- Upscon, Ralph H (Stout
Skycraft Corporation); Structural
tests of a stainless steel wing panel by hydrostatic loading; naca-tn-786;
November 1940
- Ku, P M (Massachusetts
Institute of Technology); Factors
affecting heat transfer in the internal-combustion engine; naca-tn-787;
December 1940
- Harmon, Hubert N; Drag
determination of the forward component of a tricycle landing gear;
naca-tn-788; December 1940
- Aitchison, C S
(National Bureau of Standards); Extension
of pack method for compressive tests; naca-tn-789; December 1940
- Paul, D A (Aluminum
Company of America) Moore, R L (Aluminum Company of America); Cyclic
stress-strain studies of metals in torsion; naca-tn-790; December
1940
- De Forest, A V
(Massachusetts Institute of Technology) Leaderman, H (Massachusetts Institute
of Technology); The
development of electrical strain gages; naca-tn-744; 1940
- Donely, Philip
Shufflebarger, C C; Tests
of a gust-alleviating flap in the gust tunnel; naca-tn-745; 1940
- Burgess, C P (Bureau of
Aeronautics, Navy Department); The
frequencies of cantilever wings in beam and torsional vibrations;
naca-tn-746; 1940
- London, Albert
(National Bureau of Standards); Principles,
practices, and progress of noise reduction in airplanes; naca-tn-748;
1940
- Ward, Kenneth E; A new method of
studying the flow of the water along the bottom of a model of a flying-boat
hull; naca-tn-749; February 1940
- Reissner, Hans (Armour
Institute of Technology); A
generalized vortex theory of the screw propeller and its application;
naca-tn-750; February 1940
- Klenperer, W B (The
Soaring Society of America, Inc); Measurement
of the forces acting on gliders in towed flight; naca-tn-753; February
1940
- Rodert, Lewis A; An
investigation of the prevention of ice on the airplane windshield;
naca-tn-754; March 1940
- Joyner, Upshur T; Mathematical
analysis of aircraft intercooler design; naca-tn-781; October 1940
- Fiock, Ernest F Marvin,
Charles F , Jr Caldwell, Frank R Roeder, Carl H; Flame
speeds and energy considerations for explosions in a spherical bomb;
naca-report-682; 1940
- Pinkel, Benjamin
Ellerbrock, Herman H , Jr; Correlation
of cooling data from an air-cooled cylinder and several multicylinder
engines; naca-report-683; 1940
- Hartman, Erwin P
Biermann, David; Static
thrust and power characteristics of six full-scale propellers;
naca-report-684; 1940
- Theodorsen, Theodore
Garrick, I E; Mechanism
of flutter.a theoretical and experimental investigation of the flutter
problem; naca-report-685; 1940
- Kantrowitz, Arthur; Stability of
castering wheels for aircraft landing gears; naca-report-686; 1940
- Stickle, George W
Naiman, Irven Crigler, John L; Effect
of exit-slot position and opening on the available cooling pressure for NACA
nose-slot cowlings; naca-report-687; 1940
- Silverstein, Abe
Katzoff, S; Aerodynamic
characteristics of horizontal tail surfaces; naca-report-688; 1940
- Wenzinger, Carl J
Harris, Thomas A; Preliminary
wind-tunnel investigation of an NACA 23012 airfoil with various arrangements
of venetian-blind flaps; naca-report-689; 1940
- Katzoff, S; Longitudinal
stability and control with special reference to slipstream effects;
naca-report-690; 1940
- Seidman, Oscar
Neihouse, A I; Free-spinning
wind-tunnel tests of a low-wing monoplane with systematic changes in wings and
tails V : effect of airplane relative density; naca-report-691;
1940
- Donely, Philip; Effective gust
structure at low altitudes as determined from the reactions of an
airplane; naca-report-692; 1940
- Imlay, Frederick H; A theoretical
study of lateral stability with an automatic pilot; naca-report-693;
1940
- Diehl, Walter S; The application
of basic data on planing surfaces to the design of flying-boat hulls;
naca-report-694; 1940
- Wetmore, J W Turner, L
I , Jr; Determination
of ground effect from tests of a glider in towed flight; naca-report-695;
1940
- Mcadam, D J Mebs, R W;
Tensile
elastic properties of typical stainless steels and nonferrous metals as
affected by plastic deformation and by heat treatment; naca-report-696;
1940
- Kuhn, Paul; Investigations
on the incompletely developed plane diagonal-tension field;
naca-report-697; 1940
- Manganiello, Eugene J;
Piston
temperatures in an air-cooled engine for various operating conditions;
naca-report-698; 1940
- Taylor, E S Leary, W A
Diver, J R; Effect of
fuel-air ratio, inlet temperature, and exhaust pressure on detonation;
naca-report-699; 1940
- Soule, H A; Preliminary
investigation of the flying qualities of airplanes; naca-report-700;
1940
- Brueggeman, W C Roop,
Frederick C; Mechanical
properties of flush-riveted joints; naca-report-701; 1940
- Olson, R E Allison, J
M; The
calculated effect of various hydrodynamic and aerodynamic factors on the
take-off of a large flying boat; naca-report-702; 1940
- Soule, H A Anderson, R
F; Design
charts relating to the stalling of tapered wings; naca-report-703;
1940
- Purser, Paul E; Wind-tunnel
investigation of an NACA 23012 airfoil with two sizes of balanced split
flap; naca-wr-l-441; November 1940
- Baals, Donald D; Wind tunnel
tests of a submerged-engine fuselage design; naca-wr-l-485; October
1940
- Von Doenhoff, Albert E;
Investigation
of the boundary layer about a symmetrical airfoil in a wind tunnel of low
turbulence; naca-wr-l-507; August 1940
- Draley, Eugene C; High-speed drag
tests of several fuselage shapes in combination with a wing;
naca-wr-l-542; August 1940
- Ellerbrock, Herman H ,
Jr; Heat-transfer
tests of two steel cylinder barrels with aluminum fins manufactured by factory
production method; naca-wr-e-195; August 1940
- Ellerbrock, Herman H ,
Jr; Heat
transfer tests of a steel cylinder barrel with aluminum fins with improved
bonding between steel barrel and aluminum base; naca-wr-e-196; July
1940
- Mann, Alvin H; Heat-transfer
tests of a steel cylinder barrel with aluminum fins of optimum
proportions; naca-wr-e-204; November 1940
- Ames, Milton B., Sears,
Richard I.; Pressure-distribution
investigation on an NACA 0009 airfoil with a 30-percent-chord plain flap and
three tabs; naca-tn-759; 1940
- Lee, Dana W.; A
study of the air movement in two aircraft-engine cylinders; naca-tn-766;
1940
- Pass, H. R.; Analysis
of wind-tunnel data on directional stability and control; naca-tn-775;
1940
- Thompson, F. L.,
Gilruth, R. R.; Notes
on the stalling of vertical tail surfaces and on fin design; naca-tn-778;
1940
- Schrenk, O.; A
Simple approximation method for obtaining the spanwise lift distribution;
naca-tm-948; 1940
- Dearborn, C. H.,
Silverstein, Abe.; Drag
Analysis of Single-Engine Military Airplanes Tested in the NACA Full-Scale
Wind Tunnel; naca-wr-l-489; 1940
- Bullivant, W Kenneth;
Tests of the
NACA 0025 and 0035 airfoils in the full-scale wind tunnel;
naca-report-708; 1941
- Holt, Marshall
(Aluminum Company of America); The
effect of methods of testing on the ultimate loads supported by stiffened flat
sheet panels under edge compression; naca-tn-811; June 1941
- Pepper, Perry A (New
York University); Minimum
induced drag in wing-fuselage interference; naca-tn-812; September
1941
- Turner, L I , Jr
Bierman, David Boothy, W B; Cooling
effects of an airplane equipped with an NACA cowling and a wing-duct cooling
system; naca-tn-813; June 1941
- Bamber, Millard J; Effects of some
present-day airplane design trends on requirements for lateral stability;
naca-tn-814; June 1941
- Ellerbrock, Herman H ,
Jr Bullock, Robert O; Cooling
and performance tests of a Continental A-75 engine; naca-tn-816; July
1941
- Jones, Robert T; Correction of
the lifting-line theory for the effect of the chord; naca-tn-817;
1941
- Mebs, R W (National
Bureau of Standards) Mcadams, D J (National Bureau of Standards); The
tensile elastic properties at low temperatures of 18:8 Cr-Ni steel as affected
by heat treatment and slight plastic deformation; naca-tn-818; July
1941
- Paul, D A (Aluminum
Company of America.) Howell, F M (Aluminum Company of America) Grieshaber, H E
(Aluminum Company of America); Comparison
of stress-strain curves obtained by single-thickness and pack methods;
naca-tn-819; August 1941
- Corson, Blake W; The
aerodynamics of a wind-tunnel fan; naca-tn-820; 1941
- Moore, R L (Aluminum
Company of America); Some
comparative tests of plain and alclad 24s-t sheet; naca-tn-821; August
1941
- Lesley, E P (Stanford
University); Tandem air
propellers - II; naca-tn-822; August 1941
- Hutton, J O (University
of Maryland); Combined
beam-column stresses of aluminum-alloy channel sections; naca-tn-824;
September 1941
- Recant, Isadore G
Wallace, Arthur R; Wind-tunnel
investigation of effect of yaw on lateral-stability characteristics III :
symmetrically tapered wing at various positions on circular fuselage with and
without a vertical tail; naca-tn-825; September 1941
- Howell, F M (Aluminum
Company of America); Variation
of properties throughout cross section of two extruded shapes;
naca-tn-826; September 1941
- Driggs, H I (Navy
Department); Analytical
determination of control system pulley-axis angles; naca-tn-827; September
1941
- Pearson, H A Garvin, J
B; Velocity
gained and altitude lost in recoveries from inclined flight paths;
naca-tn-829; October 1941
- Peterson, John B
(National Bureau of Standards); Damping
characteristics of dashpots; naca-tn-830; 1941
- Rea, James Buchanan
(Massachusetts Institute of Technology); A
method of determining the equilibrium performance and the stability of an
engine equipped with an exhaust turbosupercharger; naca-tn-831; November
1941
- Pollard, R E (National
Bureau of Standards) Reinhart, Fred M (National Bureau of Standards); Relief
of residual stress in streamline tie rods by heat treatment; naca-tn-832;
November 1941
- Knight, Montgomery
(Georgia School of Technology) Hegner, Ralph A (Georgia School of Technology);
Analysis of
ground effect on the lifting airscrew; naca-tn-835; December 1941
- Olson, Roland E Lina,
Lindsay J; Hydrodynamic
tests of a 1/10-size model of the hull of the Latecoere 521 flying boat : NACA
model 83; naca-tn-836; December 1941
- Jones, Robert; Notes
on the stability and control of tailless airplanes; naca-tn-837;
1941
- Holt, Marshall
(Aluminum Company of America); Tests
on stiffened circular cylinders; naca-tn-800; March 1941
- Wenzinger, Carl J
Bowen, John D; Tests
of round and flat spoilers on a tapered wing in the NACA 19-foot pressure wind
tunnel; naca-tn-801; March 1941
- Rhode, Richard V; Some effects of
rainfall on flight of airplanes and on instrument indications;
naca-tn-803; April 1941
- Roark, Raymond J
(University of Wisconsin); Stresses
and deflections in thin shells and curved plates due to concentrated and
variously distributed loading; naca-tn-806; May 1941
- Donlan, Charles C; Spin tests of
two models of a low-wing monoplane to investigate scale effect in the model
test range; naca-tn-807; May 1941
- Lowry, John G; Wind-tunnel
investigation of an NACA 23012 airfoil with several arrangements of slotted
flaps with extended lips; naca-tn-808; 1941
- Imlay, Frederick H; The theoretical
lateral motions of an automatically controlled airplane subjected to a yawing
moment disturbance; naca-tn-809; June 1941
- Shortal, Joseph A
Osterbout, Clayton J; Preliminary
stability and control tests in the NACA free-flight wind tunnel and
correlation with flight tests; naca-tn-810; June 1941
- Newell, Joseph S
(Massachusetts Institute of Technology) Reissner, Eric (Massachusetts
Institute of Technology); Shear
lag in corrugated sheets used for the chord member of a box beam;
naca-tn-791; 1941
- Stickley, G W (Aluminum
Company of America); Effect
of alternately high and low repeated stresses upon the fatigue strength of
25S-T aluminum alloy; naca-tn-792; 1941
- Templin, R L (Aluminum
Company of America) Howell, F M (Aluminum Company of America) Hartmann, E C
(Aluminum Company of America); The
compressive yield strength of extruded shapes of 24st aluminum alloy;
naca-tn-793; 1941
- Buck, Richard S (Pratt
& Whitney Aircraft); Two-stage
supercharging; naca-tn-794; February 1941
- Wasielewski, Eugene W
King, J Austin; Effect
of several supercharger control methods on engine performance;
naca-tn-795; February 1941
- Ames, Milton B Sears,
Richard I; Determination
of control-surface characteristics from NACA plain-flap and tab data;
naca-tn-796; 1941
- KATZOFF S Mutterperl,
William; The
end-plate effect of a horizontal-tail surface on vertical tail surface;
naca-tn-797; February 1941
- Hill, H N (Aluminum
Company of America); Compression
tests of some 17S-T aluminum-alloy specimens of I cross section;
naca-tn-798; March 1941
- Rodert, Lewis A; The effects of
aerodynamic heating on ice formations on airplane propellers; naca-tn-799;
March 1941
- Shufflebarger, C C; Tests of a
gust-alleviating wing in the gust tunnel; naca-tn-802; April 1941
- Recant, Isidore G
Wallace, Arthur R; Wind-tunnel
investigation of the effect of vertical position of the wing on the side flow
in the region of the vertical tail; naca-tn-804; April 1941
- Roop, Frederick C
(National Bureau of Standards); Effect
of aging on mechanical properties of aluminum-alloy rivets; naca-tn-805;
April 1941
- Recant, I G; Plate
method of ground representation for wind-tunnel determination of elevator
effectiveness in landing; naca-tn-823; September 1941
- Kuhn, Paul; Ultimate
stresses developed by 24S-T sheet in incomplete diagonal tension;
naca-tn-833; December 1941
- Rothrock, A M Spencer,
R C Miller, Cearcy D; A
high-speed motion-picture study of normal combustion, knock and preignition in
a spark-ignition engines; naca-report-704; 1941
- House, Rufus O Wallace,
Arthur R; Wind-tunnel
investigation of effect of interference on lateral-stability characteristics
of four NACA 23012 wings, an elliptical and a circular fuselage and vertical
fins; naca-report-705; 1941
- Wenzinger, Carl J
Rogallo, Francis M; Wind-tunnel
investigation of spoiler, deflector, and slot lateral-control devices on wings
with full-span split and slotted flaps; naca-report-706; 1941
- Gracey, William; The
additional-mass effect of plates as determined by experiments;
naca-report-707; 1941
- Jones, Robert T Cohen,
Doris; An
analysis of the stability of an airplane with free controls;
naca-report-709; 1941
- Spencer, R C; Preignition
characteristics of several fuels under simulated engine conditions;
naca-report-710; 1941
- Gilruth, R R White, M
D; Analysis
and prediction of longitudinal stability of airplanes; naca-report-711;
1941
- Stickle, George W
Crigler, John L; Propeller
analysis from experimental data; naca-report-712; 1941
- Rogallo, F M; Internal-flow
systems for aircraft; naca-report-713; 1941
- Dutee, Francis J; An apparatus
for measuring rates of discharge of a fuel-injection system;
naca-report-714; 1941
- Gilruth, R R Turner, W
N; Lateral
control required for satisfactory flying qualities based on flight tests of
numerous airplanes; naca-report-715; 1941
- Bailey, F J , Jr; A simplified
theoretical method of determining the characteristics of a lifting rotor in
forward flight; naca-report-716; 1941
- Waldron, C D; Flow
coefficients of monosleeve valves; naca-report-717; 1941
- Harris, Thomas A Lowry,
John G; Pressure
distribution over NACA 23012 airfoil with a slotted and a split flap;
naca-report-718; 1941
- Brevoort, M J Joyner, U
T; The
problem of cooling an air-cooled cylinder on an aircraft engine;
naca-report-719; 1941
- Stickle, George W
Naiman, Irven Crigler, John L; Pressure
available for cooling with cowling flaps; naca-report-720; 1941
- Ames, Milton B Sears,
Richard I; Determination
of control-surface characteristics from NACA plain-flap and tab data;
naca-report-721; 1941
- Jones, Robert T Cohen,
Doris; A
graphical method of determining pressure distribution in two-dimensional
flow; naca-report-722; 1941
- Harris, Thomas A
Recant, Isidore G; Wind-tunnel
investigation of NACA 23012, 23021, and 23030 airfoils equipped with
40-percent-chord double slotted flaps; naca-report-723; 1941
- Roop, Frederick C; Effect of aging
on mechanical properties of aluminum-alloy rivets; naca-report-724;
1941
- Stickle, George W
Crigler, John L Naiman, Irven; Effect
of body nose shape on the propulsive efficiency of a propeller;
naca-report-725; 1941
- Biermann, Arnold E
Ellerbrock, Herman H , Jr; The
design of fins for air-cooled cylinders; naca-report-726; 1941
- Voss, Fred; Design
of nozzles for the individual cylinder exhaust jet propulsion system;
naca-report-765; April 1941
- Ames, Milton B; Wind-tunnel
investigation of control-surface characteristics III : a small aerodynamic
balance of various nose shapes used with a 30-percent-chord flap on an NACA
0009 airfoil; naca-wr-l-301; August 1941
- Eastman, Donald R; Wind-tunnel
investigation of control-surface characteristics IV : a medium aerodynamic
balance of various nose shapes used with a 30-percent-chord flap on an NACA
0009 airfoil; naca-wr-l-355; September 1941
- Sears, Richard I; Wind-tunnel
investigation of control-surface characteristics I : effect of gap on the
aerodynamic characteristics of an NACA 0009 airfoil with a 30-percent-chord
plain flap; naca-wr-l-377; June 1941
- Hoggard, H Page, Jr; Wind-tunnel
investigation of control-surface characteristics II : a large aerodynamic
balance of various nose shapes with a 30-percent-chord flap on an NACA 0009
airfoil; naca-wr-l-380; August 1941
- Garvin, J B; An
analytical study of wing and tail loads associated with an elevator
deflection; naca-wr-l-443; June 1941
- Turner, Thomas R; Wind-tunnel
investigation of perforated split flaps for use as dive brakes on a
rectangular NACA 23012 airfoil; naca-wr-l-445; July 1941
- Schuldenfrei, Marvin J;
Wind-tunnel
investigation of an NACA 23021 airfoil with two sizes of balanced split
flaps; naca-wr-l-449; February 1941
- Olson, Roland E; Tank tests of a
1/5 full-size dynamically similar model of the Army OA-9 amphibian with
motor-driven propellers : NACA model 117; naca-wr-l-475; December
1941
- Conway, Robert N; The selection
of propellers for high thrust at low airspeed; naca-wr-l-483; October
1941
- Tifford, Arthur N; Internally
finned honeycomb radiators; naca-wr-l-492; December 1941
- Mastrocola, Nicholas;
Static
characteristics of Hamilton Standard propellers having Clark Y and NACA 16
series blade sections; naca-wr-l-529; August 1941
- Gray, W H; Wind-tunnel
tests of two Hamilton Standard propellers embodying Clark Y and NACA 16 series
blade sections; naca-wr-l-530; August 1941
- Platt, Robert C; A flight
investigation of the boundary-layer characteristics and profile drag of the
NACA 35-215 laminar-flow airfoil at high Reynolds numbers; naca-wr-l-532;
May 1941
- Lowry, John G; Power-off
wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane;
naca-wr-l-543; June 1941
- Krsek, Alois, Jr; Investigation
of naphthalene as a possible aircraft fuel; naca-wr-e-168; August
1941
- Eckert, E., Weise, W.;
The
temperature of unheated bodies in a high-speed gas stream; naca-tm-1000;
1941
- Goett, Harry J., Pass,
H. R.; Effect of
propeller operation on the pitching moments of single-engine monoplanes;
naca-wr-l-761; 1941
- Pierce, Harold B; Dynamic stress
calculations for two airplanes in various gusts; naca-wr-l-484; September
1941
- Miller, Cearcy D; A study by
high-speed photography of combustion and knock in a spark-ignition engine;
naca-report-727; 1942
- Kaplan, Carl; On
the use of residue theory for treating the subsonic flow of a compressible
fluid; naca-report-728; 1942
- Bell, E Barton; Test of
single-stage axial-flow fan; naca-report-729; 1942
- Robinson, Russell G
Delano, James B; An
investigation of the drag of windshields in the 8-foot high-speed wind
tunnel; naca-report-730; 1942
- Jones, Robert T Cohen,
Doris; Determination
of optimum plan forms for control surfaces; naca-report-731; 1942
- Harris, Thomas A Lowry,
John G; Pressure
distribution over an NACA 23012 airfoil with a fixed slot and a slotted
flap; naca-report-732; 1942
- Lundquist, Eugene E
Stowell, Elbridge Z; Critical
compressive stress for flat rectangular plates supported along all edges and
elastically restrained against rotation along the unloaded edges;
naca-report-733; 1942
- Lundquist, Eugene E
Stowell, Elbridge Z; Critical
compressive stress for outstanding flanges; naca-report-734; 1942
- Lundquist, Eugene E
Stowell, Elbridge Z; Restraint
provided a flat rectangular plate by a sturdy stiffener along an edge of the
plate; naca-report-735; 1942
- Theodorsen, Theodore
Garrick, I E; Nonstationary
flow about a wing-aileron-tab combination including aerodynamic balance;
naca-report-736; 1942
- Levy, Samuel; Bending
of rectangular plates with large deflections; naca-report-737; 1942
- Katzoff, S Sweberg,
Harold H; Ground effect
on downwash angles and wake location; naca-report-738; 1942
- Kuhn, Paul Chiarito,
Patrick T; Shear lag in
box beams methods of analysis and experimental investigations;
naca-report-739; 1942
- Levy, Samuel; Square
plate with clamped edges under normal pressure producing large
deflections; naca-report-740; 1942
- Theodorsen, Theodore
Garrick, I E; Flutter
calculations in three degrees of freedom; naca-report-741; 1942
- Rogallo, F M Spano,
Bartholomew S; Wind-tunnel
investigation of an NACA 23012 airfoil with 30 percent-chord venetian-blind
flaps; naca-report-742; 1942
- Harris, Thomas A
Recant, Isidore G; Investigation
in the 7- by 10-foot wind tunnel of ducts for cooling radiators within an
airplane wing; naca-report-743; 1942
- Mcpherson, Albert E
Ramberg, Walter Levy, Samuel; Normal-pressure
tests of circular plates with clamped edges; naca-report-744; 1942
- Robinson, Russell G
Becker, John V; High-speed
tests of conventional radial-engine cowlings; naca-report-745; 1942
- Silverstein, Abe
Wilson, Herbert A , Jr; Drag
and propulsive characteristics of air-cooled engine-nacelle installations for
large airplane; naca-report-746; 1942
- Biermann, David
Hartman, Edwin P; Wind-tunnel
tests of four- and six-blade single- and dual-rotating tractor propellers;
naca-report-747; 1942
- Ramberg, Walter
Mcpherson, Albert E Levy, Samuel; Normal-pressure
tests of rectangular plates; naca-report-748; 1942
- Biermann, David Conway,
Robert N; Propeller
charts for the determination of the rotational speed for the maximum ratio of
the propulsive efficiency to the specific fuel consumption;
naca-report-749; 1942
- Becker, John V LEONARD
LLOYD H; High-speed
tests of a model twin-engine low-wing transport airplane; naca-report-750;
1942
- Diehl, Walter S; The mean
aerodynamic chord and the aerodynamic center of a tapered wing;
naca-report-751; 1942
- Mccullough, George B;
A method for
determining the rate of heat transfer from a wing or streamline body;
naca-report-830; December 1942
- Schweitzer, P H (The
Pennsylvania State College) Deluca, Frank, Jr (The Pennsylvania State
College); The tracer gas
method of determining the charging efficiency of two-stroke-cycle diesel
engines; naca-tn-838; 1942
- Forbes, J E
(Massachusetts Institute of Technology) Taylor, E S (Massachusetts Institute
of Technology); Rise
in temperature of the charge in its passage through the inlet valve and port
of an air-cooled aircraft engine cylinder; naca-tn-839; 1942
- Atchison, C S (National
Bureau of Standards) Miller, James A (National Bureau of Standards); Tensile
and pack compressive tests of some sheets of aluminum alloy, 1025 carbon
steel, and chromium-nickel steel; naca-tn-840; February 1942
- Weller, R (State
College of Washington) Hiddlehurst, D J (State College of Washington) Steiner,
R (State College of Washington); The
photoviscous properties of fluids; naca-tn-841; February 1942
- Mutchler, Willard
(National Bureau of Standards) Galvin, W G (National Bureau of Standards); Tidewater and
weather-exposure tests on metals used in aircraft II.; naca-tn-842;
February 1942
- Hartmann, E C (Aluminum
Company of America) Sharp, W H (Aluminum Company of America); A
summary of results of various investigations of the mechanical properties of
aluminum alloys at low temperatures; naca-tn-843; May 1942
- Klemperer, W B
(Southern California Soaring Association, Inc); Investigation
of the forces acting on gliders in automobile-pulley-winch and airplane towed
flight; naca-tn-844; March 1942
- Lundquist, Eugene E
Schwartz, Edward B; A
study of general instability of box beams with truss-type ribs;
naca-tn-866; November 1942
- Moore, R L (Aluminum
Company of America) Holt, Marshall (Aluminum Company of America); Beam
and torsion tests of aluminum-alloy 615-T tubing; naca-tn-867; October
1942
- Clark, Donald S
(California Institute of Technology); The
influence of impact velocity on the tensile characteristics of some aircraft
metals and alloys; naca-tn-868; October 1942
- HARTMANN E C (Aluminum
Company of America) Stickley, G W (Aluminum Company of America); Summary
of results of tests made by aluminum research laboratories of spot-welded
joints and structural elements; naca-tn-869; November 1942
- Ruffner, Benjamin F
(Oregon State College, Corvallis, Oreg); Stress
analysis of monocoque fuselage bulkheads by the photoelastic method;
naca-tn-870; December 1942
- Niles, Alfred S
(Stanford University, California) Viscovich, Steven J (Stanford University,
California); Stability of
elastically supported columns; naca-tn-871; March 23, 1942
- Levy, Samuel (National
Bureau of Standards, Washington, D.C) Mcpherson, Albert E (National Bureau of
Standards, Washington, D.C) Ramberg, Walter (National Bureau of Standards,
Washington D.C); Torsion
tests of a monocoque box; naca-tn-872; November 1942
- Mcpherson, Albert E
(National Bureau of Standards) Ramberg, Walter (National Bureau of Standards)
Levy, Samuel (National Bureau of Standards); Bending
tests of a monocoque box; naca-tn-873; 1942
- Von Hippel, Arthur R
(Massachusetts Institute of Technology) Dietz, A G H (Massachusetts Institute
of Technology); Curing
of resin-wood combinations by high-frequency heating; naca-tn-874;
December 1942
- Klemperer, W B (Douglas
Aircraft Company, Inc); A
rosette strain computer; naca-tn-875; December 1942
- Wildhack, W A (National
Bureau of Standards, Washington, D.C) Goerke, V H (National Bureau of
Standards, Washington, D.C); The
limiting useful deflections of corrugated metal diaphragms; naca-tn-876;
December 1942
- Paul, D A (Aluminum
Company of America, New Kensington, Penna); An
exploration of the longitudinal tensile and compressive properties throughout
an extruded shape of 24S-T aluminum alloy; naca-tn-877; December
1942
- Katzoff, S Sweberg,
Harold H; Ground effect
on downwash angles and wake location; naca-tn-845; May 1942
- Levy, Samuel (National
Bureau of Standards); Square
plate with clamped edges under normal pressure producing large
deflections; naca-tn-847; 1942
- Mcpherson, Albert E
(National Bureau of Standards) Ramberg, Walter (National Bureau of Standards)
Levy, Samuel (National Bureau of Standards); Normal-pressure
tests of circular plates with clamped edges; naca-tn-848; 1942
- Ramberg, Walter
(National Bureau of Standards) Mcpherson, Albert E (National Bureau of
Standards) Levy, Samuel (National Bureau of Standards); Normal-pressure
tests of rectangular plates; naca-tn-849; June 1942
- Workman, E J
(University of New Mexico) Holzer, R E (University of New Mexico); A
preliminary investigation of the electrical structure of thunderstorms;
naca-tn-850; July 1942
- Lundquist, Eugene E
Stowell, Elbridge Z; Strength
tests of thin-walled elliptic duralumin cylinders in pure bending and in
combined pure bending and torsion; naca-tn-851; June 1942
- Dolan, Thomas J
(University of Illinois, Urbana, Illinois); Effects
of range of stress and of special notches on fatigue properties of aluminum
alloys suitable for airplane propellers; naca-tn-852; June 1942
- Levy, Samuel (National
Bureau of Standards) Greenman, Samuel (National Bureau of Standards); Bending
with large deflection of a clamped rectangular plate with length-width ratio
of 1.5 under normal pressure; naca-tn-853; April 14, 1942
- Cohen, Doris; A
method for determining the camber and twist of a surface to support a given
distribution of lift; naca-tn-855; August 1942
- Ramberg, Walter Levy,
Samuel Mcpherson, Albert E; Effect
of rivet and spot-weld spacing on the strength of axially loaded
sheet-stringer panels; naca-tn-856; August 1942
- STRICKLEY G W (Aluminum
Company of America); Improvement
of fatigue life of an aluminum alloy by overstressing; naca-tn-857; August
1942
- Truscott, Starr Dawson,
John R; A
comparison of the results from general tank tests of 1/6- and 1/12-full-size
models of the British Singapore IIC flying boat; naca-tn-858; August
1942
- Dunn, Louis G
(California Institute of Technology, Pasadena, Calif); On
the distribution of stress in a thin plate elastically supported along two
edges at loads beyond the stability limit; naca-tn-859; October
1942
- Lundquist, Eugene E
Schwartz, Edward B; The
critical compression load for a universal testing machine when the specimen is
loaded through knife edges; naca-tn-860; September 1942
- Munger, Maurice
Wilsted, H D Mulcahy, B A; The
effect of valve cooling upon maximum permissible engine output as limited by
knock; naca-tn-861; September 1942
- Moore, R L (Aluminum
Company of America); An
investigation of the effectiveness of stiffeners on shear-resistant
plate-girder webs; naca-tn-862; September 1942
- Hootman, J A Jones, A
R; Results
of landing tests of various airplanes; naca-tn-863; September 1942
- Workman, E J
(University of New Mexico) Helzer, R E (University of New Mexico) Pelsor, G T
(University of New Mexico); The
electrical structure of thunderstorms; naca-tn-864; November 1942
- Hartmann, E C (Aluminum
Company of America) Stickley, G W (Aluminum Company of America); The
direct-stress fatigue strength of 17S-T aluminum alloy throughout the range
from 1/2 to 500,000,000 cycles of stress; naca-tn-865; September
1942
- Templin, R L (Aluminum
Company of America) Fogwell, J W (Aluminum Company of America); Design
of tools for press-countersinking or dimpling 0.040-inch-thick-24S-T
sheet; naca-tn-854; August 1942
- Smith, Norman F; Aerodynamic
tests of an M-31 bomb in the 8-foot high-speed tunnel; naca-wr-l-132;
August 25, 1942
- Sears, Richard I; Wind tunnel
investigation of control surface characteristics IX : some analytical
considerations and experimental test results for an internally balanced
flap; naca-wr-l-339; July 1942
- Hoggard, H Page, Jr; Wind tunnel
investigation of control-surface characteristics X : a 30-percent-chord plain
flap with straight contour on the NACA 0015 airfoil; naca-wr-l-366;
September 1942
- Ashworth, C Dixon; Tests in the
19-foot pressure tunnel of a 1/2.75-scale model of the F4U-1 airplane with
several balanced elevators, full-span flaps, and droppable gas tank;
naca-wr-l-440; October 1942
- Schuette, Evan H; Strength tests
of thin-wall truncated cones of circular section; naca-wr-l-442; December
1942
- Phillips, William H; A flight
investigation of short-period longitudinal oscillations of an airplane with
free elevator; naca-wr-l-444; May 1942
- Runckel, Jack F; The effect of
pitch on force and moment characteristics of full-scale propellers of five
solidities; naca-wr-l-446; June 1942
- Hoggard, H Page, Jr; Wind-tunnel
investigation of control-surface characteristics VII : a medium aerodynamic
balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015
airfoil; naca-wr-l-448; July 1942
- Underwood, W J; Notes on the
effects of trailing-edge shapes of low-drag airfoils on profile drag and the
trim and balance of control surfaces; naca-wr-l-450; March 1942
- Walker, Walter G; Summary of V-G
records taken on transport airplanes from 1932 to 1942; naca-wr-l-453;
July 1942
- Liddell, Robert B; Wind-tunnel
investigation of control-surface characteristics VI : a 30-percent-chord plain
flap on the NACA 0015 airfoil; naca-wr-l-454; June 1942
- Silverstein, Abe; Tests of
propeller-speed cooling blowers; naca-wr-l-455; July 1942
- Wright, Ray M; Investigation
of drag and pressure distribution of windshields at high speeds;
naca-wr-l-462; 1942
- Mattson, Axel T; Tests of a
large spherical turret and a modified turret on a typical bomber fuselage;
naca-wr-l-463; October 1942
- Fehlner, Leo F; A study of the
effect of adverse yawing moment on lateral maneuverability at a high lift
coefficient; naca-wr-l-465; September 1942
- Lowry, John G; Adjustment
of stick force by a nonlinear aileron-stick linkage; naca-wr-l-467;
November 1942
- Olson, Roland E; The
longitudinal stability of flying boats as determined by tests of models in the
NACA tank II : effect of variations in form of hull on longitudinal
stability; naca-wr-l-468; November 1942
- Pearson, H A; Condensation
trails : where they occur and what can be done about them; naca-wr-l-474;
September 1942
- Benson, James M; The porpoising
characteristics of a planing surface representing the forebody of a
flying-boat hull; naca-wr-l-479; May 1942
- Lowry, John G; Wind-tunnel
investigation of a plain aileron and a balanced aileron on a tapered wing with
full-span duplex flaps; naca-wr-l-481; July 1942
- Baals, Donald D; High-speed
tests of a ducted body with various air-outlet openings; naca-wr-l-486;
May 1942
- Knopf, George S; A method for
the design of cooling systems for aircraft power-plant installations;
naca-wr-l-491; March 1942
- Kuhn, Paul; The
influence of bulkhead spacing on bending stresses due to torsion;
naca-wr-l-501; May 1942
- Fedziuk, Henry A; High-speed
wind-tunnel tests of gun openings in the nose of the fuselage of a 1/4-scale
model; naca-wr-l-502; July 1942
- Wallace, Arthur R; Wind tunnel
investigation of effect of yaw on lateral-stability characteristics IV :
symmetrically tapered wing with a circular fuselage having a wedge-shaped rear
and a vertical tail; naca-wr-l-520; March 1942
- Gottlieb, Robert; Test data on
the shear strength of machine countersunk-riveted joints assembled by an NACA
flush-riveting procedure; naca-wr-l-523; December 1942
- Glodeck, Edward; Performance
characteristics of mixed-flow impeller and vaned diffuser with several
modifications; naca-wr-e-197; July 1942
- King, J Austin; Performance of
two-stage turbosupercharger using mixed-flow impellers; naca-wr-e-203;
October 1942
- Multhopp, R.; Aerodynamics
of the fuselage; naca-tm-1036; 1942
- Keune, F.; Two-dimensional
potential flow past an ordinary thick wing profile; naca-tm-1023;
1942
- Semenov, N. N.; Thermal theory
of combustion and explosion; naca-tm-1024; 1942
- Sokolik, A. S.; Self-ignition
and combustion of gases; naca-tm-1025; 1942
- Bleeker, W.; The
formation of ice on aircraft; naca-tm-1027; 1942
- Robitzsch, M.; The
icing of aircraft; naca-tm-1028; 1942
- Mohr, Ernst; The
navier-stokes stress principle for viscous fluids; naca-tm-1029;
1942
- Hantzsche, W., Wendt,
H.; The
compressible potential flow past elliptic symmetrical cylinders at zero angle
of attack and with no circulation; naca-tm-1030; 1942
- Blumrich, S.; Contribution
to the design of plywood shells; naca-tm-1031; 1942
- Fuchs, D.; Wind-tunnel
investigations of diving brakes; naca-tm-1033; 1942
- Ackeret, J., Keller, D.
C.; Aerodynamic
heat-power engine operating on a closed cycle; naca-tm-1034; 1942
- Steiglitz, A.; Control
of torsional vibrations by pendulum masses; naca-tm-1035; 1942
- Gillis, Clarence L; Wind-tunnel
investigation of control-surface characteristics VIII : a large aerodynamic
balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015
airfoil; naca-wr-l-378; July 1942
- Seidman, Oscar; Influence of
loading condition on piloting technique for spin recovery for pursuit
airplanes; naca-wr-l-461; June 1942
- N. N. Semenov; Thermal
Theory of Combustion and Explosion III. Theory of Normal Flame
Propagation; naca-tm-1026; 1942
- Jones, Robert T., Ames,
Milton B., Jr.; Wind-tunnel
investigation of control-surface characteristics V : the use of a beveled
trailing edge to reduce the hinge moment of a control surface;
naca-wr-l-464; 1942
- Recant, Isidore G.,
Swanson, Robert S.; Determination
of the stability and control characteristics of airplanes from tests of
powered models; naca-wr-l-710; 1942
- Levy, Samuel (National
Bureau of Standards) Krupen, Philip (National Bureau of Standards); Large-deflection
theory for end compression of long rectangular plates rigidly clamped along
two edges; naca-tn-884; 1943
- W. D. Kroll; Tables
of stiffness and carry-over factor for flat rectangular plates under
compression; naca-arr-3k27; November, 1943
- W. D. Kroll, Gordon P.
Fisher, George J. Heimrel; Charts
for calculation of the critical stress for local instability of columns with
I-, Z-, channel and rectangular-tube section; naca-arr-3k04; November,
1943
- Eugene E. Lundquist,
Elbridge Z. Stowell, Evan H. Schuette; Principles
of moment distribution applied to stability of structures composed of bars or
plates; naca-arr-3k06; November 1943
- Ribner, Herbert S; Propellers in
yaw; naca-report-820; December 1943
- Seliger, Victor
(Lockheed Aircraft Corporation); Effect
of rivet pitch upon the fatigue strength of single-row riveted joints of
0.025- to 0.025-inch 24S-T alclad; naca-tn-900; July 1943
- Moore, R L (Aluminum
Company of America) Wescoat, C (Aluminum Company of America); Bearing
strengths of some wrought-aluminum alloys; naca-tn-901; August 1943
- Lundquist, Eugene E
Rossman, Carl A Houbolt, John C; A
method for determining the column curve from tests of columns with equal
restraints against rotation on the ends; naca-tn-903; August 1943
- Sherwood, A W
(University of Maryland); The
strength of thin-wall cylinders of D cross section in combined pure bending
and torsion; naca-tn-904; September 1943
- (Author(s) Not
Available); Some
investigations of the general instability of stiffened metal cylinders I :
review of theory and bibliography; naca-tn-905; 1943
- (Author(s) Not
Available); Some
investigations of the general instability of stiffened metal cylinders II :
preliminary tests of wire-braced specimens and theoretical studies;
naca-tn-906; 1943
- (Author(s) Not
Available); Some
investigations of the general instability of stiffened metal cylinders III :
continuation of tests of wire-braced specimens and preliminary tests of
sheet-covered specimens; naca-tn-907; 1943
- (Author(s) Not
Available); Some
investigations of the general instability of stiffened metal cylinders IV :
continuation of tests of sheet-covered specimens and studies of the buckling
phenomena of unstiffened circular cylinders; naca-tn-908; 1943
- (Author(s) Not
Available); Some
investigations of the general instability of stiffened metal cylinders VII :
stiffened metal cylinders subjected to combined bending and torsion;
naca-tn-911; November 1943
- Aitchison, C S
(National Bureau of Standards) Miller, James A (National Bureau of Standards);
A subpress
for compressive tests; naca-tn-912; December 1943
- Aitchison, C S
(National Bureau of Standards) Miller, James A (National Bureau of Standards);
Tensile and
compressive tests of magnesium alloy J-1 sheet; naca-tn-913; December
1943
- Dolan, Thomas J
(University of Illinois); Certain
mechanical strength properties of aluminum alloys 25S-T and X76S-T;
naca-tn-914; October 1943
- Livengood, James C
(Massachusetts Institute of Technology) Stanitz, John D (Massachusetts
Institute of Technology); The
effect of inlet-valve design, size, and lift on the air capacity and output of
a four-stroke engine; naca-tn-915; November 1943
- Sharp, W H (Aluminum
Company of America); The
effect of the type of specimen on the shear strengths of driven rivets;
naca-tn-916; November 1943
- Donnell, L H (Chance
Vought Aircraft); The
stability of isotropic or orthotopic cylinders or flat or curved panels,
between and across stiffeners, with any edge conditions between hinged and
fixed, under any combination of compression and shear; naca-tn-918;
December 1943
- Rogowski, A R
(Massachusetts Institute of Technology) Taylor, C Fayette (Massachusetts
Institute of Technology); Part-throttle
operation and control of a piston-ported two-stroke cylinder; naca-tn-919;
November 1943
- Scott, Merit
(Pennsylvania State College, State College, PA) Weber, Robert L (Pennsylvania
State College, State College, PA); Requirements
for auxiliary stiffeners attached to panels under combined compression and
shear; naca-tn-921; September 16, 1943
- Kynoch, William
(University of Michigan, Ann Arbor, Mich) Patronsky, L A (University of
Michigan, Ann Arbor, Mich); Effect
of fillers and of mixing procedure on the strength of plastic materials;
naca-tn-878; 1943
- Moore, R L (Aluminum
Company of America, New Kensington, Penna); Torsional
strength of aluminum-alloy round tubing; naca-tn-879; 1943
- Weske, John R (Case
School of Applied Science); Methods
of measurement of high air velocities by the hot-wire method; naca-tn-880;
February 1943
- Weske, John R (Case
School of Applied Science); A
hot-wire circuit with very small time lag; naca-tn-881; February
1943
- Niles, Alfred S
(Stanford University, Calif); Tests
of flat panels with four types of stiffeners; naca-tn-882; 1943
- Holt, Marshall
(Aluminum Company of America); Tests
of aluminum-alloy stiffened-sheet specimens cut from an airplane wing;
naca-tn-883; 1943
- Moore, R L (Aluminum
Company of America) Paul, D A (Aluminum Company of America); Torsion
tests of 24S-T aluminum-alloy noncircular bar and tubing; naca-tn-885;
1943
- Mebs, R W (National
Bureau of Standards) Mcadam, D J , Jr (National Bureau of Standards); Torsional
elastic properties of 18:8 chromium-nickel steel as affected by plastic
deformation and by heat treatment; naca-tn-886; 1943
- Mcpherson, Albert E
(National Bureau of Standards); A
portable calibrator for dynamic strain gages; naca-tn-887; February
1943
- Hill, H N (Aluminum
Company of America); Torsion
of flanged members with cross sections restrained against warping;
naca-tn-888; March 1943
- Kies, J A (National
Bureau of Standards) Holshouser, W L (National Bureau of Standards); Effects
of prior fatigue-stressing of the impact resistance of chromium-molybdenum
aircraft steel; naca-tn-889; March 1943
- Delano, James B; Pressure
distribution on the fuselage of a midwing airplane model at high speeds;
naca-tn-890; February 1943
- Shih-I, Pai (California
Institute of Technology); Turbulent
flow between rotating cylinders; naca-tn-892; March 1943
- Hildebrand, Francis B
(Massachusetts Institute of Technology) Reissner, Eric (Massachusetts
Institute of Technology); Least-work
analysis of the problem of shear lag in box beams; naca-tn-893;
1943
- Hildebrand, Francis B
(Massachusetts Institute of Technology, Cambridge, Mass); The
exact solution of shear-lag problems in flat panels and box beams assumed
rigid in the transverse direction; naca-tn-894; 1943
- Levy, Samuel (National
Bureau of Standards); Large-deflection
theory of curved sheet; naca-tn-895; May 1943
- Osgood, William R
(National Bureau of Standards); Round
heat-treated chromium-molybdenum-steel tubing under combined loads;
naca-tn-896; July 1943
- Sharp, W H (Aluminum
Company of America) Moore, R L (Aluminum Company of America); Bearing
tests of magnesium-alloy sheet; naca-tn-897; June 1943
- Mcpherson, A E
(National Bureau of Standards); Adaptor
for measuring principal strains with Tuckerman strain gage; naca-tn-898;
1943
- Holt, M (Aluminum
Company of America); Column
strength of magnesium alloy AM-57S; naca-tn-899; July 1943
- Russell, H W (Battelle
Memorial Institute) Gillett, H W (Battelle Memorial Institute) Jackson, L R
(Battelle Memorial Institute) Foley, G M (Battelle Memorial Institute); The effect of
surface finish on the fatigue performance of certain propeller materials;
naca-tn-917; December 1943
- Moore, R L (Aluminum
Company of America) Wescoat, C (Aluminum Company of America); Bearing
strengths of bare and alclad XA75S-T and 24S-T81 aluminum alloy sheet;
naca-tn-920; December 1943
- Charters, Alex C , Jr
(California Institute of Technology); Transition
between laminar and turbulent flow by transverse contamination;
naca-tn-891; March 1943
- (Author(s) Not
Available); Some
investigations of the general instability of stiffened metal cylinders VI :
stiffened metal cylinders subjected to combined bending and transverse
shear; naca-tn-910; 1943
- Kaplan, Carl; On
a new method for calculating the potential flow past a body of revolution;
naca-report-752; 1943
- Olson, Roland E Land,
Norman S; Methods used in
the NACA tank for the investigation of the longitudinal-stability
characteristics of models of flying boats; naca-report-753; 1943
- Sanders, J C Wilsted, H
D Mulcahy, B A; Operating
temperatures of a sodium-cooled exhaust valve as measured by a
thermocouple; naca-report-754; 1943
- Gilruth, R R; Requirements
for satisfactory flying qualities of airplanes; naca-report-755;
1943
- Rothrock, Addison M
Krsek, Alois, Jr Jones, Anthony W; The
induction of water to the inlet air as a means of internal cooling in
aircraft-engine cylinders; naca-report-756; 1943
- Gerrish, Harold C Meem,
J Lawrence, Jr; The
measurement of fuel-air ratio by analysis for the oxidized exhaust gas;
naca-report-757; 1943
- Sinnette, John T Schey,
Oscar W King, J Austin; Performance
of NACA eight-stage axial-flow compressor designed on the basis of airfoil
theory; naca-report-758; 1943
- Pearson, Henry A; Derivation of
charts for determining the horizontal tail load variation with any elevator
motion; naca-report-759; 1943
- Sanders, Newell D; A method of
estimating the knock rating of hydrocarbon fuel blend; naca-report-760;
1943
- Miller, Cearcy D Olsen,
H Lowell; Identification
of knock in NACA high-speed photographs of combustion in a spark-ignition
engine; naca-report-761; 1943
- Greenberg, Harry
Sternfield, Leonard; A
theoretical investigation of the lateral oscillations of an airplane with free
rudder with special reference to the effect of friction; naca-report-762;
1943
- Stack, John; Tests
of airfoils designed to delay the compressibility burble; naca-report-763;
1943
- Allen, H Julian Look,
Bonne C; A
method for calculating heat transfer in the laminar flow region of bodies;
naca-report-764; 1943
- Parkinson, John B
Olson, Roland E Draley, Eugene C Luoma, Arvo A; Aerodynamic
and hydrodynamic tests of a family of models of flying hulls derived from a
streamline body -- NACA model 84 series; naca-report-766; 1943
- Hood, Manley J Allen, H
Julian; The
problem of longitudinal stability and control at high speeds;
naca-report-767; 1943
- Kaplan, Carl; The
flow of a compressible fluid past a curved surface; naca-report-768;
1943
- Campbell, John P
Seacord, Charles L , Jr; The
effect of mass distribution on the lateral stability and control
characteristics of an airplane as determined by tests of a model in the
free-flight tunnel; naca-report-769; 1943
- Swanson, Robert S Toll,
Thomas A; Jet-boundary
corrections for reflection-plane models in rectangular wind tunnel;
naca-report-770; 1943
- Johnston, J Ford; Review of
flight tests of NACA C and D cowlings on the XP-42 airplane;
naca-report-771; 1943
- Von Doenhoff, Albert E
Tetervin, Neal; Determination
of general relations for the behavior of turbulent boundary layers;
naca-report-772; 1943
- Becker, John V Baals,
Donald D; Analysis of
heat and compressibility effects in internal flow systems and high-speed tests
of a ram-jet system; naca-report-773; 1943
- Lowry, John G; Resume
of hinge-moment data for unshielded horn- balanced control surfaces;
naca-wr-l-169; June 1943
- Purser, Paul E; Wind-tunnel
investigation of control-surface characteristics XIV : NACA 0009 airfoil with
a 20-percent-chord double plain flap; naca-wr-l-290; June 1943
- Ribner, Herbert S; Proposal for a
propeller side-force factor; naca-wr-l-336; December 1943
- Schuldenfrei, Marvin;
Some notes
on the determination of the stick-fixed neutral point from wind-tunnel
data; naca-wr-l-344; September 1943
- Anderson, R A; Wind
tunnel tests of ailerons at various speeds IV : ailerons of 0.20 airfoil chord
and true contour with 0.35 aileron-chord extreme blunt-nose balance on the
NACA 23012 airfoil; naca-wr-l-433; August 1943
- Denaci, H G; Wind
tunnel tests of ailerons at various speeds V : pressure distributions over the
NACA 66,2-216 and NACA 23012 airfoils with various balances on 0.20-chord
ailerons; naca-wr-l-434; November 1943
- Crandall, Stewart M; Wind-tunnel
investigation of trimming tabs on a thickened and beveled aileron on a tapered
low-drag wing; naca-wr-l-435; March 1943
- Nelson, W J; Wind
tunnel investigation of rear underslung fuselage ducts; naca-wr-l-438;
September 1943
- Dingeldein, Richard C;
Full-scale
tunnel investigation of the pressure distribution over the tail of the P-47B
airplane; naca-wr-l-439; May 1943
- Hoggard, H Page; Wind tunnel
investigation of control-surface characteristics XI : various large overhang
and internal-type aerodynamic balances for a straight- contour flap on the
NACA 0015 airfoil; naca-wr-l-447; 1943
- Tetervin, Neal; Tests in the
NACA two-dimensional low-turbulence tunnel of airfoil sections designed to
have small pitching moments and high lift-drag ratios; naca-wr-l-452;
September 1943
- Toll, Thomas A; Jet-boundary
corrections for reflection-plane models in rectangular wind tunnels;
naca-wr-l-458; May 1943
- Turner, Thomas R; Wind-tunnel
investigation of effect of yaw on lateral-stability characteristics V :
symmetrically tapered wing with a circular fuselage having a horizontal and a
vertical tail; naca-wr-l-459; June 1943
- Gelbart, Abe; On
a function-theory method for obtaining potential-flow patterns of a
compressible fluid; naca-wr-l-460; July 1943
- Schuette, Evan H; Critical
stresses for plates; naca-wr-l-466; October 1943
- Riebe, John M; Wind-tunnel
investigation of an NACA 23012 airfoil with a 0.30-airfoil-chord double
slotted flap; naca-wr-l-469; December 1943
- Moggio, Edwin M; The
longitudinal shear strength required in double-angle columns of 24S-T aluminum
alloy; naca-wr-l-472; May 1943
- Hastings, Charles E; NACA radio
ground-speed system for aircraft; naca-wr-l-477; February 1943
- Draper, John W; Free-flight-tunnel
investigation of the effect of the fuselage length and the aspect ratio and
size of the vertical tail on lateral stability and control; naca-wr-l-487;
April 1943
- Mendelsohn, Robert A;
Wind-tunnel
tests of a piston-type control booster on an airfoil and aileron model;
naca-wr-l-494; November 1943
- Crate, Harold; A
preliminary study of machine-countersunk flush rivets subjected to a combined
static and alternating shear load; naca-wr-l-495; December 1943
- Mattson, Axel T; The effect of
spinner-body gap on the pressures available for cooling in the NACA E-type
cowling; naca-wr-l-497; March 1943
- Mckinney, Marion O ,
Jr; Flight
tests of a glider model towed by twin parallel towlines; naca-wr-l-498;
April 1943
- Levin, L Ross; Tests
of 10-inch 24S-T aluminum-alloy shear panels with 1-1/2-inch holes I;
naca-wr-l-500; June 1943
- Pitkin, Marvin; Effect of wing
leading-edge slots on the spin and recovery characteristics of airplanes;
naca-wr-l-504; April 1943
- Fischel, Jack; Wind-tunnel
investigation of a full-span retractable flap in combination with full-span
plain and internally balanced ailerons on a tapered wing; naca-wr-l-506;
August 1943
- Benson, James M; Hydrodynamic-stability
tests of a model of a flying boat and of a planing surface having a small
downward projection (hook) on the planing bottom near the step;
naca-wr-l-518; 1943
- Schuette, Evan H; Test data on
the shear strength of joints assembled with round-head and brazier-head
rivets; naca-wr-l-519; June 1943
- Seacord, Charles L ,
Jr; Effect
of wing loading and altitude on lateral stability and control characteristics
of an airplane as determined by tests of a model in the free-flight
tunnel; naca-wr-l-522; June 1943
- Mckee, John W; Wind-tunnel
investigation of a plain aileron with thickened and beveled trailing edges on
a tapered low-drag wing; naca-wr-l-526; 1943
- Houbolt, John C; A preliminary
study of the effect of compressive load on the fairness of a low-drag wing
specimen with Z-section stiffeners; naca-wr-l-527; 1943
- Braslow, Albert L; Investigation
of surface irregularities on an NACA 63(420)-416, a=1.0 airfoil section for
the Glenn L. Martin Company design 195; naca-wr-l-534; October 1943
- Dow, Norris F; The
analysis of strains indicated by multiple-strand resistance-type wire strain
gages used as rosettes; naca-wr-l-536; 1943
- Ritchie, Virgil S; A simplified
chart for determining Mach number and true airspeed from airspeed-indicator
readings; naca-wr-l-473; March 1943
- Hoggard, H. Page, Jr.;
Wind tunnel
investigation of control surface characteristics XII : various cover-plate
alinements on the NACA 0015 airfoil with a 30 percent chord flap and large
sealed internal balance; naca-wr-l-511; 1943
- Sears, Richard I.; Wind-tunnel
data on the aerodynamic characteristics of airplane control surfaces;
naca-wr-l-663; 1943
- Purser, Paul E., Riebe,
John M.; Wind-tunnel
investigation of control-surface characteristics XV : various contour
modifications of a 0.30-airfoil-chord plain flap on an NACA 66(215)-014
airfoil; naca-wr-l-668; 1943
- Gillis, Clarence L,
Lockwood, Vernard E; Wind-tunnel
investigation of control-surface characteristics XIII : various flap overhangs
used with a 30-percent-chord flap in an NACA 66-009 airfoil;
naca-wr-l-314; 1943
- Letko, W, Denaci, H G,
Freed, C; Wind tunnel
tests of ailerons at various speeds I : ailerons of 0.20 airfoil chord and
true contour with 0.35 aileron-chord extreme blunt nose balance on the NACA
66,2-216 airfoil; naca-wr-l-431; 1943
- Denaci, H G, Bird, J D;
Wind-tunnel
tests of ailerons at various speeds II : ailerons of 0.20 airfoil chord and
true contour with 0.60 aileron-chord sealed internal balance on the NACA
66,2-216 airfoil; naca-wr-l-432; 1943
- Vogeley, A W; Flight
measurements of compressibility effects on a three-blade thin Clark Y
propeller operating at constant advance-diameter ratio and blade angle;
naca-wr-l-505; 1943
- Guggenheim Aeronautical
Laboratory; Some
Investigations of the General Instability of Stiffened Metal Cylinders V -
Stiffened Metal Cylinders Subjected to Pure Bending; naca-tn-909; August
1943
- Richard T. Whitcomb; The relation
between spanwise variations in the critical Mach number and spanwise load
distributions; naca-cb-l4l07; December 1944
- Garrick, I E Kaplan,
Carl; On the
flow of a compressible fluid by the hodograph method I : unification and
extension of present-day results; naca-report-789; 1944
- Houbolt, John C; Bending and
shear stresses developed by the instantaneous arrest of the root of a moving
cantilever beam; naca-report-828; November 1944
- Benson, James M; Piloting of
flying boats with special reference to porpoising and skipping;
naca-tn-923; February 1944
- Hilderbrand, Francis B
(Massachusetts Institute of Technology); A
least-squares procedure for the solution of the lifting-line integral
equation; naca-tn-925; February 1944
- Hildebrand, Francis B
(Massachusetts Institute of Technology) Reissner, Eric (Massachusetts
Institute of Technology); The
influence of the aerodynamic span effect on the magnitude of the
torsional-divergence velocity and on the shape of the corresponding deflection
mode; naca-tn-926; 1944
- Mebs, R W (National
Bureau of Standards) Mcadam, D J , Jr (National Bureau of Standards); The
influence of plastic deformation and of heat treatment on Poisson's ratio for
18:8 chromium-nickel steel; naca-tn-928; February 1944
- Schuette, Evan H
Bartone, Leonard M Mandel, Merven W; Tensile
tests of round-head, flat-head, and brazier-head rivets; naca-tn-930;
March 1944
- Brueggeman, W C
(National Bureau of Standards) Mayer, M , Jr (National Bureau of Standards);
Guides for
preventing buckling in axial fatigue tests of thin sheet-metal specimens;
naca-tn-931; April 1944
- Reissner, Eric
(Massachusetts Institute of Technology); On
the general theory of thin airfoils for nonuniform motion; naca-tn-946;
1944
- Demer, L J (University
of Notre Dame) Kavanaugh, E S (University of Notre Dame); Ovalization
of tubes under bending and compression; naca-tn-922; March 1944
- Niles, Alfred S
(Stanford University); Elastic
properties of channels with unflanged lightening homes; naca-tn-924; March
1944
- Hill, H N (Aluminum of
America); Determination
of stress-strain relations from "offset" yield strength values;
naca-tn-927; February 1944
- Mignot, J E (Lockheed
Aircraft Corporation) Combs, Henry (Lockheed Aircraft Corporation) Ensrud, A F
(Lockheed Aircraft Corporation); Analysis
of circular shell-supported frames; naca-tn-929; 1944
- Emmons, Howard W; The numerical
solution of compressible fluid flow problems; naca-tn-932; 1944
- Zamboky, A N (Aluminum
Company of America); Artificial
aging of riveted joints made in alclad 24S-T sheet using A17S-T, 17S-T, and
24S-T rivets; naca-tn-948; September 1944
- Levy, Samuel (National
Bureau of Standards) Goldenberg, Daniel (National Bureau of Standards)
Zibritosky, George (National Bureau of Standards); Simply
supported long rectangular plate under combined axial load and normal
pressure; naca-tn-949; October 1944
- Hoff, N J (Polytechnic
Institute of Brooklyn) Kempner, Joseph (Polytechnic Institute of Brooklyn); Numerical
procedures for the calculation of the stresses in monocoques II : diffusion of
tensiles stringer loads in reinforced flat panels with cut-outs;
naca-tn-950; November 1944
- Brueggeman, W C
(National Bureau of Standards) Mayer, M JR (National Bureau of Standards)
Smith, W H (National Bureau of Standards); Axial
fatigue tests at zero mean stress of 24S-T aluminum-alloy sheet with and
without a circular hole; naca-tn-955; 1944
- Hersey, Mayo D
(Massachusetts Institute of Technology); Bibliography
of piston ring lubrication; naca-tn-956; October 1944
- Tsien, Hsue-Shen
(California Institute of Technology); The
"limiting line" in mixed subsonic and supersonic flow of compressible
fluids; naca-tn-961; 1944
- Stack, John; Tests
of airfoils designed to delay the compressibility burble; naca-tn-976;
December 1944
- Draper, C S
(Massachusetts Institute of Technology) Taylor, E S (Massachusetts Institute
of Technology) Lancor, J H (Massachusetts Institute of Technology) Coffey, R T
(Massachusetts Institute of Technology); Development
of detonation detector suitable for use in flight; naca-tn-977; December
1944
- Winston, A W; Effect
of aging aircraft structures on magnesium parts; naca-tn-979; October
1944
- Goodier, J N (Cornell
University) Thomson, W T (Cornell University); Applicability
of similarity principles to structural models; naca-tn-933; July
1944
- Hoff, N J (Polytechnic
Institute of Brooklyn) Levy, Robert S (Polytechnic Institute of Brooklyn)
Kempner, Joseph (Polytechnic Institute of Brooklyn); Numerical
procedures for the calculation of the stresses in Monocoques I : diffusion of
tensile stringer loads in reinforced panels; naca-tn-934; June 1944
- Boden, R H
(Massachusetts Institute of Technology) Schecter, Harry (Massachusetts
Institute of Technology); Dynamics
of the inlet system of a four-stroke engine; naca-tn-935; 1944
- Bradley, Kathryn H
(National Bureau of Standards) Axilrod, B M (National Bureau of Standards); Plastic
mountings for aircraft windshields; naca-tn-936; May 1944
- Ballhaus, W F (Stanford
University) Niles, A S (Stanford University); Simplified
truss stability criteria; naca-tn-937; July 1944
- Hoff, N J (Polytechnic
Institute of Brooklyn, Brooklyn, N.Y) Klein, Bertram (Polytechnic Institute of
Brooklyn, Brooklyn, N.Y); The
inward bulge type buckling of monocoque cylinders I : calculation of the
effect upon the buckling stress of a compressive force, a nonlinear direct
stress distribution, and a shear force; naca-tn-938; 1944
- Hoff, N J (Polytechnic
Institute of Brooklyn, Brooklyn, N.Y) Fuchs, S J (Polytechnic Institute of
Brooklyn, Brooklyn, N.Y) Cirillo, Adam J (Polytechnic Institute of Brooklyn,
Brooklyn, N.Y); The
inward bulge type buckling of monocoque cylinders II : experimental
investigation of the buckling in combined bending and compression;
naca-tn-939; 1944
- Manson, S S; Charts
for rapid analysis of 45 degree strain-rosette data; naca-tn-940; May
1944
- Manson, S S; An
automatic electrical analyzer for 45 degree strain-rosette data;
naca-tn-941; May 1944
- Hartman, E C (Aluminum
Company of America) Wescoat, C (Aluminum Company of America); The
shear of aluminum alloy driven rivets as affected by increasing D/t
ratios; naca-tn-942; July 1944
- Head, Richard M
(California Institute of Technology, Pasadena, California) Sechler, Ernest J
(California Institute of Technology, Pasadena, California); Normal
pressure tests on unstiffened flat plates; naca-tn-943; 1944
- Ramberg, Walter
(National Bureau of Standard) Levy, Samuel (National Bureau of Standard)
Fienup, Kenneth L (National Bureau of Standard); Effect
of curvature on strength of axially loaded sheet-stringer panels;
naca-tn-944; August 1944
- Mcmaster, R C
(California Institute of Technology) Manildi, J F (California Institute of
Technology) Woolsey, C C (California Institute of Technology); Nondestructive
test methods for spot welds in aluminum alloys; naca-tn-945; November
1944
- Koffewl, William K
Biermann, Arnold E; A
unit laboratory engine oil system providing for a remote indication of oil
flow and oil consumption together with blow-by measurement; naca-tn-952;
September 1944
- Mcpherson, A E
(National Bureau of Standards) Goldenberg, D (National Bureau of Standards)
Zibritosky, G (National Bureau of Standards); Torsion
test to failure of a monocoque box; naca-tn-953; October 1944
- Campbell, William R
(National Bureau of Standards); Performance
tests of wire strain gages I : calibration factors in tension;
naca-tn-954; November 1944
- Turner, Philip S
(National Bureau of Standards) Doran, Jewel (National Bureau of Standards)
Reinhart, Frank W (National Bureau of Standards); Fairing
compositions for aircraft surfaces; naca-tn-958; November 1944
- Brueggeman, W C
(National Bureau of Standards) Krupen, P (National Bureau of Standards) Roop,
F C (National Bureau of Standards); Axial
fatigue of 10 airplane wing-beam specimens by the resonance method;
naca-tn-959; December 1944
- Mutchler, Willard
(National Bureau of Standards); The
effect of temperature on sheet metals for airplane firewalls; naca-tn-965;
December 1944
- Zender, George W
Schuette, Evan H Weinberger, Robert A; Data
on material properties and panel compressive strength of a plastic-bonded
material of glass cloth and canvas; naca-tn-975; August 16, 1944
- Ruffner, Benjamin F
(Oregon State College) Schmidt, Calvin L (Oregon State College); Stresses
at cut-outs in shear resistant webs as determined by the photoelastic
method; naca-tn-984; 1944
- Teplitz, Jerome; Effects of
small angles of sweep and moderate amounts of dihedral on stalling and lateral
characteristics of a wing-fuselage combination equipped with partial- and
full-span double slotted flaps; naca-report-800; 1944
- Jones, Robert T; A method for
studying the hunting oscillations of and airplane with a simple type of
automatic control; naca-report-801; 1944
- Ellis, Macon C , Jr
Brown, Clinton E; NACA
investigation of a jet-propulsion system applicable to flight;
naca-report-802; 1944
- Crane, Robert M
Holtzclaw, Ralph W; Wind-tunnel
investigation of the effects of profile modification and tabs on the
characteristics of ailerons on a low-drag airfoil; naca-report-803;
1944
- Goett, Harry J Delaney,
Noel K; Effect of tilt
of the propeller axis on the longitudinal-stability characteristics of
single-engine airplanes; naca-report-774; 1944
- Theodorsen, Theodore;
The theory
of propellers I : determination of the circulation function and the mass
coefficient for dual-rotating propellers; naca-report-775; 1944
- Theodorsen, Theodore;
The theory
of propellers II : method for calculating the axial interference;
naca-report-776; 1944
- Theodorsen, Theodore;
The theory
of propellers III : the slipstream contraction with numerical values for
two-blade and four-blade propellers; naca-report-777; 1944
- Theodorsen, Theodore;
The theory
of propellers IV : thrust, energy, and efficiency formulas for single and dual
rotating propellers with ideal circulation distribution; naca-report-778;
1944
- Schey, Oscar W Rollin,
Verne G Ellerbrock, Herman H , Jr; The
effect of increased cooling surface on performance of aircraft-engine
cylinders as shown by tests of the NACA cylinder; naca-report-779;
1944
- Heaslet, Max A; Compressible
potential flow with circulation about a circular cylinder;
naca-report-780; 1944
- Goett, Harry J Jackson,
Roy P Belsley, Steven E; Wind-tunnel
procedure for determination of critical stability and control characteristics
of airplanes; naca-report-781; 1944
- Allen, H Julian
Vincenti, Walter G; Wall
interference in a two-dimensional-flow wind tunnel, with consideration of the
effect of compressibility; naca-report-782; 1944
- Goldstein, Arthur W
Ellerbrock, Herman H , Jr; Compressibility
and heating effects on pressure loss and cooling of a baffled cylinder
barrel; naca-report-783; 1944
- Reuter, J George
Valerino, Michael F; Intercooler
cooling-air weight flow and pressure drop for minimum drag loss;
naca-report-784; 1944
- Miller, Cearcy D Logan,
Walter O , Jr; Preknock
vibrations in a spark-ignition engine cylinder as revealed by high-speed
photography; naca-report-785; 1944
- Turner, L Richard
Desmon, Leland G; Performance
of blowdown turbine driven by exhaust gas of nine-cylinder radial engine;
naca-report-786; 1944
- Cohen, Doris; A
theoretical investigation of the rolling oscillations of an airplane with
ailerons free; naca-report-787; 1944
- Garrick, I E; On
the plane potential flow past a lattice of arbitrary airfoils;
naca-report-788; 1944
- Garrick, I E Kaplan,
Carl; On the
flow of a compressible fluid by the hodograph method II : fundamental set of
particular flow solutions of the Chaplygin differential equation;
naca-report-790; 1944
- Greenberg, Harry
Sternfield, Leonard; A
theoretical investigation of longitudinal stability of airplane with free
controls including effect of friction in control system; naca-report-791;
1944
- (Author(s) Not
Available); Flight studies
of the horizontal-tail loads experienced by a fighter airplane in abrupt
maneuvers; naca-report-792; 1944
- Theodorsen, Theodore
Regier, Arthur; Experiments
on drag of revolving disks, cylinders, and streamline rods at high speeds;
naca-report-793; 1944
- Kaplan, Carl; The
flow of a compressible fluid past a circular arc profile; naca-report-794;
1944
- Batterson, Sidney A; The NACA impact
basin and water landing tests of a float model at various velocities and
weights; naca-report-795; 1944
- Donlan, Charles; An interim
report on the stability and control of tailless airplanes;
naca-report-796; 1944
- Phillips, William H; Application of
spring tabs to elevator controls; naca-report-797; 1944
- Jones, Robert T
Greenberg, Harry; Effect
of hinge-moment parameters on elevator stick forces in rapid maneuvers;
naca-report-798; 1944
- Pearson, Henry A Aiken,
William S , Jr; Charts
for the determination of wing torsional stiffness required for specified
rolling characteristics or aileron reversal speed; naca-report-799;
1944
- Swanson, Robert S
Gillis, Clarence L; Wind-tunnel
calibration and correction procedures for three-dimensional models;
naca-wr-l-1; October 1944
- Maclachlan, Robert; Investigation
of effect of sideslip on lateral stability characteristics I : circular
fuselage with variations in vertical-tail area and tail length with and
without horizontal tail surface; naca-wr-l-12; May 1944
- Warren A. Tucker,
Arthur R. Wallace; Scale-effects
in a turbulent tunnel of the NACA 65(3)-418, a=1.0 airfoil; naca-wr-l-128;
September 1944
- Corson, Blake W , Jr;
Application
of the method of least squares to engine-cooling analysis; naca-wr-l-130;
August 1944
- Pearson, E O , Jr; Aerodynamic
tests of an AN-M-65-AEON 1000-pound radio-controlled bomb in the LMAL 16-foot
high-speed tunnel; naca-wr-l-131; June 1944
- Theodorsen, Theodore;
Airfoil-contour
modifications based on (epsilon)-curve method of calculating pressure
distribution; naca-wr-l-135; July 1944
- Naiman, Irven; Numerical
evaluation of the (epsilon)-integral occurring in the Theodorsen arbitrary
airfoil potential theory; naca-wr-l-136; April 1944
- Brilmyer, Harold G; Secondary
stresses in open box beams subjected to torsion; naca-wr-l-14; November
1944
- Bulloch, Marjorie E; Wind-tunnel
investigation of control-surface characteristics XVI : pressure distribution
over an NACA 0009 airfoil with 0.30-airfoil-chord beveled-trailing-edge
flaps; naca-wr-l-205; April 1944
- Huber, Paul W; Heat-capacity
lag in turbine-working fluids; naca-wr-l-21; May 1944
- Phillips, W H; Stability
of a body stabilized by fins and suspended from an airplane; naca-wr-l-28;
April 1944
- Becker, John V
Korycinski, Peter F; Aerodynamic
tests of a full-scale TBF-1 aileron installation in the Langley 16-foot
high-speed tunnel; naca-wr-l-31; December 1944
- Sternfield, Leonard; A theoretical
investigation of longitudinal stability of airplanes with free controls
including effect of friction in control system; naca-wr-l-430; February
1944
- Kantrowitz, Arthur; Effects of
heat-capacity lag in gas dynamics; naca-wr-l-457; 1944
- Chiarito, Patrick T; Shear-lag tests
of two box beams with corrugated covers loaded to failure; naca-wr-l-482;
1944
- Dobrowski, Charles V;
Compressive
strength of flat panels with Z-section stiffeners; naca-wr-l-499; February
1944
- Levin, L Ross; Tests
of 10 inch 24S-T aluminum-alloy shear panels with 1-1/2 inch holes II : panels
having holes with notched edges; naca-wr-l-512; April 1944
- Cleary, Harold E; Variation of
peak pitching-moment coefficients for six airfoils as affected by
compressibility; naca-wr-l-515; October 1944
- Wood, Clotaire; A flight
investigation of the effect of surface roughness on wing profile drag with
transition fixed; naca-wr-l-521; September 1944
- Levin, L Ross; Tests
of beams having webs with large circular lightening holes; naca-wr-l-524;
February 1944
- Harman, Sidney M; Determination
of the effect of wing flexibility on lateral maneuverability and a comparison
of calculated rolling effectiveness with flight results; naca-wr-l-525;
1944
- Reisert, Thomas D; Tests of a
1/17-scale model of the XBDR-1 airplane in the NACA gust tunnel;
naca-wr-l-539; February 1944
- Baals, Donald D; Simple curves
for determining the effects of compressibility on pressure drop through
radiators; naca-wr-l-6; September 1944
- Ellisman, Carl; Effect in
flight of the propeller cuffs and spinner on pressure recovery in front of a
double-row radial aircraft engine in a twin-engine airplane;
naca-wr-e-169; March 1944
- Plumly, Howard D; A
laboratory-tested constant-level oil sump to prevent aeration of scavenged oil
from an aircraft engine; naca-wr-e-182; April 1944
- Englert, Gerald W; Analysis and
correlation of data obtained by six laboratories on fuel-vapor loss from fuel
tanks during simulated flight; naca-wr-e-185; December 1944
- Black, Dugald O; Flight
variables affecting fuel-vapor loss from a fuel tank; naca-wr-e-186;
December 1944
- Vierthaler, Walter A;
Experimental
study of the coating found on scuffed cast-iron piston rings during operation
in nitrided-steel cylinders; naca-wr-e-29; November 1944
- Bull, Arthur W; Knock-limited
performance of pure hydrocarbons blended with a base fuel in a full-scale
aircraft-engine cylinder I : eight paraffins, two olefins; naca-wr-e-33;
May 1944
- Mulcahy, B A Wilsted, H
D; Cylinder-head
cooling by means of a shield in the exhaust passage; naca-wr-e-34; June
1944
- Hensley, Reece V; Relative
effects of cylinder-head and inlet-mixture temperatures upon knock limits of
fuels; naca-wr-e-37; October 1944
- Latzko, H.; Heat
transfer in a turbulent liquid or gas stream; naca-tm-1068; 1944
- Sottorf, W.; Analysis
of experimental investigations of the planing process on the surface of
water; naca-tm-1061; 1944
- Imming, Harry S; The effect of
piston-head temperature on knock-limited power; naca-wr-e-35; July
1944
- Greenberg, Harry; Calculation of
stick forces for an elevator with a spring tab; naca-wr-l-129; June
1944
- Pitkin, Marvin; Force test of a
1/5-scale model of the type GB-5 controllable glide bomb; naca-wr-l-133;
March 27, 1944
- Ribner, Herbert S.; Notes on the
propeller and slipstream in relation to stability; naca-wr-l-25;
1944
- Lockwood, Vernard E.;
Wind-tunnel
investigation of control-surface characteristics XVII : beveled-trailing-edge
flaps of 0.20, 0.30, and 0.40 airfoil chord on an NACA 0009 airfoil;
naca-wr-l-666; 1944
- Goranson, R. Fabian.;
A method for
predicting the elevator deflection required to land; naca-wr-l-95;
1944
- Cook, Harvey A,
Vandeman, Jack E, Brown, Kenneth D; Effect
of several methods of increasing knock-limited power on cylinder
temperatures; naca-wr-e-36; 1944
- Tetervin, Neal; A method for
the rapid estimation of turbulent boundary-layer thickness for calculating
profile drag; naca-wr-l-16; 1944
- Garner, I Elizabeth; Wind-tunnel
investigation of control-surface characteristics XX : plain and balanced flaps
on an NACA 0009 rectangular semispan tail surface; naca-wr-l-186;
1944
- Quinn, John H; Tests
of the NACA 653-018 airfoil section with boundary-layer control by
suction; naca-wr-l-209; 1944
- Liddell, Robert B; Wind-tunnel
investigation of control-surface characteristics XIX : a double flap with an
overhang and an internal aerodynamic balance; naca-wr-l-215; 1944
- Sears, Richard I,
Liddell, Robert B; Wind-tunnel
investigation of control-surface characteristics XVIII : a linked overhang
aerodynamic balance; naca-wr-l-350; 1944
- Rogallo, F M; Collection
of balanced-aileron test data; naca-wr-l-419; 1944
- Boshar, John; The
determination of span load distribution at high speeds by use of high-speed
wind-tunnel section data; naca-wr-l-436; 1944
- Lowry, John G, Maloney,
James A, Garner, I Elizabeth; Wind-tunnel
investigation of shielded horn balances and tabs on a 0.7-scale model of XF6F
vertical tail surface; naca-wr-l-516; 1944
- Charles W. Frick,
Wallace F. Davis, Lauros M. Randall, Emmet A. Mossman; An
Experimental Investigation of NACA Submerged-Duct Entrances;
naca-acr-5i20; November, 1945
- Herbert S. Ribner; Propellers in
yaw; naca-report-820; 1945
- Samuel Levey, Kenneth
L. Fienup, Ruth M. Wooley; Analysis
of square shear web above buckling load; naca-tn-962; February 1945
- Shames, Sidney J; Air-consumption
parameters for automatic mixture control of aircraft engines;
naca-report-804; 1945
- Putnam, Abbott A; An analysis of
life expectancy of airplane wings in normal cruising flight;
naca-report-805; 1945
- Benser, William A
Moses, Jason J; An
investigation of backflow phenomenon in centrifugal compressors;
naca-report-806; 1945
- Peiser, A M Wilkerson,
M; A method
of analysis of v-g records from transport operations; naca-report-807;
1945
- Brown, Clinton E
Parker, Hermon M; A
method for the calculation of external lift, moment, and pressure drag of
slender open-nose bodies of revolution at supersonic speeds;
naca-report-808; 1945
- Lundquist, Eugene E
Stowell, Elbridge Z Schuette, Evan H; Principles
of moment distribution applied to stability of structures composed of bars or
plates; naca-report-809; 1945
- Mayo, Wilbur L; Analysis and
modification of theory for impact of seaplanes on water; naca-report-810;
1945
- Male, Donald W Evvard,
John C; Preignition-limited
performance of several fuels; naca-report-811; 1945
- Bellman, Donald R
Evvard, John C; Knock-limited
performance of several internal coolants; naca-report-812; 1945
- Sanders, J C; Correlation
of exhaust-valve temperatures with engine operating conditions and valve
design; naca-report-813; 1945
- Perl, W Tucker, M; A general
representation for axial-flow fans and turbines; naca-report-814;
1945
- Bullock, Robert O
Keetch, Robert C Moses, Jason J; Method
of matching performance of compressor systems with that of aircraft power
sections; naca-report-815; 1945
- Kayten, Gerald G Koven,
William; Comparison of
wind-tunnel and flight measurements of stability and control characteristics
of a Douglas A-26 airplane; naca-report-816; August 11, 1945
- Collins, John H Bisson,
Edmond E Schmiedlin, Ralph F; Nitrited-steel
piston rings for engines of high specific power; naca-report-817;
1945
- Manganiello, Eugene J
Bogatsky, Donald; An
experimental investigation of rectangular exhaust-gas ejectors applicable for
engine cooling; naca-report-818; 1945
- Ribner, Herbert S; Formulas for
propellers in yaw and charts of the side-force derivative;
naca-report-819; 1945
- Marble, Frank E Ritter,
William K Miller, Mahlon A; Effect
of NACA injection impeller on mixture distribution of double-row radial
aircraft engine; naca-report-821; 1945
- Zimmerman, Richard H;
Calculations
of economy of 18-cylinder radial aircraft engine with exhaust-gas turbine
geared to the crankshaft at cruising speed; naca-report-822; 1945
- Campbell, John P; Experimental
verification of a simplified vee-tail theory and analysis of available data on
complete models with vee tails; naca-report-823; 1945
- Abbott, Ira H Von
Doenhoff, Albert E Stivers, Louis, Jr; Summary
of airfoil data; naca-report-824; 1945
- Kayten, Gerald G; Analysis of
wind-tunnel stability and control tests in terms of flying qualities of
full-scale airplanes; naca-report-825; 1945
- Cohen, Doris; A
method for determining the camber and twist of a surface to support a given
distribution of lift, with applications to the load over a sweptback wing;
naca-report-826; 1945
- Schuette, Evan H; Charts for the
minimum-weight design of 24s-t aluminum-alloy flat compression panels with
longitudinal z-section stiffeners; naca-report-827; 1945
- Sweberg, Harold H
Dingeldein, Richard C; Summary
of measurements in Langley full-scale tunnel of maximum lift coefficients and
stalling characteristics of airplanes; naca-report-829; 1945
- Hardy, J K; An
analysis of the dissipation of heat in conditions of icing from a section of
the wing of the C-46 airplane; naca-report-831; 1945
- Graham, Donald J
Nitzberg, Gerald E Olson, Robert N; A
systematic investigation of pressure distributions at high speeds over five
representative NACA low-drag and conventional airfoil sections;
naca-report-832; 1945
- Allen, H Julian; General theory
of airfoil sections having arbitrary shape or pressure distribution;
naca-report-833; 1945
- Kittel, J Howard; Table of
interplanar spacings for crystal-structure determinations by X-ray diffraction
with molybdenum, copper, cobalt, iron, and chromium radiations;
naca-tn-1000; October 1945
- Mayo, Wilbur L; Analysis and
modification of theory for impact of seaplanes on water; naca-tn-1008;
December 1945
- Hoff, N J (Polytechnic
Institute of Brooklyn, Brooklyn, N.Y) Boley, Bruno A (Polytechnic Institute of
Brooklyn, Brooklyn, N.Y) Klein, Bertram (Polytechnic Institute of Brooklyn,
Brooklyn, N.Y); Stresses
in and general instability of monocoque cylinders with cutouts II :
calculation of the stresses in a cylinder with a symmetric cutout;
naca-tn-1014; July 1945
- White, Roland J
(Curtiss-Wright Corporation) Klampe, Dean G (Curtiss-Wright Corporation); Force and
moment coefficients for a thin airfoil with flap and tab in a form useful for
stability and control calculations; naca-tn-960; 1945
- Mebs, R W (National
Bureau of Standards) Mcadam, D J (National Bureau of Standards); Shear
elastic properties of some high strength nonferrous metals as affected by
plastic deformation and by heat treatment; naca-tn-967; 1945
- Hoff, N J (Polytechnic
Institute of Brooklyn, Brooklyn, N.Y) Klein, Bertram (Polytechnic Institute of
Brooklyn, Brooklyn, N.Y); The
inward bulge type buckling of monocoque cylinders III : revised theory which
considers the shear strain energy; naca-tn-968; 1945
- Bergman, Stefan (Brown
University, Providence, R.I); Graphical
and analytical methods for the determination of a flow of a compressible fluid
around an obstacle; naca-tn-973; 1945
- Campbell, William R
(National Bureau of Standards); Performance
tests of wire strain gages II : calibration factors in compression;
naca-tn-978; September 1945
- Bennett, J A (National
Bureau of Standards); Effect
of fatigue-stressing short of failure on some typical aircraft metals;
naca-tn-992; October 1945
- Leary, J R (Aluminum
Company of America) Holt, Marshall (Aluminum Company of America); Column
strength of extruded magnesium alloys AM-C58S and AM-C58S-T5; naca-tn-994;
December 1945
- Jessup, R S (National
Bureau of Standards) Cragoe, C S (National Bureau of Standards); Net
heat of combustion of AN-F-28 aviation gasolines; naca-tn-996; May 14,
1945
- Campbell, William R
(National Bureau of Standards); Performance
tests of wire strain gages III : calibrations at high tensile strains;
naca-tn-997; December 1945
- Reid, Elliot G
(Stanford, University); Studies
of blade shank and pitch distribution for constant-speed propellers;
naca-tn-947; 1945
- Bruhn, Elmer F (Purdue
University); Tests on
thin-walled celluloid cylinders to determine the interaction curves under
combined bending, torsion, and compression or tension loads; naca-tn-951;
1945
- Sechler, E E
(California Institute of Technology) Frederick, J L (California Institute of
Technology); The strength of
semielliptical cylinders subjected to combined loadings; naca-tn-957;
February 1945
- Keenan, Joseph H
(Massachusetts Institute of Technology) Neumann, Ernest P (Massachusetts
Institute of Technology); Friction
in pipes at supersonic and subsonic velocities; naca-tn-963; 1945
- Axilrod, B M (National
Bureau of Standards) Jirauch, D H (National Bureau of Standards); Bonding
strengths of adhesives at normal and low temperatures; naca-tn-964;
1945
- Templin, R L (Aluminum
Company of America) Hartmann, E C (Aluminum Company of America); The
elastic constants for wrought aluminum alloys; naca-tn-966; 1945
- Bers, Lipman (Brown
University, Providence, R.I); On
a method of constructing two-dimensional subsonic compressible flows around
closed profiles; naca-tn-969; 1945
- Bers, Lipman (Brown
University, Providence, R.I); On
the circulatory subsonic flow of a compressible fluid past a circular
cylinder; naca-tn-970; 1945
- Andrews, H J (Aluminum
Company of America) Holt, M (Aluminum Company of America); Fatigue
tests on 1/8-inch aluminum alloy rivets; naca-tn-971; February 1945
- Bergman, Stefan (Brown
University, Providence, R.I); On
two-dimensional flows of compressible fluids; naca-tn-972; 1945
- Wescoat, C (Aluminum
Company of America) Moore, R L (Aluminum Company of America); Bearing
strengths of 75S-T aluminum-alloy sheet and extruded angle; naca-tn-974;
February 1945
- Hamermesh, Bernard (New
York University) Reines, Frederick (New York University) Korff, Serge A (New
York University); A
photoelectric hygrometer; naca-tn-980; May 1945
- Moore, R L (Aluminum
Company of America) Wescoat, C (Aluminum Company of America); Bearing
strengths of 24S-T aluminum alloy plate; naca-tn-981; June 1945
- Gwathmey, A T
(University of Virginia) Leidheiser, H (University of Virginia) Smith, G P
(University of Virginia); The
chemical action of oils on single crystals of metals; naca-tn-982;
November 1945
- Brueggeman, W C
(National Bureau of Standards) Mayer, M , Jr (National Bureau of Standards)
Smith, W H (National Bureau of Standards); Axial
fatigue test at two stress amplitudes of 0.032-inch 24S-T sheet specimens with
a circular hole; naca-tn-983; July 1945
- Mcadams, William H
(Massachusetts Institute of Technology) Nicolai, Lloyd A (Massachusetts
Institute of Technology) Keenan, Joseph H (Massachusetts Institute of
Technology.); Measurements
of recovery factors and coefficients of heat transfer in a tube for subsonic
flow of air; naca-tn-985; June 1945
- Sachs, George (Case
School of Applied Science) Smith, Charles S (Case School of Applied Science)
Lubahn, Jack D (Case School of Applied Science) Davis, Gordon E (Case School
of Applied Science) Ebert, Lynn J (Case School of Applied Science); Nondestructive
measurement of residual and enforced stresses by means of x-ray diffraction I
: correlated abstract of the literature; naca-tn-986; September
1945
- Sachs, George (Case
School of Applied Science) Smith, Charles S (Case School of Applied Science)
Lubahn, Jack D (Case School of Applied Science) Davis, Gordon E (Case School
of Applied Science) Ebert, Lynn J (Case School of Applied Science); Nondestructive
measurement of residual and enforced stresses by means of x-ray diffraction II
: some applications to aircraft problems; naca-tn-987; November
1945
- Ramberg, Walter
(National Bureau of Standards) Mcpherson, A E (National Bureau of Standards)
Levy, Samuel (National Bureau of Standards); Strength
of wing beams under axial and transverse loads; naca-tn-988; September
1945
- Rinker, R C (National
Bureau of Standards) Kline, G M (National Bureau of Standards); Survey
of adhesives and adhesion; naca-tn-989; August 1945
- Weske, John R (Case
School of Applied Science); Measurement
of the arithmetic mean velocity of a pulsating flow of high velocity by the
hot-wire method; naca-tn-990; April 1945
- Axilrod, Benjamin M
(National Bureau of Standards) Koenig, Evelyn (National Bureau of Standards);
Properties
of some expanded plastics and other low-density materials; naca-tn-991;
September 1945
- Pian, Theodore
Hsueh-Huang (Massachusetts Institute of Technology); Analytical
study of transmission of load from skin to stiffeners and rings of pressurized
cabin structure; naca-tn-993; October 1945
- Kempner, Joseph; Application of
a numerical procedure to stress analysis of stringer-reinforced panels;
naca-wr-l-11; March 1945
- Joyner, Upshur T; Charts of
pressure, density, and temperature changes at an abrupt increase in
cross-sectional area of flow of compressible air; naca-wr-l-13;
1945
- Bennett, Charles V; Stability and
control characteristics of a fighter airplane in inverted flight attitude as
determined by model tests; naca-wr-l-15; August 1945
- Erwin, Mary A; Hinge
moments of sealed-internal-balance arrangements for control surfaces I :
theoretical investigation; naca-wr-l-174; August 1945
- Church, Oleta; Wind-tunnel
investigation of control-surface characteristics XXI : medium and large
aerodynamic balances of two nose shapes and a plain overhang used with a
0.40-airfoil-chord flap on an NACA 0009 airfoil; naca-wr-l-175; March
1945
- Kenimer, Robert L; An infrared
cloud indicator I : analysis of infrared-radiation exchange with tables and
chart for calibration of the cloud indicator; naca-wr-l-18; November
1945
- Sweberg, Harold H; Note on
compressibility effects on downwash at the tail at subcritical speeds;
naca-wr-l-19; March 1945
- Brilmyer, Harold G; Stresses near
the juncture of a closed and an open torsion box as influenced by bulkhead
flexibility; naca-wr-l-2; August 1945
- Roy, J Albert; Column
and plate compressive strengths of aircraft structural materials : 17S-T
aluminum-alloy sheet; naca-wr-l-20; June 1945
- Kamm, Robert W; Spin-tunnel
tests of airplane models with extreme variations in mass distribution along
the three body axes; naca-wr-l-22; March 1945
- Lietzke, A F; Effect
of fuel volatility and mixture temperature on the knocking characteristics of
a liquid-cooled single-cylinder test engine; naca-wr-l-26; April
1945
- Boyet, H; A
method for determining oil-cooler performance requirements in series
operation; naca-wr-l-3; September 1945
- Roy, J Albert; Column
and plate compressive strengths of aircraft structural materials : extruded
24S-T aluminum alloy; naca-wr-l-32; July 1945
- Schade, Robert O; Tests of a
linked differential flap system designed to minimize the reduction in
effective dihedral caused by power; naca-wr-l-4; August 1945
- Mourhess, Mary J; Numerical
evaluation of the wake-survey equations for subsonic flow including the effect
of energy addition; naca-wr-l-5; November 1945
- Pendley, Robert E; Effect of
propeller-axis angle of attack on thrust distribution over the propeller disk
in relation to wake-survey measurement of thrust; naca-wr-l-517; December
1945
- Boxer, Emanuel; Wind-tunnel
investigation of alternative propellers operating behind deflected wing flaps
for the XB-36 airplane; naca-wr-l-533; December 1945
- Schultz, Wayne F; Performance
selection charts for gliders and twin-engine tow planes; naca-wr-l-537;
May 1945
- Feigenbaum, D; Estimation
of the performance and longitudinal stability and control of a lifting-body
type of cargo airplane from tests of simplified models; naca-wr-l-541;
June 1945
- Migotsky, Eugene; Full-scale-tunnel
performance tests of the PV-2 helicopter rotor; naca-wr-l-545; April
1945
- Hollingworth, Thomas A;
Investigation
of effect of sideslip on lateral stability characteristics II : rectangular
midwing on circular fuselage with variations in vertical-tail area and
fuselage length with and without horizontal tail surface; naca-wr-l-8;
April 1945
- Luecker, Arthur R; Comparisons of
methods of computing bending moments in helicopter rotor blades in the plane
of flapping; naca-wr-l-9; August 1945
- Galvin, Herman B; Laboratory
investigation of icing in the carburetor and supercharger inlet elbow of an
aircraft engine I : description of setup and testing technique;
naca-wr-e-170; December 1945
- Mulholland, Donald R;
Laboratory
investigation of icing in the carburetor and supercharger inlet elbow of an
aircraft engine II : determination of the limiting-icing conditions;
naca-wr-e-171; December 1945
- Renner, Clark E; Laboratory
investigation of icing in the carburetor and supercharger inlet elbow of an
aircraft engine V : effect of injection of water-fuel mixtures and
water-ethanol-fuel mixtures on the icing characteristics; naca-wr-e-174;
December 1945
- Brightwell, Virginia L;
Relation
between fuel economy and crank angle for the maximum rate of pressure
rise; naca-wr-e-179; May 1945
- Male, Donald W; The effect of
six aromatic amines on the preignition-limited performance of 28-R aviation
fuel in a CFR engine; naca-wr-e-180; May 1945
- Rowe, William H; Process of
lead-deposit accumulations on aircraft-engine spark plugs; naca-wr-e-181;
December 1945
- Kramer, Walter E; Reduction of
fuel-vapor loss by omitting some of the fuel constituents normally lost during
flight; naca-wr-e-184; August 1945
- Kemp, Richard H; Operating
stresses in aircraft-engine crankshafts and connecting rods I : slip-ring and
bush combinations for dynamic-strain measurements; naca-wr-e-187; May
1945
- Cook, Harvey A Held,
Louis F Pritchard, Ernest I; The
influence of exhaust pressure on knock-limited performance; naca-wr-e-188;
April 1945
- Brown, Kenneth D; The effect of
valve clearance on knock-limited performance and engine cooling;
naca-wr-e-189; April 1945
- Barnett, Henry C; Smoking
characteristics of various fuels as determined by open-cup and
laboratory-burner smoke tests; naca-wr-e-190; September 1945
- Calvert, Howard F; Operating
stresses in aircraft-engine crankshafts and connecting rods II :
instrumentation and test results; naca-wr-e-191; August 1945
- Addie, A N; Characteristics
of the BMW 801D2 automatic engine control as determined from bench tests;
naca-wr-e-192; April 1945
- Lietzke, A F; Effect
of engine-operating variables and internal coolants on spark-advance
requirements of a liquid-cooled cylinder; naca-wr-e-198; May 1945
- Huppert, Merle C; Nitrous oxide
supercharging of an aircraft-engine cylinder; naca-wr-e-199; June
1945
- Miller, George R; Control of
cylinder temperatures by thermostatically operated internal-coolant
valves; naca-wr-e-200; July 1945
- Black, Fred O , Jr; A cooling
correlation equation for a double-row radial engine based on the temperature
of the exhaust-valve seat; naca-wr-e-201; April 1945
- Henneberry, Hugh M; Economy of
internally cooling only the overheated cylinders of aircraft engines;
naca-wr-e-202; July 1945
- Tower, Leonard K; Suitability of
ethers as aviation fuel components the knock-limited performance of several
ethers blended with AN-F-28 fuel; naca-wr-e-207; 1945
- Evvard, John C; A relation
between knock-limited or preignition-limited air-fuel ratio at lean mixtures
and fuel-air ratio at rich mixtures; naca-wr-e-208; November 1945
- Calvin C. Blackman and
H. Jack White; Flight
and Test-Stand Investigation of High-Performance Fuels in Modified Double-Row
Radial Air-Cooled Engines III - Knock-Limited Performance of 33-R as Compared
With a Triptane Blend and 28-R in Flight; naca-wr-e-263; August
1945
- Heinicke, Orville H; Effect of
water-alcohol injection and maximum economy spark advance on knock-limited
performance and fuel economy of a large air-cooled cylinder;
naca-wr-e-264; August 1945
- Wilcox, E C; Tests
of an adjustable-area exhaust nozzle for jet-propulsion engines;
naca-wr-e-265; August 1945
- Mesrobian, John M; Air-flow and
performance characteristics of the engine-stage supercharger of a double-row
radial aircraft engine I : effect of operating variables; naca-wr-e-266;
August 1945
- Rodgers, Franklin A; The effect of
high-resistance ignition cable on the erosion of spark-plug electrodes;
naca-wr-e-267; September 1945
- Erwin, Robert D , Jr;
Effect of
maximum cruise-power operation at ultra-lean mixture and increased spark
advance on the mechanical condition of cylinder components; naca-wr-e-268;
September 1945
- Essig, Robert H; Sea-level
performance tests of a 22-inch-diameter pulse-jet engine at various simulated
ram pressures; naca-wr-e-269; October 1945
- Green, L J; The
two-dimensional incompressible potential flow over corrugated and distorted
infinite surfaces; naca-wr-e-38; 1945
- Peters, M D; The
effect of high temperature of the cylinder head on the knocking tendency of an
air-cooled engine cylinder; naca-wr-e-39; February 1945
- Breisch, John H; Endurance tests
of a 22-inch-diameter pulse-jet engine with a neoprene-coated valve grid;
naca-wr-e-270; October 1945
- (Author(s) Not
Available); NACA
investigation of fuels corresponding to specification AN-F-58 : results of
studies in single combustors of J-33, J-34, J-35, and NENE turbojet
engines; naca-rm-e8k12; November 16, 1945
- Loitsianskii, L. G.; Some basic laws
of isotropic turbulent flow; naca-tm-1079; 1945
- Ris, V. F.; On
the automatic regulation of output in centrifugal compressors;
naca-tm-1081; 1945
- Mckinney, Elizabeth G;
Wind-tunnel
investigation of control-surface characteristics XXII : medium and large
aerodynamic balances of two nose shapes and a plain overhang used with a
0.20-airfoil-chord flap on an NACA 0009 airfoil; naca-wr-l-196; June
1945
- Crane, Robert M.; Computation of
hinge-moment characteristics of horizontal tails from section data;
naca-wr-a-11; 1945
- White, Maurice D.; Estimation of
stick-fixed neutral points of airplanes; naca-wr-l-116; 1945
- Spearman, M. Leroy.; Wind tunnel
investigation of control-surface characteristics XXIII : a 0.25-airfoil-chord
flap with tab having a chord twice the flap chord on an NACA 0009 airfoil;
naca-wr-l-47; 1945
- Fischel, Jack.; Hinge moments
of sealed-internal-balance arrangements for control surfaces II : experimental
investigation of fabric seals in the presence of a thin-plate overhang;
naca-wr-l-52; 1945
- Bielat, Ralph P.; A simple method
for estimating terminal velocity including effect of compressibility on
drag; naca-wr-l-78; 1945
- Kelly, Richard L; The
low-temperature solubility of 42 aromatic amines in aviation gasoline;
naca-wr-e-167; 1945
- Lyons, Richard E,
Coles, Willard D; Laboratory
investigation of icing in the carburetor and supercharger inlet elbow of an
aircraft engine III : heated air as a means of de-icing the carburetor and
supercharger inlet elbow; naca-wr-e-172; 1945
- Shames, Sidney J,
Howes, William; Determination
of air-consumption parameters for two radial aircraft engines;
naca-wr-e-193; 1945
- Brown, Kenneth D,
Richard, Paul H, Wilson, Robert W; Correlation
of the characteristics of single-cylinder and flight engines in tests of
high-performance fuels in an air-cooled engine II : knock-limited charge-air
flow and cylinder temperatures; naca-wr-e-272; 1945
- Hall, Eldon W; A
theoretical analysis of the performance of a diesel engine-compressor-turbine
combination for aircraft; naca-wr-e-31; 1945
- Hollingworth, Thomas A;
Investigation
of effect of sideslip on lateral stability characteristics III : rectangular
low wing on circular fuselage with variations in vertical-tail area and
fuselage length with and without horizontal tail surface; naca-wr-l-17;
1945
- Bird, J D; Effect
of leakage past aileron nose on aerodynamic characteristics of plain and
internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil;
naca-wr-l-172; 1945
- Cleary, Harold E; Effects of
compressibility on maximum lift coefficients for six propeller airfoils;
naca-wr-l-514; 1945
- MacDougall, George F,
Jr., Scheiter, Leslie E; Longitudinal-trim
tests of a 0.059-scale model of the Curtiss-Wright XP-55 airplane;
naca-wr-l-538; 1945
- Stowell, Elbridge Z,
Schwartz, Edward B, Houbolt, John C; Bending
and shear stresses developed by the instantaneous arrest of the root of a
cantilever beam rotating with constant angular velocity about a transverse
axis through the root; naca-wr-l-27; 1945
- S. B. Batdorf, Manuel
Stein, Charles Libove; Critical
combinations of longitudinal and transverse direct stress for an infinitely
long flat plate with edges elastically restrained against rotation;
naca-arr-l6a05a; March 1946
- Louis S. Stivers, Fred
J. Rice, Jr.; Aerodyanmic
Characteristics of Four NACA Airfoil Sections Designed for Helicopter Rotor
Blades; naca-rb-l5k02; February 1946
- Levy, Samuel (National
Bureau of Standards) Woolley, Ruth M (National Bureau of Standards) Corrick,
Josephine N (National Bureau of Standards); Analysis
of deep rectangular shear web above buckling load; naca-tn-1009; March
1946
- Jones, Robert T; Properties of
low-aspect-ratio pointed wings at speeds below and above the speed of
sound; naca-tn-1032; 1946
- Tsien, Hsue-Shen
(California Institute of Technology) Kuo, Yung-Huai (California Institute of
Technology); Two-dimensional
irrotational mixed subsonic and supersonic flow of a compressible fluid and
the upper critical Mach number; naca-tn-995; May 1946
- Richard T. Whitcomb; Investigation
of the characteristics of a high-aspect-ratio wing in the Langley 8-foot
high-speed tunnel; naca-rm-l6h28a; Aug 1946
- Charles Libove, Manuel
Stein; Charts for
Critical Combinations of Longitudinal and Transverse Direct Stress for Flat
Rectangular Plates; naca-arr-l6a05; March 1946
- Van Dyke, Milton D; Aerodynamic
characteristics including scale effect of several wings and bodies alone and
in combination at a Mach number of 1.53; naca-rm-a6k22; December 20,
1946
- Ferri, Antonio; Application of
the method of characteristics to supersonic rotational flow;
naca-report-841; 1946
- Ruffner, B F (Oregon
State College); Stress
analysis of columns and beam columns by the photoelastic method;
naca-tn-1002; March 1946
- Holt, Marshall
(Aluminum Company of America) Leary, J R (Aluminum Company of America); The column
strength of aluminum alloy 75S-T extruded shapes; naca-tn-1004;
1946
- Turner, P S (National
Bureau of Standards) Thomason, R H (National Bureau of Standards); Correlation
between strength properties in standard test specimens and molded phenolic
parts; naca-tn-1005; May 1946
- Bers, Lipman (Brown
University); Velocity
distribution on wing sections of arbitrary shape in compressible potential
flow I : symmetric flows obeying the simplified density-speed relation;
naca-tn-1006; April 1946
- Freeman, Hugh B; Boundary-layer-control
tests of two wings in the Langley Propeller-Research Tunnel; naca-tn-1007;
1946
- Miller, James A
(National Bureau of Standards); Stress-strain
and elongation graphs for aluminum alloy R301 sheet; naca-tn-1010;
February 1946
- Campbell, William R
(National Bureau of Standards); Errors
in indicated strain for a typical wire strain gage caused by restraining,
temperature changes, and weathering; naca-tn-1011; April 1946
- Bers, Lipman (Brown
University); Velocity
distribution on wing sections of arbitrary shape in compressible potential
flow II : subsonic symmetric adiabatic flows; naca-tn-1012; June
1946
- Hoff, N J (Polytechnic
Institute of Brooklyn) Boley, Bruno A (Polytechnic Institute of Brooklyn); Stresses in and
general instability of monocoque cylinders with cutouts I : experimental
investigation of cylinders with a symmetric cutout subjected to pure
bending; naca-tn-1013; 1946
- Ashkenas, I L; The
development of a lateral-control system for use with large-span flaps;
naca-tn-1015; 1946
- Theodorsen, Theodore
Naiman, Irven; Pressure
distributions for representative airfoils and related profiles;
naca-tn-1016; February 1946
- Stalder, Jackson R
Zeiller, E Lewis; A
method for the determination of air infiltration rates in airplane cabins;
naca-tn-1017; April 1946
- Bergman, Stefan (Brown
University); Methods for
determination and computation of flow patterns of a compressible fluid;
naca-tn-1018; September 1946
- Karabinos, Joseph V
Lamberti, Joseph M; The
synthesis and purification of aromatic hydrocarbons I : butylbenzene;
naca-tn-1019; 1946
- Ebersole, Earl R; The synthesis
and purification of aromatic hydrocarbons II : 1, 2, 4-trimethylbenzene;
naca-tn-1020; 1946
- Buess, C M Karabino, J
V Kunz, P V Gibbons, L C; The
synthesis and purification of aromatic hydrocarbons III : isobutylbenzene,
sec-butylebenzene and tert-butylbenzene; naca-tn-1021; June 1946
- Miller, James A
(National Bureau of Standards); A
fixture for compressive tests of thin sheet metal between lubricated steel
guides; naca-tn-1022; April 1946
- Slabey, Vernon A; The synthesis
of methylenecyclobutane, spiropentane, and 2-methyl-1-butene from
pentaerythrityl tetrabromide; naca-tn-1023; February 1946
- Robinson, J V (Stanford
University) Woods, W W (Stanford University); A
general method of selecting foam inhibitors; naca-tn-1025; May 1946
- Hottel, H C
(Massachusetts Institute of Technology) Williams, G C (Massachusetts Institute
of Technology); Charts
of thermodynamic properties of fluids encountered in calculations of internal
combustion engine cycles; naca-tn-1026; May 1946
- Leary, J R (Aluminum
Company of America) Holt, Marshall (Aluminum Company of America); Column
strength of aluminum alloy 14S-T extruded shapes and rod; naca-tn-1027;
May 1946
- Theodorsen, Theodore;
Extension of
the Chaplygin proofs on the existence of compressible-flow solutions to the
supersonic region; naca-tn-1028; March 1946
- Theodorsen, Theodore;
A condition
on the initial shock; naca-tn-1029; March 1946
- Jackson, L R (Battelle
Memorial Institute) Wilson, W M (University of Illinois) Moore, H F
(University of Illinois) Grover, H J (Battelle Memorial Institute); The
fatigue characteristics of bolted lap joints of 24S-T Alclad sheet
materials; naca-tn-1030; October 1946
- Warshawsky, Isidoro; A multiple
bridge for elimination of contact-resistance errors in resistance strain-gauge
measurements; naca-tn-1031; March 1946
- Garrick, I E; Bending-torsion
flutter calculations modified by subsonic compressibility corrections;
naca-tn-1034; May 1946
- Stanitz, John D Lucia,
Robert E Masselle, Francis L; Steady-
and intermittent-flow coefficients of poppet intake valves; naca-tn-1035;
March 1946
- Hartmann, E C (Aluminum
Company of America) Zamboky, A N (Aluminum Company of America); Comparison
of static strengths of machine countersunk riveted joints in 24S-T, X75S-T,
and Alclad 75S-T sheet; naca-tn-1036; May 1946
- Gilbert, Mitchell
Haddock, Gordon Metzler, Allen; A
study of combustion in a flowing gas; naca-tn-1037; April 1946
- Becker, John V Cooper,
Morton; Structural
hinge-moment increments caused by hinge-axis distortion; naca-tn-1038;
April 1946
- Nowick, A S Machlin, E
S; Quantitative
treatment of the creep of metals by dislocation and rate-process theories;
naca-tn-1039; April 1946
- Reid, Elliott G
(Stanford University); Wake
studies of eight model propellers; naca-tn-1040; July 1946
- Mcpherson, A E
(National Bureau of Standards) Levy, Samuel (National Bureau of Standards)
Zibritosky, George (National Bureau of Standards); Effect
of normal pressure on strength of axially loaded sheet-stringer panels;
naca-tn-1041; July 1946
- Campbell, William R
(National Bureau of Standards); Performance
tests of wire strain gages IV : axial and transverse sensitivities;
naca-tn-1042; June 1946
- Benser, William A
Wilcox, Ward W Voit, Charles H; Charts
for the rapid calculation of the work required to compress dry air;
naca-tn-1043; April 1946
- Spreiter, John R
Steffen, Paul J; Effect
of Mach and Reynolds numbers on maximum lift coefficient; naca-tn-1044;
March 28, 1946
- Neihouse, Jacob H
Lichtenstein, Jacob H Pepoon, Philip W; Tail-design
requirements for satisfactory spin recovery; naca-tn-1045; April
1946
- Letko, William Goodman,
Alex; Preliminary
wind-tunnel investigation at low speed of stability and control
characteristics of swept back wings; naca-tn-1046; April 1946
- Woolley, Ruth M
(National Bureau of Standards) Corrick, Josephine N (National Bureau of
Standards) Levy, Samuel (National Bureau of Standards); Clamped
long rectangular plate under combined axial load and normal pressure;
naca-tn-1047; June 1946
- Braslow, Albert L; Two dimensional
wind-tunnel investigation of low drag vertical-tail,horizontal-tail, and wing
sections equipped with sealed internally balanced control surfaces;
naca-tn-1048; April 1946
- Murray, Harry E; Wind-tunnel
investigation of end-plate effects of horizontal tails on a vertical tail
compared with available theory; naca-tn-1050; January 21, 1946
- Fleming, W A Dietz, R
O; Altitude-wind-tunnel
investigations of thrust augmentation of a turbojet engine performance with
tail-pipe burning; naca-rm-e6i20; September 25, 1946
- Maclachlan, Robert
Levitt, Joseph; Wind-tunnel
investigation of the effect of canopies on directional stability
characteristics of a single engine airplane model; naca-tn-1052; May
1946
- Sipko, Michael A
Cotton, Charles B Lusk, James B; Use
of ducked head baffles to reduce rear-row cylinder temperatures of an
air-cooled aircraft engine; naca-tn-1053; August 1946
- Lamb, J J (National
Bureau of Standards) Albrecht, Isabelle (National Bureau of Standards)
Axilrod, B M (National Bureau of Standards); Impact
strength and flexural properties of laminated plastics at high and low
temperatures; naca-tn-1054; August 1946
- Wright, Ray H
Donaldson, Coleman Dup; Comparison
of two-dimensional air flows about an NACA 0012 airfoil of 1-inch chord at
zero lift in open and closed 3-inch jets and corrections for jet-boundary
interference; naca-tn-1055; May 1946
- Dawson, John R Walter,
Robert C; The effects of
various parameters on the load at which spray enters the propellers of a
flying boat; naca-tn-1056; May 1946
- King, Douglas A Hill,
Mary A; General tank
tests of a 1/10-size model of the hull of the Boeing XPBB-1 flying boat -
Langley Tank Model 175; naca-tn-1057; July 1946
- Peterson, James P; Strain
measurements and strength tests of 25-inch diagonal-tension beams of 75S-T
aluminum alloy; naca-tn-1058; May 1946
- Ankenbruck, Herman O;
Effects of
tip dihedral on lateral stability and control characteristics as determined by
tests of a dynamic wind model in the Langley Free-Flight Tunnel;
naca-tn-1059; July 1946
- Phillips, William H; An
investigation of additional requirements for satisfactory elevator control
characteristics; naca-tn-1060; June 1946
- Tucker, Warren A; Wind tunnel
investigation of effect of wing location, power, and flap deflection on
effective dihedral of a typical single-engine fighter-airplane model with tail
removed; naca-tn-1061; May 1946
- Dawson, John R Walter,
Robert C Hay, Elizabeth S; Tank
tests to determine the effect of varying design parameters of planing-tail
hulls I : effect of varying length, width, and plan-form taper of
afterbody; naca-tn-1062; May 1946
- Levin, L Ross Nelson,
David H; Comparison of
measured and calculated stresses in built-up beams; naca-tn-1063; May
1946
- Boshar, John Davis,
Philip; Consideration
of dynamic loads on the vertical tail by the theory of flat yawing
maneuvers; naca-tn-1065; June 1946
- Kuhn, Paul Moggio,
Edwin M; Stresses around
large cut-outs in torsion boxes; naca-tn-1066; May 1946
- Neustein, Joseph
Schafer, Louis J , Jr; Comparison
of several methods of predicting the pressure loss at altitude across a
baffled aircraft-engine cylinder; naca-tn-1067; May 1946
- Ritter, William K
Ginsburg, Ambrose Redlitz, Alfred G; Effects
of axial-plane curvature and passage-area variation on flow capacity of
radial-discharge impeller with conventional inlet buckets; naca-tn-1068;
May 1946
- Marble, Frank E Ritter,
William K Miller, Mahlon A; Effect
of the NACA injection impeller on the mixture distribution of a double-row
radial aircraft engine; naca-tn-1069; May 1946
- Zerbe, John Selna,
James; An
empirical equation for the coefficient of heat transfer to a flat surface from
a plane heated-air jet directed tangentially to the surface; naca-tn-1070;
June 1946
- Heimerl, George J
Woods, Walter; Effect
of brake forming on the strength of 24S-T aluminum-alloy sheet;
naca-tn-1072; May 1946
- Theodorsen, Theodore;
Note on the
theorems of Bjerknes and Crocco; naca-tn-1073; May 1946
- Schueller, Carl F
Korycinski, Peter F Strass, H Kurt; Tests
of a full-scale horizontal tail surface in the Langley 16-foot high-speed
tunnel; naca-tn-1074; May 1946
- Luoma, Arvo A; Effect
of compressibility on section characteristics of an airfoil with a round-nose
slotted fraise aileron; naca-tn-1075; May 1946
- Bishop, Robert C Lomax,
Harvard; A
simplified method for determining from flight data the rate of change of
yawing-moment coefficient with sideslip; naca-tn-1076; June 1946
- Sivells, James C
Deters, Owen J; Jet-boundary
and plan-form corrections for partial-span models with reflection plane, end
plate, or no end plate in a closed circular wind tunnel; naca-tn-1077;
June 1946
- Gilbert, Mitchell
Howard, John N Hicks, Bruce L; An
analysis of the factors affecting the state of fuel and air mixtures;
naca-tn-1078; May 1946
- Lowry, John G Turner,
Thomas R; Pressure
distribution over a plug-type spoiler-slot aileron on a tapered wing with full
span slotted flaps; naca-tn-1079; June 1946
- Cotter, William E; Summary and
analysis of data on damping in yaw and pitch for a numbers of airplane
models; naca-tn-1080; May 1946
- Jones, Robert T
Margolis, Kenneth; Flow
over a slender body of revolution at supersonic velocities; naca-tn-1081;
July 08, 1946
- Hartwig, Frederick J ,
Jr; Comparative
effectiveness of a convection type and a radiation-type cooling cap on a
turbo-supercharger.; naca-tn-1082; June 1946
- Gustafson, F B G C
Myers, JR; Stalling of
helicopter blades; naca-tn-1083; June 1946
- Goranson, R Fabian; Flight tests of
experimental beveled-trailing-edge Frise ailerons on a fighter airplane;
naca-tn-1085; July 1946
- Czarnecki, K R
Pasamanick, Jerome; Langley
full-scale-tunnel investigation of the fuselage boundary layer on a typical
fighter airplane with a single liquid-cooled engine; naca-tn-1087; June
1946
- Soule, Hartley A; Influence of
large amounts of wing sweep on stability and control problems of aircraft;
naca-tn-1088; June 1946
- Hoff, N J (Polytechnic
Institute of Brooklyn) Boley, Bruno A (Polytechnic Institute of Brooklyn); The shearing
rigidity of curved panels under compression; naca-tn-1090; August
1946
- Locke, F W S , Jr
(Bureau of Aeronautics, Navy Department); An
analysis of the main spray characteristics of some full-size multi-engined
flying boats; naca-tn-1091; July 1946
- Bell, E Barton Morgan,
James E Disher, John H Mercer, Jack R; Flight
investigation of the cooling characteristics of a two-row radial engine
installation I : cooling correlation; naca-tn-1092; July 1946
- Shortal, Joseph A
Maggin, Bernard; Effect
of sweepback and aspect ratio on longitudinal stability characteristics of
wings at low speeds; naca-tn-1093; July 1946
- Mckinney, Marion O; Experimental
determination of the effects of dihedral, vertical-tail area, and lift
coefficient on lateral stability and control characteristics;
naca-tn-1094; July 1946
- Bergman, Stefan (Brown
University); On supersonic
and partially supersonic flows; naca-tn-1096; December 1946
- Nelson, David H; Effect of
change in cross section upon stress distribution in circular shell-supported
frames; naca-tn-1098; July 1946
- Braslow, Albert L; Two-dimensional
wind-tunnel investigation of sealed 0.22-airfoil-chord internally balanced
ailerons of different contour on an NACA 65(112)- 213 airfoil;
naca-tn-1099; July 1946
- Dawson, John R Mckann,
Robert Hay, Elizabeth S; Tank
tests to determine the effect of varying design parameters of planing-tail
hulls II : effect of varying depth of step, angle of after- body keel, length
of afterbody chine, and gross load; naca-tn-1101; July 1946
- Kittel, Howard; The crystal
structure at room temperature of eight forged heat-resisting alloys;
naca-tn-1102; July 1946
- Budiansky, Bernard Hu,
Pai C; The
Lagrangian multiplier method of finding upper and lower limits to critical
stresses of clamped plates; naca-tn-1103; July 1946
- Drake, Hubert; Experimental
determination of the effects of directional stability and rotary damping in
yaw on lateral stability and control characteristics; naca-tn-1104; July
1946
- Sanders, Newell D; Performance
parameters for jet-propulsion engines; naca-tn-1106; July 1946
- Shaw, Milton C Macks, E
Fred; Load
capacity of aluminum-alloy crankpin bearings as determined in a centrifugal
bearing test machine; naca-tn-1108; September 1946
- Morgan, James E Hill, E
John Blackman, Calvin C; Flight
investigation of the cooling characteristics of a two-row radial engine
installation II : cooling-air pressure recovery and pressure distribution;
naca-tn-1109; July 1946
- Braslow, Albert L
Loftin, Laurence K , Jr; Two-dimensional
wind-tunnel investigation of an approximately 14-percent-thick NACA
66-series-type airfoil section with a double slotted flap; naca-tn-1110;
August 1946
- Corson, Blake W
Maynard, Julian D; Investigation
of the effect of a tip modification and thermal de-icing air flow on propeller
performance; naca-tn-1111; July 1946
- Corson, Blake W
Maynard, Julian D; Analysis
of propeller efficiency losses associated with heated-air thermal
de-icing; naca-tn-1112; July 1946
- Wood, George P; Calculation of
surface temperatures in steady supersonic flight; naca-tn-1114; December
1946
- Lees, Lesters
(California Institute of Technology, Pasadena, California) Lin, Chia Chiao
(California Institute of Technology, Pasadena, California); Investigation
of the stability of the laminar boundary layer; naca-tn-1115; September
1946
- Faldetta, Richard D
Holms, Authur G; Strain-gage
study of internally cooled exhaust valves having various throat designs;
naca-tn-1116; August 1946
- Machlin, E S Nowick, A
S; Stress
rupture of heat resisting alloys as a rate process; naca-tn-1126;
September 1946
- Kleckner, Harold F; Flight tests of
an all-movable horizontal tail with geared unbalancing tabs on the Curtiss
XP-42 airplane; naca-tn-1139; October 1946
- Purser, Paul E Spear,
Margaret F; Tests to
determine effects of slipstream rotation on the lateral stability
characteristics of a single-engine low-wing aircraft model; naca-tn-1146;
September 1946
- Adams, Richard E
Silsby, Norman S; Flight
investigation of the effect of a local change in wing contour on chordwise
pressure distribution at high speeds; naca-tn-1152; September 1946
- Cook, Harvey A Held,
Louis F Pritchard, Ernest I; Comparison
of relative sensitivities of the knock limits of two fuels to six engine
variables; naca-tn-1117; August 1946
- Heimerl, George J
Woods, Walter; Increasing
the compressive strength of 24S-T aluminum-alloy sheet by flexure rolling;
naca-tn-1119; August 1946
- Aiken, William S; Standard
nomenclature for airspeeds with tables and charts for use in calculation of
airspeed; naca-tn-1120; September 1946
- Robinson, Harold L; High-speed
investigation of skin wrinkles on two NACA airfoils; naca-tn-1121; August
1946
- Hu, Pai C Lundquist,
Eugene E Batdorf, S B; Effect
of small deviations from flatness on effective width and buckling of plates in
compression; naca-tn-1124; September 1946
- Crate, Harold
Ochiltree, David W Graves, Walter T; Effect
of ratio of rivet pitch to rivet diameter on the fatigue strength of riveted
joints of 24S-T aluminum alloy sheet; naca-tn-1125; September 1946
- Lees, Lester; A
discussion of the application of the Prandtl-Glauert method to subsonic
compressible flow over a slender body of revolution; naca-tn-1127;
September 1946
- Barlow, William H; Flight
investigation at high speeds of the drag of three airfoils and a circular
cylinder representing full-scale propeller shanks; naca-tn-1129; September
1946
- Reynolds, E E
(University of Michigan) Freeman, J W (University of Michigan) White, A E
(University of Michigan); Evaluation
of two high-carbon precision-cast alloys at 1700 and 1800 F by the rupture
test; naca-tn-1130; September 1946
- Male, Donald W; The effect of
engine variables on the prediction-limited performance of three fuels;
naca-tn-1131; September 1946
- Clark, Thomas P
Vierthaler, Walter A; An
electron microscope study of used nitrated-steel piston rings;
naca-tn-1132; September 1946
- Manson, S S Morgan, W
C; Effect of
misalignment of strain-gage components of strain rosettes; naca-tn-1133;
September 1946
- Von Glahn, Uwe Renner,
Clark E; Development of
a protected air scoop for the reduction of induction-system icing;
naca-tn-1134; September 1946
- (Author(s) Not
Available); Standard
procedures for rating and testing multistage axial-flow compressors;
naca-tn-1138; September 1946
- Westfall, John R; Measurements of
landing-gear forces and horizontal-tail loads in landing tests of a large
bomber-type airplane; naca-tn-1140; September 1946
- Peiser, A M Walker, W
G; An
analysis of the airspeeds and normal accelerations of Boeing S-307 airplanes
in commercial transport operation; naca-tn-1141; September 1946
- Peiser, A M; An
analysis of the airspeeds and normal accelerations of Douglas DC-3 airplanes
in commercial transport operation; naca-tn-1142; September 1946
- Theodorsen, Theodore
Regier, Arthur A; The
problem of noise reduction with reference to light airplanes;
naca-tn-1145; August 1946
- Rennak, Robert M
Messing, Wesley E Morgan, James E; Flight
investigation of the cooling characteristics of a two-row radial engine
installation III : engine temperature distribution; naca-tn-1147; October
1946
- Guentert, D C Todd, D J
Simmons, W P , Jr; Flow
tests of an NACA-designed supercharger inlet elbow and the effects of various
components on the flow characteristics at the elbow outlet; naca-tn-1148;
October 1946
- Turner, L Richard
Lowdermilk, Warren H Lord, Albert M; Performance
of hoods for aircraft exhaust-gas turbines; naca-tn-1149; November
1946
- Hu, Pai C Libove,
Charles; A
relaxation procedure for the stress analysis of a continuous beam-column
elastically restrained against deflection and rotation at the supports;
naca-tn-1150; October 1946
- Sanders, J C Sanders, N
D; A
preliminary study of a propeller powered by gas jets issuing from the blade
tips; naca-tn-1155; November 1946
- Schuette, Evan H Barab,
Sual Mccracken, Howard L; Compressive
strength of 24S-T aluminum-alloy flat panels with longitudinal formed
hat-section stiffeners; naca-tn-1157; December 1946
- Maggin, Bernard Shanks,
Robert E; The effect of
geometric dihedral on the aerodynamic characteristics of a 40 degree
swept-back wing of aspect ratio 3; naca-tn-1169; December 1946
- Hoff, N J (Polytechnic
Institute of Brooklyn) Libby, Paul A (Polytechnic Institute of Brooklyn)
Klein, Bertran (Polytechnic Institute of Brooklyn); Numerical
procedures for the calculation of the stresses in monocoques III : calculation
of the bending moments in fuselage frames; naca-tn-998; 1946
- Hoff, N J (Polytechnic
Institute of Brooklyn) Klein, Bertram (Polytechnic Institute of Brooklyn)
Libby, Paul A (Polytechnic Institute of Brooklyn); Numerical
procedures for the calculation of the stresses in monocoques IV : influence
coefficients of curved bars for distortions in their own plane;
naca-tn-999; April 1946
- Kaplan, Carl; Effect
of compressibility at high subsonic velocities on the lifting force acting on
an elliptic cylinder; naca-report-834; 1946
- Jones, Robert T; Properties of
low-aspect-ratio pointed wings at speeds below and above the speed of
sound; naca-report-835; 1946
- Garrick, I E; Bending-torsion
flutter calculations modified by subsonic compressibility corrections;
naca-report-836; 1946
- Aiken, William S , Jr;
Standard
nomenclature for airspeeds with tables and charts for use in calculation of
airspeed; naca-report-837; 1946
- Boshar, John Davis,
Philip; Consideration
of dynamic loads on the vertical tail by the theory of flat yawing
maneuvers; naca-report-838; 1946
- Brown, Clinton E; Theoretical
lift and drag of thin triangular wings at supersonic speeds;
naca-report-839; 1946
- Gustafson, F B Myers, G
C , Jr; Stalling of
helicopter blades; naca-report-840; 1946
- Perl, W Epstein, H T;
Some effects
of compressibility on the flow through fans and turbines; naca-report-842;
1946
- Sivells, James C
Deters, Owen J; Jet-boundary
and plan-form corrections for partial-span models with reflection-plane,
end-plate, or no end-plate in a closed circular wind tunnel;
naca-report-843; 1946
- Dawson, John R Walter,
Robert C Hay, Elizabeth S; Tank
tests to determine the effect on planing-tail hulls of varying length, width,
and plan-form taper of afterbody; naca-report-844; 1946
- Nowick, A S Machlin, E
S; Quantitative
treatment of the creep of metals by dislocation and rate-process theories;
naca-report-845; 1946
- Garrick, I E Rubinow, S
I; Flutter
and oscillating air-force calculations for an airfoil in two-dimensional
supersonic flow; naca-report-846; October 1946
- Batdorf, S B Houbolt,
John C; Critical
combinations of shear and transverse direct stress for an infinitely long flat
plate with edges elastically restrained against rotation; naca-report-847;
1946
- Budiansky, Bernard Hu,
Pai C; The
Lagrangian multiplier method of finding upper and lower limits to critical
stresses of clamped plates; naca-report-848; 1946
- Vincenti, Walter G
Graham, Donald J; The
effect of wall interference upon the aerodynamic characteristics of an airfoil
spanning a closed-throat circular wind tunnel; naca-report-849;
1946
- Shaw, Milton C
Nussdorfer, Theodore; A
visual photographic study of cylinder lubrication; naca-report-850;
1946
- Jones, Robert T; Thin oblique
airfoils at supersonic speed; naca-report-851; 1946
- Barlow, William H; Flight
investigation at high speeds of the drag of three airfoils and a circular
cylinder representing full-scale propeller shanks; naca-report-852;
1946
- Pinkel, Benjamin
Manganiello, Eugene J Bernardo, Everett; Cylinder-temperature
correlation of a single-cylinder liquid-cooled engine; naca-report-853;
1946
- Turner, William N
Steffen, Paul J Clousing, Lawrence A; Compressibility
effects on the longitudinal stability and control of a pursuit-type airplane
as measured in flight; naca-report-854; 1946
- Miller, Cearcy D; Relation
between spark-ignition engine knock, detonation waves, and autoignition as
shown by high-speed photography; naca-report-855; 1946
- Miller, Cearcy D; The NACA
high-speed motion-picture camera optical compensation at 40,000 photographs
per second; naca-report-856; 1946
- Miller, Cearcy D Olsen,
H Lowell Logan, Walter O , Jr Osterstrom, Gordon E; Analysis
of spark-ignition engine knock as seen in photographs taken at 200,000 frames
per second; naca-report-857; 1946
- Neustein, Joseph
Schafer, Louis J , Jr; Comparison
of several methods of predicting the pressure loss at altitude across a
baffled aircraft-engine cylinder; naca-report-858; 1946
- Clousing, Lawrence A
Turner, William N Rolls, L Stewart; Measurements
in flight of the pressure distribution on the right wing of a pursuit-type
airplane at several values of Mach number; naca-report-859; 1946
- Marble, Frank E Miller,
Marlon A Bell, E Barton; Analysis
of cooling limitations and effect of engine-cooling improvements on
level-flight cruising performance of four-engine heavy bomber;
naca-report-860; 1946
- Bullock, Robert O
Wilcox, Ward W Moses, Jason J; Experimental
and theoretical studies of surging in continuous-flow compressors;
naca-report-861; 1946
- Jones, Alun R; An
investigation of a thermal ice-prevention system for a twin-engine transport
airplane; naca-report-862; 1946
- Harrison, L P (U.S.
Weather Bureau); Lightning
discharges to aircraft and associated meteorological conditions;
naca-tn-1001; May 1946
- Emmons, Howard W
(Harvard University); The
theoretical flow of a frictionless, adiabatic, perfect gas inside of a
two-dimensional hyperbolic nozzle; naca-tn-1003; May 1946
- Jones, Robert T; Wing plan forms
for high-speed flight; naca-tn-1033; March 1946
- Crandall, Stewart M
Murray, Harry E; Analysis
of available data on the effects of tabs on control-surface hinge moments;
naca-tn-1049; May 1946
- Quinn, John H , Jr; Wind-tunnel
investigation of boundary-layer control by suction on the NACA 653-418, a =
1.0 airfoil section with a 0.29-airfoil-chord double slotted flap;
naca-tn-1071; June 1946
- Corson, Blake W
Maynard, Julian D; The
effect of simulated icing on propeller performance; naca-tn-1084; June
1946
- Turner, Richard L Lord,
Albert M; Thermodynamic
charts for the computation of combustion and mixture temperatures at constant
pressure; naca-tn-1086; June 1946
- Jones, Robert T; Thin oblique
airfoils at supersonic speed; naca-tn-1107; September 1946
- Garrick, I E Rubinow, S
I; Flutter
and oscillating air-force calculations for an airfoil in a two-dimensional
supersonic flow; naca-tn-1158; October 1946
- Bartoo, Edward R; Turbosupercharger-rotor
temperature in flight; naca-tn-1159; October 1946
- Cleaves, Alden P
Sherrick, Mildred E; The
infrared spectra of spiropentane methylenecyclobutane and
2-methyl-1-butene; naca-tn-1160; October 1946
- Lamberti, J M Reynolds,
T W Chanan, H H; The
synthesis and purification of aromatic hydrocarbons IV :
1,2,3-trimethylbenzene; naca-tn-1163; November 1946
- Ebersole, Earl R; The synthesis
and purification of aromatic hydrocarbons V : 1-ethyl-3-methylbenzene;
naca-tn-1164; November 1946
- Kunen, Alfred E
Hartwig, Frederick J Bressman, Joseph R; Tensile
properties of a sillimanite refractory at elevated temperatures;
naca-tn-1165; November 1946
- Reisert, Thomas D; An analysis of
the fatigue life of an airplane wing structure under overload conditions;
naca-wr-l-10; February 1946
- Foster, Gerald V; Wind-tunnel
investigation of an NACA 66-series 16-percent-thick low-drag tapered wing with
Fowler and split flaps; naca-wr-l-134; 1946
- Adler, Alfred A; Variation with
Mach number of static and total pressures through various screens;
naca-wr-l-23; February 1946
- Rickey, E A; Tests
of a 1/7-scale powered model of the Kaiser tailless airplane in the Langley
full-scale tunnel; naca-wr-l-531; March 1946
- Chapman, Gilbert E; Laboratory
investigation of icing in the carburetor and supercharger inlet elbow of an
aircraft engine VI : effect of modifications to fuel-spray nozzle on icing
characteristics; naca-wr-e-175; 1946
- Ellisman, Carl; Investigation
of ice formation in the induction system of an aircraft engine I : ground
tests; naca-wr-e-176; March 1946
- Zlotowski, Edward D; Investigation
of ice formation in the induction system of an aircraft engine II : flight
tests; naca-wr-e-177; June 1946
- Niemi, Richard O; The effect of
ethylene dibromide on the knock-limited performance of leaded and nonleaded S
reference fuel; naca-wr-e-183; February 1946
- Conrad, E William; An
investigation of cowl-flap and cowl-outlet designs for the Boeing B-29
power-plant installation; naca-wr-e-206; 1946
- Robert W. Wilson, Paul
H. Richard, Kenneth D. Brown; Correlation
of the Characteristics of Single-Cylinder and Flight Engines in Test of
High-Performance Fuels in an Air-Cooled Engine I- Cooling Characteristics;
naca-wr-e-271; July 1946
- Jagger, James M; Altitude-wind-tunnel
tests of power-plant installation in jet-propelled fighter; naca-wr-e-274;
February 1946
- Schwartz, Irving R; Tests of cast
aluminum-alloy mixed-flow impellers; naca-wr-e-277; April 1946
- Lieblein, Seymour; Hydraulic
characteristics of the NACA injection impeller; naca-wr-e-278; May
1946
- Anderson, Roy I; Single-cylinder
engine tests of porous chrome-plated cylinder barrels with special bore
coatings for radial air-cooled engines; naca-wr-e-28; 1946
- Zlotowski, E E; Laboratory
investigation of icing in the carburetor and supercharger inlet elbow of an
aircraft engine IV : effect of throttle design and method of throttle
operation on induction-system icing characteristics; naca-wr-e-284;
1946
- Dugan, Paul D; Air-flow
and performance characteristics of engine-stage supercharger of a double-row
radial aircraft engine II : effect of design variables; naca-wr-e-285;
August 1946
- Perchonok, Eugene
Wilcox, Fred A Sterbentz, William H; Investigation
of the performance of a 20-inch ram jet using preheated fuel;
naca-rm-e6i23; October 28, 1946
- Mattson, Axel T; Investigation
of dive brakes and a dive-recovery flap on a high-aspect-ratio wing in the
Langley 8-foot high-speed tunnel; naca-rm-l6h28c; August 28, 1946
- Pretsch, J.; Calibration
tunnel for high speed; naca-tm-1103; 1946
- Saari, Martin J.,
Wallner, Lewis. E.; Altitude-wind-tunnel
investigation of performance of several propellers on YP-47M airplane at high
blade loading IIAeroproducts H20C-162-X11M2 four-blade propeller;
naca-rm-e6i24; 1946
- Pfender, John. F.; Effect of fuel
composition, engine operating variables, and spark-plug type and condition on
preignition-limited performance of an R-2800 cylinder; naca-rm-e6j08;
1946
- Wallner, Lewis. E.,
Sorin, Solomon. M.; Altitude-wind-tunnel
investigation of performance of several propellers on YP-47M airplane at high
blade loading. II :Curtiss 838-1C2-18R1 four-blade propeller;
naca-rm-e6j14; 1946
- Downing, Richard. M.,
Finger, Harold. B.; Effect
of three modifications on performance of auxiliary-stage supercharger for
V-1710-93 engine; naca-rm-e6j18; 1946
- Saari, Martin. J.,
Sorin, Solomon. M.; Altitude-wind-tunnel
investigation of performance of several propellers on YP-47M airplane at high
blade loadings IV :Curtiss 732-1C2-0 four-blade propeller; naca-rm-e6j23;
1946
- Saari, Martin. J.,
Wallner, Lewis. E.; Altitude-wind-tunnel
investigation of performance of several propellers on YP-47M airplane at high
blade loadings V :Curtiss 836-14C2-18R1 four-blade propeller /Martin J. Saari
and Lewis E. Wallner; naca-rm-e6j31; 1946
- Douglas, John. E.,
Schwartz, Irving. R.; Performance
of the modified V-1710-93 engine-stage supercharger with a constant-area
vaneless diffuser; naca-rm-e6k22; 1946
- Saari, Martin. J.,
Sorin, Solomon. M.; Altitude-wind-tunnel
investigation of performance of several propellers on YP-47M airplane at high
blade loadings VI :Hamilton Standard 6507A-2 four- and three-blade
propellers; naca-rm-e6k26; 1946
- Downing, Richard M.,
Finger, Harold B.; Performance
of the 19XB 10-stage axial flow compressor; naca-rm-e6l04; 1946
- Mulholland, Donald R.,
Zlotowski, Edward D.; Investigation
of operating characteristics of an engine equipped with modifications to
eliminate fuel-evaporation icing; naca-rm-e6l04a; 1946
- Fleming, William A.; Characteristics
of a hot jet discharged from a jet-propulsion engine; naca-rm-e6l27a;
1946
- Kuhl, R., Raab, K.; A photographic
profile recorder for airscrews and wing models; naca-tm-1088; 1946
- Fischer, Karl; Investigation
of flow in a centrifugal pump; naca-tm-1089; 1946
- Di Guidonia, Atti; The effect on
the Sperry directional gyro in turning; naca-tm-1091; 1946
- von Karman, Th.; On Laminar and
Turbulent Friction; naca-tm-1092; 1946
- Podorozhny, A. A.; Investigation
of the behavior of thin-walled panels with cutouts; naca-tm-1094;
1946
- Rollin, Vern G; The effect of
liquid and ice particles on the erosion of a supercharger-inlet cover and
diffuser vanes; naca-wr-e-178; June 1946
- Bressman, Joseph R; The effect of a
low-loss air valve on performance of a 22-inch-diameter pulse-jet engine;
naca-wr-e-279; June 12, 1946
- Kuenzig, John K,
Palter, H; Aerodynamics of
the carburetor air scoop and the engine cowling of a single engine
torpedo-bomber type airplane; naca-wr-e-280; June 1946
- G. Stamm; Investigations
of Pressure Distribution on Fast Flying Bodies; naca-tm-1101; 1946
- H. Falk; The
Influence of the Jet of a Propulsion Unit on Nearby Wings; naca-tm-1104;
1946
- B. Gothert; Plane
and Three Dimensional Flow at High Subsonic Speeds; naca-tm-1105;
1946
- Chapman G. E.,
Zlotowski, E E; Laboratory
investigation of icing in the carburetor and supercharger inlet elbow of an
aircraft engine IV : effect of throttle design and method of throttle
operation on induction-system icing characteristics; naca-wr-e-173;
1946
- Monroe, Louis L, Saari,
Martin J; An
investigation of cowl inlets for the B-29 power-plant installation;
naca-wr-e-205; 1946
- White, H. Jack, Gammon,
Goldie L; Correlation of
mixture temperature data obtained from bare intake-mani; naca-wr-e-273;
1946
- Barnett, Henry C; An evaluation
of the knock-limited performance of triptane; naca-wr-e-276; 1946
- Coulter, Earl E,
Larkin, Robert G., Gabriel, David S; Efficiency
of a radial-flow exhaust-gas turbosupercharger turbine with a 12.75-inch tip
diameter; naca-wr-e-281; 1946
- Valerino, Michael F,
Essig, Robert H, Hughes, Richard F; The
effect of increase in combustion-air inlet temperature from 80 to 130 F on the
sea-level performance of a 22-inch-diameter pulse-jet engine;
naca-wr-e-283; 1946
- Stivers, Louis S, Jr,
Rice, Fred J , Jr; Aerodynamic
characteristics of four NACA airfoil sections designed for helicopter rotor
blades; naca-wr-l-29; 1946
- Cahill, Jones F; Aerodynamic
data for a wing section of the Republic XF-12 airplane equipped with a double
slotted flap; naca-wr-l-544; 1946
- Batdorf, S B
Schildcrout, Murry Stein, Manuel; Critical
stress of thin-walled cylinders in axial compression; naca-report-887;
1947
- Stein, Manuel Neff,
John; Buckling
stresses of simply supported rectangular flat plates in shear;
naca-tn-1222; March 1947
- Batdorf, S B
Schildcrout, Murry Stein, Manuel; Critical
shear stress of long plates with transverse curvature; naca-tn-1346; June
1947
- Jack Fischel, Leslie E.
Schneiter; High-speed
wind-tunnel investigation of high lift and aileron-control characteristics of
an NACA 65-210 semi-span wing; naca-tn-1473; Nov 1947
- Paul E. Purser,
Margaret F. Spear; Wind-tunnel
investigation of effects of unsymmetrical horizontal-tail arrangements on
power-on static longitudinal stability of a single-engine airplane model;
naca-tn-1474; Oct 1947
- Herman O. Ankenbruck,
Marion O. Mckinney, Jr; Generalized
performance comparison of large conventional, tail boom, and tailless
airplanes; naca-tn-1477; Oct 1947
- John B. Garvin; Flight
measurements of aerodynamic loads on the horizontal tail surface of a
fighter-type airplane; naca-tn-1483; Nov 1947
- John C. Evvard, L.
Richard Turner; Theoretical
lift distribution and upwash velocities for thin wings at supersonic
speeds; naca-tn-1484; Nov 1947
- Herman H. Ellerbrock,
Jr, Chester R. Wcislo, Howard E. Dexter; Analysis,
verification, and application of equations and procedures for design of
exhaust-pipe shrouds; naca-tn-1495; Dec 1948
- J. Howard Kittel; Comparison of
crystal structures of 10 wrought heat resisting alloys at elevated
temperatures with their crystal structures at room temperatures;
naca-tn-1488; Nov 1947
- Richard P. Krebs, John
Palasics; Analytical
comparison of a standard turbojet engine, a turbojet engine with a tail-pipe
burner, and a ram-jet engine; naca-rm-e6l11; Feb 1947
- Eugene Perchonok,
William H. Sterbentz, Fred A. Wilcox; Performance
of a 20-inch steady-flow ram jet at high altitudes and ram-pressure
ratios; naca-rm-e6l06; Jun 1947
- Carl A. Sandahl; Free-flight
investigation of fullspan, 0.2 chord plain ailerons at high subsonic,
transonic, and supersonic speeds to determine some effects of wing sweepback,
taper, aspect ratio, and section-thickness ratio; naca-rm-l7f30; Aug
1947
- William N. Gardner,
Howard J. Curfman, Jr.; Flight
investigation to determine the hinge moments of a beveled-edge aileron on a 45
degree sweptback wing at transonic and low supersonic speeds;
naca-rm-l7h26; Nov 1947
- Anderson, Roger A; Determination
of coupled modes and frequencies of swept wings by use of power series;
naca-rm-l7h28; October 20, 1947
- James J. Gallagher,
James N. Mueller; Preliminary
tests to determine the maximum lift of wings at supersonic speeds;
naca-rm-l7j10; Dec 1947
- Macon C. Ellis, Jr.,
Lowell E. Hasel, Carl E. Grigsby; Supersonic-tunnel
tests of two supersonic airplane model configurations; naca-rm-l7j15; Dec
1947
- S. B. Batdorf, Manuel
Stein; Critical
combinations of shear and direct stress for simply supported rectangular flat
plates; naca-tn-1223; Mar 1947
- S. Katzoff, Robert S.
Finn, James C. Laurence; Interference
method for obtaining the potential flow past an arbitrary cascade of
airfoils; naca-tn-1252; May 1947
- Reginald B. Bland, T.
D. Reisert; An application
of statistical data in the development of gust-load criterions;
naca-tn-1268; Apr 1947
- James C. Sivells,
Robert H. Neely; Method
for calculating wing characteristics by lifting-line theory using nonlinear
section lift data; naca-tn-1269; Apr 1947
- Charles V. Bennett,
Joseph L. Johnson; Experimental
determination of the damping in roll and aileron rolling effectiveness of
three wings having 2 degree, 42 degree and 62 degree sweepback;
naca-tn-1278; May 1947
- Leonard Sternfield; Some
considerations of the lateral stability of high-speed aircraft;
naca-tn-1282; May 1947
- W. E. Moeckel; Theoretical
aerodynamic coefficients of two-dimensional supersonic biplanes;
naca-tn-1316; Jun 1947
- J. Mayo Greenberg; Some
considerations on an airfoil in an oscillating stream; naca-tn-1372; Aug
1947
- S. Katzoff, Harriet E.
Bogdonoff, Howard Boyet; Comparisons
of theoretical and experimental lift and pressure distributions on airfoils in
cascade; naca-tn-1376; Jul 1947
- Paul E. Purser, M.
Leroy Spearman, William R. Bates; Preliminary
investigation at low speed of downwash characteristics of small-scale
sweptback wings; naca-tn-1378; Jul 1947
- John C. Evvard; Distribution of
wave drag and lift in the vicinity of wing tips at supersonic speeds;
naca-tn-1382; Jul 1947
- Norris F. Dow, William
A. Hickman; Effect of
variation in diameter and pitch of rivets on compressive strength of panels
with Z-section stiffeners - panels of various lengths with close stiffener
spacing; naca-tn-1421; Sep 1947
- William A. Hickman,
Norris F. Dow; Compressive
strength of 24S-T aluminum-alloy flat panels with longitudinal formed
hat-section stiffeners having a ratio of stiffener thickness to skin thickness
equal to 1.00; naca-tn-1439; Sep 1947
- Samuel J. Rosenfeld; Analytical and
experimental investigation of bolted joints; naca-tn-1458; Oct 1947
- Nicholas H. Van Dorn,
John Deyoung; A
comparison of three theoretical methods of calculating span load distribution
on swept wings; naca-tn-1476; Nov 1947
- Neal Tetervin; Boundary-layer
momentum equations for three-dimensional flow; naca-tn-1479; Oct
1947
- George J. Heimerl; Determination
of plate compressive strengths; naca-tn-1480; Dec 1947
- Sidney R. Alexander; Results of
tests to determine the effect of a conical windshield on the drag of a bluff
body at supersonic speeds; naca-rm-l6k08a; Jan 1947
- Charles W. Mathews, Jim
Rogers Thompson; Drag
measurements at transonic speeds of NACA 65-009 airfoils mounted on a freely
falling body to determine the effects of sweepback and aspect ratio;
naca-rm-l6k08c; Jan 1947
- Macon C. Ellis, Jr.,
Lowell E. Hase; Preliminary
tests at supersonic speeds of triangular and swept-back wings;
naca-rm-l6l17; Feb 1947
- Paul E. Purser, M.
Leroy Spearman; Wind-tunnel
tests at low speed of swept and yawed wings having various plan forms.;
naca-rm-l7d23; May 1947
- George P. Wood; Performance
possibilities of the turbojet system as a power plant for supersonic
airplanes; naca-rm-l7h05a; Aug 1947
- Huntsberger, Ralph F;
A study of
several parameters controlling the trajectories of a supersonic antiaircraft
missile powered with solid- or liquid-fuel rockets; naca-rm-a6g22; April
24, 1947
- Brown, Harvey H
Rathert, George A , Jr Clousing, Lawrence A; Flight-test
measurements of aileron control surface behavior at super critical Mach
numbers; naca-rm-a7a15; April 23, 1947
- Chapman, Dean R
Perkins, Edward W; Experimental
investigation of the effects of viscosity on the drag of bodies of revolution
at a Mach number 1.5; naca-rm-a7a31a; April 03, 1947
- Nitzberg, Gerald E
Sluder, Loma E; An
empirically derived method for calculating pressure distribution at
supercritical Mach numbers and moderate angles of attack; naca-rm-a7b07;
April 1947
- Stivers, Louis S , Jr
Adams, Charles N , Jr; High-speed
wind-tunnel investigation of the effects of compressibility on a pitot-static
tube; naca-rm-a7f12; August 04, 1947
- Ilk, Richard J; Characteristics
of a 15-percent-chord and a 35-percent-chord plain flap on the NACA 0006
airfoil section at high subsonic speeds; naca-rm-a7h19; October 02,
1947
- Gault, Donald E; An experimental
investigation of NACA submerged air inlets on a 1/5-scale model of a fighter
airplane; naca-rm-a7i06; December 05, 1947
- Vincenti, Walter G
Nielsen, Jack N Matteson, Frederick H; Investigation
of wing characteristics at a Mach number of 1.53 I : triangular wings of
aspect ratio 2; naca-rm-a7i10; December 19, 1947
- Ilk, Richard J; High-speed
aerodynamic characteristics of four thin NACA 63-series airfoils;
naca-rm-a7j23; December 31, 1947
- Moeckel, W E Connors, J
F Schroeder, A H; Investigation
of shock diffusers at Mach number 1.85 I : projecting single-shock cones;
naca-rm-e6k27; June 17, 1947
- Bohanon, H R Wilcox, E
C; Theoretical
investigation of thrust augmentation of turbojet engines by tail-pipe
burning; naca-rm-e6l02; January 28, 1947
- Moeckel, W E Connors, J
F Schroeder, A H; Investigation
of shock diffusers at Mach number 1.85 II : projecting double-shock cones;
naca-rm-e6l13; June 17, 1947
- Evvard, John C Blakey,
John W; The
use of perforated inlets for efficient supersonic diffusion;
naca-rm-e7c26; June 25, 1947
- Gabriel, David S
Martinson, E Vincent Essig, Robert H; Experimental
investigation of performance and operating characteristics of a tail-pipe
burner for a turbojet engine; naca-rm-e7g03; October 30, 1947
- Jones, Robert J; Wing plan forms
for high-speed flight; naca-report-863; 1947
- Holms, Arthur G
Faldetta, Richard D; Effects
of temperature distribution and elastic properties of materials on
gas-turbine-disk stresses; naca-report-864; 1947
- Sivells, James C Neely,
Robert H; Method for
calculating wing characteristics by lifting-line theory using nonlinear
section lift data; naca-report-865; 1947
- Shaw, M C Nussdorfer, T
J , Jr; An
analysis of the full-floating journal bearing; naca-report-866;
1947
- Milwitzky, Benjamin; A theoretical
investigation of hydrodynamic impact loads on scalloped-bottom seaplanes and
comparisons with experiment; naca-report-867; 1947
- Toll, Thomas A; Summary of
lateral-control research; naca-report-868; 1947
- Goldstein, Arthur W
Jerison, Meyer; Isolated
and cascade airfoils with prescribed velocity distribution;
naca-report-869; 1947
- Parkinson, John B
Olson, Roland E Harr, Marvin I; Tank
investigation of a powered dynamic model of a large long-range flying
boat; naca-report-870; 1947
- Manson, S S; Determination
of elastic stresses in gas-turbine disks; naca-report-871; 1947
- Garrick, I E Rubinow, S
I; Theoretical
study of air forces on an oscillating or steady thin wing in a supersonic main
stream; naca-report-872; July 1947
- Manganiello, Eugene J
Valerino, Michael F Bell, E Barton; High-altitude
flight cooling investigation of a radial air-cooled engine;
naca-report-873; 1947
- Batdorf, S B; A
simplified method of elastic-stability analysis for thin cylindrical
shells; naca-report-874; 1947
- Orlin, W James Lindner,
Norman J Butterly, Jack G; Application
of the analogy between water flow with a free surface and two-dimensional
compressible gas flow; naca-report-875; 1947
- Lees, Lester; The
stability of the laminar boundary layer in a compressible fluid;
naca-report-876; 1947
- Hamilton, William T
Nelson, Warren H; Summary
report on the high-speed characteristics of six model wings having NACA
65sub1-series sections; naca-report-877; 1947
- Goldstein, Arthur W; Analysis of
performance of jet engine from characteristics of components I : aerodynamic
and matching characteristics of turbine component determined with cold
air; naca-report-878; 1947
- Katzoff, S Finn, Robert
S Laurence, James C; Interference
method for obtaining the potential flow past an arbitrary cascade of
airfoils; naca-report-879; 1947
- Pinkel, I Irving
Shames, Harold; Analysis
of jet-propulsion-engine combustion-chamber pressure losses;
naca-report-880; 1947
- Childs, J Howard
Mccafferty, Richard J Surine, Oakley W; Effect
of combustor-inlet conditions on performance of an annular turbojet
combustor; naca-report-881; 1947
- Greenberg, Harry; Frequency-response
method for determination of dynamic stability characteristics of airplanes
with automatic controls; naca-report-882; 1947
- Sawyer, Richard H; Flight
measurements of the lateral control characteristics of narrow-chord ailerons
on the trailing edge of a full-span slotted flap; naca-report-883;
1947
- Jones, Robert T; Effects of
sweepback on boundary layer and separation; naca-report-884; 1947
- Boshar, John; Flight
investigation on a fighter-type airplane of factors which affect the loads and
load distributions on the vertical tail surfaces during rudder kicks and
fishtails; naca-report-885; 1947
- Cook, Harvey A
Heinicke, Orville H Haynie, William H; Spark-timing
control based on correlation of maximum-economy spark timing, flame-front
travel, and cylinder-pressure rise; naca-report-886; 1947
- Spurr, Robert A Allen,
H Julian; A
theory of unstaggered airfoil cascades in compressible flow;
naca-report-888; 1947
- Heslet, Max A Lomax,
Harvard Jones, Arthur L; Voltera's
solution of the wave equation as applied to three-dimensional supersonic
airfoil problems; naca-report-889; September 1947
- Liepmann, Hans W Fila,
Gertrude H; Investigations
of effects of surface temperature and single roughness elements on
boundary-layer transition; naca-report-890; 1947
- Pinkel, Benjamin Karp,
Irvin M; A
thermodynamic study of the turbojet engine; naca-report-891; 1947
- Manganiello, Eugene J
Valerino, Michael F Bell, E Barton; High-altitude
flight cooling investigation of a radial air-cooled engine; naca-tn-1089;
August 1947
- Mitchler, Willard
(National Bureau of Standards); Marine
exposure tests on stainless steel sheet; naca-tn-1095; February
1947
- Moore, R L (Aluminum
Company of America); Observations
on the behavior of some noncircular aluminum alloy sections loaded to failure
in torsion; naca-tn-1097; February 1947
- Mebs, R W (National
Bureau of Standards) Mcadam, D J (National Bureau of Standards); Elastic
properties in tension and shear of high strength nonferrous metals and
stainless steel - effect of previous deformation and heat treatment;
naca-tn-1100; March 1947
- Purser, Paul E Cook,
Charles B; Collection and
analysis of hinge-moment data on control-surface tabs; naca-tn-1113; April
1947
- Brown, Harvey H
Clousing, Lawrence A; Wing
pressure-distribution measurements up to 0.866 Mach number in flight on a
jet-propelled airplane; naca-tn-1181; March 1947
- Herrig, Joseph L
Bogdonoff, Seymour M; Performance
of axial-flow fan and compressor blades designed for high loadings;
naca-tn-1201; February 1947
- Powell, Allen S; Reactions with
steel of compounds containing chemical groups used in lubricant additives;
naca-tn-1207; 1947
- Conner, D William; Effect of
reflex camber on the aerodynamic characteristics of a highly tapered
moderately swept-back wing at Reynolds numbers up to 8,000,000;
naca-tn-1212; March 1947
- Kantrowitz, Arthur; The formation
and stability of normal shock waves in channel flows; naca-tn-1225; March
1947
- Cross, Howard C
(Battelle Memorial Institute) Freeman, J W (University of Michigan); A
metallurgical investigation of large forged discs of low-carbon N-155
alloy; naca-tn-1230; April 1947
- Watkins, Charles E; The streamline
pattern in the vicinity of an oblique airfoil; naca-tn-1231; March
1947
- Tolefson, Harold B; Preliminary
analysis of NACA measurements of atmospheric turbulence within a thunderstorm
- U.S. Weather Bureau thunderstorm project; naca-tn-1233; March
1947
- Quinn, John H , Jr; Drag tests of
an NACA 65(215)-114, a = 1.0 practical-construction airfoil section equipped
with a 0.295-airfoil-chord slotted flap; naca-tn-1236; April 1947
- Howard, Frank L
(National Bureau of Standards) Mears, Thomas W (National Bureau of Standards)
Fookson, A (National Bureau of Standards) Pomerantz, Philip (National Bureau
of Standards) Brooks, Donald B; The
preparation and physical properties of several aliphatic hydrocarbons and
intermediates; naca-tn-1247; May 1947
- Livengood, James C
(Massachusetts Inst. of Tech) Wallour, Chapin (Massachusetts Inst. of Tech);
A study of
piston-ring friction; naca-tn-1249; April 1947
- Gustafson, F B Gessow,
Alfred; Effect of blade
stalling on the efficiency of a helicopter rotor as measured in flight;
naca-tn-1250; April 1947
- Scher, Stanley H; Effect of 40
degree sweepback on the spin and recovery characteristics of a 1/25-scale
model of a typical fighter-type airplane as determined by free-spinning-tunnel
tests; naca-tn-1256; April 1947
- Liepmann, Hans Wolfgang
(California Institute of Technology) Laufer, John (California Institute of
Technology); Investigations
of free turbulent mixing; naca-tn-1257; August 1947
- Rathert, George A , Jr;
Flight
investigation of the effects on airplane static longitudinal stability of a
bungee and engine-tilt modifications; naca-tn-1260; May 1947
- Myers, Garry C , Jr; Flight
measurements of helicopter blade motion with a comparison between theoretical
and experimental results; naca-tn-1266; April 1947
- Neely, Robert H
Bollech, Thomas V Westrick, Gertrude C; Experimental
and calculated characteristics of several NACA 44-series wings with aspect
ratios of 8, 10, and 12 and taper ratios of 2.5 and 3.5; naca-tn-1270; May
1947
- Bogdonoff, Seymour M
Hess, Eugene E; Axial-flow
fan and compressor blade design data on 52.5 degrees stagger and further
verification of cascade data by rotor tests; naca-tn-1271; April
1947
- Sherman, Albert; Interference of
wing and fuselage from tests of 30 combinations with triangular and elliptical
fuselages in the NACA variable-density tunnel; naca-tn-1272; May
1947
- Dow, Norris F Hickman,
William A Mccracken, Howard L; Compressive-strength
comparisons of panels having aluminum-alloy sheet and stiffeners with panels
having magnesium-alloy sheet and aluminum alloy stiffeners; naca-tn-1274;
April 1947
- Swanson, Robert S
Crandall, Stewart M Miller, Sadie; A
lifting-surface-theory solution and tests of an elliptic tail surface of
aspect ratio 3 with a 0.5-chord 0.85-span elevator; naca-tn-1275; May
1947
- Fullmer, Felicien F; Two-dimensional
wind-tunnel investigation of the NACA 64(sub 1)-012 airfoil equipped with two
types of leading-edge flap; naca-tn-1277; May 1947
- Manson, S S; Determination
of elastic stresses in gas-turbine disks; naca-tn-1279; 1947
- Manson, S S Morgan, W
C; Distribution of
bearing reactions on a rotating shaft supported on multiple journal
bearings; naca-tn-1280; May 1947
- Ross, Robert D; An electrical
computer for the solution of shear-lag and bolted-joint problems;
naca-tn-1281; May 1947
- Von Doenhoff, Albert E
Abbott, Frank T; The
Langley two-dimensional low-turbulence pressure tunnel; naca-tn-1283; May
1947
- Imlay, Frederick H; Theoretical
motions of hydrofoil systems; naca-tn-1285; June 1947
- Maggin, Bernard
Bennett, Charles V; Flight
tests of an airplane model with a 62 degree swept-back wing in the Langley
free-flight tunnel; naca-tn-1288; May 1947
- Dingeldein, Richard C
Schaefer, Raymond F; Full-scale
investigation of the aerodynamic characteristics of a typical single-rotor
helicopter in forward flight; naca-tn-1289; May 1947
- Parkinson, John B; Appreciation
and determination of the hydrodynamic qualities of seaplanes;
naca-tn-1290; May 1947
- Quinn, John H; Tests
of the NACA 64(SUB 1)A212 airfoil section with a slat, a double slotted flap,
and boundary-layer control by suction; naca-tn-1293; May 1947
- Toll, Thomas A Queijo,
M J Brewer, Jack D; Wind-tunnel
investigation of the effects of surface-covering distortion on the
characteristics of a flap having undistorted contour maintained for various
distances ahead of the trailing edge; naca-tn-1296; May 1947
- Kruszewski, Edwin T; Bending
stresses due to torsion in a tapered box beam; naca-tn-1297; May
1947
- Furlong, G Chester
Fitzpatrick, James E; Effects
of Mach number and Reynolds number on the maximum lift coefficient of a wing
of NACA 230-series airfoil sections; naca-tn-1299; May 1947
- Hall, Charles F; The effect of
modifications to the horizontal-tail profile on the high-speed longitudinal
control of a pursuit airplane; naca-tn-1302; August 1947
- Riebe, John M Naeseth,
Rodger L; Effect of
aerodynamic refinement on the aerodynamic characteristics of a flying-boat
hull; naca-tn-1307; June 1947
- Kempner, Joseph Duberg,
John E; Charts for
stress analysis of reinforced circular cylinders under lateral loads;
naca-tn-1310; May 1947
- Tendeland, Thorval
Steinmetz, Charles P; A
comparative study of weights and sizes of flat-plate exhaust-gas-to-air heat
exchangers with and without fins; naca-tn-1312; July 1947
- Anderson, Robert J
Ritter, William K; An
investigation of the effect of blade curvature on centrifugal-impeller
performance; naca-tn-1313; May 1947
- Webster, A P (Bureau of
Medicine and Surgery, Navy Department); Free-falls
and parachute descents in the standard atmosphere; naca-tn-1315; June
1947
- Hicks, Bruce L
Montgomery, Donald Wasserman, Robert H; On
the one-dimensional theory of steady compressible fluid flow in ducts with
friction and heat addition; naca-tn-1336; July 1947
- Stone, Ralph W , Jr
Burk, Sanger M , Jr; Effect
of horizontal-tail position on the hinge moments of an unbalanced rudder in
attitudes simulating spin conditions; naca-tn-1337; June 1947
- Crigler, John L Jaquis,
Robert E; Propeller-efficiency
charts for light airplanes; naca-tn-1338; July 1947
- Hagerman, John R; Wind-tunnel
investigation of the effect of power and flaps on the static longitudinal
stability and control characteristics of a single-engine high-wing airplane
model.; naca-tn-1339; July 1947
- Jones, Robert T; Subsonic flow
over thin oblique airfoils at zero lift; naca-tn-1340; June 1947
- Batdorf, S B; A
simplified method of elastic-stability analysis for thin cylindrical shells I
: Donnell's equation; naca-tn-1341; June 1947
- Batdorf, S B; A
simplified method for elastic stability analysis for thin cylindrical shells
II : modified equilibrium equation; naca-tn-1342; June 1947
- Bergrun, Norman R; A method for
numerically calculating the area and distribution of water impingement on the
leading edge of an airfoil in a cloud; naca-tn-1397; August 1947
- Mayo, Wilbur L; Solutions for
hydrodynamic impact force and response of a two-mass system with an
application to an elastic airframe; naca-tn-1398; August 1947
- Stone, Ralph W Burk,
Sanger M , Jr; Hinge-moment
characteristics of balanced elevator and rudder for a specific tail
configuration on a fuselage in spinning attitudes; naca-tn-1400; August
1947
- Ivey, H Reese Bowen,
Edward N JR Oborny, Lester F; Introduction
to the problem of rocket-powered aircraft performance; naca-tn-1401;
December 1947
- Brewer, Jack D Queijo,
M J; Wind-tunnel
investigation of the effect of tab balance on tab and control-surface
characteristics; naca-tn-1403; August 1947
- Miller, Cearcy D; The optical
system of the NACA 400,000-frame-per-second motion-picture camera;
naca-tn-1405; August 1947
- Forsyth, Charles M
Gray, William E , Jr; A
comparison of flight test results on a scout-bomber airplane with 4.7 degree
and with 10 degree geometric dihedral in the wing outer panels;
naca-tn-1407; August 1947
- Hirshfeld, M A Miller,
Cearcy D; Instantaneous
ultraviolet knock spectra correlated with high-speed photographs;
naca-tn-1408; August 1947
- Hess, W F (Rensselaer
Polytechnic Institute) Wyant, R A (Rensselaer Polytechnic Institute) Winsor, F
J (Rensselaer Polytechnic Institute); The
effect of preheating and postheating on the quality of spot welds in aluminum
alloys; naca-tn-1415; November 1947
- Drell, I L Wear, J D;
Experimental
studies of knock-limited blending characteristics of aviation fuels III :
aromatics and cycloparaffins; naca-tn-1416; August 1947
- Lankford, John L; Investigation
of the pressure-loss characteristics of a turbojet inlet screen;
naca-tn-1418; September 1947
- Jones, Arthur L
Flanagan, Mildred G Sluder, Loma; An
application of lifting-surface theory to the prediction of angle-of-attack
hinge-moment parameters for aspect ratio 4.5 wings; naca-tn-1420;
September 1947
- Ribner, Herbert S; The stability
derivatives of low-aspect-ratio triangular wings at subsonic and supersonic
speeds; naca-tn-1423; September 1947
- Lewis, William Kline,
Dwight B Steinmetz, Charles P; A
further investigation of the meteorological conditions conducive to aircraft
icing; naca-tn-1424; October 1947
- White, Maurice D Lomax,
Harvard Turner, Howard L; Sideslip
angles and vertical-tail loads in rolling pull-out maneuvers.;
naca-tn-1122; April 1947
- Spahr, J Richard; Lateral-control
characteristics of various spoiler arrangements as measured in flight;
naca-tn-1123; 1947
- Weske, John R (Case
School of Applied Science); An
investigation of the aerodynamic characteristics of a rotating axial-flow
blade grid; naca-tn-1128; February 1947
- Moore, R L (Aluminum
Company of America); Bearing
strength of some sand-cast magnesium alloys; naca-tn-1136; February
1947
- Mcpherson, A E
(National Bureau of Standards); Device
for measuring principal curvature and principal strains on a nearly plane
surface; naca-tn-1137; February 1947
- Ivey, H Reese Stickle,
George W Schuettler, Alberta; Charts
for determining the characteristics of sharp-nose airfoils in two-dimensional
flow at supersonic speeds; naca-tn-1143; 1947
- Sadoff, Melvin Turner,
William N Clousing, Lawrence A; Measurements
of the pressure distribution on the horizontal-tail surface of a typical
propeller-driven pursuit airplane in flight I : effects of compressibility in
steady straight and accelerated flight; naca-tn-1144; July 1947
- Quinn, John H; Summary
of drag characteristics of practical-construction wing sections;
naca-tn-1151; 1947
- Ross, Sydney (Stanford
University); Foaming volume
and foam stability; naca-tn-1153; February 1947
- Harper, Charles W
Jones, Arthur L; A
comparison of the lateral motion calculated for tailless and conventional
airplanes; naca-tn-1154; February 1947
- Gelbart, Abe (Syracuse
University); On subsonic
compressible flows by a method of correspondence I - methods for obtaining
subsonic circulatory compressible flows about two-dimensional bodies;
naca-tn-1170; March 1947
- GELBART ABE (Syracuse
University) Bartnoff, Shepard (Syracuse University); On
subsonic compressible flows by a method of correspondence II : application of
methods to studies of flow with circulation about a circular cylinder;
naca-tn-1171; April 1947
- Holt, Marshall
(Aluminum Company of America) Feil, G W (Aluminum Company of America); Comparative
tests on extruded 14S-T and extruded 24S-T hat-shape stiffener sections;
naca-tn-1172; March 1947
- Danforth, Edward C B ,
III Reeder, John P; Flight
measurements of internal cockpit pressures in several fighter-type
airplanes; naca-tn-1173; February 1947
- Kemp, R H Morgan, W C
Manson, S S; The application
of high-temperature strain gauges to the measurements of vibratory stresses in
gas-turbine buckets; naca-tn-1174; April 1947
- Swanson, Robert S
Crandall, Stewart M; Lifting-surface-theory
aspect-ratio corrections to the lift and hinge-moment parameters for full-span
elevators on horizontal tail surfaces; naca-tn-1175; February 1947
- Kuhn, Paul Rafel,
Norman Griffith, George E; Stresses
around rectangular cut-outs with reinforced coaming stringers;
naca-tn-1176; 1947
- Levin, L Ross Nelson,
David H; Effect of rivet
or bolt holes on the ultimate strength developed by 24S-T and Alclad 75S-T
sheet in incomplete diagonal tension; naca-tn-1177; 1947
- Darsow, John F Selna,
James; A
flight investigation of the thermal performance of an air-heated
propeller; naca-tn-1178; April 1947
- Ivey, H Reese; Notes
on the theoretical characteristics of two-dimensional supersonic airfoils;
naca-tn-1179; 1947
- Locke, F W S , Jr
(Bureau of Aeronautics, Navy Department); A
collection of the collapsed results of general tank tests of miscellaneous
flying-boat-hull models; naca-tn-1182; March 1947
- Coleman, Robert P
Feingold, Arnold M; Theory
of ground vibrations of a two-blade helicopter rotor on anisotropic flexible
supports; naca-tn-1184; 1947
- Orlin, W James Lindner,
Norman J Bitterly, Jack G; Application
of the analogy between water flow with a free surface and two-dimensional
compressible gas flow; naca-tn-1185; February 1947
- Harrison, W N (National
Bureau of Standards) Moore, D G (National Bureau of Standards) Richmond, J C
(National Bureau of Standards); Review
of an investigation of ceramic coatings for metallic turbine parts and other
high-temperature applications; naca-tn-1186; March 1947
- Sawyers, Richard H; Flight
measurements of the lateral control characteristics of narrow-chord ailerons
on the trailing edge of a full-span slotted flap; naca-tn-1188; February
1947
- Runckel, Jack F Davey,
Richard S; Pressure-distribution
measurements on the rotating blades of a single-stage axial-flow
compressor; naca-tn-1189; February 1947
- Beeler, De E Gerard,
George; Wake
measurements behind a wing section of a fighter airplane in fast dives;
naca-tn-1190; March 1947
- Cahill, Jones F; Two-dimensional
wind-tunnel investigation of four types of high-lift flap on an NACA 65-210
airfoil section; naca-tn-1191; February 1947
- Talkin, Herbert W; Charts showing
relations among primary aerodynamic variables for helicopter-performance
estimation; naca-tn-1192; February 1947
- Sternfield, Leonard; Effect of
product of inertia on lateral stability; naca-tn-1193; March 1947
- Liepmann, Hans W
(California Institute of Technology) Fila, Gertrude H (California Institute of
Technology); Investigation
of effects of surface temperature and single roughness elements on
boundary-layer transition; naca-tn-1196; April 1947
- Dunn, Louis G
(California Institute of Technology); Some
investigations of the general instability of stiffened metal cylinders VIII :
stiffened metal cylinders subjected to pure torsion; naca-tn-1197; May
1947
- Kahane, A; Charts
of pressure rise obtainable with airfoil-type axial-flow cooling fans;
naca-tn-1199; March 1947
- Warfield, Calvin N; Tentative
tables for the properties of the upper atmosphere; naca-tn-1200;
1947
- Sadoff, Melvin
Clousing, Lawrence A; Measurements
of the pressure distribution on the horizontal tail surface of a typical
propeller-driven pursuit airplane in flight II : the effect of angle of
sideslip and propeller operation; naca-tn-1202; May 1947
- Simpkinson, Scott H
Millenson, Morton B Eatherton, Laurel J; Effect
of centrifugal force on the elastic curve of a vibrating cantilever beam;
naca-tn-1204; February 1947
- Niles, Donald E
Schuette, Evan H; Data
on optimum length, shear strength, and tensile strength of age-hardened 17S-T
machine-countersunk rivets in 75S-T sheet; naca-tn-1205; March 1947
- Macks, E Fred Shaw,
Milton C; In-line
aircraft-engine bearing loads III : main-bearing loads; naca-tn-1206;
February 1947
- Campbell, John A Drake,
Hubert M; Investigation
of stability and control characteristics of an airplane model with skewed wing
in the Langley free-flight tunnel; naca-tn-1208; May 1947
- Sutor, Alois T
Corrington, Lester C Dudugjian, Carl; Exhaust-valve
temperatures in a liquid-cooled aircraft-engine cylinder as affected by engine
operating variables; naca-tn-1209; February 1947
- Maclachlan, Robert
Ribner, Herbert; Effect
of slipstream rotation in producing asymmetric forces on a fuselage;
naca-tn-1210; March 1947
- Lindsey, W F Daley,
Bernard N Humphreys, Milton D; The
flow and force characteristics of supersonic airfoils at high subsonic
speeds; naca-tn-1211; March 1947
- Johnsen, I A Ritter, W
K Anderson, R J; Performance
of a radial-inlet impeller designed on the basis of two-dimensional-flow
theory for an infinite number of blades; naca-tn-1214; March 1947
- Ginsburg, Ambrose
Ritter, William K Palasics, John; Effects
on performance of changing the division of work between increase of angular
velocity and increase of radius of rotation in an impeller; naca-tn-1216;
February 1947
- Cook, Harvey A
Heinicke, Orville H Haynie, William H; Spark-timing
control based on correlation of maximum-economy spark timing, flame-front
travel, and cylinder pressure rise; naca-tn-1217; February 1947
- Kaplan, Carl; Effect
of compressibility at high subsonic velocities on the moment acting on an
elliptic cylinder; naca-tn-1218; March 1947
- Duberg, John E Kempner,
Joseph; Stress analysis
by recurrence formula of reinforced circular cylinders under lateral
loads; naca-tn-1219; March 1947
- Boman, David S Nagey,
Tibor F Doyle, Ronald B; Effect
of exhaust pressure on the performance of an 18-cylinder air-cooled radial
engine with a valve overlap of 40 degrees; naca-tn-1220; March 1947
- Valerino, Michael F
Kaufman, Samuel J Hughes, Richard F; Effect
of exhaust pressure on the cooling characteristics of an air-cooled
engine; naca-tn-1221; March 1947
- Hanson, Carl M
Anderson, Seth B; Flight
tests of a double-hinged horizontal tail surface with reference to
longitudinal-stability and control characteristics; naca-tn-1224; May
1947
- Ivey, H Reese Bowen,
Edward N , Jr; Theoretical
supersonic lift and drag characteristics of symmetrical wedge-shape-airfoil
sections as affected by sweepback outside the Mach cone; naca-tn-1226;
March 1947
- Smith, Newell H; Exploratory
investigation of laminar-boundary-layer oscillations on a rotating disk;
naca-tn-1227; May 1947
- Braslow, Albert L; Two-dimensional
wind-tunnel investigation of a 10.7-percent-thick symmetrical tail section
with a 0.40 airfoil-chord control surface and a 0.20 control-surface-chord
tab; naca-tn-1228; June 1947
- Greenberg, Harry; Frequency-response
method for determination of dynamic stability characteristics of airplanes
with automatic controls; naca-tn-1229; March 1947
- Bollinger, Lowell M
Williams, David T; Experiments
on stability of Bunsen-burner flames for turbulent flow; naca-tn-1234;
June 1947
- Harris, Maxwell
Schlaff, Bernard A; An
investigation of a thermal ice-prevention system for a cargo airplane VIII :
metallurgical examination of the wing leading-edge structure after 225 hours
of flight operation of the thermal system; naca-tn-1235; April 1947
- Parkinson, John B
Olson, Roland E Haar, Marvin I; Tank
investigation of a powered dynamic model of a large long-range flying boat -
Langley tank model 180; naca-tn-1237; March 1947
- Gerrish, Harold C Meem,
J Lawrence, Jr Scadron, Marvin D Colnar, Anthony; The
NACA mixture analyzer and its application to mixture-distribution measurement
in flight; naca-tn-1238; March 1947
- Wallace, Authur R
Rossi, Peter F Wells, Evalyn G; Wind-tunnel
investigation of the effect of power and flaps on the static longitudinal
stability characteristics of a single-engine low-wing airplane model;
naca-tn-1239; April 1947
- Crouse, W A (National
Bureau of Standards) Caudill, D C (National Bureau of Standards) Reinhart, F W
(National Bureau of Standards); Effect
of simulated service conditions on plastics; naca-tn-1240; July
1947
- Farb, Daniel; Experimental
investigation of the stress distribution around reinforced circular cut-outs
in skin stringer panels under axial loads; naca-tn-1241; March 1947
- Stanitz, John D; An analysis of
the factors that affect the exhaust process of a four-stroke-cycle
reciprocating engine; naca-tn-1242; April 1947
- Cleaves, Alden P
Carver, Mildred S; A
spectrophotometric method for identification and estimation of
alkylnaphthalenic-type hydrocarbons in kerosene; naca-tn-1243; April
1947
- Lewis, James P; Wind-tunnel
investigation of icing of an engine cooling-fan installation;
naca-tn-1246; April 1947
- Norris, Charles B; An analysis of
the compressive strength of honeycomb cores for sandwich construction;
naca-tn-1251; 1947
- Diesendruck, Leo; Iterative
interference methods in the design of thin cascade blades; naca-tn-1254;
May 1947
- Allen, Julian Nitzberg,
Gerald E; The effect of
compressibility on the growth of the laminar boundary layer on low-drag wings
and bodies; naca-tn-1255; July 1947
- Gasich, Welko E; Experimental
verification of two methods for computing the take-off ground run of
propeller-driven aircraft; naca-tn-1258; June 1947
- Voldrich, C B (Battelle
Memorial Institute) Armstrong, E T (Battelle Memorial Institute); Effect
of variables in welding technique on the strength of direct-current
metal-arc-welded joints in aircraft steel I : static tension and bending
fatigue tests of joints in SAE 4130 steel sheet; naca-tn-1261; July
1947
- Eisenstadt, Bertram J;
Boundary-induced
upwash for yawed and swept-back wings in closed circular wind tunnels;
naca-tn-1265; May 1947
- Gessow, Alfred Myers,
Garry C; Flight tests of
a helicopter in autorotation, including a comparison with theory;
naca-tn-1267; April 1947
- Helfand, B B; Meteorological
conditions associated with flight measurements of atmospheric turbulence;
naca-tn-1273; June 1947
- Von Doenhoff, Albert E
Stivers, Louis S O'Connor, James M; Low-speed
tests of five NACA 66-series airfoils having mean lines designed to give high
critical Mach numbers; naca-tn-1276; May 1947
- Lowry, John G
Schneiter, Leslie E; Investigation
at low speed of the longitudinal stability characteristics of a 60 degree
swept-back tapered low-drag wing; naca-tn-1284; May 1947
- Maggin, Bernard
Bennett, Charles V; Low-speed
stability and damping-in-roll characteristics of some highly swept wings;
naca-tn-1286; May 1947
- Maggin, Bernard
Bennett, Charles V; Flight
tests of an airplane model with 42 degree swetpback wing in the Langley
free-flight tunnel; naca-tn-1287; May 1947
- Fischel, Jack
Tamburello, Vito; Investigation
of effect of span, spanwise location, and chordwise location of spoilers on
lateral control characteristics of a tapered wing; naca-tn-1294; May
1947
- Sandahl, Carl A Vollo,
Samuel D; Wind-tunnel
investigation of the air load distribution on two combinations of lifting
surface and fuselage; naca-tn-1295; May 1947
- Fitzpatrick, James E
Furlong, G Chester; Effect
of spoiler-type lateral-control devices on the twisting moments of NACA
230-Series airfoil sections; naca-tn-1298; May 1947
- Heimerl, George J
Niles, Donald E; Column
and plate compressive strengths of aircraft structural martials extruded
0-1HTA magnesium alloy; naca-tn-1156; 1947
- Kline, G M (National
Bureau of Standards) Reinhart, F W (National Bureau of Standards) Rinker, R C
(National Bureau of Standards) De Lollis, N J (National Bureau of Standards);
Effect of
catalysts and pH strength of resin-bonded plywood; naca-tn-1161; April
1947
- Woods, Walter Heimerl,
George J; Effect of brake
forming in various tempers on the strength of Alclad 75S-T aluminum-alloy
sheet; naca-tn-1162; 1947
- Batterson, Sidney A; Variation of
hydrodynamic impact loads with flight-path angle for a prismatic float at 0
and -3 degree trim and with a 22 1/2 degree angle of dead rise;
naca-tn-1166; April 1947
- Kelin, Milton M; Pressure
distributions and force tests of an NACA 65-210 airfoil section with a
50-percent-chord flap; naca-tn-1167; 1947
- Reissner, Eric
(Massachusetts Institute of Technology) Stevens, John E (Massachusetts
Institute of Technology); Effect
of finite span on the airload distributions for oscillating wings. II -
Methods of calculation and examples of application; naca-tn-1195; October
1947
- Hoff, J (Polytechnic
Institute of Brooklyn) Boley, Bruno A (Polytechnic Institute of Brooklyn)
Klein, Bertram (Polytechnic Institute of Brooklyn); Stresses
in and general instability of monocoque cylinders with cutouts III :
calculation of the buckling load of cylinders with symmetric cutout subjected
to pure bending; naca-tn-1263; May 1947
- Selma, James Zerbe,
John E; A
method for calculating the heat required for the prevention of fog formations
on the inside surfaces of single-panel bullet-resisting windshields during
diving flight; naca-tn-1301; July 1947
- Ribner, Herbert S; A transonic
propeller of triangular plan form; naca-tn-1303; May 1947
- Mendelsohn, Robert A;
Wind-tunnel
investigation of the boundary layer and wake and their relation to airfoil
characteristics.NACA 65(sub 1)-012 airfoil with a true contour flap and a
beveled-trailing-edge flap; naca-tn-1304; June 1947
- Yates, Campbell C
Riebe, John M; Effect
of length-beam on the aerodynamic characteristics of flying-boat hulls;
naca-tn-1305; June 1947
- Yates, Campbell C
Riebe, John M; Aerodynamic
characteristics of three planing-tail flying-boat hulls.; naca-tn-1306;
June 1947
- Maclachlan, Robert
Letko, William; Correlation
of two experimental methods of determining the rolling characteristics of
unswept wings; naca-tn-1309; May 1947
- Freeman, J W
(University of Michigan) White, A E (University of Michigan) Reynolds, E E
(University of Michigan.); An
investigation of the high-temperature properties of chromium-base alloys at
1350 F; naca-tn-1314; May 1947
- Campbell, W R (National
Bureau of Standards) Medbery, A F (National Bureau of Standards); Performance
tests of wire strain gages V : error in indicated bending strains in thin
sheet metal due to thickness and rigidity of gage; naca-tn-1318; July
1947
- Pierce, Harold B; Investigation
of the dynamic response of airplane wings to gusts; naca-tn-1320; June
1947
- Putnam, Abbott A; An improved
method for calculating the dynamic response of flexible airplanes to
gusts; naca-tn-1321; May 1947
- Perl, W; Calculation
of compressible flows past aerodynamic shapes by use of the streamline
curvature; naca-tn-1328; June 1947
- Deters, Owen J; Estimation of
control forces of spring-tab ailerons from wind-tunnel data; naca-tn-1333;
June 1947
- Holms, Arthur G
Faldetta, Richard D; Effects
of temperature distribution and elastic properties of materials on
gas-turbine-disk stresses; naca-tn-1334; June 1947
- Batdorf, S B
Shildcrout, Murry Stein, Manuel; Critical
stress of thin-walled cylinders in axial compression; naca-tn-1343;
1947
- Batdorf, S B Stein,
Manuel Schildcrout, Murry; Critical
stress of thin-walled cylinders in torsion; naca-tn-1344; June 1947
- Batdorf, S B Stein,
Manuel Schildcrout, Murry; Critical
combinations of torsion and direct axial stress for thin-walled cylinders;
naca-tn-1345; June 1947
- Batdorf, S B
Schildcrout, Murry Stein, Manuel; Critical
combinations of shear and longitudinal direct stress for long plates with
transverse curvature; naca-tn-1347; June 1947
- Batdorf, S B Stein,
Manuel Schildcrout, Murry; Critical
shear stress of curved rectangular panels; naca-tn-1348; May 1947
- (Author(s) Not
Available); Performance and
ranges of application of various types of aircraft-propulsion system;
naca-tn-1349; August 1947
- Jones, Robert T; Estimated
lift-drag ratios at supersonic speed; naca-tn-1350; July 1947
- Mendelsohn, Robert A
Brewer, Jack D; Comparison
between the measured and theoretical span loadings on a moderately
swept-forward and a moderately swept-back semispan wing; naca-tn-1351;
July 1947
- Letko, William
Feigenbaum, David; Wind-tunnel
investigation of split trailing-edge lift and trim flaps on a tapered wing
with 23 degree sweepback; naca-tn-1352; July 1947
- Regier, Arthur A; Effect of
distance on airplane noise; naca-tn-1353; June 1947
- Hicks, Chester W
Hubbard, Harvey H; Comparison
of sound emission from two-blade, four-blade, and seven-blade propellers;
naca-tn-1354; July 1947
- Sakmann, B W
(Massachusetts Institute of Technology) Grossman, N (Massachusetts Institute
of Technology) Irvine, John W , Jr (Massachusetts Institute of Technology); A study of
metal transfer between sliding surfaces; naca-tn-1355; September
1947
- Carter, Arthur W
Clement, Eugene P Morewitz, Alvin H; An
investigation of effects of reversed-type longitudinal steps on resistance and
spray characteristics of a flying-boat hull; naca-tn-1356; July
1947
- Hubbard, Harvey H
Regier, Arthur A; Propeller-loudness
charts for light airplanes; naca-tn-1358; July 1947
- Maggin, Bernard; Experimental
verification of the rudder-free stability theory for an airplane model
equipped with a rudder having positive floating tendencies and various amounts
of friction; naca-tn-1359; July 1947
- Lees, Lester; The
stability of the laminar boundary layer in a compressible fluid;
naca-tn-1360; July 1947
- Kuhn, Paul; Deformation
analysis of wing structures; naca-tn-1361; July 1947
- Habel, Louis W
Gallagher, James J; Tests
to determine the effect of heat on the pressure drop through radiator
tubes; naca-tn-1362; July 1947
- Milwitzky, Benjamin; A theoretical
investigation of hydrodynamic impact loads on scalloped-bottom seaplanes and
comparisons with experiment; naca-tn-1363; July 1947
- Kuhn, Paul Peterson,
James P; Strength
analysis of stiffened beam webs; naca-tn-1364; July 1947
- Eppes, James V D
(Massachusetts Institute of Technology) Livengood, James C (Massachusetts
Institute of Technology) Taylor, C Fayette (Massachusetts Institute of
Technology); The effect of
changing the ratio of exhaust-valve flow capacity to inlet-valve flow capacity
on volumetric efficiency and output of a single- cylinder engine;
naca-tn-1365; October 1947
- Livengood, James C
(Massachusetts Institute of Technology) Eppes, James V D (Massachusetts
Institute of Technology); Effect
of changing manifold pressure, exhaust pressure, and valve timing on the air
capacity and output of a four-stroke engine operated with inlet valves of
various diameters and lifts; naca-tn-1366; December 1947
- Desmon, Leland G Doyle,
Ronald B; Effect of
exhaust pressure on the performance of a 12-cylinder liquid-cooled engine;
naca-tn-1367; July 1947
- Loftin, Laurence K ,
Jr; Theoretical and
experimental data for a number of NACA 6A-series airfoil sections;
naca-tn-1368; July 1947
- Schade, Robert O; Effect of
geometric dihedral on the aerodynamic characteristics of two isolated vee-tail
surfaces; naca-tn-1369; July 1947
- Mckinney, Marion O , Jr
Drake, Hubert M; Correlation
of experimental and calculated effects of product of inertia on lateral
stability; naca-tn-1370; July 1947
- Moeckel, W E Connors, J
F; Charts
for the determination of supersonic air flow against inclined planes and
axially symmetric cones; naca-tn-1373; July 1947
- Wear, Jerrold D
Sanders, Newell D; Experimental
studies of the knock-limited blending characteristics of aviation fuels II :
investigation of leaded paraffinic fuels in an air-cooled cylinder;
naca-tn-1374; July 1947
- Ekstein, Hans (Armour
Research Foundation) Siegel, Stanley (Armour Research Foundation); Limits
of precision in the determination of lattice parameters and stresses by the
Debye-Scherrer method; naca-tn-1375; October 1947
- Lowry, John G Crandall,
Stewart M; Wind-tunnel
investigation of unshielded horn balances on a horizontal tail surface;
naca-tn-1377; July 1947
- Hagerman, John R; Wind-tunnel
investigation of the effect of power and flaps on the static lateral stability
and control characteristics of a single-engine high-wing airplane model;
naca-tn-1379; July 1947
- Reynolds, E E
(University of Michigan) Freeman, J W (University of Michigan) White, A E
(University of Michigan); The
1350 F stress-rupture properties of two wrought alloys and three cast
alloys; naca-tn-1380; November 1947
- Smith, Norman F; Numerical
evaluation of mass-flow coefficient and associated parameters from wake-survey
equations; naca-tn-1381; August 1947
- Tetervin, Neal; A review of
boundary-layer literature; naca-tn-1384; July 1947
- Miller, James A
(National Bureau of Standards); Stress-strain
and elongation graphs for Alclad aluminum-alloy 75S-T sheet; naca-tn-1385;
November 1947
- Holtzclaw, Ralph W
Dods, Jules B , Jr; Wind-tunnel
investigation of drooped ailerons on a 16-percent-thick low-drag airfoil;
naca-tn-1386; August 1947
- Locke, F W S , Jr
(Bureau of Aeronautics, Navy Department); A
preliminary correlation of the behavior of water rudders on seaplanes and
flying boats; naca-tn-1387; August 1947
- Herrig, L Joseph
Bogdonoff, Seymour M; Performance
of an axial-flow compressor rotor designed for a pitch-section lift
coefficient of 1.2; naca-tn-1388; May 1947
- Dow, Norris F Hickman,
William A; Design charts
for flat compression panels having longitudinal extruded Y-section stiffeners
and comparison with panels having formed Z-section stiffeners;
naca-tn-1389; August 1947
- Pearson, E O , Jr; Effect of
compressibility on the distribution of pressures over a tapered wing of NACA
230-series airfoil sections; naca-tn-1390; July 1947
- Lewis, William (U. S.
Weather Bureau); Icing
properties of noncyclonic winter stratus clouds; naca-tn-1391; September
1947
- Lewis, William (U. S.
Weather Bureau); Icing
zones in a warm front system with general precipitation; naca-tn-1392;
July 1947
- Boshar, John; Flight
investigation on a fighter-type airplane of factors which affect the loads and
load distributions on the vertical tail surfaces during rudder kicks and
fishtails; naca-tn-1394; August 1947
- Quinn, John H; Wind-tunnel
investigation of the NACA 654-421 airfoil section with a double slotted flap
and boundary layer control by suction; naca-tn-1395; July 1947
- Graham, Donald J; High-speed
tests of an airfoil section cambered to have critical Mach numbers higher than
those attainable with a uniform-load mean line; naca-tn-1396; July
1947
- Hartwig, Frederick J
Sheflin, Bob W Jones, Robert J; Preliminary
investigation of a gas turbine with sillimanite ceramic rotor blades;
naca-tn-1399; July 1947
- Stevenson, David B
Byrne, Robert W; High-speed
wind-tunnel tests of an NACA 16-009 airfoil having a 32.9-percent-chord flap
with an overhang 20.7 percent of the flap chord; naca-tn-1406; August
1947
- Deters, Owen J Russell,
Robert T; Investigation
of a spoiler-type lateral control system on a wing with full-span flaps in the
Langley 19-foot pressure tunnel; naca-tn-1409; August 1947
- Hess, W F (Rensselaer
Polytechnic Institute) Wyant, R A (Rensselaer Polytechnic Institute) Winsor, F
J (Rensselaer Polytechnic Institute); The
spot welding of Alclad 24S-T in thicknesses of 0.064, 0.081, and 0.102
inch; naca-tn-1411; November 1947
- Michel, Donald J
Hickel, Robert O Voit, Charles H; Performance
of a double-row radial aircraft engine with three methods of safety-fuel
injection; naca-tn-1413; August 1947
- Hammack, Jerome B; Investigation
of thrust losses due to shanks of a flared-shank two-blade propeller on a
slender-nose airplane; naca-tn-1414; August 1947
- Stevenson, David B
Adler, Alfred A; High-speed
wind-tunnel tests of an NACA 0009-64 airfoil having a 33.4-percent-chord flap
with an overhang 20.1 percent of the flap chord; naca-tn-1417; September
1947
- Brown, Byron Bradshaw,
Guy R; Method of
designing vaneless diffusers and experimental investigation of certain
undetermined parameters; naca-tn-1426; September 18, 1947
- (Author(s) Not
Available); Notes and
tables for use in the analysis of supersonic flow; naca-tn-1428; December
1947
- Evvard, John C; The effects of
yawing thin pointed wings at supersonic speeds; naca-tn-1429; September
1947
- Deters, Owen J Russell,
Robert T; Investigation
of the Aileron and tab of a spring-tab lateral-control system in the Langley
19-foot pressure tunnel; naca-tn-1431; September 1947
- Good, J N Godfrey,
Douglas; Changes found
on run-in and scuffed surfaces of steel chrome plate, and cast iron;
naca-tn-1432; October 1947
- Goodman, Stanley
(National Bureau of Standards) Boyd, Evelyn (National Bureau of Standards); Instability of
outstanding flanges simply supported at one edge and reinforced by bulbs at
other edge; naca-tn-1433; December 1947
- Jones, Alun R Holdaway,
George H Steinmetz, Charles P; A
method for calculating the heat required for windshield thermal ice prevention
based on extensive flight tests in natural icing conditions; naca-tn-1434;
November 1947
- Benscoter, S U (Bureau
of Aeronautics, Navy Department); Impact
theory for seaplane landings; naca-tn-1437; October 1947
- Hess, W F (Rensselaer
Polytechnic Institute) Winsor, F J (Rensselaer Polytechnic Institute); Further
investigation of preheating and postheating in spot-welding 0.040-inch Alclad
24S-T; naca-tn-1440; December 1947
- Deters, Owen J; Comparison of
the control-force characteristics of two types of lateral-control system for
large airplanes; naca-tn-1441; September 1947
- Johnson, Robert L
Swikert, Max A Bisson, Edmond E; Friction
at high sliding velocities; naca-tn-1442; October 1947
- Turner, L Richard
Noyes, Robert N; The
performance of a composite engine consisting of a reciprocating spark-ignition
engine, a blow-down turbine, and a steady-flow turbine; naca-tn-1447;
October 1947
- Margolis, Kenneth; Supersonic wave
drag of sweptback tapered wings at zero lift; naca-tn-1448; October
1947
- Harmon, Sidney M; Theoretical
supersonic wave drag of untapered sweptback and rectangular wings at zero
lift; naca-tn-1449; October 1947
- Goldstein, Arthur W; Analysis of
performance of jet engine from characteristics of components I : aerodynamic
and matching characteristics of turbine component determined with cold
air; naca-tn-1459; October 1947
- Racisz, Stanley F; Investigation
of NACA 65 (112) A111 (approx.) airfoil with 0.35-chord slotted flap at
Reynolds numbers up to 25 million; naca-tn-1463; 1947
- Kempner, Joseph; Recurrence
formulas and differential equations for stress analysis of cambered box
beams; naca-tn-1466; October 1947
- Dow, Norris F Hickman,
William A; Effect of
variation in diameter and pitch of rivets on compressive strength of panels
with Z-section stiffeners: panels of various stiffener spacings that fail by
local buckling; naca-tn-1467; October 1947
- Tosti, Louis P; Low-speed
static stability and damping-in-roll characteristics of some swept and unswept
low-aspect-ratio wings; naca-tn-1468; October 1947
- Neel, Carr B., Jr,
Bergrun, Norman R., Jukoff, David, Schlaff, Bernard A; The
calculation of the heat required for wing thermal ice prevention in specified
icing conditions; naca-tn-1472; December 1947
- Creagh, John W R
Hartmann, Melvin J Arthur, W Lewis, Jr; An
investigation of valve-overlap scavenging over a wide range of inlet and
exhaust pressures; naca-tn-1475; November 1947
- Polhamus, Edward C
Moss, Robert J; Wind-tunnel
investigation of the stability and control characteristics of a complete model
equipped with a vee tail; naca-tn-1478; November 1947
- Kuhn, Paul Griffith,
George E; Diagonal
tension in curved webs; naca-tn-1481; November 1947
- Gallaher, George L
Boughan, Rolla B; A
method of calculating the compressive strength of Z-stiffened panels that
develop local instability; naca-tn-1482; November 1947
- Nielsen, Jack N; Effect of
aspect ratio and taper on the pressure drag at supersonic speeds of unswept
wings at zero lift; naca-tn-1487; November 1947
- Barina, Frank J; Comparative
performance of two vaneless diffusers designed with different rates of passage
curvature for mixed-flow impellers; naca-tn-1490; November 1947
- Gray, V H Campbell, R
G; A method
for estimating heat requirements for ice prevention on gas-heated hollow
propeller blades; naca-tn-1494; December 1947
- Letko, William; Investigation
of the fuselage interference on a Pitot-static tube extending forward from the
nose of the fuselage; naca-tn-1496; December 1947
- John DeYoung; Theoretical
Additional Span Loading Characteristics of Wings with Arbitrary Sweep, Aspect
Ratio, and Taper Ratio; naca-tn-1491; December 1947
- Wilson, Herbert A , Jr,
Silverstein, Abe; Aerodynamic
characteristics of a 4-engine monoplane showing comparison of air-cooled and
liquid-cooled engine installations; naca-wr-l-471; May 1947
- Murray, Harry E Wells,
Evalyn G; Wind-tunnel
investigation of the effect of wing-tip fuel tanks on characteristics of
unswept wings in steady roll; naca-tn-1317; June 1947
- Harmon, Sidney M
Swanson, Margaret D; Calculations
of the supersonic wave drag of nonlifting wings with arbitrary sweepback and
aspect ratio : wings swept behind the Mach lines; naca-tn-1319; May
1947
- Hess, W F (Rensselaer
Polytechnic Institute) Wyant, R A (Rensselaer Polytechnic Institute) Winsor, F
J (Rensselaer Polytechnic Institute); The
spot welding of dissimilar aluminum alloys in the 0.040-inch thickness;
naca-tn-1322; October 1947
- Schuette, Evan H
Mcculloch, James C; Charts
for the minimum-weight design of multiweb wings in bending; naca-tn-1323;
June 1947
- Hoff, N J (Polytechnic
Institute of Brooklyn) Kase, Harry (Polytechnic Institute of Brooklyn)
Liebowitz, Harold (Polytechnic Institute of Brooklyn); Interaction
between the spars of semimonocoque wings with cutouts; naca-tn-1324; July
1947
- Miller, Robert W
Leshnover, Samuel; Hydrodynamic
impact loads in smooth water for a prismatic float having an angle of dead
rise of 30 degrees; naca-tn-1325; June 1947
- Tamburello, Vito Weil,
Joseph; Wind-tunnel
investigation of the effect of power and flaps on the static lateral
characteristics of a single-engine low-wing airplane model; naca-tn-1327;
June 1947
- Regier, Arthur A
Barmby, John G Hubbard, Harvey H; Effect
of critical Mach number and flutter on maximum power loading of ducked
fans; naca-tn-1330; June 1947
- Runyan, Raymond A
Jeffries, Robert J; Empirical
method for frequency compensation of the hot-wire anemometer;
naca-tn-1331; June 1947
- Solomon, Joseph Henney,
Floyd W; The
subsonic aerodynamic characteristics of two double-wedge airfoil sections
suitable for supersonic flight; naca-rm-a6g24; May 12, 1947
- Herriot, John G; : The linear
perturbation theory of axially symmetric compressible flow with application to
the effect of compressibility on the pressure coefficient at the surface of a
body of revolution; naca-rm-a6h19; July 18, 1947
- Mccormack, Gerald M
Stevens, Victor I , Jr; An
investigation of the low-speed stability and control characteristics of
swept-forward and swept-back wing in the Ames 40- by 80-foot wind tunnel;
naca-rm-a6k15; June 10, 1947
- Allen, H Julian
Heaslet, Max A Nitzberg, Gerald E; The
interaction of boundary layer and compression shock and its effect upon
airfoil pressure distributions; naca-rm-a7a02; April 10, 1947
- Spreiter, John R
Galster, George M Cooper, George E; Flight
observations of aileron flutter at high Mach numbers as affected by several
modifications; naca-rm-a7b03; April 25, 1947
- Heaslet, Max A
Nitzberg, Gerald E; The
calculation of drag for airfoil sections and bodies of revolution at
subcritical speeds; naca-rm-a7b06; April 23, 1947
- Laitone, Edmund V
Pardee, Otway O'm; Location
of detached shock wave in front of a body moving at supersonic speeds;
naca-rm-a7b10; May 06, 1947
- Hall, Charles F
Fitzgerald, Fred F; An
approximate method for calculating the effect of surface roughness on the drag
of an airplane; naca-rm-a7b24; July 23, 1947
- Axelson, John A; Longitudinal
stability and control of high-speed airplanes with particular reference to
dive recovery; naca-rm-a7c24; September 04, 1947
- Jessen, Henry, Jr; A summary
report on the effects of Mach number on the span load distribution on wings of
several models; naca-rm-a7c28; July 15, 1947
- Dannenberg, Robert E;
The
development of jet-engine Nacelles for a high-speed bomber design;
naca-rm-a7d10; August 29, 1947
- Hunton, Lynn W Dew,
Joseph K; Measurements of
the damping in roll of large-scale swept-forward and swept-back wings;
naca-rm-a7d11; July 30, 1947
- Anderson, Adrien, E; An
investigation at low speed of a large-scale triangular wing of aspect ratio
two I : characteristics of a wing having a double-wedge airfoil section with
maximum thickness at 20-percent chord; naca-rm-a7f06; November 13,
1947
- Boddy, Lee E Williams,
Walter C; A
summary and analysis of data on dive-recovery flaps; naca-rm-a7f09;
September 09, 1947
- Turner, Howard L; A comparison
with flight data of vertical-tail loads in various maneuvers estimated from
sideslip angles and rudder deflections; naca-rm-a7f25; December 11,
1947
- Erickson, Albert L
Stephenson, Jack D; A
suggested method of analyzing for transonic flutter of control surfaces based
on available experimental evidence; naca-rm-a7f30; December 16,
1947
- Brown, Harvey H Rolls,
L Stewart Clousing, Lawrence A; An
analysis of longitudinal-control problems encountered in flight at transonic
speeds with a jet-propelled airplane; naca-rm-a7g03; September 25,
1947
- Rolls, L Stewart; Comparison
between flight-measured and calculated span load distribution at high Mach
numbers; naca-rm-a7g17; November 26, 1947
- Rathert, George A , Jr
Cooper, George E; Wing-flow
tests of a triangular wing of aspect ratio two I : effectiveness of several
types of trailing-edge flaps on flat-plate models; naca-rm-a7g18; November
14, 1947
- Clousing, Lawrence A;
Precautions
for flight testing near the speed of sound; naca-rm-a7g25; November 05,
1947
- Walling, Walter C; An
investigation of the effect of tip shape on the low-speed aerodynamic
characteristics of large-scale swept wings; naca-rm-a7h13; November 13,
1947
- Anderson, Adrien E; An
investigation at low speed of a large-scale triangular wing of aspect ratio
two II : the effect of airfoil section modifications and the determination of
the wake downwash; naca-rm-a7h28; December 10, 1947
- White, Maurice D
Sadoff, Melvin Clousing, Lawrence A Cooper, George E; Preliminary
results of a flight investigation to determine the effect of negative flap
deflection on high-speed longitudinal-control characteristics;
naca-rm-a7i26; December 16, 1947
- Martin, Norman J; Tests of
submerged duct installation on a modified airplane in the Ames 40- by 80-foot
wind tunnel; naca-rm-a7i29; December 11, 1947
- Lundin, Bruce T Dowman,
Harry W Gabriel, David S; Experimental
investigation of thrust augmentation of a turbojet engine at zero ram by means
of tail-pipe burning; naca-rm-e6j21; January 06, 1947
- Jonash, Edmund R
Barnett, Henry C Stricker, Edward G; Investigation
of carbon deposition in an I-16 jet-propulsion engine at static sea-level
conditions; naca-rm-e6k01; April 29, 1947
- Cleaves, Alden P
Carver, Mildred S; Application
of an ultraviolet spectrophotometric method to the estimation of
alkylnaphthalenes in 10 experimental jet-propulsion fuels; naca-rm-e6k08;
April 30, 1947
- Imming, Harry S
Bellman, Donald R; Knock-limited
power outputs from a CFR engine using internal coolants III : four alkyl
amines, three alkanolamines six amides, and eight heterocyclic compounds;
naca-rm-e6l05a; February 03, 1947
- Acker, Loren W
Kleinknecht, Kenneth S; Flight
comparison of performance and cooling characteristics of exhaust-ejector
installation with exhaust-collector-ring installation; naca-rm-e6l13a;
February 14, 1947
- Zettle, Eugene V Bolz,
Ray E Dittrich, R T; Effect
of fuel on performance of a single combustor of an I-16 turbojet engine at
simulated altitude conditions; naca-rm-e7a24; July 03, 1947
- Lord, Albert M Donnola,
Joseph; Investigation
of pressure losses in several turbosupercharger nozzle hoses;
naca-rm-e7b11; February 11, 1947
- Brown, W Byron; Cooling of gas
turbines I : effects of addition of fins to blade tips and rotor, admission of
cooling air through part of nozzles, and change in thermal conductivity of
turbine components; naca-rm-e7b11a; February 11, 1947
- Wolfenstein, Lincoln
Meyer, Gene L Mccarthy, John S; Cooling
of gas turbines II : effectiveness of rim cooling of blades;
naca-rm-e7b11b; March 18, 1947
- Brown, W Byron
Livingood, John N; Cooling
of gas turbine III : analysis of rotor and blade temperature in liquid-cooled
gas turbine; naca-rm-e7b11c; February 11, 1947
- Brown, W Byron Monroe,
William R; Cooling of gas
turbine IV : calculated temperature distribution in the trailing part of a
turbine blade using direct liquid cooling; naca-rm-e7b11d; April 18,
1947
- Livingood, John N Sams,
Eldon W; Cooling of gas
turbines VI : computed temperature distribution through cross section of
water-cooled turbine blade; naca-rm-e7b11f; May 1947
- Sanders, J C Mendelson,
Alexander; Theoretical
evaluation of methods of cooling the blades of gas turbines;
naca-rm-e7b11g; February 11, 1947
- Reuter, J George
Gazley, Carl, Jr; Computed
temperature distribution and cooling of solid gas-turbine blades;
naca-rm-e7b11h; February 11, 1947
- Pinkel, I Irving; Determination
of ram-jet combustion-chamber temperatures by means of total-pressure
surveys; naca-rm-e7c03; March 03, 1947
- Laskin, Eugene B
Kofskey, Milton G; Increase
in stable-air-flow operating range of a mixed-flow compressor by means of a
surge inhibitor; naca-rm-e7c05; April 03, 1947
- Laskin, Eugene B
Kofskey, Milton G; Performance
of a mixed-flow impeller in combination with a semivaneless diffuser;
naca-rm-e7c05a; April 04, 1947
- Dietz, Robert O
Fleming, William A; Altitude-wind-tunnel
investigation of thrust augmentation of a turbojet engine II : performance
with water injection at compressor inlet; naca-rm-e7c12; May 19,
1947
- Black, Dugald O
Messing, Wesley E; Test-stand
investigation of a rectangular ram-jet engine; naca-rm-e7d11; May 07,
1947
- Gold, Harold Straight,
David M; A
fuel-distribution control for continuous-flow manifold injection on
reciprocating engines; naca-rm-e7d22; June 06, 1947
- Sather, Bernard I
Foster, Hampton H; Preliminary
evaluation of the performance of a uniflow two-stroke-cycle spark-ignition
engine combined with a blowdown turbine and a steady-flow turbine;
naca-rm-e7d29; November 25, 1947
- Kittel, J Howard; Preliminary
investigation of effects of gamma radiation on age-hardening rate of an
aluminum-copper alloy; naca-rm-e7e12; June 20, 1947
- Kittel, J Howard; Preliminary
investigation of effects of alpha-particle bombardment on the creep rate of
aluminum; naca-rm-e7e13; July 03, 1947
- Fleming, William A
Golladay, Richard L; Altitude-wind-tunnel
investigation of thrust augmentation of a turbojet engine III : performance
with tail-pipe burning in standard-size tail pipe; naca-rm-e7f10; August
11, 1947
- Dittrich, Ralph T; Combustion-efficiency
investigation of special fuels in single tubular-type combustor at simulated
altitude conditions; naca-rm-e7f11; August 15, 1947
- Tischler, Adelbert O
Dittrich, Ralph T; Fuel
investigation in a tubular-type combustor of a turbojet engine;
naca-rm-e7f12; August 1947
- Moeckel, W E Connors, J
F; Investigation
of shock diffusers at Mach number 1.85 III : multiple-shock and curved-contour
projecting cones; naca-rm-e7f13; August 13, 1947
- Lidman, William G; Determination
of stress-rupture parameters for four heat-resisting alloys;
naca-rm-e7g18a; August 25, 1947
- Jones, William L
Dowman, Harry W; Investigation
of thrust augmentation of a 1600-pound thrust centrifugal-flow-type turbojet
engine by injection of refrigerants at compressor inlets; naca-rm-e7g23;
August 25, 1947
- Kleinknecht, Kenneth S;
Flight
investigation of the heat requirements for ice prevention on aircraft
windshields; naca-rm-e7g28; September 05, 1947
- Ellisman, Carl; Flight
investigation of thrust augmentation of a turbojet engine by water-alcohol
injection; naca-rm-e7g29; September 29, 1947
- Bressman, Joseph R
Livingood, John N B; Cooling
of gas-turbines VII : effectiveness of air cooling of hollow turbine blades
with inserts; naca-rm-e7g30; October 20, 1947
- Whitcomb, Richard T; An
investigation of the effects of sweep on the characteristics of a
high-aspect-ratio wing in the Langley 8-foot high-speed tunnel;
naca-rm-l6j01a; February 14, 1947
- Erwin, John R Wright,
Linwood C Kantrowitz, Arthur; Investigation
of an experimental supersonic axial-flow compressor; naca-rm-l6j01b;
August 07, 1947
- Nichols, Mark R
Rinkoski, Donald W; A
low-speed investigation of an annular transonic air inlet; naca-rm-l6j04;
April 14, 1947
- Alexander, Sidney R; Drag
measurements of symmetrical circular-arc and NACA 65-009 rectangular airfoils
having an aspect ratio of 2.7 as determined by flight tests at supersonic
speeds; naca-rm-l6j14; March 07, 1947
- Alexander, Sidney R
Katz, Ellis; Drag
characteristics of rectangular and swept-back NACA 65-009 airfoils having
aspect ratios of 1.5 and 2.7 as determined by flight tests at supersonic
speeds; naca-rm-l6j16; February 24, 1947
- ALEXANDER SIDNEY R
Katz, Ellis; Flight tests to
determine the effect of length of a conical windshield on the drag of a bluff
body at supersonic speeds; naca-rm-l6j16a; January 29, 1947
- Mastrocola, N
Assadourian, A; Low-speed
wind-tunnel tests of a pilotless aircraft having horizontal and vertical wings
and cruciform tail; naca-rm-l6j18a; August 19, 1947
- Pitkin, Marvin Garner,
William N Curfman, Howard J , Jr; Results
of preliminary flight investigation of aerodynamic characteristics of the NACA
two-stage supersonic research model RM-1 stabilized in roll at transonic and
supersonic velocities; naca-rm-l6j23; March 19, 1947
- Huber, Paul W; Preliminary
tests of a burner for ram-jet applications; naca-rm-l6k08b; January 15,
1947
- Jones, Robert T
Sternfield, Leonard; A
method for predicting the stability in roll of automatically controlled
aircraft based on the experimental determination of the characteristics of an
automatic pilot; naca-rm-l6k12; January 17, 1947
- Sweberg, Harold H
Lange, Roy H; Summary
of available data relating to Reynolds number effects on the maximum lift
coefficients of swept-back wings; naca-rm-l6l20a; March 04, 1947
- Ellerbrock, Herman H ,
Jr; General
treatment of compressible flow in ejectors and example of its application to
problem of effect of ejector addition on thrust of jet-propulsion units;
naca-rm-l6l23; June 16, 1947
- Mathews, Charles W
Thompson, Jim Rogers; Free-fall
measurements at transonic velocities of the drag of a wing-body configuration
consisting of a 45 degree swept-back wing mounted forward of the maximum
diameter on a body of fineness ratio 12; naca-rm-l6l26; April 02,
1947
- Mastrocola, N; Effect
of number of fins on the drag of a pointed body of revolution at low
supersonic velocities; naca-rm-l7a08; April 07, 1947
- Katz, Ellis R; Results
of flight tests at supersonic speeds to determine the effect of body nose
fineness ratio on body and wing drag; naca-rm-l7b19; June 26, 1947
- Silsby, Norman S; Comparative
drag measurements at transonic speeds of 6-percent-thick airfoils of
symmetrical double-wedge and circular-arc sections from tests by the NACA
wing-flow method; naca-rm-l7b20; April 08, 1947
- Tucker, Warren A
Nelson, Robert L; Drag
characteristics of rectangular and swept-back NACA 65-009 airfoils having
various aspect ratios as determined by flight tests at supersonic speeds;
naca-rm-l7c05; April 22, 1947
- Loving, Donald L; Aerodynamic
measurements made during Navy investigation of human tolerance to wind
blasts; naca-rm-l7c25; March 11, 1947
- Adams, Richard E
Silsby, Norman S; Tests
of a horizontal-tail model through the transonic speed range by the NACA
wing-flow method; naca-rm-l7c25a; April 11, 1947
- Sandahl, Carl A Marino,
Alfred A; Free-flight
investigation of control effectiveness of full-span 0.2-chord plain ailerons
at high subsonic, transonic, and supersonic speeds to determine some effects
of section thickness and wing sweepback; naca-rm-l7d02; May 29,
1947
- Johnston, J Ford
Danforth, Edward C B; Some
pressure-distribution measurements on a swept-wing at transonic speeds by the
NACA wing-flow method; naca-rm-l7d22; June 06, 1947
- Johnson, Harold I; Measurements of
aerodynamic characteristics of a 35 degree sweptback NACA 65-009 airfoil model
with 1/4-chord plain flap by the NACA wing-flow method; naca-rm-l7f13;
August 05, 1947
- Schneiter, Leslie E
Ziff, Howard L; Preliminary
investigation of spoiler lateral control on a 42 degree sweptback wing at
transonic speeds; naca-rm-l7f19; August 12, 1947
- Sedov, L.; Scale
effect and optimum relations for sea surface planing; naca-tm-1097;
1947
- Busemann, Adolf; Infinitesimal
conical supersonic flow; naca-tm-1100; 1947
- Sanger, E., Bredt, I.;
A ram-jet
engine for fighters; naca-tm-1106; 1947
- Theil, G., Weissinger,
F.; Six-component
measurements on a straight and a 35 degree swept-back trapezoidal wing with
and without split flap; naca-tm-1107; 1947
- Lemme, H. G.; Force
and pressure-distribution measurements on a rectangular wing with a slotted
droop nose and with either plain and split flaps in combination or a slotted
flap; naca-tm-1108; 1947
- Ackeret, J., Feldmann,
F., Rott, N.; Investigations
of compression shocks and boundary layers in gases moving at high speed;
naca-tm-1113; 1947
- Gothert, B., Kawalki,
K. H.; Calculation of
Compressible Flows with local regions of supersonic velocity;
naca-tm-1114; 1947
- Eckert, Korbacher; The flow
through axial turbine stages of large radial blade length; naca-tm-1118;
1947
- Weissinger, J.; The lift
distribution of swept-back wings; naca-tm-1120; 1947
- Ulrich, A.; Theoretical
investigation of drag reduction in maintaining the laminar boundary layer by
suction; naca-tm-1121; 1947
- ; Systematic
wind-tunnel measurements on missiles; naca-tm-1122; 1947
- Encke, W.; Investigations
on experimental impellers for axial blowers; naca-tm-1123; 1947
- Sauer, R.; Method
of characteristics for three-dimensional axially symmetrical supersonic
flows; naca-tm-1133; 1947
- Bussmann, K., Ulrich,
A.; Systematic
investigations of the influence of the shape of the profile upon the position
of the transition point; naca-tm-1185; 1947
- Van Dorn, Nicholas H.,
DeYoung, John.; A
comparison of three theoretical methods of calculating span load distribution
on swept wings; naca-rm-a7c31; 1947
- Hickel, Robert O.,
Snider, William E.; Acceleration
characteristics of R-3350 engine equipped with NACA injection impeller;
naca-rm-e6l03a; 1947
- Kohl, Robert. C.,
Diggs, Donald. R.; Effect
of various methods of boundary-layer control on performance of V-1710-93
engine-stage supercharger; naca-rm-e6l19; 1947
- Rosenbaum, Burt M.; The crystal
structure at room temperature of six cast heat-resisting alloys;
naca-rm-e7d23; 1947
- Schum, Harold J.,
Buckner, Howard A.; Investigation
of 10-stage axial flow X24C-2 compressor. : I Performance at inlet pressure of
21 inches mercury absolute and inlet temperature of 538 degree;
naca-rm-e7g11; 1947
- Dowman, Harry W.,
Anderson, William G.; Investigation
of sea-level performance of I-16 turbojet engine at zero ram with XFR-1 intake
duct shroud, and tail pipe; naca-rm-e7g24; 1947
- Finger, Harold B.,
Schum, Harold J., Buckner, Howard A; Investigation
of X24C-2 10-stage axial-flow compressor. : II-Effect of inlet-air pressure
and temperature on performance; naca-rm-e7h22; 1947
- Hoyt, Jack W., Kottas,
Harry; Investigation
of turbine of Mark 25 torpedo power plant with five nozzld designs;
naca-rm-e7i03; 1947
- Saari, Martin J.,
Wallner, Lewis E.; Preliminary
results of an altitude-wind-tunnel investigation of a TG-100 gas
turbine-propeller engine :IV. Compressor and turbine performance
characteristics; naca-rm-e7j20; 1947
- Anderson, Joseph L.; Wind-tunnel
development of means to alleviate buffeting on the North American XP-82
airplane at high speeds; naca-rm-a6l10; 1947
- Bunnel, Mort V.,
Delany, Noel K.; Comparison
of wind-tunnel predictions with flight measurements of the
longitudinal-stability and control characteristics of a douglas BTD-1
airplane; naca-rm-a6l30; 1947
- Turner, Howard L.; Buffeting of
external fuel tanks at high speeds on a grumman F7F-3 airplane;
naca-rm-a7a07; 1947
- Barnes, Robert H.; High-speed load
distribution on the wing of a 3/16-scale model of the Douglas XSB2D-1 airplane
with flaps defected; naca-rm-a7a30; 1947
- Stalder, Jackson R.,
Wadleigh, Kenneth R.; A
preliminary study of ram-actuated cooling systems for supersonic aircraft;
naca-rm-a7c04; 1947
- Robinson, Robert C.; High-speed
aerodynamic characteristics of a 1/7-scale model of the Northrop YB-49
airplane; naca-rm-a7c13; 1947
- Barnes, Robert H.; High-speed load
distribution on the wing of a 3/16-scale model of a scout-bomber airplane with
flaps deflected /y Robert H. Barnes; naca-rm-a7d23; 1947
- Perone, Angelo,
Berthold, Cecil L.; Aerodynamic
characteristics of a portion of the horizontal tail from a douglas C-74
airplane with fabric-covered elevators; naca-rm-a7d28; 1947
- McCullough, George B.,
Weiberg, James A., Gault, Donald E.; Stick-fixed
stability and control characteristics of the consolidated vultee model 240
airplane as estimated from tests of a 0.092-scale powered model;
naca-rm-a7f19; 1947
- Anderson, Seth B.,
Christofferson, Frank E., Clousing, Lawrence A.; Flight
measurements of the flying qualities of a Lockheed P-80A airplane (Army no.
44-85099)- longitudinal-stability and -control characteristics;
naca-rm-a7g01; 1947
- Hunton, Lynn W.; Force tests of
the boeing XB-47 full-scale empennage in the Ames 40- by 80-foot wind
tunnel; naca-rm-a7h12; 1947
- Millenson, M.B.,
Manson, S.S.; Investigation
of rim cracking in turbine wheels with welded blades; naca-rm-e6l17; Feb.
12, 1947
- Conrad, E. W., Durham,
J. D.; Preliminary
results of an altitude-wind-tunnel investigation of a TG-100A gas
turbine-propeller engine II - windmilling characteristics; naca-rm-e7g25;
1947
- Geisenheyner, Robert
M., Berdysz, Joseph J.; Preliminary
results of an altitude-wind-tunnel investigation of a TG-100A gas
turbine-propeller engine III - pressure and temperature distributions;
naca-rm-e7j02; 1947
- Krueger, W.; Systematic
wind-tunnel measurements on a laminar wing with nose flap; naca-tm-1119;
1947
- Shultz-Grunow, F.; Gas-dynamic
investigations of the pulse-jet tube, parts I and II; naca-tm-1131;
1947
- Eckert, B.; Possibilities
of reducing the length of axial superchargers for aircraft motors;
naca-tm-1132; 1947
- Yudin, E. Y.; On
the vortex sound from rotating rods; naca-tm-1136; 1947
- Zborowski, Helmut; Rocket power
plants based on Nitric Acid and their specific propulsive weights;
naca-tm-1145; 1947
- Schwier, W.; Lift
increase by blowing out air, tests on airfoil of 12 percent thickness, using
various types of flap; naca-tm-1148; 1947
- Ilgmann, G., Moller,
E.; Three-component
force and mass-flow measurements on a jet nacelle; naca-tm-1149;
1947
- Weise, A.; The
separation of flow due to compressibility shock; naca-tm-1152; 1947
- Nekrasov, A. I.; Theory of wings
in nonstationary flow; naca-tm-1154; 1947
- Hantzsche, W., Wendt,
H.; Cones in
supersonic flow; naca-tm-1157; 1947
- Ludwieg, H.; Drag
corrections in high-speed wind tunnels; naca-tm-1163; 1947
- Kruger, W.; Drag
reduction by suction of the boundary layer separated behind shock wave
formation at high mach numbers; naca-tm-1168; 1947
- Denkmeier, H., Gross,
K.; Description of
Russian aircraft engines "AM 35" and "AM 38"; naca-tm-1169; 1947
- Kuhl, H.; Preliminary
report on the fundamentals of the control of turbine-propeller jet power
plants; naca-tm-1172; 1947
- Hausenblas; Pressure
distribution measurements on a turbine rotor blade passing behind a turbine
nozzle lattice; naca-tm-1173; 1947
- Pollmann, Erich; Temperatures
and stresses on hollow blades for gas turbines; naca-tm-1183; 1947
- Zobel, Th.; Development
and construction of an interferometer for optical measurements of density
fields; naca-tm-1184; 1947
- Ilyushin, A. A.; The
elasto-plastic stability of plates; naca-tm-1188; 1947
- Lewis, William; A flight
investigation of the meteorological conditions conducive to the formation of
ice on airplanes; naca-tn-1393; 1947
- Sivells, James C.; Experimental
and calculated characteristics of three wings of NACA 64-210 and 65-210
airfoil sections with and without 2 degree washout; naca-tn-1422;
1947
- Hunter, P. A., Vensel,
J. R.; A
flight investigation to increase the safety of a light airplane;
naca-tn-1203; 1947
- Bates, William R.; Collection and
Analysis of Wind-Tunnel Data on the Characteristics of Isolated Tail Surfaces
with and Without End Plates; naca-tn-1291; 1947
- Malvestuto, Frank S
Gale, Lawrence J; Formulas
for additional mass corrections to the moments of inertia of airplanes;
naca-tn-1187; February 1947
- Mossman, Emmet A.,
Gault, Donald E.; Development
of NACA submerged inlets and a comparison with wing leading-edge inlets for a
1/4-scale model of a fighter airplane; naca-rm-a7a31; 1947
- Martin, Norman J.; Tests of
submerged duct installation on the Ryan FR-1 airplane in the Ames 40- by
80-foot wind tunnel /y Norman J. Martin; naca-rm-a7d14; 1947
- Turner, Howard L.,
Cooper, George E.; Partial
measurements in flight of the flying qualities of a Grumman XF7F-1 airplane
with a modified vertical tail; naca-rm-a7d15; 1947
- Anderson, Seth B.,
Cooper, George E.; Flight
measurements of the flying qualities of lockheed P-80A airplane (Army No.
44-85099). -lateral- and directional-stability and control
characteristics; naca-rm-a7j24; 1947
- Robert C. Robinson and
Angelo Perone; High-speed
longitudinal stability and control of the Bell P-39N-1 airplane as calculated
from propeller-off tests of a 0.35-scale; naca-rm-a6l27; 1947
- Cleary, Joseph W.,
Gray, Lyle J.; High-speed
wind-tunnel tests of a model of the lockheed YP-80A airplane including
correlation with flight tests and tests of dive-recovery flaps;
naca-rm-a7a29; 1947
- Richard T. Whitcomb; Method for
Stress Analysis of a Swept Propeller; naca-rm-L8F11; September,
1948
- Emmet A. Mossman,
Lauros M. Randall; An
experimental investigation of the design variables for NACA;
naca-rm-a7i30; January, 1948
- Budiansky, Bernard
Connor, Robert W Stein, Manuel; Buckling
in shear of continuous flat plates; naca-tn-1565; April 1948
- Mary M. Neice; Tables
and charts of flow parameters across oblique shocks; naca-tn-1673; Aug
1948
- Bernard Budiansky,
Manuel Stein, Arthur C. Gilbert; Buckling
of a long square tube in torsion and compression; naca-tn-1751; November
1948
- J. W. Freeman, E. E.
Reynolds, A. E. WHITE; The
rupture-test characteristics of heat-resistant sheet alloys at 1700 F and 1800
F; naca-tn-1465; Feb 1948
- L. R. Jackson, H. C.
Cross, J. M. Berry; Tensile,
fatigue, and creep properties of forged aluminum alloys at temperatures up to
800 F; naca-tn-1469; Mar 1948
- E. S. Machlin; Dislocation
theory of the fatigue of metals; naca-tn-1489; Jan 1948
- B. W. Sakmann, B. G.
Rightmire; An
investigation of fretting corrosion under several conditions of oxidation;
naca-tn-1492; June 1948
- G. Guderley; Non-stationary
gas flow in thin pipes with variable cross section; naca-tm-1196; December
1948
- N. J. Hoff, Bertram
Klein, Bruno A. Boley; The
inward bulge type buckling of monocoque cylinders V : revised strain energy
theory which assumes a more general deflected shape at buckling;
naca-tn-1505; Sep 1948
- J. W. Freeman, E. E.
Reynolds, A. E. White; A
metallurgical investigation of five forged gas-turbine discs of Timken
alloy; naca-tn-1531; Jun 1948
- E. E. Reynolds, J. W.
Freeman, A. E. White; A
metallurgical investigation of a contour-forged disc of EME alloy;
naca-tn-1534; Nov 1948
- E. E. Reynolds, J. W.
Freeman, A. E. White; A
metallurgical investigation of two turbosupercharger discs of 19-9DL
alloy; naca-tn-1535; Nov 1948
- E. G. Thomsen, I.
Cornet, I. Lotze, J. E. Dorn; Investigation
of the validity of an ideal theory of elasto-plasticity for wrought aluminum
alloys; naca-tn-1552; Jul 1948
- William N. Findley,
Will J. Worley; Mechanical
properties of five laminated plastics; naca-tn-1560; Aug 1948
- Robert L. Johnson,
Douglas Godfrey, Edmond E. Bisson; Friction
of solid films on steel at high sliding velocities; naca-tn-1578; Apr
1948
- B. M. Rosenbaum; X-ray
diffraction investigation of minor phases of 20 high-temperature alloys;
naca-tn-1580; Jul 1948
- Thomas A. Toll, M. J.
Queijo; Approximate
relations and charts for low-speed stability derivatives of swept wings;
naca-tn-1581; May 1948
- Donald R. Mulholland,
Porter J. Perkins; Investigation
of effectiveness of air-heating a hollow steel propeller for protection
against icing I : unpartitioned blades; naca-tn-1586; May 1948
- Porter J. Perkins,
Donald R. Mulholland; Investigation
of effectiveness of air-heating a hollow steel; naca-tn-1587; May
1948
- Donald R. Mulholland,
Porter J. Perkins; Investigation
of effectiveness of air-heating a hollow steel propeller for protection
against icing : 25-percent partitioned blades; naca-tn-1588; May
1948
- G. Merritt Preston,
Calvin C. Blackman; Effects
of ice formations on airplane performance in level cruising flight;
naca-tn-1598; May 1948
- Bernard A. Schlaff,
James Selna; An
investigation of a thermal ice-prevention system for a cargo airplane IX : the
temperature of the wing leading-edge structure as established in flight;
naca-tn-1599; Jun 1948
- Charles A. Hoffman, G.
Mervin Ault; Application of
statistical methods to study of gas-turbine blade failures; naca-tn-1603;
Jun 1948
- Alfred Gessow; Standard
symbols for helicopters; naca-tn-1604; Jun 1948
- Felicien F. Fullmer,
Jr; Two-dimensional
wind-tunnel investigation of an NACA 64-009 airfoil equipped with two types of
leading-edge flap; naca-tn-1624; Jun 1948
- D. G. Moore, L. H.
Bolz, W. N. Harrison; A
study of ceramic coatings for high-temperature protection of molybdenum;
naca-tn-1626; Jul 1948
- William Gracey; The
experimental determination of the moments of inertia of airplanes by a
simplified compound-pendulum method; naca-tn-1629; Jun 1948
- Stanley F. Racisz, John
H. Quinn; Wind-tunnel
investigation of boundary-layer control by suction on NACA 655-424 airfoil
with double slotted flap; naca-tn-1631; Jun 1948
- Jean Gilman, Jr; Wind-tunnel
tests and analysis of two 10-foot-diameter six-blade dual-rotating tractor
propeller differing in pitch distribution; naca-tn-1634; Jun 1948
- Harry Press; A
statistical analysis of gust-velocity measurements as affected by pilots and
airplanes; naca-tn-1645; Jun 1948
- Leslie E. Schneiter,
James M. Watson; Low-speed
wind-tunnel investigation of various plain-spoiler configurations for lateral
control on a 42 degree sweptback wing; naca-tn-1646; Jun 1948
- A. W. Vogeley; Sound-level
measurements of a light airplane modified to reduce noise reaching the
ground; naca-tn-1647; Jul 1948
- Gerald W. Brewer, Ralph
W. May, Jr; Investigation
of a one-seventh-scale powered model of a twin-boom airplane and a comparison
of its stability, control, and performance with those of a similar all-wing
airplane; naca-tn-1649; Oct 1948
- J. Conrad Crown; Supersonic
nozzle design; naca-tn-1651; Jun 1948
- A. Kahane; Investigation
of axial-flow fan and compressor rotors designed for three-dimensional
flow; naca-tn-1652; Jul 1948
- Harvey H. Hubbard; Sound from
dual-rotating and multiple single-rotating propellers; naca-tn-1654; July
1948
- Marion O. Mckinney,
Robert E. Shanks; Lateral
stability and control characteristics of a free-flying model having an unswept
wing with an aspect ratio of 2; naca-tn-1658; Jul 1948
- Jack Fischel, Leslie E.
Schneiter; High-speed
wind-tunnel investigation of an NACA 65-210 semispan wing equipped with plug
and retractable ailerons and a full-span slotted flap; naca-tn-1663; Jul
1948
- Holms, Arthur G
Jenkins, Joseph E; Effect
of strength and ductility on burst characteristics of rotating disks;
naca-tn-1667; July 1948
- Elbridge Z. Stowell; Critical shear
stress of an infinitely long plate in the plastic region; naca-tn-1681;
Aug 1948
- George B. Mccullough,
Donald E. Gault; An
experimental investigation of an NACA 631-012 airfoil section with
leading-edge suction slots; naca-tn-1683; Aug 1948
- H. Press, E. T.
Binckley; A
preliminary evaluation of the use of ground radar for the avoidance of
turbulent clouds; naca-tn-1684; Sep 1948
- Lagerstrom, P A
(California Institute of Technology); Linearized
supersonic theory of conical wings; naca-tn-1685; 1950
- John G. Lowry, John M.
Riebe; Effect of
length-beam ratio on aerodynamic characteristics of flying-boat hulls without
wing interference; naca-tn-1686; Sep 1948
- K. R. Czarnecki, Don D.
Davis, Jr; Dynamometer-stand
investigation of the muffler used in the demonstration of light-airplane noise
reduction; naca-tn-1688; Oct 1948
- W. E. Moeckel, J. C.
Evvard; Load
distributions due to steady roll and pitch for thin wings at supersonic
speeds; naca-tn-1689; Aug 1948
- Daniel Savitsky; Theoretical and
experimental wing-tip accelerations of a small flying boat during landing
impacts; naca-tn-1690; Sep 1948
- James P. Lewis, Howard
C. Stevens; Icing and
de-icing of a propeller with internal electric blade heaters;
naca-tn-1691; Aug 1948
- F. R. Steinbacher, Hsu
Lo; Determination
of bending moments in pressure-loaded rings of arbitrary shape when
deflections are considered; naca-tn-1692; Sep 1948
- Walter G. Walker; An analysis of
the airspeeds and normal accelerations of Martin M-130 airplanes in commercial
transport operation; naca-tn-1693; Sep 1948
- Margaret F. Steiner; Analysis of
planning data for use in predicting hydrodynamic impact loads;
naca-tn-1694; Aug 1948
- Paul J. Carpenter; Effect of wind
velocity on performance of helicopter rotors as investigated with the Langley
helicopter apparatus; naca-tn-1698; Oct 1948
- John C. Evvard; A linearized
solution for time-dependent velocity potentials near three-dimensional wings
at supersonic speeds; naca-tn-1699; Sep 1948
- Authur L. Jones, John
R. Spreiter, Alberta Alksne; The
rolling moment due to sideslip of triangular, trapezoidal, and related plan
forms in supersonic flow; naca-tn-1700; Oct 1948
- Morris A. Zipkin,
George W. Lewis, Jr; Analytical
and experimental performance of an explosion-cycle combustion chamber for a
jet-propulsion engine; naca-tn-1702; Sep 1948
- H. Page Hoggard, Jr,
John R. Hagerman; Downwash
and wake behind untapered wings of various aspect ratios and angles of
sweep; naca-tn-1703; Oct 1948
- Albert L. Braslow,
Fioravante Visconti; Investigation
of boundary-layer Reynolds number for transition on an NACA 65(215)-114
airfoil in the Langley two-dimensional low-turbulence pressure tunnel;
naca-tn-1704; Oct 1948
- George E. Griffith; Experimental
investigation of the effects of plastic flow in a tension panel with a
circular hole; naca-tn-1705; Sep 1948
- Sidney M. Harmon; Stability
derivatives of thin rectangular wings at supersonic speeds : wing diagonal
ahead of tip mach lines; naca-tn-1706; Nov 1948
- Warren A. Tucker,
Robert L. Nelson; Theoretical
characteristics in supersonic flow of constant-chord partial-span control
surfaces on rectangular wings having finite thickness; naca-tn-1708; Sep
1948
- Gerald Hieser, Charles
F. Whitcomb; Investigation
of the effects of a nacelle on the aerodynamic characteristics of a swept wing
and the effects of sweep on a wing alone; naca-tn-1709; Oct 1948
- Alexander Gomza, Paul
Seide; Minimum-weight
design of simply supported transversely stiffened plates under
compression; naca-tn-1710; Sep 1948
- Thomas A. Toll, Leslie
E. Schneiter; Approximate
relations for hinge-moment parameters of control surfaces on swept wings at
low Mach numbers; naca-tn-1711; Oct 1948
- A. R. Bobrowsky; Analytical
method of determining transmission of particles and radiation through great
thickness of matter; naca-tn-1712; Sep 1948
- Guy R. Bradshaw, Eugene
B. Laskin; Experimental
study of effect of vaneless-diffuser diameter on diffuser performance;
naca-tn-1713; Oct 1948
- George L. Gallaher; Plate
compressive strength of FS-1H magnesium-alloy sheet and a maximum-strength
formula for magnesium-alloy and aluminum-alloy formed sections;
naca-tn-1714; Oct 1948
- Vera Huckel; Tables
of hypergeometric functions for use in compressible-flow theory;
naca-tn-1716; Oct 1948
- Harold B. Pierce; Gust-tunnel
investigation of a 45 degree swept-forward-wing model; naca-tn-1717; Oct
1948
- Clarence B. Cohen; Influence of
leading-edge suction on lift-drag ratios of wings at supersonic speeds;
naca-tn-1718; Oct 1948
- Allen R. Stokke,
William S. Aiken, Jr; Flight
measurements of buffeting tail loads; naca-tn-1719; Oct 1948
- Robert L. Johnson, Max
A. Seikert, Edmond E. Bisson; Friction
at high sliding velocities of surfaces lubricated with sulfur as an
additive; naca-tn-1720; Oct 1948
- A. W. Vogeley; Calculation
of the effect of thrust-axis inclination on propeller disk loading and
comparison with flight measurements; naca-tn-1721; Oct 1948
- Joseph Weil, William C.
Sleeman, Jr; Prediction of
the effects of propeller operation on the static longitudinal stability of
single-engine tractor monoplanes with flaps retracted; naca-tn-1722; Oct
1948
- Joseph L. Johnson,
Leonard Sternfield; A
theoretical investigation of the effect of yawing moment; naca-tn-1723;
Oct 1948
- Hsu Lo; Determination
of transient skin temperature of conical bodies during short-time, high-speed
flight; naca-tn-1725; Oct 1948
- William W. Hodges,
David R. Woodward; Spray
characteristics of four flying-boat hulls as affected by length-beam
ratio; naca-tn-1726; Oct 1948
- Leonard Sternfield,
Ordway B. Gates, Jr; A
simplified method for the determination and analysis of the
neutral-lateral-oscillatory-stability boundary; naca-tn-1727; Oct
1948
- Paul Kuhn, James P.
Peterson; Shear lag in
axially loaded panels; naca-tn-1728; Oct 1948
- William S. Aiken, Jr;
Flight
determination of wing and tail loads on a fighter-type airplane by means of
strain-gage measurements; naca-tn-1729; Oct 1948
- Dezso Ladanyi; Effects
of temporal tangential bearing acceleration on performance characteristics of
slider and journal bearings; naca-tn-1730; Oct 1948
- D. G. Moore, J. C.
Richmond, W. N. Harrison; High-temperature
attack of various compounds on four heat-resisting alloys; naca-tn-1731;
Oct 1948
- M. J. Queijo, Byron M.
Jaquet; Calculated
effects of geometric dihedral on the low-speed rolling derivatives of swept
wings; naca-tn-1732; Oct 1948
- Walter G. Walker; An analysis of
the airspeeds and normal accelerations of Sikorsky S-42A airplanes in
commercial transport operation; naca-tn-1733; Oct 1948
- Paul W. Harper, Roy E.
Flanigan; Investigation
of the variation of maximum lift for a pitching airplane model and comparison
with flight results; naca-tn-1734; Oct 1948
- Richard B. Parisen,
John C. Armstrong, Sidney C. Huntley; Theoretical
evaluation of the ducted-fan turbojet engine; naca-tn-1745; Nov
1948
- Leland G. Desmon, Eldon
W. Sams; Performance of
exhaust-gas blowdown turbine and various engine systems using a 12-cylinder
liquid-cooled engine; naca-tn-1735; Nov 1948
- Harold Mirels; Theoretical
method for solution of aerodynamic forces on thin wings in nonuniform
supersonic stream with an application to tail surfaces; naca-tn-1736; Nov
1948
- Norris F. Dow, William
A. Hickman; Effect of
variation in diameter and pitch of rivets on compressive strength of panels
with Z-section stiffeners panels that fail by local buckling and have various
values of width-to-thickness ratio for the webs of the stiffeners;
naca-tn-1737; Nov 1948
- Harry E. Murray; Comparison with
experiment of several methods of predicting the lift of wings in subsonic
compressible flow; naca-tn-1739; Oct 1948
- Reese H. Ivey, Robert
R. Morrissette; An
approximate determination of the lift of slender cylindrical bodies and
wing-body combinations at very high supersonic speeds; naca-tn-1740; Oct
1948
- Robert J. Nuber, James
R. Needham, Jr; Exploratory
wind-tunnel investigation of the effectiveness of area suction in eliminating
leading-edge separation over an NACA 641A212 airfoil; naca-tn-1741; Nov
1948
- Vernard E. Lockwood,
James M. Watson; Stability
and control characteristics at low speed of an airplane model having a 38.7
degree sweptback wing with aspect ratio 4.51, taper ratio 0.54, and
conventional tail surfaces; naca-tn-1742; Dec 1948
- S. A. Sjoberg, J. P.
Reeder; Flight
measurements of the stability, control, and stalling characteristics of an
airplane having a 35 degree sweptback wing without slots and with
80-percent-span slots and a comparison with wind-tunnel data;
naca-tn-1743; Nov 1948
- John D. Stanitz; Two-dimensional
compressible flow in conical mixed-flow compressors; naca-tn-1744; Nov
1948
- Howard W. Emmons; Flow of a
compressible fluid past a symmetrical airfoil in a wind tunnel and in free
air; naca-tn-1746; Nov 1948
- Roger A. Anderson, John
C. Houbolt; Determination
of coupled and uncoupled modes and frequencies of natural vibration of swept
and unswept wings from uniform cantilever modes; naca-tn-1747; Nov
1948
- S. Katzoff, Margery E.
Hannah; Calculation of
tunnel-induced upwash velocities for swept and yawed wings; naca-tn-1748;
Nov 1948
- Stanley U. Benscoter;
Shear flows
in multicell sandwich sections; naca-tn-1749; Nov 1948
- Roger W. Peters; Buckling tests
of flat rectangular plates under combined shear and longitudinal
compression; naca-tn-1750; Nov 1948
- Edward C. Polhamus; Jet-boundary-induced-upwash
velocities for swept reflection-plane models mounted vertically in 7- by
10-foot, closed, rectangular wind tunnels; naca-tn-1752; Nov 1948
- Harry C. Mickleboro; Evaluation of a
fixed spoiler as a gust alleviator; naca-tn-1753; Nov 1948
- Walter G. Walker; An analysis of
the airspeed and normal accelerations of Douglas DC-2 airplanes in commercial
transport operation; naca-tn-1754; Nov 1948
- Ross L. Levin; Ultimate
stresses developed by 24S-T and Alclad 75S-T aluminum-alloy sheet in
incomplete diagonal tension; naca-tn-1756; Nov 1948
- Ralph E. Grey, H. Dean
Wilsted; Performance of
conical jet nozzles in terms of flow and velocity coefficients;
naca-tn-1757; Nov 1948
- J. W. Freeman, E. E.
Reynolds, D. N. Frey; Properties
of 19-9DL alloy bar stock at 1200 F; naca-tn-1758; Nov 1948
- F. E. West, J. M.
Hallisy; Effect of
compressibility on normal-force, pressure, and load characteristics of a
tapered wing of NACA 66-series airfoil sections with split flaps;
naca-tn-1759; Dec 1948
- Marcus F. Heidmann,
David Novik; Control
considerations for optimum power proportionment in turbine-propeller
engines; naca-tn-1762; Dec 1948
- Mungall, Robert C; Flight
investigation of a combined geared unbalancing-tab and servotab control system
as used with an all-movable horizontal tail; naca-tn-1763; December
1948
- Walter J. Klinar,
Thomas L. Snyder; Influence
of tail length upon the spin-recovery characteristics of a
trainer-type-airplane model; naca-tn-1764; Dec 1948
- Warren A. Tucker,
Robert L. Nelson; The
flexible rectangular wing in roll at supersonic flight speeds;
naca-tn-1769; Dec 1948
- Victor I. Stevens; Theoretical
basic span loading characteristics of wings with arbitrary sweep, aspect
ratio, and taper ratio; naca-tn-1772; Dec 1948
- Laurence K. Loftin,
William J. Bursnall; The
effects of variations in Reynolds number between 3.0 x 10 to the power 6 and
25.0 x 10 to the power 6 upon the aerodynamic characteristics of a number of
NACA 6-series airfoil sections; naca-tn-1773; Dec 1948
- Alexander Mendelson; Calculated
performance of a compression-ignition engine-compressor-turbine combination
based on experimental data; naca-tn-1774; Dec 1948
- Donald R. Bellman, Jack
C. Humphrey; Photographic
study of combustion in a rocket engine I : variation in combustion of liquid
oxygen and gasoline with seven methods of propellant injection;
naca-rm-e8f01; Aug 1948
- Lawrence J. Gale, Ira
P. Jones; Effects of
antispin fillets and dorsal fins on the spin and recovery characteristics of
airplanes as determined from free-spinning-tunnel tests; naca-tn-1779; Dec
1948
- Jack N. Nielsen, Edward
W. Perkins; Charts for the
conical part of the downwash field of swept wings at supersonic speeds;
naca-tn-1780; Dec 1948
- Walter G. Walker, Ivan
K. Hadlock; An analysis of
the airspeeds and normal accelerations of Boeing B-247 and B-247D airplanes in
commercial transport operation; naca-tn-1783; Dec 1948
- Ascher H. Shapiro, R.
Douglas Smith; Friction
coefficients in the inlet length of smooth round tubes; naca-tn-1785; Nov
1948
- William m. Kauffman,
Allan Smith, Charles J. Liddell, Jr, George E. Cooper; Flight
tests of an apparatus for varying dihedral effect in flight; naca-tn-1788;
Dec 1948
- Morton Cooper, Peter F.
Korycinski; The effects of
compressibility on the lift, pressure, and load characteristics of a tapered
wing of NACA 66-series airfoil sections; naca-tn-1697; Oct 1948
- M. B. Millenson, S. S.
Manson; Determination
of stresses in gas-turbine disks subjected to plastic flow and creep;
naca-tn-1636; Jun 1948
- Wilber B. Huston,
Calvin N. Warfield, Anna Z. Stone; A
study of skin temperatures of conical bodies in supersonic flight;
naca-tn-1724; Oct 1948
- Leslie E. Schneiter,
Rodger L. Naeseth; Wind-tunnel
investigation at low speed of the lateral control characteristics of ailerons
having three spans and three trailing-edge angles on a semispan wing
model; naca-tn-1738; Nov 1948
- J. F. Connors, A. H.
Schroeder; Preliminary
investigation of effects of combustion in ram jet on performance of supersonic
diffusers I : shock diffuser with triple-shock projecting cone;
naca-rm-e8f15; Sep 1948
- Roland Breitwieser; Performance of
a ram-jet-type combustor with flame holders immersed in the combustion
zone; naca-rm-e8f21; Nov 1948
- Eugene V. Zettle,
William P. Cook; Performance
investigation of can-type combustor II : water injection at various stations
in combustor; naca-rm-e8f28; Sep 1948
- Clyde C. Swett, Jr.; Investigation
of spark gaps subjected to altitude and air velocity conditions;
naca-rm-e8i17; Nov 1948
- Sterbentz, William H
Wilcox, Fred A; Investigation
of effects of movable exhaust-nozzle plug on operational performance of
20-inch ram jet; naca-rm-e8d22; July 27, 1948
- David G. Stone; Flight-test
evaluation of the longitudinal stability and control characteristics of
0.5-scale models of the lark pilotless-aircraft configuration;
naca-rm-l7i26; Feb 1948
- J. G. Barmby, J. M.
Teitelbaum; Initial flight
tests of the NACA FR-2, a high-velocity rocket-propelled vehicle for transonic
flutter research; naca-rm-l7j20; Mar 1948
- Edward C. B. Danforth,
J. Ford Johnston; Pressure
distribution over a sharp-nose body of revolution at transonic speeds by the
NACA wing-flow method; naca-rm-l7k12; Mar 1948
- S. A. Clevenson,
William T. Lauten, Jr.; Flutter
investigation in the transonic range of six airfoils attached to three freely
falling bodies; naca-rm-l7k17; May 1948
- Hsu Lo; Determination
of transient skin temperature of conical bodies during short-time, high-speed
flight; naca-rm-l7k17a; Apr 1948
- Carl A. Sandahl, H.
Kurt Strass; Additional
results in a free-flight investigation of control effectiveness of full-span,
0.2-chord plain ailerons at high subsonic, transonic, and supersonic speeds to
determine some effects of wing sweepback, aspect ratio, taper, and section
thickne; naca-rm-l7l01; Apr 1948
- Warren a. Tucker; Notes on geared
tabs at supersonic speeds; naca-rm-l7l04; Jul 1948
- Paul E. Purser; Effect of a
pilot's canopy on the drag of an NACA RM-2 drag research model in flight at
transonic and supersonic speeds; naca-rm-l7l22; Apr 1948
- Axel T. Mattson, Donald
L. Loving; Force, static
longitudinal stability, and control characteristics of a one-sixteenth-scale
model of the Bell XS-1 transonic research airplane at high Mach numbers;
naca-rm-l8a12; Jun 1948
- John G. Lowry, John A.
Axelson, Harold I. Johnson; Effects
of sweep on controls; naca-rm-l8a28c; Jun 1948
- John B. Wright; High-speed
wind-tunnel tests of a one-sixteenth-scale model of the D-558 research
airplane : D-588-1 speed-reduction brake and symmetrical-profile wing
characteristics; naca-rm-l8b06; Jun 1948
- Richard H. Sawyer, Fred
L. Daum; Measurement
through the speed of sound of static pressures on the rear of unswept and
sweptback circular cylinders and on the rear and sides of a wedge by the NACA
wing-flow method; naca-rm-l8b13; Jul 1948
- Marion O. McKinney,
Jr., Hubert M. Drake; Free-flight-tunnel
tests of a target-seeking glide-bomb model with flicker lateral control;
naca-rm-l8b20; Jul 1948
- Leroy Spearmen; Longitudinal
stability and control characteristics at transonic speeds of a semispan
airplane model having a 45 degree sweptback wing and tail as obtained by the
transonic-bump method; naca-rm-l8c11; Jun 1948
- Charles C. Smith, Jr.;
The effects
of fuel sloshing on the lateral stability of a free-flying airplane model;
naca-rm-l8c16; Jun 1948
- Sherman A. Clevenson,
Reginald R. Lundstrom, Ellwyn E. Angle; Flight
test of NACA FR-1-B, a low acceleration rocket-propelled vehicle for transonic
flutter research; naca-rm-l8c24; Jul 1948
- James C. Sivells,
William D. Conner; Preliminary
investigation at a Mach number of 1.9 and a Reynolds number of 2,200,000 of
three ailerons applicable to the Bell XS-2 airplane design; naca-rm-l8d02;
May 1948
- Carl A. Sandahl; Free-flight
investigation of the rolling effectiveness of several delta wing : aileron
configurations at transonic and supersonic speeds; naca-rm-l8d16; Aug
1948
- Howard J. Curfman, Jr.,
William N. Gardner; Theoretical
analysis of the motions of an aircraft stabilized in roll by a
displacement-response, flicker-type automatic pilot; naca-rm-l8d19; Jul
1948
- Sidney R. Alexander; Effect of
windshield shape of a pilot's canopy on the drag of an NACA RM-2 drag research
model in flight at transonic speeds; naca-rm-l8e04; Jul 1948
- H. Kurt Strass; Free-flight
investigation of the rolling effectiveness at high subsonic, transonic, and
supersonic speeds of leading-edge and trailing-edge ailerons in conjunction
with tapered and untapered plan forms; naca-rm-l8e10; Jul 1948
- Carl A. Sandahl; Free-flight
investigation at transonic and supersonic speeds of the rolling effectiveness
of a 42.7 degree sweptback wing having partial-span ailerons;
naca-rm-l8e25; Oct 1948
- Carl A. Sandahl; Free-flight
investigation at transonic and supersonic speeds of a wing-aileron
configuration simulating the D-558-2 airplane; naca-rm-l8e28; Jul
1948
- Donald C. Cheatham, Max
C. Kurbjun; Transonic drag
characteristics of a wing-body combination showing the effect of a large wing
fillet; naca-rm-l8f08; Sep 1948
- John P. Mayer; A
limit pressure coefficient and an estimation of limit forces on airfoils at
supersonic speeds; naca-rm-l8f23; Aug 1948
- Carl A. Sandahl; Free-flight
investigation at transonic and supersonic speeds of the rolling effectiveness
of a thin, unswept wing having partial-span ailerons; naca-rm-l8g20a; Oct
1948
- K. R. Czarnecki, C. F.
Schueller; Investigation
of interaction effects arising from side-wall boundary layers in supersonic
wind-tunnel tests of airfoils; naca-rm-l8g27; Nov 1948
- Antonio Ferri, Louis M.
Nucci; Theoretical and
experimental analysis of low-drag supersonic inlets having a circular cross
section and a central body at Mach numbers of 3.30, 2.75, and 2.45;
naca-rm-l8h13; Nov 1948
- Bernard Maggin, Robert
E. Shanks; Experimental
determination of the lateral stability of a glider towed by a single towline
and correlation with an approximate theory; naca-rm-l8h23; Nov 1948
- Lowell E. Hasel, Donald
E. Coletti; Investigation
of two pitot-static tubes at supersonic speeds; naca-rm-l8i02; Nov
1948
- Reginald R. Lundstrom,
WIlliam T. Lauten, Jr., Ellwyn E. Angle; Transonic-flutter
investigation of wings attached to two low-acceleration rocket-propelled
vehicles; naca-rm-l8i30; Nov 1948
- Harold S. Johnson,
Robert F. Thompson; Investigation
of horn balances on a 45 degree sweptback horizontal tail surface at high
subsonic speeds; naca-rm-l8j01; Dec 1948
- H. W. Russell, L. R.
Jackson, H. J. Grover, W. W. Beaver; Fatigue
strength and related characteristics of aircraft joints II : fatigue
characteristics of sheet and riveted joints of 0.040-inch 24S-T, 75S-T, and
R303-T275 aluminum alloys; naca-tn-1485; Feb 1948
- Max A. Heaslet, Harvard
Lomax; The
use of source-sink and doublet distributions extended to the solution of
boundary value problems in supersonic flow; naca-tn-1515; Jan 1948
- Arthur L. Jones,
Alberta Alkene; The
damping due to roll of triangular, trapezoidal, and related plan forms in
supersonic flow; naca-tn-1548;
- George J. Heimerl; Methods of
constructing charts for adjusting test results for the compressive strength of
plates for differences in material properties; naca-tn-1564; Apr
1948
- Roger A. Anderson, John
C. Houbolt; Effect of shear
lag on bending vibration of box beams; naca-tn-1583; May 1948
- Harry L. Runyan, John
L. Sewall; Experimental
investigation of the effects of concentrated weights on flutter;
naca-tn-1594; Jun 1948
- W. Perl, H. E. Moses;
Velocity
distribution on symmetrical airfoils in closed tunnels by conformal
mapping; naca-tn-1642; Jun 1948
- Warren A. Tucker; Characteristics
of thin triangular wings with triangular-tip control surfaces at supersonic
speeds with Mach lines behind the leading edge; naca-tn-1600; May
1948
- Warren A. Tucker; Characteristics
of thin triangular wings with constant-chord full-span control surfaces at
supersonic speeds; naca-tn-1601; Jul 1948
- R. S. Genco, I. L.
Drell; Knock-limited
performance of several branched paraffins and olefins; naca-tn-1616; Jun
1948
- Stephen H. Maslen; Method for
calculation of pressure distributions on thin conical bodies of arbitrary
cross section in supersonic stream; naca-tn-1659; Jul 1948
- Warren A. Tucker,
Robert L. Nelson; Characteristics
of thin triangular wings with constant-chord partial-span control surfaces at
supersonic speeds; naca-tn-1660; Jul 1948
- Clarence B. Cohen, John
C. Evvard; Graphical
method of obtaining theoretical lift distributions on thin wings at supersonic
speeds; naca-tn-1676; Aug 1948
- Wilber B. Huston,
Calvin N. Warfield, Anna Z. Stone; A
study of skin temperatures of conical bodies in supersonic flight;
naca-rm-l7j21; Jan 1948
- Vearl N. Huff, Clyde S.
Calvert; Charts for the
computation of equilibrium composition of chemical reactions in the
carbon-hydrogen-oxygen-nitrogen system at temperatures from 2000 to 5000
K; naca-tn-1653; Jul 1948
- Franklin W. Diederich,
Bernard Budiansky; Divergence
of swept wings; naca-tn-1680; Aug 1948
- Nancy E. Wall; Chordwise
pressure distributions on a 12-foot-span wing of NACA 66-series airfoil
sections up to a mach number of 0.60; naca-tn-1696; Oct 1948
- Reece V. Hensley; Mollier
diagrams for air saturated with water vapor at low temperatures;
naca-tn-1715; Sep 1948
- Cleary, Joseph W Gray,
Lyle J; High-speed
wind-tunnel tests of a model pursuit airplane and correlation with flight-test
results; naca-rm-a7i16; January 21, 1948
- Davis, Wallace F
Goldstein, David L; Experimental
investigation at supersonic speeds of twin-scoop duct inlets of equal area I :
an inlet enclosing 61.5 percent of the maximum circumference of the
forebody; naca-rm-a7j27; January 21, 1948
- Axelson, John A; A summary and
analysis of wind-tunnel data on the lift and hinge-moment characteristics of
control surfaces up to a Mach number of 0.90; naca-rm-a7l02; April 30,
1948
- Hopkins, Edward J; A wind-tunnel
investigation at low speed of various lateral controls on a 45 degree
swept-back wing; naca-rm-a7l16; April 09, 1948
- Olson, Robert N
Lawrence, Leslie F; High-speed
wind-tunnel tests of a 1/78-scale model of the Lockheed YP-80A airplane;
naca-rm-a7l24; May 28, 1948
- Perkins, Edward W; Experimental
investigation of the effects of support interference on the drag of bodies of
revolution at a Mach number of 1.5; naca-rm-a8b05; May 07, 1948
- Goldstein, David L
Davis, Wallace F; Experimental
investigation at supersonic speeds of twin-scoop duct inlets of equal area II
: effects of slots upon an inlet enclosing 61.5 percent of the maximum
circumference of the forebody; naca-rm-a8c11; June 09, 1948
- Johnson, Ben H , Jr; Investigation
of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel I :
characteristics of a plain wing; naca-rm-a8d07; June 02, 1948
- Davis, Wallace F
Edwards, Sherman S; Experimental
investigation at supersonic speeds of twin-scoop duct inlets of equal area III
: inlet enclosing 37.2 percent of the maximum circumference of the
forebody; naca-rm-a8e04; July 22, 1948
- Vincenti, Walter G Van
Dyke, Milton D Matteson, Frederick H; Investigation
of wing characteristics at a Mach number of 1.53 II : swept wings of taper
ratio 0.5; naca-rm-a8e05; June 28, 1948
- Nielsen, Jack N
Matteson, Frederick H Vincenti, Walter G; Investigation
of wing characteristics at a Mach number of 1.53 III : unswept wings of
differing aspect ratio and taper ratio; naca-rm-a8e06; June 21,
1948
- Allen, H Julian; The asymmetric
adjustable supersonic nozzle for wind-tunnel application; naca-rm-a8e17;
July 23, 1948
- Anderson, Joseph L
Krumm, Walter J; High-speed
aerodynamic characteristics of a lateral-control model I : NACA 0012-64
section with 20-percent-chord plain aileron and 0 degree and 45 degrees
sweepback; naca-rm-a8h12; September 27, 1948
- Johnson, Ben H , Jr
Demele, Fred A; Investigation
of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel III
: the effectiveness of a constant-chord aileron; naca-rm-a8i17; November
19, 1948
- Woodward, William H
Bobrowsky, A R; Preliminary
investigation of a ceramic lining for a combustion chamber for gas-turbine
use; naca-rm-e7h20; April 12, 1948
- Ordin, Paul M Miller,
Riley O Diehl, John M; Preliminary
investigation of hydrazine as a rocket fuel; naca-rm-e7h21; May 24,
1948
- Luidens, Roger W
Hunczak, Henry; Preliminary
investigation of cone-type diffusers designed for minimum spillage at
inlet; naca-rm-e7k19; May 03, 1948
- Sterbentz, W H
Perchonok, E Wilcox, F A; Investigation
of effects of several fuel-injection locations on operational performance of a
20-inch ram jet; naca-rm-e7l02; June 08, 1948
- Kinghorn, George F
Disher, John H; Free-flight
investigation of 16-inch diameter supersonic ram-jet unit; naca-rm-e8a26;
May 28, 1948
- Sloop, J L Kinney,
George R; Internal-film
cooling of rocket nozzles; naca-rm-e8a29a; June 08, 1948
- Miller, Riley O Ordin,
Paul M; Theoretical
performance of some rocket propellants containing hydrogen, nitrogen, and
oxygen; naca-rm-e8a30; May 26, 1948
- Pinkel, I Irving; Equations for
the design of two-dimensional supersonic nozzles; naca-rm-e8b02; June 21,
1948
- Haddock, Gordon W
Childs, J Howard; Preliminary
investigation of combustion in flowing gas with various turbulence
promoters; naca-rm-e8c02; June 07, 1948
- Perchonok, Eugene
Wishnek, George Wilcox, Fred A; Some
effects of gutter flame-holder dimensions on combustion-chamber performance of
20-inch ram jet; naca-rm-e8c22; July 30, 1948
- Messing, Wesley E
Black, Dugald O; Effect
of variation in fuel pressure on combustion performance of rectangular ram
jet; naca-rm-e8i28; November 24, 1948
- Evvard, John C Wyatt,
Demarquis D; Investigation
of a variable Mach number supersonic tunnel with nonintersecting
characteristics; naca-rm-e8j13; November 15, 1948
- Olsen, H Lowell Miller,
Cearcy D; The
interdependence of various types of autoignition and knock;
naca-report-912; 1948
- Locke, F W S (Bureau of
Aeronautics, Navy Department); A
graphical method for interpolation of specific flying boats from collapsed
results of general tests of flying-boat-hull models; naca-tn-1259;
1948
- Turner, L Richard
Addie, Albert N Zimmerman, Richard H; Charts
for the analysis of one-dimensional steady compressible flow;
naca-tn-1419; 1948
- Wang, Chi-Teh
(Massachusetts Institute of Technology); Nonlinear
large-deflection boundary-value problems of rectangular plates;
naca-tn-1425; March 1948
- Houbolt, John C
Anderson, Roger A; Calculation
of uncoupled modes and frequencies in bending or torsion of nonuniform
beams; naca-tn-1522; February 1948
- Moore, R L (Aluminum
Company of America); Bearing
strength of some aluminum-alloy sand castings; naca-tn-1523; August
1948
- Parkinson, John B; Take-off
performance of light twin-float sea- planes; naca-tn-1524; February
1948
- Zender, George Libove,
Charles; Stress and
distortion measurements in a 45 degree swept box beam subjected to bending and
to torsion; naca-tn-1525; March 1948
- Pierce, Harold B; Tests of a 45
degree sweptback-wing model in the Langley gust tunnel; naca-tn-1528;
February 1948
- Handelman, G H (Brown
University) Prager, William (Brown University); Plastic
buckling of a rectangular plate under edge thrusts; naca-tn-1530; August
1948
- Freeman, J W
(University of Michigan) Reynolds, E E (University of Michigan) White, A E
(University of Michigan); A
metallurgical investigation of two contour forged gas-turbine discs of 19-9DL
alloy; naca-tn-1532; September 1948
- Reynolds, E E
(University of Michigan) Freeman, J W (University of Michigan) White, A E
(University of Michigan); A
metallurgical investigation of two large discs of CSA alloy; naca-tn-1533;
September 1948
- Marin, Joseph
(Pennsylvania State College) Faupel, J H (Pennsylvania State College) Dutton,
V L (Pennsylvania State College); Biaxial
plastic stress-strain relations for 24S-T aluminum alloy; naca-tn-1536;
May 1948
- Anderson, Robert J
Ritter, William K Parsons, Shirley R; Apparent
effect of inlet temperature on adiabatic efficiency of centrifugal
compressors; naca-tn-1537; February 1948
- Otto, Edward W; Analysis of
accuracy of gas-filled bellows for sensing gas density; naca-tn-1538;
February 1948
- Sadoff, Melvin
Clousing, Lawrence A; Measurements
of the pressure distribution on the horizontal-tail surface of a typical
propeller-driven pursuit airplane in flight III : tail loads in abrupt pull-up
push-down maneuvers; naca-tn-1539; February 1948
- Gray, W H Davidson, R
E; The
effect of tip modification and thermal de-icing air flow on propeller
performance as determined from wind-tunnel tests; naca-tn-1540; February
1948
- Lovell, Powell M , Jr;
The effect
of wing bending deflection on the rolling moment due to sideslip;
naca-tn-1541; February 1948
- Gessow, Alfred; Effect of
rotor-blade twist and plan-form taper on helicopter hovering performance;
naca-tn-1542; February 1948
- Margolis, Kenneth; Effect of
chordwise location of maximum thickness on the supersonic wave drag of
sweptback wings; naca-tn-1543; March 1948
- Levin, L Ross; Strength
of thin-web beams with transverse load applied at an intermediate upright;
naca-tn-1544; February 1948
- Cahill, Jones F Racisz,
Stanley F; Wind-tunnel
investigation of seven thin NACA airfoil sections to determine optimum
double-slotted-flap configurations; naca-tn-1545; April 1948
- Lindsey, W F Stevenson,
D B Daley, Bernard N; Aerodynamics
characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and
0.8; naca-tn-1546; September 1948
- Garrison, Charlie C
Clement, Eugene P; Tank
tests of three types of afterbodies on a flying-boat model with basic hull
length-beam ratio of 10.0; naca-tn-1547; March 1948
- Moeckel, W E; Effect
of yaw at supersonic speeds on theoretical aerodynamic coefficients of thin
pointed wings with several types of trailing edge; naca-tn-1549; March
1948
- Lamb, J J (National
Bureau of Standards) Boswell, Isabelle (National Bureau of Standards) Axilrod,
B M (National Bureau of Standards); Tensile
and compressive properties of laminated plastics at high and low
temperatures; naca-tn-1550; July 1948
- Thomsen, E G
(University of California) Lotze, I (University of California) Dorn, J E
(University of California); Fracture
strength of 75S-T aluminum alloy under combined stress; naca-tn-1551; July
1948
- Hickman, William A Dow,
Norris F; Compressive
strength of 24S-T aluminum-alloy flat panels with longitudinal formed
hat-section stiffeners having four ratios of stiffener thickness to skin
thickness; naca-tn-1553; March 1948
- Frick, Charles W; Application of
the linearized theory of supersonic flow to the estimation of control-surface
characteristics; naca-tn-1554; March 1948
- Stowell, Elbridge Z; A unified
theory of plastic buckling of columns and plates; naca-tn-1556; April
1948
- Budiansky, Bernard
Seide, Paul; Compressive
buckling of simply supported plates with transverse stiffeners;
naca-tn-1557; April 1948
- Voldrich, C B (Battelle
Memorial Institute) ARMSTRONG E T (Battelle Memorial Institute); Effect
of variables in welding technique on the strength of direct-current
metal-arc-welded joints in aircraft steel II : repeated-stress tests of joints
in SAE 4130 seamless steel tubing; naca-tn-1262; April 1948
- Heaslet, Max A Lomax,
Harvard; The
use of source-sink and doublet distributions extended to the solution of
boundary-value problems in supersonic flow; naca-report-900; 1948
- Sinnette, John T , Jr;
Analysis of
effect of basic design variables on subsonic axial-flow-compressor
performance; naca-report-901; 1948
- Jones, Robert T; Subsonic flow
over thin oblique airfoils at zero lift; naca-report-902; 1948
- Loftin, Laurence K ,
Jr; Theoretical and
experimental data for a number of NACA 6A-series airfoil sections;
naca-report-903; 1948
- Barnett, Henry C; Estimation of
F-3 and F-4 knock-limited performance ratings for ternary and quaternary
blends containing triptane or other high-antiknock aviation-fuel blending
agents; naca-report-904; 1948
- Dingeldein, Richard C
Schaefer, Raymond F; Full-scale
investigation of aerodynamic characteristics of a typical single-rotor
helicopter in forward flight; naca-report-905; 1948
- Millenson, M B Manson,
S S; Determination
of stresses in gas-turbine disks subjected to plastic flow and creep;
naca-report-906; 1948
- Pinkel, I Irving; Equations for
the design of two-dimensional supersonic nozzles; naca-report-907;
1948
- Ribner, Herbert S
Malvestuto, Frank S , Jr; Stability
derivatives of triangular wings at supersonic speeds; naca-report-908;
1948
- Schubauer, G B
Skramstad, H K; Laminar-boundary-layer
oscillations and transition on a flat plate; naca-report-909; 1948
- Quinn, John H , Jr; Summary of drag
characteristics of practical-construction wing sections; naca-report-910;
1948
- Swanson, Robert S
Crandall, Stewart M; Lifting-surface-theory
aspect-ratio corrections to the lift and hinge-moment parameters for full-span
elevators on horizontal tail surfaces; naca-report-911; 1948
- Bollinger, Lowell M
Williams, David T; Experiments
on stability of Bunsen-burner flames for turbulent flow; naca-report-913;
1948
- Simpkinson, Scott H
Eatherton, Laurel J Millenson, Morton B; Effect
of centrifugal force on the elastic curve of a vibrating cantilever beam;
naca-report-914; 1948
- Sinnette, John T Voss,
William J; Extension of
useful operating range of axial-flow compressors by use of adjustable Stator
blades; naca-report-915; 1948
- Nissen, James M
Gadebero, Burnett L Hamilton, William T; Correlation
of the drag characteristics of a typical pursuit airplane obtained from
high-speed wind-tunnel and flight tests; naca-report-916; 1948
- Scherrer, Richard; The effects of
aerodynamic heating and heat transfer on the surface temperature of a body of
revolution in steady supersonic flight; naca-report-917; 1948
- Imlay, Frederick H; Theoretical
motions of hydrofoil systems; naca-report-918; 1948
- Huston, Wilber B; Accuracy of
airspeed measurements and flight calibration procedures; naca-report-919;
1948
- Baals, Donald D Smith,
Norman F Wright, John B; The
development and application of high-critical-speed nose inlets;
naca-report-920; 1948
- Deyoung, John Harper,
Charles W; Theoretical
symmetric span loading at subsonic speeds for wings having arbitrary plan
form; naca-report-921; 1948
- Brown, Clinton E Adams,
Mac C; Damping in
pitch and roll of triangular wings at supersonic speeds; naca-report-892;
1948
- Perl, W Moses, H E; Velocity
distributions on two-dimensional wing-duct inlets by conformal mapping;
naca-report-893; 1948
- Kaplan, Carl; On
similarity rules for transonic flows; naca-report-894; 1948
- Sanders, J C Schramm, W
B; Analysis
of variation of piston temperature with piston dimensions and undercrown
cooling; naca-report-895; 1948
- Cesaro, Richard S Matz,
Norman; Pressure-sensitive
system for gas-temperature control; naca-report-896; 1948
- Osterstrom, Gordon E;
Knocking
combustion observed in a spark-ignition engine with simultaneous direct and
Schlieren high-speed motion pictures and pressure records;
naca-report-897; 1948
- Stowell, Elbridge Z; A unified
theory of plastic buckling of columns and plates; naca-report-898;
1948
- Libove, Charles
Batdorf, S B; A
general small-deflection theory for flat sandwich plates; naca-report-899;
1948
- Boelter, L M K
(University of California) Dempster, E R (University of California) Bromberg,
R (University of California) Gier, J T (University of California); An
investigation of aircraft heaters XXVI : development of a sensitive
plated-type thermopile for measuring radiation; naca-tn-1450; July
1948
- Hoff, N J (Polytechnic
Institute of Brooklyn) Boley, Bruno A (Polytechnic Institute of Brooklyn)
Viggiano, Louis R (Polytechnic Institute of Brooklyn); Stresses
in and general instability of monocoque cylinders with cutouts IV : pure
bending tests of cylinders with side cutout; naca-tn-1264; February
1948
- Norris, C B (Forest
Products Laboratory) Voss, A W (Forest Products Laboratory); An
improved photoelastic method for determining plane stresses; naca-tn-1410;
1948
- Reissner, H
(Polytechnic Institute of Brooklyn) Morduchow, M (Polytechnic Institute of
Brooklyn); A
theoretical study of the dynamic properties of helicopter-blade systems;
naca-tn-1430; November 1948
- Hoff, N J (Polytechnic
Institute of Brooklyn) Klein, Bertram (Polytechnic Institute of Brooklyn); Stresses in and
general instability of monocoque cylinders with cutouts V : calculation of the
stresses in cylinders with side cutout; naca-tn-1435; 1948
- Hoff, N J (Polytechnic
Institute of Brooklyn) Klein, Bertram (Polytechnic Institute of Brooklyn)
Boley, Bruno A (Polytechnic Institute of Brooklyn); Stresses
in and general instability of monocoque cylinders with cutouts VI :
calculation of the buckling load of cylinders with side cutout subjected to
pure bending; naca-tn-1436; March 1948
- Crouse, W A (National
Bureau of Standards) Caudill, D C (National Bureau of Standards) Reinhart, F W
(National Bureau of Standards); Effect
of simulated service conditions on plastics during accelerated and 2-year
weathering tests; naca-tn-1438; May 1948
- Borsari, Palamede
(Massachusetts Institute of Technology) Yu, Ai-Ting (Massachusetts Institute
of Technology); Shear
lag in a plywood sheet-stringer combination used for the chord member of a box
beam; naca-tn-1443; March 1948
- Hodge, Webster
(Battelle Memorial Institute) Eastwood, L W (Battelle Memorial Institute)
Lorig, C H (Battelle Memorial Institute) Cross, H C (Battelle Memorial
Institute); Development of
cast aluminum alloys for elevated-temperature service; naca-tn-1444;
1948
- Boelter, L M K
(University of California) Young, G (University of California) Iversen, H W
(University of California); An
investigation of aircraft heaters XXVII : distribution of heat-transfer rate
in the entrance section of a circular tube; naca-tn-1451; July 1948
- Boelter, L M K
(University of California) Romie, F E (University of California) Guibert, A G
(University of California) Miller, M A (University of California); An
investigation of aircraft heaters XXVIII : equations for steady-state
temperature distribution caused by thermal sources in flat plates applied to
calculation of thermocouple errors, heat-meter corrections, and heat transfer
by pin-fin plates; naca-tn-1452; August 1948
- Boelter, L M K
(University of California) Grossman, L M (University of California)
Martinelli, R C (University of California) Morrin, E H (University of
California); An
investigation of aircraft heaters XXIX : comparison of several methods of
calculating heat losses from airfoils; naca-tn-1453; October 1948
- Campbell, William R
(National Bureau of Standards); Performance
tests of wire strain gages VI : effect of temperature on calibration factor
and gage resistance; naca-tn-1456; 1948
- Gwathmey, Allan T
(University of Virginia) Leidheiser, Henry (University of Virginia) Smith, G
Pedro (University of Virginia); Influence
of crystal plane and surrounding atmosphere on chemical activities of single
crystals of metals; naca-tn-1460; June 1948
- Gwathmey, Allan T
(University of Virginia) Leidheiser, Henry (University of Virginia) Smith, G
Pedro (University of Virginia); Influence
of crystal plane and surrounding atmosphere on some types of friction and wear
between metals; naca-tn-1461; June 1948
- Wang, Chi-Teh (Brown
University); Bending of
rectangular plates with large deflections; naca-tn-1462; April 1948
- Howell, F M (Aluminum
Company of America) Stickley, G W (Aluminum Company of America) Lyst, J O
(Aluminum Company of America); Effects
of surface finish, of certain defects, and of repair of defects by welding on
fatigue strength of 355-T6 sand-castings and effects of prior fatigue
stressing on tensile properties; naca-tn-1464; April 1948
- Leary, W A
(Massachusetts Institute of Technology) Taylor, E S (Massachusetts Institute
of Technology) Taylor, C F (Massachusetts Institute of Technology); The
effect of fuel composition, compression pressure, and fuel-air ratio on the
compression-ignition characteristics of several fuels; naca-tn-1470; March
1948
- Smith, C B (Forest
Products Laboratory) Voss, A W (Forest Products Laboratory); Stress
distribution in a beam of orthotropic material subjected to a concentrated
load; naca-tn-1486; March 1948
- Colburn, A P
(University of Delaware) Gazley, Carl, Jr (University of Delaware) Schoenborn,
E M (University of Delaware) Sutton, C S (University of Delaware); Effect
of local boiling and air entrainment on temperatures of liquid-cooled
cylinders; naca-tn-1498; March 1948
- Hoff, N J (Polytechnic
Institute of Brooklyn) Boley, Bruno A (Polytechnic Institute of Brooklyn)
Nardo, S V (Polytechnic Institute of Brooklyn); The
inward bulge type buckling of monocoque cylinders IV : experimental
investigation of cylinders subjected to pure bending; naca-tn-1499;
September 1948
- Kaufman, Samuel J
Boman, David S; Comparison
of computed performance of composite power plants using 18-cylinder aircraft
engines with 62 degrees and 40 degrees valve overlap; naca-tn-1500;
1948
- Prager, W (Brown
University); On the
interpretation of combined torsion and tension tests of thin-wall tubes;
naca-tn-1501; 1948
- Moore, R L (Aluminum
Company of America); Bearing
tests of 14S sheet and plate; naca-tn-1502; August 1948
- Moore, R L (Aluminum
Company of America); Bearing
strengths of some aluminum-alloy rolled and extruded sections;
naca-tn-1503; September 1948
- Lomax, Harvard; Sideslip angles
and vertical-tail loads developed by periodic control deflections;
naca-tn-1504; 1948
- Jones, Arthur L Sluder,
Loma; An
application of Falkner's surface-loading method to predictions of hinge-moment
parameters for swept-back wings; naca-tn-1506; February 1948
- (Author(s) Not
Available); Symbols for
combustion research; naca-tn-1507; June 1948
- Valerino, Michael F
Kaufman, Samuel J; Cylinder-temperature
and cooling-air-pressure instrumentation for air-cooled-engine cooling
investigations; naca-tn-1509; 1948
- Sjoberg, S A Reeder, J
P; Flight
measurements of the lateral and directional stability and control
characteristics of an airplane having a 35 degree sweptback wing
40-percent-span slots and a comparison with wind-tunnel data;
naca-tn-1511; 1948
- Miller, James A
(National Bureau of Standards); Stress-strain
and elongation graphs for Alclad aluminum-alloy 24S-T sheet; naca-tn-1512;
May 1948
- Miller, James A
(National Bureau of Standards); Stress-strain
and elongation graphs for Alclad aluminum-alloy 24S-T81 sheet;
naca-tn-1513; May 1948
- Langdon, Howard H
(State College of Washington) Fried, Bernard (State College of Washington); Fatigue of
gusseted joints; naca-tn-1514; September 1948
- Milwitzky, Benjamin; A generalized
theoretical and experimental investigation of the motions and hydrodynamic
loads experienced by V-bottom seaplanes during step-landing impacts;
naca-tn-1516; February 1948
- Spearman, M Leroy; Wind-tunnel
investigation of an NACA 0009 airfoil with 0.25-and 0.50-airfoil-chord plain
flaps tested independently and in combination; naca-tn-1517; March
1948
- Dow, Norris F Hickman,
William A; Structural
evaluation of an extruded magnesium-alloy T-stiffened panel; naca-tn-1518;
February 1948
- Budiansky, Bernard
Seide, Paul Weinberger, Robert A; The
buckling of a column on equally spaced deflectional and rotational
springs; naca-tn-1519; March 1948
- Lewis, James P; De-icing
effectiveness of external electric heaters for propeller blades;
naca-tn-1520; February 1948
- Migotsky, Eugene; Full-scale
investigation of the blade motion of the PV-2 helicopter rotor;
naca-tn-1521; March 1948
- Norris, C B (Forest
Products Laboratory) Mackin, G E (Forest Products Laboratory); An
investigation of mechanical properties of honeycomb structures made of
resin-impregnated paper; naca-tn-1529; May 1948
- Budiansky, Bernard Hu,
Pai C Connor, Robert W; Notes
on the Lagrangian multiplier method in elastic-stability analysis;
naca-tn-1558; May 1948
- Budiansky, Bernard
Connor, Robert W; Buckling
stresses of clamped rectangular flat plates in shear; naca-tn-1559; May
1948
- Johnson, Daniel P
(National Bureau of Standards); Calibration
of altimeters under pressure conditions simulating dives and climbs;
naca-tn-1562; March 1948
- Benscoter, Stanley U;
Effect of
partial wing lift in seaplane landing impact; naca-tn-1563; April
1948
- Brown, Clinton E Adams,
Mac C; Damping in
pitch and roll of triangular wings at supersonic speeds; naca-tn-1566;
April 1948
- Manson, S V; Simulated-altitude
investigations of performance of tubular aircraft oil coolers;
naca-tn-1567; April 1948
- Gringorten, I I Press,
H; A
meteorological measure of maximum gust velocities in clouds; naca-tn-1569;
April 1948
- Carter, Arthur W Haar,
Marvin I; Hydrodynamic
qualities of a hypothetical flying boat with a low-drag hull having a
length-beam ratio of 15; naca-tn-1570; April 1948
- Ribner, Herbert S
Malvestuto, Frank S , Jr; Stability
derivatives of triangular wings at supersonic speeds; naca-tn-1572; May
1948
- Brewer, Jack D
Polhamus, Josephine F; Wind-tunnel
investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and
0.50- airfoil chord plain sealed flaps; naca-tn-1574; April 1948
- Neihouse, Anshal I; The effect of
variations in moments of inertia on spin and recovery characteristics of a
single- engine low-wing monoplane with various tail arrangements, including a
twin tail; naca-tn-1575; May 1948
- Fullmer, Felicien F; Wind-tunnel
investigation of a systematic series of modifications to a flying-boat
hull; naca-tn-1576; May 1948
- Von Doenhoff, Albert E;
Note on
similarity conditions for flows with heat transfer; naca-tn-1577; April
1948
- Racisz, Stanley F
Cahill, Jones F; Wing-tunnel
investigation of effects of forward movements of transition on section
characteristics of a low-drag airfoil with a 0.24-chord sealed plain
aileron; naca-tn-1582; May 1948
- Stowell, Elbridge Z
Houbolt, John C Batdord, S B; An
evaluation of some approximate methods of computing landing stresses in
aircraft; naca-tn-1584; May 1948
- Evvard, John C; Theoretical
distribution of lift on thin wings at supersonic speeds : (an extension);
naca-tn-1585; May 1948
- Visconti, Fioravante;
Investigation
of an approximately 0.178-chord-thick NACA 6-series-type airfoil section
equipped with sealed internally balanced 0.20-chord ailerons and with a
0.05-chord tab; naca-tn-1590; May 1948
- Loftin, Laurence K , Jr
Cohen, Kenneth S; Aerodynamic
characteristics of a number of modified NACA four-digit-series airfoil
sections; naca-tn-1591; June 1948
- Burcher, Marie A; Compressible
flow tables for air; naca-tn-1592; August 1948
- Mclellan, Charles H
Cangelosi, John I; Effects
of nacelle position on wing-nacelle interference; naca-tn-1593; June
1948
- Gustafson, F B Gessow,
Alfred; Analysis of
flight-performance measurements on a twisted, plywood-covered helicopter rotor
in various flight conditions; naca-tn-1595; June 1948
- Brueggeman, W C
(National Bureau of Standards) Mayer, M JR (National Bureau of Standards); Axial fatigue
tests at zero mean stress of 24S-T and 75S-T aluminum-alloy strips with a
central circular hole; naca-tn-1611; 1948
- Boman, David S Kaufman,
Samuel J; Effect of
reducing valve overlap on engine and compound-power-plant performance;
naca-tn-1612; June 1948
- Ivey, H Reese Klunker,
E Bernard Bowen, Edward N; A
method for determining the aerodynamic characteristics of two-and
three-dimensional shapes at hypersonic speeds; naca-tn-1613; July
1948
- Callaghan, Edmund E
Euggeri, Robert S; Investigation
of the penetration on an air jet directed perpendicularly to an air
stream; naca-tn-1615; June 1948
- Lord, Albert M
Heinicke, Orville H Stricker, Edward G; Effect
of exhaust pressure on knock-limited performance of an air-cooled
aircraft-engine cylinder; naca-tn-1617; June 1948
- Dittrich, Ralph T; Effects of
fuel-nozzle carbon deposition on combustion efficiency of single tubular-type,
reverse-flow turbojet combustor at simulated altitude conditions;
naca-tn-1618; June 1948
- Heaslet, Max A Lomax,
Harvard; The
calculation of downwash behind supersonic wings with an application to
triangular plan forms; naca-tn-1620; June 1948
- Heaslet, Max A Lomax,
Harvard; Two-dimensional
unsteady lift problems in supersonic flight; naca-tn-1621; June
1948
- Malkus, Willem V R
Bishop, Richard H Briggs, Robert O; Analysis
and preliminary design of an optical instrument for the measurement of drop
size and free-water content of clouds; naca-tn-1622; June 1948
- Nitzberg, Gerald E
Crandall, Stewart; Some
fundamental similarities between boundary-layer flow at transonic and low
speeds; naca-tn-1623; June 1948
- Phillips, William H; Effect of
steady rolling on longitudinal and directional stability; naca-tn-1627;
June 1948
- Tolefson, H B; An
analysis of the variation with altitude of effective gust velocity in
convective-type clouds; naca-tn-1628; June 1948
- Milwitzky, Benjamin; A generalized
theoretical investigation of the hydrodynamic pitching moments experienced by
V-Bottom seaplanes during step-landing impacts and comparisons with
experiment; naca-tn-1630; June 1948
- Pierce, Harold B
Trauring, Mitchell; Gust-tunnel
tests to determine influence of airfoil section characteristics on gust-load
factors; naca-tn-1632; July 1948
- Loftin, Laurence K
Cohen, Kenneth S; An
evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil
section with a special mean-camber line designed to produce a high critical
Mach number; naca-tn-1633; July 1948
- Sandlin, Charles W; Strength tests
of shear webs with uprights not connected to the flanges; naca-tn-1635;
June 1948
- Tucker, M Rousso, M D;
Experimental
investigation of the jet-boundary constriction correction for a model spanning
a closed circular tunnel; naca-tn-1638; June 1948
- Davis, Don D , Jr
Sweberg, Harold H; Investigation
of some factors affecting comparisons of wind-tunnel and flight measurements
of maximum lift coefficients for a fighter-type airplane; naca-tn-1639;
June 1948
- Dow, Norris F Hickman,
William A; Direct-reading
design charts for 75S-T aluminum-alloy flat compression panels having
longitudinal straight-web Y-section stiffeners; naca-tn-1640; August
1948
- Busch, Arthur M
Cleaves, Alden P Hibbard, Robert R; A
method for determination of aromatics in 150 degree to 300 degree C fractions
of crude petroleum by measurement of aniline-point rise; naca-tn-1641;
June 1948
- Haar, Marvin I; Tank tests of a
1/10-size model of a hypothetical flying boat with a hull length-beam ratio of
9.0; naca-tn-1648; July 1948
- Wick, Bradford H; Chordwise and
spanwise loadings measured at low speed on a triangular wing having an aspect
ratio of two and an NACA 0012 airfoil section; naca-tn-1650; 1948
- Campbell, William R
(National Bureau of Standards); Test
of six types of Bakelite-bonded wire strain gages; naca-tn-1656; July
1948
- Daley, Bernard N
Humphreys, Milton D; Effects
of compressibility on the flow past thick airfoil sections; naca-tn-1657;
July 1948
- Batdorf, S B
Schildcrout, Murry; Critical
axial-compressive stress of a curved rectangular panel with a central
chordwise stiffener; naca-tn-1661; July 1948
- Spreiter, John R; Aerodynamic
properties of slender wing-body combinations at subsonic, transonic, and
supersonic speeds; naca-tn-1662; July 1948
- Huber, Paul W
Kantrowitz, Arthur; A
device for measuring sonic velocity and compressor Mach number;
naca-tn-1664; July 1948
- Stack, John Lindsey, W
F; Characteristics
of low-aspect ratio wings at supercritical Mach numbers; naca-tn-1665;
August 1948
- Gessow, Alfred; Flight
investigation of effects of rotor-blade twist on helicopter performance in the
high-speed and vertical-autorotative-descent conditions; naca-tn-1666;
August 1948
- Queijo, M J Jaquet,
Byron M; Investigation
of effects of geometric dihedral on low-speed static stability and yawing
characteristics of an untapered 45 degree sweptback-wing model of aspect ratio
2.61; naca-tn-1668; September 1948
- Phillips, William
Hewitt; Appreciation
and prediction of flying qualities; naca-tn-1670; August 1948
- Letko, William Cowan,
John W; Effect of taper
ratio on low-speed static and yawing stability derivatives of 45 degree
sweptback wings with aspect ratio of 2.61; naca-tn-1671; July 1948
- Margolis, Kenneth; Supersonic wave
drag of nonlifting sweptback tapered wings with Mach lines behind the line of
maximum thickness; naca-tn-1672; August 1948
- Lowry, John G
Schneiter, Leslie E; Estimation
of effectiveness of flap-type controls on sweptback wings; naca-tn-1674;
August 1948
- Tendeland, Thorval
Schlaff, Bernard A; Temperature
gradients in the wing of a high-speed airplane during dives from high
altitudes; naca-tn-1675; July 1948
- Bollech, Thomas V; Experimental
and calculated characteristics of several high-aspect-ratio tapered wings
incorporating NACA 44-series, 230-series, and low-drag 64- series airfoil
sections; naca-tn-1677; September 1948
- Mirels, Harold; Theoretical
wave drag and lift of thin supersonic ring airfoils; naca-tn-1678; August
1948
- Sjoberg, S A Reeder, J
P; Flight
measurements of the longitudinal stability, stalling, and lift characteristics
of an airplane having a 35 degrees sweptback wing without slots and with
40-percent-span slots and a comparison with wind-tunnel data;
naca-tn-1679; August 1948
- Stalder, Jackson, R
Jukoff, David; Heat
transfer to bodies traveling at high speed in the upper atmosphere;
naca-tn-1682; August 1948
- Essig, Robert H
Bohanon, H R Gabriel, David S; Jet
diffuser for simulating ram-pressure and altitude conditions on a
turbojet-engine static test stand; naca-tn-1687; August 1948
- Hanson, Frederick H ,
Jr Mossman, Emmet A; Effect
of pressure recovery on the performance of a jet-propelled airplane;
naca-tn-1695; September 1948
- Goldstein, Arthur W
Alpert, Sumner Beede, William; Analysis
of performance of a jet engine from characteristics of components II :
interaction of components as determined from engine operation;
naca-tn-1701; September 1948
- Bollinger, Lowell M
Williams, David T; Effect
of Reynolds number in turbulent-flow range on flame speeds of Bunsen-burner
flames; naca-tn-1707; September 1948
- Hoff, N J (Polytechnic
Institute of Brooklyn) Libby, Paul A (Polytechnic Institute of Brooklyn); Recommendations
for numerical solution of reinforced-panel and fuselage-ring problems;
naca-tn-1786; December 1948
- Desmon, Leland G Doyle,
Ronald B; Calculated
performance of 12-cylinder liquid-cooled engine with exhaust-gas turbine
geared to crankshaft; naca-tn-1602; June 1948
- Povolny, John H Chelko,
Louis J; Cylinder-head
temperatures and coolant heat rejections of a multicylinder, liquid-cooled
engine of 1710-cubic-inch displacement; naca-tn-1606; June 1948
- Moses, Jason J
Kazberovich, Thomas I; Effect
of size and number of outlet pipes on design of collectors for rating and
testing axial-flow compressors; naca-tn-1607; June 1948
- Cleaves, Alden P
Carver, Mildred S Hibbard, Robert R; Quantitative
analysis of ternary mixtures of naphthalene, 1-methylnaphthalene, and
2-methylnaphthalene by ultraviolet spectrophotometry; naca-tn-1608; June
1948
- Reynolds, Thaine W
Ebersole, Earl R; Effect
of hydrocarbon type and chain length on uniform flame movement in quiescent
fuel-air mixtures; naca-tn-1609; June 1948
- (Author(s) Not
Available); A restricted
list of aircraft materials research projects; naca-rm-8c29; May 04,
1948
- (Author(s) Not
Available); Bibliography of
NACA and other reports on air inlets and internal flows; naca-rm-8j05;
October 11, 1948
- Leary, W A
(Massachusetts Institute of Technology) Taylor, E S (Massachusetts Institute
of Technology) Taylor, C F (Massachusetts Institute of Technology); A
rapid compression machine suitable for studying short ignition delays;
naca-tn-1332; February 1948
- Davis, Wallace F
Brajnikoff, George B Goldstein, David L Speigel, Joseph M; An
experimental investigation at supersonic speeds of annular duct inlets
situated in a region of appreciable boundary layer; naca-rm-a7g15;
September 1948
- Cleary, Joseph W Krumm,
Walter J; High-speed
aerodynamic characteristics of horn and overhang balances on a full-scale
elevator; naca-rm-a7h29; February 27, 1948
- Boddy, Lee E Morrill,
Charles P , Jr; The
high-speed aerodynamic effects of modifications to the wing and wing-fuselage
intersection of an airplane model with the wing swept back 35 degrees;
naca-rm-a7j02; February 18, 1948
- Boddy, Lee E Morrill,
Charles P , Jr; The
aerodynamic effects of rockets and fuel tanks mounted under the swept-back
wing of an airplane model; naca-rm-a7j03; April 23, 1948
- Axelson, John A Crown,
J Conrad; An
analysis of the effects of wing aspect ratio and tail location on static
longitudinal stability below the Mach number of lift divergence;
naca-rm-a7j13; January 09, 1948
- Anderson, Joseph L
Martin, Andrew; High-speed
aerodynamic characteristics of a model tail plane with modified NACA 65-010
sections and 0 degree and 45 degrees sweepback; naca-rm-a7j22; January 12,
1948
- Rose, Leonard M; Low-speed
investigation of a small triangular wing of aspect ratio 2.0 I : the effect of
combination with a body revolution and height above a ground plane;
naca-rm-a7k03; August 27, 1948
- Edwards, George G
Stephenson, Jack D; Tests
of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind
tunnel I : the effect of Reynolds number and Mach number on the aerodynamic
characteristics of the wing with flap undeflected; naca-rm-a7k05; January
22, 1948
- Dods, Jules B , Jr; Wind-tunnel
investigation of horizontal tails I : unswept and 35 degrees swept-back plan
forms of aspect ratio 3; naca-rm-a7k24; April 22, 1948
- Morrill, Charles P , Jr
Boddy, Lee E; High-speed
stability and control characteristics of a fighter airplane model with a
swept-back wing and tail; naca-rm-a7k28; April 14, 1948
- Tolhurst, William H ,
Jr; An
investigation of the downwash and wake behind large-scale swept and unswept
wings; naca-rm-a7l05; February 02, 1948
- Rose, Leonard M; Low-speed
investigation of a small triangular wing of aspect ratio 2.0 II : flaps on
flat-plate models; naca-rm-a7l11; August 09, 1948
- Stough, Carl J
Kauffman, William M; A
flight investigation and analysis of the lateral-oscillation characteristics
of an airplane; naca-rm-a7l31; June 03, 1948
- Messing, Wesley E
Black, Dugald O; Subsonic
flight investigation of rectangular ram jet over range of altitudes;
naca-rm-e7h26; January 19, 1948
- Kepple, William L; Determination
of aircraft antenna loads produced by natural icing conditions;
naca-rm-e7h26a; February 18, 1948
- Perchonok, Eugene
Sterbentz, William H Moore, Stanley H; Indirect
methods for obtaining ram-jet exhaust-gas temperature applied to fuel-metering
control; naca-rm-e7h27; January 14, 1948
- Brown, W Byron
Livingood, John N B; Cooling
of gas turbines VIII : theoretical temperature distributions through gas
turbine with special blades and cooling fins on the rim; naca-rm-e7i22a;
February 17, 1948
- Bolz, Ray E Schroeter,
Thomas T Zettle, Eugene V; A
comparison of the simulated-altitude performance of two turbojet combustor
types; naca-rm-e7i25; October 07, 1948
- Novik, David Otto,
Edward W; An
analysis of control requirements and control parameters for direct-coupled
turbojet engines; naca-rm-e7i25a; February 18, 1948
- Wilsted, H D Stemples,
W D; Preliminary
estimate of performance of a turbojet engine when inlet pressure is reduced
below exhaust pressure; naca-rm-e7i30; February 18, 1948
- Humble, Leroy V Doyle,
Ronald B; Calculated
condenser performance for a steam turbine power plant for aircraft;
naca-rm-e7j01; May 20, 1948
- Hill, Francis U Mark,
Herman; Performance of
experimental turbojet-engine combustor I : performance of a one-eighth segment
of an experimental turbojet-engine combustor; naca-rm-e7j13; April 21,
1948
- Farmer, J Elmo Darmara,
F N Poulson, Francis D; Cyclic
engine test of cast vitallium turbine buckets I; naca-rm-e7j23; February
19, 1948
- Farmer, J Elmo Deutsch,
George C Sikora, Paul F; Cyclic
engine test of cast vitallium turbine buckets II; naca-rm-e7j24; January
12, 1948
- Rowe, William H Ordin,
Paul M Diehl, John M; Investigation
of the diborane - hydrogen peroxide propellant combination; naca-rm-e7k07;
May 28, 1948
- Baron, Burnett Dowman,
Harry W Dackis, William C; Experimental
investigation of thrust augmentation of axial-flow-type 4000-pound-thrust
turbojet engine by water and alcohol injection at compressor inlet;
naca-rm-e7k14; July 08, 1948
- Brightwell, Virginia L
Peters, Max D Sanders, J C; Comparison
of hovering performance of helicopters powered by jet-propulsion and
reciprocating engines; naca-rm-e7k21; June 11, 1948
- Kemp, Richard H Morgan,
William C; Analytical
investigation of distribution of centrifugal stresses and their relation to
limiting operating temperatures in gas-turbine blades; naca-rm-e7l05;
April 12, 1948
- Ritter, William K
Johnsen, Irving A; Performance
of 24-inch supersonic axial-flow compressor in air I : performance of
compressor rotor at design tip speed of 1600 feet per second;
naca-rm-e7l10; May 17, 1948
- Farmer, J Elmo; Relation of
nozzle-blade and turbine-bucket temperatures to gas temperatures in a turbojet
engine; naca-rm-e7l12; April 30, 1948
- Dietz, Robert O , Jr
Wishnek, George Kuenzig, John K; Altitude-wind-tunnel
investigation of thrust augmentation of a turbojet engine IV : performance
with tail-pipe burning and water injection; naca-rm-e7l16; June 15,
1948
- Koenig, Robert J
Dandois, Marcel; Control
during starting of gas-turbine engines; naca-rm-e7l17; June 17,
1948
- Morgan, W C Kemp, R H
Manson, S S; Vibration of
turbine blades in a turbojet engine during operation; naca-rm-e7l18; April
22, 1948
- Wright, Linwood C; Investigation
to determine contraction ratio for supersonic-compressor rotor;
naca-rm-e7l23; April 30, 1948
- Wear, Jerrold D Jonash,
Edmund R; Combustion-efficiency
and altitude-limit investigations of five fuels in an annular turbojet
combustor; naca-rm-e7l30; June 07, 1948
- Davis, Wallace F
Brajnikoff, George B; Pressure
recovery at supersonic speeds through annular duct inlets situated in a region
of appreciable boundary layer I : addition of energy to the boundary
layer; naca-rm-a8a13; April 1948
- Ilk, Richard J; The
effectiveness at high speeds of a 10-percent-chord plain trailing-edge flap on
the NACA 65-210 airfoil section; naca-rm-a8a21; June 14, 1948
- Dods, Jules B , Jr; Wind-tunnel
investigation of horizontal tails II : unswept and 35 degree swept-back plan
forms of aspect ratio 4.5; naca-rm-a8b11; June 03, 1948
- Hall, Charles F
Barclay, F Dorn; An
experimental investigation of NACA submerged inlets at high subsonic speeds I:
inlets forward of the wing leading edge; naca-rm-a8b16; June 09,
1948
- Rose, Leonard; Low-speed
investigation of a small triangular wing of aspect ratio 2.0 III : static
stability with twin vertical fins; naca-rm-a8c03; August 24, 1948
- Boyd, John W Frick,
Charles W; Investigation
at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees
swept airfoil of biconvex section at zero lift; naca-rm-a8c22; June 10,
1948
- Rathert, George A , Jr
Cooper, George E; Visual
observations of the shock wave in flight; naca-rm-a8c25; May 24,
1948
- Reynolds, Robert M
Smith, Donald W; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
subsonic Mach and Reynolds number effects on the characteristics of the wing
and on the effectiveness of an elevon; naca-rm-a8d20; October 11,
1948
- Stephenson, Jack D
Amuedo, Arthur R; Tests
of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind
tunnel II : the effectiveness and hinge moments of a constant-chord plain
flap; naca-rm-a8e03; September 21, 1948
- Hanson, Frederick H ,
Jr Dannenberg, Robert E; Effect
of a nacelle on the low-speed aerodynamic characteristics of a swept-back
wing; naca-rm-a8e12; July 21, 1948
- Stalder, Jackson R
Spies, Ray J , Jr; An
experimental investigation of an exhaust-gas-to-air heat exchanger for use on
jet-stack-equipped engines; naca-rm-a8e14; October 05, 1948
- Bandettini, Angelo
Johnson, Ben H , Jr; Investigation
of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel II :
the effect of constant-chord leading- and trailing-edge flaps on the low-speed
characteristics of the wing; naca-rm-a8f15; October 18, 1948
- Holzhauser, Curt A
Martin, Norman J; An
experimental investigation at large scale of several configurations of an NACA
submerged air intake; naca-rm-a8f21; October 19, 1948
- Katzen, Elliott D
Frick, Charles W Boyd, John W; Investigation
at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees
swept airfoil of biconvex section at several angles of attack;
naca-rm-a8f22; September 24, 1948
- Erickson, Albert L
Robinson, Robert C; Some
preliminary results in the determination of aerodynamic derivatives of control
surfaces in the transonic speed range by means of a flush-type electrical
pressure cell; naca-rm-a8h03; October 08, 1948
- Berggren, Robert E
Summers, James L; Aerodynamic
characteristics at subsonic and supersonic Mach numbers of a thin triangular
wing of aspect ratio 2 I : maximum thickness at 20 percent of the chord;
naca-rm-a8i16; November 19, 1948
- Walker, Harold J
Berggren, Robert E; Aerodynamic
characteristics at subsonic and supersonic Mach numbers of a thin triangular
wing of aspect ratio 2 II : maximum thickness at midchord; naca-rm-a8i20;
December 03, 1948
- Millenson, M B
Wilterdink, P I; Empirical
mode constants for calculating frequencies of axial-flow compressor
blades; naca-rm-e8a20; April 23, 1948
- Von Glahn, Uwe; Ice protection
of turbojet engines by inertia separation of water I : alternate-duct
system; naca-rm-e8a27; May 28, 1948
- Ruggeri, Robert S; Investigation
of the aerodynamic and icing characteristics of a recessed fuel cell vent
assembly I : rear wall vent tube mounting; naca-rm-e8a27b; March 29,
1948
- Von Glahn, Uwe; Ice protection
of turbojet engines by inertia separation of water II : single-offset-duct
system; naca-rm-e8a28; June 08, 1948
- Gold, Harold Koenig,
Robert J; Bench and
engine operation of a fuel-distribution control; naca-rm-e8a28a; June 14,
1948
- Von Glahn, Uwe; Ice protection
of turbojet engines by inertia separation of water III : annular submerged
inlets; naca-rm-e8a29; June 08, 1948
- Mendelson, Alexander;
Effect of
aerodynamic hysteresis on critical flutter speed at stall; naca-rm-e8b04;
June 18, 1948
- Mendelson, Alexander;
Effect of
centrifugal force on critical flutter speed on a uniform cantilever beam;
naca-rm-e8b05; June 18, 1948
- Ruggeri, Robert S; Investigation
of the aerodynamic and icing characteristics of a recessed fuel cell vent
assembly : ramp floor vent-tube mounting; naca-rm-e8b05a; March 30,
1948
- (Author(s) Not
Available); Preliminary
survey of the aircraft fire problem; naca-rm-e8b18; May 21, 1948
- Ross, Albert O Nettles,
J Cary Esterly, John R; Performance
of J33 turbojet engine with shaft power extraction II : compressor;
naca-rm-e8b27b; August 24, 1948
- Mccafferty, Richard J;
Effect of
fuels and fuel-nozzle characteristics on performance of an annular combustor
at simulated altitude conditions; naca-rm-e8c02a; September 28,
1948
- Ruggeri, Robert S; Investigation
of the aerodynamic and icing characteristics of a recessed fuel cell vent
assembly III : NACA flush-inlet-type vent; naca-rm-e8c05; April 23,
1948
- Gold, Harold Straight,
David M; A
fuel-distribution control for gas-turbine engines; naca-rm-e8c08; June 14,
1948
- Miller, R C Cervenka, A
J; Effect of
inlet-air parameters on combustion limit and flame length in 8-inch-diameter
ram-jet combustion chamber; naca-rm-e8c09; July 22, 1948
- Millenson, M B Manson,
S S Farmer, J Elmo; Study
of stress states in gas-turbine disk as determined from measured
operating-temperature distributions; naca-rm-e8c16; July 21, 1948
- Acker, Loren W; Preliminary
results of natural icing of an axial-flow turbojet engine; naca-rm-e8c18;
August 06, 1948
- Kottas, Harry Sheflin,
Bob W; Investigation
of high-temperature operation of liquid-cooled gas turbines I : turbine wheel
of aluminum alloy, a high-conductivity nonstrategic material;
naca-rm-e8d12; July 22, 1948
- Callaghan, Edmund E
Ruggeri, Robert S Krebs, Richard P; Experimental
investigation of hot-gas bleedback for ice protection of turbojet engines I :
nacelle with offset air inlet; naca-rm-e8d13; July 09, 1948
- Huddleston, S C
Wilsted, H D Ellis, C W; Performance
of several air ejectors with conical mixing sections and small secondary flow
rates; naca-rm-e8d23; July 19, 1948
- Meyer, Andre J , Jr
Hanson, Morgan P; Vibration
survey of NACA 24-inch supersonic axial-flow compressor; naca-rm-e8d30;
July 30, 1948
- Bowman, William D; Analytical
investigation of effect of water-cooled turbine blades on performance of
turbine-propeller power plants; naca-rm-e8e10; August 16, 1948
- Good, James N; Residual
stress analysis of overspeeded disk with central hole by x-ray
diffraction; naca-rm-e8e11; July 23, 1948
- Acker, Loren W; Natural icing
of an axial-flow turbojet engine in flight for a single icing condition;
naca-rm-e8f01a; August 12, 1948
- Goldstein, Arthur W; Design and
performance of experimental axial-discharge mixed-flow compressor I : impeller
design theory; naca-rm-e8f04; August 12, 1948
- Pinkel, I Irving
Shames, Harold; Altitude-wind-tunnel
investigation of a 4000-pound-thrust axial-flow turbojet engine VI :
combustion-chamber performance; naca-rm-e8f09e; August 04, 1948
- Cook, William P Zettle,
Eugene V; Performance
investigation of can-type combustor I : instrumentation, altitude operational
limits and combustion efficiency; naca-rm-e8f17; September 16, 1948
- Duffy, Robert T Grey,
Ralph E Wilsted, H D; Operating
temperatures of I-40-5 turbojet engine burner liners and the effect of
temperature variation on burner-liner service life; naca-rm-e8f29; August
23, 1948
- Guentert, Donald C
Mankuta, Harry; Investigation
of performance of single-stage axial-flow compressor using NACA 5509-34 blade
section; naca-rm-e8f30; September 30, 1948
- Gendler, Stanley L
Koffel, William K; Investigation
of the I-40 jet-propulsion engine in the Cleveland altitude wind tunnel I :
performance and windmilling drag characteristics; naca-rm-e8g02; August
24, 1948
- Dietz, Robert O
Geisenheyner, Robert M; Investigation
of the I-40 jet-propulsion engine in the Cleveland altitude wind tunnel II :
analysis of compressor performance characteristics; naca-rm-e8g02a; August
26, 1948
- Krebs, Richard P
Foshag, Frederick C; Investigation
of the I-40 jet-propulsion engine in the Cleveland altitude wind tunnel III :
analysis of turbine performance and effect of tail-pipe design on engine
performance; naca-rm-e8g02b; August 26, 1948
- Hensley, Reece V; Investigation
of the I-40 jet-propulsion engine in the Cleveland Altitude wind tunnel IV :
analysis of combustion-chamber performance; naca-rm-e8g02c; August 25,
1948
- Golladay, Richard L
Gendler, Stanley L; Investigation
of the I-40 jet-propulsion engine in the Cleveland altitude wind tunnel V :
operational characteristics; naca-rm-e8g02d; August 25, 1948
- Schroeder, Albert H
Connors, James F; Preliminary
investigation of effects of combustion in ram jet performance of supersonic
diffusers II : perforated supersonic inlet; naca-rm-e8g16; October 04,
1948
- Freche, John C Sheflin,
Bob W; Investigation
of a gas turbine with National Bureau of Standards body 4811 ceramic rotor
blades; naca-rm-e8g20; October 28, 1948
- Valerino, Michael F; Generalized
charts for determination of pressure drop of a high-speed compressible fluid
in heat-exchanger passages I : air heated in smooth passages of constant area
with constant wall temperature; naca-rm-e8g23; October 05, 1948
- Meyer, Gene L; Determination
of average heat-transfer coefficients for a cascade of symmetrical impulse
turbine blades I : heat transfer from blades to cold air; naca-rm-e8h12;
November 10, 1948
- Boksenbom, Aaron S
Novik, David; Control
requirements and control parameters for a ram jet with variable-area exhaust
nozzle; naca-rm-e8h24; November 17, 1948
- Black, Dugald O
Messing, Wesley E; Effect
of three flame-holder configurations on subsonic flight performance of
rectangular ram jet over range of altitudes; naca-rm-e8i01; November 24,
1948
- Howard, Ephraim, M
Wilcox, Fred A Dupree, David T; Combustion-chamber
performance with four fuels in Bumblebee 18-inch ram jet incorporating various
rake- or gutter-type flame holders; naca-rm-e8i01a; December 02,
1948
- Kochendorfer, Fred D
Nettles, J Cary; An
analytical method of estimating turbine performance; naca-rm-e8i16;
December 29, 1948
- Morse, C Robert; Comparison of
National Bureau of Standards ceramic coatings L-7C and A-417 on turbine blades
in a turbojet engine; naca-rm-e8i20; December 22, 1948
- Schroeder, Albert H
Connors, James F; Preliminary
investigation of effects of combustion in ram jet on performance of supersonic
diffusers III : normal-shock diffuser; naca-rm-e8j18; December 22,
1948
- Hawkins, W Kent Meyer,
Carl L; Altitude-wind-tunnel
investigation of operational characteristics of Westinghouse X24C-4B axial
flow turbojet engine; naca-rm-e8j25; November 23, 1948
- Meyer, Carl L Bloomer,
Harry E; Altitude-wind-tunnel
investigation of performance and windmilling drag characteristics of
Westinghouse X24C-4B axial-flow turbojet engine; naca-rm-e8j25a; November
23, 1948
- Sanders, Newell D
Palasics, John; Analysis
of effects of inlet pressure losses on performance of axial-flow type turbojet
engine; naca-rm-e8j25b; 1948
- Fleming, William A
Saari, Martin J; Inlet
icing and effectiveness of hot-gas bleedback for ice protection of turbojet
engine; naca-rm-e8j25c; November 26, 1948
- Wallner, Lewis E; Investigation
of performance of turbojet engine with constant- and variable-area exhaust
nozzles; naca-rm-e8j25d; November 26, 1948
- Fleming, William A
Wallner, Lewis E; Altitude-wind-tunnel
investigation of tail-pipe burning with a Westinghouse X24C-4B axial-flow
turbojet engine; naca-rm-e8j25e; December 13, 1948
- Krebs, Richard P
Suozzi, Frank L; Altitude-Wind-Tunnel
investigation of Westinghouse 19B-2, 19B-8, and 19XB-1 Jet-Propulsion Engines
II : analysis of turbine performance of 19B-8 engine; naca-rm-e8j28a;
November 24, 1948
- Fleming, William A
Dietz, Robert O JR; Altitude-wind-tunnel
investigation of Westinghouse 19B-2, 19B-8, and 19XB-1 jet-propulsion engines
III : performance and windmilling drag characteristics; naca-rm-e8j28b;
November 26, 1948
- Dietz, Robert O
Kuenzig, John K; Altitude-Wind-Tunnel
investigation of Westinghouse 19B-2, 19B-8, and 19XB-1 Jet-Propulsion Engines
IV : analysis of compressor performance; naca-rm-e8j28c; November 26,
1948
- Boyd, Bemrose; Altitude-Wind-Tunnel
investigation of Westinghouse 19B-2, 19B-8, and 19XB-1 jet-propulsion engines
V : combustion chamber performance; naca-rm-e8j28d; November 26,
1948
- Morrissette, Robert R
Oborny, Lester F; Theoretical
characteristics of two-dimensional supersonic control surfaces;
naca-rm-l8g12; July 27, 1948
- Letko, William Jaquet,
Byron M; Effect of
airfoil profile of symmetrical sections on the low-speed static-stability and
yawing derivatives of 45 degrees sweptback wing models of aspect ratio
2.61; naca-rm-l8h10; November 09, 1948
- Brewer, Jack D Fisher,
Lewis R; Effect of taper
ratio on the low-speed rolling stability derivatives of swept and unswept
wings of aspect ratio 2.61; naca-rm-l8h18; November 09, 1948
- Fischel, Jack
Schneiter, Leslie E; An
investigation at low speed of a 51.3 degree sweptback semispan wing equipped
with 16.7-percent-chord plain flaps and ailerons having various spans and
three trailing-edge angles; naca-rm-l8h20; November 12, 1948
- Queijo, M J
Lichtenstein, Jacob H; The
effects of high-lift devices on the low-speed stability of a tapered 37.5
degree sweptback wing of aspect ratio 3 in straight and rolling flow;
naca-rm-l8i03; November 09, 1948
- Donaldson, Coleman Dup;
Note on the
importance of imperfect-gas effects and variation of heat capacities on the
isentropic flow of gases; naca-rm-l8j14; December 10, 1948
- Laszlo, F.; Rotating
disks in the region of permanent deformation; naca-tm-1192; 1948
- Olson, Walter T.,
Schroeter, Thomas T.; Effect
of distribution of basket-hole area on simulated altitude performance of 25
1/2-inch-diameter annular-type turbojet combustor; naca-rm-e8a02;
1948
- Conrad, Earl W., Dietz,
Robert O., Golladay, Richard L.; Altitude-wind-tunnel
investigation of a 3000-pound-thrust acial-flow turbojet engine:I. Analysis of
turbine performance; naca-rm-e8a23; 1948
- Dietz, Robert O.,
Berdysz, Joseph J., Howard, Ephraim M.; Altitude-wind-tunnel
investigation of a 3000-pound-thrust axial-flow turbojet engine:II. Analysis
of compressor performance; naca-rm-e8a26a; 1948
- Campbell, Carl E.; Altitude-wind-tunnel
investigation of a 3000-pound-thrust axial-flow turbojet engine:III. Analysis
of combustion-chamber performance; naca-rm-e8b19; 1948
- Saari, Martin J.,
Prince, William R.; Altitude-wind-tunnel
investigation of a 3000-pound-thrust axial-flow turbojet engine:VII - pressure
and temperature distributions; naca-rm-e8c17; 1948
- Hawkins, W. Kent,
Meyer, Carl L.; Altitude-wind-tunnel
investigation of a 3000-pound-thrust axial-flow turboject engine IV -
operational characteristics; naca-rm-e8b19a; 1948
- Sanders, Newell D.,
Palasics, John; Altitude-wind-tunnel
investigation of a 3000-pound-thrust axial-flow turbojet engine VI : analysis
of effects of inlet pressure losses; naca-rm-e8c16a; 1948
- Fleming, William A.; Altitude-wind-tunnel
investigation of a 4000-pound-thrust axial-flow turbojet engine I :
performance and windmilling drag characteristics; naca-rm-e8f09;
1948
- Fleming, William A.,
Golladay, Richard L.; Altitude-wind-tunnel
investigation of a 4000-pound-thrust axial-flow turbojet engine III :
performance characteristics with the high-flow compressor; naca-rm-e8f09b;
1948
- Dietz, Robert C.,
Suozzi, Frank L.; Altitude-wind-tunnel
investigation of a 4000-pound-thrust axial-flow turbojet engine IV : analysis
of compressor performance; naca-rm-e8f09c; 1948
- Krebs, Richard P.,
Hensley, Reece V.; Altitude-wind-tunnel
investigation of a 4000-pound-thrust axial-flow turbojet engine V : analysis
of turbine performance; naca-rm-e8f09d; 1948
- Saari, Martin J.,
Wallner, Lewis E.; Preliminary
results of an altitude-wind-tunnel investigation of an axial-flow gas
turbine-propeller engine I : performance characteristics; naca-rm-e8f10;
1948
- Conrad, E. W., Durham,
J. D.; Preliminary
results of an altitude-wind-tunnel investigation of an axial-flow gas
turbine-propeller engine II : windmilling characteristics; naca-rm-e8f10a;
1948
- Geisenheyner, Robert
M., Berdysz, Joseph J.; Preliminary
results of an altitude-wind-tunnel investigation of an axial-flow gas
turbine-propeller engine III : pressure and temperature distributions;
naca-rm-e8f10b; 1948
- Wallner, Lewis E.,
Saari, Martin J.; Preliminary
results of an altitude-wind-tunnel investigation of an axial-flow gas
turbine-propeller engine IV : compressor and turbine performance
characteristics; naca-rm-e8f10c; 1948
- Geisenheyner, Robert
M., Berdysz, Joseph J.; Preliminary
results of an altitude-wind-tunnel investigation of an axial-flow gas
turbine-propeller engine V : combustion-chamber characteristics;
naca-rm-e8f10d; 1948
- Ginsburg, Ambrose,
Creagh, John W. R., Ritter, William K.; Pefromance
investigations of a large centrifugal compressor from an experimental turbojet
engine; naca-rm-e8h13; 1948
- Wyatt, DeMarquis D.; Experimental
pressure distribution on fuselage nose and pilot canopy of supersonic airplane
at Mach Number 1.90; naca-rm-e8i07; 1948
- Shames, Harold,
Seashore, Ferris L.; Design
data for graphical construction of two-dimensional sharp-edge-throat
supersonic nozzles; naca-rm-e8j12; 1948
- Fleming, William A.; Altitude-wind-tunnel
investigation of Westinghouse 19B-2, 19B-8, and 19XB-1 jet-propulsion engines
I : operational characteristics; naca-rm-e8j28; 1948
- Childs, J. Howard,
McCafferty, Richard J.; Simulated
altitude performance of combustor of westinghouse 19XB-1 jet-propulsion
engine; naca-rm-e8j29; 1948
- Wagner, Herbert; Planing of
watercraft; naca-tm-1139; 1948
- Weber, Kehl; Wind-tunnel
measurements on the Henschel Missile "Zitterrochen" in subsonic and supersonic
velocities and Wind-tunnel measurements on the wing of the Henschel Missile
"Zitterrochen" in subsonic and supersonic velocities; naca-tm-1159;
1948
- Regenscheit, B.; Venturi tube
with varying mass flow; naca-tm-1191; 1948
- Fischel, Jack., Ivey,
Margaret F.; Collection of
test data for lateral control with full-span flaps; naca-tn-1404;
1948
- Hunter, Paul A.; Flight
measurements of the flying qualities of five light airplanes;
naca-tn-1573; 1948
- Corrington, Lester C.,
Fisher, William F.; Effect
of preignition on cylinder temperatures, pressures, power output, and piston
failures; naca-tn-1637; 1948
- Gale, Lawrence J.; Effect of
landing flaps and landing gear on the spin and recovery characteristics of
airplanes; naca-tn-1643; 1948
- Johnson, Harold S.; Wind-tunnel
investigation of effects of tail length on the longitudinal and lateral
stability characteristics of a single-propeller airplane model;
naca-tn-1766; 1948
- Scherrer, Richard.,
Wimbrow, William R.; Wind-tunnel
investigation at a Mach number of 1.53 of an airplane with a triangular
wing; naca-rm-a7j05; 1948
- Hopkins, Edward J.; An exploratory
investigation of the relative merits of split and chord-extension flaps on a
45 degrees swept-back wing; naca-rm-a8a16; 1948
- Delany, Noel K.; An
investigation of submerged air inlets on a 1/4-scale model of a typical
fighter-type airplane; naca-rm-a8a20; 1948
- Perone, Angelo.,
Erickson, Albert L.; Wind-tunnel
investigation of transonic aileron flutter of a semispan wing model with an
NACA 23013 section; naca-rm-a8d27; 1948
- Kolbe, Carl D.,
Tinling, Bruce E.; Tests
of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind
tunnel III :the effectiveness and hinge moments of a skewed wing-tip flap;
naca-rm-a8e21; 1948
- Brajnikoff, George B.;
Pressure
recovery at supersonic speeds through annular duct inlets situated in a region
of appreciable boundary layer II :effect of an oblique shock wave immediately
ahead of the inlet; naca-rm-a8f08; 1948
- Dods, Jules, B., Jr.;
Wind-tunnel
investigation of horizontal tails III :unswept and 35 degrees swept-back plan
forms of aspect ratio 6; naca-rm-a8h30; 1948
- Hall, Charles F.,
Frank, Joseph L.; Ram-recovery
characteristics of NACA submerged inlets at high subsonic speeds;
naca-rm-a8i29; 1948
- L. Gutin; On
the Sound Field of a Rotating Propeller; naca-tm-1195; 1948
- Reece V. Hensley
(Flight Propulsion Laboratory, Cleveland, Ohio); Theoretical
Analysis of the Performance of a Supersonic Ducted Rocket; naca-rm-e7i05;
1948
- John H. Disher (Flight
Propulsion Laboratory, Cleveland, Ohio); Flight
Investigation of a 20-inch-diameter Steady-Flow Ram Jet; naca-rm-e7i05a;
1948
- Walter J. Klinar,
Lawrence J. Gale; Wind-tunnel
investigation of the spinning characteristics of a model of a twin-tail
low-wing personal-owner-type airplane with linked and unlinked rudder and
aileron controls; naca-tn-1801; January 1949
- F. B. Gustafson; The application
of airfoil studies to helicopter rotor design; naca-tn-1812; February
1949
- Paul Seide, Manuel
Stein; Compressive
buckling of simply supported plates with longitudinal stiffeners;
naca-tn-1825; March, 1949
- Manuel Stein, Robert W.
Fralich; Critical shear
stress of infinitely long, simply supported plate with transverse
stiffeners; naca-tn-1851;
- Murry Schildcrout,
Manuel Stein; Critical
Axial-Compressive Stress of a Curved Rectangular Panel with a Central
Longitudal Stiffener; naca-tn-1879; May 1949
- NACA Subcommitte on
Turbines; Provisional
symbols and definitions for aircraft turbines; naca-tn-1508; Mar
1949
- M. D. Burdick, R. E.
Moreland, R. F. Geller; Strength
and creep characteristics of ceramic bodies at elevated temperatures;
naca-tn-1561; Apr 1949
- Arvo A. Luoma; An
investigation of the section characteristics of plain unsealed ailerons on an
NACA 66,1-115 airfoil section in the Langley 8-foot high-speed tunnel;
naca-tn-1596; Jan 1949
- Hugh L. Dryden, Ira H.
Abbott; The
design of low-turbulence wind tunnels; naca-tn-1755; Nov 1949
- J. W. Freeman, Howard
C. Cross; NACA and Office
of Naval Research metallurgical investigation of two large forged discs of
S-590 alloy; naca-tn-1760; Feb 1949
- Howard C. Cross, J. W.
Freeman; Office of Naval
Research and NACA metallurgical investigation of a large forged disc of S-816
alloy; naca-tn-1765; Feb 1949
- Maxwell Alfred Heaslet,
Harvard Lomax; The
application of Green's theorem to the solution of boundary-value problems in
linearized supersonic wing theory; naca-tn-1767; Apr 1949
- Jim Rogers Thompson; A rapid
graphical method for computing the pressure distribution at supersonic speeds
on a slender arbitrary body of revolution; naca-tn-1768; Jan 1949
- Howard C. Cross, J. W.
Freeman; Office of Naval
Research and NACA metallurgical investigation of a large forged disc of
Inconel X alloy; naca-tn-1770; Apr 1949
- Philip M. Edge; Hydrodynamic
impact loads in smooth water for a prismatic float having an angle of dead
rise of 40 degrees; naca-tn-1775; Jan 1949
- Norris F. Dow, Albert
S. Keevil, Jr; Direct-reading
design charts for 24S-T aluminum-alloy flat compression panels having
longitudinal formed Z-section stiffeners; naca-tn-1778; Jan 1949
- Margaret F. Steiner; Comparison of
over-all impact loads obtained during seaplane landing tests with loads
predicted by hydrodynamic theory; naca-tn-1781; Jan 1949
- Arthur W. Carter; Effect of hull
length-beam ratio on the hydrodynamic characteristics of flying boats in
waves; naca-tn-1782; Jan 1949
- Jerome B. Hammack; Flight
investigation in climb and at high speed of a two-blade and a three-blade
propeller; naca-tn-1784; Jan 1949
- Norris F. Dow, William
A. Hickman; Comparison of
the structural efficiency of panels having straight-web and curved-web
Y-section stiffeners; naca-tn-1787; Jan 1949
- Robert S. Ruggeri, Uwe
Von Glahn, Vern G. Rollin; Investigation
of aerodynamic and icing characteristics of recessed fuel-vent
configurations; naca-tn-1789; Mar 1949
- Willard D. Coles; Investigation
of icing characteristics of typical light-airplane engine induction
systems; naca-tn-1790; Feb 1949
- George H. Holdaway; Corrosion tests
of a heated wing utilizing an exhaust-gas-air mixture for ice prevention;
naca-tn-1791; Jan 1949
- Robert V. Hess,
Clifford S. Gardner; Study
by the Prandtl-Glauert method of compressibility effects and critical Mach
number for ellipsoids of various aspect ratios and thickness ratios;
naca-tn-1792; Jan 1949
- Dwight B. Kline; Investigation
of meteorological conditions associated with aircraft icing in layer-type
clouds for 1947-48 winter; naca-tn-1793; Jan 1949
- Thomas D. Reisert; Gust-tunnel
investigation of a wing model with semichord line swept back 30 degrees;
naca-tn-1794; Jan 1949
- Chung-Hua Wu, Lincoln
Wolfenstein; Application of
radial-equilibrium condition to axial-flow compressor and turbine design;
naca-tn-1795; Jan 1949
- William H Phillips; Theoretical
analysis of oscillations of a towed cable; naca-tn-1796; Jan 1949
- Gerald M. McCormack,
Woodrow L. Cook; A
study of stall phenomena on a 45 degree swept-forward wing; naca-tn-1797;
Jan 1949
- Kenneth Margolis; Effect of
thickness on the lateral force and yawing moment of a sideslipping delta wing
at supersonic speeds; naca-tn-1798; Jan 1949
- John P. Reeder, F. B.
Gustafson; On the flying
qualities of helicopters; naca-tn-1799; Jan 1949
- Norris F. Dow, Ralph E.
Hubka, William M. Roberts; Direct-reading
design charts for 24S-T aluminum-alloy flat compression panels having
longitudinal straight-web Y-section stiffeners; naca-tn-1777; Jan
1949
- Dean R. Chapman; Laminar mixing
of a compressible fluid; naca-tn-1800; Feb 1949
- Jack Fischel; Wind-tunnel
investigation of an NACA 65-210 semispan wing equipped with circular plug
ailerons and a full-span slotted flap; naca-tn-1802; Jan 1949
- Harvard Lomax, Loma
Sluder; Downwash in the
vertical and horizontal planes of symmetry behind a triangular wing in
supersonic flow; naca-tn-1803; Jan 1949
- R. B. Clark, W. T.
Sparrow; Effect of
longitudinal steps on skipping characteristics of PB2Y-6 flying boat;
naca-tn-1804; Jan 1949
- Neal Tetervin; Remarks
concerning the behavior of the laminar boundary layer in compressible
flows; naca-tn-1805; Jan 1949
- Robert C. Kohl, Howard
Z. Herzig, Warren J. Whitney; Effects
of partial admission on performance of a gas turbine; naca-tn-1807; Feb
1949
- Antonio Ferri; Method
for evaluating from shadow or Schlieren photographs the pressure drag in
two-dimensional or axially symmetrical flow phenomena with detached shock;
naca-tn-1808; Feb 1949
- Antonio Ferri; The
method of characteristics for the determination of supersonic flow over bodies
of revolution at small angles of attack; naca-tn-1809; Feb 1949
- M. C. Huppert, Charles
MacGregor; Comparison
between predicted and observed performance of gas-turbine stator blade
designed for free-vortex flow; naca-tn-1810; Apr 1949
- C. W. Frick, R. S.
Chubb; The
longitudinal stability of elastic swept wings at supersonic speed;
naca-tn-1811; Feb 1949
- Gerald E. Nitzberg,
Stewart Crandall; A
study of flow changes associated with airfoil section drag rise at
supercritical speeds; naca-tn-1813; Feb 1949
- Vincent L. Lavalle,
Merle C. Huppert; Effects
of several design variables on turbine-wheel weight; naca-tn-1814; Feb
1949
- Eric Reissner; On
compressibility corrections for subsonic flow over bodies of revolution;
naca-tn-1815; Feb 1949
- Barrett S. Baldwin,
Jr.; Triangular
wings cambered and twisted to support specified distributions of lift at
supersonic speeds; naca-tn-1816; Feb 1949
- Leonard Sternfield; Effect of
automatic stabilization on the lateral oscillatory stability of a hypothetical
airplane at supersonic speeds; naca-tn-1818; Mar 1949
- Israel Taback; The
response of pressure measuring systems to oscillating pressures;
naca-tn-1819; Feb 1949
- Bernard Wiener; Ambient
pressure determination at high altitudes by use of free-molecule theory;
naca-tn-1821; Mar 1949
- Paul Seide, John F.
Eppler; The
buckling of parallel simply supported tension and compression members
connected by elastic deflectional springs; naca-tn-1823; Feb 1949
- Max A. Heaslet, Harvard
Lomax, John R. Spreiter; Linearized
compressible-flow theory for sonic flight speeds; naca-tn-1824; Jan
1950
- Samuel Katzoff,
Clifford S. Gardner, Leo Diesendruck, Bertram J. Eisenstadt; Linear
theory of boundary effects in open wind tunnels with finite jet lengths;
naca-tn-1826; Mar 1949
- Stanley U. Benscoter,
Myron L. Gossard; Matrix
methods for calculating cantilever-beam deflections; naca-tn-1827; Mar
1949
- Arthur W. Carter,
Irving Weinstein; Effect
of forebody warp on the hydrodynamic qualities of a hypothetical flying boat
having a hull length-beam ratio of 15; naca-tn-1828; Mar 1949
- L. A.Harney, J. F. T.
Saur, A. R. Robinson; A
statistical study of wave conditions at four open-sea localities in the North
Pacific Ocean; naca-tn-1493; Jan 1949
- Leslie F. Lawrence,
James L. Summers; Wind-tunnel
investigation of a tailless triangular-wing fighter aircraft at Mach numbers
from 0.5 to 1.5; naca-rm-a9b16; Jun 1949
- Jules B. Dods, Jr.; Wind-tunnel
investigation of horizontal tails V : 45 degree swept-back plan form of aspect
ratio 2; naca-rm-a9d05; Sep 1949
- Robert T. Madden; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
investigation at a Mach number of 1.53 to determine the effects of cambering
and twisting the wing for uniform load at a lift coefficient of 0.25;
naca-rm-a9c07; May 1949
- Victor I. Stevens, John
W. Boyd; A
comparison of theoretical and experimental loading on a 63 degrees swept-back
wing at supersonic speeds; naca-rm-a9c16; Sep 1949
- Angelo Bandettini,
Verlin D. Reed; The
aerodynamic characteristics throughout the subsonic speed range of a thin,
sharp-edged horizontal tail of aspect ratio 4 equipped with a constant-chord
elevator; naca-rm-a9e05; Jun 1949
- Newton A. Mas; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
characteristics for symmetrical wing sections at high subsonic and moderate
supersonic Mach numbers; naca-rm-a9e09; Jul 1949
- Jack N. Nielsen,
Frederick H. Matteson; Calculative
method for estimating the interference pressure field at zero lift on a
symmetrical swept-back wing mounted on a circular cylindrical body;
naca-rm-a9e19; Aug 1949
- Gerald M. McCormack; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
aerodynamic characteristics in sideslip of a large-scale model having a 63
degree swept-back vertical tail; naca-rm-a9f14; Oct 1949
- Ben H. Johnson, Jr.,
Francis W. Rollins; Investigation
of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel V :
static longitudinal stability and control throughout the subsonic speed range
of a semispan model of a supersonic airplane; naca-rm-a9i01; Dec
1949
- J. Lloyd Jones, Fred A.
Demele; Aerodynamic
Study of a Wing-Fuselage Combination Employing a Wing Swept back 63 deg -
Characteristics Throughout the Subsonic Speed Range with the Wing Cambered and
Twisted for a Uniform Load at a Lift Coefficient of 0.25; naca-rm-a9d25;
Aug 1949
- Clyde Hayes; Preliminary
investigation of a variable mass-flow supersonic nose inlet;
naca-rm-l9j11; Dec 1949
- Carl A. Sandahl, H.
Kurt Strass; Comparative
tests of the rolling effectiveness of constant-chord, full-delta, and
half-delta ailerons on delta wings at transonic and supersonic speeds;
naca-rm-l9j26; Dec 1949
- James M. Benson, Thomas
W. Williams; Preliminary
investigation of the use of afterglow for visualizing low-density compressible
flows; naca-rm-l9a24a; Feb 1949
- Charles H. McLellan,
Thomas W. Williams, Mitchel H. Bertram; Investigation
of a two-step nozzle in an 11-inch hypersonic tunnel; naca-rm-l9g26; Oct
1949
- W. J. McCann; Thermodynamic
charts for internal-combustion-engine fluids; naca-tn-1883; Jul
1949
- John D. Stanitz,
Gaylord O. Ellis; Two-dimensional
compressible flow in centrifugal compressors with straight blades;
naca-tn-1932; Aug 1949
- Jack D. Stephenson; The effects of
aerodynamic brakes upon the speed characteristics of airplanes;
naca-tn-1939; Sep 1949
- Laurence K. Loftin,
Jr., Hamilton A. Smith; Aerodynamic
characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7
x 10(exp 6) to 9.0 x 10(exp 6); naca-tn-1945; Oct 1949
- N. J. Hoff, Bruno A.
Boley, Merven W. Mandel; Stresses
in and general instability of monocoque cylinders with cutouts VIII :
calculation of the buckling load of cylinders with long symmetric cutout
subjected to pure bending; naca-tn-1963; Oct 1949
- Albert E. McPherson, J.
Evans, Samuel Levy; Influence
of wing flexibility on force-time relation in shock strut following vertical
landing impact; naca-tn-1995; Nov 1949
- Morris Morduchow; On internal
damping of rotating beams; naca-tn-1996; Dec 1949
- Marion O. McKinney,
Jr.; Analysis of
means of improving the uncontrolled lateral motions of personal airplanes;
naca-tn-1997; Dec 1949
- Madden, Robert T; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
characteristics at a Mach number of 1.53 including effect of small variations
of sweep; naca-rm-a8j04; January 26, 1949
- Reed, Verlin D Johnson,
Ben H , Jr; Investigation
of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel IV :
the effect of a constant-chord leading-edge flap at high subsonic speeds;
naca-rm-a8k19; January 20, 1949
- Rathert, George A , Jr
Hanson, Carl M Rolls, L Stewart; Investigation
of a thin straight wing of aspect ratio 4 by the NACA wing-flow method : lift
and pitching-moment characteristics of the wing alone; naca-rm-a8l20;
February 14, 1949
- Scherrer, Richard
Gowen, Forrest R Wimbrow, William R; Heat-transfer
and boundary-layer transition on a heated 20 degree cone at a Mach number of
1.53; naca-rm-a8l28; January 10, 1949
- Allen, H Julian; Estimation of
the forces and moments acting on inclined bodies of revolution of high
fineness ratio; naca-rm-a9i26; November 14, 1949
- Edwards, Sherman S; Experimental
investigation at supersonic speeds of side scoops employing boundary-layer
suction; naca-rm-a9i29; December 12, 1949
- Huff, Vearl N Calvert,
Clyde S Erdmann, Virginia C; Theoretical
performance of diborane as a rocket fuel; naca-rm-e8i17a; January 10,
1949
- Maslen, Stephen H; Pressure
distributions on thin conical body of elliptic cross section at Mach number
1.89; naca-rm-e8k05; January 20, 1949
- Meyer, Carl L; Altitude-wind-tunnel
investigation of AN-F-58 fuel in experimental version of J47 turbojet
engine; naca-rm-e8l13; May 02, 1949
- Kinney, George R
Lidman, William G; Investigation
of ceramic, graphite, and chrome-plated graphite nozzles on rocket engine;
naca-rm-e8l16; March 07, 1949
- Wyatt, Demarquis D; Experimental
pressure distribution on a asymmetrical nonconical body at Mach number
1.90; naca-rm-e9b03; February 24, 1949
- Rowe, William H Ordin,
Paul M Diehl, John M; Experimental
investigation of liquid diborane - liquid oxygen propellant combination in
100-pound-thrust rocket engine; naca-rm-e9c11; May 09, 1949
- Carlton, William W
Messing, Wesley E; Free-flight
performance of 16-inch-diameter supersonic ram-jet units I : four units
designed for combustion-chamber-inlet Mach number of 0.12 at free-stream Mach
number of 1.6 (units A-2, A-3, A-4, and A-5); naca-rm-e9f22; September 22,
1949
- Sterbentz, William H;
Analysis and
experimental observation of pressure losses in ram-jet combustion
chambers; naca-rm-e9h19; November 04, 1949
- Stack, John Lindsey, W
F; Characteristics
of low-aspect-ratio wings at supercritical Mach numbers; naca-report-922;
1949
- Olson, Roland E Land,
Norman S; Effect of
afterbody length and keel angle on minimum depth of step for landing stability
and on take-off stability of a flying boat; naca-report-923; 1949
- Crigler, John L; Application of
Theodorsen's theory to propeller design; naca-report-924; 1949
- Harmon, Sidney M; Stability
derivatives at supersonic speeds of thin rectangular wings with diagonals
ahead of tip Mach lines; naca-report-925; 1949
- Vogeley, A W; Sound-level
measurements of a light airplane modified to reduce noise reaching the
ground; naca-report-926; 1949
- Phillips, William H; Appreciation
and prediction of flying qualities; naca-report-927; 1949
- Goldstein, Arthur W
Alpert, Sumner Beede, William Kovach, Karl; Analysis
of performance of jet engine from characteristics of components II :
interaction of components as determined from engine operation;
naca-report-928; 1949
- Machlin, E S; Dislocation
theory of the fatigue of metals; naca-report-929; 1949
- Kochendorfer, Fred D
Nettles, J Cary; An
analytical method of estimating turbine performance; naca-report-930;
1949
- Lundin, Bruce T
Povolny, John H Chelko, Louis J; Correlation
of cylinder-head temperatures and coolant heat rejections of a multicylinder,
liquid-cooled engine of 1710-cubic-inch displacement; naca-report-931;
1949
- Bollinger, Lowell M
Williams, David T; Effect
of Reynolds number in turbulent-flow range on flame speeds of bunsen burner
flames; naca-report-932; 1949
- Grey, Ralph E Wilsted,
H Dean; Performance of
conical jet nozzles in terms of flow and velocity coefficients;
naca-report-933; 1949
- Hoff, N J Libby, Paul
A; Recommendations
for numerical solution of reinforced-panel and fuselage-ring problems;
naca-report-934; 1949
- Stanitz, John D; Two-dimensional
compressible flow in turbomachines with conic flow surfaces;
naca-report-935; 1949
- Brown, W Byron
Bradshaw, Guy R; Design
and performance of family of diffusing scrolls with mixed-flow impeller and
vaneless diffuser; naca-report-936; 1949
- Turner, L Richard
Bogart, Donald; Constant-pressure
combustion charts including effects of diluent addition; naca-report-937;
1949
- Cahill, Jones F; Summary of
section data on trailing-edge high-lift devices; naca-report-938;
1949
- Tucker, Warren A
Nelson, Robert L; Theoretical
characteristics in supersonic flow of two types of control surfaces on
triangular wings; naca-report-939; 1949
- Dryden, Hugh L Abbott,
Ira H; The
design of low-turbulence wind tunnels; naca-report-940; 1949
- Weil, Joseph Sleeman,
William C , Jr; Prediction
of the effects of propeller operation on the static longitudinal stability of
single-engine tractor monoplanes with flaps retracted; naca-report-941;
1949
- Sivells, James C
Spooner, Stanley H; Investigation
in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210
airfoil sections with various type flaps; naca-report-942; 1949
- Sternfield, Leonard
Gates, Ordway B , Jr; A
simplified method for the determination and analysis of the
neutral-lateral-oscillatory-stability boundary; naca-report-943;
1949
- Stalder, Jackson R
Jukoff, David; Heat
transfer to bodies traveling at high speed in the upper atmosphere;
naca-report-944; 1949
- Heaslet, Max A Lomax,
Harvard; Two-dimensional
unsteady lift problems in supersonic flight; naca-report-945; 1949
- Handelman, G H Prager,
W; Plastic
buckling of a rectangular plate under edge thrusts; naca-report-946;
1949
- Graham, Donald J; The development
of cambered airfoil sections having favorable lift characteristics at
supercritical Mach numbers; naca-report-947; 1949
- Kauffman, William M
Liddell, Charles J , Jr Smith, Allan Van Dyke, Rudolph D , Jr; An
apparatus for varying effective dihedral in flight with application to a study
of tolerable dihedral on a conventional fighter airplane; naca-report-948;
1949
- Schubauer, G B
Spangenberg, W G; Effect
of screens in wide-angle diffusers; naca-report-949; 1949
- Nichols, Mark R Keith,
Arvid L , Jr; Investigation
of a systematic group of NACA 1-series cowlings with and without spinners;
naca-report-950; 1949
- Tsu, Tsung-Chi
(Massachusetts Institute of Technology); Theory
of the inlet and exhaust processes of internal-combustion engines;
naca-tn-1446; 1949
- Boelter, L M K
(University of California) Poppendiek, H (University of California) Young, G
(University of California) Andersen, J R (University of California); An
investigation of aircraft heaters XXX : nocturnal irradiation as a function of
altitude and its use in determination of heat requirements of aircraft;
naca-tn-1454; 1949
- Boelter, L M K
(University of California) Guibert, A G (University of California) Romie, F E
(University of California) Sanders, V D (University of California) Rademacher,
J M (University of California); An
investigation of aircraft heaters XXXI : summary of laboratory testing of
several exhaust-gas and air heat exchangers; naca-tn-1455; July
1949
- Niles, Alfred S
(Stanford University); Overbalancing
in residual-liquidation computations; naca-tn-1457; February 1949
- Schuette, E H (The Dow
Chemical Company); Observations
on the maximum average stress of flat plates buckled in edge compression;
naca-tn-1625; February 1949
- Heimerl, George J
Roberts, William M; Determination
of plate compressive strengths at elevated temperatures; naca-tn-1806;
February 1949
- Pride, Richard A
Heimerl, George J; Plastic
buckling of simply supported compressed plates; naca-tn-1817; April
1949
- Levin, L Ross Sandlin,
Charles W , Jr; Strength
analysis of stiffened thick beam webs; naca-tn-1820; March 1949
- Seide, Paul Stowell,
Elbridge Z; Elastic and
plastic buckling of simply supported metalite type sandwich plates in
compression; naca-tn-1822; February 1949
- Hildebrand, F B
(Massachusetts Institute of Technology) Reissner, E (Massachusetts Institute
of Technology) Thomas, G B (Massachusetts Institute of Technology.); Notes
on the foundations of the theory of small displacements of orthotropic
shells; naca-tn-1833; March 1949
- Goodman, Alex Fisher,
Lewis R; Investigation
at low speeds of the effect of aspect ratio and sweep on rolling stability
derivatives of untapered wings; naca-tn-1835; March 1949
- Runyan, Harry L
Watkins, Charles E; Flutter
of a uniform wing with an arbitrarily placed mass according to a
differential-equation analysis and a comparison with experiment;
naca-tn-1848; March 1949
- Seide, Paul; Compressive
buckling of flat rectangular metalite type sandwich plates with simply
supported loaded edges and clamped unloaded edges; naca-tn-1886; May
1949
- Marin, Joseph
(Pennsylvania State College) Shelson, William (Pennsylvania State College); Biaxial fatigue
strength of 24S-T aluminum alloy; naca-tn-1889; May 1949
- Nikolsky, A A
(Princeton University) Seckel, Edward (Princeton University); An
analytical study of the steady vertical descent in autorotation of
single-rotor helicopters; naca-tn-1906; June 1949
- Moeckel, W E; Approximate
method for predicting form and location of detached shock waves ahead of plane
or axially symmetric bodies; naca-tn-1921; July 1949
- Fischel, Jack Watson,
James M; Investigation
of spoiler ailerons for use as speed brakes or glide-path controls on two NACA
65-Series wings equipped with full-span slotted flaps; naca-tn-1933;
August 1949
- Stowell, Elbridge Z
Pride, Richard A; Plastic
buckling of extruded composite sections in compression; naca-tn-1971;
October 1949
- Stein, Manuel Yaeger,
David J; Critical shear
stress of a curved rectangular panel with a central stiffener;
naca-tn-1972; October 1949
- Stein, Manuel Sanders,
Lyell Crate, Harold; Critical
stress of ring-stiffened cylinders in torsion; naca-tn-1981; November
1949
- Schaefer, Raymond F
Smith, Hamilton A; Aerodynamic
characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers
from 1.8 x 10(exp 6) to 11.0 x 10(exp 6).; naca-tn-1998; December
1949
- (Author(s) Not
Available); Summary of the
availability and performance problems of high octane number fuels;
naca-rm-9d13; April 15, 1949
- W. Kruger; On
Wind Tunnel Tests and Computations Concerning the Problem of Shrouded
Propellers; naca-tm-1202; February 1949
- Mccormack, Gerald M
Walling, Walter C; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
investigation of a large-scale model at low speed; naca-rm-a8d02; January
21, 1949
- Perkins, Edward W
Canning, Thomas N; Investigation
of downwash and wake characteristics at a Mach number of 1.53 I : rectangular
wing; naca-rm-a8l16; March 1949
- Christiani, R Duane
Randall, Lauros M; A
preliminary experimental investigation of a submerged cascade inlet;
naca-rm-a9a24; March 25, 1949
- Perkins, Edward W
Canning, Thomas N; Investigation
of downwash and wake characteristics at a Mach number of 1.53 II : triangular
wing; naca-rm-a9d20; June 06, 1949
- Frick, Charles W Olson,
Robert N; Flow studies in
the asymmetric adjustable nozzle of the Ames 6-by 6-foot supersonic wind
tunnel; naca-rm-a9e24; September 15, 1949
- Mossman, Emmet A; A comparison of
two submerged inlets at subsonic and transonic speeds; naca-rm-a9f16;
September 15, 1949
- Martin, Norman J
Holzhauser, Curt A; An
experimental investigation at large scale of single and twin NACA submerged
side intakes at several angles of sideslip; naca-rm-a9f20; August
1949
- Polentz, Perry P; Comparison of
the aerodynamic characteristics of the NACA 0010 and 0010-64 airfoil sections
at high subsonic Mach numbers; naca-rm-a9g19; October 07, 1949
- Nitzberg, Gerald E
Crandall, Stewart M Polentz, Perry P; A
preliminary investigation of the usefulness of camber in obtaining favorable
airfoil-section drag characteristics at supercritical speeds;
naca-rm-a9g20; October 07, 1949
- Tinling, Bruce E
Dickson, Jerald K; Tests
of a model horizontal tail of aspect ratio 4.5 in the Ames 12-foot pressure
wing tunnel II : elevator hinge line normal to the plane of symmetry;
naca-rm-a9h11a; October 17, 1949
- Jones, J Lloyd Demele,
Fred A; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
effects at subsonic speeds of a constant-chord elevon on a wing cambered and
twisted for a uniform load at a lift coefficient of 0.25; naca-rm-a9i27;
December 05, 1949
- Rolls, L Stewart; The effects of
scale and test technique on the validity of small-scale measurements of the
aerodynamic characteristics of a wing with the leading edge swept back 63
degrees; naca-rm-a9j06; December 09, 1949
- Johnsen, Irving A
Wright, Linwood C Hartmann, Melvin J; Performance
of 24-inch supersonic axial-flow compressor in air II : performance of
compressor rotor at equivalent tip speeds from 800 to 1765 feet per
second; naca-rm-e8g01; January 21, 1949
- English, Robert E
Mccready, Robert J Mccready, John S; Some
effects of stator cone angle and blade-tip leakage on 40 percent reaction
turbine having rotor-blade caps; naca-rm-e8i21; March 23, 1949
- Meyer, Andre J , Jr
Calvert, Howard F; Vibration
survey of blades in 10-stage axial-flow compressor I : static
investigation; naca-rm-e8j22; January 31, 1949
- Meyer, Andre J , Jr
Calvert, Howard F; Vibration
survey of blades in 10-stage axial-flow compressor II : dynamic
investigation; naca-rm-e8j22a; January 31, 1949
- Meyer, Andre J , Jr
Calvert, Howard F; Vibration
survey of blades in 10-stage axial-flow compressor III : preliminary engine
investigation; naca-rm-e8j22b; January 31, 1949
- Jonash, Edmund R Wear,
Jerrold D; Carbon
deposition of 19 fuels in an annular turbojet combustor; naca-rm-e8k22;
February 03, 1949
- Armstrong, J C Wilsted,
H D; Comparison of
performance of AN-F-58 and AN-F-32 fuels in J33-A-23 turbojet engine;
naca-rm-e8k24; June 02, 1949
- Jagger, James M Mirels,
Harold; Experimental
pressure distributions over wing tips at Mach number 1.9 I : wing tip with
subsonic leading edge; naca-rm-e8k26; January 27, 1949
- Acker, Loren W
Kleinknecht, Kenneth S; Comparison
of flight performance of AN-F-58 and AN-F-32 fuels in J35 turbojet engine;
naca-rm-e8l02; April 07, 1949
- Tauschek, Max J Sather,
Bernard I Biermann, Arnold E; An
analysis of a highly compounded two-stroke-cycle compression-ignition
engine; naca-rm-e8l09; April 04, 1949
- Wright, Linwood C
Klapproth, John F; Performance
of supersonic axial-flow compressors based on one-dimensional analysis;
naca-rm-e8l10; March 25, 1949
- Dowman, Harry W
Younger, George G; Comparison
of performance of AN-F-58 fuel and gasoline in J34-WE-22 turbojet engine;
naca-rm-e8l10a; April 07, 1949
- Dupree, D T Nussdorfer,
T J Sterbentz, W H; Altitude-wind-tunnel
investigation of various can-type burners in Bumblebee 18-inch ram jet;
naca-rm-e8l20; March 16, 1949
- Stricker, Edward G
Rayle, Warren D; Altitude
performance of AN-F-58 fuels in J35-C-3 single combustor; naca-rm-e8l20a;
June 14, 1949
- Dittrich, Ralph, T
Jackson, Joseph L; Altitude
performance of AN-F-58 fuels in J33-A-21 single combustor; naca-rm-e8l24;
April 08, 1949
- Foster, Hampton H
Tauschek, Max J Schuricht, F Ralph; Experimental
study of loop-scavenged compression-ignition cylinder for gas-generator
use; naca-rm-e8l30; April 04, 1949
- Sather, Bernard I
Tauschek, Max J; Study
of compressor systems for a gas-generator engine; naca-rm-e9a28; April 13,
1949
- Huppert, M C Nettles, J
C; Performance of
J33 turbojet engine with shaft-power extraction III : turbine performance;
naca-rm-e9b01; June 06, 1949
- Lundin, Bruce T; Investigation
of several clamshell variable-area exhaust nozzles for turbojet engines;
naca-rm-e9b02; May 26, 1949
- Dietz, Robert O , Jr
Krebs, Richard P; Effect
of hot-gas bleedback ice prevention on performance of a turbojet engine with
fixed-area tail-pipe nozzle; naca-rm-e9b23; May 16, 1949
- English, Robert E
Hauser, Cavour H; Turbine-rotor-blade
designs based on one-dimensional-flow theory I : performance of single-stage
turbine having 40-percent reaction; naca-rm-e9c15; June 10, 1949
- Callaghan, Edmund E
Ruggeri, Robert S; Experimental
investigation of hot-gas bleedback for ice protection of turbojet engines II :
nacelle with long straight air inlet; naca-rm-e9c16; May 26, 1949
- Perkins, Porter J , Jr
Millenson, Morton B; An
electric thrust meter suitable for flight investigation of propellers;
naca-rm-e9c17; May 09, 1949
- Lietzke, A F
Henneberry, Hugh M; Evaluation
of piston-type gas-generator engine for subsonic transport operation.;
naca-rm-e9d01; July 15, 1949
- Wear, Jerrold D
Douglass, Howard W; Carbon
deposition from AN-F-58 fuels in a J33 single combustor; naca-rm-e9d06;
June 24, 1949
- Dallas, Thomas
Ellisman, C; Analysis and
preliminary investigation of eddy-current heating for icing protection of
axial-flow-compressor blades; naca-rm-e9e06; August 08, 1949
- Ruggeri, Robert S
Callaghan, Edmund E; Experimental
investigation of hot-gas bleedback for ice protection of turbojet engines III
: nacelle with short straight air inlet; naca-rm-e9e12; August 04,
1949
- Burtt, Jack R; Investigation
of performance of typical inlet stage of multistage axial-flow compressor;
naca-rm-e9e13; July 18, 1949
- Wilsted, H D
Huddleston, S C Ellis, C W; Effect
of temperature on performance of several ejector configurations;
naca-rm-e9e16; June 13, 1949
- Swett, Clyde C , Jr; Spark ignition
of flowing gases I : energies to ignite propane-air mixtures in pressure range
of 2 to 4 inches mercury absolute; naca-rm-e9e17; August 04, 1949
- Ordin, Paul M Miller,
Riley O; Experimental
performance of chlorine trifluoride-hydrazine propellant combination in
100-pound-thrust rocket engine; naca-rm-e9f01; August 15, 1949
- Male, Donald W
Cervenka, Adolph J; Design
factors for 4- by 8-inch ram-jet combustor; naca-rm-e9f09; August 11,
1949
- Wilterdink, P I; Experimental
investigation of rim cracking in disks subjected to high temperature
gradients; naca-rm-e9f16; September 1949
- Baker, Sol Perchonok,
Eugene; Investigation
of internal regenerative fuel-heating system for 20-inch ram jet;
naca-rm-e9f20; September 1949
- Maxwell, W A; Properties
of certain intermetallics as related to elevated-temperature applications I :
molybdenum disilicide; naca-rm-e9g01; October 06, 1949
- Weiss, Solomon Pesman,
Gerard J; Bibliography of
classified aircraft-fire literature; naca-rm-e9h03a; November 18,
1949
- Connors, James F
Schroeder, Albert H; Experimental
investigation of pressure fluctuations in 3.6 inch ram jet at Mach number
1.92; naca-rm-e9h12; October 13, 1949
- Cummings, J L Baughman,
L E; Downwash in
vortex region behind trapezoidal-wing tip at Mach number 1.91;
naca-rm-e9h15; November 10, 1949
- Ross, Albert O Huppert,
Merle C; Analytical
determination of effect of water injection on power output of
turbine-propeller engine; naca-rm-e9h17; November 03, 1949
- Morgan, W C Kemp, R H
Manson, S S; Vibration of
loosely mounted turbine blades during service operation of a turbojet engine
with centrifugal compressor and straight-flow combustion chambers;
naca-rm-e9i07; November 03, 1949
- Mirels, Harold Jagger,
James M; Experimental
pressure distributions over wing tips at Mach number 1.9 II : wing tip with
subsonic trailing edge; naca-rm-e9i22a; December 21, 1949
- Schade, Robert O; Langley
free-flight-tunnel investigation of the automatic lateral stability
characteristics of a model equipped with a gyro stabilizing unit that provided
either flicker-type or hunting control; naca-rm-l8k04; January 11,
1949
- Mitchell, Jesse L
Gillis, Clarence, L; Flight
tests at transonic and supersonic speeds of an airplane-like configuration
with thin straight sharp-edge wings and tail surfaces; naca-rm-l8k04a;
January 05, 1949
- Rainey, Robert W
Boatright, William B; Hinge-moment
measurements of a wing with leading-edge and trailing-edge flaps at a Mach
number of 1.93; naca-rm-l8k12a; January 14, 1949
- Mitchell, Meade H , Jr
Conner, D William; Control
effectiveness and hinge-moment measurements at a Mach number of 1.9 of a nose
flap and trailing-edge flap on a highly tapered low- aspect-ratio wing;
naca-rm-l8k17a; January 10, 1949
- Sandahl, Carl A; Free-flight
investigation at transonic and supersonic speeds of the rolling effectiveness
of several aileron configurations on a tapered wing having 42.7 degrees
sweepback; naca-rm-l8k23; January 11, 1949
- Pendley, Robert E
Smith, Norman F; An
investigation of the characteristics of three NACA 1-series nose inlets at
subcritical and supercritical Mach numbers; naca-rm-l8l06; January 13,
1949
- Alexander, Sidney R; Flight
investigations at low supersonic speeds to determine the effectiveness of
cones and a wedge in reducing the drag of round-nose bodies and airfoils;
naca-rm-l8l07a; March 03, 1949
- Goin, Kennith L; Investigation
at a Mach number of 1.9 and a Reynolds number of 2.2 x 10(exp 6) of several
flap-type lateral-control devices on a wing having 42.7 degrees sweepback of
the leading edge; naca-rm-l9a18a; March 11, 1949
- Teitelbaum, Jerome M
Seaberg, Ernest C; An
experimental investigation of a gyro-actuated roll control system installed in
a subsonic test vehicle; naca-rm-l9b24a; April 20, 1949
- Lauten, William T
Barmby, J G; Continuation of
wing flutter investigation in the transonic range and presentation of a
limited summary of flutter data; naca-rm-l9b25b; April 21, 1949
- Schwartz, Ira R; Investigations
of an annular diffuser-fan combination handling rotating flow;
naca-rm-l9b28; April 25, 1949
- Donaldson, Coleman Dup;
An
approximate method for estimating the incompressible laminar boundary-layer
characteristics on a flat plate in slipping flow; naca-rm-l9c02; May 02,
1949
- Sandahl, Carl A Bland,
William M , Jr Strass, H Kurt; Effects
of some airfoil-section variations on wing-aileron rolling effectiveness and
drag as determined in free flight at transonic and supersonic speeds;
naca-rm-l9d12; July 22, 1949
- Ritchie, Virgil S; Effects of
certain flow nonuniformities on lift, drag, and pitching moment for a
transonic-airplane model investigated at a Mach number of 1.2 in a nozzle of
circular cross section; naca-rm-l9e20a; August 31, 1949
- Cooper, Morton Smith,
Norman F Kainer, Julian H; A
pressure-distribution investigation of a supersonic aircraft fuselage and
calibration of the Mach number 1.59 nozzle of the Langley 4- by 4- foot
supersonic tunnel; naca-rm-l9e27a; July 29, 1949
- Katz, Ellis R; Flight
investigation at high-subsonic, transonic, and supersonic speeds to determine
zero-lift drag of bodies of revolution having fineness ratio of 6.04 and
varying positions of maximum diameter; naca-rm-l9f02; August 31,
1949
- Conner, D William May,
Ellery B , Jr; Control
effectiveness load and hinge-moment characteristics of a tip control surface
on a delta wing at a Mach number of 1.9; naca-rm-l9h05; October 07,
1949
- Conner, D William May,
Ellery B , Jr; Control
effectiveness and hinge-moment characteristics of a tip control surface on a
low-aspect-ratio pointed wing at a Mach number of 1.9; naca-rm-l9h26;
October 05, 1949
- Katz, Ellis; Flight
investigation from high subsonic to supersonic speeds to determine the
zero-lift drag of a transonic research vehicle having wings of 45 degree
sweepback, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil
sections; naca-rm-l9h30; October 27, 1949
- Lattanzi, Bernardino.,
Bellante, Erno.; Wind-tunnel
tests on various types of dive brakes mounted in proximity of the leading edge
of the wing; naca-tm-1161; 1949
- Filzek, B.; Investigations
on the stability, oscillation, and stress conditions of airplanes with tab
control. Second partial report : application of the solutions obtained in
the first partial report to tab-controlled airplanes; naca-tm-1198;
1949
- ; Compression
shocks in two-dimensional gas flows; naca-tm-1199; 1949
- Dupleich, Paul.; Rotation in
free fall of rectangular wings of elongated shape; naca-tm-1201;
1949
- Iglisch, Rudolf; Exact
calculation of laminar boundary layer in longitudinal flow over a flat plate
with homogeneous suction; naca-tm-1205; 1949
- Ilyushin, A. A.; The theory of
plasticity in the case of simple loading accompanied by strain-hardening;
naca-tm-1207; 1949
- Falkovich, S. V.; On the theory
of the Laval nozzle; naca-tm-1212; 1949
- Taganov, G.I.; Gas
motion in a local supersonic region and conditions of potential-flow
breakdown; naca-tm-1213; 1949
- Rothstein, W.; Flow
pattern in a converging-divirging nozzle; naca-tm-1215; 1949
- ; An
approximate method for calculation of the laminar boundary layer with suction
for bodies of arbitrary shape; naca-tm-1216; 1949
- Schlichting, H.; Lecture series
"Boundary layer theory" - part I : Laminar flows; naca-tm-1217;
1949
- Schlichting, H.; Lecture series
"Boundary layer theory" - part II : Turbulent flows; naca-tm-1218;
1949
- Kempf,
Gunther|uDeutsche Akademie der Luftfahrtforschung.; Moments
of cambered round bodies; naca-tm-1227; 1949
- Schroder, K.; Behavior
of the laminar boundary layer for periodically oscillating pressure
variation; naca-tm-1228; 1949
- ; Heat
transmission in the boundary layer; naca-tm-1229; 1949
- ; Effect
of acceleration of elongated bodies of revolution upon the resistance in a
compressible flow; naca-tm-1230; 1949
- Prandtl, L.; Report
on investigation of developed turbulence; naca-tm-1231; 1949
- Lipkes, Y.M.; Investigation
of conditions of titanium carbonization - IV; naca-tm-1235; 1949
- ; A
class of de Laval nozzles; naca-tm-1236; 1949
- ; Two-dimensional
motion of a gas at large supersonic velocities; naca-tm-1239; 1949
- Gothert, B.; Airfoil
measurements in the DVL high-speed wind tunnel (2.7-meter diameter);
naca-tm-1240; 1949
- ; Lift
force of an arrow-shaped wing; naca-tm-1245; 1949
- Arnoldi, Walter E.; Response of a
rotating propeller to aerodynamic excitation; naca-rm-8i07; 1949
- Jones, Alun R., Lewis,
William; A
review of instruments developed for the measurement of the meteorological
factors conducive to aircraft icing; naca-rm-a9c09; 1949
- Cook, William P., Koch,
Richard G.; Altitude
performance of AN-F-58 fuels in British Rolls-royce nene singe combustor;
naca-rm-e9d08; 1949
- Sams, Eldon W., Desmon,
Leland G.; Heat transfer
from high-temperature surfaces to fluids III - correlation of heat-transfer
data for air flowing in silicon carbide tube with rounded entrance, inside
diameter of 3/4 inch, and effective length of 12 inches; naca-rm-e9d12;
1949
- Hart, Roger G., Katz,
Ellis R.; Flight
investigations at high-subsonic, transonic, and supersonic speeds to determine
zero-lift drag of fin-stabilized bodies of revolution having fineness ratios
of 12.5, 8.91, and 6.04 and varying positions of maximum diameter;
naca-rm-l9i30; 1949
- Vlasov, V. S.; Some
new problems on shells and thin structures; naca-tm-1204; 1949
- Ginzel, F.; Calculation
of counterrotating propellers; naca-tm-1208; 1949
- Eckert, E.,
Vietinghoff-Scheel, K. V.; Experimental
study of flow past turbine blades; naca-tm-1209; 1949
- Vlasov, V. Z.; Computation
of thin-walled prismatic shells; naca-tm-1234; 1949
- Sottorf, W.; Systematic
model researches on the stability limits of the DVL series of float
designs; naca-tm-1254; 1949
- Jones, Alun R., Lewis,
William.; Recommended
values of meteorological factors to be considered in the design of aircraft
ice-prevention equipment; naca-tn-1855; 1949
- Guibert, A. G.,
Robbins, W. M., Janssen, E.; Determination
of rate, area, and distribution of impingement of water drops on various
airfoils from trajectories obtained on the differential analyzer;
naca-rm-9a05; 1949
- B. Filzek; Investigations
on the Stability, Oscillation, and Stress Conditions of Airplanes with Tab
Control First Partial Report - Derivation of the Equations of Motions and
their General Solutions; naca-tm-1197; 1949
- A. Buske and W. Rolli;
Measurment
of Oil-Film Pressures in Journal Bearings under Constant and Variable
Loads; naca-tm-1200; 1949
- B. Gothert and K.H.
Kawalki; The
Compressible Flow Past Various Plane Profiles Near Sonic Velocity;
naca-tm-1203; 1949
- Gothert and Rober; Systematic
Investigations of the Effects of Plan Form and Gap Between the Fixed Surface
and Control Surface on Simple Flapped Wings; naca-tm-1206; 1949
- G. Ernst and M. Kramer;
Development
of Spoiler Controls for Remote Control of Flying Missiles; naca-tm-1210;
1949
- F. Pfeiffer and W.
Meyer-Koing; The
Characteristics Method Applied to Stationary Two-Dimensional and Rotationally
Symmetrical Gas Flows; naca-tm-1211; 1949
- D. Kuchemann; Jet
Diffusion in Proximity of a Wall; naca-tm-1214; 1949
- P. Hohler; The
Influence of the Application of Power During Spin Recovery of Multiengine
Airplanes; naca-tm-1219; 1949
- M. Kohler and W. Mautz;
Pressure-Distribution
Measurements of the Tail Surface of a Rotating Model of the Design
BFW-M31; naca-tm-1220; 1949
- P. Hohler and I. V.
Koppen; Experimental
Flights for Testing of a Reactor as an Expedient for the Termination of
Dangerous Spins; naca-tm-1221; 1949
- J. Meixner; Lame's
Wave Functions of the Ellipsoid of Revolotion; naca-tm-1224; 1949
- Lange and Wacke; Test Report on
Three- and Six-Component Measurements on a Series of Tapered Wings of Small
Aspect Ratio (Partial Report: Trapezoidal Wing); naca-tm-1225; 1949
- R. Buschner; On
the Installation of Jet Engine Nacelles on a Wing. Fourth Partial Report:
Pressure-Distribution Measurments on a Sweptback Wing with Jet Engine
Nacelle; naca-tm-1226; 1949
- C. Schmieden and K. H.
Kawalki; Contribution to
the Problem of Flow at High Speed; naca-tm-1233; 1949
- I. Flugge and K.
Klotter; On
the Motions of an Oscillating System Under the Influence of Flip-Flop
Controls; naca-tm-1237; 1949
- R. Honl; Two-Dimensional
Wing Theory in the Supersonic Range; naca-tm-1238; 1949
- Dr. W. Tollmien; Theory of
Characteristics; naca-tm-1242; 1949
- Manfred Schafer and W.
Tollmien; Two-Dimensional
Potential Flows; naca-tm-1243; 1949
- Manfred Schafer and W.
Tollmien; Rotationally
Symmetric Potential Flows; naca-tm-1244; 1949
- W. Sottorf; Landing
Procedure in Model Ditching Tests of Bf 109; naca-tm-1247; 1949
- K. L. Zeyen; Susceptibility
to Welding Cracking, Welding Sensitivity, Susceptibility to Welding Seam
Cracking, and Test Methods for these Failures; naca-tm-1249; 1949
- Th. Zobel; Flow
Measurements by Means of Light Interference; naca-tm-1253; 1949
- Manuel Stein, J. Lyell
Snaders, Jr., Harold Crate; Critical
stress of ring-stiffened cylinders in torsion; naca-report-989;
1950
- Stanley Corrsin,
Mahinder S. Uberoi; Spectrums
and diffusion in a round turbulent jet; naca-tn-2124; Jul 1950
- H. Kurt Strass, E. M.
Fields, E. D. Schult; Free-flight
investigation at transonic and supersonic speeds of the rolling effectiveness
of a partial-span aileron on an inversely tapered sweptback wing;
naca-rm-l50b08; May 1950
- William G. Lidman, H.
J. Hamjian; Properties of a
boron carbide-iron ceramal; naca-tn-2050; Mar 1950
- Norman J. Martin, Curt
A. Holzhauser; Analysis
of factors influencing the stability characteristics of symmetrical
twin-intake Air-induction systems; naca-tn-2049; Mar 1950
- Ira P. Jones, Walter J.
Klinar; Spin-tunnel
investigation to determine the effect on spin recoveries of reducing the
opening shock load of spin-recovery parachutes; naca-tn-2051; Mar
1950
- Charles A. Hoffman,
Charles Yaker; Effects
of an aging treatment on life of small cast vitallium gas-turbine blades;
naca-tn-2052; Mar 1950
- Reece V. Hensley, Frank
E. Rom, Stanley L. Koutz; Effect
of heat and power extraction on turbojet-engine performance I : analytical
method of performance evaluation with compressor-outlet air bleed;
naca-tn-2053; Mar 1950
- Vera Huckel, Barbara J.
Durling; Tables of
wing-aileron coefficients of oscillating air forces for two-dimensional
supersonic flow; naca-tn-2055; Mar 1950
- Lipman Bers; Velocity
distribution on wing sections of arbitrary shape in compressible potential
flow III : circulatory flows obeying the simplified density-speed
relation; naca-tn-2056; Mar 1950
- Abe Gilbart, Daniel
Resch; A
method of computing subsonic flows around given airfoils; naca-tn-2057;
Mar 1950
- Lipman Bers; On
the continuation of a potential gas flow across the sonic line;
naca-tn-2058; Apr 1950
- Harold B. Finger; Method of
experimentally determining radial distributions of velocity through axial-flow
compressor; naca-tn-2059; Apr 1950
- John C. Houbolt; A recurrence
matrix solution for the dynamic response of aircraft in gusts;
naca-tn-2060; Mar 1950
- Paul W. Harper, Roy E.
Flanigan; The effect of
rate of change of angle of attack on the maximum lift of a small model;
naca-tn-2061; Mar 1950
- Anshal I Neihouse,
Philip W. Pepoon; Dynamic
similitude between a model and a full-scale body for model investigation at
full-scale Mach number; naca-tn-2062; Mar 1950
- Charles E. Watkins; Effect of
aspect ratio on the air forces and moments of harmonically oscillating thin
rectangular wings in supersonic potential flow; naca-tn-2064; Apr
1950
- Charles Loewner; A
transformation theory of the partial differential equations of gas
dynamics; naca-tn-2065; Apr 1950
- Leonard K. Tower, Henry
E. Alquist; Correlation of
effects of fuel-air ratio, compression ratio, and inlet-air temperature on
knock limits of aviation fuels; naca-tn-2066; Apr 1950
- Chung-Hua Wu, John T.
Sinnette, Robert E. Forrette; Theoretical
effect of inlet hub-tip-radius ratio and design specific mass flow on design
performance of axial-flow compressors; naca-tn-2068; Apr 1950
- I. L. Drell, J. R.
Branstetter; Knock-limited
performance of fuel blends containing ethers; naca-tn-2070; Apr
1950
- Robert E. English,
William W. Wachtl; Charts
of thermodynamic properties of air and combustion products from 300 degrees to
3500 degrees R; naca-tn-2071; Apr 1950
- I. M. K. Boelter, R.
Leasure, F. E. Romie; An
investigation of aircraft heaters XXXIII : experimental determination of
thermal and hydrodynamical behavior of air flowing along finned plates;
naca-tn-2072; Mar 1950
- Elbridge Z. Stowell; Stress and
strain concentration at a circular hole in an infinite plate;
naca-tn-2073; Apr 1950
- Hamilton A. Smith,
Raymond F. Schaefer; Aerodynamic
characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of
three airfoil sections formed by cutting off various amounts from the rear
portion of the NACA 0012 airfoil section; naca-tn-2074; Apr 1950
- Robert O. Schade; Free-flight-tunnel
investigation of dynamic longitudinal stability as influenced by the static
stability measured in wind-tunnel force tests under conditions of constant
thrust and constant power; naca-tn-2075; Apr 1950
- Robert L. Johnson,
Douglas Godfrey, Edmond E. Bisson; Friction
of surface films formed by decomposition of common lubricants of several
types; naca-tn-2076; Apr 1950
- Jackson R. Stalder,
Morris W. Rubesin, Thorval Tendeland; A
determination of the laminar-, transitional-, and turbulent-boundary-layer
temperature-recovery factors on a flat plate in supersonic flow;
naca-tn-2077; Jun 1950
- Henry A. Pearson,
William A. McGowan, James J. Donegan; Horizontal
tail loads in maneuvering flight; naca-tn-2078; Apr 1950
- Leo L. Beranek, Fred S.
Elwell, John P. Roberts; Experiments
in external noise reduction of light airplanes; naca-tn-2079; May
1950
- Harold S. Johnson, John
R. Hagerman; Wind-tunnel
investigation at low speed of an unswept untapered semispan wing of aspect
ratio 3.13 equipped with various 25-percent-chord plain flaps;
naca-tn-2080; Apr 1950
- Paul H. Wise, Kasper T.
Serijan, Irving A. Goodman; Correlation
of physical properties with molecular structure for dicyclic hydrocarbons : I
-2-n-alkylbiphenyl, 1,1-diphenylalkane,a,w-diphenylalkane;
1,1-dicyclohexylalkane, and a,w-dicyclohexylalkane series; naca-tn-2081;
May 1950
- K. O. Bogardus, G. W.
Stickley, F. M. Howell; A
review of information on the mechanical properties of aluminum alloys at low
temperatures; naca-tn-2082; May 1950
- Bruce T. Lundin; Theoretical
analysis of various thrust-augmentation cycles for turbojet engines;
naca-tn-2083; May 1950
- W. J. Kommers; Strength
properties of rayon-mat honeycomb core materials; naca-tn-2084; Apr
1950
- James A. Miller; Stress-strain
and elongation graphs for aluminum-alloy 75S-T6 sheet; naca-tn-2085; Apr
1950
- Paul J. Carpenter,
Russell S. Paulnock; Hovering
and low-speed performance and control characteristics of an
aerodynamic-servocontrolled helicopter rotor system as determined on the
Langley helicopter tower; naca-tn-2086; May 1950
- Richard Scherrer,
Forrest E. Gowan; Comparison
of theoretical and experimental heat transfer on a cooled 20 degrees cone with
a laminar boundary layer at a Mach number of 2.02; naca-tn-2087; May
1950
- Bernard Lubarsky; Performance and
load-range characteristics of turbojet engine in transonic speed range;
naca-tn-2088; May 1950
- Powell M. Lovell, Jr.,
Paul P. Stassi; A
comparison of the lateral controllability with flap and plug ailerons on a
sweptback-wing model; naca-tn-2089; May 1950
- Walter G. Vincenti; Comparison
between theory and experiment for wings at supersonic speeds;
naca-tn-2100; Jun 1950
- Arthur G. Hansen, Peggy
L. Yohner; A
numerical procedure for designing cascade blades with prescribed velocity
distribution in incompressible potential flow; naca-tn-2101; Jun
1950
- George Fryburg; Review of
literature pertinent to fire-extinguishing agents and to basic mechanisms
involved in their action; naca-tn-2102; May 1950
- Cloyce E. Matheny; Maximum
pitching angular accelerations of airplanes measured in flight;
naca-tn-2103; May 1950
- H. W. Eickner; Evaluation
of several adhesives and processes for bonding sandwich constructions of
aluminum facings on paper honeycomb core; naca-tn-2106; May 1950
- G. W. Englert, A. O.
Ross; Investigation
of first stage of two-stage turbine designed for free-vortex flow;
naca-tn-2107; Jun 1950
- G. Allen; Analytical
method for determining transmission and absorption of time-dependent radiation
through thick absorbers III : absorber with radioactive daughter products;
naca-tn-2108; Jun 1950
- Harold Shames, Seymour
C. Himmel, Darnold Blivas; Frequency
response of positive-displacement variable stroke fuel pump; naca-tn-2109;
Jun 1950
- Robert E. Blue; Interferometer
corrections and measurements of laminar boundary layers in supersonic
stream; naca-tn-2110; Jun 1950
- Robert F. Smiley; A study of
water pressure distribution during landings with special reference to a
prismatic model having a heavy beam loading and a 30 degree angle of dead
rise; naca-tn-2111; Jul 1950
- Albert L. Braslow,
Fioravante Visconti; Further
experimental studies of area suction for the control of the laminar boundary
layer on a porous bronze NACA 64A010 airfoil; naca-tn-2112; May
1950
- Vearl N. Huff, Virginia
E. Morrell; General method
for computation of equilibrium composition and temperature of chemical
reactions; naca-tn-2113; Jun 1950
- Sidney M. Harmon,
Isabella Jeffreys; Theoretical
lift and damping in roll of thin wings with arbitrary sweep and taper at
supersonic speeds : supersonic leading and trailing edges; naca-tn-2114;
May 1950
- John R. Jack; Theoretical
wave drags and pressure distributions for axially symmetric open-nose
bodies; naca-tn-2115; Jun 1950
- Vernon H. Gray; Improvements in
heat transfer for anti-icing of gas-heated airfoils with internal fins and
partitions; naca-tn-2126; Jul 1950
- Franklin Moore; Linearized
supersonic axially symmetric flow about open-nosed bodies obtained by use of
stream function; naca-tn-2116; Jun 1950
- Herman H. Lowell; Design and
applications of hot-wire anemometers for steady-state measurements at
transonic and supersonic airspeeds; naca-tn-2117; Jul 1950
- Fred E. Macks, Zolton
N. Nemeth; Investigation
of 75-millimeter-bore cylindrical roller bearings at high speeds;
naca-tn-2128; Jul 1950
- John J. Rebeske, Jr.;
Investigation
of a NACA high-speed optical torquemeter; naca-tn-2118; Jun 1950
- John C. Samuels, B. M.
Gale; Effect
of humidity on performance of turbojet engines; naca-tn-2119; Jun
1950
- Harold V. Soule,
Alexander P. Sabol; Development
and preliminary investigation of a method of obtaining hypersonic aerodynamic
data by firing models through highly cooled gases; naca-tn-2120; Jul
1950
- J. G. Barmby, H. J.
Cunningham, I. E. Garrick; Study
of effects of sweep on the flutter of cantilever wings; naca-tn-2121; Jun
1950
- Kenneth Margolis; Theoretical
calculations of the lateral force and yawing moment due to rolling at
supersonic speeds for sweptback tapered wings with streamwise tips : subsonic
leading edges; naca-tn-2122; Jun 1950
- John Laufer; Investigation
of turbulent flow in a two-dimensional channel; naca-tn-2123; Jul
1950
- Richard T. Whitcomb; A discussion of
the design of highly swept propeller blades; naca-rm-l50a23; May,
1950
- Robert N. Noyes; Prandtl-Meyer
flow for a diatomic gas of variable specific heat; naca-tn-2125; Jun
1950
- J. U. Jovellanos, E. S.
Taylor, C. F. Taylor; An
investigation of the effect of tetraethyl lead and ethyl nitrite on the
autoignition characteristics of isooctane and triptane; naca-tn-2127; Jun
1950
- Harry E. Murray,
Frederick C. Grant; Method
of calculating the lateral motions of aircraft based on the Laplace
transform; naca-tn-2129; Jul 1950
- William Perl; Calculation
of transonic flows past thin airfoils by integral method; naca-tn-2130;
Jul 1950
- Richard Scherrer; Boundary-layer
transition on a cooled 20 degree cone at Mach numbers of 1.5 and 2.0;
naca-tn-2131; Jul 1950
- Edwin T. Kruszewski,
John C. Houbolt; The
calculation of modes and frequencies of a modified structure from those of the
unmodified structure; naca-tn-2132; Jul 1950
- G. B. Schubauer, P. S.
Klebanoff; Investigation
of separation of the turbulent boundary layer; naca-tn-2133; Aug
1950
- Theodore Berman; Comparison of
model and full-scale spin test results for 60 airplane designs;
naca-tn-2134; Jul 1950
- John C. Martin; The calculation
of downwash behind wings of arbitrary plan form at supersonic speeds;
naca-tn-2135; Jul 1950
- Kenneth B. Amer; Theory of
helicopter damping in pitch or roll and a comparison with flight
measurements; naca-tn-2136; Oct 1950
- Dean R. Chapman; An analysis of
base pressure at supersonic velocities and comparison with experiment;
naca-tn-2137; Jul 1950
- Robert G. Deissler; Analytical and
experimental investigation of adiabatic turbulent flow in smooth tubes;
naca-tn-2138; Jul 1950
- Norris F. Dow, William
A. Hickman; Effect of
variation in rivet diameter and pitch on the average stress at maximum load
for 24S-T3 and 75S-T6 aluminum-alloy, flat, Z-stiffened panels that fail by
local instability; naca-tn-2139; Jul 1950
- John DeYoung; Theoretical
antisymmetric span loading for wings of arbitrary plan form at subsonic
speeds; naca-tn-2140; Jul 1950
- Rudolph C. Haefeli,
Harold Mirels, John L. Cummings; Charts
for estimating downwash behind rectangular, trapezoidal, and triangular wings
at supersonic speeds; naca-tn-2141; Aug 1950
- Robert G. Dorsch, Paul
T. Hacker; Photomicrographic
investigation of spontaneous freezing temperatures of supercooled water
droplets; naca-tn-2142; Jul 1950
- Edmond E. Bisson, Max
A. Swikert, Robert L. Johnson; Effect
of chemical reactivity of lubricant additives on friction and surface welding
at high sliding velocities; naca-tn-2144; Aug 1950
- Harold Mirels; Lift-cancellation
technique in linearized supersonic-wing theory; naca-tn-2145; Aug
1950
- Herbert Spencer Ribner;
On the
effect of subsonic trailing edges on damping in roll and pitch of thin
sweptback wings in a supersonic stream; naca-tn-2146; Aug 1950
- Herbert Spencer Ribner;
Some conical
and quasi-conical flows in linearized supersonic-wind theory;
naca-tn-2147; Aug 1950
- William R. Wimbrow,
Richard Scherrer; Laminar-boundary-layer
heat-transfer characteristics of a body with a pressure gradient at supersonic
speeds; naca-tn-2148; Aug 1950
- Elmer A. Horton,
Stanley Frank Racisz, Nicholas J. Paradiso; Investigation
of boundary-layer control to improve the lift and drag characteristics of the
NACA 65-2 415 airfoil section with double slotted and plain flaps;
naca-tn-2149; Aug 1950
- C. C. Schufflebarger,
Harry C. Mickleboro; Flight
investigation of the effect of transient wing response on measured
accelerations of a modern transport airplane in rough air; naca-tn-2150;
Aug 1950
- Warren A. Tucker,
Robert O. Piland; Estimation
of the damping in roll of supersonic-leading-edge wing-body combinations;
naca-tn-2151; Jul 1950
- Charles Brazer Norris,
L. A. Ringelstetter; Shear
stress distribution along glue line between skin and cap-strip of an aircraft
wing; naca-tn-2152; Jul 1950
- Alfred Gessow; An
analysis of the autorotative performance of a helicopter powered by rotor-tip
jet units; naca-tn-2154; Jul 1950
- Tibor F. Nagey, Cecil
G. Martin; Calculated
engine performance and airplane range for variety of turbine-propeller
engines; naca-tn-2155; Aug 1950
- Sidney M. Harmon, John
C. Martin; Theoretical
calculations of the lateral force and yawing moment due to rolling at
supersonic speeds for sweptback tapered wings with streamwise tips supersonic
leading edges; naca-tn-2156; Jul 1950
- H. E. Grieshaber; Static and
impact strengths of riveted and spot-welded beams of Alclad 14S-T6, Alclad
75S-T6, and various tempers of Alclad 24S aluminum alloy; naca-tn-2157;
Aug 1950
- Neal Tetervin, Chia
Chiao Lin; A
general integral form of the boundary-layer equation for incompressible flow
with an application to the calculation of the separation point of turbulent
boundary layers; naca-tn-2158; Aug 1950
- Carl Kaplan; On
the particular integrals of the Prandtl-Busemann iteration equations for the
flow of a compressible fluid; naca-tn-2159; Aug 1950
- Robert E. Dannenberg;
Measurements
of section characteristics of a 45 degree swept wing spanning a rectangular
low-speed wind tunnel as affected by the tunnel walls; naca-tn-2160; Aug
1950
- Vearl N. Huff, Sanford
Gordon; Tables of
thermodynamic functions for analysis of aircraft-propulsion systems;
naca-tn-2161; Aug 1950
- E. E. Reynolds, James
W. Freeman, Albert Easton White; Investigation
of properties of AISI type 310B alloy sheet at high temperatures;
naca-tn-2162; Aug 1950
- John C. Houbolt,
Elbridge Z. Stowell; Critical
stress of plate columns; naca-tn-2163; Aug 1950
- Vernon G. Ward, Charles
F. Whitcomb, Merwin D. Pearson; An
NACA transonic test section with tapered slots tested at Mach numbers to
1.26; naca-rm-l50b14; Mar 1950
- Joseph T. Hamrick,
Ambrose Ginsburg, Walter M. Osborn; Method
of analysis for compressible flow through mixed-flow centrifugal impellers of
arbitrary design; naca-tn-2165; Aug 1950
- Perry L. Blackshear,
Jr.; Sonic-flow-orifice
temperature probe for high-gas-temperature measurements; naca-tn-2167; Sep
1950
- M. J. Queijo, Walter D.
Wolhart; Experimental
investigation of the effect of vertical-tail size and length of fuselage shape
and length on the static lateral stability characteristics of a model with 45
degree sweptback wing and tail surfaces; naca-tn-2168; Aug 1950
- Harold S. Johnson, John
R. Hageman; Wind-tunnel
investigation at low speed of a 45 degree sweptback untapered semispan wing of
aspect ratio 1.59 equipped with various 25-percent chord plain flaps;
naca-tn-2169; Aug 1950
- Gordon L. Dugger; Effect of
initial mixture temperature on flame speeds and blow-off limits of propane -
air flames; naca-tn-2170; Aug 1950
- Charles Herbert
McLellan, Thomas W. Williams, Mitchel H. Bertram; Investigation
of a two-step nozzle in the Langley 11-inch hypersonic tunnel;
naca-tn-2171; Sep 1950
- Leonard M. Rose, John
M. Altman; Low-speed
investigation of the stalling of a thin, faired, double-wedge airfoil with
nose flap; naca-tn-2172; Aug 1950
- Paul B. Gooderum,
George P. Wood; Density
fields around a sphere at Mach numbers 1.30 and 1.62; naca-tn-2173; Aug
1950
- James L. Amick; Comparison of
the experimental pressure distribution on an NACA 0012 profile at high speeds
with that calculated by the relaxation method; naca-tn-2174; Aug
1950
- William Letko, Donald
R. Riley; Effect of an
unswept wing on the contribution of unswept-tail configuration to the
low-speed static and rolling-stability derivatives of a midwing airplane
model; naca-tn-2175; Aug 1950
- Thomas L. Coleman, Paul
W. J. Schumacher; An
analysis of the normal accelerations and airspeeds of a four-engine airplane
type in postwar commercial transport operations on trans-Pacific and
Caribbean-South American routes; naca-tn-2176; Aug 1950
- George B. McCullough,
William M. Haire; Low-speed
characteristics of four cambered, 10-percent-thick NACA airfoil sections;
naca-tn-2177; Aug 1950
- Arthur M. Trout, Eldon
W. Hall; Method for
determining optimum division of power between jet and propeller for maximum
thrust power of a turbine-propeller engine; naca-tn-2178; Sep 1950
- Seymour Lieblein; Turning-angle
design rules for constant-thickness circular-arc inlet guide vanes in axial
annular flow; naca-tn-2179; Sep 1950
- Douglas Godfrey, Edmond
E. Bisson; Effectiveness
of molybdenum disulfide as a fretting-corrosion inhibitor; naca-tn-2180;
Sep 1950
- Ralph W. Stone, Jr.,
Sanger M. Burk, Jr., William Bihrle, Jr.; The
aerodynamic forces and moments on a one-tenth-scale model of a fighter
airplane in spinning attitudes as measured on a rotary balance in the Langley
20-foot free-spinning tunnel; naca-tn-2181; Sep 1950
- Marcus F. Heidmann; Analysis of
effect of variations in primary variables on time constant and
turbine-inlet-temperature overshoot of turbojet engine; naca-tn-2182; Sep
1950
- Melvin S. Feder,
Richard Hood; Analysis
for control application of dynamic characteristics of turbojet engine with
tail-pipe burning; naca-tn-2183; Sep 1950
- Burt L. Taylor, III,
Frank L. Oppenheimer; Investigation
of frequency-response characteristics of engine speed for a typical
turbine-propeller engine; naca-tn-2184; Sep 1950
- Walter J. Engel; Bonding
investigation of titanium carbide with various elements; naca-tn-2187; Sep
1950
- James P. Peterson; Experimental
investigation of stiffened circular cylinders subjected to combined torsion
and compression; naca-tn-2188; Sep 1950
- Walter F. Lindsey,
William L. Chew; The
development and performance of two small tunnels capable of intermittent
operation at Mach numbers between 0.4 and 4.0; naca-tn-2189; Sep
1950
- H. Kurt Strass; The effect of
spanwise aileron location on the rolling effectiveness of wings with 0 degree
and 45 degree sweep at subsonic, transonic, and supersonic speeds;
naca-rm-l50a27; Apr 1950
- William Perl, Milton M.
Klein; Theoretical
investigation and application of transonic similarity law for two dimensional
flow; naca-tn-2191; Oct 1950
- John C. Roberts, Paul
F. Yaggy; A
survey of the flow at the plane of the propeller of a twin-engine
airplane; naca-tn-2192; Sep 1950
- Robert B. Spooner; Effect of
heat-capacity lag on a variety of turbine-nozzle flow processes;
naca-tn-2193; Oct 1950
- Israel Taback; The
NACA oil-damped V-G recorder; naca-tn-2194; Oct 1950
- Carl J. Stough, William
M. Kauffman; A flight
investigation and analysis of the lateral-oscillation characteristics of an
airplane; naca-tn-2195; Oct 1950
- Ivey H. Reese, Charles
W. Cline; Effect of
heat-capacity lag on the flow through oblique shock waves; naca-tn-2196;
Oct 1950
- Harold J. Walker, Mary
B. Ballantyne; Pressure
distribution and damping in steady pitch at supersonic Mach numbers of flat
swept-back wings having all edges subsonic; naca-tn-2197; Oct 1950
- H. J. Hamjian, William
G. Lidman; Sintering
mechanism between zirconium carbide and columbium; naca-tn-2198; Oct
1950
- Harold S. Johnson, John
R. Hagerman; Wind-tunnel
investigation at low speed of the lateral control characteristics of an
unswept untapered semi-span wing of aspect ratio 3.13 equipped with various
25-percent-chord plain ailerons; naca-tn-2199; Oct 1950
- Robert A. Gardiner,
Jacob Zarovsky; Rocket-powered
flight test of a roll-stabilized supersonic missile configuration;
naca-rm-l9k01a; Jan 1950
- Howard L. Turner; Measurement of
the moments of inertia of an airplane by a simplified method;
naca-tn-2201; Oct 1950
- Paul F. Brinich; Boundary-layer
measurements in 3.84- by 10-inch supersonic channel; naca-tn-2203; Oct
1950
- Harold B. Pierce; Gust-tunnel
investigation of a wing model with semichord line swept back 60 degrees;
naca-tn-2204; Oct 1950
- Julian H. Kainer, Jack
E. Marte; Theoretical
supersonic characteristics of inboard trailing-edge flaps having arbitrary
sweep and taper : Mach lines behind flap leading and trailing edges;
naca-tn-2205; Oct 1950
- Fred Werren, Charles
Brazer Norris; Analysis
of shear strength of honeycomb cores for sandwich constructions;
naca-tn-2208; Oct 1950
- C. L. Pekeris; Free
oscillations of an atmosphere in which temperature increases linearly with
height; naca-tn-2209; Oct 1950
- E. D. Kane, G. J.
Maslach; Impact-pressure
interpretation in a rarefied gas at supersonic speeds; naca-tn-2210; Oct
1950
- Kazimierz Roman
Czarnecki, James N. Mueller; An
approximate method of calculating pressures in the tip region of a rectangular
wing of circular-arc section at supersonic speeds; naca-tn-2211; Oct
1950
- Carr B. Neel, Jr.,
Loren G. Bright; The
effect of ice formations on propeller performance; naca-tn-2212; Oct
1950
- M. J. Turner, S.
Rabinowitz; Aerodynamic
coefficients for an oscillating airfoil with hinged flap, with tables for a
Mach number of 0.7; naca-tn-2213; Oct 1950
- Chung-Hua Wu; Formulas
and tables of coefficients for numerical differentiation with function values
given at unequally spaced points and application to solution of partial
differential equations; naca-tn-2214; Nov 1950
- Seymour Lieblein,
Donald M. Sandercock; Compressibility
correction for turning angles of axial-flow inlet guide vanes;
naca-tn-2215; Dec 1950
- Fred E. Macks, Zolton
N. Nemeth; Investigation
of 75-millimeter-bore cylindrical roller bearings at high speeds II :
lubrication studies - effect of oil-inlet location, angle, and velocity for
single-jet lubrication; naca-tn-2216; Nov 1950
- James L. Hassell,
Charles V. Bennett; The
dynamic lateral control characteristics of airplane models having unswept
wings with round-and sharp-leading-edge sections; naca-tn-2219; Nov
1950
- Marion K. Taylor; A balsa-dust
technique for air-flow visualization and its application to flow through model
helicopter rotors in static thrust; naca-tn-2220; Nov 1950
- M. Leroy Spearman; An
investigation of a supersonic aircraft configuration having a tapered wing
with circular-arc sections and 40 degree sweepback; naca-rm-l9l08; Apr
1950
- Charles H. McLellan,
Thomas W. Williams, Ivan E. Beckwith; Investigation
of the flow through a single-stage two-dimensional nozzle in the Langley
11-inch hypersonic tunnel; naca-tn-2223; Dec 1950
- Anthony B. Marmo; Multiple-film
back-reflection camera for atomic strain studies; naca-tn-2224; Nov
1950
- N. J. Hoff; Bending
and buckling of rectangular sandwich plates; naca-tn-2225; Nov 1950
- M. Morduchow, F. G.
Hinchey; Theoretical
analysis of oscillations in hovering of helicopter blades with inclined and
offset flapping and lagging hinge axes; naca-tn-2226; Dec 1950
- John A. Kelly; Effects
of modifications to the leading-edge region on the stalling characteristics of
the NACA 63(sub 1)-012 airfoil section; naca-tn-2228; Nov 1950
- John M. Riebe, James M.
Watson; The
effect of end plates on swept wings at low speed; naca-tn-2229; Nov
1950
- John H. Lamneck, Paul
H. Wise; Synthesis and
purification of alkyldiphenylmethane hydrocarbons I : 2-methyldiphenylmethane,
3-methyldiphenylmethane, 2-ethyldiphenylmethane, 4-ethyldiphenylmethane and
4-isopropyldiphenylmethane; naca-tn-2230; Dec 1950
- Frank C. Smith, William
Charles Brueggeman, Richard H. Harwell; Comparison
of fatigue strengths of bare and Alclad 24S-T3 aluminum-alloy sheet specimens
tested at 12 and 1000 cycles per minute; naca-tn-2231; Dec 1950
- Richard R. Heldenfels,
George W. Zender, Charles Libove; Stress
and distortion analysis of a swept box beam having bulkheads perpendicular to
the spars; naca-tn-2232; Nov 1950
- Robert F. Peterson; The
boundary-layer and stalling characteristics of the NACA 64A010 airfoil
section; naca-tn-2235; Nov 1950
- Antonio Ferri; Supersonic
flow around circular cones at angles of attack; naca-tn-2236; Nov
1950
- George A. Rathert, Jr.,
Stewart L. Rolls, Carl M. Hanson; The
transonic characteristics of a low-aspect-ratio triangular wing with a
constant-chord flap as determined by wing-flow tests, including correlation
with large-scale tests; naca-rm-a50e10; Aug 1950
- Jack N. Nielsen,
Elliott D. Katzen, Kenneth K. Tang; Lift
and pitching-moment interference between a pointed cylindrical body and
triangular wings of various aspect ratios at Mach numbers of 1.50 and
2.02; naca-rm-a50f06; Sep 1950
- Henry C. Lessing; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
effect of sideslip on aerodynamic characteristics at a Mach number of 1.4 with
the wing twisted and cambered; naca-rm-a50f09; Sep 1950
- John C. Heitmeyer; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
effect of Reynolds number at supersonic Mach numbers on the longitudinal
characteristics of a wing twisted and cambered for uniform load;
naca-rm-a50g10; Oct 1950
- Murray Tobak, David E.
Reese, Jr., Benjamin H. Beam; Experimental
damping in pitch of 45 degree triangular wings; naca-rm-a50j26; Dec
1950
- Lomax, Harvard Heaslet,
Max A Fuller, Franklyn B; Formulas
for source, doublet, and vortex distributions in supersonic wing theory;
naca-tn-2252; December 1950
- Morris Morduchow; A theoretical
analysis of elastic vibrations of fixed-ended and hinged helicopter blades in
hovering and vertical flight; naca-tn-1999; Jan 1950
- G. B. Schubauer, W. G.
Spangenberg, P. S. Klebanoff; Aerodynamic
characteristics of damping screens; naca-tn-2001; Jan 1950
- G. A. Morkrzycki; Application of
the Laplace transformation to the solution of the lateral and longitudinal
stability equations; naca-tn-2002; Jan 1050
- John J. Rebeske, Jr.;
Investigation
of a NACA high-speed strain-gage torquemeter; naca-tn-2003; Jan
1950
- Robert A. Gardiner,
Jacob Zarovsky, H. O. Ankenbruck; An
investigation of the stability of a system composed of a subsonic canard
airframe and a canted-axis gyroscope automatic pilot; naca-tn-2004; Jan
1950
- Arnold R. Beckhardt; A theoretical
investigation of the effect on the lateral oscillations of an airplane of an
automatic control sensitive to yawing accelerations; naca-tn-2006; Jan
1950
- Arthur L. Jones,
Alberta Alksne; The
load distribution due to sideslip on triangular, trapezoidal, and related plan
forms in supersonic flow; naca-tn-2007; Jan 1950
- Clarence W. Matthews;
The design,
operation, and uses of the water channel as an instrument for the
investigation of compressible-flow phenomena; naca-tn-2008; Jan
1950
- Julian H. Kainer; Theoretical
calculations of the supersonic pressure distribution and wave drag for a
limited family of tapered sweptback wings with symmetrical parabolic-arc
sections at zero lift; naca-tn-2009; Jan 1950
- Jack D. Brewer, Jacob
H. Lichtenstein; Effect
of horizontal tail on low-speed static lateral stability characteristics of a
model having 45 degree sweptback wing and tail surfaces; naca-tn-2010; Jan
1950
- John DeYoung; Spanwise
loading for wings and control surfaces of low aspect ratio; naca-tn-2011;
Jan 1950
- Marshall Holt; Results
of shear fatigue tests of joints with three-sixteenth-6-inch-diameter
24S-T31; naca-tn-2012; Feb 1050
- Roy H. Lange, Huel C.
McLemore; Static
longitudinal stability and control of a convertible-type airplane as affected
by articulated-and rigid-propeller operation; naca-tn-2014; Feb
1950
- Sidney A. Batterson, A.
Ethelda McArver; Water
landing investigation of a model having a heavy beam loading and a 30 degree
angle of dead rise; naca-tn-2015; Feb 1050
- William Bihrle, Jr.; Floating
characteristics of rudders and elevators in spinning attitudes as determined
from hinge-moment-coefficient data with application to personal-owner-type
airplanes; naca-tn-2016; Jan 1950
- Leonard M. Rose, John
M. Altman; Low-speed
investigation of a thin, faired, double-wedge airfoil section with nose flaps
of various chords; naca-tn-2018; Feb 1950
- Robert S. Ruggeri,
Edmund E. Callaghan, Dean T. Bowden; Penetration
of air jets issuing from circular, square, and elliptical orifices directed
perpendicularly to an air stream; naca-tn-2019; Feb 1950
- Jerome B. Hammack, A.
W. Vogeley; Propeller
flight investigation to determine the effects of blade loading;
naca-tn-2022; Jan 1950
- Orville R. Harris; Determination
of the rate of roll of pilotless aircraft research models by means of
polarized radio waves; naca-tn-2023; Feb 1950
- Harvey H. Hubbard; Sound
measurements for five shrouded propellers at static conditions;
naca-tn-2024; Apr 1950
- Carroll S. Eian; Effect of valve
overlap and compression ratio on variation of measured performance with
exhaust pressure of aircraft cylinder and on computed performance of compound
power plant; naca-tn-2025; Feb 1950
- G. Allen; Tables
for determining reduction of energy and intensity of X-rays and gamma-rays at
various scattering angles in small thickness of matter; naca-tn-2026; Feb
1950
- Robert L. Johnson, Max
A. Swikert, Edmond E. Bisson; Friction
and wear of hot-pressed bearing materials containing molybdenum disulfide;
naca-tn-2027; Feb 1950
- John r. Erwin, James C.
Emery; Effect of
tunnel configuration and testing technique on cascade performance;
naca-tn-2028; Feb 1050
- S. B. Batdorf; The
interpretation of biaxial-tension experiments involving constant stress
ratios; naca-tn-2029; Feb 1950
- Sydney Ross; Variation
with temperature of surface tension of lubricating oils.; naca-tn-2030;
Feb 1050
- W. W. Woods, J. V.
Robinson; Comparative
foaming characteristics of aeronautical lubricating oils; naca-tn-2031;
Feb 1950
- J. V. Robinson, W. W.
Woods; Foaming of
mixtures of pure hydrocarbons; naca-tn-2032; Feb 1950
- J. V. Robinson; Rise of air
bubbles in aircraft lubricating oils; naca-tn-2033; Feb 1950
- Barry Moskowitz, W. E.
Moeckel; First-order
theory for unsteady motion of thin wings at supersonic speeds;
naca-tn-2034; Feb 1950
- Bernard Mazelsky,
Franklin W. Diederich; A
method of determining the effect of airplane stability on the gust load
factor; naca-tn-2035; Feb 1950
- Bernard Mazelsky; Charts of
airplane acceleration ratio for gusts of arbitrary shape; naca-tn-2036;
Feb 1950
- M. J. Whitman, R. W.
Hall, C. Yaker; Resistance
of six cast high-temperature alloys to cracking caused by thermal shock;
naca-tn-2037; Feb 1950
- Paul F. Barrett; Compressive
properties of titanium sheet at elevated temperatures; naca-tn-2038; Feb
1950
- Douglas Godfrey; Investigation
of fretting corrosion by microscopic observation; naca-tn-2039; Feb
1950
- Jerold M. Bidwell; Analysis of an
induction blowdown supersonic tunnel; naca-tn-2040; Apr 1950
- George B. McCullough,
Donald E. Gault; An
experimental investigation of the NACA 631-012 airfoil section with
leading-edge and midchord suction slots; naca-tn-2041; Feb 1950
- Herbert S. Ribner; Time-dependent
downwash at the tail and the pitching moment due to normal acceleration at
supersonic speeds; naca-tn-2042; Feb 1950
- Richard S. Cesaro,
Robert J. Koenig, George J. Pack; Experimental
analysis of a pressure-sensitive system for sensing gas temperature;
naca-tn-2043; Feb 1950
- Julian H. Allen; Pressure
distribution and some effects of viscosity on slender inclined bodies of
revolution; naca-tn-2044; Mar 1950
- Maurice Tucker; Approximate
turbulent boundary-layer development in plane compressible flow along
thermally insulated surfaces with application to supersonic-tunnel contour
correction; naca-tn-2045; Mar 1950
- John A. Zalovcik; A method of
calibrating airspeed installations on airplanes at transonic and supersonic
speeds by use of temperature measurements; naca-tn-2046; Mar 1950
- Harold J. Walker, Mary
B. Ballantyne; Pressure
distribution and damping in steady roll at supersonic Mach numbers of flat
swept-back wing with subsonic edges; naca-tn-2047; Mar 1950
- Kenneth Margolis; Theoretical
lift and damping in roll of thin sweptback tapered wings with raked-in and
cross-stream wing tips at supersonic speeds.subsonic leading edges;
naca-tn-2048; Mar 1950
- Merwin Sibulkin,
William K. Koffel; Chart
for simplifying calculations of pressure drop of a high-speed compressible
fluid under simultaneous action of friction and heat transfer - application to
combustion-chamber cooling passages; naca-tn-2067; Mar 1950
- Arthur M. Trout; Theoretical
turbojet thrust augmentation by evaporation of water during compression as
determined by use of a Mollier diagram; naca-tn-2104; Jun 1950
- E. Clinton Wilcox; Turbojet thrust
augmentation by evaporation of water prior to mechanical compression as
determined by use of psychrometric chart; naca-tn-2105; Jun 1950
- Benjamin Pinkel, Robert
N. Noyes, Michael F. Valerino; Method
for determining pressure drop of air flowing through constant-area passages
for arbitrary heat-input distributions; naca-tn-2186; Sep 1950
- Perkins, Edward W
Canning, Thomas N; Investigation
of downwash and wake characteristics at a Mach number of 1.53 III : swept
wings; naca-rm-a9k02; February 23, 1950
- Hunczak, Henry R
Kremzier, Emil J; Characteristics
of perforated diffusers at free-stream Mach number 1.90; naca-rm-e50b02;
May 08, 1950
- Spakowski, A E Evans, A
Hibbard, R R; Determination
of aromatics and olefins in wide-boiling petroleum fractions;
naca-rm-e50d03; June 26, 1950
- Disher, John H
Rabinowitz, Leonard; Free-flight
performance of 16-inch-diameter supersonic ram-jet units III : four units
designed for combustion-chamber-inlet Mach number of 0.245 at free-stream Mach
number of 1.8 (Units D-1, D-2, D-3, and D-4); naca-rm-e50d07; June 28,
1950
- Luidens, Roger W Simon,
Paul C; Aerodynamic
characteristics of NACA RM-10 missile in 8- by 6-foot supersonic wind tunnel
at Mach numbers from 1.49 to 1.98 I : presentation and analysis of pressure
measurements (stabilizing fins removed); naca-rm-e50d10; July 20,
1950
- Ladanyi, Dezso J Sloop,
John L Humphrey, Jack C Morrell, Gerald; Starting
of rocket engine at conditions of simulated altitude using crude
monoethylaniline and other fuels with mixed acid; naca-rm-e50d20; July 19,
1950
- Esenwein, Fred T Obery,
Leonard J Schueller, Carl F; Aerodynamic
characteristics of NACA RM-10 missile in 8- by 6-foot supersonic wind tunnel
at Mach numbers from 1.49 to 1.98 II : presentation and analysis of force
measurements; naca-rm-e50d28; July 21, 1950
- Lowdermilk, Warren H
Grele, Milton D; Influence
of tube-entrance configuration on average heat-transfer coefficients and
friction factors for air flowing in an Inconel tube; naca-rm-e50e23;
August 23, 1950
- Childs, J Howard; Preliminary
correlation of efficiency of aircraft gas-turbine combustors for different
operating conditions; naca-rm-e50f15; September 21, 1950
- Johnson, Lavern A
Meyer, Carl L; Altitude
performance characteristics of turbojet-engine tail-pipe burner with
variable-area exhaust nozzle using several fuel systems and flame holders;
naca-rm-e50f28; December 29, 1950
- Mahoney, John J Dugan,
Paul D Budinger, Raymond E Goelzer, H Fred; Investigation
of blade-row flow distributions in axial-flow-compressor stage consisting of
guide vanes and rotor-blade row; naca-rm-e50g12; November 28, 1950
- Prince, William R
Mcaulay, John E; Altitude
performance characteristics of tail-pipe burner with convergingconical burner
section on J47 turbojet engine; naca-rm-e50g13; December 19, 1950
- Gerstein, Melvin
Levine, Oscar Wong, Edgar L; Fundamental
flame velocities of pure hydrocarbons I : alkanes, alkenes, alkynes benzene,
and cyclohexane; naca-rm-e50g24; September 28, 1950
- Barnett, Henry C; Antiknock
evaluation of hydrocarbons and ethers as aviation fuel components;
naca-rm-e50h02; October 05, 1950
- Cohen, C B Valerino, A
S; Investigation
of operating pressure ratio of a supersonic wind tunnel utilizing distributed
boundary-layer suction in test section; naca-rm-e50h04; November
1950
- Miller, Riley O; Low-temperature
ignition-delay characteristics of several rocket fuels with mixed acid in
modified open-cup-type apparatus; naca-rm-e50h16; October 17, 1950
- Shillito, T B Jones, W
L Kahn, R W; Altitude test
chamber investigation of performance of a 28-inch ram-jet engine II : effects
of gutter width and blocked area on operating range and combustion
efficiency; naca-rm-e50h21; November 06, 1950
- Connors, James F; Effect of
ram-jet pressure pulsations on supersonic-diffuser performance;
naca-rm-e50h22; November 20, 1950
- Desmon, Leland G Sams,
Eldon W; Correlation of
forced-convection heat-transfer data for air flowing in smooth platinum tube
with long-approach entrance at high surface and inlet-air temperatures;
naca-rm-e50h23; November 02, 1950
- Levine, Oscar Wong,
Edgar L Gerstein, Melvin; Fundamental
flame velocities of pure hydrocarbons II : alkadienes; naca-rm-e50h25;
November 03, 1950
- Olson, Walter T Childs,
J Howard; NACA research
on combustors for aircraft gas turbines I : effects of operating variables on
steady-state performance; naca-rm-e50h31; October 18, 1950
- Wilcox, Fred A; Free-jet
performance of 16-inch ram-jet engine with several fuels; naca-rm-e50i06;
October 31, 1950
- Olson, Walter T Childs,
J Howard Jonash, Edmund R; Turbojet
combustion efficiency at high altitudes; naca-rm-e50i07; October 27,
1950
- Gibbons, Louis C; Factors in
selecting fuels for gas-turbine powered aircraft; naca-rm-e50i18; November
13, 1950
- Luidens, Roger W Simon,
Paul C; Aerodynamic
characteristics of NACA RM 10 missile in 8 by 6 foot supersonic wind tunnel at
Mach numbers from 1.49 to 1.98. III : analysis of force distribution at angle
of attack (stabilizing fins removed); naca-rm-e50i19; December 12,
1950
- Rebeske, John J , Jr
Parisen, Richard B Schum, Harold J; Investigation
of centrifugal compressor operated as a centripetal refrigeration turbine;
naca-rm-e50i20; December 04, 1950
- Scadron, Marvin D
Gettelman, Clarence C Pack, George J; Performance
of three high-recovery-factor thermocouple probes for room-temperature
operation; naca-rm-e50i29; December 21, 1950
- Gammon, Benson E Genco,
Russell S Gerstein, Melvin; A
preliminary experimental and analytical evaluation of diborane as a ram-jet
fuel; naca-rm-e50j04; December 22, 1950
- Belles, Frank E; A preliminary
investigation of wall effects on pressure-inflammability limits of propane-air
mixtures; naca-rm-e50j10a; December 18, 1950
- Garrett, Floyd B Yaker,
Charles; Turbojet-engine
evaluation of AISI 321 and AISI 347 stainless steels as nozzle-blade
materials; naca-rm-e9k17; February 27, 1950
- Farmer, J Elmo Stepka,
Francis S Garrett, Floyd B; Temperature
and pressure distributions in dual parallel jets impinging on the ground from
a turbojet engine; naca-rm-e9l01; February 20, 1950
- Freche, John C; Further
investigation of a gas turbine with National Bureau of Standards body 4811C
ceramic rotor blades; naca-rm-e9l07; March 09, 1950
- Diederich, Franklin W;
Calculation
of the aerodynamic loading of swept and unswept flexible wings of arbitrary
stiffness; naca-report-1000; 1950
- Frey, D N Freeman, J W
White, A E; Fundamental
effects of aging on creep properties of solution-treated low-carbon n-155
alloy; naca-report-1001; 1950
- Reissner, Eric; On the theory
of oscillating airfoils of finite span in subsonic compressible flow;
naca-report-1002; 1950
- Evvard, John C; Use of source
distributions for evaluating theoretical aerodynamics of thin finite wings at
supersonic speeds; naca-report-951; 1950
- Manson, S S; Direct
method of design and stress analysis of rotating disks with temperature
gradient; naca-report-952; 1950
- Goldstein, Arthur W
Mager, Artur; Attainable
circulation about airfoils in cascade; naca-report-953; 1950
- Stanitz, John D Ellis,
Gaylord O; Two-dimensional
compressible flow in centrifugal compressors with straight blades;
naca-report-954; 1950
- Wu, Chung-Hua
Wolfenstein, Lincoln; Application
of radial-equilibrium condition to axial-flow compressor and turbine
design; naca-report-955; 1950
- Heaslet, Max A Lomax,
Harvard Spreiter, John R; Linearized
compressible-flow theory for sonic flight speeds; naca-report-956;
1950
- Lomax, Harvard Sluder,
Loma Heaslet, Max A; The
calculation of downwash behind supersonic wings with an application to
triangular plan forms; naca-report-957; 1950
- Chapman, Dean R; Laminar mixing
of a compressible fluid; naca-report-958; 1950
- (Author(s) Not
Available); One-dimensional
flows of an imperfect diatomic gas; naca-report-959; 1950
- Heimerl, George J
Roberts, William M; Determination
of plate compressive strengths at elevated temperatures; naca-report-960;
1950
- Heaslet, Max A Lomax,
Harvard; The
application of Green's theorem to the solution of boundary-value problems in
linearized supersonic wing theory; naca-report-961; 1950
- Spreiter, John R; The aerodynamic
forces on slender plane- and cruciform-wing and body combinations;
naca-report-962; 1950
- Gooderum, Paul B Wood,
George P Brevoort, Maurice J; Investigation
with an interferometer of the turbulent mixing of a free supersonic jet;
naca-report-963; 1950
- Loftin, Laurence K, Jr
Bursnall, William J; The
effects of variations in Reynolds number between 3.0 x 10sub6 and 25.0 x
10sub6 upon the aerodynamic characteristics of a number of NACA 6-series
airfoil sections; naca-report-964; 1950
- Frick, C W Chubb, R S;
The
longitudinal stability of elastic swept wings at supersonic speed;
naca-report-965; 1950
- Runyan, Harry L
Watkins, Charles E; Flutter
of a uniform wing with an arbitrarily placed mass according to a
differential-equation analysis and a comparison with experiment;
naca-report-966; 1950
- Seide, Paul Stowell,
Elbridge Z; Elastic and
plastic buckling of simply supported solid-core sandwich plates in
compression; naca-report-967; 1950
- Goodman, Alex Fisher,
Lewis R; Investigation
at low speeds of the effect of aspect ratio and sweep on rolling stability
derivatives of untapered wings; naca-report-968; 1950
- Bird, John D; Some
theoretical low-speed span loading characteristics of swept wings in roll and
sideslip; naca-report-969; 1950
- Malvestuto, Frank S ,
Jr Margolis, Kenneth Ribner, Herbert S; Theoretical
lift and damping in roll at supersonic speeds of thin sweptback tapered wings
with streamwise tips, subsonic leading edges, and supersonic trailing
edges; naca-report-970; 1950
- Malvestuto, Frank S ,
Jr Margolis, Kenneth; Theoretical
stability derivatives of thin sweptback wings tapered to a point with
sweptback or sweptforward trailing edges for a limited range of supersonic
speeds; naca-report-971; 1950
- Tucker, Warren A
Nelson, Robert L; The
effect of torsional flexibility on the rolling characteristics at supersonic
speeds of tapered unswept wings; naca-report-972; 1950
- Johnson, Harold I; Flight
investigation of the effect of various vertical-tail modifications on the
directional stability and control characteristics of a propeller-driven
fighter airplane; naca-report-973; 1950
- Kantrowitz, Arthur; The supersonic
axial-flow compressor; naca-report-974; 1950
- Reissner, Eric; Small bending
and stretching of sandwich-type shells; naca-report-975; 1950
- Katzoff, S Gardner,
Clifford S Diesendruck, Leo Eisenstadt, Bertram J; Linear
theory of boundary effects in open wind tunnels with finite jet lengths;
naca-report-976; 1950
- Laverne, Melvin E
Boksenbom, Aaron S; Frequency
response of linear systems from transient data; naca-report-977;
1950
- Costello, George R; Method of
designing cascade blades with prescribed velocity distributions in
compressible potential flows; naca-report-978; 1950
- Lessen, Martin; On stability of
free laminar boundary layer between parallel streams; naca-report-979;
1950
- Boksenbom, Aaron S
Hood, Richard; General
algebraic method applied to control analysis of complex engine types;
naca-report-980; 1950
- Lundin, Bruce T; Theoretical
analysis of various thrust-augmentation cycles for turbojet engines;
naca-report-981; 1950
- Coles, Willard D
Rollin, Vern G Mulholland, Donald R; Icing-protection
requirements for reciprocating-engine induction system; naca-report-982;
1950
- Mirels, Harold Haefeli,
Rudolph C; Line-vortex
theory for calculation of supersonic downwash; naca-report-983;
1950
- Curfman, Howard J
Gardiner, Robert A; Method
for determining the frequency-response characteristics of an element or system
from the system transient output response to a known input function;
naca-report-984; 1950
- Zalovcik, John A; A radar method
of calibrating airspeed installations on airplanes in maneuvers at high
altitudes and at transonic and supersonic speeds; naca-report-985;
1950
- Brown, Clinton E; The
reversibility theorem for thin airfoils in subsonic and supersonic flow;
naca-report-986; 1950
- Sanders, John C Chapin,
Edward C; Equilibrium
operating performance of axial-flow turbojet engines by means of idealized
analysis; naca-report-987; 1950
- Mathews, Charles W
Thompson, Jim Rogers; Comparative
drag measurements at transonic speeds of rectangular sweptback NACA 65-009
airfoils mounted on a freely falling body; naca-report-988; 1950
- Klunker, E G Ivey, H
Reese; An
analysis of supersonic aerodynamic heating with continuous fluid
injection; naca-report-990; 1950
- Press, Harry; The
application of the statistical theory of extreme values to gust-load
problems; naca-report-991; 1950
- Hall, Eldon W Wilcox, E
Clinton; Theoretical
comparison of several methods of thrust augmentation for turbojet engines;
naca-report-992; 1950
- Gessow, Alfred Amer,
Kenneth B; An introduction
to the physical aspects of helicopter stability; naca-report-993;
1950
- Livingood, John N B
Brown, W Byron; Analysis
of spanwise temperature distribution in three types of air-cooled turbine
blade; naca-report-994; 1950
- Herriot, John G; Blockage
corrections for three-dimensional-flow closed-throat wind tunnels, with
consideration of the effect of compressibility; naca-report-995;
1950
- Hubbard, Harvey H
Regier, Arthur A; Free-space
oscillating pressures near the tips of rotating propellers;
naca-report-996; 1950
- Donely, Philip; Summary of
information relating to gust loads on airplanes; naca-report-997;
1950
- Corrsin, Stanley
Uberoi, Mahinder S; Further
experiments on the flow and heat transfer in a heated turbulent air jet;
naca-report-998; 1950
- Stack, John Draley,
Eugene C Delano, James B Feldman, Lewis; Investigation
of the NACA 4-(3)(8)-045 two-blade propellers at forward Mach numbers to 0.725
to determine the effects of compressibility and solidity on performance;
naca-report-999; 1950
- Hasel, Lowell E
Sinclair, Archibald R; A
pressure-distribution investigation of a supersonic-aircraft fuselage and
calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot
supersonic tunnel; naca-rm-l50b14a; April 07, 1950
- Stone, David G; Wing-dropping
characteristics of some straight and swept wings at transonic speeds as
determined with rocket-powered models; naca-rm-l50c01; May 26, 1950
- Nelson, Robert L; Large-scale
flight measurements of zero-lift drag at Mach numbers form 0.86 to 1.5 of a
wing-body combination having a 60 degree triangular wing with NACA 65A003
sections; naca-rm-l50d26; June 1950
- Nelson, William J
Bloetscher, Frederick; Preliminary
investigation of porous walls as a means of reducing tunnel boundary effects
at low-supersonic Mach numbers; naca-rm-l50d27; September 13, 1950
- Stoney, William E , Jr
Katz, Ellis; Pressure
measurements on a sharply converging fuselage afterbody with jet on and off at
Mach numbers from 0.8 to 1.6; naca-rm-l50f06; August 10, 1950
- Mitchell, Meade H , Jr;
Effects of
varying the size and location of trailing-edge flap-type controls on the
aerodynamic characteristics of a unswept wing at a Mach number of 1.9;
naca-rm-l50f08; August 16, 1950
- Becht, Robert E Few,
Albert G , Jr; Stability
characteristics at low speed of a 1/4-scale Bell X-5 airplane model with
various modifications to the basic model configurations; naca-rm-l50f23;
August 16, 1950
- Strass, H Kurt Fields,
E M Purser, Paul E; Experimental
determination of effect of structural rigidity on rolling effectiveness of
some straight and swept wings at Mach numbers from 0.7 to 1.7;
naca-rm-l50g14b; October 04, 1950
- Pepper, William B , Jr
Hoffman, Sherwood; Transonic
flight test to compare the zero-lift drag of underslung and symmetrical
nacelles varied chordwise at 40 percent semispan of a 45 degree sweptback,
tapered wing; naca-rm-l50g17a; October 25, 1950
- Davis, Don D , Jr Wood,
George P; Preliminary
investigation of reflections of oblique waves from a porous wall;
naca-rm-l50g19a; November 09, 1950
- Katz, Ellis Marley,
Edward T Pepper, William B; Flight
investigation at Mach numbers from 0.8 to 1.4 to determine the zero-lift drag
of wings with 'M' and 'W' plan forms; naca-rm-l50g31; September 18,
1950
- Luoma, Arvo A Wright,
John B; Longitudinal
stability and control characteristics at high subsonic speeds of two models of
a transonic research airplane with wings and horizontal tails of aspect ratios
4.2 and 2; naca-rm-l50h07; September 29, 1950
- Faget, Maxime A
Dettwyler, H Rudolph; Initial
flight investigation of a twin engine supersonic ram jet; naca-rm-l50h10;
September 15, 1950
- D'Aiutolo, Charles T
Mason, Homer P; Preliminary
results of the flight investigation between Mach numbers of 0.80 and 1.36 of a
rocket-powered model of a supersonic airplane configuration having a tapered
wing with circular-arc sections and 40 degree sweepback; naca-rm-l50h29a;
October 31, 1950
- Bertram, Mitchel H; Investigation
of the pressure-ratio requirements of the Langley 11-inch hypersonic tunnel
with a variable-geometry diffuser; naca-rm-l50i13; October 06, 1950
- Purser, Paul E
Thibodaux, Joseph G Jackson, H Herbert; Note
on some observed effects of rocket motor operation on the base pressures of
bodies in free light; naca-rm-l50i18; November 16, 1950
- Bond, Aleck C; Experimental
investigation of a flat plate paddle jet vane operating on a rocket jet;
naca-rm-l50i20; November 15, 1950
- Schult, Eugene D; Comparison of
large scale flight measurements of zero lift drag at Mach numbers from 0.9 to
1.7 of two wing-body combinations having similar 60 degree triangular wings
with NACA 65A003 sections; naca-rm-l50i22; October 25, 1950
- Niewald, Roy J Moul,
Martin T; The
longitudinal stability, control effectiveness, and control hinge moment
characteristics obtained from a flight investigation of a canard missile
configuration at transonic and supersonic speeds; naca-rm-l50i27; November
24, 1950
- Becht, Robert E; Stability and
control characteristics of a 1/4-scale Bell X-5 airplane model in the landing
configuration; naca-rm-l50j27; December 18, 1950
- Adamson, David
Boatright, William B; Investigation
of downwash, sidewash, and Mach number distribution behind a rectangular wing
at a Mach number of 2.41; naca-rm-l50g12; 1957
- Lo, Hsu Crate, Harold
Schwartz, Edward B; Buckling
of thin-walled cylinder under axial compression and internal pressure;
naca-tn-2021; 1950
- Zender, George W
Heldenfels, Richad R; Stress
and distortion measurements in a 45 degree swept box beam subjected to
antisymmetrical bending and torsion; naca-tn-2054; April 1950
- Merten, Kenneth F
Rodriguez, Jose L Beck, Edgar B; A
comparison of theoretical and experimental wing bending moments during
seaplane landings; naca-tn-2063; April 1950
- Seide, Paul Barrett,
Paul F; The
stability of the compression cover of box beams stiffened by posts;
naca-tn-2153; August 1950
- Rom, Frank E Koutz,
Stanley L; Effect of heat
and power extraction on turbojet-engine performance II : effect of
compressor-outlet air bleed for specific modes of engine operation;
naca-tn-2166; August 1950
- Mendelson, Alexander
Gendler, Selwyn; Analytical
determination of coupled bending-torsion vibrations of cantilever beams by
means of station functions; naca-tn-2185; September 1950
- Koutz, Stanley L
Hensley, Reece V Rom, Frank E; Effect
of heat and power extraction on turbojet-engine performance III : analytical
determination of effects of shaft-power extraction; naca-tn-2202; October
1950
- Wu, M H Lee; Analysis
of plane-stress problems with axial symmetry in strain-hardening range;
naca-tn-2217; December 1950
- Levine, Joseph; Statistical
explanation of spontaneous freezing of water droplets; naca-tn-2234;
December 1950
- Wier, John E (National
Bureau of Standards) Pons, Dorothy C (National Bureau of Standards) Axilrod,
Benjamin M (National Bureau of Standards); Effects
of molding conditions on some physical properties of glass-fabric
unsaturated-polyester laminates; naca-rm-50j19; November 09, 1950
- Hamilton, William T
Cleary, Joseph W; Wind-tunnel
tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds :
stability and control characteristics; naca-rm-a50a03; April 21,
1950
- Dannenberg, Robert E
Blackaby, James R; An
experimental investigation of a jet-engine nacelle in several positions on a
37.25 degree swept-back wing; naca-rm-a50a13; April 19, 1950
- Weiberg, James A Carel,
Hubert C; Wind-tunnel
investigation at low speed of a wing swept-back 63 degrees and twisted and
cambered for a uniform load at a lift coefficient of 0.5; naca-rm-a50a23;
May 09, 1950
- Olson, Robert N Mead,
Merrill H; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
effectiveness of an elevon as a longitudinal control and the effects of camber
and twist on the maximum lift-drag ratio at supersonic speeds;
naca-rm-a50a31a; May 08, 1950
- Krumm, Walter J; Pressure
coefficients at Mach numbers from 0.60 to 0.85 for a semispan wing with NACA
0012-64 section, 20-percent-chord plain aileron, and 0 degree and 45 degree
sweepback; naca-rm-a50b13; April 19, 1950
- Axelson, John A Taylor,
Robert A; Preliminary
investigation of the transonic characteristics of an NACA submerged inlet;
naca-rm-a50c13; June 05, 1950
- Spahr, J Richard
Robinson, Robert A; Wind-tunnel
investigation at Mach numbers of 2.0 and 2.9 of several configurations of a
supersonic ram-jet test vehicle; naca-rm-a50c20; August 18, 1950
- Cleary, Joseph W
Mellenthin, Jack A; Wind-tunnel
tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds :
additional stability and control characteristics and the aerodynamic effects
of external stores and ram jets; naca-rm-a50c30; June 13, 1950
- Berggren, Robert E
Graham, Donald J; Effects
of leading-edge radius and maximum thickness-chord ratio on the variation with
Mach number of the aerodynamic characteristics of several thin NACA airfoil
sections; naca-rm-a50d04; July 03, 1950
- Winograd, Lee Van Dyke,
Rudolph D , Jr; Flight
determination of the effects of rudder-pedal-force characteristics on the
aiming error in azimuth of a conventional fighter airplane;
naca-rm-a50d06; July 05, 1950
- Cleary, Joseph W
Mellenthin, Jack A; Wind-tunnel
tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds : wing
and fuselage pressure distribution; naca-rm-a50d07; June 22, 1950
- Boltz, Frederick W
Beam, Benjamin H; The
effects of compressibility on the pressures on a body of revolution and on the
aerodynamic characteristics of a wing-nacelle combination consisting of the
body of revolution mounted on a swept-back wing; naca-rm-a50e09; July 26,
1950
- Boddy, Lee E; Investigation
at high subsonic speeds of methods of alleviating the adverse interference at
the root of a swept-back wing; naca-rm-a50e26; August 10, 1950
- Holzhauser, Curt A; An experimental
investigation at large scale of an NACA submerged intake and deflector
installation on the rearward portion of a fuselage; naca-rm-a50f13; August
30, 1950
- Delany, Noel K Hayter,
Nora-Lee F; Low-speed
investigation of a 0.16-scale model of the X-3 airplane : longitudinal
characteristics; naca-rm-a50g06; September 08, 1950
- Heinle, Donovan R; Effect of
dihedral change on the theoretical dynamic lateral response characteristics of
a low-aspect-ratio straight-wing supersonic airplane; naca-rm-a50h02;
December 07, 1950
- Winograd, Lee Cooper,
George E Rathert, George A , Jr Rolls, L Stewart; Preliminary
flight investigation of the wing-dropping tendency and lateral-control
characteristics of a 35 degree swept-wing airplane at transonic Mach
numbers; naca-rm-a50h03; September 11, 1950
- Cook, Woodrow L
Griffin, Roy N Mccormack, Gerald M , Jr; The
use of area suction for the purpose of delaying separation of air flow at the
leading edge of a 63 degree swept-back wing; naca-rm-a50h09; November 22,
1950
- Krumm, Walter J Cleary,
Joseph W; High-speed
aerodynamic characteristics of a lateral-control model III : section
characteristics, fence studies, and tabulated pressure coefficients with
modified NACA 0012-64 section, 26.6-percent-chord, plain aileron, 0 and 45
degree sweepback; naca-rm-a50h17; November 22, 1950
- Boltz, Federick W
Buell, Donald A; Wind-tunnel
investigation of the effects of a jet engine nacelle on the aerodynamic
characteristics of a 37.25 degree swept back wing at high subsonic speeds;
naca-rm-a50h23; October 24, 1950
- Sadoff, Melvin Sisk,
Thomas R; Summary report
of results obtained during demonstration tests of the Northrop X-4
airplanes; naca-rm-a50i01; December 13, 1950
- Nelson, Warren H; Wind-tunnel
investigation of a 1/6-scale model of the Bumblebee XPM missile at high
subsonic speeds; naca-rm-a50i11; December 11, 1950
- Weiberg, James A Carel,
Hubert C; Wind-tunnel
investigation at low speed of a wing swept back 63 degrees and twisted and
cambered for uniform load at a lift coefficient of 0.5 and with a thickened
tip section; naca-rm-a50i14; November 21, 1950
- Walker, Harold J
Stivers, Louis S , Jr; Investigation
of the downwash and wake behind a triangular wing of aspect ratio 4 at
subsonic and supersonic Mach numbers; naca-rm-a50i14a; December 12,
1950
- Summers, James L Page,
William A; Lift and moment
characteristics at subsonic Mach numbers of four 10-percent-thick airfoil
sections of varying trailing-edge thickness; naca-rm-a50j09; December 20,
1950
- Triplett, William C Van
Dyke, Rudolph D , Jr; Preliminary
flight investigation of the dynamic longitudinal-stability characteristics of
a 35 degree swept-wing airplane; naca-rm-a50j09a; December 11, 1950
- Stivers, Louis S , Jr
Malick, Alexander W; Wind-tunnel
investigation at Mach numbers from 0.50 to 1.29 of an unswept tapered wing of
aspect ratio 2.67 with leading- and trailing-edge flaps - trailing-edge flaps
deflected; naca-rm-a50j09b; December 13, 1950
- Hall, Charles F
Heitmeyer, John C; Aeronautical
study of a wing-fuselage combination employing a wing swept back 63 degrees :
characteristics at supersonic speeds of a model with the wing twisted and
cambered for uniform load; naca-rm-a9j24; January 09, 1950
- Matthews, Howard F; The effect of
accelerating a hypothetical aircraft through the transonic range with controls
fixed; naca-rm-a9j26; April 04, 1950
- Edwards, George G
Boltz, Frederick W; An
analysis of the forces and pressure distribution on a wing with the leading
edge swept back 37.25 degrees; naca-rm-a9k01; March 30, 1950
- Mccormack, Gerald M
Cook, Woodrow L; Effects
of boundary-layer control on the longitudinal characteristics of a 45 degrees
swept-forward wing-fuselage combination; naca-rm-a9k02a; February 02,
1950
- Dannenberg, Robert E;
A design
study of leading-edge inlets for unswept wings; naca-rm-a9k02b; June 30,
1950
- Nelson, Warren, H
Erickson, Albert L; The
effect of aspect ratio on the subsonic aerodynamic characteristics of wings
with NACA 65(sub 1)-210 sections; naca-rm-a9k18; February 03, 1950
- Wick, Bradford H
Graham, David; Exploratory
investigation of the effect of skewed plain nose flaps on the low-speed
characteristics of a large-scale triangular-wing-fuselage model;
naca-rm-a9k22; January 12, 1950
- Stivers, Louis S
Malick, Alexander W; Wing-tunnel
investigation at Mach numbers from 0.50 to 1.29 of an all-movable triangular
wing of aspect ratio 4 alone and with a body; naca-rm-a9l01; February 02,
1950
- Krumm, Walter J
Anderson, Joseph L; High-speed
aerodynamic characteristics of a lateral-control model II : modified NACA
0012-64 section with a 26.6-percent-chord, plain, trailing-edge aileron; wing
unswept and swept back 45 degrees; naca-rm-a9l27; March 15, 1950
- Rolls, L Stewart
Rathert, George A , Jr; Tests
of a small-scale NACA submerged inlet at transonic Mach numbers;
naca-rm-a9l29; February 23, 1950
- Ellerbrock, Herman H ,
Jr Schafer, Louis J , Jr; Application
of blade cooling to gas turbines; naca-rm-e50a04; May 31, 1950
- Ellerbrock, Herman H ,
Jr Ziemer, Robert R; Preliminary
analysis of problem of determining experimental performance of air-cooled
turbine I : methods for determining heat-transfer characteristics;
naca-rm-e50a05; June 12, 1950
- Ellerbrock, Herman H ,
Jr; Preliminary
analysis of problem of determining experimental performance of air-cooled
turbine II : methods for determining cooling-air-flow characteristics;
naca-rm-e50a06; June 07, 1950
- Grey, Ralph E
Brightwell, Virginia L Barson, Zelmar NACA; Altitude-chamber
performance of British Rolls-Royce Nene II engine III : 18.00-inch-diameter
jet nozzle; naca-rm-e50a31; July 10, 1950
- Doyle, Ronald B; Calculated
performance of nuclear turbojet powered airplane at flight Mach number of
0.9; naca-rm-e50b23; May 11, 1950
- Mcdonald, Glen E; Measurement of
uniform flame movement in carbon monoxide - air mixtures containing either
added D2O or H2O; naca-rm-e50c10; July 05, 1950
- Acker, Loren W
Kleinknecht, Kenneth S; Effects
of inlet icing on performance of axial-flow turbojet engine in natural icing
conditions; naca-rm-e50c15; May 25, 1950
- Hanson, Morgan P; Effect of
blade-root fit and lubrication on vibration characteristics of ball-root-type
axial-flow-compressor blades; naca-rm-e50c17; June 15, 1950
- Hubbartt, James E; Comparison of
outside-surface heat-transfer coefficients for cascades of turbine blades;
naca-rm-e50c28; July 17, 1950
- Eckert, E R G Jackson,
Thomas W; Analytical
investigation of flow and heat transfer in coolant passages of free-convection
liquid-cooled turbines; naca-rm-e50d25; July 18, 1950
- Brown, W Byron
Rossbach, Richard J; Numerical
solution of equations for one-dimensional gas flow in rotating coolant
passages; naca-rm-e50e04; June 26, 1950
- Silvern, David H
Slivka, William R; Analytical
investigation of turbines with adjustable stator blades and effect of these
turbines on jet-engine performance; naca-rm-e50e05; July 17, 1950
- Fleming, William A
Wallner, Lewis E Wintler, John T; Effect
of compressor-outlet bleedoff on turbojet-engine performance;
naca-rm-e50e17; August 07, 1950
- Ellerbrock, Herman H ,
Jr Ziemer, Robert R; Preliminary
analysis of problem of determining experimental performance of air-cooled
turbine III : methods for determining power and efficiency;
naca-rm-e50e18; August 02, 1950
- Zettle, Eugene V Mark,
Herman; Simulated
altitude performance of two annular combustors with continuous axial openings
for admission of primary air; naca-rm-e50e18a; August 03, 1950
- Schramm, Wilson B
Nachtigall, Alfred J Arne, Vernon L; Preliminary
analysis of effects of air cooling turbine blades on turbojet-engine
performance; naca-rm-e50e22; August 02, 1950
- Jansen, Emmert T
Thorman, H Carl; Altitude
performance characteristics of tail-pipe burner with variable-area exhaust
nozzle; naca-rm-e50e29; August 11, 1950
- Brown, W Byron
Donoughe, Patrick L; Extension
of boundary-layer heat-transfer theory to cooled turbine blades;
naca-rm-e50f02; August 11, 1950
- Straight, David M Gold,
Harold; Experimental
and analytical study of balanced-diaphragm fuel distributors for gas-turbine
engines; naca-rm-e50f05; August 14, 1950
- Brown, W Byron Esgar,
Jack B; Analytical
determination of local surface heat-transfer coefficients for cooled turbine
blades from measured metal temperatures; naca-rm-e50f09; August 11,
1950
- Weinstein, Maynard I;
Investigation
of perforated convergent-divergent diffusers with initial boundary layer;
naca-rm-e50f12; August 15, 1950
- Wear, Jerrold D Locke,
Theodore E; Effect of
retractable ignition plug on plug fouling by carbon deposits;
naca-rm-e50f14; August 24, 1950
- Shillito, T B Jones, W
L Henzel, J G , Jr; Altitude-test-chamber
investigation of performance of a 28-inch ram-jet engine I : combustion and
operational performance of four combustion-chamber configurations;
naca-rm-e50f16; August 23, 1950
- Chelko, Louis J; Penetration of
liquid jets into a high-velocity air stream; naca-rm-e50f21; August 14,
1950
- Long, Roger A; Fabrication
and properties of hot-pressured molybdenum disilicide; naca-rm-e50f22;
August 24, 1950
- Drake, Wray V Drell, I
L; Survey of
less-inflammable hydraulic fluids for aircraft; naca-rm-e50f29; September
07, 1950
- Wilsted, H D Armstrong,
J C; Effect
of fuel volatility on altitude starting limits of a turbojet engine;
naca-rm-e50g10; September 11, 1950
- Conrad, E William
Sobolewski, Adam E; Investigation
of effects of inlet-air velocity distortion on performance of turbojet
engine; naca-rm-e50g11; September 13, 1950
- Hibbard, Robert R
Drell, Isadore L Metzler, Allen J Spakowski, Adolph E; Combustion
efficiencies in hydrocarbon-air systems at reduced pressures;
naca-rm-e50g14; September 13, 1950
- Wilcox, Fred Baker, Sol
Perchonok, Eugene; Free-jet
investigation of a 16-inch ram jet at Mach numbers of 1.35, 1.50, and
1.73; naca-rm-e50g19; October 02, 1950
- Kaufman, Samuel J
Isely, Francis D; Preliminary
investigation of heat transfer to water flowing in an electrically heated
Inconel tube; naca-rm-e50g31; September 27, 1950
- Glasser, Philip W; Performance of
4600-pound-thrust centrifugal-flow-type turbojet engine with water-alcohol
injection at inlet; naca-rm-e50h07; October 09, 1950
- Sather, Bernard I
Tauschek, Max J; Study
of compressor systems for a gas-generator engine; naca-rm-e50h08; October
16, 1950
- Cummings, John L
Haefeli, Rudolph C; Downwash
in vortex region behind rectangular half-wing at Mach number 1.91;
naca-rm-e50h10; October 26, 1950
- Rayle, Warren D
Douglass, Howard W; Investigation
of ignition characteristics of AN-F-32 and two AN-F-58a fuels in single
can-type turbojet combustor; naca-rm-e50h16a; October 13, 1950
- Humble, L V Wachtl, W W
Doyle, R B; Preliminary
analysis of three cycles for nuclear propulsion of aircraft;
naca-rm-e50h24; October 13, 1950
- Von Glahn, Uwe Blatz,
Robert E; Investigation
of power requirements for ice prevention and cyclical de-icing of inlet guide
vanes with internal electric heaters; naca-rm-e50h29; December 1950
- Wallner, Lewis E Saari,
Martin J; Altitude
investigation of performance of turbine-propeller engine and its
components; naca-rm-e50h30; October 05, 1950
- Gray, Vernon H Bowden,
Dean T; Icing
characteristics and anti-icing heat requirements for hollow and internally
modified gas-heated inlet guide vanes; naca-rm-e50i08; December 05,
1950
- Jackson, Joseph L; Spontaneous
ignition temperatures of pure hydrocarbons and commercial fluids;
naca-rm-e50j10; December 20, 1950
- Sloop, John L Morrell,
Gerald; Temperature
survey of the wake of two closely located parallel jets; naca-rm-e9i21;
February 06, 1950
- Mark, Herman Zettle,
Eugene V; Effect of air
distribution on radial temperature distribution in one-sixth sector of annular
turbojet combustor; naca-rm-e9i22; April 05, 1950
- Pesman, Gerard J; Analysis of
multiengine transport airplane fire records; naca-rm-e9j19; May
1950
- Busch, Arthur M; Correlation of
laboratory smoke test with carbon deposition in turbojet combustors;
naca-rm-e9k04; February 03, 1950
- Thorman, H Carl
Mcaulay, John E; Altitude-wind-tunnel
investigation of turbine performance in J47 turbojet engine;
naca-rm-e9k10; September 21, 1950
- Hauser, Cavour H Plohr,
Henry W Sonder, Gerhard; Study
of flow conditions and deflection angle at exit of two-dimensional cascade of
turbine rotor blades at critical and supercritical pressure ratios;
naca-rm-e9k25; March 10, 1950
- Bell, Arthur H Farmer,
J Elmo; Transient
operating characteristics of a turbojet engine when subjected to steep changes
in fuel flow; naca-rm-e9k25a; February 20, 1950
- Campbell, Carl E; Altitude-wind-tunnel
investigation of combustion-chamber performance on J47 turbojet engine;
naca-rm-e9l02; December 15, 1950
- Meyer, Andre' J
Calvert, Howard F Morse, C Robert; Effects
of obstructions in compressor inlet on blade vibration in 10-stage axial-flow
compressor; naca-rm-e9l05; February 13, 1950
- Yuriev, I.M.; Subsonic
gas flow past a wing profile; naca-tm-1250; 1950
- ; On
the formation of shock waves in subsonic flows with local supersonic
velocities; naca-tm-1251; 1950
- Falkovich, S.V.; Vibration of a
wing of finite span in a supersonic flow; naca-tm-1257; 1950
- ; Exact
solutions of equations of gas dynamics; naca-tm-1260; 1950
- Schlichting, H.; Amplitude
distribution and energy balance of small disturbances in plate flow;
naca-tm-1265; 1950
- Brodel, Walter.; Theory of
plane, symmetrical intake diffusers; naca-tm-1267; 1950
- Damkohler, Gerhard.; Isentropic
phase changes in dissociating gases and the method of sound dispersion for the
investigation of homogeneous gas reactions with very high speed;
naca-tm-1268; 1950
- Damkohler, Gerhard.; Isentropic
phase changes in dissociating gases and the method of sound dispersion for the
investigation of homogeneous gas reactions with very high speed
:Conclusion; naca-tm-1269; 1950
- Sanger, Eugen; The
gas kinetics of very high flight speeds; naca-tm-1270; 1950
- Hahnemann, H., Ehret,
L.; Effect
of intense sound waves on a stationary gas flame; naca-tm-1271;
1950
- Schuh, H.; The
solution of the laminar-boundary-layer equation for the flat plate for
velocity and temperature fields for variable physical properties and for the
diffusion field at high concentration; naca-tm-1275; 1950
- Mangler, W.; General
solution of Prandtl's boundary-layer equation; naca-tm-1278; 1950
- Ruden, P.; Two-dimensional
symmetrical inlets with external compression; naca-tm-1279; 1950
- Lutz, Otto.; Graphical
determination of wall temperatures for heat transfers through walls of
arbitrary shape; naca-tm-1280; 1950
- Ludwieg, H.; Instrument
for measuring the wall shearing stress of turbulent boundary layers;
naca-tm-1284; 1950
- Ludwieg, Hubert.,
Tillmann, W.; Investigations
of the wall-shearing stress in turbulent boundary layers; naca-tm-1285;
1950
- Kuntze, Wilhelm.; Dependence of
the elastic strain coefficient of copper on the pre-treatment;
naca-tm-1287; 1950
- Kohlmann, H.; The
development of a hollow blade for exhaust gas turbines; naca-tm-1289;
1950
- Seaberg, Ernest C.; Theoretical
investigation of a proportional-plus-flicker automatic pilot;
naca-rm-l50i19; 1950
- Sokolov, N. A.; Hydrodynamic
properties of planing surfaces and flying boats; naca-tm-1246; 1950
- Gantmacher, F. R.,
Levin, L. M.; Equations
of motion of a rocket; naca-tm-1255; 1950
- Povolny, John H.,
Bogdan, Louis J., Chelko, Louis J.; Cylinder-head
temperatures and coolant heat rejection of a multicylinder liquid-cooled
engine of 1650-cubic-inch displacement; naca-tn-2069; 1950
- Frank, Joseph L.; Pressure-Distribution
and Ram-Recovery Characteristics of NACA Submerged Inlets at High Speed
Subsonic Speeds; naca-rm-a50e02; 1950
- Graham, David.; Chordwise and
spanwise loadings measured at a large triangular wing having an aspect ratio
of 2 and a thin, subsonic-type airfoil section; naca-rm-a50a04a;
1950
- Voit, Charles H.,
Guentert, Donald C., Dugan, James F.; Performance
of high-pressure-ratio axial-flow compressor using highly cambered NACA
65-series blower blades at high Mach numbers; naca-rm-e50a09; 1950
- Golladay, Richard L.,
Bloomer, Harry E.; Altitude
performance and operational characteristics of 29-inch-diameter tail-pipe
burner with several fuel systems and fuel-cooled stage-type flame holders on
J35-A-5 turbojet engine / Richard L. Golladay and Harry E. Bloomer;
naca-rm-e50a19; 1950
- Huntley, Sidney C.; Altitude-chamber
performance of British Roll-Royce Nene II engine IV :effect of operational
variables on temperature distribution at combustion-chamber outlets;
naca-rm-e50b10; 1950
- Messing, Wesley E.,
Simpkinson, Scott H.; Free-flight
performance of 16-inch-diameter supersonic ram-jet units II :five units
designed for combustion-chamber-inlet Mach number of 0.16 at free-stream Mach
number of 1.60 (units B-1, B-2, B-3, B-4, and B-5) /c Wesley E. Messing and
Scott H. Simpkin; naca-rm-e50b14; 1950
- Freche, John C.,
Diaguila, A. J.; Heat-transfer
and operating characteristics of aluminum forced-convection and
stainless-steel natural-convection water-cooled single-stage turbines;
naca-rm-e50d03a; 1950
- Moeckel, W. E.; Experimental
investigation of supersonic flow with detached shock waves for Mach numbers
between 1.8 and 2.9; naca-rm-e50d05; 1950
- Jones, William L.,
Bogdan, Louis J.; Experimental
investigation of thrust augmentation of 4000-pound-thrust
centrifugal-flow-type turbojet engine by bleedoff; naca-rm-e50d17;
1950
- Shillito, Thomas B.,
Harp, James L., Jr.; Effect
of inlet temperature and humidity on thrust augmentation of turbojet engine by
compressor-inlet injection; naca-rm-e50d19; 1950
- Voit, Charles H.,
Guentert, Donald C., Dugan, James F.; Effect
of Mach number on over-all performance of single-stage axial-flow compressor
designed for high pressure ratio; naca-rm-e50d26; 1950
- Behun, M., Rom, F. E.,
Hensley, R. V.; Evaluation
of a ducted-fan power plant designed for high output and good cruise fuel
economy; naca-rm-e50e01; 1950
- von Glahn, Uwe., Blatz,
Robert E.; Investigation
of aerodynamic and icing characteristics of water-inertia-separation inlets
for turbojet engines; naca-rm-e50e03; 1950
- Krebs, Richard R.,
Himmel, Seymore C., Blivas, Darnold., Shames, Harold.; Dynamic
investigation of turbine-propeller engine under altitude conditions;
naca-rm-e50j24; 1950
- A. Huffschmid; Investigation
of the Model ME210 in the Spin Wind Tunnel of the DVL, Fourth Partial Report -
Model with Long Fuselage and with a Vee Tail; naca-tm-1222; 1950
- Stuper; Flight
Experiences and Tests on Two Airplanes with Suction Slots; naca-tm-1232;
1950
- E. W. Sponder; Investigations
of Lateral Stability of a Glide Bomb Using Automatic Control Having no Time
Lag; naca-tm-1248; 1950
- I.A. Kiebel; Some
Studies on the Flow of a Gas in the Region of Transition Through the Velocity
of Sound; naca-tm-1252; 1950
- H. Blasius; The
Boundary Layers in Fluids with Little Friction; naca-tm-1256; 1950
- Maurice Roy; Theoretical
Investigations on the Efficiency and the Conditions for the Realization of Jet
Engines; naca-tm-1259; 1950
- Roger W. Luidens and
Robert T. Madden (Lewis Flight Propulsion Laboratory, Cleveland, Ohio); Interpretation
of Boundary-Layer Pressure-Rake Data in Flow with a Detached Shock;
naca-rm-e50i29a; 1950
- Hartmann, Melvin J,
Tysl, Edward R; Performance
of 24-inch supersonic axial-flow compressor in air III : compressor
performance with inlet guide vanes; naca-rm-e50d27; July 10, 1950
- Manuel Stein, J.
Mayers; A
small-deflection theory for curved sandwich plates; naca-report-1008;
1951
- Alvin H. Sacks, John R.
Spreiter; Theoretical
investigation of submerged inlets at low speeds; naca-tn-2323; August,
1951
- John M. Hedgepeth, S.
B. Batdorf, J. Lyell Sanders, Jr.; On
the angular distribution of slip lines in polycrystalline aluminum alloy;
naca-tn-2577; December 1951
- Hans Ekstein; X-ray
diffraction by bent crystal lamellae; naca-tn-2448; Sep 1951
- William Arthur Vogeley;
Axial-momentum
theory for propellers in compressible flow; naca-tn-2164; Jul 1951
- Morton Cooper, Robert
A. Webster; The use of an
uncalibrated cone for determination of flow angles and Mach numbers at
supersonic speeds; naca-tn-2190; Mar 1951
- Milton D. Van Dyke; A study of
second-order supersonic-flow theory; naca-tn-2200; Jan 1951
- Richard B. Skoog,
Harvey H. Brown; A
method for the determination of the spanwise load distribution of a flexible
swept wing at subsonic speeds; naca-tn-2222; Mar 1951
- Bernard E. Klunker,
Keith C. Harder; On
the second-order tunnel-wall-constriction corrections in two-dimensional
compressible flow; naca-tn-2350; Apr 1951
- Robert W. Higgins,
Constantine C. Pappas; An
experimental investigation of the effect of surface heating on boundary-layer
transition on a flat plate in supersonic flow; naca-tn-2351; Apr
1951
- William Bihrle, Jr.; Floating
characteristics of a plain and a horn-balanced rudder at spinning attitudes as
determined from rotary tests on a model of a typical low-wing personal-owner
airplane; naca-tn-2359; May 1951
- Richard J. Spahr,
Robert R. Dickey; Effect
of tail surfaces on the base drag of a body of revolution at Mach numbers of
1.5 and 2.0; naca-tn-2360; Apr 1951
- Braney H. Little, Jr.,
Stafford W. Wilbur; Turbulence-intensity
measurements in a jet of air issuing from a long tube; naca-tn-2361; May
1951
- E. S. Kavanaugh,
William Dale Drinkwater; Torsional
strength of stiffened D-tubes; naca-tn-2362; May 1951
- Eric Reissner; On
the application of Mathieu functions in the theory of subsonic compressible
flow past oscillating airfoils; naca-tn-2363; May 1951
- S. S. Shu; On
two-dimensional flow after a curved stationary shock (with special reference
to the problem of detached shock waves); naca-tn-2364; May 1951
- William R. Slivka,
David H. Silvern; Analytical
evaluation of aerodynamic characteristics of turbines with nontwisted rotor
blades; naca-tn-2365; May 1951
- Robert L. Johnson,
Marshal B. Peterson, Max A Swikert; Friction
at high sliding velocities of oxide films on steel surfaces
boundary-lubricated with stearic-acid solutions; naca-tn-2366; May
1951
- M. H. Lee Wu; General
plastic behavior and approximate solutions of rotating disk in
strain-hardening range; naca-tn-2367; May 1951
- Robert D. Ingebo; Vaporization
rates and heat-transfer coefficients for pure liquid drops; naca-tn-2368;
Jul 1951
- Eric Reissner, Manuel
Stein; Torsion and
transverse bending of cantilever plates; naca-tn-2369; Jun 1951
- John T. Sinette, Jr.,
George R. Costello; Possible
application of blade boundary-layer control to improvement of design and
off-design performance of axial-flow turbomachines; naca-tn-2371; May
1951
- Rudolph W. Hensel; Rectangular-wind-tunnel
blocking corrections using the velocity-ratio method; naca-tn-2372; Jun
1951
- Louis H. Smaus, Elwood
C. Stewart; Practical
methods of calculation involved in the experimental study of an autopilot and
the autopilot-aircraft combination; naca-tn-2373; Jun 1951
- Gordon L. Dugger; Effect of
initial mixture temperature on flame speed of methane-air, propane-air and
ethylene-air mixtures; naca-tn-2374; May 1951
- Donald S. Woolston,
Harry L. Runyan; On
the use of coupled modal functions in flutter analysis; naca-tn-2375; Jun
1951
- F. R. Steinbacher, C.
N. Gaylord, W. K. Rey; Method
for analyzing indeterminate structures stressed above proportional limit;
naca-tn-2376; Jun 1951
- W. A. Crouse, Margie
Carickhoff, Margaret A. Fisher; Effect
of fuel immersion on laminated plastics; naca-tn-2377; Jun 1951
- Aaron S. Boksenbom,
Richard Hood; Automatic
control systems satisfying certain general criterions on transient
behavior; naca-tn-2378; Jun 1951
- James R. Blackaby; An
investigation of the effects of jet-outlet cut-off angle on thrust direction
and body pitching moment; naca-tn-2379; Jun 1951
- Dwight G. Moore, Mary
A. Mason; Effectiveness
of ceramic coatings in reducing corrosion of five heat-resistant alloys by
lead-bromide vapors; naca-tn-2380; Jun 1951
- D. N. Frey, J. W.
Freeman, A. E. White; Fundamental
aging effects influencing high-temperature properties of solution-treated
Inconel X; naca-tn-2385; Jun 1951
- Dwight G. Moore,
Stanley G. Benner, William N. Harrison; Studies
of high-temperature protection of a titanium-carbide ceramal by chromium-type
ceramic-metal coatings; naca-tn-2386; Jun 1951
- H. J. Grover, S. M.
Bishop, L. R. Jackson; Fatigue
strengths of aircraft materials : axial-load fatigue tests on notched sheet
specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel with
stress-concentration factors of 2.0 and 4.0; naca-tn-2389; Jun 1951
- H. J. Grover, S. M.
Bishop, L. R. Jackson; Fatigue
strengths of aircraft materials : axial-load fatigue tests on notched sheet
specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel with
stress-concentration factor of 5.0; naca-tn-2390; Jun 1951
- Samuel Katzoff, Margery
E. Hannah; Further
comparisons of theoretical and experimental lift and pressure distributions on
airfoils in cascade at low-subsonic speed; naca-tn-2391; Aug 1951
- Roger A. Anderson; Charts giving
critical compressive stress of continuous flat sheet divided into
parallelogram-shaped panels; naca-tn-2392; Jul 1951
- M. Holt, I. D. Eaton;
Effects of
design details on the fatigue strength of 355-T6 sand-cast aluminum alloy;
naca-tn-2394; Jul 1951
- Donald A. Howard; Bench-test
investigation of the transient-response characteristics of several simulated
airplanes incorporating an autopilot sensitive to yawing accelerations;
naca-tn-2395; Jul 1951
- Arthur G. Holms, Joseph
E. Jenkins, Andrew J. Repko; Influence
of tensile strength and ductility on strengths of rotating disks in presence
of material and fabrication defects of several types; naca-tn-2397; Jun
1951
- Vernon A. Slabey, Paul
H. Wise; Synthesis of
cyclopropane hydrocarbons from methylcyclopropyl ketone III :
2-cyclopropyl-1-butene, cis and trans 2-cyclopropyl-2-butene, and
2-cyclopropylbutane; naca-tn-2398; Jun 1951
- Vernon J. Rossow; Applicability
of the hypersonic similarity rule to pressure distributions which include the
effects of rotation for bodies of revolution at zero angle of attack;
naca-tn-2399; Jun 1951
- Eckert, E R G Low,
George M; Temperature
distribution in internally heated walls of heat exchangers with noncircular
flow passages using coolants with very low Prandtl number; naca-tn-2401;
July 1951
- Sumner Alpert, Rose M.
Litrenta; Construction
and use of charts in design studies of gas turbines; naca-tn-2402; Jul
1951
- Fred E. Weick, L. E.
Flanagan, Jr., H. H. Cherry; An
analytical investigation of effect of high-lift flaps on take-off of light
airplanes; naca-tn-2404; Sep 1951
- Elmer A. Horton,
Stanley Frank Racisz, Nicholas J. Paradiso; Investigation
of NACA 64,2-432 and 64,3-440 airfoil sections with boundary-layer control and
an analytical study of their possible applications; naca-tn-2405; Jul
1951
- Ruth N. Weltmann,
Steven Fairweather, Daryl Papke; Application
of x-ray absorption to measurement of small air-density gradients;
naca-tn-2406; Jul 1951
- Chung-Hua Wu, Curtis A.
Brown; Method of
analysis for compressible flow arbitrary turbomachine blades on general
surface of revolution; naca-tn-2407; Jul 1951
- John D. Stanitz; Approximate
design method for high-solidity blade elements in compressors and
turbines; naca-tn-2408; Jul 1951
- Robert G. Deissler; Analytical
investigation of fully developed laminar flow in tubes with heat transfer with
fluid properties variable along the radius; naca-tn-2410; Jul 1951
- George P. Wood, Paul B.
Gooderum; Method of
determining initial tangents of contours of flow variables behind a curved,
axially symmetric shock wave; naca-tn-2411; Jul 1951
- John C. Martin, Frank
S. Malvestuto, Jr.; Theoretical
force and moments due to sideslip of a number of vertical tail configurations
at supersonic speeds; naca-tn-2412; Sep 1951
- Paul F. Barrett, Paul
Seide; An
experimental determination of the critical bending moment of a box beam
stiffened by posts; naca-tn-2414; Jul 1951
- Christopher C. Kraft,
Jr., Arthur Assadourian; Experimental
study of an angle-of-attack vane mounted ahead of the nose of an airplane for
use as a sensing device for an acceleration alleviator; naca-tn-2415; Jul
1951
- Albert I. Bellin,
Richard D. Messina, Paul B. Richards; Preliminary
study of stability of flow from two ducts discharging into a common duct;
naca-tn-2417; Jul 1951
- John D. Stanitz, Vasily
D. Prian; A
rapid approximate method for determining velocity distribution on impeller
blades of centrifugal compressors; naca-tn-2421; Jul 1951
- D. G. Moore, L. H.
Bolz, J. W. Pitts, W. N. Harrison; Study
of chromium-frit-type coatings for high-temperature protection of
molybdenum; naca-tn-2422; Jul 1951
- Harry C. Mickleboro,
Charles C. Shufflebarger; Flight
investigation of the effect of transient wing response on wing strains of a
twin-engine transport airplane in rough air; naca-tn-2424; Jul 1951
- Joseph Marin, B. H.
Ulrich, W. P. Hughes; Plastic
stress-strain relations for 75S-T6 aluminum alloy subjected to biaxial tensile
stresses; naca-tn-2425; Aug 1951
- Llewellyn M. K.
Boelter, V. D. Sanders, George Young, M. Morgan, E. H. Morrin; An
investigation of aircraft heaters XXXIV : experimental determination of
thermal and hydrodynamical behavior of air flowing between a flat and a
wave-shaped plate; naca-tn-2426; Aug 1951
- L. M. K. Boelter, R. W.
Lockhart; An
investigation of aircraft heaters XXXV : thermocouple conduction error
observed in measuring surface temperatures; naca-tn-2427; Jul 1951
- L. M. K. Boelter, W. R.
Elswick, V. D. Sanders, M. W. Rubesin; An
investigation of aircraft heaters XXXVI : preliminary investigation of a
combustion- type aircraft heater; naca-tn-2428; Aug 1951
- Raymond L. Chuan,
Richard J. Magnus; Study
of vortex shedding as related to self-excited torsional oscillations of an
airfoil; naca-tn-2429; Sep 1951
- Harold F. Hipsher, Paul
H. Wise; Synthesis,
purification and physical properties of hydrocarbons of the naphthalene series
I: 1-methylnaphthalene, 1-ethylnaphthalene, 1-butylnaphthalene, and
1-isobutylnaphthalene; naca-tn-2430; Aug 1951
- Fabio R. Goldshmied; Skin friction
of incompressible turbulent boundary layer under adverse pressure
gradients; naca-tn-2431; Aug 1951
- Luigi Crocco; Transformations
of the hodograph flow equation and the introduction of two generalized
potential functions; naca-tn-2432; Aug 1951
- W. F. Brown, Jr.,
George Sachs; A
critical review of notch sensitivity in stress-rupture tests;
naca-tn-2433; Aug 1951
- William A. Hickman,
Norris F. Dow; Direct-reading
design charts for 75S-T6 aluminum-alloy flat compression panels having
longitudinal extruded Z-section stiffeners; naca-tn-2435; May 1951
- Chan-Mou Tchen; Heat delivery
in a compressible flow and applications to hot-wire anemometry;
naca-tn-2436; Aug 1951
- Coleman dup Donaldson,
Jim J. Jones; Some
measurements of the effect of gaseous imperfections on the critical pressure
ratio in air and the speed of sound in nitrogen; naca-tn-2437; Aug
1951
- Jackson R. Stalder,
Glen Goodwin, Marcus O. Creager; Heat-transfer
to bodies in a high-speed rarefied-gas stream; naca-tn-2438; Aug
1951
- Rolf Landauer; A
theory of conductivity of cold-worked copper; naca-tn-2439; Sep
1951
- Donald R. Riley; Wind-tunnel
investigation and analysis of the effects of end plates on the aerodynamic
characteristics of an unswept wing; naca-tn-2440; Aug 1951
- Enoch J. Durbin; Optical methods
involving light scattering for measuring size and concentration of
condensation particles in supercooled hypersonic flow; naca-tn-2441; Aug
1951
- M. M. Frocht; A
photoelastic investigation of stress concentrations due to small fillets and
grooves in tension; naca-tn-2442; Aug 1951
- Frank M. Hamaker,
Stanford E. Neice, A. J. Eggers, Jr.; The
similarity law for hypersonic flow about slender three-dimensional shapes;
naca-tn-2443; Aug 1951
- B. M. Axilrod, Martha
A. Sherman; Effect of
stress-solvent crazing on tensile strength of polymethyl methacrylate;
naca-tn-2444; Aug 1951
- Paul E. Purser, M.
Leroy Spearman; Wind-tunnel
tests at low speed of swept and yawed wings having various plan forms;
naca-tn-2445; Dec 1951
- Hans Ekstein; Statistical
fluctuation of intensity in Debye-Scherrer lines due to random orientation of
crystal grains; naca-tn-2447; Aug 1951
- Benjamin Milwitzky,
Dean C. Lindquist; Evaluation
of the reduced-mass method of representing wing-lift effects in free-fall drop
tests of landing gears; naca-tn-2400; Jul 1951
- Hans Ekstein; Width
of Debye-Scherrer lines for finite spectral width of primary beam;
naca-tn-2446; Sep 1951
- Robert J. Cohen; Aerodynamic
characteristics of four bodies of revolution showing some effects of afterbody
shape and fineness ratio at free-stream Mach numbers from 1.50 to 1.99;
naca-rm-e51c06; may 1951
- Benson E. Gammon; Preliminary
evaluation of the air and fuel specific-impulse characteristics of several
potential ram-jet fuels I : octene-1, aluminum, and aluminum - octene-1
slurries; naca-rm-e51c12; Apr 1951
- Zelmar Barson, Arthur
F. Sargent, Jr.; Effect
of fuel volatility on performance of tail-pipe burner; naca-rm-e51c14; Apr
1951
- Eugene Perchonok, John
M. Farley; Internal flow
and burning characteristics of 16-inch ram jet operating in a free jet at Mach
numbers of 1.35 and 1.73; naca-rm-e51c16; May 1951
- Benson E. Gammon; Preliminary
evaluation of the air and fuel specific-impulse characteristics of several
potential ram-jet fuels II - magnesium and magnesium - octene-1 slurries;
naca-rm-e51c23; May 1951
- Leonard K. Tower,
Robert J. Branstetter; Combustion
performance evaluation of magnesium-hydrocarbon slurry blends in a simulated
tail-pipe burner; naca-rm-e51c26; May 1951
- James T. Dipiazza; Limits of
flammability of pure hydrocarbon-air mixtures at reduced pressures and room
temperature; naca-rm-e51c28; may 1951
- William H. Sterbentz,
John C. Evvard; Criterions
for prediction and control of ram-jet flow pulsations; naca-rm-e51c27; May
1951
- Robert W. Kahn, Shigeo
Nakanishi, James L. Harp, Jr.; Altitude-test-chamber
investigation of performance of a 28-inch ram-jet engine IV, effect of
inlet-air temperature, combustion-chamber-inlet Mach number, and fuel
volatility on combustion performance; naca-rm-e51d11; Jul 1951
- Donald J. Michel,
Ambrose Ginsberg, John Mizisin; Experimental
investigation of flow in the rotating passages of a 48-inch impeller at low
tip speeds; naca-rm-e51d20; Jun 1951
- Walter T. Olson, Louis
C. Gibbons; Status of
combustion research on high-energy fuels for ram jets; naca-rm-e51d23; Oct
1951
- Fred D. Kochendorfer,
Morris D. Rousso; Performance
characteristics of aircraft cooling ejectors having short cylindrical
shrouds; naca-rm-e51e01; May 1951
- Ralph E. Grey, H. G.
Krull, A. F. Sargent; Altitude
investigation of 16 flame-holder and fuel-system configurations in tail-pipe
burner; naca-rm-e51e03; Dec 1951
- Gerald Morrell; Investigation
of internal film cooling of 1000-pound-thrust liquid-ammonia - liquid-oxygen
rocket-engine combustion chamber; naca-rm-e51e04; Jul 1951
- Robert T. Madden, Emil
J. Kremzier; Data
presentation of force characteristics of several engine-strut-body
configurations at Mach numbers of 1.8 and 2.0; naca-rm-e51e29; Aug
1951
- Albert W. Hall, James
M. McKay; Comparison of
airfoil sections on two triangular-wing-fuselage configurations at transonic
speeds from tests by the NACA wing-flow method; naca-rm-l51f01; Aug
1951
- Morris D. Rousso, Fred
D. Kochendorfer; Velocity
and temperature fields in circular jet expanding from choked nozzle into
quiescent air; naca-rm-e51f18; Jul 1951
- Edgar M. Cortright,
Jr., Albert H. Schroeder; Investigation
at Mach number 1.91 of side and base pressure distributions over conical
boattails without and with jet flow issuing from base; naca-rm-e51f26; Sep
1951
- Fred H. Goelzer, Edgar
M. Cortright, Jr.; Investigation
at Mach number 1.88 of half of a conical-spike diffuser mounted as a side
inlet with boundary-layer control; naca-rm-e51g06; Sep 1951
- Clarence C. Gettelman,
Lloyd N. Krause; Characteristics
of a wedge with various holder configurations for static-pressure measurements
in subsonic gas streams; naca-rm-e51g09; Sep 1951
- Leonard Rudlin; Preliminary
results of a determination of temperatures of flames by means of K-band
microwave attenuation; naca-rm-e51g20; Sep 1951
- E. Howard, R. W.
Luidens, J. L. Allen; Force
and pressure characteristics for a series of nose inlets at Mach numbers from
1.59 to 1.99 V : analysis and comparison on basis of ram-jet aircraft range
and operational characteristics; naca-rm-e51g23; Sep 1951
- Eugene Perchonok, Fred
Wilcox, Donald Pennington; Effect
of angle of attack and exit nozzle design on the performance of a 16-inch ram
jet at Mach numbers from 1.5 to 2.0; naca-rm-e51g26; Oct 1951
- Philip J. Evans, Jr.;
Analytical
investigation of ram-jet-engine performance in flight Mach number range from 3
to 7; naca-rm-e51h02; Oct 1951
- John R. Jack, Warren C.
Burgess; Aerodynamics of
slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6)
to 15 x 10(exp 6) : body of revolution with near-parabolic forebody and
cylindrical afterbody; naca-rm-e51h13; Nov 1951
- John R. Jack; Aerodynamic
characteristics of a slender cone-cylinder body of revolution at a Mach number
of 3.85; naca-rm-e51h17; Nov 1951
- Eugene D. Schult; Large-scale
flight measurements of zero-lift drag at Mach numbers from 0.8 to 1.6 of a
wing-body combination having an unswept 4.5 percent thick wing with modified
hexagonal sections; naca-rm-l51a15; Mar 1951
- Paul E. Purser; Notes on
low-lift buffeting and wing dropping at Mach numbers near 1;
naca-rm-l51a30; Mar 1951
- Harold S. Johnson; Wind-tunnel
investigation at subsonic and low transonic speeds of the effects of aileron
span and spanwise location on the rolling characteristics of a test vehicle
with three untapered 45 degree sweptback wings; naca-rm-l51b16; Apr
1951
- Norman F. Smith, Julian
H. Kainer, Robert A. Webster; An
investigation of a supersonic aircraft configuration having a tapered wing
with circular-arc section and 40 degree sweepback : a pressure-distribution
study of the aerodynamic characteristics of the wing at Mach number 1.40;
naca-rm-l51c06; Apr 1951
- David G. Stone; Comparisons of
the effectiveness and hinge moments of all-movable delta and flap-type
controls on various wings; naca-rm-l51c22; Apr 1951
- William B. Pepper, Jr.,
Sherwood Hoffman; Comparison
of zero-lift drags determined by flight tests at transonic speeds of
symmetrically mounted nacelles in various spanwise positions on a 45 degrees
sweptback wing and body combination; naca-rm-l51d06; May 1951
- Arvo A. Luoma; Aerodynamic
characteristics of four wings of sweepback angles 0 degree, 35 degrees, 45
degrees, and 60 degrees, NACA 65A006 airfoil section, aspect ratio 4, and
taper ratio 0.6 in combination with a fuselage at high subsonic Mach numbers
and Mach num; naca-rm-l51d13; Jun 1951
- Charles H. McLellan,
Mitchel H. Bertram, John A. Moore; An
investigation of four wings of square plan form at a Mach number of 6.86 in
the Langley 11-inch hypersonic tunnel; naca-rm-l51d17; Jun 1951
- H. Kurt Strass, E. M.
Fields, Eugene D. Schult; Some
effects of spanwise aileron location and wing structural rigidity on the
rolling effectiveness of 0.3-chord flap-type ailerons on a tapered wing having
63 degrees sweepback at the leading edge and NACA 64A005; naca-rm-l51d18a;
Jun 1951
- William M. Bland, Jr.,
Albert E. Dietz; Some
effects of fuselage interference, wing interference, and sweepback on the
damping in roll of untapered wings as determined by techniques employing
rocket-propelled vehicles; naca-rm-l51d25; Oct 1951
- Edward F. Ulmann,
Douglas R. Lord; An
investigation of flow characteristics at Mach number 4.04 over 6- and
9-percent-thick; naca-rm-l51d30; Jul 1951
- Richard I. Sears, C. F.
Merlet; Flight
determination of drag and pressure recovery of a nose inlet of parabolic
profile at Mach numbers from 0.8 to 1.7; naca-rm-l51e02; Oct 1951
- Paul E. Purser; Review of some
recent data on buffet boundaries; naca-rm-l51e02a; May 1951
- John G. Lowry, Jones F.
Cahill; Review of the
maximum-lift characteristics of thin and swept wings; naca-rm-l51e03; Jun
1951
- Jacob Zarovsky; System analyses
and autopilot design for automatic roll stabilization of a supersonic
pilotless aircraft; naca-rm-l51e07; Jul 1951
- Mitchell Lopatoff; Wind-flow study
of pressure-drag reduction at transonic speed by projecting a jet of air from
the nose of a prolate spheroid of fineness ratio 6; naca-rm-l51e09; Oct
1951
- Joseph Weil, Edward C.
Polhamus; Aerodynamic
characteristics of wings designed for structural improvement;
naca-rm-l51e10a; May 1951
- John P. Mayer, Clarence
L. Gillis; Division of
load among the wing, fuselage, and tail of aircraft; naca-rm-l51e14a; May
1951
- Clement J. Welsh,
Carlos A. Demoraes; Results
of flight tests to determine drag of parabolic and cone-cylinder bodies of
very large fineness ratios at supersonic speeds; naca-rm-l51e18; Aug
1951
- Roger G. Hart; Flight
investigation of the drag of round-nosed bodies of revolution at Mach numbers
from 0.6 to 1.5 using rocket-propelled test vehicles; naca-rm-l51e25; Jul
1951
- Ira R. Schwartz; A preliminary
investigation of combustion with rotating flow in an annular combustion
chamber; naca-rm-l51e25a; Sep 1951
- Franklin W. Deiderich,
W. Owen Latham; Calculated
aerodynamic loadings of M, W, and delta wings in incompressible flow;
naca-rm-l51e29; Aug 1951
- Robert W. Herr; Preliminary
experimental investigation of flutter characteristics of M and W wings;
naca-rm-l51e31; Aug 1951
- Donald L. Loving,
Claude V. Williams; Basic
pressure measurements on a fuselage and a 45 degrees sweptback wing-fuselage
combination at transonic speeds in the slotted test section of the Langley
8-foot high-speed tunnel; naca-rm-l51f05; Sep 1951
- Vernard E. Lockwood,
Joseph E. Fikes; Aerodynamic
characteristics at transonic speeds of a tapered 45 degree sweptback wing of
aspect ratio 3 having a full-span flap-type control; naca-rm-l51f06a; Aug
1951
- Donald L. Loving, Bruce
B. Estabrooks; Transonic-wing
investigation in the Langley 8-foot high-speed tunnel at high subsonic Mach
numbers and at a Mach number of 1.2 : analysis of pressure distribution of
wing-fuselage configuration having a wing of 45 degrees sweptback, aspect
ratio 4, t; naca-rm-l51f07; Sep 1951
- Warren A. Tucker; A method for
the design of sweptback wings warped to produce specified flight
characteristics at supersonic speeds; naca-rm-l51f08; Sep 1951
- Ray H. Wright, Virgil
S. Ritchie; Characteristics
of a transonic test section with various slot shapes in the Langley 8-foot
high-speed tunnel; naca-rm-l51h10; Oct 1951
- Claude E. Sanders, Jr.;
Damping in
roll of straight and 45 degree swept wings of various taper ratios determined
at high subsonic, transonic, and supersonic speeds with rocket-powered
models; naca-rm-l51h14; Oct 1951
- Charles F. Hall, John
C. Heitmeyer; Lift,
drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic
speeds : twisted and cambered triangular wing of aspect ratio 2 with NACA
0003-63 thickness distribution; naca-rm-a51e01; Jun 1951
- James M. McKay, Albert
W. Hall; The
effects on the aerodynamic characteristics of reversing the wing of a
triangular wing-body combination at transonic speeds as determined by the NACA
wing-flow method; naca-rm-l51h23; Oct 1951
- William C. Moseley,
Jr., James M. Watson; Investigation
of wing-tip ailerons on a 51.3 degrees sweptback wing at transonic speeds by
the transonic-bump method; naca-rm-l51h27; Nov 1951
- Ralph P. Bielat, Daniel
E. Harrison, Domenic A. Coppolino; An
investigation at transonic speeds of the effects of thickness ratio and of
thickened root sections on the aerodynamic characteristics of wings with 47
degrees sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test
section of the Lang; naca-rm-l51i04a; Oct 1951
- Byron M. Jaquet, M. J.
Queijo; Low-speed
wind-tunnel investigation of lateral control characteristics of a 60 degrees
triangular-wing model having half-delta tip controls; naca-rm-l51i10; Nov
1951
- Milton D. Humphreys; Pressure
pulsations on rigid airfoils at transonic speeds; naca-rm-l51i12; Dec
1951
- William C. Martz, James
D. Church, John W. Goslee; Free-flight
investigation to determine force and hinge-moment characteristics at zero
angle of attack of a 60 degrees sweptback half-delta tip control on a 60
degrees sweptback delta wing at Mach numbers between 0.68 and 1.44;
naca-rm-l51i14; Dec 1951
- Benson E. Gammon; Preliminary
evaluation of the air and fuel specific-impulse characteristics of several
potential ram-jet fuels IV - hydrogen, a-methylnaphthalene, and carbon;
naca-rm-e51f05; Aug 1951
- Robert W. Rainey; Langley 9-inch
supersonic tunnel tests of several modifications of a supersonic missile
having tandem cruciform lifting surfaces : three-component data results of
models having ratios of wing span to tail span equal to 1; naca-rm-l9l30;
Mar 1951
- Lionel L. Levy, Jr.,
Earl D. Knechtel; Experimental
study of the effect of sweepback on transonic aileron flutter;
naca-rm-a51e04; Sep 1951
- E. Ray Phelps, Frank A.
Lazzeroni; Wind-tunnel
investigation of the aerodynamic characteristics of a one-fifteenth-scale
model of the Northrop MX-775A missile; naca-rm-a51e28; Oct 1951
- Earl C. Watson; Some low-speed
characteristics of an air-induction system having scoop-type inlets with
provisions for boundary-layer control; naca-rm-a51f15; Aug 1951
- Howard F. Matthews,
Elwood C. Stewart; A
comparison of the calculated maximum-maneuver response characteristics of
three air-to-air, beam-rider, guided missiles having different lift
ratios; naca-rm-a51f18; Sep 1951
- Edward W. Perkins,
Forrest E. Gowen, Leland H. Jorgensen; Aerodynamic
characteristics of the NACA RM-10 research missile in the Ames 1- by 3- foot
supersonic wind tunnel no. 2 : pressure and force measurements at Mach numbers
of 1.52 and 1.98; naca-rm-a51g13; Sep 1951
- Edward J. Hopkins,
Hubert C. Carel; Experimental
and theoretical study of the effects of body size on the aerodynamic
characteristics of an aspect ratio 3.0 wing-body combination;
naca-rm-a51g24; Oct 1951
- William C. Triplett, G.
Allan Smith; Longitudinal
frequency-response characteristics of a 35 degree swept-wing airplane as
determined from flight measurements, including a method for the evaluation of
transfer functions; naca-rm-a51g27; Sep 1951
- John C. Heitmeyer; Lift, drag, and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds :
plane triangular wing of aspect ratio 3 with NACA 0003-63 section;
naca-rm-a51h02; Sep 1951
- John C. Heitmeyer; Lift, drag, and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds :
plane 45 degree swept-back wing of aspect ratio 3, taper ratio 0.4 with
3-percent- thick, biconvex section; naca-rm-a51h10; Sep 1951
- Maurice D. White, Bonne
C. Look; Load
distribution over a fuselage in combination with a swept wing at small angles
of attack and transonic speeds; naca-rm-a51h15; Nov 1951
- James Selna, Bernard A.
Schlaff; An
investigation of the drag and pressure recovery of a submerged inlet and a
nose inlet in the transonic flight range with free-fall models;
naca-rm-a51h20; Dec 1951
- John C. Heitmeyer; Lift, drag, and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds :
body of revolution; naca-rm-a51h22; Oct 1951
- Jack D. Stephenson,
Ralph Selan; The static
longitudinal characteristics at Mach numbers up to 0.95 of a triangular-wing
canard model having a triangular control; naca-rm-a51i07; Dec 1951
- W. C. Hugli, Jr., W. C.
Axt; Hydrodynamic
investigation of a series of hull models suitable for small flying boats and
amphibians; naca-tn-2503; November, 1953
- Joseph W. Cleary,
George L. Stevens; The
effects at transonic speeds of thickening the trailing edge of a wing with a
4-percent-thick circular-arc airfoil; naca-rm-a51j11; Dec 1951
- Hardrath, Herbert F
Ohman, Lachlan; A
study of elastic and plastic stress concentration factors due to notches and
fillets in flat plates; naca-tn-2566; December 1951
- Alvin Seiff, Carl A
Sandahl; The
effect of nose shape on the drag of bodies of revolution at zero angle of
attack; naca-rm-a51j25; Nov 1951
- Morris W. Rubesin,
Charles B. Rumsey, Steven A. Varga; A
summary of available knowledge concerning skin friction and heat transfer and
its application to the design of high-speed missiles; naca-rm-a51j25a; Nov
1951
- Richard Scherrer, David
H. Dennis; Lateral control
characteristics and dihedral effect of a wing-body combination with a variable
incidence triangular wing and wing-tip ailerons at a Mach number of 1.52;
naca-rm-a50h10; Jan 1951
- E. Ray Phelps; A
comparison of the experimental and theoretical loading over triangular wings
at supersonic speeds; naca-rm-a50j17; Jan 1953
- Duberg, John E Wilder,
Thomas W , III; Inelastic
column behavior; naca-tn-2267; 1951
- Fred B. Sutton, Andrew
Martin; Aerodynamic
characteristics including pressure distribution of a fuselage and three
combinations of the fuselage with swept-back wings at high subsonic
speeds; naca-rm-a50j26a; Feb 1951
- Robert N. Olson,
Merrill H. Mead; Aerodynamic
study of a wing-fuselage combination employing a wing swept back 63 degrees :
effectiveness at supersonic speeds of a 30-percent chord, 50-percent semispan
elevon as a lateral control device; naca-rm-a50k07; Jan 1951
- Donald W. Smith, John
C. Heitmeyer; Lift,
drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic
speeds : plane triangular wing of aspect ratio 2 with NACA 0005-63
section; naca-rm-a50k21; Feb 1951
- John C. Heitmeyer, Jack
D. Stephenson; Lift,
drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic
speeds : plane triangular wing of aspect ratio 4 with NACA 0005-63
section; naca-rm-a50k24; Feb 1951
- John C. Heitmeyer,
Willard G. Smith; Lift,
drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic
speeds : plane triangular wing of aspect ratio 2 with NACA 0003-63
section; naca-rm-a50k24a; Feb 1951
- E. Ray Phelps, Willard
G. Smith; Lift, drag, and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds :
triangular wing of aspect ratio 4 with NACA 0005-63 thickness distribution,
cambered and twisted for trapezoidal span load distribution;
naca-rm-a50k24b; Feb 1951
- Willard G. Smith, E.
Ray Phelps; Lift, drag, and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds -
triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution,
cambered and twisted for a trapezoidal span load distribution;
naca-rm-a50k27a; Feb 1951
- David E. Reese, E. Ray
Phelps; Lift, drag, and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds :
plane tapered wing of aspect ratio 3.1 with 3-percent-thick, biconvex
section; naca-rm-a50k28; Jan 1951
- Julian H. Allen, Edward
W. Perkins; Characteristics
of flow over inclined bodies of revolution; naca-rm-a50l07; Mar
1951
- Richard Scherrer, David
H. Dennis; Damping in a
roll of a missile configuration with a modified triangular wing and a
cruciform tail at a Mach number of 1.52; naca-rm-a51a03; Mar 1951
- John F. Stroud, Warren
E. Anderson; Preliminary
data on the effect of body-nose bluntness on the drag and pressure recovery of
a side-inlet-body combination at Mach numbers of 1.4 and 1.7;
naca-rm-a51a09; Apr 1951
- Richard J. Spahr,
Robert A. Robinson; Wind-tunnel
investigation at Mach numbers of 1.5 and 2.0 of a canard missile
configuration; naca-rm-a51c08; May 1951
- George B. Brajnikoff,
Arthur W. Rogers; Characteristics
of four nose inlets as measured at Mach numbers between 1.4 and 2.0;
naca-rm-a51c12; Jun 1951
- John W. Boyd; A
comparison of the experimental and theoretical loading over triangular wings
in sideslip at supersonic speeds; naca-rm-a51c13; May 1951
- John C. Heitmeyer; Lift, drag, and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds :
plane triangular wing of aspect ratio 4 with 3-percent-thick, biconvex
section; naca-rm-a51d30; Jun 1951
- Carpenter, Paul J; Effects of
compressibility on the performance of two full-scale helicopter rotors;
naca-tn-2277; 1951
- George B. McCullough,
Donald E. Gault; Examples
of Three representative types of airfoil section stall at low speeds;
naca-tn-2502; September 1951
- Robert W. Rainey; Langley 9-inch
supersonic tunnel tests of several modifications of a supersonic missile;
naca-rm-l50i29a; Mar 1951
- Norman S. Silsby, James
M. McKay; Contributions
of wing, tail, and fuselage to the aerodynamic characteristics of a semispan
model of a supersonic airplane configuration at transonic speeds from tests by
the NACA wing-flow method; naca-rm-l51e01; Jul 1951
- Michael F. Valerino,
Ronald B. Doyle; Method
for determining pressure drop of monatomic gases flowing in turbulent motion
through constant-area passages with simultaneous friction and heat
addition; naca-tn-2328; Apr 1951
- Franklin W. Diederich;
Charts and
tables for use in calculations of downwash of wings of arbitrary plan
form; naca-tn-2353; May 1951
- Alois T. Sutor, Morris
A. Zipkin; Method of
matching components and predicting performance of turbine-propeller
engine; naca-tn-2450; Sep 1951
- I. Flugge-Lotz; Mathematical
improvement of method for computing Poisson integrals involved in
determination of velocity distribution on airfoils; naca-tn-2451; Oct
1951
- I. D. Eaton, Marshall
Holt; Flexural
fatigue strengths of riveted box beams - Alclad 14S-T6, Alclad 75S-T6, and
various tempers of Alclad 24S; naca-tn-2452; Nov 1951
- Robert F. Smiley; An experimental
study of water-pressure distributions during landings and planing of a heavily
loaded rectangular flat-plate model; naca-tn-2453; Sep 1951
- James C. Sivells,
Rachel M. Salmi; Jet-boundary
corrections for complete and semispan swept wings in closed circular wind
tunnels; naca-tn-2454; Sep 1951
- Chung-Hua Wu, Curtis A.
Brown; A
method of designing turbomachine blades with a desirable thickness
distribution for compressible flow along an arbitrary stream filament of
revolution; naca-tn-2455; Sep 1951
- Michael Behun, Harrison
C. Chandler, Jr.; Analytical
method for determining performance of turbojet-engine tail-pipe heat
exchangers; naca-tn-2456; Sep 1951
- Charles E. Watkins; Air forces and
moments on triangular and related wings with subsonic leading edges
oscillating in supersonic potential flow; naca-tn-2457; Sep 1951
- Rinaldo J. Brun, Joseph
Levine, Kenneth S. Kleinknecht; An
instrument employing a coronal discharge for the determination of droplet-size
distribution in clouds; naca-tn-2458; Sep 1951
- Erva C. Levine,
Marshall B. Peterson; Formation
of sulfide films on steel and effect of such films on static friction;
naca-tn-2460; Sep 1951
- H. J. Cunningham; Analysis of
pure-bending flutter of a cantilever swept wing and its relation to
bending-torsion flutter; naca-tn-2461; Sep 1951
- Martin R. Kinsler; Influence of
refraction on the applicability of the Zehnder-Mach interferometer to studies
of cooled boundary layers; naca-tn-2462; Sep 1951
- William J. Bursnall,
Lawrence K. Loftin, Jr.; Experimental
investigation of the pressure distribution about a yawed circular cylinder in
the critical Reynolds number range; naca-tn-2463; Sep 1951
- Gaylord O. Ellis, John
D. Stanitz, Leonard J. Sheldrake; Two
axial-symmetry solutions for incompressible flow through a centrifugal
compressor with and without inducer vanes; naca-tn-2464; Sep 1951
- Edmund E. Callaghan,
Robert S. Ruggeri; A
general correlation of temperature profiles downstream of a heated-air jet
directed perpendicularly to an air stream; naca-tn-2466; Sep 1951
- Chieh-Chien Chang; The aerodynamic
behavior of a harmonically oscillating finite sweptback wing in supersonic
flow; naca-tn-2467; Oct 1951
- John J. Harper; Investigation
at low speed of 45 degrees and 60 degrees sweptback, tapered, low-drag wings
equipped with various types of full-span, trailing-edge flaps;
naca-tn-2468; Oct 1951
- J. W. Freeman, E. E.
Reynolds, A. E. White; Rupture
properties of low carbon N-155 type alloys made with a columbium-tantalum
ferro-alloy; naca-tn-2469; Oct 1951
- Ordway B. Gates, Jr.,
Leonard Sternfield; Effect
of an autopilot sensitive to yawing velocity on the lateral stability of a
typical high-speed airplane; naca-tn-2470; Sep 1951
- Franklin K. Moore; Unsteady
laminar boundary-layer flow; naca-tn-2471; Sep 1951
- D. N. Frey, J. W.
Freeman, A. E. White; Fundamental
effects of cold-working on creep properties of low-carbon N-155 alloy;
naca-tn-2472; Oct 1051
- H. W. Liepmann, J.
Laufer, Kate Liepmann; On
the spectrum of isotropic turbulence; naca-tn-2473; Nov 1951
- Walter Castles, Jr.,
Robin B. Gray; Empirical
relation between induced velocity, thrust, and rate of descent of a helicopter
rotor as determined by wind-tunnel tests on four model rotors;
naca-tn-2474; Oct 1951
- Norman R. Bergrun; An empirical
method permitting rapid determination of the area, rate, and distribution of
water-drop impingement on an airfoil of arbitrary section at subsonic
speeds; naca-tn-2476; Sep 1951
- James H. Walls; Investigation
of the air-compression process during drop tests of an oleo-pneumatic landing
gear; naca-tn-2477; Sep 1951
- Kennedy F. Rubert,
Jerome Persh; A
procedure for calculating the development of turbulent boundary layers under
the influence of adverse pressure gradients; naca-tn-2478; Sep 1951
- W. Byron Brown, Patrick
L. Donoughe; Tables of exact
laminar-boundary-layer solutions when the wall is porous and fluid properties
are variable; naca-tn-2479; Sep 1951
- Thomas F. Gelder, James
P. Lewis; Comparison of
heat transfer from airfoil in natural and simulated icing conditions;
naca-tn-2480; Sep 1951
- Marvin Schulderfrei,
Paul Comisarow, Kenneth W. Goodson; Stability
and control characteristics of a complete airplane model having a wing with
quarter-chord line swept back 40 degrees, aspect ratio 2.50, and taper ratio
0.42; naca-tn-2482; Dec 1951
- John D. Bird, Byron M.
Jaquet, John W. Cowan; Effect
of fuselage and tail surfaces on low-speed yawing characteristics of a
swept-wing model as determined in curved-flow test section of Langley
stability tunnel; naca-tn-2483; Oct 1951
- Stanley H. Scher; Pilot escape
from spinning airplanes as determined from free-spinning-tunnel tests;
naca-tn-2485; Oct 1951
- Robert R. Morrissette,
Lester F. Oborny; Theoretical
characteristics of two-dimensional supersonic control surfaces;
naca-tn-2486; Oct 1951
- Harvey H. Brown; Flight
investigation of some factors affecting the critical tail loads on large
airplanes; naca-tn-2490; Sep 1951
- William G. Lidman, H.
J. Hamjian; Kinetics of
sintering chromium carbide; naca-tn-2491; Aug 1951
- Chung-Hua Wu, Eleanor
L. Costilow; A method of
solving the direct and inverse problem of supersonic flow along arbitrary
stream filaments of revolution in turbomachines; naca-tn-2492; Sep
1951
- H. J. Reissner, L.
Meyerhoff; Analysis of an
axial compressor stage with infinitesimal and finite blade spacing;
naca-tn-2493; Oct 1951
- Herbert C. Nelson; Lift and moment
on oscillating triangular and related wings with supersonic edges;
naca-tn-2494; Sep 1951
- John J. Harper; Wind-tunnel
investigation of effects of various aerodynamic balance shapes and sweepback
on control-surface characteristics of semispan tail surfaces with NACA 0009,
0015, 66-009, 66(215)-014, and circular-arc airfoil sections;
naca-tn-2495; Oct 1951
- Harvard Lomax, Max A.
Heaslet; Generalized
conical-flow fields in supersonic wing theory; naca-tn-2497; Sep
1951
- Harry Press, Herbert C.
McClanahan, Jr.; Flight
investigation of the effect of atmospheric turbulence on the climb performance
of an airplane; naca-tn-2498; Oct 1051
- E. B. Klunker, F.
Edward McLean; Laminar
friction and heat transfer at Mach numbers from 1 to 10; naca-tn-2499; Oct
1951
- Altman, John M Hayter,
Nora-Lee F; A comparison of
the turbulent boundary-layer growth on an unswept and a swept wing;
naca-tn-2500; September 1951
- Sinnette, John T
Costello, George R Cummings, Robert L; Expressions
for measuring the accuracy of approximate solutions to compressible flow
through cascades of blades with examples of use; naca-tn-2501; October
1951
- Goodman, Alex; Effects
of wing position and horizontal-tail position on the static stability
characteristics of models with unswept and 45 degree sweptback surfaces with
some reference to mutual interference; naca-tn-2504; October 1951
- Shen, S F
(Massachusetts Institute of Technology) Lin, C C (Massachusetts Institute of
Technology); On the attached
curved shock in front of a sharp-nosed axially symmetrical body placed in a
uniform stream; naca-tn-2505; October 1951
- Lin, C C (Massachusetts
Institute of Technology) Shen, S F (Massachusetts Institute of Technology); An analytic
determination of the flow behind a symmetrical curved shock; naca-tn-2506;
October 1951
- Dubois, G B (Cornell
University) Mabie, H H (Cornell University) Ocvirk, F W (Cornell University);
Experimental
investigation of oil film pressure distribution for misaligned plain
bearings; naca-tn-2507; October 1951
- Benson, James M Havens,
Robert F Woodward, David R; Landing
characteristics in waves of three dynamic models of flying boats;
naca-tn-2508; 1952
- Lawrence, Leslie F
Schmidt, Stanley F Looschen, Floyd W; A
self-synchronizing stroboscopic Schlieren system for the study of unsteady air
flows; naca-tn-2509; October 1951
- Hacker, Paul T; Experimental
values of the surface tension of supercooled water; naca-tn-2510; October
1951
- Braun, W H Klein, M M;
Calculation
of higher approximations for two-dimensional compressible flow by a simplified
iteration process; naca-tn-2511; October 1951
- Hoffman, C A Robards, C
F; Effects
of some solution treatments followed by an aging treatment on the life of
small cast gas-turbine blades of a cobalt-chromium-base alloy II : effect of
selected combinations of soaking time, temperature, and cooling rate;
naca-tn-2513; October 1951
- Hubka, Ralph E Dow,
Norris F Seide, Paul; Relative
structural efficiencies of flat balsa-core sandwich and stiffened-panel
construction; naca-tn-2514; October 1951
- Ferri, Antonio; The linearized
characteristics method and its application to practical nonlinear supersonic
problems; naca-tn-2515; October 1951
- SCHWOPE A D (Battelle
Memorial Institute) Jackson, L R (Battelle Memorial Institute); A
survey of creep in metals; naca-tn-2516; November 1951
- Boetler, L M K
(University of California) Young, G (University of California) Greenfield, M L
(University of California) Sanders, V D (University of California) Morgan, M
(University of California); An
investigation of aircraft heaters XXXVII : experimental determination of
thermal and hydrodynamical behavior of air flowing along a flat plate
containing turbulence promotors; naca-tn-2517; October 1951
- Burgess, Warren C , Jr
Seashore, Ferris L; Criterions
for condensation-free flow in supersonic tunnels; naca-tn-2518; December
1951
- Krause, Lloyd N; Effects of
pressure-rake design parameters on static-pressure measurement for rakes used
in subsonic free jets; naca-tn-2520; October 1951
- Moore, Franklin K; Laminar
boundary layer on a circular cone in supersonic flow at a small angle of
attack; naca-tn-2521; October 1951
- Smith, Earl F; A
graphical method for plotting amplitude and phase angle of transfer functions
of dynamic systems without factoring polynomials; naca-tn-2522; November
1951
- Mcandrew, Joseph B
(Armour Research Foundation) Colner, William H (Armour Research Foundation)
Francis, Howard T (Armour Research Foundation); Rotogenerative
detection of corrosion currents; naca-tn-2523; November 1951
- Boelter, L M K
(University of California) Sanders, V D (University of California) Romie, F E
(University of California); An
investigation of aircraft heaters XXXVIII : determination of thermal
performance of rectangular- and trapezoidal-shaped inner-skin passages for
anti-icing systems; naca-tn-2524; November 1951
- Gadeberg, Burnett L; The effect of
rate of change of angle of attack on the maximum lift coefficient of a pursuit
airplane; naca-tn-2525; October 1951
- Pinkel, I Irving; Determination
of ram-jet combustion-chamber temperatures by means of total-pressure
surveys; naca-tn-2526; December 1951
- Ivey, H Reese Harder,
Keith C; A
velocity-correction formula for the calculation of transonic mach number
distributions over diamond-shaped airfoils; naca-tn-2527; November
1951
- Yaggy, Paul F; A
method for predicting the upwash angles induced at the propeller plane of a
combination of bodies with an upswept wing; naca-tn-2528; October
1951
- Benscoter, Stanley
Urner (California Institute of Technology); Secondary
stresses in thin-walled beams with closed cross sections; naca-tn-2529;
October 1951
- Russell, Walter R
Gracey, William Letko, William Fournier, Paul G; Wind-tunnel
investigation of six shielded total-pressure tubes at high angles of attack
subsonic speeds; naca-tn-2530; November 1951
- Low, George M; Simplified
method for calculation of compressible laminar boundary with arbitrary
free-stream pressure gradient; naca-tn-2531; October 1951
- Dorsch, Robert G Boyd,
Bemrose; X-ray
diffraction study of the internal structure of supercooled water;
naca-tn-2532; October 1951
- Halfman, Robert L
(Massachusetts Institute of Technology) Johnson, H C (Massachusetts Institute
of Technology) Haley, S M (Massachusetts Institute of Technology); Evaluation
of high-angle attack aerodynamic-derivative data and stall-flutter prediction
techniques; naca-tn-2533; November 1951
- Goodman, Alex Wolhart,
Walter D; Experimental
investigation of the low-speed static and yawing stability characteristics of
a 45 degrees sweptback high-wing configuration with various twin vertical wing
fins; naca-tn-2534; November 1951
- Fuller, Franklyn B
Briggs, Benjamin R; Minimum
wave drag of bodies of revolution with a cylindrical center section;
naca-tn-2535; October 1951
- Johnson, Aldie E , Jr
Buchert, Kenneth P; Critical
combinations of bending, shear, and transverse compressive stresses for
buckling of infinitely long flat plates; naca-tn-2536; December
1951
- Walker, Richard (Iowa
State College); Heat
capacity lag in gases; naca-tn-2537; November 1951
- Hess, W F (Rensselaer
Polytechnic Institute) Wyant, R A (Rensselaer Polytechnic Institute) Winsor, F
J (Rensselaer Polytechnic Institute) Nash, R R (Rensselaer Polytechnic
Institute); Mechanical and
corrosion tests of spot-welded aluminum alloys; naca-tn-2538; December
1951
- Wang, Chi-Teh (New York
University) Chou, Pei-Chi (New York University); Application
of variational methods to transonic flows with shock waves; naca-tn-2539;
November 1951
- Serbin, H (Purdue
University) Costilow, E L (Purdue University); Application
of response function to calculation of flutter characteristics of a wing
carrying concentrated masses; naca-tn-2540; November 1951
- Lin, C C (Massachusetts
Institute of Technology) Shen, S F (Massachusetts Institute of Technology); Studies on von
Karman's similarity theory and its extension to compressible flows : a
critical examination of similarity theory for incompressible flows;
naca-tn-2541; November 1951
- Lin, C C (Massachusetts
Institute of Technology) Shen, S F (Massachusetts Institute of Technology); Studies of von
Karman's similarity theory and its extension to compressible flows : a
similarity theory for turbulent boundary layer over a flat plate in
compressible flow; naca-tn-2542; November 1951
- Shen, S F; Studies
of von Karman's similarity theory and its extension to compressible flow :
investigation of turbulent boundary layer over a flat plate in compressible
flow by the similarity theory; naca-tn-2543; November 1951
- Dayton, R W (Battelle
Memorial Institute) Simons, E M (Battelle Memorial Institute); The
hydrodynamic lubrication of cyclically loaded bearings; naca-tn-2544;
November 1951
- Dayton, R W (Battelle
Memorial Institute) Simons, E M (Battelle Memorial Institute) Fend, F A
(Battelle Memorial Institute); Discrepancies
between theoretical and observed behavior of cyclically loaded bearings;
naca-tn-2545; November 1951
- Johnston, Herrick L
(Ohio State University) Mattox, Robert W (Ohio State University) Powers,
Robert W (Ohio State University); Viscosities
of air and nitrogen at low pressures; naca-tn-2546; November 1951
- Ehlers, F Edwards
(Brown University) Cohen, Hirsh G (Brown University); An
investigation by the hodograph method of flow through a symmetrical nozzle
with locally supersonic regions; naca-tn-2547; November 1951
- Adams, Mac C; Determination
of shapes of boattail bodies of revolution for minimum wave drag;
naca-tn-2550; November 1951
- Runyan, Harry, L; Effect of
various parameters including Mach number on the single-degree-of-freedom
flutter of a control surface in potential flow; naca-tn-2551; December
1951
- Henderson, Arthur, Jr;
Pitching-moment
derivatives Cmq and Cma at supersonic speeds for a slender-delta-wing and
slender-body combination and approximate solutions for broad-delta-wing and
slender-body combinations; naca-tn-2553; December 1951
- Lomax, Harvard Byrd,
Paul F; Theoretical
aerodynamic characteristics of a family of slender wing-tail-body
combinations; naca-tn-2554; November 1951
- Brewer, Jack D Fisher,
Lewis R; Effect of taper
ratio on the low-speed rolling stability derivatives of swept and unswept
wings of aspect ratio 2.61; naca-tn-2555; November 1951
- Serijan, K T Goodman, I
A Yankauskas, W J; Infrared
spectra of 59 dicyclic hydrocarbons; naca-tn-2557; November 1951
- Woolston, Donald S
Castile, George E; Some
effects of variations in several parameters including fluid density on the
flutter speed of light uniform cantilever wings; naca-tn-2558; December
1951
- Stever, Guyford H
(Massachusetts Institute of Technology) Rathbun, Kenneth C (Massachusetts
Institute of Technology); Theoretical
and experimental investigation of condensation of air in hypersonic wind
tunnels; naca-tn-2559; November 1951
- Mazelsky, Bernard; Numerical
determination of indicial lift of a two-dimensional sinking airfoil at
subsonic Mach numbers from oscillatory lift coefficients with calculations for
Mach number 0.7; naca-tn-2562; December 1951
- Cole, Henry A
(University of Washington) Ganzer, Victor M (University of Washington); Experimental
investigations of rolling performance of straight and sweptback flexible wings
with various ailerons; naca-tn-2563; December 1951
- Seidl, R J (Forest
Products Laboratory) Fahey, D J (Forest Products Laboratory); Properties
of honeycomb cores as affected by fiber type, fiber orientation, resin type,
and amount; naca-tn-2564; November 1951
- Gates, Ordway B , Jr;
A
theoretical analysis of the effects of several auxiliary damping devices on
the lateral stability and controllability of a high-speed aircraft;
naca-tn-2565; December 1951
- Lin, T C (University of
California) Schaaf, S A (University of California); Effect
of slip on flow near a stagnation point and in a boundary layer;
naca-tn-2568; December 1951
- Hacker, Paul T Dorsch,
Robert G; A
summary of meteorological conditions associated with aircraft icing and a
proposed method of selecting design criterions for ice-protection
equipment; naca-tn-2569; November 1951
- Bidwell, Jerold M; Application of
the Von Karman momentum theorem to turbulent boundary layers;
naca-tn-2571; December 1951
- Pitts, Joseph W
(National Bureau of Standards) MOORE DWIGHT G (National Bureau of Standards);
Ceramic
coatings for prevention of carbon absorption in four heat-resistant
alloys; naca-tn-2572; December 1951
- Kundu, D N (Ohio State
University) Boyle, F G (Ohio State University) Pool, M L (Ohio State
University); Development of
auxiliary cyclotron equipment for using tritium as bombarding particles in a
cyclotron; naca-tn-2573; December 1951
- Phillips, William H; Theoretical
analysis of some simple types of acceleration restrictors; naca-tn-2574;
December 1951
- Funk, Jack Binckley,
Earle T; A
flight investigation of the effect of center-of-gravity location on gust
loads; naca-tn-2575; December 1951
- Johnson, Aldie E , Jr
Batdorf, S B; A
study of slip formation in polycrystalline aluminum; naca-tn-2576;
December 1951
- Smaus, Louis, H Gore,
Marvin R Waugh, Merle G; A
comparison of predicted and experimentally determined longitudinal dynamic
responses of a stabilized airplane; naca-tn-2578; December 1951
- Eggers, A J , Jr Savin,
Raymond C; Approximate
methods for calculating the flow about nonlifting bodies of revolution at high
supersonic airspeeds; naca-tn-2579; December 1951
- Weltmann, Ruth N Kuhns,
Perry W; An
analysis of an x-ray absorption method for measurement of high gas
temperatures; naca-tn-2580; December 1951
- Yen, Kuo Tai
(Polytechnic Institute of Brooklyn) Gunturkun, Sadettin (Polytechnic Institute
of Brooklyn); Deflections
of a simply supported rectangular sandwich plate subjected to transverse
loads; naca-tn-2581; December 1951
- Smiley, Robert F; A semiempirical
procedure for computing the water-pressure distribution on flat and v-bottom
prismatic surfaces during impact or planing; naca-tn-2583; December
1951
- Prian, Vasily D Michel,
Donald J; An
analysis of flow in rotating passage of large radial-inlet centrifugal
compressor at tip speed of 700 feet per second; naca-tn-2584; December
1951
- Wolhart, Walter D; Influence of
wing and fuselage on the vertical-tail contribution to the low-speed rolling
derivatives of midwing airplane models with 45 degree sweptback surfaces;
naca-tn-2587; December 1951
- Voit, Charles H
Thomson, Arthur R; An
analytical investigation using aerodynamic limitations of several designs of
high stage pressure ratio multistage compressors; naca-tn-2589; December
1951
- Moskowitz, Barry
Maslen, Stephen H; Experimental
pressure distributions over two wing-body combinations at Mach number 1.9;
naca-rm-e50j09; February 05, 1951
- Farley, John M Prince,
William R; Turbine
performance characteristics of a python turbine-propeller engine investigated
in altitude wind tunnel; naca-rm-e50j12; May 1951
- Wu, Chung-Hua; Survey
of available information on internal flow losses through axial
turbomachines; naca-rm-e50j13; January 26, 1951
- Shillito, Thomas B
Younger, George G Henzel, James G , Jr; Altitude-test-chamber
investigation of performance of a 28-inch ram-jet engine III : combustion and
operational performance of three flame holders with a center pilot burner;
naca-rm-e50j20; February 06, 1951
- Esenwein, Fred T
Valerino, Alfred S; Force
and pressure characteristics for a series of nose inlets at Mach numbers from
1.59 to 1.99 I : conical spike all-external compression inlet with subsonic
cowl lip; naca-rm-e50j26; January 19, 1951
- Obery, L J Englert, G
W; Force and
pressure characteristics for a series of nose inlets at Mach numbers from 1.59
to 1.99 II : isentropic-spike all-external compression inlet;
naca-rm-e50j26a; February 09, 1951
- Weinstein, Maynard I
Davids, Joseph; Force
and pressure characteristics for a series of nose inlets at Mach numbers from
1.59 to 1.99 III : conical-spike all-external-compression inlet with
supersonic cowl lip; naca-rm-e50j30; February 14, 1951
- Fleming, W A Conrad, E
William Young, A W; Experimental
investigation of tail-pipe-burner design variables; naca-rm-e50k22; March
05, 1951
- Nussdorfer, T Wilcox, F
Perchonok, E; Investigation
at zero angle of attack of a 16-inch ram jet engine in 8- by 6-foot
supersonic; naca-rm-e50l04; March 02, 1951
- Jaffe, Leonard Coss,
Bert A Daykin, Donald R; An
electromagnetic flowmeter for rocket research; naca-rm-e50l12; March 06,
1951
- Rabb, Leonard North,
Warren J; Free-flight
performance of 16-inch diameter supersonic ram-jet units IV : performance of
ram-jet units designed for combustion chamber inlet Mach number of 0.21 at
free-stream Mach number of 1.6 over a range flight conditions;
naca-rm-e50l18; February 26, 1951
- Wilcox, Ward W Robbins,
William H; Design and
performance of an experimental axial-discharge mixed-flow compressor II :
over-all performance of impeller and supersonic-diffuser combination;
naca-rm-e51a02; April 30, 1951
- Gerstein, Melvin Wong,
Edgar L Levine, Oscar; Flame
velocities of four alkylsilanes; naca-rm-e51a08; March 09, 1951
- Foster, Hampton H; Ignition-energy
requirements in a single tubular combustor; naca-rm-e51a24; March 27,
1951
- Branstetter, J Robert
Lord, Albert M Gerstein, Melvin; Combustion
properties of aluminum as ram-jet fuel; naca-rm-e51b02; March 28,
1951
- Madden, Robert T
Kremzier, Emil; Force
and pressure characteristics for a series of nose inlets at Mach numbers from
1.59 to 1.99 IV : conical-spike external-internal compression inlet utilizing
perforated cowl; naca-rm-e51b05; March 28, 1951
- Sibulkin, Merwin; Theoretical and
experimental investigation of additive drag; naca-rm-e51b13; May 21,
1951
- Mccafferty, Richard J;
Liquid-fuel-distribution
and fuel-state effects on combustion performance of a single tubular
combustor; naca-rm-e51b21; May 1951
- Gordon, Sanford Huff,
Vearl N; Theoretical
performance of lithium and fluorine as a rocket propellant;
naca-rm-e51c01; May 10, 1951
- Fox, Jerome L; Preliminary
investigation of Helmholtz resonators for damping pressure fluctuations in
3.6-inch ram jet at Mach number 1.90; naca-rm-e51c05; May 22, 1951
- Eckert, E R G Kinsler,
Martin R Cochran, Reeves B; Wire
cloth as porous material for transpiration-cooled walls; naca-rm-e51h23;
November 13, 1951
- Ordin, Paul M Douglass,
Howard W Rowe, William H; Investigation
of the liquid fluorine-liquid diborane propellant combination in a
100-pound-thrust rocket engine; naca-rm-e51i04; November 30, 1951
- Cortright, Edgar M ,
Jr; Preliminary
investigation of a translating cowl technique for improving take-off
performance of a sharp-lip supersonic diffuser; naca-rm-e51i24; November
28, 1951
- Levine, Oscar Gerstein,
Melvin; Fundamental
flame velocities of pure hydrocarbons III : extension of tube method of high
flame velocities - acetylene-air mixtures; naca-rm-e51j05; December 03,
1951
- Moeckel, W E Evans, P J
, Jr; Preliminary
investigation of use of conical flow separation for efficient supersonic
diffusion; naca-rm-e51j08; December 17, 1951
- Belles, Frank E Simon,
Dorothy M; Variation of
the pressure limits of flame propagation with tube diameter for propane-air
mixtures; naca-rm-e51j09; December 05, 1951
- Swett, Clyde C , Jr; Spark ignition
of flowing gases II : effect of electrode parameters on energy required to
ignite a propane-air mixture; naca-rm-e51j12; December 18, 1951
- Foster, Hampton H; Effect of spark
repetition rate on the ignition limits of a single tubular combustor /Hampton
H. Foster; naca-rm-e51j18; December 06, 1951
- Callaghan, Edmund E
Coles, Willard D; Experimental
investigation of effect of jet exit configuration on thrust and drag;
naca-rm-e51j22; December 20, 1951
- Rainey, Robert W; Langley 9-inch
supersonic tunnel tests of several modifications of a supersonic missile
having tandem cruciform lifting surfaces : three-component data results of
models having ratios of wing span to tail span equal to and less than 1 and
some static; naca-rm-l50g07; March 07, 1951
- Wood, Raymond B
Fleming, Frank F; A
transonic-wing investigation in the Langley 8-foot high-speed tunnel at high
subsonic Mach numbers and at a Mach number of 1.2 : wing-fuselage
configuration having a wing of 60 degree sweepback, aspect-ratio 4, taper
ratio 0.6, and NACA 65A006 airf; naca-rm-l50j25; January 24, 1951
- Spearman, M Leroy
Webster, Robert A; An
investigation at Mach numbers of 1.40 and 1.59 of the effects of aileron
profile on the aerodynamic characteristics of a complete model of a supersonic
aircraft configuration; naca-rm-l50j31; January 15, 1951
- Smith, Norman F Marte,
Jack E; An
investigation of a supersonic aircraft configuration having a tapered wing
with circular-arc sections and 40 degree sweepback : force characteristics of
the complete configuration and its various components at Mach numbers of 1.40
and 1.59; naca-rm-l50k14; January 22, 1951
- Gillis, Clarence L
Vitale, A James; Wing-on
and wing-off longitudinal characteristics of an airplane configuration having
an thin unswept tapered wing of aspect ratio 3, as obtained from
rocket-propelled models at Mach numbers from 0.8 to 1.4; naca-rm-l50k16;
March 14, 1951
- Wineman, Andrew R; Preliminary
investigation of a fin-actuated jet-vane control system for stabilization of
rocket-powered models; naca-rm-l50k17; January 17, 1951
- Gillespie, Warren, Jr
Arbic, Richard G; Large-scale
flight measurements of zero-lift drag at Mach numbers from 0.90 to 1.95 of an
arrow wing in combination with a small body; naca-rm-l50k28a; January 12,
1951
- Ferri, Antonio Nucci,
Louis M; The
origin of aerodynamic instability of supersonic inlets at subcritical
conditions; naca-rm-l50k30; January 26, 1951
- Faget, Maxine A Watson,
Raymond S Bartlett, Walter A , Jr; Free-jet
tests of a 6.5-inch-diameter ram-jet engine at Mach numbers 1.81 and 2.00;
naca-rm-l50l06; March 07, 1951
- Kennedy, Robert M; Effects of a
fuselage flap dive brake on the aerodynamic characteristics of 1/30 scale
semispan model of the Bell X-5 variable-sweep airplane at a Mach number 1.24
as determined by the NACA wing flow method; naca-rm-l50l11a; February 08,
1951
- Spreemann, Kenneth P
Alford, William J , Jr; Investigation
of the effects of geometric changes in an underwing pylon suspended external
store installation on the aerodynamic characteristics of a 45 degree sweptback
wing at high subsonic speeds; naca-rm-l50l12; March 05, 1951
- Conner, D William
Mitchell, Meade H , Jr; Effects
of spoiler on airfoil pressure distribution and effects of size and location
of spoilers on the aerodynamic characteristics of a tapered unswept wing of
aspect ratio 2.5 at a Mach number of 1.90; naca-rm-l50l20; January 24,
1951
- Dettwyler, H Rudolph
Bond, Aleck C; Flight
performance of a twin-engine supersonic ram jet from 2,300 to 67,200 feet
altitude; naca-rm-l50l27; February 19, 1951
- Cahn, Maurice S Bryan,
Carroll R; A
transonic-wing investigation in the Langley 8-foot high-speed tunnel at high
subsonic Mach numbers and at a Mach number of 1.2. : wing-fuselage
configuration having a wing of 0 degrees sweepback, aspect ratio 4.0,taper
ratio 0.6, and NACA 65A006 ai; naca-rm-l51a02; March 06, 1951
- Tuovila, W J; Some
experiments on the flutter of sweptback cantilever wing models at Mach number
1.3; naca-rm-l51a11; March 15, 1951
- Spreemann, Kenneth P
Alford, William J , Jr; Small-scale
investigation at transonic speeds of the effects of thickening the inboard
section of a 45 degrees sweptback wing of aspect ratio 4, taper ratio 0.3, and
NACA 65A006 airfoil section; naca-rm-l51f08a; August 09, 1951
- Regier, Arthur A
Martin, Dennis J; Recent
experimental flutter studies; naca-rm-l51f11; June 12, 1951
- Pepper, William B , Jr
Hoffman, Sherwood; Comparison
of zero-lift drags determined by flight tests at transonic speeds of
symmetrically mounted nacelles in various chordwise positions at the wing tip
of a 45 degrees sweptback wing and body combination; naca-rm-l51f13;
September 17, 1951
- Sleeman, William C , Jr
Klevatt, Paul L Linsley, Edward L; Comparison
of transonic characteristics of lifting wings from experiments in a small
slotted tunnel and the Langley high-speed 7- by 10-foot tunnel;
naca-rm-l51f14; November 05, 1951
- Pepper, William B; The effect on
zero-lift drag of an indented fuselage or a thickened wing-root modification
to a 45 degrees sweptback wing-body configuration as determined by flight
tests at transonic speeds; naca-rm-l51f15; September 20, 1951
- Katz, Ellis Stoney,
William E , Jr; Base
pressures measured on several parabolic-arc bodies of revolution in free
flight at Mach numbers from 0.8 to 1.4 and at large Reynolds numbers;
naca-rm-l51f29; October 26, 1951
- Vogler, Raymond D
Turner, Thomas R Lockwood, Vernard, E; An
investigation at transonic speeds of the effects of control chord and span on
the control characteristics of a tapered wedge-type wing of aspect ratio 2.5 :
transonic-bump method; naca-rm-l51g03; September 20, 1951
- Sanders, E Claude
Edmondson, James L; Damping
in roll of rocket-powered test vehicles having swept, tapered wings of low
aspect ratio; naca-rm-l51g06; October 08, 1951
- Wittliff, Charles E
Byrne, Robert W; Preliminary
investigation of a supersonic scoop inlet derived from a conical-spike nose
inlet; naca-rm-l51g11; September 11, 1951
- Martz, C William
Church, James D; Flight
investigation at subsonic, transonic, and supersonic velocities of the
hinge-moment characteristics, lateral-control effectiveness, and wing damping
in roll of a 60 degrees sweptback delta wing with half-delta tip ailerons;
naca-rm-l51g18; September 21, 1951
- Danforth, Edward C B;
A
correlation of experimental zero-lift drag of rectangular wings with
symmetrical NACA 65-series airfoil sections by means of the transonic
similarity law for wings of finite aspect ratio; naca-rm-l51g20; September
17, 1951
- Passera, Anthony L; A theoretical
investigation of the influence of autopilot natural frequency upon the dynamic
performance characteristics of a supersonic canard missile configuration with
a pitch-attitude control system; naca-rm-l51h02; October 09, 1951
- Strass, H Kurt Marley,
Edward, T; Rolling
effectiveness of all-movable wings at small angles of incidence at Mach
numbers from 0.6 to 1.6; naca-rm-l51h03; October 09, 1951
- Hatch, John E , Jr
Hargrave, L Keith; Effects
of Reynolds number on the aerodynamic characteristics of a delta wing at Mach
number of 2.41; naca-rm-l51h06; October 22, 1951
- Gillespie, Warren, Jr;
Jet effects
on pressures and drags of bodies; naca-rm-l51j29; November 09, 1951
- Mathews, Charles W
Talmage, Donald B Whitten, James B; Effects
on longitudinal stability and control characteristics of a B-29 airplane of
variations in stick-force and control-rate characteristics obtained through
use of a booster in the elevator-control system; naca-tn-2238; February
1951
- Gossard, Myron L; An iterative
transformation procedure for numerical solution of flutter and similar
characteristic-value problems; naca-tn-2346; May 1951
- Heidmann, Marcus F
Humphrey, Jack C; Fluctuations
in a spray formed by two impinging jets; naca-tn-2349; April 1951
- Campbell, John P
Mckinney, Marion O; Summary
of methods for calculating dynamic lateral stability and response and for
estimating lateral stability derivatives; naca-tn-2409; July 1951
- Moeckel, Wolfgang E; Flow separation
ahead of blunt bodies at supersonic speeds; naca-tn-2418; July 1951
- Stalder, Jackson R
Zurick, Vernon J; Theoretical
aerodynamic characteristics of bodies in a free-molecule-flow field;
naca-tn-2423; July 1951
- Holms, Arthur G; A biharmonic
relaxation method for calculating thermal stress in cooled irregular
cylinders; naca-tn-2434; August 1951
- Furlong, G Chester
Bollech, Thomas V; Effect
of ground interference on the aerodynamic characteristics of a 42 degrees
sweptback wing; naca-tn-2487; October 1951
- Griffith, George E; Stresses in a
two-bay noncircular cylinder under traverse loads; naca-tn-2512; October
1951
- Runyan, Harry L
Watkins, Charles E; Considerations
on the effect of wind-tunnel walls on oscillating air forces for
two-dimensional subsonic compressible flow; naca-tn-2552; December
1951
- (Author(s) Not
Available); Cooperative
investigation of relationship between static and fatigue properties of
heat-resistant alloys at elevated temperatures; naca-rm-51a04; March 07,
1951
- Freeman, J W
(University of Michigan) White, A E (University of Michigan.); Properties
of low-carbon N-155 alloy bar stock from 1200 to 1800 F; naca-rm-51b05;
May 03, 1951
- Kline, G M (National
Bureau of Standards); The
properties of three cast polyester resins of Sierracin 212, 212A, and
250A; naca-rm-51b23; April 23, 1951
- Wier, John E (National
Bureau of Standards) Pons, Dorothy C (National Bureau of Standards) Axilrod,
Benjamin M (National Bureau of Standards); Effects
of humidity during fabrication on some physical properties of glass-fabric
unsaturated-polyester laminates; naca-rm-51c21; July 18, 1951
- (Author(s) Not
Available); Review of
current and anticipated lubricant problems in turbojet engines;
naca-rm-51d20; April 20, 1951
- Freeman, J W
(University of Michigan and Battelle Memorial Institute) Cross, Howard C
(University of Michigan and Battelle Memorial Institute); Notes
on heat-resistant materials in Britain from technical mission October 13 to
November 30, 1950; naca-rm-51d23; May 14, 1951
- Macgregor, C W
(Massachusetts Institute of Technology) Walcott, F J , Jr (Massachusetts
Institute of Technology); Investigation
of torsion creep-to-rupture properties of N-155 alloy; naca-rm-51e04;
August 21, 1951
- Miller, James A
(National Bureau of Standards) Jacobs, Pearl V (National Bureau of Standards);
Effective
modulus in plastic buckling of high-strength aluminum-alloy sheet;
naca-rm-51g11; September 20, 1951
- Gadeberg, Burnett L
Ziff, Howard L; Flight
determined buffet boundaries of ten airplanes and comparisons with five
buffeting criteria; naca-rm-a50i27; January 05, 1951
- Hunton, Lynn W Dew,
Joseph K; The effects of
camber and twist on the aerodynamic loading and stalling characteristics of a
large-scale 45 degree swept-back wing; naca-rm-a50j24; January 24,
1951
- Mccormack, Gerald M
Tolhurst, William H , Jr; The
effects of boundary-layer control on the longitudinal characteristics of a
swept-back wing using suction through streamwise slots in the outboard portion
of the wing; naca-rm-a50k06; January 05, 1951
- Stivers, Louis S , Jr
Malick, Alexander W; Wind-tunnel
investigation at Mach numbers from 0.50 to 1.29 of an unswept, tapered wing of
aspect ratio 2.67 with leading- and trailing-edge flaps - leading-edge flaps
deflected; naca-rm-a50k10; February 26, 1951
- Tinling, Bruce E Kolk,
W Richard; The effects of
centrally mounted wing-tip tanks on the subsonic aerodynamic characteristics
of a wing of aspect ratio 10 with 35 degrees of sweepback; naca-rm-a50k15;
February 21, 1951
- Smith, Donald W
Heitmeyer, John C; Lift,
drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic
speeds : plane triangular wing of aspect ratio 2 with NACA 0008-63
section; naca-rm-a50k20; February 1951
- Tinling, Bruce E Kolk,
W Richard; The effects of
Mach number and Reynolds number on the aerodynamic characteristics of several
12-percent-thick wings having 35 degrees of sweepback and various amounts of
camber; naca-rm-a50k27; February 23, 1951
- Stivers, Louis S , Jr
Malick, Alexander W; Wind-tunnel
investigation at Mach numbers from 0.50 to 1.29 of an unswept, tapered wing of
aspect ratio 2.67 with leading- and trailing-edge flaps : flaps deflected in
combination; naca-rm-a50k27b; February 26, 1951
- Demele, Fred A Sutton,
Fred B; The
effects of increasing the leading-edge radius and adding forward camber on the
aerodynamic characteristics of a wing with 35 degrees of sweepback;
naca-rm-a50k28a; February 09, 1951
- Rathert, George A , Jr
Ziff, Howard L Cooper, George E; Preliminary
flight investigation of the maneuvering accelerations and buffet boundary of a
35 degree swept-wing airplane at high altitude and transonic speeds;
naca-rm-a50l04; February 21, 1951
- Mccullough, George B
Nitzberg, Gerald E Kelly, John A; Preliminary
investigation of the delay of turbulent flow separation by means of
wedge-shaped bodies; naca-rm-a50l12; March 1951
- Delaney, Noel K Hayter,
Nora-Lee F; Low-speed
investigation of a 0.16 scale model of the X-3 airplane : lateral and
directional characteristics; naca-rm-a51a16; March 16, 1951
- Selna, James; Preliminary
investigation of a submerged inlet and a nose inlet in the transonic flight
range with free-fall models; naca-rm-a51b14; June 18, 1951
- Stivers, Louis S , Jr
Walker, Harold J Beard, Luther, Jr; Experimental
downwash and wake characteristics at subsonic and supersonic Mach numbers
behind an unswept, tapered wing, of aspect ratio 2.67 with leading-and
trailing-edge flaps; naca-rm-a51b16; April 21, 1951
- Wetzel, Benton E Pfyl,
Frank A; Measurements of
downwash and sidewash behind cruciform triangular wings at Mach number
1.4; naca-rm-a51b20; April 04, 1951
- Graham, David Koenig,
David G; Tests in the
Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect
ratio 2 triangular wing and an all-movable horizontal tail : longitudinal
characteristics; naca-rm-a51b21; April 23, 1951
- Ernst, Edward A
Anderson, Seth B Van Dyke, Rudolph D , Jr; Flight
measurements of the wing-dropping tendency of a straight-wing jet airplane at
high subsonic Mach numbers; naca-rm-a51b28; April 24, 1951
- Hemenover, Albert D
Graham, Donald J; Influence
of airfoil trailing-edge angle and trailing-edge-thickness variation on the
effectiveness of a plain flap at high subsonic Mach numbers;
naca-rm-a51c12a; May 22, 1951
- Hopkins, Edward J; A
semi-empirical method for calculating the pitching moment of bodies of
revolution at low Mach numbers; naca-rm-a51c14; May 17, 1951
- Kolbe, Carl D
Bandettini, Angelo; Investigation
in the Ames 12-foot pressure wind tunnel of a model horizontal tail of aspect
ratio 3 and taper ratio 0.5 having the quarter-chord line swept back 45
degrees; naca-rm-a51d02; June 25, 1951
- James, Harry A Dew,
Joseph K; Effects of
double-slotted flaps and leading-edge modifications on the low-speed
characteristics of a large-scale 45 degrees swept-back wing with and without
camber and twist; naca-rm-a51d18; July 23, 1951
- Rose, Leonard M; Low-speed
characteristics of a wing having 63 degrees sweepback and uniform camber;
naca-rm-a51d25; June 26, 1951
- Johnson, Ben H , Jr
Shibata, Harry H; Characteristics
throughout the subsonic speed range of a plane wing and of a cambered and
twisted wing, both having 45 degrees of sweepback; naca-rm-a51d27; July
12, 1951
- Reynolds, Robert M
Sammonds, Robert I; Subsonic
Mach and Reynolds number effects on the surface pressures, gap flow, pressure
recovery, and drag of a nonrotating NACA 1-series E-type cowling at an angle
of attack of 0 degrees; naca-rm-a51e03; July 17, 1951
- Anderson, Seth B; Measurements in
flight of the longitudinal characteristics of two jet aircraft, one with a
diving tendency and the other with a climbing tendency at high Mach
numbers; naca-rm-a51e14; October 05, 1951
- Maki, Ralph L; The
use of two-dimensional section data to estimate the low-speed wing lift
coefficient at which section stall first appears on a swept wing;
naca-rm-a51e15; July 27, 1951
- Liddell, Charles J , Jr
Creer, Brent Y Van Dyke, Rudolph D , Jr; A
flight study of requirements for satisfactory lateral oscillatory
characteristics of fighter aircraft; naca-rm-a51e16; July 25, 1951
- Holzhauser, Curt A; An experimental
investigation at subsonic speeds of a scoop-type air-induction system for a
supersonic airplane; naca-rm-a51e24; July 19, 1951
- Dannenberg, Robert E;
Low-speed
characteristics of a 45 degree swept wing with leading-edge inlets;
naca-rm-a51e29; August 13, 1951
- Olson, Robert N Chubb,
Robert S; Wind-tunnel
tests of a 1/12-scale model of the X-3 airplane at subsonic and supersonic
speeds.; naca-rm-a51f12; September 14, 1951
- Allen, Edwin C; Investigation
of a triangular wing in conjunction with a fuselage and horizontal tail to
determine downwash and longitudinal-stability characteristics : transonic bump
method; naca-rm-a51f12a; August 17, 1951
- Heitmeyer, John C
Hightower, Ronald C; Lift,
drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic
speeds : plane triangular wing of aspect ratio 4 with 3-percent-thick rounded
nose section; naca-rm-a51f21; August 29, 1951
- Cooper, George E Bray,
Richard S; Schlieren
investigation of the wing shock-wave boundary-layer interaction in flight;
naca-rm-a51g09; September 19, 1951
- Sorenson, Robert M
Wyss, John A Kyle, James C; Preliminary
investigation of the pressure fluctuations in the wakes of two-dimensional
wings at low angles of attack; naca-rm-a51g10; October 30, 1951
- Kolbe, Carl D Boltz,
Frederick W; The forces and
pressure distribution at subsonic speeds on a plane wing having 45 degrees of
sweepback, an aspect ratio of 3, and a taper ratio of 0.5; naca-rm-a51g31;
October 16, 1951
- Ankenbruck, Herman O
Sadoff, Melvin O'Hare, William; Stability
and control measurements obtained during USAF-NACA cooperative flight-test
program on the X-4 airplane (USAF No. 46-677); naca-rm-a51h09; October 26,
1951
- Graham, David Koenig,
David G; Tests in the
Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect
ratio 4 triangular wing and an all-movable horizontal tail - longitudinal
characteristics; naca-rm-a51h10a; October 16, 1951
- Frank, Joseph L Taylor,
Robert A; Comparison of
drag, pressure recovery, and surface pressure of a scoop-type inlet and an
NACA submerged inlet at transonic speeds; naca-rm-a51h20a; December 17,
1951
- Friedman, Morris D; Arrangement of
bodies of revolution in supersonic flow to reduce wave drag;
naca-rm-a51i20; December 17, 1951
- Wyss, John A Sorenson,
Robert M; An
investigation of the control-surface flutter derivatives of an NACA 65(sub
1)-213 airfoil in the Ames 16-foot high-speed wind tunnel; naca-rm-a51j10;
December 21, 1951
- Golladay, Richard L
Bloomer, Harry E; Investigation
of altitude starting and acceleration characteristics of J47 turbojet
engine; naca-rm-e50g07; January 10, 1951
- Robards, C F Gangler, J
J; Some
properties of beryllium oxide and beryllium oxide - columbium ceramals;
naca-rm-e50g21; March 02, 1951
- Perkins, Porter J; Flight
instrument for measurement of liquid-water content in clouds at temperatures
above and below freezing; naca-rm-e50j12a; March 05, 1951
- Cicala, Placido.; Present state
of development in nonsteady motion of a lifting surface; naca-tm-1277;
1951
- Loitsianskii, L. G.; Approximate
method of integration of laminar boundary layer in incompressible fluid;
naca-tm-1293; 1951
- Ovsiannikov, L. V.; Gas flow with
straight transition line; naca-tm-1295; 1951
- Teichmann, Alfred.; State and
development of flutter calculation; naca-tm-1297; 1951
- Tillmann, W.; Additional
measurements of the drag of surface irregularities in turbulent boundary
layers; naca-tm-1299; 1951
- Sohngen, Heinz.,
Schwarz, L., Dietze, F.; Three
papers from conference on "Wing and tail-surface oscillations :March 6-8,
1941, Munich; naca-tm-1306; 1951
- Szablewski, W.; Contributions
to the theory of the spreading of a free jet issuing from a nozzle;
naca-tm-1311; 1951
- de Guillenchmidt, P.;
Calculation
of the bending stresses in helicopter rotor blades; naca-tm-1312;
1951
- Abramyan, B. L.; Torsion and
bending of prismatic rods of hollow rectangular section; naca-tm-1319;
1951
- Cortright, Edgar M.,
Jr., Schroeder, Albert H.; Preliminary
investigation of effectiveness of base bleed in reducing drag of blunt-base
bodies in supersonic stream; naca-rm-e51a26; 1951
- Fields, E. M., Strass,
H. Kurt.; Free-flight
measurements at Mach numbers from 0.7 to 1.6 of some effects of
airfoil-thickness distribution and trailing-edge angle on aileron rolling
effectiveness and drag for wings with 0 and 45 degrees sweepback;
naca-rm-l51g27; 1951
- Vlasov, V. S.; Basic
differential equations in general theory of elastic shells; naca-tm-1241;
1951
- Weinig, F.; Flight
performance of a jet power plant III - operating characteristics of a jet
power plant as a function of altitude; naca-tm-1258; 1951
- Greenberg, Harry; A survey of
methods for determining stability parameters of an airplane from dynamic
flight measurements; naca-tn-2340; 1951
- Phillips, William H.,
Kraft, Christopher C., Jr.; Theoretical
study of some methods for increasing the smoothness of flight through rough
air; naca-tn-2416; 1951
- Wise, P. H., Serijan,
K. T., Goodman, I. A.; Correlation
of physical properties with molecular structure for some dicyclic hydrocarbons
having high thermal-energy release per unit volume; naca-report-1003;
1951
- Mirels, Harold.; A
lift-cancellation technique in linearized supersonic-wing theory;
naca-report-1004; 1951
- Mendelson, Alexander.,
Gendler, Selwyn.; Analytical
determination of coupled bending-torsion vibrations of cantilever beams by
means of station functions; naca-report-1005; 1951
- Wilcox, E. Clinton.,
Trout, Arthur M.; Analysis
of thrust augmentation of turbojet engines by water injection at compressor
inlet including charts for calculating compression processes with water
injection; naca-report-1006; 1951
- Pearson, Henry A.,
Mcgowan, William A., Donegan, James J.; Horizontal
tail loads in maneuvering flight; naca-report-1007; 1951
- Godfrey, Douglas.; Investigation
of fretting by microscopic observation; naca-report-1009; 1951
- Houbolt, John C.; A recurrence
matrix solution for the dynamic response of aircraft in gusts;
naca-report-1010; 1951
- Otto, Edward W.,
Taylor, Burt L, III.; Dynamics
of a turbojet engine considered as a quasi-static system;
naca-report-1011; 1951
- Delano, James B.; Investigation
of the NACA 4-(5)(08)-03 and NACA 4-(10)(08)-03 two-blade propellers at
forward Mach numbers to 0.725 to determine the effects of camber and
compressibility on performance; naca-report-1012; 1951
- Merten, Kenneth F.,
Beck, Edgar B.; Effects
of wing flexibility and variable air lift upon wing bending moment during
landing impacts of a small seaplane; naca-report-1013; 1951
- Barmby, J. G.,
Cunningham, H. J., Garrick, I. E.; Study
of effects of sweep on the flutter of cantilever wings; naca-report-1014;
1951
- Eckert, E. R. G.,
Jackson, Thomas W.; Analysis
of turbulent free-convection boundary layer on flat plate;
naca-report-1015; 1951
- Erwin, John R., Emery,
James C.; Effect of
tunnel configuration and testing technique on cascade performance;
naca-report-1016; 1951
- Taylor, Burt L., III.,
Oppenheimer, Frank L.; Investigation
of frequency-response characteristics of engine speed for a typical
turbine-propeller engine; naca-report-1017; 1951
- Sternfield, Leonard.,
Gates, Ordway B., Jr.; A
theoretical analysis of the effect of time lag in an automatic stabilization
system on the lateral oscillatory stability of an airplane;
naca-report-1018; 1951
- Scull, Wilfred E.; Relation
between inflammables and ignition sources in aircraft environments;
naca-report-1019; 1951
- Humble, Leroy V.,
Lowdermilk, Warren H., Desmon, Leland G.; Measurements
of average heat-transfer and friction coefficients for subsonic flow of air in
smooth tubes at high surface and fluid temperatures; naca-report-1020;
1951
- Wu, M. H. Lee.; Analysis of
plane-plastic stress problems with axial symmetry in strain-hardening
range; naca-report-1021; 1951
- Eckert, E. R. G., Low,
George M.; Temperature
distribution in internally heated walls of heat exchangers composed of
nonnuclear flow passages; naca-report-1022; 1951
- Weeton, John W.; Diffusion of
chromium in alpha cobalt-chromium solid solutions; naca-report-1023;
1951
- Diederich, Franklin W.;
Calculation
of the Lateral Control of Swept and Unswept Flexible Wings of Arbitrary
Stiffness; naca-report-1024; 1951
- Braslow, Albert L.,
Burrows, Dale L., Tetervin, Neal., Visconti, Fioravante.; Experimental
and theoretical studies of area suction for the control of the laminar
boundary layer on an NACA 64a010 airfoil; naca-report-1025; 1951
- Barnett, Henry C.; NACA
investigation of fuel performance in piston-type engines;
naca-report-1026; 1951
- Lo, Hsu., Crate,
Harold., Schwartz, Edward B.; Buckling
of thin-walled cylinder under axial compression and internal pressure;
naca-report-1027; 1951
- Watkins, Charles E.; Effect of
aspect ratio on the air forces and moments of harmonically oscillating thin
rectangular wings in supersonic potential flow; naca-report-1028;
1951
- Stowell, Elbridge Z.;
Compressive
strength of flanges; naca-report-1029; 1951
- Schubauer, G. B.,
Klebanoff, P. S.; Investigation
of separation of the turbulent boundary layer; naca-report-1030;
1951
- Bird, John D., Jaquet,
Byron M.; A
study of the use of experimental stability derivatives in the calculation of
the lateral disturbed motions of a swept-wing airplane and comparison with
flight results; naca-report-1031; 1951
- Stalder, Jackson R.,
Goodwin, Glen., Creager, Marcus O.; A
comparison of theory and experiment for high-speed free-molecule flow;
naca-report-1032; 1951
- Vincenti, Walter G.; Comparison
between theory and experiment for wings at supersonic speeds;
naca-report-1033; 1951
- Fischel, Jack., Watson,
James M.; Investigation
of spoiler ailerons for use as speed brakes or glide-path controls on two NACA
65-series wings equipped with full-span slotted flaps; naca-report-1034;
1951
- Mckinney, Marion O.,
Jr.; Analysis of
means of improving the uncontrolled lateral motions of personal airplanes;
naca-report-1035; 1951
- Chapman, Dean R.,
Perkins, Edward W.; Experimental
investigation of the effects of viscosity on the drag and base pressure of
bodies of revolution at a Mach number 1.5; naca-report-1036; 1951
- Huff, Vearl N., Gordon,
Sanford., Morrell, Virginia E.; General
method and thermodynamic tables for computation of equilibrium composition and
temperature of chemical reactions; naca-report-1037; 1951
- Becker, John V.; Wind-tunnel
investigation of air inlet and outlet openings on a streamline body;
naca-report-1038; 1951
- Kaplan, Carl.; On
the particular integrals of the Prandtl-Busemann iteration equations for the
flow of a compressible fluid; naca-report-1039; 1951
- Corrsin, Stanley.,
Uberoi, Mahinder S.; Spectra
and diffusion in a round turbulent jet; naca-report-1040; 1951
- Goin, Kennith L.; Equations and
charts for the rapid estimation of hinge-moment and effectiveness parameters
for trailing-edge controls having leading and trailing edges swept ahead of
the Mach lines; naca-report-1041; 1951
- Sternfield, Leonard; Some effects of
nonlinear variation in the directional-stability and damping-in-yawing
derivatives on the lateral stability of an airplane; naca-report-1042;
1951
- Heldenfels, Richard R.;
A numerical
method for the stress analysis of stiffened-shell structures under nonuniform
temperature distributions; naca-report-1043; 1951
- Ferri, Antonio.; The method of
characteristics for the determination of supersonic flow over bodies of
revolution at small angles of attack; naca-report-1044; 1951
- Ferri, Antonio.; Supersonic flow
around circular cones at angles of attack; naca-report-1045; 1951
- Tetervin, Neal., Lin,
Chia Chiao.; A general
integral form of the boundary-layer equation for incompressible flow with an
application to the calculation of the separation point of turbulent boundary
layers; naca-report-1046; 1951
- Seide, Paul., Barrett,
Paul F.; The
stability of the compression cover of box beams stiffened by posts;
naca-report-1047; 1951
- Allen, H. Julian.,
Perkins, Edward W.; A
study of effects of viscosity on flow over slender inclined bodies of
revolution; naca-report-1048; 1951
- Queijo, M. J., Wolhart,
Walter D.; Experimental
investigation of the effect of vertical-tail size and length and of fuselage
shape and length on the static lateral stability characteristics of a model
with 45 degree sweptback wing and tail surfaces; naca-report-1049;
1951
- Cohen, Doris.; Formulas
for the supersonic loading, lift, and drag of flat swept-back wings with
leading edges behind the Mach line; naca-report-1050; 1951
- Chapman, Dean R.; An analysis of
base pressure at supersonic velocities and comparison with experiment;
naca-report-1051; 1951
- Jones, Arthur L.,
Alksne, Alberta.; A
summary of lateral-stability derivatives calculated for wing plan forms in
supersonic flow; naca-report-1052; 1951
- Laufer, John.; Investigation
of turbulent flow in a two-dimensional channel; naca-report-1053;
1951
- Lomax, Harvard.,
Heaslet, Max A., Fuller, Franklyn B.; Integrals
and integral equations in linearized wing theory; naca-report-1054;
1951
- Scherrer, Richard.; Comparison of
theoretical and experimental heat-transfer characteristics of bodies of
revolution at supersonic speeds; naca-report-1055; 1951
- Deyoung, John.; Theoretical
antisymmetric span loading for wings of arbitrary plan form at subsonic
speeds; naca-report-1056; 1951
- Horton, Elmer A.,
Loftin, Laurence K., Racisz, Stanley F., Quinn, John.; Analysis
of the effects of boundary-layer control in the take-off and power-off landing
performance characteristics of a liaison type of airplane;
naca-report-1057; 1951
- Reynolds, E. E.,
Freeman, J. W., White, A. E.; Influence
of chemical composition on rupture properties at 1200 degrees F. of forged
chromium-cobalt-nickel-iron base alloys in solution-treated and aged
condition; naca-report-1058; 1951
- Stone, Ralph W , Jr
Hultz, Burton E; Summary
of spin and recovery characteristics of 12 models of flying wing and
unconventional type airplanes; naca-rm-l50l29; March 1951
- Gold, H., Rosenzweig,
S.; Altitude
operation of gas-turbine engine with variable-area fuel-nozzle system;
naca-rm-e51a04; 1951
- Tannenbaum, Stanley.,
Murphy, Maurice F.; The
preparation, physical properties, and heats of combustion of four
alkylsilanes; naca-rm-e51a05; 1951
- Cook, William P.,
Butze, Helmut F.; Investigation
of altitude ignition, acceleration and steady-state operation with single
combustor of J47 turbojet engine; naca-rm-e51a25; 1951
- Saari, M. J., Wintler,
J. T.; Altitude-wind-tunnel
investigation of performance characteristics of a J47d prototype (RX1-1)
turbojet engine with fixed-area exhaust nozzle; naca-rm-e51b06;
1951
- Wilsted, H. D., Grey,
R. E.; Altitude-performance
and Reynolds number investigation of centrifugal-flow-compressor turbojet
engine; naca-rm-e51b07; 1951
- Lazar, James.,
DeRocher, Wilfred L., Jr.; Correlation
of analog solutions with experimental sea-level transient data for controlled
turbine-propeller engine, including analog results at altitudes;
naca-rm-e51b08; 1951
- Callaghan, Edmund E.,
von Glahn, Uwe., Gray, Vernon H.; NACA
investigation of icing-protection systems for turbojet-engine
installations; naca-rm-e51b12; 1951
- Conrad, E. William.,
McAulay, John E.; Altitude-wind-tunnel
investigation of performance characteristics of a J47D prototype (RX1-1)
turbojet engine with variable-area exhaust nozzle; naca-rm-e51c15;
1951
- ; Review
of problems of conservation of strategic materials for turbine engines;
naca-rm-e51c21; 1951
- Graham, Robert C.,
Klapproth, John F., Barina, Frank J.; Investigation
of off-design performance of shock-in-rotor type supersonic blading;
naca-rm-e51c22; 1951
- Desmon, Leland G.,
Mosher, Don R.; Preliminary
study of circulation in an apparatus suitable for determining corrosive
effects of hot flowing liquids; naca-rm-e51d12; 1951
- Schwartzbart, H.,
Jones, M. H., Brown, W. F., Jr.; Observations
on Bauschinger effect in copper and brass; naca-rm-e51d13; 1951
- Yaker, C., Robards, C.
F., Garrett, F. B.; Investigation
of mechanisms of blade failure of forged hastalloy B and cast Stellite 21
turbine blades in turbojet engine; naca-rm-e51d16; 1951
- Ferguson, Robert R.; Effect of
surface finish on fatigue properties at elevated temperatures I :low-carbon
N-155 with grain size of A.S.T.M. 1; naca-rm-e51d17; 1951
- Perkins, Porter J.,
Kline, Dwight B.; Analysis
of meteorological data obtained during flight in a supercooled stratiform
cloud of high liquid-water content; naca-rm-e51d18; 1951
- Wallner, Lewis E.,
Wintler, John T.; Experimental
investigation of typical constant- and variable-area exhaust nozzles and
effects on axial-flow turbojet-engine performance; naca-rm-e51d19;
1951
- Vasu, George., Pack,
George J.; Analysis of
experimental sea-level transient data and analog method of obtaining altitude
response for turbine-propeller engine with relay-type speed control;
naca-rm-e51d26; 1951
- Delio, Gene J.,
Schwent, Glennon V.; Instrumentation
for recording transient performance of gas-turbine engines and control
systems; naca-rm-e51d27; 1951
- Wachtl, William. W.,
Rom, Frank E.; Analysis
of the liquid-metal turbojet cycle for propulsion of nuclear powered
aircraft; naca-rm-e51d30; 1951
- Mankuta, Harry.,
Guentert, Donald C.; Some
effects of solidity on turning through constant-thickness circular-arc guide
vanes in axial annular flow; naca-rm-e51e07; 1951
- Perkins, Porter J.,
McCullough, Stuart., Lewis, Ralph D.; A
simplified instrument for recording and indicating frequency and intensity of
icing conditions encountered in flight; naca-rm-e51e16; 1951
- Rebeske, John J., Jr.,
Berkey, William E., Forrette, Robert E.; Over-all
performance of J35-A-23 two-stage turbine; naca-rm-e51e22; 1951
- Long, Roger A., Esgar,
Jack B.; Experimental
investigation of air-cooled turbine blades in turbojet engine VII :rotor-blade
fabrication procedures; naca-rm-e51e23; 1951
- Arne, Vernon L.,
Nachtigall, Alfred J.; Calculated
effects of turbine rotor-blade cooling-air flow, altitude, and compressor
bleed point on performance of a turbojet engine; naca-rm-e51e24;
1951
- Lietzke, A. F., Nagey,
T. F.; Measurement of
distortion in second experimental control rod with temperature patterns
simulating shim rod out and shim rod 50 percent inserted for Argonne Naval
Reactor / A. F. Lietzke and T. F. Nagey; naca-rm-e51e25; 1951
- Armstrong, John C.; Altitude-ignition
limit of a turbojet engine using a condenser-discharge ignition system / John
C. Armstrong; naca-rm-e51f11; 1951
- Hauser, Cavour H.,
Plohr, Henry W.; Two-dimensional
cascade investigation of the maximum exit tangential velocity component and
other flow conditions at the exit of several turbine blade designs at
supercritical pressure ratios; naca-rm-e51f12; 1951
- English, Robert E.,
Cavicchi, Richard H.; Comparison
of measured efficiencies of nine turbine designs with efficiencies predicted
by two empirical methods; naca-rm-e51f13; 1951
- Oppenheimer, Frank L.,
Jacques, James R.; Investigation
of dynamic characteristics of a turbine-propeller engine; naca-rm-e51f15;
1951
- Krebs, Richard P.; Preliminary
investigation of the control of a gas-turbine engine for a helicopter /
Richard P. Krebs; naca-rm-e51f19; 1951
- Gangler, James J.,
Engel, Walter J.; Resistance
of various materials to attack by molten bismuth-lead eutectic at elevated
temperatures; naca-rm-e51f21; 1951
- Gould, Lawrence I.; Preliminary
investigation of the supersonic flow field downstream of wire-mesh nozzles in
a constant-area duct / Lawrence I. Gould; naca-rm-e51f25; 1951
- Moses, J. J., Serovy,
G. K.; Some
effects of blade trailing-edge thickness on performance of a single-stage
axial-flow compressor; naca-rm-e51f28; 1951
- Lubarsky, Bernard.; Experimental
investigation of forced-convection heat-transfer characteristics of
lead-bismuth eutectic; naca-rm-e51g02; 1951
- Bogart, Donald.; Estimation of
neutron energy for first resonance from absorption cross section for thermal
neutrons; naca-rm-e51g03; 1951
- Levine, Joseph.,
Kleinknecht, Kenneth S.; Adaptation
of a cascade impactor to flight measurement of droplet size in clouds;
naca-rm-e51g05; 1951
- Esgar, Jack B., Lea,
Alfred L.; Determination
and use of the local recovery factor for calculating the effectiveness gas
temperature for turbine blades / Jack B. Esgar and Alfred L. Lea;
naca-rm-e51g10; 1951
- Jenkins, Joe E.,
Buchele, Donald R., Long, Roger A.; A
specially constructed metallograph for use at elevated temperatures;
naca-rm-e51g12; 1951
- Garrett, F. B., Yaker,
C.; Relation
of engine turbine-blade life to stress-rupture properties of the alloys,
Stellite 21, Hastelloy B, Cast S-816, Forged S-816, X-40, Nimonic 80,
Refractory 26, N-155, and Iconel X; naca-rm-e51g13; 1951
- Silvern, David H.,
Slivka, William R.; Experimental
investigation of an 0.8 hub-tip radius-ratio,nontwisted-rotor-blade
turbine; naca-rm-e51g14; 1951
- Schwed, Philip.; Resolution of
annealing experiments for the study of nonequilibrium states;
naca-rm-e51g24; 1951
- Lieblein, Seymour.,
Ackley, Richard H.; Secondary
flows in annular cascades and effects on flow in inlet guide vanes;
naca-rm-e51g27; 1951
- Thurston, Sidney.,
Brunk, Ralph E.; Performance
of a cascade in an annular vortex-generating tunnel over range of Reynolds
numbers; naca-rm-e51g30; 1951
- Macks, E. F., Nemeth,
Z. N., Anderson, W. J.; Preliminary
investigation of molybdenum disulfide-air-mist lubrication for roller bearings
operating to DN values of 1 x 10(exp 6) and ball bearings operating to
temperatures of 1000 F; naca-rm-e51g31; 1951
- Stewart, Warner L.; Analytical
investigation of flow through high-speed mixed-flow turbine;
naca-rm-e51h06; 1951
- Lown, Harold.,
Hartmann, Melvin J.; :Investigation
of a 24-inch shock-in-rotor type supersonic compressor designed for simple
radial equilibrium behind normal shock; naca-rm-e51h08; 1951
- Simon, Dorothy M.,
Wong, Edgar, L.; Flame
velocities over a wide composition range for pentane-air, ethylene-air, and
propyne-air flames; naca-rm-e51h09; 1951
- Smith, Gordon T.,
Hickel, Robert O.; Experimental
investigation of air-cooled turbine blade in turbojet engine VIII :rotor
blades with capped leading edges; naca-rm-e51h14; 1951
- Ellis, C. W.,
Hollister, D. P., Sargent, A. F., Jr.; Preliminary
investigation of cooling-air ejector performance at pressure ratios from 1 to
10; naca-rm-e51h21; 1951
- Wilsted, H. D.,
Armstrong, J. C.; Preliminary
results of turbojet-engine altitude-starting investigation;
naca-rm-e51h30; 1951
- Warshawsky, I., Estrin,
M.; A
multiple-range self-balancing thermocouple potentiometer; naca-rm-e51h31;
1951
- Sobolewski, A. E.,
Farley, J. M.; Steady-state
engine windmilling and engine speed decay characteristics of an axial-flow
turbojet engine; naca-rm-e51i06; 1951
- Farley, John M.; Altitude wind
tunnel investigation of the performance of compressor, combustor, and turbine
components of prototype J47D (RX1-1) turbojet engine; naca-rm-e51i13;
1951
- Kaufman, S. J.,
Henderson, R. W.; Forced-convection
heat transfer to water at high pressures and temperatures in the nonboiling
region; naca-rm-e51i18; 1951
- Wallner, Lewis E.,
Jansen, Emmert T.; Full-scale
investigation of cooling shroud and ejector nozzle for a turbojet engine
:afterburner installation; naca-rm-e51j04; 1951
- Stepka, Francis S.,
Hickel, Robert O.; Experimental
investigation of air-cooled turbine blades in turbojet engine IX :evaluation
of the durability of noncritical rotor blades in engine operation;
naca-rm-e51j10; 1951
- Fleming, William A.; Effects of
altitude on turbojet engine performance; naca-rm-e51j15; 1951
- Nielsen, Jack N.,
Kaattari, George E.; Method
for estimating lift interference of wing-body combinations at supersonic
speeds; naca-rm-a51j04; 1951
- Tarr, Philip R.; Methods for
connection to revolving thermocouples; naca-rm-e50j23a; 1951
- Kovach, Karl., Beede,
William L., Hamrick, Joseph T.; Experimental
evaluation by thermodynamic methods of work input to a centrifugal compressor
operating with water injection; naca-rm-e50j31; 1951
- Eckert, E. R. G.,
Jackson, Thomas W., Francisco, Allen C.; Investigations
of slot configurations for film-cooled turbine blades by flow visualization
methods; naca-rm-e50k01; 1951
- McCullough, Stuart.,
Perkins, Porter J.; Flight
camera for photographing cloud droplets in natural suspension in the
atmosphere; naca-rm-e50k01a; 1951
- Wyatt, DeMarquis D.,
Hunczak, Henry R.; An
investigation of convergent-divergent diffusers at Mach number 1.85;
naca-rm-e50k07; 1951
- Gowan, William H., Jr.,
Mulholland, Donald R.; Effectiveness
of thermal-pneumatic airfoil-ice-protection system; naca-rm-e50k10a;
1951
- Fox, Jerome L.; Supersonic
tunnel investigation by means of inclined-plate technique to determine
performance of several nose inlets over Mach number range of 1.72 to 2.18;
naca-rm-e50k14; 1951
- Jansen, Emmert T.,
McAulay, John E.; Compressor
performance characteristics of a python turbine-propeller engine investigated
in altitude wind tunnel; naca-rm-e50k24; 1951
- Young, Allen E.,
McCullough, Stuart., Smith, Richard L.; Power
unit for high-intensity light source; naca-rm-e50k27; 1951
- Evans, Jerry E., Jr.;
Thermal
conductivity of 14 metals and alloys up to 1100 F; naca-rm-e50l07;
1951
- Brown, W. F., Jr.,
Schwartzbart, H., Jones, M. H.; Tensile
fracturing characteristics of several high-temperature alloys as influenced by
orientation in respect to forging direction; naca-rm-e50l28; 1951
- Beede, William L,
Hamrick, Joseph T, Withee, Joseph R , Jr; Evaluation
of centrifugal compressor performance with water injection;
naca-rm-e51e21; 1951
- Cesaro, Richard S.,
Lazar, James; Graphic
analysis of american and british axial-flow turbojet engine performance trends
(current and future); naca-rm-51k29; 1951
- Vincent, K. R., Gale,
B. M.; Altitude
performance of J35-A-17 turbojet engine in an altitude chamber;
naca-rm-e50i15; 1951
- Donald R. Buchele and
Pierce B. Day (Lewis Flight Propulsion Laboratory, Cleveland, Ohio); Interferometer
with Large Working Field Utilizing Schlieren Optics; naca-rm-e50i27;
1951
- W. E. Moeckel (Lewis
Flight Propulsion Laboratory, Cleveland, Ohio); Flow
Separation Ahead of a Blunt Axially Symmetric Body at Mach Numbers 1.76 to
2.10; naca-rm-e51i25; 1951
- Maynard I. Weinstein;
Performance
of supersonic scoop inlets; naca-rm-E52A22; February, 1952
- The Division of
Research Information; Supplementary
bibliography of NACA reports related to instrumentation and research
techniques; naca-rm-52d11; Jun 1952
- Carl E. Grigsby; Tests at Mach
number 1.62 of a series of missile configurations having tandem cruciform
lifting surfaces; naca-rm-l51j15; Jan 1952
- Charles F. Merlet,
Howard S. Carter; Total-pressure
recovery of a circular underslung inlet with three different nose shapes at a
Mach number of 1.42; naca-rm-l51k05; Feb 1952
- H. Kurt Strass, E. M.
Fields, Eugene D. Schult; Free-flight
measurements of some effects of aileron span, chord, and deflection and of
wing flexibility on the rolling effectiveness of ailerons on sweptback wings
at Mach numbers between 0.8 and 1.6; naca-rm-l51k16; Jan 1952
- H. Kurt Strass; Summary of some
effective aerodynamic twisting-moment coefficients of various wing-control
configurations at Mach numbers from 0.6 to 1.7 as determined from
rocket-powered models; naca-rm-l51k20; Jan 1952
- Edward F. Ulmann,
Robert W. Dunning; Some
effects of fin plan on the static stability of fin body combination at Mach
number 4.06; naca-rm-l52d15a; Jul 1952
- R. G. MacLeod; Low-speed
wind-tunnel investigation of a fixed and a free-floating wing-tip aileron on a
wing with leading edge swept back 51.3 degrees; naca-rm-l51h16a; Feb
1952
- Merrill H. Mead; Observations of
unsteady flow phenomena for an inclined body fitted with stabilizing fins;
naca-rm-a51k05; Jan 1952
- John F. Stroud; Experimental
investigation of the effect of forebody bluntness on the pressure recovery and
drag of a twin-scoop inlet-body combination at Mach numbers of 1.4 and
1.7; naca-rm-a51k14; Feb 1952
- John R. Spreiter; Downwash and
sidewash fields behind cruciform wings; naca-rm-a51l17; Jan 1952
- Howard F. Matthews,
Walter E. McNeill; The
effect of various missile characteristics on airframe frequency response;
naca-rm-a51l17a; Jan 1952
- John B. McDevitt; A correlation
by means of the transonic similarity rules of the experimentally determined
characteristics of 22 rectangular wings of symmetrical profile;
naca-rm-a51l17b; Feb 1952
- Donald W. Smith, Verlin
D. Reed; A
comparison of the chordwise pressure distribution and spanwise distribution of
loading at subsonic speeds on two triangular wings of aspect ratio 2 having
NACA 0005 and 0008 sections; naca-rm-a51l21; May 1952
- Robert H. Barnes; An analysis of
the effect of structural feedback on the flutter of a control surface having a
power-boost system; naca-rm-a51i25; Jun 1952
- S. Sherman Edwards; Experimental
and theoretical study of factors influencing the longitudinal stability of an
air-to-air missile at a Mach number of 1.4; naca-rm-a51j19; Jan
1952
- Ellis G. Slack; Experimental
investigation of heat transfer through laminar and turbulent boundary layers
on a cooled flat plate at a mach number of 2.4; naca-tn-2686; Apr
1952
- Herbert F. Hardrath,
Elmer C. Utley, Jr.; An
experimental investigation of the behavior of 24S-T4 aluminum alloy subjected
to repeated stresses of constant and varying amplitudes; naca-tn-2798; Oct
1952
- Paul Kuhn, Herbert F.
Hardrath; An
engineering method for estimating notch-size effect in fatigue tests on
steel; naca-tn-2805; Oct 1952
- Coleman duP. Donaldson,
Roy H. Lange; Study
of the pressure rise across shock waves required to separate laminar and
turbulent boundary layers; naca-rm-l52c21; may 1952
- Alexander D. Hammond,
James M. Watson; The
aerodynamic characteristics at transonic speeds of an all-movable, tapered, 45
degrees sweptback, aspect-ratio-4 tail surface deflected about a skewed hinge
axis; naca-rm-l52d28; Jul 1952
- Harvey H. Hubbard; A survey of the
aircraft-noise problem with special reference to its physical aspects;
naca-tn-2701; May 1952
- Chung-Hua Wu, Curtis A.
Brown, Vasily D. Prian; An
approximate method of determining the subsonic flow in an arbitrary stream
filament of revolution cut by arbitrary turbomachine blades; naca-tn-2702;
Jun 1952
- Charles E. Shepard,
Isidore Warshawsky; Electrical
techniques for compensation of thermal time lag of thermocouples and
resistance thermometer elements; naca-tn-2703; May 1952
- Joseph Marin, W. P.
Hughes; Fatigue
strengths of 14S-T4 aluminum alloy subjected to biaxial tensile stresses;
naca-tn-2704; Jun 1952
- Robert H Wasserman; Theory of
supersonic potential flow in turbomachines; naca-tn-2705; Jun 1952
- Donald J. Michel, John
Mizisin, Vasily Prian; Effect
of changing passage configuration on internal-flow characteristics of a
48-inch centrifugal compressor; naca-tn-2706; May 1952
- Arthur L. Jones, John
S. White; Analogue-computer
simulation of an autopilot servo system having nonlinear response
characteristics; naca-tn-2707; Jun 1952
- Wallace E. Howell; Comparison of
three multicylinder icing meters and critique of multicylinder method;
naca-tn-2708; Jun 1952
- Darnley M. Howard,
Frank C. Smith; Fatigue
and static tests of flush-riveted joints; naca-tn-2709; Jun 1952
- Ivan E. Beckwith,
Herbert W. Ridyard, Nancy Cromer; The
aerodynamic design of high Mach number nozzles utilizing axisymmetric flow
with application to a nozzle of square test section; naca-tn-2711; Jun
1952
- John H. Hilton, Jr.; Flow
characteristics over a lifting wedge of finite aspect ratio with attached and
detached shock waves at a Mach number of 1.40; naca-tn-2712; Jun
1952
- Sidney C. Huntley; Effect of
compressor-outlet air bleed on performance of a centrifugal-flow turbojet
engine with a constant-area jet nozzle; naca-tn-2713; Jun 1952
- Almer D. Crim, Marlin
E. Hazen; Normal
accelerations and operating conditions encountered by a helicopter in air-mail
operations; naca-tn-2714; Jun 1952
- Julian H. Kainer, Mary
Dowd King; The theoretical
characteristics of triangular-tip control surfaces at supersonic speeds Mach
lines behind trailing edges; naca-tn-2715; Jul 1952
- R. S. Barker; Effect
of open circular holes on tensile strength and elongation of sheet specimens
of a magnesium alloy; naca-tn-2716; Jun 1952
- H. W. Eickner, W. Z.
Olson, R. F. Blomquist; Effect
of temperatures from -70 to 600 F on strength of adhesive-bonded lap shear
specimens of clad 24S-T3 Aluminum alloy and of cotton-and glass-fabric plastic
laminates; naca-tn-2717; Jun 1952
- Hans J. Reissner,
Leonard Meyerhoff, Martin Bloom; Two-dimensional
steady nonviscous and viscous compressible flow through a system of
equidistant blades; naca-tn-2718; Jun 1952
- E. Epremian, R. F.
Mehl; Investigation
of statistical nature of fatigue properties; naca-tn-2719; Jun 1952
- W. F. Lindsey, Milton
D. Humphreys; Effects
of aspect ratio on air flow at high subsonic Mach numbers; naca-tn-2720;
Jul 1952
- Franklin K. Moore; Displacement
effect of a three-dimensional boundary layer; naca-tn-2722; Jun
1952
- Franklin K. Moore; Use of the
boundary layer of a cone to measure supersonic flow inclination;
naca-tn-2723; Jun 1952
- Keith C. Harder; Transonic
similarity rules for lifting wings; naca-tn-2724; Jun 1952
- W. E. Moeckel; Interaction
of oblique shock waves with regions of variable pressure, entropy, and
energy; naca-tn-2725; Jun 1952
- John R. Spreiter; On the
application of transonic similarity rules; naca-tn-2726; Jun 1952
- John P. Roberts, Leo L.
Beranek; Experiments in
external noise reduction of a small pusher-type amphibian airplane;
naca-tn-2727; Jul 1952
- Samuel Kraus; An
analysis of supersonic flow in the region of the leading edge of curved
airfoils, including charts for determining surface-pressure gradient and
shock-wave curvature; naca-tn-2729; Jun 1952
- W. F. Lindsey; Choking
of a subsonic induction tunnel by the flow from an induction nozzle;
naca-tn-2730; Jul 1952
- H. J. Hamjian, W. G.
Lidman; Influence of
structure on properties of sintered chromium carbide; naca-tn-2731; Jun
1952
- Leo Cohen; Theoretical
investigation of velocity diagrams of a single-stage turbine for a turbojet
engine at maximum thrust per square foot turbine frontal area;
naca-tn-2732; Jun 1952
- E. R. G. Eckert, John
N. B. Livingood; Method
for calculation of heat transfer in laminar region of air flow around
cylinders of arbitrary cross section (including large temperature differences
and transpiration cooling); naca-tn-2733; Jun 1952
- Robert K. Souter,
Joseph B. Emerson; Summary
of available hail literature and the effect of hail on aircraft in flight;
naca-tn-2734; Sep 1952
- Walter G. Walker, Paul
W. J. Schumacher; An
analysis of the normal accelerations and airspeeds of a two-engine type of
transport airplane in commercial operations on routes in the central United
States from 1948 to 1950; naca-tn-2735; Jul 1952
- James J. Kramer, John
D. Stanitz; Two-dimensional
shear flow in a 90 degree elbow; naca-tn-2736; Jun 1952
- Joseph Marin, H. A. B.
Wiseman; Plastic
stress-strain relations for combined tension and compression;
naca-tn-2737; Jul 1952
- Bernard Mazelsky,
Joseph A. Drischler; Numerical
determination of indicial lift and moment functions for a two-dimensional
sinking and pitching airfoil at Mach numbers 0.5 and 0.6; naca-tn-2739;
Jul 1952
- Randall C. Maydew,
Constantine C. Pappas; Experimental
investigation of the local and average skin friction in the laminar boundary
layer on a flat plate at a Mach number of 2.4; naca-tn-2740; Jul
1952
- John D. Bird, Jacob H.
Lichtenstein, Byron M. Jaquet; Investigation
of the influence of fuselage and tail surfaces on low-speed static stability
and rolling characteristics of a swept-wing model; naca-tn-2741; Jul
1952
- Paul F. Brinich, Nick
S. Diaconis; Boundary-layer
development and skin friction at mach number 3.05; naca-tn-2742; Jul
1952
- W. Flugge; Landing-gear
impact; naca-tn-2743; Oct 1952
- Milton D. Van Dyke; Practical
calculation of second-order supersonic flow past nonlifting bodies of
revolution; naca-tn-2744; Jul 1952
- J. W. Freeman, J. F.
Ewing, A. E. White; Influence
of chemical composition on rupture test properties at 1500 F of forged
chromium-cobalt-nickel-iron base alloys; naca-tn-2745;
- F. N. Rhines, A. W.
Cochardt; Preview of
behavior of grain boundaries in creep of aluminum bicrystals;
naca-tn-2746; Jul 1952
- Chung-Hua Wu, Curtis A.
Brown, Eleanor L. Costilow; Analysis
of flow in a subsonic mixed-flow impeller; naca-tn-2749; Aug 1952
- Chung-Hau Wu; Matrix
and relaxation solutions that determine subsonic through flow in an axial-flow
gas turbine; naca-tn-2750; Jul 1952
- Franklin W. Diederich;
A simple
approximate method for calculating spanwise lift distributions and aerodynamic
influence coefficients; naca-tn-2751; Aug 1952
- Neal Tetervin, David A.
Levine; A
study of the stability of the laminar boundary layer as affected by changes in
the boundary-layer thickness in regions of pressure gradient and flow through
the surface; naca-tn-2752; Aug 1952
- James E. Fitzpatrick,
WIlliam C. Schneider; Effects
of Mach number variation between 0.07 and 0.34 and Reynolds number variation
between 0.97 x 10(exp 6) and 8.10 x 10(exp 6) power on the maximum lift
coefficient of a wing of NACA 64-210 airfoil sections; naca-tn-2753; Aug
1952
- James L. Amick; A method of
selecting the thickness, hollowness, and size of a supersonic wing for least
drag and sufficient bending strength at specified flight conditions;
naca-tn-2754; Jul 1952
- Leslie W. Lassiter; Noise from
intermittent jet engines and steady-flow jet engines with rough burning;
naca-tn-2756; Aug 1952
- Leslie W. Lassiter,
Harvey H. Hubbard; Experimental
studies of noise from subsonic jets in still air; naca-tn-2757; Aug
1952
- Robert L. Johnson, Max
A. Swikert, Edmond E. Bisson; Wear
and sliding friction properties of nickel alloys suited for cages of
high-temperature rolling-contact bearings I : alloys retaining mechanical
properties to 600 F; naca-tn-2758; Aug 1952
- Robert L. Johnson, Max
A. Swikert, Edmond E. Bisson; Wear
and sliding friction properties of nickel alloys suited for cages of
high-temperature rolling-contact bearings II : alloys retaining mechanical
properties above 600 F; naca-tn-2759; Aug 1952
- Paul Seide; Derivation
of stability criterions for box beams with longitudinally stiffened covers
connected by posts; naca-tn-2760; Aug 1952
- Almer d. Crim, John P.
Reeder, James B. Whitten; Instrument-flight
results obtained with a combined-signal flight indicator modified for
helicopter use; naca-tn-2761; Aug 1952
- John M. Riebe, Rodger
L. Naeseth; Aerodynamic
characteristics of three deep-step planing-tail flying-boat hulls and a
transverse-step hull with extended afterbody; naca-tn-2762; Aug
1952
- John C. Houbolt, Eldon
E. Kordes; Gust-response
analysis of an airplane including wing bending flexibility; naca-tn-2763;
Aug 1952
- Dorris M. Ehret; Accuracy of
approximate methods for predicting pressures on pointed nonlifting bodies of
revolution in supersonic flow; naca-tn-2764; Aug 1952
- Eziaslav N. Harrin; A flight
investigation of the effect of shape and thickness of the boundary layer on
the pressure distribution in the presence of shock; naca-tn-2765; Sep
1952
- Richard R. Heldenfels,
William M. Roberts; Experimental
and theoretical determination of thermal stresses in a flat; naca-tn-2769;
Aug 1952
- Myron L. Gossard, Paul
Seide, William M. Roberts; Thermal
buckling of plates; naca-tn-2771; Aug 1952
- Perry L. Blackshear,
Jr.; Driving
standing waves by heat addition; naca-tn-2772; Aug 1952
- Mitchel H. Bertram; An approximate
method for determining the displacement effects and viscous drag of laminar
boundary layers in two-dimensional hypersonic flow; naca-tn-2773; Sep
1952
- Neal Tetervin; A
method for finding a least-squares polynomial that passes through a specified
point with specified derivatives; naca-tn-2774; Sep 1952
- Byron M. Jaquet; Effect of
linear spanwise variations of twist and circular-arc camber on low-speed
static stability, rolling, and yawing characteristics of a 45 degree sweptback
wing of aspect ratio 4 and taper ratio 0.6; naca-tn-2775; Aug 1952
- John M. Hedgepeth; Theoretical
distribution of slip angles in an aggregate of face-centered cubic
crystals; naca-tn-2777; Aug 1952
- M. A. Sherman; Stress
and strain at onset of crazing of polymethyl methacrylate at various
temperatures; naca-tn-2778; Sep 1952
- B. M. Axilrod, M. A.
Sherman, V. Cohen, I. Wolock; Effects
of moderate biaxial stretch-forming on tensile and crazing properties of
acrylic plastic glazing; naca-tn-2779; Oct 1952
- Harry C. Mickleboro,
Richard B. Fahrer, C. C. Shufflebarger; Flight
investigation of transient wing response on a four-engine bomber airplane in
rough air with respect to center-of-gravity accelerations; naca-tn-2780;
Sep 1952
- H. G. Lew; Bending
of thin plates with compound curvature; naca-tn-2782; Oct 1952
- Martin B. Biles, J. A.
Putnam; Use
of a consolidated porous medium for measurement of flow rate and viscosity of
gases at elevated pressures and temperatures; naca-tn-2783; Sep
1952
- Morris Morduchow,
Joseph H. Clarke; Method
for calculation of compressible laminar boundary-layer characteristics in
axial pressure gradient with zero heat transfer; naca-tn-2784; Sep
1952
- Stanley U. Benscoter,
Richard H. MacNeal; Introduction
to electrical-circuit analogies for beam analysis; naca-tn-2785; Sep
1952
- Stanley U. Benscoter,
Richard H. MacNeal; Equivalent-plate
theory for a straight multicell wing; naca-tn-2786; Sep 1952
- Dean R. Chapman; Airfoil
profiles for minimum pressure drag at supersonic velocities : application of
shock-expansion theory, including consideration of hypersonic range;
naca-tn-2787; Sep 1952
- S. F. Murray, Robert L.
Johnson; Effects of
solvents in improving boundary lubrication of steel by silicones;
naca-tn-2788; Sep 1952
- A. J. Eggers; On
the calculation of flow about objects traveling at high supersonic speeds;
naca-tn-2811; Oct 1952
- C. W. MacGregor, N.
Grossman; Effects of
cyclic loading on mechanical behavior of 24S-T4 and 75S-T6 aluminum alloys and
SAE 4130 steel; naca-tn-2812; Oct 1952
- Robert F. Smiley; The application
of planing characteristics to the calculation of the water-landing loads and
motions of seaplanes of arbitrary constant cross section; naca-tn-2814;
Nov 1952
- Joseph L. Sims,
Emmanuel Schnitzer; A
theoretical investigation of the effect of partial wing lift of hydrodynamic
landing characteristics of V-bottom seaplanes in step impacts;
naca-tn-2815; Nov 1952
- Robert F. Smiley; Water-pressure
distribution during landings of a prismatic model having an angle of dead rise
of 22 1/2 degrees and beam-loading coefficients of 0.48 and 0.97;
naca-tn-2816; Nov 1952
- Robert F. Smiley; A theoretical
and experimental investigation of the effects of yaw on pressures, forces, and
moments during seaplane landings and planing; naca-tn-2817; Nov
1952
- Stephen H. Maslen; Second
approximation to laminar compressible boundary layer on flat plate in slip
flow; naca-tn-2818; Nov 1952
- Jacob H. Lichtenstein,
James L. Williams; Effect
of high-lift devices on the static-lateral-stability derivatives of a 45
degree sweptback wing of aspect ratio 4.0 and taper ratio 0.6 in combination
with a body; naca-tn-2819; Nov 1952
- Marvin Shinbrot; An analysis of
the errors in curve-fitting problems with an application to the calculation of
stability parameters from flight data; naca-tn-2820; Nov 1952
- J. W. Clark; Torsion
tests of aluminum-alloy stiffened circular cylinders; naca-tn-2821; Nov
1952
- J. W. Clark; Torsion
tests of aluminum-alloy stiffened circular cylinders; naca-tn-2823; Nov
1952
- Stanley F. Racisz; Effects of
independent variations of mach number and reynolds number on the maximum lift
coefficients of four NACA 6-series airfoil sections; naca-tn-2824; Nov
1952
- Gerald E. Nitzberg,
Stewart M. Crandall; A
comparative examination of some measurements of airfoil section lift and drag
at supercritical speeds; naca-tn-2825; Nov 1952
- J. R. Ketchum, R. T.
Craig; Simulation of
linearized dynamics of gas-turbine engines; naca-tn-2826; Nov 1952
- E. B. Klunker, Conrad
Rennemann, Jr.; Effect
of a finite trailing-edge thickness on the drag of rectangular and delta wings
at supersonic speeds; naca-tn-2828; Nov 1952
- George P. Wood; Experiments on
transonic flow around wedges; naca-tn-2829; Nov 1952
- William M. Schulze,
George C. Ashby, Jr., John R. Erwin; Several
combination probes for surveying static and total pressure and flow
direction; naca-tn-2830; Nov 1952
- Margery E. Hannah,
Kenneth Margolis; Span
load distributions resulting from constant angle of attack, steady rolling
velocity, steady pitching velocity, and constant vertical acceleration for
tapered sweptback wings with streamwise tips subsonic leading edges and
supersonic trailing ...; naca-tn-2831; Dec 1952
- Walter G. Vincenti,
Cleo B. Wagoner; Theoretical
study of the transonic lift of a double-wedge profile with detached bow
wave; naca-tn-2832; Dec 1952
- Roy Steiner; An
analysis of normal accelerations and airspeeds of one type of twin-engine
transport airplane in commercial operations over a northern transcontinental
route; naca-tn-2833; Now 1952
- John D. Stanitz,
Gaylord O. Ellis; Flow
surfaces in rotating axial-flow passages; naca-tn-2834; Nov 1952
- John Mizisin, Donald J.
Michel; Effect of
changing passage configuration on internal-flow characteristics of a 48-inch
centrifugal compressor II : change in hub shape; naca-tn-2835; Nov
1952
- D. C. Hamilton, W. R.
Morgan; Radiant-interchange
configuration factors; naca-tn-2836; Dec 1952
- I. J. Kolodner, F.
Reiche, H. F. Ludloff; Corrections
for drag, lift, and moment of an axially symmetrical body placed in a
supersonic tunnel having a two-dimensional pressure gradient;
naca-tn-2837; Nov 1952
- Virgil E. Schrock; Calorimetric
determination of constant-pressure specific heats of carbon dioxide at
elevated pressures and temperatures; naca-tn-2838; Dec 1952
- John P. Reeder, James
B. Whitten; Some effects of
varying the damping in pitch and roll on the flying qualities of a small
single-rotor helicopter; naca-tn-2459; Jan 1952
- Y. C. Fung, A. Kaplan;
Buckling of
low arches or curved beams of small curvature; naca-tn-2840; Nov
1952
- Nemeth, Zolton N Macks,
E Fred Anderson, William J; Investigation
of 75-millimeter-bore deep-groove ball bearings under radial load at high
speeds I : oil-flow-studies; naca-tn-2841; December 1952
- Ulysse J. Blanchard; The planing
characteristics of a surface having a basic angle of dead rise of 40 degrees
and horizontal chine flare; naca-tn-2842; Dec 1952
- James C. Laurence, L.
Gene Landes; Auxiliary
equipment and techniques for adapting the constant-temperature hot-wire
anemometer to specific problems in air-flow measurements; naca-tn-2843;
Nov 1952
- John Dimeff, Ralph K.
Hallett, Jr., C. Frederick Hansen; X-ray
instrumentation for density measurements in a supersonic flow field;
naca-tn-2845; Dec 1952
- Robert L. Johnson, Max
A. Swikert, Edmond E. Bisson; Effective
lubrication range for steel surfaces boundary lubricated at high sliding
velocities by various classes of synthetic fluids; naca-tn-2846; Dec
1952
- Robert E. Dannenberg,
James A. Weiberg; Section
characteristics of a 10.5-percent-thick airfoil with area suction as affected
by chordwise distribution of permeability; naca-tn-2847; Dec 1952
- Charles E. Frank, Angus
U. Blackham, Donald E. Swarts; Investigation
of spontaneous ignition temperatures of organic compounds with particular
emphasis on lubricants; naca-tn-2848; Dec 1952
- H. F. Ludloff, M. B.
Friedman; Corrections for
lift, drag, and moment of an airfoil in a supersonic tunnel having a given
static pressure gradient; naca-tn-2849; Dec 1952
- Henry B. Suydam; Hydrodynamic
characteristics of a low-drag, planing-tail flying boat hull;
naca-tn-2481; Jan 1952
- Jerome B. Hammack; The aerodynamic
design of supersonic propellers from structural considerations;
naca-tn-2851; Dec 1952
- Carr B. Neel, Jr.; An
investigation utilizing an electrical analogue of cyclic de-icing of a hollow
steel propeller with an external blade shoe; naca-tn-2852; Dec 1952
- W. F. Lindsey, Bernard
N. Daley; Effect of
compressibility on the flow past a two-dimensional bump; naca-tn-2484; Apr
1952
- Robert S. Ruggeri; General
correlation of temperature profiles downstream of a heated air jet directed at
various angles to air stream; naca-tn-2855; Dec 1952
- Alfred A. Marino, N.
Mastrocola; Wind-tunnel
investigation of the contribution of a vertical tail to the directional
stability of a fighter-type airplane; naca-tn-2488;
- Albert A Schy, Ordway
B. Gates, Jr.; A
theoretical method of analyzing the effects of yaw-damper dynamics on the
stability of an aircraft equipped with a second-order yaw damper;
naca-tn-2857; Dec 1952
- Arthur Henderson, Jr.;
Supersonic
wave drag of nonlifting delta wings with linearly varying thickness ratio;
naca-tn-2858; Dec 1952
- Blake W. Corson, Jr.,
Julian D. Maynard; The
Langley 2,000-horsepower propeller dynamometer and tests at high speed of an
NACA 10-(3)(08)-03 two-blade propeller; naca-tn-2859; Dec 1952
- Herbert S. Ribner, E.
Leonard Arnoff; Interaction
between a supersonic stream and a parallel subsonic stream bounded by fluid at
rest; naca-tn-2860; Dec 1952
- J. M. Hodge, W. T.
Lankford; Influence of
nonmartensitic transformation products on mechanical properties of tempered
martensite; naca-tn-2862; Dec 1952
- Simon Ostrach; Laminar
natural-convection flow and heat transfer of fluids with and without heat
sources in channels with constant wall temperatures; naca-tn-2863; Dec
1952
- B. F. Ruffner, Eloise
Hout; Stresses and
deformations in wings subjected to torsion; naca-tn-2600; Feb 1952
- Manuel Stein, J.
Mayers; Compressive
buckling of simply supported curved plates and cylinders of sandwich
construction; naca-tn-2601; Jan 1952
- W. D. Manly, Paul A.
Beck; Survey
of the chromium-cobalt-nickel phase diagram at 1200 C; naca-tn-2602; Feb
1952
- E. L. Kamen, Paul A.
Beck; Survey
of portions of the cobalt-chromium-iron-nickel quaternary system;
naca-tn-2603; Feb 1952
- Chung-Hua Wu; A
general theory of three-dimensional flow in subsonic and supersonic
turbomachines of axial-, radial-, and mixed-flow types; naca-tn-2604; Jan
1952
- Alvin H. Sacks; Behavior of
vortex system behind cruciform wings - motions of fully rolled-up
vortices; naca-tn-2605; Jan 1952
- Arleigh P. Helfer; Electrical
pressure integrator; naca-tn-2607; Jun 1952
- Harold Mirels; Estimate
of slip effect on compressible laminar-boundary-layer skin friction;
naca-tn-2609; Jan 1952
- John D. Stanitz; One-dimensional
compressible flow in vaneless diffusers of radial- and mixed-flow centrifugal
compressors, including effects of friction, heat transfer and area change;
naca-tn-2610; Jan 1952
- W. Flugge; Stress
problems in pressurized cabins; naca-tn-2612; Feb 1952
- Bernard Mazelsky; Determination
of indicial lift and moment of a two-dimensional pitching airfoil at subsonic
mach numbers from oscillatory coefficients with numerical calculations for a
Mach number of 0.7; naca-tn-2613; Feb 1952
- Frank E. Marble, Irving
Michelson; Analytical
investigation of some three-dimensional flow problems in turbomachines;
naca-tn-2614; Mar 1952
- Carr B. Neel, Jr.,
Charles P. Steinmetz; The
calculated and measured performance characteristics of a heated-wire
liquid-water-content meter for measuring icing severity; naca-tn-2615; Jan
1952
- J. C. Evvard, Lawrence
R. Marcus; Achievement of
continuous wall curvature in design of two-dimensional symmetrical supersonic
nozzles; naca-tn-2616; Jan 1952
- A. D. Schwope, F. R.
Shober, L. R. Jackson; Creep
in metals; naca-tn-2618;
- Kenneth Margolis; Some remarks on
an approximate method of estimating the wave drag due to thickness at
supersonic speeds of three-dimensional wings with arbitrary profile;
naca-tn-2619; Feb 1952
- Chi-Teh Wang; Principle
and application of complementary energy method for thin homogeneous and
sandwich plates and shells with finite deflections; naca-tn-2620; Feb
1952
- E. B. Klunker, Keith C.
Harder; Comparison of
supersonic minimum-drag airfoils determined by linear and nonlinear
theory; naca-tn-2623; Feb 1952
- Gordon L. Dugger,
Sheldon Heimel; Flame
speeds of methane-air, propane-air, and ethylene-air mixtures at low initial
temperatures; naca-tn-2624; Feb 1952
- Walter G. Walker, Roy
Steiner; Summary of
acceleration and airspeed data from commercial transport airplanes during the
period from 1933 to 1945; naca-tn-2625; Feb 1952
- John R. Meyer, Jr.; An
investigation of bending-moment distribution on a model helicopter rotor blade
and a comparison with theory; naca-tn-2626; Feb 1952
- Stanley Fultz, M. L.
Pool; Coincidence
method applied to ion beam measurement; naca-tn-2627; Feb 1952
- Douglas Godfrey, Edmond
E. Bisson; Bonding of
molybdenum disulfide to various materials to form a solid lubricating film I :
the bonding mechanism; naca-tn-2628; Feb 1952
- R. G. Deissler, C. S.
Eian; Analytical and
experimental investigation of fully developed turbulent flow of air in a
smooth tube with heat transfer with variable fluid properties;
naca-tn-2629; Feb 1952
- Robert V. Hess; A solution of
the Navier-Stokes equation for source and sink flows of a viscous
heat-conducting compressible fluid; naca-tn-2630; Feb 1952
- Frank M. Hamaker,
Thomas J. Wong; The
similarity law for nonsteady hypersonic flows and requirements for the
dynamical similarity of related bodies in free flight; naca-tn-2631; Feb
1952
- Fred M. Reinhart; Corrosion of
magnesium alloy ZK60A in marine atmosphere and tidewater; naca-tn-2632;
Feb 1952
- Ralph W. Stone, Jr.; Estimation of
the maximum angle of sideslip for determination of vertical-tail loads in
rolling maneuvers; naca-tn-2633; Feb 1952
- Gene J. Delio; Evaluation
of three methods for determining dynamic characteristics of a turbojet
engine; naca-tn-2634; Feb 1952
- Simon Ostrach; An
analysis of laminar free-convection flow and heat transfer about a flat plate
parallel to the direction of the generating body force; naca-tn-2635; Feb
1952
- Fred E. Macks, William
J. Anderson, Zolton N. Nemeth; Influence
of lubricant viscosity on operating temperatures of 75-millimeter-bore
cylindrical-roller bearing at high speeds; naca-tn-2636; Feb 1952
- Paul Seide; Compressive
buckling of flat rectangular metalite type sandwich plates with simply
supported loaded edges and clamped unloaded edges; naca-tn-2637; Feb
1952
- H. J. Grover, W. S.
Hyler, L. R. Jackson; Fatigue
strengths of aircraft materials : axial-load fatigue tests on notched sheet
specimens of 24S-T3 and 75S-T6 aluminum alloys and of SAE 4130 steel with
stress-concentration factor of 1.5; naca-tn-2639; Feb 1952
- P. P. Bijlaard, G. P.
Fisher; Interaction of
column and local buckling in compression members; naca-tn-2640; Mar
1952
- John C. Martin; A vector study
of linearized supersonic flow applications to nonplanar problems;
naca-tn-2641; Jun 1952
- Marcel Dandois, David
Novik; Application of
linear analysis to an experimental investigation of a turbojet engine with
proportional speed control; naca-tn-2642; Feb 1952
- John C. Martin,
Isabella Jeffreys; Span
load distributions resulting from angle of attack, rolling, and pitching for
tapered sweptback wings with streamwise tips; naca-tn-2643; Jul
1952
- Dale L. Burrows, Milton
A. Schwartzberg; Experimental
investigation of an NACA 64A010 airfoil section with 41 suction slots on each
surface for control of laminar boundary layer; naca-tn-2644; Apr
1952
- Dean C. Lindquist; Effects of wing
lift and weight on landing-gear loads; naca-tn-2645; Mar 1952
- A. J. Eggers, Jr.,
Clarence A. Syvertson; Inviscid
flow about airfoils at high supersonic speeds; naca-tn-2646; Mar
1952
- Philip Schwed; Implication
of the transport equation for the semiempirical treatment of shields;
naca-tn-2647; Mar 1952
- S. E. Slaymaker, Robert
R. Lynn, Robin B. Gray; Experimental
investigation of transition of a model helicopter rotor from hovering to
vertical autorotation; naca-tn-2648; Mar 1952
- William B. Briggs; Effect of Mach
number on the flow and application of compressibility corrections in a
two-dimensional subsonic-transonic compressor cascade having varied
porous-wall suction at the blade tips; naca-tn-2649; Mar 1952
- M. L. Pool, S. Fultz;
Radioautographic
method for examining distribution of particles in a cyclotron beam;
naca-tn-2650; Mar 1952
- Stephen H. Maslen; Supersonic
conical flow; naca-tn-2651; Mar 1952
- John D. Stanitz,
Gaylord O. Ellis; Two-dimensional
flow on general surfaces of revolution in turbomachines; naca-tn-2654; Mar
1952
- Paul A. Libby, Morris
Morduchow, Martin Bloom; Critical
study of integral methods in compressible laminar boundary layers;
naca-tn-2655; Mar 1952
- Walter Castles, Jr.,
Noah C. New; A blade-element
analysis for lifting rotors that is applicable for large inflow and blade
angles and any reasonable blade geometry; naca-tn-2656; Jul 1952
- Artur Mager, Arthur G.
Hansen; Laminar
boundary layer over flat plate in a flow having circular streamlines;
naca-tn-2658; Mar 1952
- John L. Patterson; A miniature
electrical pressure gage utilizing a stretched flat diagram; naca-tn-2659;
Apr 1952
- Harry Press; An
approach to the prediction of the frequency distribution of gust loads on
airplanes in normal operations; naca-tn-2660; Apr 1952
- Paul Kuhn, James P.
Peterson, L. Ross Levin; A
summary of diagonal tension Part I : methods of analysis; naca-tn-2661;
May 1952
- Paul Kuhn, James P.
Peterson, L. Ross Levin; A
summary of diagonal tension Part II : experimental evidence; naca-tn-2662;
May 1952
- Harry Press, Robert L.
McDougal; The gust and
gust-load experience of a twin-engine low-altitude transport airplane in
operation on a northern transcontinental route; naca-tn-2663; Apr
1952
- Howard A. Stine,
Richard Scherrer; Experimental
investigation of the turbulent-boundary-layer temperature-recovery factor on
bodies of revolution at Mach numbers from 2.0 to 3.8; naca-tn-2664; Mar
1952
- Alfred Gessow, Almer D.
Crim; An
extension of lifting rotor theory to cover operation at large angles of attack
and high inflow conditions; naca-tn-2665; Apr 1952
- G. V. R. Rao; Two-dimensional
subsonic flow past elliptic cylinder by the variational method;
naca-tn-2666; Mar 1952
- W. D. Hayes, R. C.
Roberts, N. Haaser; Generalized
linearized conical flow; naca-tn-2667; Mar 1952
- Daniel Friedman,
Willard R. Westphal; Experimental
investigation of a 90 degree cascade diffusing bend with an area ratio of
1.45:1 and with several inlet boundary layers; naca-tn-2668; Apr
1952
- Barry Moskowitz; Approximate
theory for calculation of lift of bodies, afterbodies, and combinations of
bodies; naca-tn-2669; Apr 1952
- Milton D. Van Dyke; High-speed
subsonic characteristics of 16 NACA 6-series airfoil sections;
naca-tn-2670; Mar 1952
- Chi-Teh Wang, Harry
Zukerberg; Investigation
of stress distribution in rectangular plates with longitudinal stiffeners
under axial compression after buckling; naca-tn-2671; Mar 1952
- Reece V. Hensley; Theoretical
augmentation of turbine-propeller engine by compressor-inlet water injection,
tail-pipe burning, and their combination; naca-tn-2672; Mar 1952
- Reece V. Hensley; Theoretical
performance of an axial-flow compressor in a gas-turbine engine operating with
inlet water injection; naca-tn-2673; Mar 1952
- John D. Bird, Donald R.
Riley; Some
experiments on visualization of flow fields behind low-aspect-ratio wings by
means of a tuft grid; naca-tn-2674; May 1952
- R. Fabian Goranson,
Christopher C. Kraft, Jr.; Measurements
of flying qualities of an F-47D-30 airplane to determine lateral and
directional stability and control characteristics; naca-tn-2675; Jul
1952
- Jack N. Nielsen,
William C. Pitts; Wing-body
interference at supersonic speeds with an application to combinations with
rectangular wings; naca-tn-2677; Apr 1952
- A. I Rush, J. W.
Freeman, A. E. White; Abnormal
grain growth in S-816 alloy; naca-tn-2678; Apr 1952
- Paul Seide; The
stability under longitudinal compression of flat symmetric corrugated-core
sandwich plates with simply supported loaded edges and simply supported or
clamped unloaded edges; naca-tn-2679; Apr 1952
- Gordon L. Dugger,
Dorothy D. Graab; Flame
speeds of 2,2,4-trimethylpentane-oxygen-nitrogen mixtures; naca-tn-2680;
Apr 1952
- Willard R. Wesphal,
James C. Dunavant; A
compressible-flow plotting device and its application to cascade flows;
naca-tn-2681; Apr 1952
- Mark R. Nichols, Edwin
B. Goral; A
low-speed investigation of a fuselage-side air inlet for use at transonic
flight speeds; naca-tn-2684; Apr 1952
- Mark R. Nichols, Donald
W. Rinkoski; A low-speed
investigation of an annular transonic air inlet; naca-tn-2685; Apr
1952
- Adolf Busemann; Application of
transonic similarity; naca-tn-2687; Apr 1952
- John C. Evvard, Stephen
H. Maslen; Three-dimensional
supersonic nozzles and inlets of arbitrary exit cross section;
naca-tn-2688; Apr 1952
- Jacob H. Lichtenstein;
Effect of
high-lift devices on the low-speed static lateral and yawing stability
characteristics of an untapered 45 degrees sweptback wing; naca-tn-2689;
May 1952
- C. Frederick Hansen,
George J. Nothwang; Condensation
of air in supersonic wind tunnels and its effects on flow about models;
naca-tn-2690; Apr 1952
- Seymour Lieblein; Theoretical and
experimental analysis of one-dimensional compressible flow in a rotating
radial-inlet impeller channel; naca-tn-2691; Apr 1952
- Coleman DuP. Donaldson;
On the form
of the turbulent skin-friction law and its extension to compressible
flows; naca-tn-2692; May 1952
- Walton L. Howes, Donald
R. Buchele; A theory and
method for applying interferometry to the measurement of certain
two-dimensional gaseous density fields; naca-tn-2693; Apr 1952
- Stanford E. Neice; A method for
stabilizing shock waves in channel flow by means of a surge chamber;
naca-tn-2694; Jun 1953
- William N. Harrison,
Joseph W. Pitts, Joseph C. Richmond, Stanley G. Benner; Migration
of cobalt during firing of ground-coat enamels on iron; naca-tn-2695; Jun
1952
- L. D. McGraw, C. A.
Snavely, H. L. Moore, P. T. Woodberry, C. L. Faust; A
fundamental study of the mechanism by which hydrogen enters metals during
chemical and electrochemical processing; naca-tn-2696; Apr 1952
- George B. Brajnikoff;
Method and
graphs for the evaluation of air-induction systems; naca-tn-2697; May
1952
- Robert W. Miller; Theoretical
analysis of hydrodynamic impact of a prismatic float having freedom in
trim; naca-tn-2698; Jun 1952
- John C. Martin, Kenneth
Margolis, Isabella Jeffreys; Calculation
of lift and pitching moments due to angle of attack and steady pitching
velocity at supersonic speeds for thin sweptback tapered wings with streamwise
tips and supersonic leading and trailing edges; naca-tn-2699; Jun
1952
- George E. Kaattari,
Jack N. Nielsen, William C. Pitts; Method
for estimating pitching-moment interference of wing-body combinations at
supersonic speed; naca-rm-a52b06; Apr 1952
- John C. Heitmeyer,
Robert B. Petersen; LIft,
drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic
speeds - twisted and cambered triangular wing of aspect ratio 2 with NACA
0005-63 thickness distributions; naca-rm-a52b08; Apr 1952
- Simon C. Sommer, James
A. Stark; The effect of
bluntness on the drag of spherical-tipped truncated cones of fineness ratio 3
at Mach numbers 1.2 to 7.4; naca-rm-a52b13; Apr 1952
- Bruce E. Tinling,
Armando E. Lopez; The
effects of Reynolds number at Mach numbers up to 0.94 on the loading on a 35
degree swept-back wing having NACA 65(1)A012 streamwise sections;
naca-rm-a52b20; Jun 1952
- Robert S. Chubb; Experimental
investigation of the static aerodynamic and dynamic damping-in-roll
characteristics of an 8-cm aircraft rocket with solid and slotted fins;
naca-rm-a52c04; Jun 1952
- Donald Conrard; Lift, drag, and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds :
plane triangular wing of aspect ratio 3 with air-to-air missile models mounted
externally; naca-rm-a52c10a; Jun 1952
- Forrest E. Gowen,
Edward W. Perkins; Drag
of circular cylinders for a wide range of Reynolds numbers and Mach
numbers; naca-rm-a52c20; Jun 1952
- Thomas N. Canning,
Billy Pat Denardo; Investigation
of lift and center of pressure of low-aspect-ratio, cruciform, triangular, and
rectangular wings in combination with a slender fuselage at high supersonic
speeds; naca-rm-a52c24; Jun 1952
- John W. Boyd; Aerodynamic
characteristics of two 25-percent-area trailing-edge flaps on an aspect ratio
2 triangular wing at subsonic and supersonic speeds; naca-rm-a52d01c; Jul
1952
- Dean R. Chapman, Robert
H. Kester; Effect of
trailing edge thickness on lift at supersonic velocities; naca-rm-a52d17;
Jul 1952
- John C. Heitmeyer; Lift, drag and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds :
plane tapered wing of aspect ratio 3.1 with 3 percent thick rounded nose
section; naca-rm-a52d23; Jul 1952
- Jack N. Nielsen, George
E. Kaattari, William C. Drake; Comparison
between prediction and experiment for all-movable wing and body combinations
at supersonic speeds : lift, pitching moment, and hinge moment;
naca-rm-a52d29; Aug 1952
- Duane W. Dugan; Effects of
three types of blunt trailing edges on the aerodynamic characteristics of a
plane tapered wing of aspect ratio 3.1, with a 3-percent- thick biconvex
section; naca-rm-a52e01; Jul 1952
- John O. Reller, Jr.,
Frank M. Hamaker; An
experimental investigation of the base pressure characteristics of nonlifting
bodies of revolution at Mach numbers from 2.73 to 4.98; naca-rm-a52e20;
Sep 1952
- David H. Dennis,
Bernard E. Cunningham; Forces
and moments on pointed blunt-nosed bodies of revolution at Mach numbers from
2.75 to 5.00; naca-rm-a52e22; Aug 1952
- John C. Heitmeyer,
Willard G. Smith; Effects
of simulated skin wrinkles on the wing surface on the aerodynamic
characteristics of two wing-body combinations employing wings of low aspect
ratio at subsonic and supersonic speeds; naca-rm-a52e23; Aug 1952
- Marvin Abramovitz; Theoretical
investigation of the performance of proportional navigation guidance systems :
effect of method of positioning the radar antenna on the speed of
response; naca-rm-a52e27; Aug 1952
- Benjamin H. Beam; The effects of
oscillation amplitude and frequency on the experimental damping in pitch of a
triangular wing having an aspect ratio of 4; naca-rm-a52g07; Sep
1952
- Edward W. Perkins,
Leland H. Jorgensen; Investigation
of the drag of various axially symmetric nose shapes of fineness ratio 3 for
Mach numbers from 1.24 to 3.67; naca-rm-a52h28; Nov 1952
- William C. Triplett,
Stuart C. Brown; Lateral
and directional dynamic-response characteristics of a 35 degree swept-wing
airplane as determined from flight measurements; naca-rm-a52i17; Dec
1952
- Elliott D. Katzen,
William C. Pitts; Comparison
between prediction and experiment for all-movable wing and body;
naca-rm-a52i30; Dec 1952
- Emil J. Kremzier,
Joseph Davids; Performance
characteristics of canard-type missile with wing-mounted nacelle engines at
Mach numbers 1.5 to 2.0; naca-rm-e52j08; Nov 1952
- Alfred S. Valerino; Effects of
internal corner fillets on pressure recovery : mass flow characteristics of
scoop-type conical supersonic inlets; naca-rm-e52j10; Dec 1952
- Leonard J. Obery, Evan
A. Fradenburgh, John F. Mello; Influence
of fuselage and canard-type control surface on the flow field adjacent to a
rearward fuselage station at a Mach number of 2.0 : data presentation;
naca-rm-e51k05; Jan 1952
- David S. Gabriel,
George G. Younger, William R. Mickelsen; Experimental
study of isothermal wake-flow characteristics of various flame-holder
shapes; naca-rm-e51k07; Jan 1952
- K. R. Vincent, S. C.
Huntley, H. D. Wilsted; Comparison
of locked-rotor and windmilling drag characteristics of an
axial-flow-compressor type turbojet engine; naca-rm-e51k15; Jan
1952
- Fred T. Esenwein, Carl
F. Schueller; Analytical
and experimental investigation of inlet-engine matching for turbojet-powered
aircraft at Mach numbers up to 2.0; naca-rm-e51k20; Feb 1952
- I. Irving Pinkel, John
S. Serafini, John L. Gregg; Pressure
distribution and aerodynamic coefficients associated with heat addition to
supersonic air stream adjacent to two-dimensional supersonic wing;
naca-rm-e51k26; Feb 1952
- Stanley L. Koutz, Reece
V. Hensley; Loitering and
range performance of turbojet-powered aircraft determined by off-design engine
cycle analysis; naca-rm-e51k29; Feb 1952
- Jackson, H Herbert; Flight
measurements of the effects of surface condition on the supersonic drag of
fin-stabilized parabolic bodies of revolution; naca-rm-l52b26; May 02,
1952
- Henry R. Hunczak; Investigation
at Mach numbers 2.98 and 2.18 of axially symmetric free-jet diffusion with a
ram-jet engine; naca-rm-e51l24; Feb 1952
- Richard Hood, WIlliam
E. Phillips, Jr.; Dynamic
response of turbine-blade temperature to exhaust-gas temperature for
gas-turbine engines; naca-rm-e52a14; Feb 1952
- Seymour Lieblein,
George W. Lewis, Jr., Donald M. Sandercock; Experimental
investigation of an axial flow compressor inlet stage operating at transonic
relative inlet Mach numbers I : over-all performance of stage with transonic
rotor and subsonic stators up to rotor relative inlet Mach number of 1.1;
naca-rm-e52a24; Mar 1952
- Thomas R. Heaton,
William R. Slivka, Leonard F. Westra; Cold-air
investigation of a turbine with nontwisted rotor blades suitable for air
cooling; naca-rm-e52a25; Mar 1952
- Albert M. Lord; An experimental
investigation of the combustion properties of a hydrocarbon fuel and several
magnesium and boron slurries; naca-rm-e52b01; Apr 1952
- Irving A. Johnsen; Investigation
of a 10-stage subsonic axial-flow research compressor I : aerodynamic
design; naca-rm-e52b18; Apr 1952
- Wesley E. Messing,
Loren W. Acker; Transonic
free-flight drag results of full-scale models of 16-inch-diameter ram-jet
engines; naca-rm-e52b19; Apr 1952
- George R. Kinney; Internal-film-cooling
experiments with 2- and 4-inch smooth-surface tubes and gas temperatures to
2000 F; naca-rm-e52b20; Apr 1952
- Emil J. Kremzier,
Murray Dryer; Aeronautical
interference effects on normal and axial force coefficients of several
engine-strut-body configurations at Mach numbers of 1.8 and 2.0;
naca-rm-e52b21; Apr 1952
- John F. Klapproth, Guy
N. Ullman, Edward R. Tysl; Performance
of an impulse-type supersonic compressor with stators; naca-rm-e52b22; Apr
1952
- S. C. Huntley, H. D.
Wilsted; Altitude
performance investigation of two flame-holder and fuel-system configurations
in short afterburner; naca-rm-e52b25; May 1952
- R. G. Dressler, C. S.
Eian; Investigation
of effective thermal conductivities of powders; naca-rm-e52c05; Jun
1952
- John R. Jack, Lawrence
I. Gould; Aerodynamics of
slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6)
to 15 x 10(exp 6) II : aerodynamic load distributions of series of five bodies
having conical noses and cylindrical afterbodies; naca-rm-e52c10; May
1952
- Reeves P. Cochran,
Francis S. Stepka, Morton H. Krasner; Experimental
investigation of air-cooled turbine blades in turbojet engine XI :
internal-strut-supported rotor blade; naca-rm-e52c21; Jun 1952
- Warner L. Sterwart,
Harold J. Schum, Warren J. Whitney; Investigation
of turbines for driving supersonic compressors I : design and performance of
first configuration; naca-rm-e52c25; Jun 1952
- Andrew E. Abramson; Investigation
of internal film cooling of exhaust nozzle of a 1000-pound-thrust
liquid-ammonia liquid-oxygen rocket; naca-rm-e52c26; Jun 1952
- George W. Lewis, Jr.;
Experimental
investigation of axial-flow compressor inlet stage operating at transonic
relative inlet Mach numbers : blade-coordinate data; naca-rm-e52c27; Jun
1952
- Harold L. Bloom; Preliminary
survey of boundary-layer development at a nominal Mach number of 5.5;
naca-rm-e52d03; Jun 1952
- A. J. Cervenka, E. E.
Dangle; Effect of
fuel-air distribution on performance of a 16-inch ram-jet engine;
naca-rm-e52d08; Jun 1952
- Ward W. Wilcox; An analysis of
the potentialities of a two-stage counterrotating supersonic compressor;
naca-rm-e52e01; Jul 1952
- Alfred S. Valerino; Performance
characteristics at Mach numbers to 2.0 of various types of side inlets mounted
on fuselage of proposed supersonic airplane I : two-dimensional
compression-ramp inlets with semicircular cowls; naca-rm-e52e02; Jul
1952
- George A. Wise, Murray
Dryer; Influence of a
canard-type control surface on flow field in vicinity of symmetrical fuselage
at Mach numbers 1.8 and 2.0; naca-rm-e52e13; Jul 1952
- Edgar M. Cortright,
Jr., James F. Connors; Survey
of some preliminary investigations of supersonic diffusers at high Mach
numbers; naca-rm-e52e20; Jul 1952
- Wesley E. Messing,
Leonard Rabb; Transonic
free-flight investigation of the total drag and of the component drags (cowl
pressure, additive, base, friction, and internal) encountered by a
16-inch-diameter ram-jet engine for Mach numbers from 0.80 to 1.43;
naca-rm-e52f02; Aug 1952
- James F. Connors,
Richard R. Woollett; Experimental
investigation of a two-dimensional split-wing ram-jet inlet at Mach number of
3.85; naca-rm-e52f04; Aug 1952
- Murray Dryer, Andrew
Beke; Performance
characteristics of a normal-shock side inlet located downstream of a canard
control surface at Mach numbers of 1.5 and 1.8; naca-rm-e52f09; Jul
1952
- L. J. Obery, H. S.
Krasnow; Influence of a
canard-type control surface on the internal and external performance
characteristics of nacelle-mounted supersonic diffusers (conical centerbody)
at a rearward body station for a Mach number of 2.0; naca-rm-e52f16; Aug
1952
- Edward R. Bartoo, John
L. Clure; Experimental
investigation of air-cooled turbine blades in turbojet engine XII : cooling
effectiveness of a blade with an insert and with fins made of a continuous
corrugated sheet; naca-rm-e52f24; Aug 1952
- Fred Wilcox, Donald
Pennington; Spreading of
exhaust jet from 16-inch ram jet at Mach number 2.0; naca-rm-e52f25; Aug
1952
- Jack B. Esgar; An
analytical method for evaluating factors affecting application of
transpiration cooling to gas turbine blades; naca-rm-e52g01; Sep
1952
- Robert E. English,
Elmer H. Davison; Investigation
of turbines suitable for use in a turbojet engine with high compressor
pressure ratio and low compressor-tip speed III : velocity-diagram study of
two-stage and downstream-stator turbines for engine operation at constant
rotative speed; naca-rm-e52g15; Nov 1952
- Robert R. Ziemer, Henry
O. Slone; Analytical
procedures for rapid selection of coolant passage configurations for
air-cooled turbine rotor blades and for evaluation of heat-transfer, strength,
and pressure-loss characteristics; naca-rm-e52g18; Sep 1952
- David S. Boman, William
E. Mallett; Investigation
of thrust augmentation using water-alcohol injection on a 5200-pound-thrust
axial-flow-type turbojet engine at static sea-level conditions;
naca-rm-e52g30; Sep 1952
- Hadley T. Richards,
Henry O. Slone, W. Byron Brown; Procedure
for calculating turbine blade temperatures and comparison of calculated with
observed values for two stationary air-cooled blades; naca-rm-e52h07; Sep
1952
- Leonard J. Obery,
Howard S. Krasnow; Performance
characteristics of canard-type missile with vertically mounted nacelle engines
at Mach numbers 1.5 to 2.0; naca-rm-e52h08; Sep 1952
- H. George Krull, Fred
W. Steffen; Performance
characteristics of one convergent and three convergent-divergent nozzles;
naca-rm-e52h12; Sep 1952
- Upson, Ralph H
(University of Minnesota) Phelps, George M (University of Minnesota) Liu,
Tung-Sheng (University of Minnesota); Equal-strength
design of tension-field webs and uprights; naca-tn-2548; 1952
- Elmer H. Davison,
Robert E. English; Investigation
of turbines suitable for use in a turbojet engine with high compressor
pressure ratio and low compressor-tip speed IV : effect of increasing blade
speed on velocity diagrams of turbine for engine operation at constant
rotative speed; naca-rm-e52h13; Nov 1952
- Paul M. Ordin, Edward
A. Rothenberg, William H. Rowe; Investigation
of liquid fluorine and hydrazine-ammonia mixture in 100-pound-thrust rocket
engine; naca-rm-e52h22; Oct 1952
- Leonard K. Tower; Effect of water
vapor on combustion of magnesium hydrocarbon slurry fuels in small-scale
afterburner; naca-rm-e52h25; Oct 1952
- Eugene Perchonok, Fred
A. Wilcox; Investigation
of ram-jet afterburning as a means of varying effective exhaust nozzle
area; naca-rm-e52h27; Nov 1952
- Paul C. Simon; Performance
characteristics at Mach numbers to 2.0 of various types of side inlets mounted
on fuselage of proposed supersonic airplane IV : rectangular cowl inlets with
two-dimensional compression ramps; naca-rm-e52h29; Oct 1952
- George A. Wise, Leonard
J. Obery; Influence of
fuselage-mounted rocket boosters on flow field at inlet and on diffuser
performance of strut-mounted engine at Mach numbers of 1.8 and 2.0;
naca-rm-e52i02; Oct 1952
- James F. Connors,
Richard R. Woolett; Some
observations of flow at the throat of a two-dimensional diffuser at a Mach
number of 3.85; naca-rm-e52i04; Nov 1952
- Carl B. Wentworth,
Herbert G. Hurrell, Shigeo Nakanishi; Evaluation
of operating characteristics of a supersonic free-jet facility for full-scale
ram-jet investigations; naca-rm-e52i08; Oct 1952
- James F. Connors,
Richard R. Woollett; Performance
characteristics of several types of axially symmetric nose inlets at Mach
number 3.85; naca-rm-e52i15; Nov 1952
- Frank, Charles E
(University of Cincinnati) Blackham, Angus U (University of Cincinnati); Investigation
of hydrocarbon ignition; naca-tn-2549; 1952
- Andrew Beke, J. L.
Allen; Force
and pressure-recovery characteristics of a conical-type nose inlet operating
at Mach numbers of 1.6 to 2.0 and at angles of attack to 9 degrees;
naca-rm-e52i30; Nov 1952
- Satish Dhawan; Direct
measurements of skin friction; naca-tn-2567; Jan 1952
- Chieh-Chien Chang; General
consideration of problems in compressible flow using the hodograph method;
naca-tn-2582; Jan 1952
- John L. Crigler, Jean
Gilman, Jr.; Calculation of
aerodynamic forces on a propeller in pitch or yaw; naca-tn-2585; Jan
1952
- D. N. Frey, J. W.
Freeman, A. E. White; Fundamental
effects of cold-work on some cobalt-chromium-nickel-iron base creep-resistant
alloys; naca-tn-2586; Jan 1952
- Herbert C. Nelson,
Julian H. Berman; Calculations
on the forces and moments for an oscillating wing-aileron combination in
two-dimensional potential flow at sonic speed; naca-tn-2590; Jan
1952
- Harold E. Cleary; The effects of
Reynolds number on the application of NACA 16-series airfoil characteristics
to propeller design; naca-tn-2591; Jan 1952
- Morton Cooper, Clyde V.
Hamilton; Orientation of
orifices on bodies of revolution for determination of stream static pressure
at supersonic speeds; naca-tn-2592; Jan 1952
- Dwight O. Fearnow; Investigation
of the structural damping of a full-scale airplane wing; naca-tn-2594; Feb
1952
- Robert T. Yntema,
Benjamin Milwintzky; An
impulse-momentum method for calculating landing-gear contact conditions in
eccentric landings; naca-tn-2596; Jan 1952
- E. R. Van Driest; Investigation
of laminar boundary layer in compressible fluids using the Crocco method;
naca-tn-2597; Jan 1952
- Melvyn Savage, Loren A.
Beatty; A
technique applicable to the aerodynamic design of inducer-type multistage
axial-flow compressors; naca-tn-2598; Mar 1952
- Marvin D. Scadron,
Isidore Warshasky; Experimental
determination of time constants and Nusselt numbers for bare-wire
thermocouples in high-velocity air streams and analytic approximation of
conduction and radiation errors; naca-tn-2599; Jan 1952
- Gerald W. Englert,
Leonard J. Obery; Evaluation
of five conical center-body supersonic diffusers at several angles of
attack; naca-rm-e51l04; May 1952
- Gerard, George (New
York University) Wildhorn, Sorrel (New York University); A
study of Poisson's ratio in the yield region; naca-tn-2561; 1952
- Wallner, Lewis E
Prince, William R; Investigation
of afterburner performance and afterburner fuel system coking of the
Westinghouse XJ34-WE-32 engine; naca-rm-e51h28; February 21, 1952
- Hennings, Glen Morrell,
Gerald; Preliminary
investigation of a chemical starting technique for the acid - gasoline rocket
propellant system; naca-rm-e52k21; 1952
- Goin, Kennith L; Theoretical
analyses to determine unbalanced trailing-edge controls having minimum hinge
moments due to deflection at supersonic speeds; naca-rm-l51f19; November
19, 1952
- Lauten, W T , Jr
Sylvester, Maurice A; Flutter
investigation of two thin, low-aspect ratio, swept, solid, metal wings in the
transonic range by use of a free-falling body; naca-rm-l51k28a; February
26, 1952
- Stoney, William E , Jr;
Pressure
distributions at Mach numbers from 0.6 to 1.9 measured in free flight on a
parabolic body of revolution with sharply convergent afterbody;
naca-rm-l51l03; April 1952
- Marley, Edward T
English, Roland D; Some
effects of aeroelasticity at Mach numbers from 0.7 to 1.6 on the rolling
effectiveness of thin flat-plate delta wings having 45 degree swept leading
edges and full-span constant-chord ailerons; naca-rm-l51l05; February 19,
1952
- Hallissy, Joseph M ,
Jr; Pressure
measurements on a body of revolution in the Langley 16-foot transonic tunnel
and a comparison with free-fall data; naca-rm-l51l07a; March 05,
1952
- Lord, Douglas R Ulmann,
Edward F; Pressure
measurements on an ogive-cylinder body at Mach number 4.04;
naca-rm-l51l20; February 26, 1952
- Grigsby, Carl E; An
investigation at Mach numbers of 1.62 and 1.93 of the lift effectiveness and
integrated downwash characteristics of several in-line missile configurations
having equal-span wings and tails; naca-rm-l52a02; April 11, 1952
- Hasel, Lowell E
Hamilton, Clyde V Sinclair, Archibald R; Preliminary
investigation of the drag characteristics of the NACA RM-10 missile at Mach
numbers of 1.40 and 1.59 in the Langley 4- by 4-foot tunnel;
naca-rm-l52a14; April 18, 1952
- Kuhn, Richard E
Wiggins, James W; Wind-tunnel
investigation of the aerodynamic characteristics in pitch of wing-fuselage
combinations at high subsonic speeds : aspect-ratio series;
naca-rm-l52a29; April 1952
- Chapman, Rowe, Jr
Morrow, John D; Longitudinal
stability and drag characteristics at Mach numbers from 0.70 to 1.37 of
rocket-propelled models having a modified triangular wing; naca-rm-l52a31;
May 02, 1952
- Purser, Paul E; An
approximation to the effect of geometric dihedral on the rolling moment due to
sideslip for wings at transonic and supersonic speeds; naca-rm-l52b01;
April 1952
- Hall, Albert W Mckay,
James M; The
effects on the aerodynamic characteristics of varying the wing thickness ratio
of a triangular wing-body configuration at transonic speeds from tests by the
NACA wing-flow method; naca-rm-l52b18; April 02, 1952
- Gillespie, Warren, Jr
Dietz, Albert E; Use
of an aerodynamically pulsed all-movable horizontal tail to obtain
longitudinal characteristics of rocket-powered models in free flight and some
initial results from an arrow-wing-body-tail configuration;
naca-rm-l52c10; May 19, 1952
- Nelson, William J
Bloetscher, Frederick; An
experimental investigation of the zero-lift pressure distribution over a wedge
airfoil in closed, slotted, and open-throat tunnels at transonic Mach
numbers; naca-rm-l52c18; June 16, 1952
- Czarnecki, K R Marte,
Jack E; Skin-friction
drag and boundary-layer transition on a parabolic body of revolution (NACA
RM-10)at a Mach number of 1.6 in the Langley 4-by-4 foot supersonic pressure
tunnel; naca-rm-l52c24; May 20, 1952
- Brown, Clarence A , Jr
Lundstrom, Reginald R; Flight
investigation from Mach number 0.8 to 2.0 to determine some effects of
wing-to-tail distance on the longitudinal stability and control
characteristics of a 60 degree delta-wing-canard missile; naca-rm-l52c26;
June 20, 1952
- Welsh, Clement J; Results of
flight tests to determine the drag of finite-length cylinders at high Reynolds
numbers for a Mach number range of 0.5 to 1.3; naca-rm-l52c31; June 16,
1952
- Hoffman, Sherwood; Transonic
flight tests to compare the zero-lift drags of underslung nacelles varied
spanwise on a 45 degree sweptback wing and body combination;
naca-rm-l52d04a; July 1952
- Wiggins, James W Kuhn,
Richard E; Wind-tunnel
investigation of the aerodynamic characteristics in pitch of wing-fuselage
combination at high subsonic speeds : sweep series; naca-rm-l52d18; July
02, 1952
- Goin, Kennith L; Effects of plan
form, airfoil section, and angle of attack on the pressures along the base of
blunt-trailing-edge wings at Mach numbers of 1.41, 1.62, and 1.96;
naca-rm-l52d21; September 16, 1952
- Estabrooks, Bruce B; An analysis of
the pressure distribution measured on a body of revolution at transonic speeds
in the slotted test section of the Langley 8-foot transonic tunnel;
naca-rm-l52d21a; June 25, 1952
- Sanders, E Claude, Jr;
Damping in
roll of models with 45, 60 and 70 degree delta wings determined at high
subsonic, transonic, and supersonic speeds with rocket-powered models;
naca-rm-l52d22a; June 25, 1952
- Leiss, Abraham; Flight
measurements at Mach numbers from 1.1 to 1.9 of the zero-lift drag of a
twin-engine supersonic ram-jet configuration; naca-rm-l52d24; June 23,
1952
- Moul, Martin T Wineman,
Andrew R; Longitudinal
stability and control characteristics from a flight investigation of a
cruciform canard missile configuration having an exposed wing-canard area
ratio of 16:1; naca-rm-l52d24a; June 25, 1952
- Hopko, Russell N
Sandahl, Carl A; Free-flight
investigation of the zero-lift drag of several wings at supersonic Mach
numbers extending to 2.6; naca-rm-l52d29; December 02, 1952
- Cole, Richard I; Pressure
distributions on bodies of revolution at subsonic and transonic speeds;
naca-rm-l52d30; July 21, 1952
- Jones, Jim J; Flow
separation from rods ahead of blunt noses at Mach number 2.72;
naca-rm-l52e05a; July 15, 1952
- Faget, Maxime A; A proposed
ram-jet control system operated by use of diffuser pressure recovery;
naca-rm-l52e05b; September 03, 1952
- Hart, Roger G; Effects
of stabilizing fins and a rear-support sting on the base pressure of a body of
revolution in free flight at Mach numbers from 0.7 to 1.3; naca-rm-l52e06;
September 22, 1952
- Judd, Joseph H Lauten,
William T , Jr; Flutter
of a 60 degree delta wing (NACA 65A003 airfoil) encountered at supersonic
speeds during the flight test of a rocket-propelled model;
naca-rm-l52e06a; September 25, 1952
- Bland, William M , Jr;
Effect of
fuselage interference on the damping in roll of delta wings of aspect ratio 4
in the Mach number range between 0.6 and 1.6 as determined with rocket
propelled vehicles; naca-rm-l52e13; July 15, 1952
- Spearman, M Leroy
Robinson, Ross B; Wind-tunnel
investigation of a ram-jet canard missile model having a wing and canard
surfaces of delta plan form with 70 degree swept leading edges : longitudinal
and lateral stability and control characteristics at a Mach number of
1.60; naca-rm-l52e15; August 1952
- Gates, Ordway B , Jr
Schy, Albert A; A
theoretical investigation of the effect of a target seeker sensitive to pitch
attitude on the dynamic stability and response characteristics of a supersonic
canard missile configuration; naca-rm-l52e19; August 26, 1952
- Coletti, Donald E; Investigation
of interference, lift, drag, and pitching moment of a series of rectangular
wing and body combinations at Mach numbers of 1.62, 1.93,and 2.41;
naca-rm-l52e26; August 13, 1952
- Wood, George P; Reflection of
shock waves from slotted walls at Mach number 1.62; naca-rm-l52e27; July
21, 1952
- Czarnecki, K R
Sinclair, Archibald, R; Preliminary
investigation of the effects of heat transfer on boundary-layer transition on
a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61;
naca-rm-l52e29a; July 29, 1952
- Curfman, Howard J , Jr
Grigsby, Carl E; Longitudinal
stability and control characteristics of a canard missile configuration for
Mach numbers from 1.1 to 1.93 as determined from free-flight and wind-tunnel
investigation; naca-rm-l52f06; August 08, 1952
- Hopko, Russell N; Preliminary
free-flight investigation of the effects of rivets and lap joints on the drag
of bodies at zero lift at supersonic Mach numbers to 2.1; naca-rm-l52f09;
August 20, 1952
- Giladett, Leo V
Wineman, Andrew R; Investigation
of vanes immersed in the jet of a solid-fuel rocket motor; naca-rm-l52f12;
September 10, 1952
- Piland, Robert O; Preliminary
free-flight investigation of the zero-lift drag penalties of several missile
nose shapes for infrared seeking devices; naca-rm-l52f23; December 09,
1952
- Rainey, Robert W; An
investigation of several supersonic missile configurations directed toward
minimizing center-of-pressure travel; naca-rm-l52g01; September 23,
1952
- D'Aiutolo, Charles T
Parker, Robert N; Preliminary
investigation of the low-amplitude damping in pitch of tailless delta- and
swept-wing configurations at Mach numbers from 0.7 to 1.35;
naca-rm-l52g09; August 20, 1952
- Cooper, Morton Hasel,
Lowell E Gapcynski, John P; A
pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of
revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36 degrees;
naca-rm-l52g14a; October 30, 1952
- Osborne, Robert S
Mugler, John P , Jr; Effects
of wing elasticity on the aerodynamic characteristics of a 45 degree
sweptback-wing-fuselage combination measured in the Langley 8-foot transonic
tunnel; naca-rm-l52g23; September 17, 1952
- Sabol, A P; A
preliminary investigation of shock-wave reflections in a small closed
ballistic range with various types of walls; naca-rm-l52g25; September 04,
1952
- Donaldson, Coleman Dup;
Heat
transfer and skin friction for turbulent boundary layers on heated or cooled
surfaces at high speeds; naca-rm-l52h04; October 02, 1952
- Grigsby, Carl E; The use of the
rolled-up vortex concept for predicting wing-tail interference and comparison
with experiment at Mach number of 1.62 for a series of missile configurations
having tandem cruciform lifting surfaces; naca-rm-l52h05; September 24,
1952
- Martz, C William
Church, James D Goslee, John W; Rocket-model
investigation to determine the force and hinge-moment characteristics of a
half-Delta tip control on a 59 degree sweptback delta wing between Mach
numbers of 0.55 and 1.43; naca-rm-l52h06; October 06, 1952
- Schult, Eugene D
Fields, E M; Free-flight
measurements of some effects of spoiler span and projection and wing
flexibility on rolling effectiveness and drag of plain spoilers on a tapered
sweptback wing at Mach numbers between 0.6 and 1.6; naca-rm-l52h06a;
October 03, 1952
- Whitcomb, Richard T; A study of the
zero-lift drag-rise characteristics of wing-body combinations near the speed
of sound; naca-rm-l52h08; September 03, 1952
- Johnson, Joseph L , Jr;
A study of
the flow field behind the triangular horizontal tail of a canard airplane at
approximately the vertical-tail location by means of a tuft grid;
naca-rm-l52h11; October 10, 1952
- Moul, Martin T Baber,
Hal T , Jr; The
longitudinal stability and control characteristics of a 60 degree delta-wing
missile having half-delta tip controls as obtained from a free-flight
investigation at transonic and supersonic speeds; naca-rm-l52h14; October
03, 1952
- Fields, E M; Some
effects of spoiler height, wing flexibility, and wing thickness on rolling
effectiveness and drag of unswept wings at Mach numbers between 0.4 and
1.7; naca-rm-l52h18; October 07, 1952
- Love, Eugene S Coletti,
Donald E Bromm, August F , Jr; Investigation
of the variation with Reynolds number of the base, wave, and skin-friction
drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62,
1.93, and 2.41 in the Langley 9-inch supersonic tunnel; naca-rm-l52h21;
October 17, 1952
- Purser, Paul E Stevens,
Joseph E; Exploratory
rocket flight tests to investigate the use of a freely spinning monoplane tail
for stabilizing a body; naca-rm-l52i05a; October 15, 1952
- Love, Eugene S; The effects of
a small jet of air exhausting from the nose of a body of revolution in
supersonic flow; naca-rm-l52i19a; November 12, 1952
- Jones, Ira P , Jr; Measurements of
aerodynamic heating obtained during demonstration flight tests of the Douglas
D-558-II airplane; naca-rm-l52i26a; November 26, 1952
- Boatright, William B;
Total
pressure and Schlieren studies of the wakes of various canard control surfaces
mounted on a missile body at a Mach number of 1.93; naca-rm-l52i29;
November 20, 1952
- Comenzo, Raymond J
Mackley, Ernest A; Preliminary
investigation of a rectangular supersonic scoop inlet with swept sides
designed for low drag at a Mach number of 2.7; naca-rm-l52j02; November
26, 1952
- Silvers, H Norman King,
Thomas J , Jr; Investigation
at high subsonic speeds of bodies mounted from the wing of an
unswept-wing-fuselage model, including measurements of body loads;
naca-rm-l52j08; November 14, 1952
- Wiley, Harleth G
Solomon, Martin; A
wind-tunnel investigation at low speeds of the aerodynamic characteristics of
various spoiler configurations on a thin 60 degrees delta wing;
naca-rm-l52j13; November 19, 1952
- Letko, William; A low-speed
experimental study of the directional characteristics of a sharp-nosed
fuselage through a large angle-of-attack range at zero angle of sideslip;
naca-rm-l52j14; November 19, 1952
- Love, Eugene S
O'Donnell, Robert M; Investigation
at supersonic speeds of the base pressure on bodies of revolution with and
without sweptback stabilizing fins; naca-rm-l52j21a; December 23,
1952
- Coletti, Donald E; Investigation
of the aerodynamic characteristics of the NACA RM-10 missile (with fins) at a
Mach number of 1.62 in the Langley 9-inch supersonic tunnel;
naca-rm-l52j23a; December 19, 1952
- Jacobsen, Carl R; Control
characteristics of trailing-edge spoilers on untapered blunt trailing-edge
wings of aspect ratio 2.7 with 0 degree and 45 degrees sweepback at Mach
numbers of 1.41 and 1.96; naca-rm-l52j28; December 03, 1952
- Bartlett, Walter A , Jr
Dettwyler, H Rudolph; Flight
test of a radial-burning solid-fuel ram jet; naca-rm-l52k03; December 10,
1952
- Chauvin, Leo T; Pressure
distribution and pressure drag for a hemispherical nose at Mach numbers 2.05,
2.54, and 3.04; naca-rm-l52k06; December 31, 1952
- Ulmann, Edward F
Dunning, Robert W; Aerodynamic
characteristics of two delta wings at Mach number 4.04 and correlations of
lift and minimum-drag data for delta wings at Mach numbers from 1.62 to
6.9; naca-rm-l52k19; December 23, 1952
- Diederich, Franklin W
Foss, Kenneth A; Charts
and approximate formulas for the estimation of aeroelastic effects on the
loading of swept and unswept wings; naca-tn-2608; February 1952
- Moore, Dwight G
(National Bureau of Standards) Mason, Mary A (National Bureau of Standards)
Harrison, William N (National Bureau of Standards); Relative
importance of various sources of defect-producing hydrogen introduced into
steel during application of vitreous coatings; naca-tn-2617; February
1952
- Stein, Manuel Anderson,
J Edward Hedgepeth, John M; Deflection
and stress analysis of thin solid wings of arbitrary plan form with particular
reference to delta wings; naca-tn-2621; February 1952
- Shinbrot, Marvin; A description
and a comparison of certain nonlinear curve-fitting techniques, with
applications to the analysis of transient-response data; naca-tn-2622;
February 1952
- Budiansky, Bernard
Kruszewski, Edwin T; Transverse
vibrations of hollow thin-walled cylindrical beams; naca-tn-2682; April
1952
- Rideout, Sheldon Paul
(University of Notre Dame) Beck, Paul A (University of Notre Dame); Survey
of portions of the chromium-cobalt-nickel-molybdenum quaternary system at 1200
degrees C; naca-tn-2683; April 1952
- Donaldson, Coleman Dup
Lange, Roy H; Study
of the pressure rise across shock waves required to separate laminar and
turbulent boundary layers; naca-tn-2770; September 1952
- Cole, Richard I Jordan,
Gareth H; The effect of a
simulated propeller slipstream on the aerodynamic characteristics of an
unswept wing panel with and without nacelles at Mach numbers from 0.30 to
0.86; naca-tn-2776; September 1952
- Merten, Kenneth F
Stephenson, Bertrand H; Some
dynamic effects of fuel motion in simplified model tip tanks on suddenly
excited bending oscillations; naca-tn-2789; September 1952
- Michael, William H ,
Jr; flow
studies in the vicinity of a modified flat-plate rectangular wing of aspect
ratio 0.25; naca-tn-2790; September 1952
- Holms, Arthur G Repko,
Andrew J; Correlation of
tensile strength, tensile ductility, and notch tensile strength with the
strength of rotating disks of several designs in the range of low and
intermediate ductility; naca-tn-2791; September 1952
- Sinclair, Archibald R
Robins, A Warner; A
method for the determination of the time lag in pressure measuring systems
incorporating capillaries; naca-tn-2793; September 1952
- Sullivan, Roger D; A comparison of
two methods of linearized characteristics for a simple unsteady flow;
naca-tn-2794; September 1952
- Rogallo, Vernon L; Effects of wing
sweep on the upwash at the propeller planes of multiengine airplanes;
naca-tn-2795; September 1952
- Schwartzberg, Milton A
Braslow, Albert L; Experimental
study of the effects of finite surface disturbances and angle of attack on the
laminar boundary layer of an NACA 64A010 airfoil with area suction;
naca-tn-2796; October 1952
- Hess, Robert V; A study of the
transient behavior of shock waves in transonic channels flows;
naca-tn-2797; October 1952
- Gray, Vernon H; Simple
graphical solution of heat transfer and evaporation from surface heated to
prevent icing; naca-tn-2799; October 1952
- Brown, W Byron
Livingood, John N B; Solutions
of laminar-boundary-equations which result in specific-weight-flow profiles
locally exceeding free-stream values; naca-tn-2800; September 1952
- Wood, George P
Gooderum, Paul B; Investigation
with an interferometer of the flow around a circular-arc airfoil at mach
numbers between 0.6 and 0.9; naca-tn-2801; October 1952
- Godfrey, Douglas
Bisson, Edmond E; Bonding
of molybdenum disulfide to various materials to form a solid lubricating film
II : friction and endurance characteristics of films bonded by practical
methods; naca-tn-2802; October 1952
- Wilterdink, P I Holms,
A G Manson, S S; A
theoretical and experimental investigation of the influence of temperature
gradients on the deformation and burst speeds of rotating disks;
naca-tn-2803; October 1952
- Kapryan, Walter J
Weinstein, Irving; The
planing characteristics of a surface having a basic angle of dead rise of 20
degrees and horizontal chine flare; naca-tn-2804; October 1952
- Ellis, Gaylord O
Stanitz, John D; Comparison
of two- and three-dimensional potential-flow solutions in a rotating impeller
passage; naca-tn-2806; October 1952
- Lina, Lindsay J Ricker,
Harry H , Jr; Measurements
of temperature variations in the atmosphere near the tropopause with reference
to airspeed calibration by the temperature method; naca-tn-2807; October
1952
- Frocht, M M (Illinois
Institute of Technology) Guernsey, R , Jr (Illinois Institute of Technology);
A special
investigation to develop a general method for three-dimensional photoelastic
stress analysis; naca-tn-2822; December 1952
- Barzelay, Martin E
(Syracuse University) Boison, James C (Syracuse University); Investigation
of stresses due to thermal gradients in typical aircraft structures;
naca-rm-51k06; January 25, 1952
- Reese, Bruce A (Purdue
University) Graham, Robert W (Purdue University); Design
of apparatus for determining heat transfer and frictional pressure drop of
nitric acid flowing through a heated tube; naca-rm-52d03; June 16,
1952
- Black, John M (Forest
Products Laboratory) Blomquist, R F (Forest Products Laboratory); Development
of metal-bonding adhesive FPL-710 with improved heat-resistant properties;
naca-rm-52f19; July 08, 1952
- Westmoreland, J C
(National Bureau of Standards); A
meter for timing the flow of very small volumes of a gas; naca-rm-52i09;
October 17, 1952
- Moore, R L (Aluminum
Company of America) Clark, J W (Aluminum Company of America); Torsion,
compression, and bending tests of tubular sections machined from 75S-T6 rolled
round rod; naca-rm-52i25; November 12, 1952
- Holzhauser, Curt A; The effect of
entrance Mach number and lip shape on the subsonic characteristics of a
scoop-type-air-induction system for a supersonic airplane;
naca-rm-a51j19a; January 09, 1952
- Cook, Woodrow L Kelly,
Mark W; The
use of area suction for the purpose of delaying separation of air flow at the
leading edge of a 63 degree swept-back wing : effects of controlling the
chordwise distribution of suction air velocities; naca-rm-a51j24; January
14, 1952
- Smith, Donald W
Shibata, Harry H Selan, Ralph; Lift,
drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic
speeds : an investigation at large Reynolds numbers of the low-speed
characteristics of several wing-body combinations; naca-rm-a51k28;
February 15, 1952
- Taylor, Robert A; Some effects of
side-wall modifications on the drag and pressure recovery of an NACA submerged
inlet at transonic speeds; naca-rm-a51l03a; February 15, 1952
- Mcfadden, Norman M
Bray, Richard S Rathert, George A , Jr; Flight
calibration of angle-of-attack and sideslip detectors on the fuselage of a 35
degree swept-wing fighter airplane; naca-rm-a52a04; February 25,
1952
- Hunton, Lynn W; Effects of
finite span on the section characteristics of two 45 degree swept-back wings
of aspect ratio 6; naca-rm-a52a10; March 17, 1952
- Cole, Henry, A , jr
Abramovitz, Marvin; Theoretical
investigation of the stability at negative static margins of a supersonic
missile with an autopilot sensitive to pitch angle and pitching velocity;
naca-rm-a52a14; March 17, 1952
- Kelly, Mark W; Low-speed
aerodynamic characteristics of a large-scale 60 degree swept-back wing with
high lift devices; naca-rm-a52a14a; March 03, 1952
- Seiff, Alvin SOMMER
SIMON C; Experimental
investigation of the drag of 30 degree, 60 degree, and 90 degree cone
cylinders at Mach numbers between 1.5 and 8.2; naca-rm-a52a14b; April 25,
1952
- Briggs, Robert O
Kerwin, William J Schmidt, Stanley F; Instrumentation
of the Ames supersonic free-flight wind tunnel; naca-rm-a52a18; April 24,
1952
- Seiff, Alvin James,
Carlton S Canning, Thomas N Boissevain, Alfred G; The
Ames supersonic free-flight wind tunnel; naca-rm-a52a24; April 25,
1952
- Rolls, L Stewart
Matteson, Frederick H; Wing
load distribution on a swept wing airplane in flight at Mach numbers up to
1.11, and comparison with theory; naca-rm-a52a31; April 14, 1952
- Maki, Ralph L; Full-scale
wind-tunnel investigation of the effects of wing modifications and
horizontal-tail location on the low-speed static longitudinal characteristics
of a 35 degree swept-wing airplane; naca-rm-a52b05; April 03, 1952
- James, Harry A; Low-speed
aerodynamic characteristics of a large-scale 45 degree swept-back wing with
partial-span slats, double-slotted flaps, and ailerons; naca-rm-a52b19;
April 28, 1952
- Emerson, Horace F Gale,
Bernard M; Aerodynamic
characteristics of two-plane, unswept tapered wings of aspect ratio 3 and
3-percent thickness from tests on a transonic bump; naca-rm-a52c07; May
02, 1952
- Blackaby, James R; An analytical
study of the comparative performance of four air-induction systems for
turbojet-powered airplanes designed to operate at Mach numbers up to 1.5;
naca-rm-a52c14; June 17, 1952
- Shibata, Harry H
Bandettini, Angelo Cleary, Joseph; An
investigation of the subsonic speed range of a full-span and a semispan model
of a plane wing and of a cambered and twisted wing, all having 45 degrees of
sweepback; naca-rm-a52d01; June 26, 1952
- Mccullough, George B
Gambucci, Bruno J; Boundary-layer
measurements on several porous materials with suction applied;
naca-rm-a52d01b; June 18, 1952
- Boltz, Frederick W
Kolbe, Carl D; The
forces and pressure distribution at subsonic speeds on a cambered and twisted
wing having 45 degrees of sweepback and aspect ratio of 3 and a taper ratio of
0.5; naca-rm-a52d22; July 18, 1952
- Dods, Jules B , Jr; Control
effectiveness and hinge-moment characteristics at low-speed of large-chord,
horn-balanced, flap-type controls on a triangular wing of aspect ratio 2;
naca-rm-a52f13; August 18, 1952
- White, Maurice D; Effect of
camber and twist on the stability characteristics of models having a 45 degree
swept wing as determined by the free-fall method at transonic speeds;
naca-rm-a52f16; August 29, 1952
- Anderson, Warren E
Frazer, Alson C; Investigation
of an NACA submerged inlet at Mach numbers from 1.17 to 1.99;
naca-rm-a52f17; September 15, 1952
- Edwards, George G
Tinling, Bruce E Ackerman, Arthur C; The
longitudinal characteristics at Mach numbers up to 0.92 of a cambered and
twisted wing having 40 degrees of sweepback and an aspect ratio of 10;
naca-rm-a52f18; September 15, 1952
- Selna, James Bright,
Loren G Schlaff, Bernard A; Investigation
of drag and pressure recovery of a scoop inlet in the transonic speed
range; naca-rm-a52f27; December 15, 1952
- Bandettini, Angelo; An
investigation at subsonic speeds of the rolling effectiveness of a small
perforated spoiler on a wing having 45 degrees of sweepback;
naca-rm-a52g02; September 15, 1952
- Chubb, Robert S; Experimental
investigation of the stability, control, and induced rolling moments of a
canard missile airframe at a Mach number of 1.7; naca-rm-a52g29; September
23, 1952
- Tinling, Bruce E; The
longitudinal characteristics at Mach numbers up to 0.9 of a wing-fuselage-tail
combination having a wing with 40 degrees of sweepback and an aspect ratio of
10; naca-rm-a52i19; December 12, 1952
- Reynolds, Robert M
Buell, Donald A Walker, John H; Investigation
of an NACA 4-(5)(05)-041 four-blade propeller with several spinners at Mach
numbers up to 0.90; naca-rm-a52i19a; December 24, 1952
- Heinle, Donovan R
Mcneill, Walter E; Correlation
of predicted and experimental lateral oscillation characteristics for several
airplanes; naca-rm-a52j06; December 15, 1952
- Guy, Lawrence D; Control
hinge-moment and effectiveness characteristics of a 60 degree half-delta tip
control on a 60 degree delta wing at Mach numbers of 1.41 and 1.96;
naca-rm-l52h13; October 14, 1952
- Raikh, A.; Calculation
of the lateral-dynamic stability of aircraft; naca-tm-1264; 1952
- Pomey, Jacques.; Friction and
wear; naca-tm-1318; 1952
- Wuest, Walter.; Development of
a laminar boundary layer behind a suction point; naca-tm-1336; 1952
- Bourcier de Carbon,
Christian.; Analytical
study of shimmy of airplane wheels; naca-tm-1337; 1952
- Scheil, Erich.; The oxidation
of metals and alloys; naca-tm-1338; 1952
- Tammann, Gustav.,
Koster, Werner.; Velocity
of action of oxygen, hydrogen sulfide, and halogens on metals;
naca-tm-1339; 1952
- Haskind, M. D.; Translational
motion of bodies under the free surface of a heavy fluid of finite depth;
naca-tm-1345; 1952
- Betchov, R.; Nonlinear
theory of a hot-wire anemometer; naca-tm-1346; 1952
- Sponder, E. W.; On the
representation of the stability region in oscillation problems with the aid of
the Hurwitz determinants; naca-tm-1348; 1952
- Tani, Itiro.; On
the design of airfoils in which the transition of the boundary layer is
delayed; naca-tm-1351; 1952
- Maekawa, T., Atsumi,
Shoichi.; Transition
caused by the laminar flow separation; naca-tm-1352; 1952
- Betchov, R., Welling,
W.; Some
experiences regarding the nonlinearity of hot wires; naca-tm-1223;
1952
- Zalovcik, John A.; Summary of
Stall-Warning Devices; naca-tn-2676; 1952
- Lewis, William,
Bergrun, Norman R.; A
probability analysis of the meteorological factors conductive to aircraft
icing in the United States; naca-tn-2738; 1952
- Costello, George R.,
Cummings, Robert L., Sinnette, John T., Jr.; Detailed
computational procedure for design of cascade blades with prescribed velocity
distributions in compressible potential flows; naca-report-1060;
1952
- Dugger, Gordon L.; Effect of
initial mixture temperature on flame speed of methane-air, propane-air, and
ethylene-air mixtures; naca-report-1061; 1952
- Johnson, Robert L.,
Swikert, Max A., Bisson, Edmond E.; Investigation
of wear and friction properties under sliding conditions of some materials
suitable for cages of rolling-contact bearings; naca-report-1062;
1952
- Chapman, Dean R.; Airfoil
profiles for minimum pressure drag at supersonic velocities -- general
analysis with application to linearized supersonic flow; naca-report-1063;
1952
- Macks, E. Fred.,
Nemeth, Zolton N.; Lubrication
and cooling studies of cylindrical-roller bearings at high speeds;
naca-report-1064; 1952
- Goodman, Irving A.,
Wise, Paul H.; Correlation
of physical properties with molecular structure for some dicyclic hydrocarbons
having high thermal-energy release per unit volume -- 2-alkylbiphenyl and the
two isomeric 2-alkylbicyclohexyl series; naca-report-1065; 1952
- Livingood, John N. B.,
Brown, W. Byron.; Analysis
of temperature distribution in liquid-cooled turbine blades;
naca-report-1066; 1952
- Mager, Arthur.; Generalization
of boundary-layer momentum-integral equations to three-dimensional flows
including those of rotating system; naca-report-1067; 1952
- Boksenbom, Aaron S.,
Hood, Richard.; Automatic
control systems satisfying certain general criterions on transient
behavior; naca-report-1068; 1952
- Kaplan, Carl.; On
a solution of the nonlinear differential equation for transonic flow past a
wave-shaped wall; naca-report-1069; 1952
- Donegan, James J.,
Pearson, Henry A.; Matrix
method of determining the longitudinal-stability coefficients and frequency
response of an aircraft from transient flight data; naca-report-1070;
1952
- Deyoung, John.; Theoretical
symmetric span loading due to flap deflection for wings of arbitrary plan form
at subsonic speeds; naca-report-1071; 1952
- Duberg, John E.,
Wilder, Thomas W., III.; Inelastic
column behavior; naca-report-1072; 1952
- Gossard, Myron L.; An iterative
transformation procedure for numerical solution of flutter and similar
characteristics-value problems; naca-report-1073; 1952
- Maxwell, W. A.; Oxidation-resistance
mechanism and other properties of molybdenum disilicide; naca-rm-e52a04;
1952
- Mayo, Wilbur L.; Hydrodynamic
impact of a system with a single elastic mode I : theory and generalized
solution with an application to an elastic airframe; naca-report-1074;
1952
- Miller, Robert W.,
Merten, Kenneth F.; Hydrodynamic
impact of a system with a single elastic mode II : comparison of experimental
force and response with theory; naca-report-1075; 1952
- Mathews, Charles W.,
Talmage, Donald B., Whitten, James B.; Effect
on longitudinal stability and control characteristics of a Boeing B-29
airplane of variations in stick-force and control-rate characteristics
obtained through use of a booster in the elevator-control system;
naca-report-1076; 1952
- Lomax, Harvard.,
Heaslet, Max A., Fuller, Franklyn B., Sluder, Loma.; Two-and
three-dimensional unsteady lift problems in high-speed flight;
naca-report-1077; 1952
- Carpenter, Paul J.; Effects of
compressibility on the performance of two full-scale helicopter rotors;
naca-report-1078; 1952
- Hubbard, Harvey H.,
Lassiter, Leslie W.; Sound
from a two-blade propeller at supersonic tip speeds; naca-report-1079;
1952
- Schy, Albert A.; A theoretical
analysis of the effects of fuel motion on airplane dynamics;
naca-report-1080; 1952
- Van Dyke, Milton D.; A study of
second-order supersonic flow theory; naca-report-1081; 1952
- Hamrick, Joseph T.,
Ginsburg, Ambrose., Osborn, Walter M.; Method
of analysis for compressible flow through mixed-flow centrifugal impellers of
arbitrary design; naca-report-1082; 1952
- Goldstein, Arthur W.;
Axisymmetric
supersonic flow in rotating impellers; naca-report-1083; 1952
- Mager, Artur., Mohoney,
John J., Budinger, Ray E.; Discussion
of boundary-layer characteristics near the wall of an axial-flow
compressor; naca-report-1085; 1952
- Michael, William H.,
Jr.; Analysis of the
effects of wing interference on the tail contributions to the rolling
derivatives; naca-report-1086; 1952
- Kinney, George R.,
Abramson, Andrew E., Sloop, John L.; Internal-liquid-film-cooling
experiments with air-stream temperatures to 2000 degrees F. in 2- and
4-inch-diameter horizontal tubes; naca-report-1087; 1952
- Adams, Gaynor J., Dugan
Duane W.; Theoretical
damping in roll and rolling moment due to differential wing incidence for
slender cruciform wings and wing-body combinations; naca-report-1088;
1952
- Runyan, Harry L.; Single-degree-of-freedom-flutter
calculations for a wing in subsonic potential flow and comparison with an
experiment; naca-report-1089; 1952
- Sivells, James C.,
Westrick, Gertrude C.; Method
for calculating lift distributions for unswept wings with flaps or ailerons by
use of nonlinear section lift data; naca-report-1090; 1952
- Fischel, Jack, Naeseth,
Rodger L., Hagerman, John R., O'hare, William M.; Effect
of aspect ratio on the low-speed lateral control characteristics of untapered
low-aspect-ratio wings equipped with flap and with retractable ailerons;
naca-report-1091; 1952
- Campbell, John P.,
Hunter, Paul A., Hewes, Donald E., Whitten, James B.; Flight
investigation of the effect of control centering springs on the apparent
spiral stability of a personal-owner airplane; naca-report-1092;
1952
- Stalder, Jackson R.,
Goodwin, Glen., Creager, Marcus O.; Heat
transfer to bodies in a high-speed rarified-gas stream; naca-report-1093;
1952
- Bryson, Arthur Earl,
Jr.; An
experimental investigation of transonic flow past two-dimensional wedge and
circular-arc sections using a Mach-Zehnder interferometer;
naca-report-1094; 1952
- Vincenti, Walter G.,
Wagoner, Cleo B.; Transonic
flow past a wedge profile with detached bow wave; naca-report-1095;
1952
- Lichtenstein, Jacob H.;
Experimental
determination of the effect of horizontal-tail size, tail length, and vertical
location on low-speed static longitudinal stability and damping pitch of a
model having 45 degree sweptback wing and tail surfaces; naca-report-1096;
1952
- Griffith, George E.; Stresses in a
two-bay noncircular cylinder under transverse loads; naca-report-1097;
1952
- Campbell, John P.,
McKinney, Marion O.; Summary
of Methods for Calculating Dynamic Lateral Stability and Response and for
Estimating Aerodynamic Stability Derivatives; naca-report-1098;
1952
- Watkins, Charles E.,
Berman, Julian N.; Air
forces and moments on triangular and related wings with subsonic leading edges
oscillating in supersonic potential flow; naca-report-1099; 1952
- Liepmann, H. W.,
Roshko, A., Dhawan, S.; On
reflection of shock waves from boundary layers; naca-report-1100;
1952
- Brown, B. Porter.,
Chilton, Robert G., Whitten, James B.; Flight
investigation of a mechanical feel device in an irreversible elevator control
system of a large airplane; naca-report-1101; 1952
- Ferri, Antonio.; The linearized
characteristics method and its application to practical nonlinear supersonic
problems; naca-report-1102; 1952
- Milwitzky, Benjamin.;
Generalized
theory for seaplane impact; naca-report-1103; 1952
- Ferri, Antonio., Nucci,
Louis M.; Preliminary
investigation of a new type of supersonic inlet; naca-report-1104;
1952
- Lomax, Harvard.,
Sluder, Loma.; Chordwise
and compressibility corrections to slender-wing theory; naca-report-1105;
1952
- Habel, Louis W.,
Henderson, James H., Miller, Mason F.; The
Langley annular transonic tunnel; naca-report-1106; 1952
- Bergrun, Norman R.; An empirically
derived basis for calculating the area, rate, and distribution of water-drop
impingement on airfoils; naca-report-1107; 1952
- Halfman, Robert L.; Experimental
aerodynamic derivatives of a sinusoidally oscillating airfoil in
two-dimensional flow; naca-report-1108; 1952
- Chapman, Dean R.,
Wimbrow, William R., Kester, Robert H.; Experimental
investigation of base pressure on blunt-trailing-edge wings at supersonic
velocities; naca-report-1109; 1952
- Klebanoff, P. S.,
Diehl, Z. W.; Some
features of artificially thickened fully developed turbulent boundary layers
with zero pressure gradient; naca-report-1110; 1952
- Macks, E Fred Nemeth,
Zolton N; Comparison of
high-speed operating characteristics of size 215 cylindrical-roller bearings
as determined in turbojet engine and in laboratory test rig;
naca-report-1084; 1952
- Holms, Arthur G; A biharmonic
relaxation method for calculating thermal stress in cooled irregular
cylinders; naca-report-1059; 1952
- Spakowski, Adolph, A.,
Belles, Frank E.; Variation
of pressure limits of flame propagation with tube diameter for various
isooctane-oxygen-nitrogen mixtures; naca-rm-e52a08; 1952
- Kofskey, Milton G.,
Rohlik, Harold E., Monroe, Daniel E.; Experimental
investigation of flow in an annular cascade of turbine nozzle blades of
constant discharge angle; naca-rm-e52a09; 1952
- Scadron, Marvin D.; Analysis of a
pneumatic probe for measuring exhaust-gas temperatures with some preliminary
experimental results; naca-rm-e52a11; 1952
- English, Robert E.,
Silvern, David H., Davison, Elmer H.; Investigation
of turbines suitable for use in a turbojet engine with high compressor
pressure ratio and low compressor-tip speed I : turbine-design requirements
for several engine operating conditions; naca-rm-e52a16; 1952
- Butze, Helmut F.; Effect of inlet
air and fuel parameters on smoking characteristics of a single tubular
turbojet engine combustor; naca-rm-e52a18; 1952
- Mark, H., Mark,
Herman., Zettle, Eugene V.; Axial-slot
air admission for controlling performance of a one-quarter-annual turbojet
combustor and comparison with complete engine; naca-rm-e52a21; 1952
- Moshos, George J.,
Serafini, John S., Brun, Rinaldo J.; Impingement
of water droplets on an NACA 65(sub 1)-212 airfoil at an angle of attack of 4
degrees; naca-rm-e52b12; 1952
- Jonash, Edmund R.,
Wear, Jerrold D., Hibbard, Robert R.; Relations
between fuel properties and combustion carbon deposition; naca-rm-e52b14;
1952
- Rosenbaum, B. M.,
Allen, G.; Calculation of
internal pressures in the fuel tube of a nuclear reactor; naca-rm-e52b28;
1952
- McCready, Robert R.,
Spooner, Robert B., Valerino, Michael F.; Distribution
of fissionable material in thermal reactors of spherical geometry for uniform
power generation; naca-rm-e52c11; 1952
- Koffel, William K.,
Kaufman, Harold R.; Empirical
cooling correlation for an experimental afterburner with an annular cooling
passage; naca-rm-e52c13; 1952
- Heller, Jack A.,
Whitney, Rose L., Cavicchi, Richard H.; Experimental
investigation of a conservatively designed turbine at four rotor-blade
solidities; naca-rm-e52c17; 1952
- Wear, Jerrold D., Cook,
William P.; Effect of fuel
properties on carbon deposition in atomizing and prevaporizing turbojet
combustors; naca-rm-e52c24; 1952
- Brown, W. Byron.,
Slone, Henry O.; Pressure
drop in coolant passages of two air-cooled turbine-blade configurations;
naca-rm-e52d01; 1952
- Finger, Harold B.,
Dugan, James F., Jr.; Analysis
of stage matching and off-design performance of multistage axial-flow
compressors; naca-rm-e52d07; 1952
- Maxwell, W. A.; Some stress
rupture and creep properties of molybdenum disilicide in the range of 1600 to
2000 F; naca-rm-e52d09; 1952
- Yaker, Charles.,
Garrett, Floyd B., Sikora, Paul F.; Investigation
of engine performance and high-temperature properties of precision-cast
turbine blades of high carbon Stellite 21 and controlled grain-size-Stellite
21; naca-rm-e52d10; 1952
- Koffel, William K.,
Kaufman, Harold R.; Investigation
of heat-transfer coefficients in an afterburner; naca-rm-e52d11;
1952
- Davison, Elmer H.,
English, Robert E.; Investigation
of turbines suitable for use in a turbojet engine with high compressor
pressure ratio and low compressor tip-speed II : velocity-diagram study of
turbine for engine operation with constant exhaust-nozzle area;
naca-rm-e52d14; 1952
- Sams, Eldon W.; Experimental
investigation of average heat-transfer and friction coefficients for air
flowing in circular tubes having square-thread-type roughness;
naca-rm-e52d17; 1952
- Costello, G. R.,
Cummings, R. L., Serovy, G. K.; Experimental
investigation of axial-flow compressor stator blades designed to obtain high
turning angles by means of boundary-layer suction; naca-rm-e52d18;
1952
- Schum, Eugene F.,
Freche, John C., Stelpflug, William J.; Comparison
of calculated and experimental temperatures of water-cooled turbine
blades; naca-rm-e52d21; 1952
- Hibbard, R. R.,
Schalla, R. L.; Solubility
of water in hydrocarbons; naca-rm-e52d24; 1952
- Ellis, C. W.,
Hollister, D. P., Wilsted, H. D.; Investigation
of performance of several double-shroud ejectors and effect of variable-area
exhaust nozzle on single ejector performance; naca-rm-e52d25; 1952
- Walker, Curtis L.,
Fenn, David B.; Investigation
of power extraction characteristics and braking requirements of a windmilling
turbojet engine; naca-rm-e52d30; 1952
- Osborn, Walter M.,
Hamrick, Joseph T.; Design
and test of mixed-flow impellers I :aerodynamic design procedure;
naca-rm-e52e05; 1952
- Povolny, John H.; Use of choked
nozzle technique and exhaust jet diffuser for extending operable range of
jet-engine research facilities; naca-rm-e52e12; 1952
- Leissler, L. Abbott.,
Hearth, Donald P.; Preliminary
investigation of effect of angle of attack on pressure recovery and stability
characteristics for a vertical-wedge-nose inlet at Mach number of 1.90;
naca-rm-e52e14; 1952
- Rebeske, John J., Jr.,
Forrette, Robert E.; Investigation
of losses in the XJ35-A-23 two-stage turbine; naca-rm-e52e15; 1952
- Haefeli, Rudolph C.; Use of fences
to increase uniformity of boundary layer on side walls of supersonic wind
tunnels; naca-rm-e52e19; 1952
- Greathouse, W. K.,
Hollister, D. P.; Preliminary
air-flow and thrust calibrations of several conical cooling-air ejectors with
a primary to secondary temperature ratio of 1.0 I :diameter ratios of 1.21 and
1.10; naca-rm-e52e21; 1952
- Withee, Joseph R., Jr.,
Beede, William L.; Design
and test of mixed-flow impellers II :experimental results, impeller model
MFI-1A; naca-rm-e52e22; 1952
- Stewart, Warner L.,
Schum, Harold J., Wong, Robert Y.; Investigation
of turbines for driving supersonic compressors II :performance of first
configuration with 2.2 percent reduction in nozzle flow area / Warner L.
Stewart, Harold J. Schum, Robert Y. Wong; naca-rm-e52e26; 1952
- Huppert, Merle C.; Preliminary
investigation of flow fluctuations during surge and blade row stall in
axial-flow compressors / c Merle C. Huppert; naca-rm-e52e28; 1952
- Nussdorfer, Theodore
J., Obery, Leonard J., Englert, Gerald W.; Pressure
recovery, drag, and subcritical stability characteristics of three conical
supersonic diffusers at stream Mach numbers from 1.7 to 2.0;
naca-rm-e51h27; 1952
- Obey, Leonard T.,
Englert, Gerald W., Nussdorfer, Theodore J., Jr.; Pressure
recovery, drag, and subcritical stability characteristics of conical
supersonic diffusers with boundary-layer removal; naca-rm-e51h29;
1952
- Conrad, E. William.,
Jansen, Emmert T.; Effects
of internal configuration on afterburner shell temperatures;
naca-rm-e51i07; 1952
- Schramm, Wilson B.,
Ziemer, Robert R.; Investigations
of air-cooled turbine rotors for turbojet engines I :experimental disk
temperature distribution in modified J33 split-disk rotor at speeds up to 6000
RPM; naca-rm-e51i11; 1952
- Meyer, Carl L.,
Johnson, LaVern A.; Performance
and operational characteristics of a python turbine-propeller engine at
simulated altitude conditions / Carl L. Meyer and Lavern A. Johnson;
naca-rm-e51i14; 1952
- Ladanyi, Dezso J.; Ignition delay
experiments with small-scale rocket engine at simulated altitude conditions
using various fuels with nitric acid oxidants / Dezso J. Ladanyi;
naca-rm-e51j01; 1952
- Kemp, Richard H.,
Moseson, Merland L.; Investigations
of air-cooled turbine rotors for turbojet engines II :mechanical design,
stress analysis, and burst test of modified J33 split-disk rotor / Richard H.
Kemp and Merland L. Moseson; naca-rm-e51j03; 1952
- Morgan, W. C., Morse,
C. R.; Experimental
investigation of the vibration characteristics of four designs of turbine
blades and of the effect produced by varying the axial spacing between nozzle
blades and turbine blades; naca-rm-e51j25; 1952
- Gray, V. H., Bowden, D.
T., von Glahn, U.; Preliminary
results of cyclical de-icing of a gas-heated airfoil; naca-rm-e51j29;
1952
- Lewis, James P.,
Bowden, Dean T.; Preliminary
investigation of cyclic de-icing of an airfoil using an external electric
heater; naca-rm-e51j30; 1952
- Desmon, Leland G.,
Mosher, Don R.; Dynamic
corrosion of a stainless-steel specimen by water at 500 F using a toroid
circulating apparatus /c Leland G. Desmon, Don R. Mosher; naca-rm-e52f03;
1952
- Deissler, Robert G.; Analysis of
fully developed turbulent heat transfer at low Peclet numbers in smooth tubes
with application to liquid metals; naca-rm-e52f05; 1952
- Himmel, Seymour C.; Some control
considerations for ram-jet engines / c Seymour Himmel; naca-rm-e52f10;
1952
- Graves, Charles C.; Effect of
oxygen concentration of the inlet oxygen-nitrogen mixture on the combustion
efficiency of a single J33 turbojet combustor; naca-rm-e52f13; 1952
- Harp, James L., Jr.,
Useller, James W., Auble, Carmon M.; Thrust
augmentation of a turbojet engine by the introduction of liquid ammonia into
the compressor inlet; naca-rm-e52f18; 1952
- Useller, James W.,
Auble, Carmon W., Harvey, Ray W., Sr.; Thrust
augmentation of a turbojet engine at simulated flight conditions by
introduction of a water-alcohol mixture into the compressor;
naca-rm-e52f20; 1952
- Topper, Leonard.; Radiant heat
transfer from flames in a single tubular turbojet combustor / Leonard
Topper; naca-rm-e52f23; 1952
- Greathouse, W. K.,
Hollister, D. P.; Preliminary
air-flow and thrust calibrations of several conical cooling-air ejectors with
a primary to secondary temperature ratio of 1.0. II :diameter ratios of 1.06
and 1.40; naca-rm-e52f26; 1952
- Metzler, Allen J.; Minimum
ignition of six pure hydrocarbon fuels of the C2 and C6 series;
naca-rm-e52f27; 1952
- Jackson, Robert J.; Effects on the
weight-flow range and efficiency of a typical axial-flow compressor inlet
stage that result from the use of a decreased blade camber or decreased
guide-vane turning; naca-rm-e52g02; 1952
- McCafferty, Richard J.,
Butze, Helmut F.; Temperature
response of turbine-blade metal covered with oxide coatings supplied by fuel
additives; naca-rm-e52g07; 1952
- Allen, J. L., Simon, P.
C.; Performance
characteristics at Mach numbers to 2.0 of various types of side inlets mounted
on fuselage of proposed supersonic airplane II :inlets utilizing half of a
conical spike; naca-rm-e52g08; 1952
- McDonald, Glen E.,
Schalla, Rose L.; Effect
of free methyl radicals on slow oxidation of propane and ethane;
naca-rm-e52g17; 1952
- Piercy, Thomas G.,
Johnson, Harry W.; Investigation
at Mach number 2.93 of half of a conical-spike diffuser mounted as a side
inlet with boundary-layer control; naca-rm-e52g23; 1952
- Renas, Paul E.,
Braithwaite, Willis M., Jansen, Emmert T.; Altitude
investigation of three flame-holder and fuel-systems configurations in a short
converging afterburner on a turbojet engine; naca-rm-e52g29; 1952
- Novik, David., Heppler,
Herbert., Dandois, Marcel.; Some
dynamic characteristics of a turbojet engine for large accelerations;
naca-rm-e52h04; 1952
- Hoffman, C. A., Cooper,
A. L.; Investigation
of titanium carbide base ceramals containing either nickel or cobalt for use
as gas-turbine blades; naca-rm-e52h05; 1952
- Hamrick, Joseph T.,
Mizisin, John.; Investigation
of flow fluctuations at the exit of a radial-flow centrifugal impeller;
naca-rm-e52h11; 1952
- Spakowski, Adolph E.;
Pressure
limits of flame propagation of pure hydrocarbon-air mixtures at reduced
pressure; naca-rm-e52h15; 1952
- Esenwein, Fred T.; Performance
characteristics at Mach numbers to 2.0 of various types of side inlets mounted
on fuselage of proposed supersonic airplane III : normal wedge inlet with
semicircular cowl; naca-rm-e52h20; 1952
- Hansen, A. G.,
Costello, G. R., Herzig, H. Z.; Effect
of geometry on secondary flows in blade rows; naca-rm-e52h26; 1952
- Mosher, Don R Desmon,
Leland G; Preliminary
investigation of corrosion by molten sodium hydroxide flowing in tubes of AISI
347 stainless steel, Inconel, and nickel having average outer-wall
temperatures of 1500 F and a circumferential temperature gradient of 20 F;
naca-rm-e51j16; March 1952
- Black, Dugald O.; Facilities and
methods used in full-scale airplane crash-fire investigation;
naca-rm-e51l06; 1952
- Schramm, Wilson B.,
Nachtigall, Alfred J.; Analysis
of coolant-flow requirements for an improved, internal-strut-supported,
air-cooled turbine-rotor blade; naca-rm-e51l13; 1952
- Dorsch, Robert G.,
Levine, Joseph.; A
photographic study of freezing of water droplets falling freely in air;
naca-rm-e51l17; 1952
- Simon, Dorothy M.,
Belles, Frank E.; An
active particle diffusion theory of flame quenching for laminar flames /
Dorothy M. Simon and Frank E. Belles; naca-rm-e51l18; 1952
- Peterson, Marshall B.,
Johnson, Robert L.; Friction
and surface damage of several corrosion-resistant materials;
naca-rm-e51l20; 1952
- Graham, David., Koenig,
David G.; Tests in the
Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect
ratio 2 triangular wing and an all-movable horizontal tail :lateral
characteristics; naca-rm-a51l03; 1952
- Sammonds, Robert I.,
Molk, Ashley J.; Effects
of propeller-spinner juncture on the pressure-recovery characteristics of an
NACA 1-series D-type cowl in combination with a four-blade single-rotation
propeller at Mach numbers up to 0.83 and at an angle of attack of 0
degrees; naca-rm-a52d01a; 1952
- Emerson, Horace F.,
Gale, Bernard M.; Transonic
aerodynamic characteristics of three thin triangular wings and a trapezoidal
wing, all of low aspect ratio; naca-rm-a52d21; 1952
- McFadden, Norman M.,
Holden, George R., Ratcliff, Jack W.; Instrumentation
and calibration technique for flight calibration of angle-of-attack systems on
aircraft; naca-rm-a52i23; 1952
- Martin, Andrew., Reed,
James F.; Correlation of
buffet boundaries predicted from wind-tunnel tests with those measured during
flight tests on the F8F-1 and X-1 airplanes -transonic-bump method;
naca-rm-a52j17; 1952
- Coe, Charles F.; The effects of
tip-mounted jet nacelles on the transonic characteristics of low-aspect-ratio
wings; naca-rm-a52j21; 1952
- Armstrong, John C.,
Wilsted, H. D.; Investigation
of several techniques for improving altitude starting limits of turbojet
engines; naca-rm-e52i03; 1952
- Berlad, A. L., Hibbard,
R. R.; Effect of
radiant energy on vaporization and combustion of liquid fuels;
naca-rm-e52i09; 1952
- Ferguson, Robert R.; Effect of
magnitude of vibratory load superimposed on mean tensile load on mechanism of
and time to fracture of specimens and correlation to engine blade;
naca-rm-e52i17; 1952
- Reynolds, Thaine W.,
Ingebo, Robert D.; Combustion
efficiency of homogeneous fuel-air mixtures in a 5-inch ram-jet-type
combustor; naca-rm-e52i23; 1952
- Butze, Helmut F.,
Jonash, Edmund R.; Turbojet
combustor efficiency with ceramic-coated liners and with mechanical control of
fuel wash on walls; naca-rm-e52i25; 1952
- Kemp, R. H., Morgan, W.
C.; Measurements of
thermal distortion of the submarine intermediate reactor "mark a" moderator
tube / R. H. Kemp and W. C. Morgan; naca-rm-e52j02; 1952
- Wear, Jerrold D.,
Dittrich, Ralph T.; Performance
of pure fuels in a single J33 combustor I :five liquid hydrocarbon fuels;
naca-rm-e52j03; 1952
- Perkins, Porter J.; Preliminary
survey of icing conditions measured during routine transcontinental airline
operation; naca-rm-e52j06; 1952
- Feiler, Charles E.,
Morrell, Gerald.; Investigation
of effects of additives on storage properties of fuming nitric acids;
naca-rm-e52j16; 1952
- Swett, Clyde C., Jr.,
Donlon, Richard H.; Spark
ignition of flowing gases III :effect of turbulence promoter on energy
required to ignite a propane-air mixture; naca-rm-e52j28; 1952
- Bemrose Boyd, Robert G.
Dorsch and George H. Brodie (Lewis Flight Propulsion Laboratory, Cleveland,
Ohio); True
Airspeed Measurement by Ionization-Tracer Technique; naca-rm-e52c31;
1952
- Simon Ostrach; An
analysis of laminar free-convection flow and heat transfer about a flat plate
paralled to the direction of the generating body force; naca-report-1111;
1953
- Vernon A. Slabey, Paul
H. Wise, Louis C. Gibbons; Hydrocarbon
and nonhydrocarbon derivatives of cyclopropane; naca-report-1112;
1953
- H. S. Ribner, M.
Tucker; Spectrum of
turbulence in a contracting stream; naca-report-1113; 1953
- Benjamin Pinkel, Irvin
M. Karp; A
thermodynamic study of the turbine-propeller engine; naca-report-1114;
1953
- John D. Stanitz; Design of
two-dimensional channels with prescribed velocity distributions along the
channel walls; naca-report-1115; 1953
- John D. Stanitz,
Leonard J. Sheldrake; Application
of a channel design method to high-solidity cascades and tests of an impulse
cascade with 90 degrees of turning; naca-report-1116; 1953
- Herbert F. Hardrath,
Lachlan Ohman; A
study of elastic and plastic stress concentration factors due to notches and
fillets in flat plates; naca-report-1117; 1953
- E. R. Eckert, John N.
B. Livingood; Method
for calculation of laminar heat transfer in air flow around cylinders of
arbitrary cross section (including large temperature differences and
transpiration cooling); naca-report-1118; 1953
- Max A. Heaslet, John R.
Spreiter; Reciprocity
relations in aerodynamics; naca-report-1119; 1953
- Dwight G. Moore, Mary
A. Mason, William N. Harrison; Relative
importance of various sources of defect-producing hydrogen introduced into
steel during application of vitreous coatings; naca-report-1120;
1953
- Satish Dhawan; Direct
measurements of skin friction; naca-report-1121; 1953
- Sheldon Paul Rideout,
Paul A. Beck; Survey
of portions of the chromium-cobalt-nickel-molybdenum quaternary system at
1,200 degrees c; naca-report-1122; 1953
- A. J. Eggers, Clarence
A. Syvertson, Samuel Kraus; A
study of inviscid flow about airfoils at high supersonic speeds;
naca-report-1123; 1953
- Franklin K. Moore; Displacement
effect of a three-dimensional boundary layer; naca-report-1124;
1953
- Harold Gold, Edward W.
Otto, Victor L. Ransom; Dynamics
of mechanical feedback-type hydraulic servomotors under inertia loads;
naca-report-1125; 1953
- Julian D. Maynard,
Seymour Steinberg; The
effect of blade-section thickness ratio on the aerodynamic characteristics of
related full-scale propellers at Mach numbers up to 0.65;
naca-report-1126; 1953
- Robert E. English,
Richard H. Cavicchi; One-dimensional
analysis of choked-flow turbines; naca-report-1127; 1953
- Herbert C. Nelson,
Julian H. Berman; Calculations
on the forces and moments for an oscillating wing-aileron combination in
two-dimensional potential flow at sonic speed; naca-report-1128;
1953
- Bernard Budiansky,
Edwin T. Kruszewski; Transverse
vibrations of hollow thin-walled cylindrical beams; naca-report-1129;
1953
- John D. Bird, Lewis R.
Fisher, Sadie M. Hubbard; Some
effects of frequency on the contribution of a vertical tail to the free
aerodynamic damping of a model oscillating in yaw; naca-report-1130;
1953
- Manuel Stein, Edward
Anderson, John Hedgepeth; Deflection
and stress analysis of thin solid wings of arbitrary plan form with particular
reference to delta wings; naca-report-1131; 1953
- Franklin K. Moore; Laminar
boundary layer on cone in supersonic flow at large angle of attack;
naca-report-1132; 1953
- I. Irving Pinkel, G.
Merritt Preson, Gerard J. Pesman; Mechanism
of start and development of aircraft crash fires; naca-report-1133;
1953
- Donald R. Bellman, Jack
C. Humphrey, Theodore Male; Photographic
investigation of combustion in a two-dimensional transparent rocket
engine; naca-report-1134; 1953
- Ames Research Staff; Equations,
tables, and charts for compressible flow; naca-report-1135; 1953
- Ralph W. Stone, Jr.; Estimation of
the maximum angle of sideslip for determination of vertical-tail loads in
rolling maneuvers; naca-report-1136; 1953
- Almer D. Crim, John P.
Reeder, James B. Whitten; Initial
results of instrument-flying trials conducted in a single-rotor
helicopter; naca-report-1137; 1953
- Henry A. Pearson; Study of
inadvertent speed increases in transport operation; naca-report-1138;
1953
- Kenneth A. Foss,
Franklin W. Diederich; Charts
and approximate formulas for the estimation of aeroelastic effects of the
lateral control of swept and unswept wings; naca-report-1139; 1953
- Franklin W. Diederich,
Kenneth A. Foss; Charts
and approximate formulas for the estimation of aeroelastic effects on the
loading of swept and unswept wings; naca-report-1140; 1953
- George B. Brajnikoff;
Method and
graphs for the evaluation of air-induction systems; naca-report-1141;
1953
- Mahinder S. Uberoi,
Stanley Corrsin; Diffusion
of heat from a line source in isotropic turbulence; naca-report-1142;
1953
- John C. Martin; A vector study
of linearized supersonic flow applications to nonplanar problems;
naca-report-1143; 1953
- John M. Riebe, Rodger
L. Naeseth; Aerodynamic
characteristics of a refined deep-step planing-tail flying-boat hull with
various forebody and afterbody shapes; naca-report-1144; 1953
- John A. Zalovick,
Lindsay J. Lina, James P. Trant, Jr.; A
method of calibrating airspeed installations on airplanes at transonic and
supersonic speeds by the use of accelerometer and attitude-angle
measurements; naca-report-1145; 1953
- Jones F. Cahill,
William J. Underwood, Robert J. Nuber, Gail A. Cheesman; Aerodynamic
forces and loadings on symmetrical circular-arc airfoils with plain
leading-edge and plain trailing-edge flaps; naca-report-1146; 1953
- Frank M. Hamaker,
Stanford E. Neice, Thomas J. Wong; The
similarity law for hypersonic flow and requirements for dynamic similarity of
related bodies in free flight; naca-report-1147; 1953
- M. M. Frocht, R.
Guernsey, Jr.; A
special investigation to develop a general method for three-dimensional
photoelastic stress analysis; naca-report-1148; 1953
- Carl Kaplan; On
transonic flow past a wave-shaped wall; naca-report-1149; 1953
- Harry L. Runyan,
Charles E. Watkins; Considerations
on the effect of wind-tunnel walls on oscillating air forces for
two-dimensional subsonic compressible flow; naca-report-1150; 1953
- Robert O. Schade, James
L. Hassell, Jr.; The
effects on dynamic lateral stability and control of large artificial
variations in the rotary stability derivatives; naca-report-1151;
1953
- Emanuel Schnitzer; Theory and
procedure for determining loads and motions in chine-immersed hydrodynamic
impacts of prismatic bodies; naca-report-1152; 1953
- John R. Spreiter; On the
application of transonic similarity rules to wings of finite span;
naca-report-1153; 1953
- Benjamin Milwitzky,
Francis E. Cook; Analysis
of landing-gear behavior; naca-report-1154; 1953
- Clarence W. Matthews;
A comparison
of the experimental subsonic pressure distributions about several bodies of
revolution with pressure distributions computed by means of the linearized
theory; naca-report-1155; 1953
- Fred S. Elwell; Experiments to
determine neighborhood reactions to light airplanes with and without external
noise reduction; naca-report-1156; 1953
- Geoge B. Dubois, Fred
W. Ocvirk; Analytical
derivation and experimental evaluation of short-bearing approximation for full
journal bearing; naca-report-1157; 1953
- B. J. Saelman, H. W.
Vick; Weight
bar charts; naca-rm-53b19; Jun 1953
- Edmund E. Callaghan,
John S. Serafini; Analytical
investigation of icing limit for diamond-shaped airfoil in transonic and
supersonic flow; naca-tn-2861; Jan 1953
- Thomas F. Gelder, James
P. Lewis, Stanley L. Koutz; Icing
protection for a turbojet transport airplane : heating requirements methods of
protection, and performance penalties; naca-tn-2866; Jan 1953
- Y. S. Tang, J. M.
Duncan, H. E. Schweyer; Heat
and momentum transfer between a spherical particle and air streams;
naca-tn-2867; Mar 1953
- Alfred Ritter,
Yung-Huai Kuo; Reflection
of a weak shock wave from a boundary layer along a flat plate I : interaction
of weak shock waves with laminar and turbulent boundary layers analyzed by
momentum-integral method; naca-tn-2868; Jan 1953
- Yung-Huai Kuo; Reflection
of weak shock wave from a boundary layer along a flat plate II : interaction
of oblique shock wave with a laminar boundary layer analyzed by
differential-equation method; naca-tn-2869; Jan 1953
- S. E. Slaymaker, Robin
B. Gray; Power-off
flare-up tests of a model helicopter rotor in vertical autorotation;
naca-tn-2870; Jan 1953
- Thomas W. Wilder, III,
William A. Brooks, Jr., Eldon E. Mathauser; The
effect of initial curvature on the strength of an inelastic column;
naca-tn-2872; Jan 1953
- Paul Seide; The
effect of longitudinal stiffeners located on one side of a plate on the
compressive buckling stress of the plate-stiffener combination;
naca-tn-2873; Jan 1953
- J. Mayers, Robert W.
Fralich, Eric Reissner; Behavior
in pure bending of a long monocoque beam of circular-arc cross section;
naca-tn-2875; Jan 1953
- Derrill B. Chambliss,
George M. Boyd, Jr.; The
planing characteristics of two V-shaped prismatic surfaces having angles of
dead rise of 20 degrees and 40 degrees; naca-tn-2876; Jan 1953
- Melvin Sadoff; On
the use of a damped sine-wave elevator motion for computing the design
maneuvering horizontal-tail load; naca-tn-2877; Jan 1953
- Maurice Tucker; Combined effect
of damping screens and streams convergence on turbulence; naca-tn-2878;
Jan 1953
- Bert A. Coss, D. R.
Daykin, Leonard Jaffe, Elmer M. Sharp; A
digital automatic multiple pressure recorder; naca-tn-2880; Jan
1953
- William Solomon; Aerodynamic
characteristics of a two-blade NACA 10-(3)(062)-045 propeller and of a
two-blade NACA 10-(3)(08)-045 propeller; naca-tn-2881; Jan 1953
- Albert J. Evans; The zero-lift
drag of a slender body of revolution (NACA RM-10 research model) as determined
from tests in several wind tunnels and in flight at supersonic speeds;
naca-tn-2944; Apr 1953
- R. D. Johnson, F. R.
Shober, A. D. Schwope; The
creep of single crystals of aluminum; naca-tn-2945; May 1953
- M. John Pilny; A
small Pirani gage for measurements of nonsteady low pressures;
naca-tn-2946; Jun 1953
- Walter F. Lindsey,
Joseph Burlock; A
variable-frequency light synchronized with a high-speed motion-picture camera
to provide very short exposure times; naca-tn-2949; May 1953
- Eugene S. Love, Carl E.
Grigsby; A
new shadowgraph technique for the observation of conical flow phenomena in
supersonic flow and preliminary results obtained for a triangular wing;
naca-tn-2950; May 1953
- Harold N. Murrow,
Chester B. Payne; Flight
investigation of the effect of transient wing response on wing strains of a
four-engine bomber airplane in rough air; naca-tn-2951; Jun 1953
- Rinaldo J. Brun, Helen
M. Gallagher, Dorothea E. Vogt; Impingement
of water droplets on NACA 65(1)-208 and 65(1)-212 airfoils at 4 degrees angle
of attack; naca-tn-2952; May 1953
- John R. Meyer, Gaetano
Falabella, Jr.; An
investigation of the experimental aerodynamic loading on a model helicopter
rotor blade; naca-tn-2953; May 1953
- Percy J. Bobbitt, Frank
S. Malvestuto, Jr.; Estimation
of forces and moments due to rolling for several slender-tail configurations
at supersonic speeds; naca-tn-2955; Jul 1953
- Charles Libove; Creep-buckling
analysis of rectangular-section columns; naca-tn-2956; Jun 1953
- Vernon L. Rogallo, John
L. McCloud, III; Surveys
of the flow fields at the propeller planes of six 40 degree sweptback
wing-fuselage-nacelle combinations; naca-tn-2957; Jun 1953
- Charles E. Frank, Angus
U. Blackham; Reaction
processes leading to spontaneous ignition of hydrocarbons; naca-tn-2958;
Jun 1053
- Doris Cohen, Morris D.
Friedman; Theoretical
investigation of the supersonic lift and drag of thin, sweptback wings with
increased sweep near the root; naca-tn-2959; Jun 1953
- Forrest E. Gowen,
Edward W. Perkins; Drag
of circular cylinders for a wide range of Reynolds numbers and Mach
numbers; naca-tn-2960; Jun 1953
- Chung-Hua Wu; Subsonic
flow of air through a single-stage and a seven-stage compressor;
naca-tn-2961; Jun 1953
- Vernon H. Gray, Uwe H.
Von Glahn; Effect of ice
and frost formations on drag of NACA 65(1)-212 airfoil for various modes of
thermal ice protection; naca-tn-2962; Jun 1953
- Norris F. Dow, William
A. Hickman, B. Walter Rosen; Effect
of variation in rivet strength on the average stress at maximum load for
aluminum-alloy, flat, Z-stiffened compression panels that fail by local
buckling; naca-tn-2963; Jun 1953
- Thomas L. Coleman, Paul
W. J. Schumacher; An
analysis of normal-acceleration and airspeed data from a four-engine type of
transport; naca-tn-2965; Aug 1953
- Jean Gilman, Jr.; Propeller-performance
charts for transport airplanes; naca-tn-2966; Jul 1953
- Albert E. Von Doenhoff,
George W. Jones, Jr.; An
analysis of the power-off landing maneuver in terms of the capabilities of the
pilot and the aerodynamic characteristics of the airplane; naca-tn-2967;
Aug 1953
- Dwight G. Moore, Mary
A. Mason; Investigation
of gases evolved during firing of vitreous coatings on steel;
naca-tn-2865; Jan 1953
- Leslie S. G. Kovasznay;
Development
of turbulence-measuring equipment; naca-tn-2839; Jan 1953
- Robert D. Ingebo; Study of
pressure effects on vaporization rate of drops in gas streams;
naca-tn-2850; Jan 1953
- Harry Press, Bernard
Mazelsky; A
study of the application of power-spectral methods of generalized harmonic
analysis to gust loads on airplanes; naca-tn-2853; Jan 1953
- Morton Cooper, John R.
Sevier, Jr.; Estimated power
reduction by water injection in a nonreturn supersonic wind tunnel;
naca-tn-2856; Jan 1953
- Abramovitz, Marvin; Theoretical
investigation of the performance of proportional navigation guidance systems :
effect of missile configuration on the speed of response; naca-rm-a52j22;
January 19, 1953
- Conrad, E William
Essig, Robert H Finger, Harold B; Effect
of rotor- and stator-blade modifications on surge performance of an 11-stage
axial-flow compressor II : redesigned compressor for XJ-40-WE-6 engine;
naca-rm-e52i10; May 25, 1953
- John J. Rebeske, Jr.,
James F. Dugan, Jr.; Matched
performance characteristics of a 16-stage axial-flow compressor and a 3-stage
turbine; naca-rm-e52h18; Apr 1953
- Joseph T. Hamrick,
Walter M. Osborn, William L. Beede; Design
and test of mixed-flow impellers III : design and experimental results for
impeller model MFI-2A and comparison with impeller model MFI-1A;
naca-rm-e52l22a; Mar 1953
- Neice, Stanford E Wong,
Thomas J; An
experimental investigation of the applicability of the hypersonic similarity
law to bodies of revolution; naca-rm-a52k07; January 27, 1953
- Mead, Merrill H; Experimental
investigation of the aerodynamic characteristics of an air-to-air missile
employing cruciform wings and tail of rectangular plan form at Mach numbers of
1.4 and 1.9; naca-rm-a52k14; February 16, 1953
- Boyd, John W Pfyl,
Frank A; Experimental
investigation of aerodynamically balanced trailing-edge control surfaces on an
aspect ratio 2 triangular wing at subsonic and supersonic speeds;
naca-rm-a52l04; February 13, 1953
- Tobak, Murray; Damping
in pitch of low-aspect-ratio wings at subsonic and supersonic speeds;
naca-rm-a52l04a; April 08, 1953
- Koenig, David G; Tests in the
Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect
ratio 3 triangular wing and an all-movable horizontal tail : longitudinal and
lateral characteristics; naca-rm-a52l15; April 13, 1953
- Heitmeyer, John C; Effect of
vertical position of the wing on the aerodynamic characteristics of three
wing-body combinations; naca-rm-a52l15a; February 18, 1953
- Swift, John T Scherrer,
Richard Stroud, John F; Preliminary
investigation of a variable-area auxiliary air-intake system at Mach numbers
from 0 to 1.3; naca-rm-a53a13; February 25, 1953
- Hall, Charles F; Lift, drag, and
pitching moment of low-aspect-ratio wings at subsonic and supersonic
speeds; naca-rm-a53a30; April 14, 1953
- Syvertson, Clarence A
Gloria, Hermilo R; An
experimental investigation of the zero-lift-drag characteristics of
symmetrical blunt-trailing-edge airfoils at Mach numbers from 2.7 to 5.0;
naca-rm-a53b02; April 29, 1953
- Holdaway, George H; Comparison of
the aerodynamic characteristics at transonic speeds of a plane wing and a
cambered and twisted wing, both having 45 degrees of sweepback and an aspect
ratio of 6; naca-rm-a53b16; May 05, 1953
- Allen, Edwin C; Experimental
investigation of the effects of plan-form taper on the aerodynamic
characteristics of symmetrical unswept wings of varying aspect ratio;
naca-rm-a53c19; May 29, 1953
- Smith, Donald W Reed,
Verlin D; Subsonic static
longitudinal stability and control characteristics of a wing-body combination
having a pointed wing of aspect ratio 2 with constant-percent-chord
trailing-edge elevons; naca-rm-a53c20; May 22, 1953
- James, Carlton S
Carros, Robert J; Experimental
investigation of the zero-lift drag of a fin-stabilized body of fineness ratio
10 at Mach numbers between 0.6 and 10; naca-rm-a53d02; June 11,
1953
- Spahr, J Richard
Dickey, Robert R; Wind-tunnel
investigation of the vortex wake and downwash field behind triangular wings
and wing-body combinations at supersonic speeds; naca-rm-a53d10; June 25,
1953
- Reese, David E , Jr; An experimental
investigation at subsonic and supersonic speeds of the torsional damping
characteristics of a constant-chord control surface of an aspect ratio 2
triangular wing; naca-rm-a53d27; July 02, 1953
- Frazer, Alson C
Anderson, Warren E; Performance
of a normal-shock scoop inlet with boundary-layer control; naca-rm-a53d29;
June 29, 1953
- Brajnikoff, George B
Stroud, John F; Experimental
investigation of the effect of entrance width-to-height ratio on the
performance of an auxiliary scoop-type inlet at Mach numbers from 0 to
1.3; naca-rm-a53e28; July 30, 1953
- Jorgensen, Leland H; Correlation by
the hypersonic similarity rule of the pressure distributions and wave drags
for minimum-drag nose shapes at zero angle of attack; naca-rm-a53f12;
August 31, 1953
- Holdaway, George H; Comparison of
theoretical and experimental zero-lift drag-rise characteristics of
wing-body-tail combinations near the speed of sound; naca-rm-a53h17;
October 16, 1953
- Edwards, Sherman
Hikido, Katsumi; A
method for estimating the rolling moments caused by wing-tail interference for
missiles at supersonic speeds; naca-rm-a53h18; November 12, 1953
- Gowen, Forrest E
Perkins, Edward W; A
study of the effects of body shape on the vortex wakes of inclined bodies at a
Mach number of 2; naca-rm-a53i17; December 1953
- Lazzeroni, Frank A; Investigation
of a missile airframe with control surfaces consisting of projecting quadrants
of the nose cone; naca-rm-a53l21; March 15, 1953
- Dangle, E E Cervenka, A
J Bahr, D W; Effects of fuel
temperature and fuel distribution on the combustion efficiency of a 16-inch
ram-jet engine at a simulated Mach number of 2.9; naca-rm-e52j14; January
08, 1953
- Allen, J L Beke,
Andrew; Force and
pressure recovery characteristics at supersonic speeds of a conical spike
inlet with bypasses discharging in an axial direction; naca-rm-e52k14;
January 30, 1953
- Hearth, Donald P
Gorton, Gerald C; Investigation
at supersonic speeds of an inlet employing conical flow separation from a
probe ahead of a blunt body; naca-rm-e52k18; January 19, 1953
- Disher, John H Kohl,
Robert C Jones, Merle L; Free-flight
performance of a rocket-boosted, air-launched 16-inch-diameter ram-jet engine
at Mach numbers up to 2.20; naca-rm-e52l02; February 03, 1953
- Medeiros, Arthur A
Benser, William A Hatch, James E; Analysis
of off-design performance of a 16-stage axial-flow compressor with various
blade modifications; naca-rm-e52l03; March 05, 1953
- Breitwieser, Roland
Gordon, Sanford Gammon, Benson; Summary
report on analytical evaluation of air and fuel specific-impulse
characteristics of several nonhydrocarbon jet-engine fuels;
naca-rm-e52l08; February 19, 1953
- Beke, Andrew Allen, J
L; Force and
pressure-recovery characteristics at supersonic speeds of a conical nose inlet
with bypasses discharging outward from the body axis; naca-rm-e52l18a;
March 05, 1953
- Reshotko, Eli; Preliminary
investigation of a perforated axially symmetric nozzle for varying nozzle
pressure ratios; naca-rm-e52j27; January 14, 1953
- Schramm, Wilson B
Nachtigall, Alfred J Arne, Vernon L; Analytical
comparison of turbine-blade cooling systems designed for a turbojet engine
operating at supersonic speed and high altitude I : liquid-cooling
systems; naca-rm-e52j29; February 20, 1953
- Schramm, Wilson B Arne,
Vernon L Nachtigall, Alfred J; Analytical
comparison of turbine-blade cooling systems designed for a turbojet engine
operating at supersonic speed and high altitude II : air-cooling systems;
naca-rm-e52j30; February 19, 1953
- Goldstein, Arthur W
Schacht, Ralph L; Performance
of a swept leading edge rotor of the supersonic type with mixed flow;
naca-rm-e52k03; January 30, 1953
- Wallner, Lewis E
Conrad, E William Prince, William R; Effect
of uneven air-flow distribution to the twin inlets of an axial-flow turbojet
engine; naca-rm-e52k06; January 26, 1953
- Trout, Arthur M
Wentworth, Carl B; Free-jet
altitude investigation of a 20-inch ram-jet combustor with a rich inner zone
of combustion for improved low-temperature-ratio operation;
naca-rm-e52l26; May 25, 1953
- Wise, George A; Influence of
end plates on lift and flow field of a canard-type control surface at a Mach
number of 2.00; naca-rm-e53a02; March 23, 1953
- Rebeske, John J , Jr
Rohlik, Harold E; Acceleration
of high-pressure-ratio single-spool turbojet engine as determined from
component performance characteristics I : effect of air bleed at compressor
outlet; naca-rm-e53a09; March 10, 1953
- Bernstein, Harry
Haefeli, Rudolph C; Investigation
of pressure recovery of a single-conical-shock nose inlet at Mach number
5.4; naca-rm-e53a12; April 06, 1953
- Schafer, Louis J
Stepka, Francis S Brown, W Byron; Comparison
of theoretically and experimentally determined effects of oxide coatings
supplied by fuel additives on uncooled turbine-blade temperature during
transient turbojet-engine operation; naca-rm-e53a19; March 30, 1953
- Lewis, James P; An analytical
study of heat requirements for icing protection of radomes;
naca-rm-e53a22; March 11, 1953
- Freche, John C
Stelpflug, William J; Investigation
of water-spray cooling of turbine blades in a turbojet engine;
naca-rm-e53a23; March 10, 1953
- Allen, J L Beke,
Andrew; Force and
pressure recovery characteristics at supersonic speeds of a conical spike
inlet with a bypass discharging from the top or bottom of the diffuser in an
axial direction; naca-rm-e53a29; March 23, 1953
- Jack, John R; Aerodynamics
of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp
6) to 15 x 10(exp 6) III : boundary layer and force measurements on a slender
cone-cylinder body of revolution; naca-rm-e53b03; April 06, 1953
- Dangle, E E Cervenka, A
J Bahr, D W; Effect of
fuel-air ratio concentration in combustion zone on combustion performance of a
16-inch ram-jet engine; naca-rm-e53b19; April 13, 1953
- Kochendorfer, Fred D;
Investigation
at a Mach number of 1.90 of a diverter-type boundary-layer removal system for
a scoop inlet; naca-rm-e53d07; June 08, 1953
- Krull, H George
Steffen, Fred W Ciepluch, Carl C; Internal
performance characteristics of variable-throat plug- and vaned-type
convergent-divergent nozzles; naca-rm-e53d09; June 23, 1953
- Jacklitch, John J , Jr
Hartmann, Melvin J; Investigation
of 16-inch impulse-type supersonic compressor rotor with turning past axial
direction; naca-rm-e53d13; July 06, 1953
- Robbins, William H
Glaser, Frederick W; Investigation
of an axial-flow-compressor rotor with circular-arc blades operating up to a
rotor-inlet relative Mach number of 1.22; naca-rm-e53d24; July 03,
1953
- Cook, Preston N , Jr
Evans, Vernida E Lezberg, Erwin A; Experimental
investigation of physical and combustion properties of several residual fuel
oils and magnesium - fuel-oil slurries in a ram-jet-type combustor;
naca-rm-e53d30; June 23, 1953
- Rothenberg, Edward A
Douglass, Howard W; Investigation
of liquid fluorine : liquid ammonia propellant combination in a
100-pound-thrust rocket engine; naca-rm-e53e08; July 03, 1953
- Bartoo, Edward R Clure,
John L; Experimental
investigation of air-cooled turbine blades in turbojet engine XIII : endurance
evaluation of several protective coatings applied to turbine blades of
nonstrategic steels; naca-rm-e53e18; July 16, 1953
- Beheim, Milton A; A preliminary
investigation at Mach number 1.91 of an inlet configuration designed for
insensitivity to positive angle-of-attack operation; naca-rm-e53e20; July
10, 1953
- Nettles, J C; The
effect of initial rate of subsonic diffusion on the stable subcritical
mass-flow range of a conical shock diffuser; naca-rm-e53e26; July 22,
1953
- Branstetter, J Robert
Gibbs, James B Kaufman, Warner B; Magnesium-slurry
combustion performance in 6.5-inch-diameter ram-jet engine mounted in
connected-pipe facility; naca-rm-e53e27; August 05, 1953
- Baughman, L Eugene
Jack, John R; Experimental
investigation of the effects of support interference on the pressure
distribution of a body of revolution at a Mach number of 3.12 and Reynolds
numbers from 2 x 10(exp 6) to 14 x 10(exp 6); naca-rm-e53e28; August 05,
1953
- Von Glahn, U; Preliminary
results of heat transfer from a stationary and rotating ellipsoidal
spinner; naca-rm-e53f02; August 06, 1953
- Walker, Curtis L
Braithwaite, Willis M Sivo, Joseph N; Altitude
evaluation of several afterburner design variables on a J47-GE-17 turbojet
engine; naca-rm-e53f10; October 23, 1953
- Fradenburgh, Evan A
Kremzier, Emil J; Performance
comparison of three canard-type ram-jet missile configurations at Mach numbers
from 1.5 to 2.0; naca-rm-e53f11; August 14, 1953
- Cervenka, A J
Perchonok, Eugene Dangle, E E; Effect
of fuel injector location and mixture control on performance of a 16-inch
ram-jet can-type combustor; naca-rm-e53f15; July 29, 1953
- Meyer, A J , Jr
Deutsch, G C Morgan, W C; Preliminary
investigation of several root designs for cermet turbine blades in turbojet
engine II : root design alterations; naca-rm-e53g02; October 13,
1953
- Valerino, Alfred S
Pennington, Donald B Vargo, Donald J; Effect
of circumferential location on angle of attack performance of twin
half-conical scoop-type inlets mounted symmetrically on the RM-10 body of
revolution; naca-rm-e53g09; September 09, 1953
- Gorton, Gerald C; Investigation
of translating-spike supersonic inlet as means of mass-flow control at Mach
numbers of 1.5, 1.8, and 2.0; naca-rm-e53g10; October 29, 1953
- Tower, Leonard K
Gammon, Benson E; Analytical
evaluation of effect of equivalence ratio inlet-air temperature and combustion
pressure on performance of several possible ram-jet fuels; naca-rm-e53g14;
1953
- Esgar, Jack B Richards,
Hadley T; Evaluation of
effects of random permeability variations on transpiration-cooled
surfaces; naca-rm-e53g16; November 30, 1953
- Freche, John C
Mckinnon, Roy A; Experimental
investigation of several water-injection configurations for turbine-blade
spray cooling in a turbojet engine; naca-rm-e53h06; October 08,
1953
- Henzel, James G , Jr
Wentworth, Carl B; Free-jet
investigation of a 20-inch ram-jet combustor utilizing high-heat-release pilot
burner; naca-rm-e53h14; October 16, 1953
- Cortright, Edgar M , Jr
Kochendorfer, Fred D; Jet
effects on flow over afterbodies in supersonic stream; naca-rm-e53h25;
November 16, 1953
- Cervenka, A J Dangle, E
E Friedman, Robert; Effect
of inlet-air temperature on performance of a 16-inch ram-jet combustor;
naca-rm-e53i03; October 29, 1953
- Serovy, George K
Robbins, William H Glaser, Frederick W; Experimental
investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet
stage at transonic inlet relative Mach numbers I : rotor design and over-all
performance at tip speeds from 60 to 100 percent of design;
naca-rm-e53i11; December 07, 1953
- Benser, William A; Analysis of
part-speed operation for high-pressure-ratio multistage axial-flow
compressors; naca-rm-e53i15; December 04, 1953
- Haefeli, Rudolph C
Bernstein, Harry; Performance
of separation nose inlets at Mach number 5.5; naca-rm-e53i23; December
1953
- Voit, Charles H; Investigation
of a high-pressure-ratio eight-stage axial-flow research compressor with two
transonic inlet stages I : aerodynamic design; naca-rm-e53i24; December
04, 1953
- Beheim, Milton A; A preliminary
investigation at Mach number 1.91 of a diffuser employing a pivoted cone to
improve operation at angle of attack; naca-rm-e53i30; December 08,
1953
- Geye, Richard P Voit,
Charles H Budinger, Ray E; Investigation
of a high-pressure-ratio eight-stage axial-flow research compressor with two
transonic inlet stages II : preliminary analysis of over-all performance;
naca-rm-e53j06; December 1953
- Morrow, John D Nelson,
Robert L; Large-scale
flight measurements of zero-lift drag of 10 wing-body configurations at Mach
numbers from 0.8 to 1.6; naca-rm-l52d18a; January 15, 1953
- Mason, Homer P; Low-lift buffet
characteristics obtained from flight tests of unswept thin intersecting
surfaces and of thick 35 degree sweptback surfaces; naca-rm-l52h12;
January 16, 1953
- Pendley, Robert E
Bryan, Carroll R; An
investigation of some factors affecting the drag of relatively large
nonlifting bodies of revolution in a slotted transonic wind tunnel;
naca-rm-l52h22; January 15, 1953
- Pendley, Robert E
Milillo, Joseph R Fleming, Frank F; An
investigation of three NACA 1-series nose inlets at subsonic and transonic
speeds; naca-rm-l52j23; January 07, 1953
- Brown, Clarence A , Jr
Bressette, Walter E; Flight
investigation of the zero-lift of two ram-jet missile configurations at Mach
numbers from 1.00 to 1.89; naca-rm-l52j24a; March 09, 1953
- Peck, Robert F
Mitchell, Jesse L; Rocket-model
investigation of longitudinal stability and drag characteristics of an
airplane configuration having a 60 degree delta wing and a high unswept
horizontal tail; naca-rm-l52k04a; January 05, 1953
- Bland, William M , Jr
Marley, Edward T; A
free-flight investigation at zero lift in the Mach number range between 0.7
and 1.4 to determine the effectiveness of an inset tab as a means of
aerodynamically relieving aileron hinge moments; naca-rm-l52k07; January
15, 1953
- Hinners, Arthur H , Jr
Lee, John B; Preliminary
investigation of the total-pressure-recovery characteristics of a 15 degree
semiangle movable-cone variable-geometry ram-jet inlet at free-jet Mach
numbers of 1.62, 2.00, 2.53, and 3.05; naca-rm-l52k10; January 08,
1953
- Bursnall, William J; Initial flutter
tests in the Langley transonic blowdown tunnel and comparison with free-flight
flutter results; naca-rm-l52k14; January 07, 1953
- Moul, Martin T; Flight
investigation of a supersonic canard missile equipped with an auxiliary
damping-in-pitch control system; naca-rm-l52k14b; February 02, 1953
- Gillis, Clarence L
Chapman, Rowe, Jr; Summary
of pitch-damping derivatives of complete airplane and missile configurations
as measured in flight at transonic and supersonic speeds; naca-rm-l52k20;
January 22, 1953
- Czarnecki, K R Lord,
Douglas R; Hinge-moment
characteristics for several tip controls on a 60 degree sweptback delta wing
at Mach number 1.61; naca-rm-l52k28; January 22, 1953
- Loposer, J Dan; Average
skin-friction coefficients from boundary layer measurements on an
ogive-cylinder body in flight at supersonic speeds; naca-rm-l52k28a;
January 16, 1953
- Knapp, Ronald J
Johnson, Wallace E; Flight
measurements of pressures on base and rear part of fuselage of the Bell X-1
research airplane at transonic speeds, including power effects;
naca-rm-l52l01; January 28, 1953
- Hatch, John E , Jr
Savelle, William M; Some
effects of a sonic jet exhaust on the loading over a yawed fin at a Mach
number of 3.03; naca-rm-l52l02a; January 27, 1953
- Mcfall, John C , Jr
Hollinger, James A; Longitudinal
stability, control effectiveness, and drag characteristics at transonic speeds
of a rocket-propelled model of an airplane configuration having an unswept
tapered wing of aspect ratio 3.0 and NACA 65A004.5 airfoil sections;
naca-rm-l52l04; January 20, 1953
- Robinson, Harold L; A transonic
wind-tunnel investigation of the effects of body indentation, as specified by
the transonic drag-rise rule, on the aerodynamic characteristics and flow
phenomena of a 45 degree sweptback-wing-body combination; naca-rm-l52l12;
February 09, 1953
- Estabrooks, Bruce B; A transonic
wind-tunnel investigation of an unswept-wing-body combination at angles of
attack up to 24 degrees; naca-rm-l52l19; February 06, 1953
- Kelly, Thomas C; Transonic
wind-tunnel investigation of the aerodynamic characteristics of a 60 degrees
triangular wing in combination with a systematic series of three bodies;
naca-rm-l52l22a; April 06, 1953
- Williams, Claude V; A transonic
wind-tunnel investigation of the effects of body indentation, as specified by
the transonic drag-rise rule, on the aerodynamic characteristics and flow
phenomena of an unswept-wing-body combination; naca-rm-l52l23; January 28,
1953
- Katzoff, S Smith,
Samuel L , III; A
theoretical analysis of the distortion of fuel-spray-particle paths in a
helicopter ram-jet engine due to centrifugal effects; naca-rm-l53a02;
April 07, 1953
- Arbic, Richard G White,
George Gillespie, Warren, Jr; Some
approximate methods for estimating the effects of aeroelastic bending of
rocket-propelled model-booster combinations; naca-rm-l53a08; March 27,
1953
- Mcdearmon, Russell W
Heinke, Harry S , Jr; Investigations
of the damping in roll of swept and tapered wings at supersonic speeds;
naca-rm-l53a13; March 03, 1953
- Sevier, John R , Jr
Hamilton, Clyde V Driver, Cornelius; Wind-tunnel
investigation of a ram-jet missile model having a wing and canard surfaces of
delta plan form with 70 degrees swept leading edges : force and moment
characteristics of various combinations of components at a Mach number of
1.6; naca-rm-l53a14; March 09, 1953
- Osborne, Robert S
Kelly, Thomas C; A
note on the drag due to lift of delta wings at Mach numbers up to 2.0;
naca-rm-l53a16a; April 09, 1953
- Harrison, Daniel E; The influence
of a change in body shape on the effects of twist and camber as determined by
a transonic wind-tunnel investigation of a 45 degree sweptback wing-fuselage
configuration; naca-rm-l53b03; August 14, 1953
- Kindell, William H; Effects of span
and spanwise and chordwise location on the control effectiveness of spoilers
on a 50 degree sweptback wing at Mach numbers of 1.41 and 1.96;
naca-rm-l53b09; April 08, 1953
- Johnson, Harold S
Hayes, William C; Wind-tunnel
investigation of the effects of various dorsal-fin and vertical-tail
configurations on the directional stability of a streamlined body at transonic
speeds : transonic-bump method; naca-rm-l53b19; April 08, 1953
- Czarnecki, K R
Sinclair, Archibald R; An
extension of the investigation of the effects of heat transfer on
boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a
Mach number of 1.61; naca-rm-l53b25; March 26, 1953
- Wallskog, Harvey A
Morrow, John D; Large-scale
flight measurements of zero-lift drag and low-lift longitudinal
characteristics of a diamond-wing-body combination at Mach numbers from 0.725
to 1.54; naca-rm-l53c17; April 20, 1953
- Kurbjun, Max C
Thompson, Jim Rogers; Free-fall
measurements of the effects of wing-body interference on the transonic drag
characteristics of swept-wing-slender-body configurations; naca-rm-l53c31;
May 28, 1953
- Carpenter, Paul J
Radin, Edward J; Investigation
of a ram-jet-powered helicopter rotor on the Langley helicopter test
tower; naca-rm-l53d02; June 03, 1953
- Dunning, Robert W
Ulmann, Edward F; Aerodynamic
characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33
having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span
trailing-edge flap; naca-rm-l53d03; May 29, 1953
- Goin, Kennith L
Westrick, Gertrude C; Effects
of trailing-edge bluntness on the lift, drag, and pitching-moment
characteristics of unswept, 45 degree swept, and 45 degree delta wings at Mach
numbers of 1.41, 1.62, and 1.96; naca-rm-l53d13; June 10, 1953
- Czarnecki, K R Lord,
Douglas R; Preliminary
investigation of the effect of fences and balancing tabs on the hinge-moment
characteristics of a tip control on a 60 degree delta wing at Mach number
1.61; naca-rm-l53d14; May 29, 1953
- Wallskog, Harvey A
Hart, Roger G; Investigation
of the drag of blunt-nosed bodies of revolution in free flight at Mach numbers
from 0.6 to 2.3; naca-rm-l53d14a; June 11, 1953
- Czarnecki, K R Lord,
Douglas R; Load
distributions associated with controls at supersonic speeds;
naca-rm-l53d15a; May 29, 1953
- Vogler, Raymond D; Wind-tunnel
investigation at high subsonic speeds of a spoiler-slot deflector combination
on an NACA 65A006 wing with quarter-chord line swept back 32.6 degrees;
naca-rm-l53d17; May 29, 1953
- Johnson, Harold I; Measurements of
aerodynamic characteristics at transonic speeds of an unswept and untapered
NACA 65-009 airfoil model of aspect ratio 3 with 1/4-chord plain flap by the
NACA wing-flow method; naca-rm-l53d21; June 10, 1953
- Rainey, Robert W; Effect of
variations in Reynolds number on the aerodynamic characteristics of three bomb
or store shapes at a Mach number of 1.62 with and without fins;
naca-rm-l53d27; June 25, 1953
- Carter, Howard S
Merlet, Charles F; Flight
determination of the pressure recovery and drag characteristics of a twin
side-inlet model at transonic speeds; naca-rm-l53e05; July 30, 1953
- Cooper, Morton Sevier,
John R , Jr; Effects of a
series of inboard plan-form modifications on the longitudinal characteristics
of two 47 degree sweptback wings of aspect ratio 3.5, taper ratio 0.2, and
different thickness distributions at Mach numbers of 1.61 and 2.01;
naca-rm-l53e07a; July 17, 1953
- Williams, Claude V
Kuhn, Richard E; A
study of the aerodynamic loads on sweptback wings at transonic speeds;
naca-rm-l53e08b; June 25, 1953
- Dettwyler, H Rudolph
Faget, Maxime A; Engineering
method of ram-jet thrust determination based on experimentally obtained
combustor parameters; naca-rm-l53e21; August 13, 1953
- Williams, Claude V; A transonic
wind-tunnel investigation of the effects of body indentation on the
aerodynamic characteristics of an approximate-delta-wing-body configuration,
and a comparison with a wing of reversed plan form; naca-rm-l53f05a;
August 13, 1953
- Dennard, John S; A preliminary
investigation of the power requirements of slotted test sections;
naca-rm-l53f10; July 07, 1953
- Nelson, William J Vick,
Allen R; Slotted-boundary
interference effects on wedge airfoils at low supersonic Mach numbers;
naca-rm-l53f11; July 30, 1953
- Arbic, Richard G
Gillespie, Warren, Jr; Free-flight
longitudinal-stability investigation including some effects of wing elasticity
from Mach numbers of 0.85 to 1.34 of a tailless missile configuration having a
45 degree sweptback wing of aspect ratio 5.5; naca-rm-l53f18; August 10,
1953
- Pendley, Robert E
Milillo, Joseph R Fleming, Frank F Bryan, Carroll R; An
experimental study of five annular air inlet configurations at subsonic and
transonic speeds; naca-rm-l53f18a; August 19, 1953
- Palmer, William E; Effect of
reduction in thickness from 6 to 2 percent and removal of the pointed tips on
the subsonic static longitudinal stability characteristics of a 60 degree
triangular wing in combination with a fuselage; naca-rm-l53f24; August 19,
1953
- Savage, Melvyn Erwin,
John R Whitley, Robert P; Investigation
of an axial-flow compressor rotor having NACA high-speed blade sections (A(sub
2)I(sub 8b) series) at mean radius relative inlet Mach numbers up to 1.13;
naca-rm-l53g02; November 30, 1953
- Carlson, Harry W; Preliminary
investigation of the effects of body contouring as specified by the transonic
area rule on the aerodynamic characteristics of a delta wing-body combination
at Mach numbers of 1.41 and 2.01; naca-rm-l53g03; September 22,
1953
- Solomon, William West,
F E , Jr Brummal, Edward M; Investigation
of spoiler ailerons with and without a gap behind the spoiler on a 45 degree
sweptback wing-fuselage combination at Mach numbers from 0.60 to 1.03;
naca-rm-l53g07a; September 14, 1953
- Wiggins, James W; Wind-tunnel
investigation at high subsonic speeds of the static longitudinal and static
lateral stability characteristics of a wing-fuselage combination having a
triangular wing of aspect ratio 2.31 and an NACA 65A003 airfoil;
naca-rm-l53g09a; August 28, 1953
- Jones, George W , Jr
Dubose, Hugh C; Investigation
of wing flutter at transonic speeds for six systematically varied wing plan
forms; naca-rm-l53g10a; August 13, 1953
- (Author(s) Not
Available); Notes on
damping in roll and load distributions in roll at high angles of attack and
high subsonic speed; naca-rm-l53g13a; August 27, 1953
- Passera, Anthony L
Nason, Martin L; The
effect of control-surface-servo natural frequency on the dynamic performance
characteristics of an acceleration control system applied to a supersonic
missile; naca-rm-l53g23a; September 29, 1953
- Moul, Martin T Baber,
Hal T , Jr; Flight
investigation at Mach numbers from 0.67 to 1.81 of the longitudinal stability
and control characteristics of a 60 degree delta-wing missile configuration
having an all-movable tail; naca-rm-l53g29; October 06, 1953
- Kemp, William B , Jr
Becht, Robert E; Damping-in-pitch
characteristics at high subsonic and transonic speeds of four 35 degree
sweptback wings; naca-rm-l53g29a; October 16, 1953
- Yeates, John E , Jr
Thompson, Jim Rogers; A
preliminary study by means of electrical frequency-analysis techniques of the
response of an airplane structure during buffeting; naca-rm-l53g31;
December 08, 1953
- Goin, Kennith L Palmer,
William E; Subsonic and
supersonic hinge-moment and effectiveness characteristics of an unbalanced
lateral control having low theoretical hinge moments at supersonic speeds;
naca-rm-l53g31a; October 19, 1953
- Swihart, John M
Whitcomb, Charles F; Pressure
distributions on three bodies of revolution to determine the effect of
Reynolds number up to and including the transonic speed range;
naca-rm-l53h04; October 15, 1953
- O'Sullivan, William J
Rumsey, Charles B Chauvin, Leo T; Exploratory
investigation of transpiration cooling to alleviate aerodynamic heating on an
8 degree cone in a free jet at a Mach number of 2.05; naca-rm-l53h06;
September 14, 1953
- Strass, H Kurt
Stephens, Emily W; An
engineering method for the determination of aeroelastic effects upon the
rolling effectiveness of ailerons on swept wings; naca-rm-l53h14; November
30, 1953
- Radin, Edward J
Carpenter, Paul J; Comparison
of the performance of a helicopter-type ram-jet engine under various
centrifugal loadings; naca-rm-l53h18a; October 07, 1953
- Ogburn, Edmund L
Grigsby, Carl E; Investigation
of Reynolds number effects for a series of cone-cylinder bodies at Mach
numbers of 1.62, 1.93, and 2.41; naca-rm-l53h21; October 07, 1953
- Henderson, Arthur, Jr;
Investigation
at Mach numbers of 1.62, 1.93, and 2.41 of the effect of oscillation amplitude
on the damping in pitch of delta-wing-body combinations; naca-rm-l53h25;
October 26, 1953
- Strass, H Kurt Marley,
Edward T; Recent
experiences with flutter failure of sweptback, tapered wings having outboard,
partial-span spoiler controls; naca-rm-l53h26; October 05, 1953
- Hinners, Arthur H , Jr
Foland, Douglas, H; Preflight
tests and flight performance of a 6.5-inch diameter ram-jet engine;
naca-rm-l53h28; November 02, 1953
- Stoney, William E , Jr;
Some
experimental effects of afterbody shape on the zero-lift drag of bodies for
Mach numbers between 0.8 and 1.3; naca-rm-l53i01; October 1953
- Spearman, M Leroy; Component tests
to determine the aerodynamic characteristics of an all-moveable 70 degree
delta canard-type control in the presence of a body at a Mach number of
1.61; naca-rm-l53i03; October 09, 1953
- Martz, C William
Goslee, John W; Rocket-model
investigation to determine the hinge-moment and normal-force properties of a
full-span, constant-chord, partially balanced trailing-edge control on a 60
degree clipped delta wing between Mach numbers of 0.50 and 1.26;
naca-rm-l53i04; October 30, 1953
- Hatch, John E , Jr
Gallagher, James J; Aerodynamic
characteristics of a 68.4 degree delta wing at Mach numbers of 1.6 and 1.9
over a wide Reynolds number range; naca-rm-l53i08; November 02,
1953
- Gardiner, Robert A; A combined
aerodynamic and guidance approach for a simple homing system;
naca-rm-l53i10a; November 02, 1953
- Spearman, M Leroy; Aerodynamic
characteristics in pitch of a series of cruciform-wing missiles with canard
controls at a Mach number of 2.01; naca-rm-l53i14; October 30, 1953
- Hasel, Lowell E; The performance
of conical supersonic scoop inlets on circular fuselages; naca-rm-l53i14a;
November 17, 1953
- Lord, Douglas R
Czarnecki, K R; Recent
information on flap and tip controls; naca-rm-l53i17a; November 17,
1953
- Robins, A Warner; Preliminary
investigation of the effects of several seeker-nose configurations on the
longitudinal characteristics of a canard-type missile at a Mach number of
1.60; naca-rm-l53i18; October 30, 1953
- Mueller, James N; An
investigation at Mach number 2.40 of flap-type controls equipped with overhang
nose balances; naca-rm-l53i21; November 17, 1953
- Curfman, Howard J , Jr
Strass, H Kurt Crane, Harold L; Investigations
toward simplification of missile control systems; naca-rm-l53i21a;
November 12, 1953
- Toll, Thomas A; Longitudinal
characteristics of wings; naca-rm-l53i21b; October 28, 1953
- Sternfield, Leonard; Several factors
affecting roll control systems of interceptors; naca-rm-l53i22a; November
06, 1953
- Gapcynski, John P
Robins, A Warner; The
effect of nose radius and shape on the aerodynamic characteristics of a
fuselage and a wing-fuselage combination at angles of attack;
naca-rm-l53i23a; October 22, 1953
- Weil, Joseph Gray, W H;
Recent
design studies directed toward elimination of pitch-up; naca-rm-l53i23c;
November 18, 1953
- Lowry, John G; Data
on spoiler-type ailerons; naca-rm-l53i24a; October 28, 1953
- English, Roland D; Some effects of
leading-edge roughness on the aileron effectiveness and drag of a thin
rectangular wing employing a full-span plain aileron at Mach numbers from 0.6
to 1.5; naca-rm-l53i25; November 04, 1953
- Sears, R I Merlet, C F
Putland, L W; Flight
determination of drag of normal-shock nose inlets with various cowling
profiles at Mach numbers from 0.9 to 1.5; naca-rm-l53i25a; October 22,
1953
- Henning, Allen B; Results of a
rocket-model investigation of control-surface buzz and flutter on a
4-percent-thick unswept wing and on 6-, 9-, and 12-percent-thick swept wings
at transonic speeds; naca-rm-l53i29; November 20, 1953
- Johnson, Harold S; Wind-tunnel
investigation at high subsonic speeds of the effect of spoiler profile on the
lateral control characteristics of a wing-fuselage combination with
quarter-chord line swept back 32.6 degrees and NACA 65A006 airfoil
section; naca-rm-l53j05a; November 20, 1953
- Morris, Odell A; Control
hinge-moment and effectiveness characteristics of several interchangeable tip
controls on a 60 degree delta wing at Mach numbers of 1.41, 1.62, and
1.96; naca-rm-l53j08a; November 25, 1953
- Johnson, Harold S; Wind-tunnel
investigation at low speed of the effect of varying the ratio of body diameter
to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of a
45 degree sweptback-wing-body combination; naca-rm-l53j09a; November 30,
1953
- Parks, James H Kehlet,
Alan B; Longitudinal
stability and trim of two rocket propelled airplane models having 45 degree
sweptback wings and tails with the horizontal tail mounted in two
positions; naca-rm-l53j12a; December 09, 1953
- Passera, Anthony L
Bridgland, Thomas F , Jr; The
influence of the control-surface-servo natural frequency upon the transient
characteristics of a flight-path-angle control system incorporating a
supersonic missile; naca-rm-l53j15; December 10, 1953
- Wiley, Harleth G Riley,
Donald R; An
experimental and theoretical investigation at high subsonic speeds of the
effects of horizontal-tail height on the aerodynamic characteristics of an
unswept, untapered tail assembly; naca-rm-l53j19; December 02, 1953
- Vogler, Raymond D; Wind-tunnel
investigation at transonic speeds of a spoiler-slot-deflector combination on
an unswept NACA 65A006 wing; naca-rm-l53j21; December 08, 1953
- Mason, Homer P; Effects of
external store mounting on the buffet, trim, and drag characteristics of
rocket-powered fuselage and store combinations between Mach numbers of 0.7 and
1.4; naca-rm-l53j22; December 10, 1953
- Spearman, M Leroy; Effect of large
deflection of a canard control and deflections of a wing-tip control on the
static-stability and induced-roll characteristics of a cruciform canard
missile at a Mach number of 2.01; naca-rm-l53k03; December 14, 1953
- Houbolt, John C; Correlation of
calculation and flight studies of the effect of wing flexibility on structural
response due to gusts; naca-tn-3006; August 1953
- Diederich, Franklin W
Zlotnick, Martin; Calculated
spanwise lift distributions and aerodynamic influence coefficients for unswept
wings in subsonic flow; naca-tn-3014; September 1953
- Garrick, I E Watkins, C
E; A
theoretical study of the effect of forward speed on the free-space
sound-pressure field around propellers; naca-tn-3018; October 1953
- Amer, Kenneth B; Method for
studying helicopter longitudinal maneuver stability; naca-tn-3022; October
1953
- Gray, W L (Boeing
Airplane Company) Schenk, K M (Boeing Airplane Company); A
method for calculating the subsonic steady-state loading on an airplane with a
wing of arbitrary plan form and stiffness; naca-tn-3030; December
1953
- Liepmann, H W
(California Institute of Technology) Robinson, M S (California Institute of
Technology); Counting
methods and equipment for mean-value measurements in turbulence research;
naca-tn-3037; October 1953
- Walker, Walter G; Summary of
revised gust-velocity data obtained from V-G records taken on civil transport
airplanes from 1933 to 1950; naca-tn-3041; November 1953
- Hickman, William A Dow,
Norris F; Direct-reading
design charts for 24S-T3 aluminum-alloy flat compression panels having
longitudinal formed hat-section stiffeners and comparisons with panels having
z-section stiffeners; naca-tn-2792; March 1953
- Leonard, Robert W
Budiansky, Bernard; On
traveling waves in beams; naca-tn-2874; 1953
- Wilder, Thomas W , III;
An analysis
of statically indeterminate trusses having members stressed beyond the
proportional limit; naca-tn-2886; February 1953
- Das, Dilip K
(University of Notre Dame) Beck, Paul A (University of Notre Dame); Survey
of portions of the iron-nickel-molybdenum and cobalt-iron-molybdenum ternary
systems at 1200 C; naca-tn-2896; February 1953
- Castles, Walter, Jr
(Georgia Institute of Technology) De Leeuw, Jacob Henri (Georgia Institute of
Technology); The normal
component of the induced velocity in the vicinity of a lifting rotor and some
examples of its application; naca-tn-2912; March 1953
- Callaghan, Edmund E
Serafini, John S; A
method for rapid determination of the icing limit of a body in terms of the
stream conditions; naca-tn-2914; March 1953
- Grover, H J (Battelle
Memorial Institute) Hyler, W S (Battelle Memorial Institute) Kuhn, Paul
(Aluminum Company of America) Landers, Charles B Howell, F M; Axial-load
fatigue properties of 24S-T and 75S-T aluminum alloy as determined in several
laboratories; naca-tn-2928; May 1953
- Stokes, George M Davis,
Don D , Jr; The attenuation
characteristics of four specially designed mufflers tested on a practical
engine setup; naca-tn-2943; May 1953
- Skopinski, T H Aiken,
William S , Jr Huston, Wilber B; Calibration
of strain-gage installations in aircraft structures for the measurements of
flight loads; naca-tn-2993; August 1953
- Eggleston, John M
Mathews, Charles W; Application
of several methods for determining transfer functions and frequency response
of aircraft from flight data; naca-tn-2997; September 1953
- Wolock, I (National
Bureau of Standards) Axilrod, B M (National Bureau of Standards) Sherman, M A
(National Bureau of Standards); Effects
of high degrees of biaxial stretch forming on crazing and other properties of
acrylic plastic glazing; naca-rm-53d14; June 29, 1953
- Smith, Willard G; Wind-tunnel
investigation at subsonic and supersonic speeds of a model of a tailless
fighter airplane employing a low-aspect-ratio swept-back wing : effects of
external fuel tanks and rocket packets on the drag characteristics;
naca-rm-a52j31; January 12, 1953
- Rolls, L Stewart
Havill, C Dewey Holden, George R; Techniques
for determining thrust in flight for airplanes equipped with afterburners;
naca-rm-a52k12; January 19, 1953
- Franks, Ralph W; Tests in the
Ames 40- by 80-foot wind tunnel of an airplane model with an aspect ratio 4
triangular wing and an all-movable horizontal tail - high-lift devices and
lateral controls; naca-rm-a52k13; February 20, 1953
- Hightower, Ronald C; Lift, drag and
pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds :
comparison of three wings of aspect ratio 2 of rectangular, swept-back and
triangular plan form, including effects of thickness distribution;
naca-rm-a52l02; February 16, 1953
- Franks, Ralph W; Tests in the
Ames 40- by 80-foot wind tunnel of two airplane models having aspect ratio 2
trapezoidal wings of taper ratios 0.33 and 0.20; naca-rm-a52l16; February
16, 1953
- Anderson, Seth B Van
Dyke, Rudolph D , Jr Matteson, Frederick H; A
flight investigation of the effect of leading-edge camber on the aerodynamic
characteristics of a swept-wing airplane; naca-rm-a52l16a; February 18,
1953
- Rolls, L Stewart; A flight
comparison of a submerged inlet and a scoop inlet at transonic speeds;
naca-rm-a53a06; March 19, 1953
- Gowen, Forrest E; Buffeting of a
vertical tail on an inclined body at supersonic Mach numbers;
naca-rm-a53a09; March 24, 1953
- Hopkins, Edward J
Carel, Hubert C; Experimental
and theoretical study of the interference at low speed between slender bodies
and triangular wings; naca-rm-a53a14; May 06, 1953
- James, Harry A
Mcfadden, Norman M Mccloud, John L , III; Comparison
of measured and predicted indicated angles of attack near the fuselages of a
triangular-wing wind-tunnel model and a swept-wing fighter airplane in
flight; naca-rm-a53a15; March 11, 1953
- Reynolds, Robert M
Sammonds, Robert I Kenyon, George C; An
investigation of a four-blade single-rotation propeller in combination with an
NACA 1-series D-type cowing at Mach numbers up to 0.83; naca-rm-a53b06;
April 13, 1953
- Matthews, Howard F
Schmidt, Stanley F; A
theoretical study of the effect of control-deflection and control-rate
limitations on the normal acceleration and roll response of a supersonic
interceptor; naca-rm-a53b11; April 29, 1953
- Tinling, Bruce E Lopez,
Armando E; The effects of
nacelles and of extended split flaps on the longitudinal characteristics of a
wing-fuselage-tail combination having a wing with 40 degrees of sweepback and
an aspect ratio of 10; naca-rm-a53d06; June 05, 1953
- Graham, David; The
low-speed lift and drag characteristics of a series of airplane models having
triangular or modified triangular wings; naca-rm-a53d14; June 15,
1953
- Koenig, David G; Tests in the
Ames 40- by 80-foot wind tunnel of an airplane configuration with a
variable-incidence triangular wing and an all-movable horizontal tail;
naca-rm-a53d21; June 25, 1953
- Holzhauser, Curt A
Cook, Woodrow L Kelly, Mark W; The
use of area suction for the purpose of improving trailing-edge flap
effectiveness on a 35 degree sweptback wing; naca-rm-a53e06; July 02,
1953
- Selan, Ralph
Bandittini, Angelo; The
effects of leading-edge extensions, a trailing-edge extension, and a fence on
the static longitudinal stability of a wing-fuselage-tail combination having a
wing with 35 degrees of sweepback and an aspect ratio of 4.5;
naca-rm-a53e12; August 07, 1953
- Abramovitz, Marvin
Schmidt, Stanley F Van Dyke, Rudolph D , Jr; Investigation
of the use of a stick force proportional to pitching acceleration for
normal-acceleration warning; naca-rm-a53e21; August 14, 1953
- Reed, Verlin D Smith,
Donald W; The lateral
control characteristics of constant-percent-chord trailing-edge elevons on a
pointed wing of aspect ratio 2 at Mach numbers up to 0.95; naca-rm-a53f03;
August 14, 1953
- Drake, William C; Lift, drag, and
hinge moments at supersonic speeds of an all-movable triangular wing and body
combination; naca-rm-a53f22; September 16, 1953
- Bray, Richard S; The effects of
fences on the high-speed longitudinal stability of a swept-wing airplane;
naca-rm-a53f23; August 31, 1953
- Hemenover, Albert D; Tests of the
NACA 0010-1.50 40/1.051 airfoil section at high subsonic Mach numbers;
naca-rm-a53g09; September 04, 1953
- Sadoff, Melvin; Flight
measurements of the horizontal-tail loads on a swept-wing fighter airplane at
transonic speeds; naca-rm-a53g10; November 06, 1953
- Anderson, Seth B; Correlation of
flight and wind-tunnel measurements of roll-off in low-speed stalls on a 35
degree swept-wing aircraft; naca-rm-a53g22; September 24, 1953
- Ziff, Howard L Rathert,
George A Gadeberg, Burnett L; An
analysis of the tracking performances of two straight-wing and two swept-wing
fighter airplanes with fixed sights in a standardized test maneuver;
naca-rm-a53h12; October 22, 1953
- Spiegel, Joseph M
Kuehn, Donald M Hofstetter, Robert U; Applications
of auxiliary air injectors to supersonic wind tunnels; naca-rm-a53i01;
November 25, 1953
- Cleary, Joseph W Boddy,
Lee E; Wind-tunnel
investigation of a 45 degree sweptback wing having a symmetrical root and a
highly cambered tip, including the effects of fences and lateral controls;
naca-rm-a53i21; November 20, 1953
- Axelson, John A; Downwash behind
a triangular wing of aspect ratio 3 - : transonic bump method;
naca-rm-a53i23; December 1953
- Holzhauser, Curt A
Martin, Robert K; The
use of a leading-edge area-suction flap to delay separation of air flow from
the leading edge of a 35 degrees sweptback wing; naca-rm-a53j26; December
10, 1953
- Zlotnick, Martin
Robinson, Samuel W , Jr; A
simplified mathematical model for calculating aerodynamic loading and downwash
for midwing wing-fuselage combinations with wings of arbitrary plan form;
naca-rm-l52j27a; January 16, 1953
- Newman, Ernest E
Cahill, Jones F; Investigation
at low speed of the flow field behind the lifting surfaces of a model equipped
with a 60 degree triangular wing and a 60 degree triangular canard tail;
naca-rm-l53c30; June 29, 1953
- Fournier, Paul G; Wind-tunnel
investigation of the aerodynamic characteristics in pitch and sideslip at high
subsonic speeds of a wing fuselage combination having a triangular wing of
aspect ratio 4; naca-rm-l53g14a; August 28, 1953
- Trimpi, Robert L; A theory for
stability and buzz pulsation amplitude in ram jets and an experimental
investigation including scale effects; naca-rm-l53g28; October 15,
1953
- Cahen, George L; Gust-tunnel
investigation of the effect of leading edge separation on the normal
accelerations experienced by a 45 degree sweptback-wing model in gusts;
naca-rm-l53j07; November 24, 1953
- Sretensky, L. N.; Motion of a
cylinder under the surface of a heavy fluid; naca-tm-1335; 1953
- Hamel, Georg.; Spiral
motions of viscous fluids; naca-tm-1342; 1953
- Rotta, J.; On
the theory of the turbulent boundary layer; naca-tm-1344; 1953
- Schlichting, Hermann.,
Moller, Egon.; Report
on the special field "Interference" to the wind-tunnel committee in February
1945; naca-tm-1347; 1953
- Yatseyev, V. I.; On a class of
exact solutions of the equations of motion of a viscous fluid;
naca-tm-1349; 1953
- Obukhoff, A. M.,
Yaglom, A. M.; The
microstructure of turbulent flow; naca-tm-1350; 1953
- Rabotnov, Y. N.; Some problems
on the theory of creep; naca-tm-1353; 1953
- Fabri, Jean.,
Siestrunck, Raymond.; Study
of the supersonic propeller; naca-tm-1355; 1953
- Sanger, Eugen.; Air admixture
to exhaust jets; naca-tm-1357; 1953
- Fradenburgh, Evan A.,
Campbell, Robert C.; Characteristics
of a canard-type missile configuration with an underslung scoop inlet at Mach
numbers from 1.5 to 2.0; naca-rm-e52j22; 1953
- Love, Eugene S.; Base pressure
at supersonic speeds on two-dimensional airfoils and on bodies of revolution
(with and without fins) having turbulent boundary layers; naca-rm-l53c02;
1953
- Allen, H. Julian,
Eggers, A. J. Jr.; A
study of the motion and aerodynamic heating of missiles entering the earth's
atmosphere at high supersonic speeds; naca-rm-a53d28; 1953
- Weick, Fred E
(Agricultural and Mechanical College of Texas) Sevelson, Maurice S
(Agricultural and Mechanical College of Texas) Mcclure, James G (Agricultural
and Mechanical College of Texas) Flanagan, Marion D (Agricultural and
Mechanical College of Texa; Investigation
of lateral control near the stall flight investigation with a light high-wing
monoplane tested with various amounts of washout and various lengths of
leading-edge slot; naca-tn-2948; May 1953
- Vasu, George., Hinde,
William L.; Effect of
engine and control limits on steady-state and transient performance of
turbojet engine with variable-area exhaust nozzle; naca-rm-e52e23;
1953
- Gabriel, David S.,
Krebs, Richard P., Wilcox, E. Clinton., Koutz, Stanley L.; Analysis
of the turbojet engine for propulsion of supersonic fighter airplanes / David
S. Gabriel, Richard P. Krebs, E.Clinton Wilcox, Stanley L.Koutz;
naca-rm-e52f17; 1953
- Finger, Harold B.,
Essig, Robert H., Conrad, E. William.; Effect
of rotor-and stator-blade modifications on surge performance of an 11-stage
axial-flow compressor I :original production compressor of XJ40-WE-6
engine; naca-rm-e52g03; 1953
- Renas, Paul E., Jansen,
Emmert T.; Altitude
performance characteristics of the J47-25 turbojet engine :data
presentation; naca-rm-e52g22; 1953
- Bloomer, Harry E.,
Walker, William J., Pantages, George L.; Altitude
investigation of XJ34-WE-32 engine performance without electronic control;
naca-rm-e51l12; 1953
- Smith, Willard G.; Wind-tunnel
investigation at subsonic and supersonic speeds of a model of a tailless
fighter airplane employing a low-aspect-ratio swept-back wing :stability and
control; naca-rm-a52j30; 1953
- Reynolds, Robert M.; Preliminary
results of an investigation of the effects of spinner shape on the
characteristics of an NACA D-type cowl behind a three-blade propeller,
including the characteristics of the propeller at negative thrust;
naca-rm-a53j02; 1953
- Calvert, Howard F.,
Meyer, Andre' J., Jr., Morse, C. Robert.; Investigation
of blade failures in a J34, eleven-stage axial-flow compressor;
naca-rm-e52i16; 1953
- Bogart, Donald.,
Valerino, Michael F.; The
sodium hydroxide reactor :effect of reactor variables on criticality and
fuel-element temperature requirements for subsonic and supersonic aircraft
nuclear propulsion; naca-rm-e52i19; 1953
- Ladanyi, Dezso J.,
Miller, Riley O., Karo, Wolf., Feiler, Charles E.; Some
fundamental aspects of nitric acid oxidants for rocket applications;
naca-rm-e52j01; 1953
- Sobolewski, Adam E.,
Miller, Robert R., McAulay, John E.; Altitude
performance investigation of two single-annular type combustors and the
prototype J40-WE-8 turbojet engine combustor with various combustor-inlet air
pressure profiles; naca-rm-e52j07; 1953
- Norgren, Carl T.,
Childs, J. Howard.; Effect
of liner air-entry holes, fuel state, and combustor size on performance of an
annular turbojet combustor at low pressures and high air-flow rates;
naca-rm-e52j09; 1953
- Campbell, Carl E.,
Welna, Henry J.; Preliminary
evaluation of turbine performance with variable-area turbine nozzles in a
turbojet engine; naca-rm-e52j20; 1953
- Foster, Hampton H.,
Straight, David M.; Effect
of fuel volatility characteristics on ignition-energy requirements in a
turbojet combustor; naca-rm-e52j21; 1953
- Farley, John M., Smith,
Robert E., Povolny, John H.; Preliminary
experiments with pilot burners for ram-jet combustors; naca-rm-e52j23;
1953
- Dugger, Gordon L.,
Graab, Dorothy D.; Flame
velocities of propane- and ethylene-oxygen-nitrogen mixtures;
naca-rm-e52j24; 1953
- Fleming, William A.; Internal
performance of several types of jet-exit configurations for supersonic
turbojet aircraft; naca-rm-e52k04; 1953
- DiPiazza, J. T.; A compilation
of summaries from NACA reports on fuels research, 1945-1952;
naca-rm-53d28; 1953
- Smith, Gordon T.,
Curren, Arthur N.; Comparison
of pressure-loss characteristics of several tail-cone air-induction systems
for air-cooled gas-turbine rotors; naca-rm-e52k07; 1953
- McAulay, John E.,
Kaufman, Harold R.; Altitude
wind tunnel investigation of the prototype J40-WE-8 turbojet engine without
afterburner; naca-rm-e52k10; 1953
- Lord, Albert M., Evans,
Vernida E.; Effect of
particle size and stabilizing additives on the combustion properties of
magnesium slurry; naca-rm-e52k12; 1953
- Deutsch, George C.,
Meyer, Andre J., Jr., Morgan, William C.; Preliminary
investigation in J33 turbojet engine of several root designs for ceramal
turbine blades; naca-rm-e52k13; 1953
- Hollister, Donald P.,
Greathouse, William K.; Performance
of double-shroud ejector configuration with primary pressure ratios from 1.0
to 10; naca-rm-e52k17; 1953
- Ladanyi, Dezso J.; Orthotoluidine
and triethylamine in rocket engine applications; naca-rm-e52k19;
1953
- Miller, Riley O.; Ignition delays
of some nonaromatic fuels with low-freezing red fuming nitric acid in
temperature range -40 to -105 F; naca-rm-e52k20; 1953
- Miller, Riley O.,
Ladanyi, Dezso J.; Ignition
delays of alkyl thiophosphites with white and red fuming nitric acids within
temperature range 80 to -105 F; naca-rm-e52k25; 1953
- Macks, E. Fred.,
Anderson, W. J., Nemeth, Zolton N.; Preliminary
comparison of 17- and 75-millimeter-bore cageless cylindrical roller bearings
with conventional cylindrical roller bearings at high speeds;
naca-rm-e52l05; 1953
- Grele, Milton D.,
Gedeon, Louis.; Forced-convection
heat-transfer characteristics of molten sodium hydroxide; naca-rm-e52l09;
1953
- Conrad, E. William.,
Campbell, Carl E.; Altitude
investigation of several afterburner configurations for the J40-WE-8 turbojet
engine; naca-rm-e52l10; 1953
- Gordon, Sanford., Huff,
Vearl N.; Theoretical
performance of liquid hydrogen and liquid fluorine as a rocket propellant;
naca-rm-e52l11; 1953
- Jansen, E. T., Renas,
P. E.; Altitude
investigation of thrust augmentation using water-alcohol injection into the
combustion chambers of an axial-flow turbojet engine; naca-rm-e52l12;
1953
- Hoffman, Charles A.; Preliminary
investigation of zirconium boride ceramals for gas-turbine blade
applications; naca-rm-e52l15a; 1953
- Walker, Curtis L.,
Braithwaite, Willis M., Fenn, David B.; Component
and over-all performance evaluation of a J47-GE-25 turbojet engine over a
range of engine-inlet Reynolds number indices; naca-rm-e52l16; 1953
- Garrett, Floyd B.,
Gyorgak, Charles A., Weeton, John Waldemar.; Behavior
of forged S-816 turbine blades in steady-state operation of J33-9 turbojet
engine with stress-rupture and metallographic evaluations / By F. B.Garrett,
C. A. Gyorgak, and J. W. Weeton; naca-rm-e52l17; 1953
- Maxwell, W. A.; Preliminary
investigation of plate-type molybdenum disilicide fuel elements for an
air-cycle nuclear reactor; naca-rm-e52l18; 1953
- Useller, James W.,
Fenn, David B., Harp, James L., Jr.; Turbojet-engine
thrust augmentation at altitude by combined ammonia injection into the
compressor inlet and afterburning; naca-rm-e52l19; 1953
- Nagey, T. F., Sams, E.
W.; Effect
of drawbar upstream location on air velocity distribution at the inlet face of
reactor segment designed by the General Electric Company; naca-rm-e52l22;
1953
- Lowell, Herman H.; Free fall and
evaporation of N-Octane droplets in the atmosphere as applied to the
jettisoning of aviation gasoline at altitude; naca-rm-e52l23a; 1953
- Hansen, Arthur G.,
Costello, George R., Herzig, Howard Z.; Smoke
studies of secondary flows in bends, tandem cascades, and high-turning
configurations; naca-rm-e52l24a; 1953
- Garrett, Floyd B.,
Gyorgak, Charles A.; Adhesive
and protective characteristics of ceramic coating A-417 and its effect on
engine life of forged Refractaloy-26 (AMS 5760) and cast stellite 21 (AMS
5385) turbine blades; naca-rm-e52l30; 1953
- Yeomans, C. M.,
Hoffman, C. A.; Thermal-shock
resistance of a ceramic comprising 60 percent boron carbide and 40 percent
titanium diboride; naca-rm-e52l31; 1953
- Robert W. Dunning and
Fred M. Smith (Langley Aeronautical Laboratory, Langley Field, Va.); Aerodynamic
Characteristics of Two Delta Wings and Two Trapezoidal Wings at Mach Number
4.04; naca-rm-l50d30a; 1953
- William J. Nelson and
James M. Cubbage, Jr. (Langley Aeronautical Laboratory, Langley Field, Va.);
Effects of
Slot Size and Geometry on the Flow in Rectangular Tunnels at Mach Numbers up
to 1.4; naca-rm-l53b16; 1953
- Chester B. Payne
(Langley Aeronautical Laboratory, Langley Field, Va.); A
Flight Investigation of Some Effects of Automatic Control on Gust Loads;
naca-rm-l53e14a; 1953
- Delwin R. Croom and
Harleth G. Wiley (Langley Aeronautical Laboratory, Langley Field, Va.); Investigation
at Transonic Speeds of the Hinge-Moment and Lift-Effectiveness Characteristics
of a Single Flap and a Tandem Flap on a 60o Delta Wing; naca-rm-l53e28a;
1953
- Gordon L. Dugger,
Dorothy M. Simon; Prediction
of flame velocities of hydrocarbon flames; naca-report-1158; 1954
- John S. Serafini; Impingement of
water droplets on wedges and double-wedge airfoils at supersonic speeds;
naca-report-1159; 1954
- Albert J. Evans; The zero-lift
drag of a slender body of revolution (NACA RM-10 research model) as determined
from tests in several wind tunnels and in flight at supersonic speeds;
naca-report-1160; 1954
- Elmo J. Mottard, J. Dan
Loposer; Average
skin-friction drag coefficients from tank tests of a parabolic body of
revolution (NACA RM-10); naca-report-1161; 1954
- Harvard Lomax; Lift
developed on unrestrained rectangular wings entering gusts at subsonic and
supersonic speeds; naca-report-1162; 1954
- Howard Z. Herzig,
Arthur G. Hansen, George R. Costello; A
visualization study of secondary flows in cascades; naca-report-1163;
1954
- H. S. Ribner; Convection
of a pattern of vorticity through a shock wave; naca-report-1164;
1954
- Franklin K. Moore; Unsteady
oblique interaction of a shock wave with a plane disturbance;
naca-report-1165; 1954
- J. C. Richmond, D. G.
Moore, H. B. Kirkpatrick, W. N. Harrison; Relation
between roughness of interface and adherence of porcelain enamel to steel;
naca-report-1166; 1954
- Albert P. Martina; Method for
calculating the rolling and yawing moments due to rolling for unswept wings
with or without flaps or ailerons by use of nonlinear section lift data;
naca-report-1167; 1954
- Harold E. Rohlik,
Milton G. Kofskey, Hubert W. Allen, Howard Z. Herzig; Secondary
flows and boundary-layer accumulations in turbine nozzles;
naca-report-1168; 1954
- James J. Donegan; Matrix methods
for determining the longitudinal-stability derivatives of an airplane from
transient flight data; naca-report-1169; 1954
- S. S. Manson; Behavior
of materials under conditions of thermal stress; naca-report-1170;
1954
- Donald R. Riley; Effect of
horizontal-tail span and vertical location on the aerodynamic characteristics
of an unswept tail assembly in sideslip; naca-report-1171; 1954
- Harry Press, Bernard
Mazelsky; A
study of the application of power-spectral methods of generalized harmonic
analysis to gust loads on airplanes; naca-report-1172; 1954
- Robert W. Leonard,
Bernard Budiansky; On
traveling waves in beams; naca-report-1173; 1954
- John Laufer; The
structure of turbulence in fully developed pipe flow; naca-report-1174;
- T. C. Lin, R. E.
Street; Effect of
variable viscosity and thermal conductivity on high-speed slip flow between
concentric cylinders; naca-report-1175; 1954
- S. Katzoff, M. Frances
Faison, Hugh C. Dubose; Determination
of mean camber surfaces for wings having uniform chordwise loading and
arbitrary spanwise loading in subsonic flow; naca-report-1176; 1954
- William J. Anderson, E.
Fred Macks, Zolton N. Nemeth; Comparison
of performance of experimental and conventional cage designs and materials for
75-millimeter-bore cylindrical roller bearings at high speed;
naca-report-1177; 1954
- T. H. Skopinski,
William S. Aiken, Jr., Wilber B. Huston; Calibration
of strain-gage installations in aircraft structures for the measurement of
flight loads; naca-report-1178; 1954
- James J. Kramer, John
D. Stanitz; A note on
secondary flow in rotating radial channels; naca-report-1179; 1954
- Walter G. Vincenti,
Cleo B. Wagoner; Theoretical
study of the transonic lift of a double-wedge profile with detached bow
wave; naca-report-1180; 1954
- John C. Houbolt, Eldon
E. Kordes; Structural
response to discrete and continuous gusts of an airplane having wing bending
flexibility and a correlation of calculated and flight results;
naca-report-1181; 1954
- E. R. G. Eckert, N. B.
Livingood; Comparison of
effectiveness of convection-, transpiration-, and film-cooling methods with
air as coolant; naca-report-1182; 1954
- Milton D. Van Dyke; Supersonic flow
past oscillating airfoils including nonlinear thickness effects;
naca-report-1183; 1954
- Walter R. Castles,
Jacob Henri De Leeuw; The
normal component of the induced velocity in the vicinity of a lifting rotor
and some examples of its application; naca-report-1184; 1954
- Max A. Heaslet, Harvard
Lomas; The
calculation of pressure on slender airplanes in subsonic and supersonic
flow; naca-report-1185; 1954
- Rose L. Schalla, Thomas
P. Clark, Glen E. McDonald; Formation
and combustion of smoke in laminar flames; naca-report-1186; 1954
- Merwin Sibulkin; Theoretical and
experimental investigation of additive drag; naca-report-1187; 1954
- Murray Tobak; On
the use of the indicial-function concept in the analysis of unsteady motions
of wings and wing-tail combinations; naca-report-1188; 1954
- Antonio Ferri, Louis M.
Nucci; Theoretical and
experimental analysis of low-drag supersonic inlets having a circular cross
section and a central body at Mach numbers 3.30, 2.75, and 2.45;
naca-report-1189; 1954
- H. J. Grover, W. S.
Hyler, Paul Kuhn, Charles B. Landers, F. M. Howell; Axial-load
fatigue properties of 24S-T and 75S-T aluminum alloy as determined in several
laboratories; naca-report-1190; 1954
- Evan A. Fradenburg, D.
Wyatt Demarquis; Theoretical
performance characteristics of sharp-lip inlets at subsonic speeds;
naca-report-1193; 1954
- Milton D. Van Dyke; A study of
hypersonic small-disturbance theory; naca-report-1194; 1954
- Norris R. Dow, Charles
Libove, Ralph E. Hubka; Formulas
for the elastic constants of plates with integral waffle-like stiffening;
naca-report-1195; 1954
- Wilmer H. Reed, III; An analytical
study of the effect of airplane wake on the lateral dispersion of aerial
sprays; naca-report-1196; 1954
- Donald C. Cheatham; A study of the
characteristics of human-pilot control response to simulated aircraft lateral
motions; naca-report-1197; 1954
- I. E. Garrick, Charles
E. Watkins; A theoretical
study of the effect of forward speed on the free-space sound-pressure field
around propellers; naca-report-1198; 1954
- John P. Campbell,
Marion O. McKinney, Jr.; A
study of the problem of designing airplanes with satisfactory inherent damping
of the dutch roll oscillation; naca-report-1199; 1954
- Kenneth B. Amer; Method for
studying helicopter longitudinal maneuver stability; naca-report-1200;
1954
- B. H. Little, Jr.,
Stafford W. Wilbur; Performance
and boundary-layer data from 12 degree and 23 degree conical diffusers of area
ratio 2.0 at Mach numbers up to choking and Reynolds numbers up to 7.5 x
10(6); naca-report-1201; 1954
- Roger A. Anderson,
Joseph W. Semonian; Charts
relating the compressive buckling stress of longitudinally supported plates to
the effective deflectional and rotational stiffness of the supports;
naca-report-1202; 1954
- M. J. Queijo, Byron M.
Jaquet, Walter D. Wolhart; Wind-tunnel
investigation at low speed of the effects of chordwise wing fences and
horizontal-tail position on the static longitudinal stability characteristics
of an airplane model with a 35 degree sweptback wing; naca-report-1203;
1954
- John M. Eggleston,
Charles W. Mathews; Application
of several methods for determining transfer functions and frequency response
of aircraft from flight data; naca-report-1204; 1954
- W. H. Gray, J. M.
Hallissy, Jr., A. R. Heath, Jr.; A
wind-tunnel investigation of the effects of thrust-axis inclination on
propeller first-order vibration; naca-report-1205; 1954
- Kermit G. Pratt, Walter
G. Walker; A
revised gust-load formula and a re-evaluation of v-g data taken on civil
transport airplanes from 1933 to 1950; naca-report-1206; 1954
- Kenneth B. Amer, Robert
J. Tapscott; Studies of the
lateral-directional flying qualities of a tandem helicopter in forward
flight; naca-report-1207; 1954
- William C. Schneider;
A comparison
of the spanwise loading calculated by various methods with experimental
loadings obtained on a 45 degree sweptback wing of aspect ratio 8.02 at a
Reynolds number of 4.0 x 10(6); naca-report-1208; 1954
- Leslie S. G. Kovasznay;
Development
of turbulence-measuring equipment; naca-report-1209; 1954
- William B. Boatright;
An analysis
of pressure studies and experimental and theoretical downwash and sidewash
behind five pointed-tip wings at supersonic speeds; naca-rm-l54b10; Apr
1954
- M. Spearman, Ross B.
Robinson; Aerodynamic
characteristics of a cruciform-wing missile with canard control surfaces and
of some very small span wing-body missiles at a Mach number of 1.41;
naca-rm-l54b11; Apr 1954
- Thomas B. Sellers,
George M. Stakes, Don D. Davis; An
experimental investigation of the transonic-flow-generation and
shock-wave-reflection characteristics of a two-dimensional wind tunnel with
17-percent-open perforated walls; naca-rm-l54b15a; Apr 1954
- Richard E. Walters; Comparison of
experimental with calculated results for the lifting effectiveness of a
flexible 45 degree sweptback wing of aspect ratio 6.0 at Mach numbers from 0.8
to 1.3; naca-rm-l54b16; Apr 1954
- H. Norman Silvers,
William J. Alford; Investigation
at high subsonic speeds of finned and unfinned bodies mounted at various
locations from the wings of unswept- and swept-wing--fuselage models,
including measurements of body loads; naca-rm-l54b18; Apr 1954
- Albert L. Braslow, Gene
J. Bingham; Subsonic
investigation of effects of body indentation on zero-lift drag characteristics
of a 45 degree sweptback wing-body combination with natural and fixed
boundary-layer transition through a range of Reynolds numbers;
naca-rm-l54b18a; Apr 1054
- Isabella J. Cole,
Kenneth Margolis; Span
load distribution resulting from constant vertical acceleration for thin
sweptback; naca-tn-3120; Jan 1954
- Lewis R. Fisher; Some effects of
aspect ratio and tail length on the contribution of a vertical tail to
unsteady lateral damping and directional stability of a model oscillating
continuously in yaw; naca-tn-3121; Jan 1954
- Robert M. O Donnell; Experimental
investigation at a Mach number of 2.41 of average skin-friction
coefficients; naca-tn-3122; Jan 1954
- Jerome Persh, Bruce M.
Bailey; Effect of
various arrangements of triangular ledges on the performance of a 23 degree
conical diffuser at subsonic Mach numbers; naca-tn-3123; Jan 1954
- Persh, Jerome Bailey,
Bruce M; A
method for estimating the effect of turbulent velocity fluctuations in the
boundary layer on diffuser total-pressure-loss measurements; naca-tn-3124;
1954
- Thomas N. Canning; A simple
mechanical analogue for studying the dynamic stability of aircraft having
nonlinear moment characteristics; naca-tn-3125; Feb 1954
- Robert E. Dannenberg;
A design
study of leading-edge inlets for unswept wings; naca-tn-3126; Mar
1954
- Louis S. Stivers, Jr.;
The
effectiveness at high subsonic Mach numbers of a 20-percent-chord plain
trailing-edge flap on the NACA 65-210 airfoil section; naca-tn-3127; Mar
1954
- William C. Pitts, Jack
N. Nielsen, Maurice P. Gionfriddo; Comparison
between theory and experiment for interference pressure field between wing and
body at supersonic speeds; naca-tn-3128; Apr 1954
- John A. Axelson, George
L. Stevens; Investigation
of a slat in several different positions on an NACA 64A010 airfoil for a wide
range of subsonic Mach numbers; naca-tn-3129; Mar 1954
- Carr B. Neel; A
procedure for the design of air-heated ice-prevention systems;
naca-tn-3130; Jun 1954
- Herbert F. Hardrath,
Walter Illg; Fatigue tests
at stresses producing failure in 2 to 10,000 cycles; naca-tn-3132; Jan
1954
- Ordway B. Gates, Jr.,
C. H. Woodling; A
method for estimating variations in the roots of the lateral-stability quartic
due to changes in mass and aerodynamic parameters of an airplane;
naca-tn-3134; Jan 1954
- William H. Michael,
Jr.; Investigation
of mutual interference effects of several vertical-tail-fuselage configuration
in sideslip; naca-tn-3135; Jan 1954
- Joseph Kempner; Creep bending
and buckling of linearly viscoelastic columns; naca-tn-3136; Jan
1954
- Joseph Kempner; Creep bending
and buckling of nonlinearly viscoelastic columns; naca-tn-3137; Jan
1954
- Joseph Kempner, Sharad
A. Patel; Creep buckling
of columns; naca-tn-3138; Jan 1954
- Nathan Ness; Time-dependent
buckling of a uniformly heated column; naca-tn-3139; Jan 1954
- W. E. Moeckel; Use
of aerodynamic heating to provide thrust by vaporization of surface
coolants; naca-tn-3140; Feb 1954
- Simon Ostrach; Combined
natural- and forced-convection laminar flow and heat transfer of fluids with
and without heat sources in channels with linearly varying wall
temperatures; naca-tn-3141; Apr 1954
- Robert L. Ferguson; A further
investigation of the effect of surface finish on fatigue properties at
elevated temperatures; naca-tn-3142; Mar 1954
- Willard D. Coles; Experimental
determination of thermal conductivity of low-density ice; naca-tn-3143;
Mar 1954
- John M. Bailey, Douglas
Godfrey; Coefficient of
friction and damage to contact area during the early stages of fretting II :
steel, iron, iron oxide, and glass combinations; naca-tn-3144; Apr
1954
- Simon Ostrach; Note
on the aerodynamic heating of an oscillating surface; naca-tn-3146; Apr
1954
- Rinaldo J. Brun, Robert
G. Dorsch; Impingement of
water droplets on an ellipsoid with fineness ration 10 in axisymmetric
flow; naca-tn-3147; May 1954
- Kenneth C. Dike; Evaluation of
alloys for vacuum brazing of sintered wrought molybdenum for
elevated-temperature applications; naca-tn-3148; May 1954
- James E. Hubbartt,
Henry O. Slone, Vernon L. Arne; Method
for rapid determination of pressure change for one-dimensional flow with heat
transfer, friction, rotation, and area change; naca-tn-3150; Jun
1954
- Paul A. Libby, Morris
Morduchow; Method for
calculation of compressible laminar boundary layer with axial pressure
gradient and heat transfer; naca-tn-3157; Jan 1954
- M. J. McGuigan, D. F.
Bryan, R. E. Whaley; Fatigue
investigation of full-scale transport-airplane wings : summary of
constant-amplitude tests through 1953; naca-tn-3190; Mar 1954
- D. G. Moore, J. W.
Pitts, W. N. Harrison; Role
of nickel dip in enameling of sheet steel; naca-tn-3207; Jun 1954
- John A. Kelly, George
B. McCullough; Aerodynamic
loads on a leading-edge flap and a leading-edge slat on the NACA 64A010
airfoil section; naca-tn-3220; Jun 1954
- C. C. Pappas; Measurement
of heat transfer in the turbulent boundary layer on a flat plate in a
supersonic flow and comparison with skin friction results; naca-tn-3222;
Jun 1954
- Joseph M. Spiegel,
Phillips J. Tunnell; An
analysis of shock-wave cancellation and reflection for porous walls which obey
an exponential mass-flow pressure-difference relation; naca-tn-3223; Aug
1954
- Duane W. Dugan, Katsumi
Hikido; Theoretical
investigation of the effects upon lift of a gap between wing and body of a
slender wing-body combination; naca-tn-3224; Aug 1954
- Walter G. Vincenti,
Duane W. Dugan, E. Ray Phelps; An
experimental study of the lift and pressure distribution on a double-wedge
profile at Mach numbers near shock attachment; naca-tn-3225; Jul
1954
- Arthur Wm. Rogers; Application of
two-dimensional vortex theory to the prediction of flow fields behind wings of
wing body combinations at subsonic and supersonic speeds; naca-tn-3227;
Sep 1954
- H. Clyde McLemore,
Michael D. Cannon; Aerodynamic
investigation of a four-blade propeller operating through an angle-of-attack
range from 0 to 180 degrees; naca-tn-3228; Jun 1954
- Carl Kaplan; The
small-disturbance method for flow of a compressible fluid with velocity
potential and stream function as independent variables; naca-tn-3229; Aug
1954
- K. R. Czarnecki, Ross
B. Robinson, John H. Hilton, Jr.; Investigation
of distributed surface roughness on a body of revolution at a Mach number of
1.61; naca-tn-3230; Jun 1954
- Aldie E. Johnson, Jr.;
Bending
tests on box beams having solid- and open-construction webs; naca-tn-3231;
Aug 1954
- Joseph W. Semonian,
Roger A. Anderson; An
analysis of the stability and ultimate bending strength of multiweb beams with
formed-channel webs; naca-tn-3232; Aug 1954
- Charles L. Shuford,
Jr.; A
review of planing theory and experiment with a theoretical study of
pure-planing lift of rectangular flat plates; naca-tn-3233; Aug
1954
- Robert D. Harrington;
Reduction of
helicopter parasite drag; naca-tn-3234; Aug 1954
- Walter B. Horne,
Bertrand H. Stephenson, Robert F. Smilely; Low
speed yawed-rolling and some other elastic characteristics of two
56-inch-diameter, 24-ply-rating aircraft tires; naca-tn-3235; Aug
1954
- Garland J. Morris,
Lindsay J. Lina; Description
and preliminary flight investigation of an instrument for detecting subnormal
acceleration; naca-tn-3252; Nov 1954
- George E. Glawe,
Charles E. Shepard; Some
effects of exposure to exhaust-gas streams on emittance and thermoelectric
power of bare-wire platinum rhodium - platinum thermocouples;
naca-tn-3253; Aug 1954
- Perry W. Kuhns; Determination
of flame temperatures from 2000 to 3000 K by microwave absorption;
naca-tn-3254; Aug 1954
- John R. Jack, Barry
Moskowitz; Experimental
investigation of temperature recovery factors on a 10 degree cone at angle of
attack at a Mach number of 3.12; naca-tn-3256; Jul 1954
- S. F. Murray, Robert L.
Johnson; Effects of
chemically active additives on boundary lubrication of steel by silicones;
naca-tn-3257; Aug 1954
- Rudolph C. Haefeli,
Harry Bernstein; Investigation
of Mach number changes obtained by discharging high-pressure pulse through
wind tunnel operating supersonically; naca-tn-3258; Aug 1954
- Milton G. Kofskey,
Hubert W. Allen; Smoke
study of nozzle secondary flows in a low-speed turbine; naca-tn-3260; Nov
1954
- Henry R. Hunczak,
Morris D. Rousso; Starting
and operating limits of two supersonic wind tunnels utilizing auxiliary air
injection downstream of the test section; naca-tn-3262; Sep 1954
- Alexander Mendelson,
Robert W. Carroll; Lift
and moment equations for oscillating airfoils in an infinite unstaggered
cascade; naca-tn-3263; Oct 1954
- Robert D. Ingebo; Vaporization
rates and drag coefficients for isooctane sprays in turbulent air streams;
naca-tn-3265; Oct 1954
- Paul F. Brinich; Boundary-layer
transition at Mach 3.12 with and without single roughness elements;
naca-tn-3267; Dec 1954
- H. W. Liepmann, G. T.
Skinner; Shearing-stress
measurements by use of a heated element; naca-tn-3268; Nov 1954
- E. C. Hartmann,
Marshall Holt, I. D. Eaton; Additional
static and fatigue tests of high-strength aluminum-alloy bolted joints;
naca-tn-3269; Jul 1954
- R. H. MacNeal; Electrical
analogies for stiffened shells with flexible rings; naca-tn-3280; Dec
1954
- Almer D. Crim; Gust
experience of a helicopter and an airplane in formation flight;
naca-tn-3354; Dec 1954
- W. S. Hyler, R. A.
Lewis, H. J. Grover; Experimental
investigation of notch-size effects on rotating-beam fatigue behavior of
75S-T6 aluminum alloy; naca-tn-3291; Nov 1954
- William H. Colner,
Howard T. Francis; Influence
of exposed area on stress-corrosion cracking of 24S aluminum alloy;
naca-tn-3292; Nov 1954
- Harold Mirels; Attenuation
in a shock tube due to unsteady-boundary-layer action; naca-tn-3278; Aug
1954
- Alvin Seiff; Examination
of the existing data on the heat transfer of turbulent boundary layers at
supersonic speeds from the point of view of Reynolds analogy;
naca-tn-3284; Aug 1954
- James A. Weiberg,
Robert E. Dannenberg; Section
characteristics of an NACA 0006 airfoil with area suction near the leading
edge; naca-tn-3285; Jan 1954
- Harvard Lomax, Franklyn
B. Fuller, Loma Sluder; Generalized
indicial forces on deforming rectangular wings in supersonic flight;
naca-tn-3286; Nov 1954
- Jackson R. Stalder,
Helmer V. Nielsen; Heat
transfer from a hemisphere-cylinder equipped with flow-separation spikes;
naca-tn-3287; Sep 1954
- Herbert C. Nelson, Ruby
A. Rainey; Comparison of
flutter calculations using various aerodynamic coefficients with experimental
results for some rectangular cantilever wings at Mach number 1.3;
naca-tn-3301; Nov 1954
- Charles H. McLellan,
Thomas W. Williams; Liquefaction
of air in the Langley 11-inch hypersonic tunnel; naca-tn-3302; Oct
1954
- Maurice J. Brevoort,
Bernard Rashis; Turbulent-heat-transfer
measurements at a Mach number of 3.03; naca-tn-3303; Sep 1954
- Milton D. Humphreys; An
investigation of a lifting 10-percent-thick symmetrical double-wedge airfoil
at mach number up to 1; naca-tn-3306; Nov 1954
- Richard E. Kuhn, John
W. Draper; An
investigation of a wing-propeller configuration employing large-chord plain
flaps and large-diameter propellers for low-speed flight and vertical
take-off; naca-tn-3307; Dec 1954
- S. A. Clevenson, E.
Widmayer, Jr., Franklin W. Diederich; An
exploratory investigation of some types of aeroelastic instability of open and
closed bodies of revolution mounted on slender struts; naca-tn-3308; Nov
1954
- Aldie E. Johnson, Jr.;
Mechanical
properties at room temperature of four cermets of tungsten carbide with cobalt
binder; naca-tn-3309; Dec 1954
- Eldon E. Mathauser; Investigation
of static strength and creep behavior of an aluminum-alloy multiweb box beam
at elevated temperatures; naca-tn-3310; Nov 1954
- W. J. Tuovila, John E.
Baker, Arthur A. Regier; Initial
experiments on flutter of unswept cantilever wings at Mach number 1.3;
naca-tn-3312; Nov 1954
- Robert G. Chilton; Some
measurements of atmosphere turbulence obtained from flow-direction vanes
mounted on an airplane; naca-tn-3313; Nov 1954
- Philip J. Hughes, John
E. Inge, Stanley B. Prosser; Tensile
and compressive stress-strain properties of some high-strength sheet alloys at
elevated temperatures; naca-tn-3315; Nov 1954
- Leslie W. Lassiter,
Robert H. Heikotter; Some
measurements of noise from three solid-fuel rocket engines; naca-tn-3316;
Dec 1954
- Warren A. Tucker; Design
considerations for wings having minimum drag due to lift; naca-tn-3317;
Dec 1954
- Morris W. Rubesin; An analytical
estimation of the effect of transpiration cooling on the heat-transfer and
skin-friction characteristics of a compressible, turbulent boundary layer;
naca-tn-3341; Dec 1954
- James R. Jedlicka, Max
E. Wilkins, Alvin Seiff; Experimental
determination of boundary-layer transition on a body of revolution at M =
3.5; naca-tn-3342; Oct 1954
- Milton D. Van Dyke; Subsonic edges
in thin-wing and slender-body theory; naca-tn-3343; Nov 1954
- Howard A. Stine, Kent
Wanlass; Theoretical and
experimental investigation of aerodynamic-heating and isothermal heat-transfer
parameters on a hemispherical nose with laminar boundary layer at supersonic
Mach numbers; naca-tn-3344; Dec 1954
- Henry C. Lessing,
Thomas B. Fryer, Merrill H. Mead; A
system for measuring the dynamic lateral stability derivatives in high-speed
wind tunnels; naca-tn-3348; Dec 1954
- W. A. Maxwell, E. M.
Grala; Investigation
of nickel-aluminum alloys containing from 14 to 34 percent aluminum;
naca-tn-3259; Aug 1954
- Peterson, Robert B; The effects of
circular end plates on the lift, drag, and pitching moment at subsonic and
supersonic speeds on a modified triangular wing having an aspect ratio of 2, a
taper ratio of 0.33, and a 45 degree swept leading edge; naca-rm-a53j14;
March 09, 1954
- Jedlicka, James R
Wilkins, Max E Seiff, Alvin; Experimental
determination of boundary-layer transition on a body of revolution at M =
3.5; naca-rm-a53l18; March 15, 1954
- Christensen, Frederik
B; An
experimental investigation of four triangular-wing-body combinations in
sideslip at Mach numbers 0.6, 0.9, 1.4, and 1.7; naca-rm-a53l22; March 15,
1954
- Heitmeyer, John C; Effect of nose
shape and trailing-edge bluntness on the aerodynamic characteristics of an
unswept wing of aspect ratio 3.1, taper ratio 0.4, and 3-percent
thickness; naca-rm-a54a04; March 15, 1954
- Katzen, Elliott D
Kuehn, Donald M Hill, William A , Jr; Investigation
of the effects of profile shape on the aerodynamic and structural
characteristics of thin, two-dimensional airfoils at supersonic speeds;
naca-rm-a54b08a; May 07, 1954
- Rosnikoff, Meyer M; Optimum lifting
bodies at high supersonic airspeeds; naca-rm-a54b15; May 07, 1954
- Boissevain, Alfred G;
Experimental
investigation of the damping in roll of cruciform triangular wing-body
combinations at Mach numbers from 1.5 to 6.0; naca-rm-a54b15a; April 07,
1954
- Kaattari, George E; Pressure
distributions on triangular and rectangular wings to high angles of attack
Mach numbers 1.45 and 1.97; naca-rm-a54d19; June 25, 1954
- Dennis, David H
Cunningham, Bernard E; Forces
and moments on inclined bodies at Mach numbers from 3.0 to 6.3;
naca-rm-a54e03; June 25, 1954
- Anderson, Warren E
Scherrer, Richard; Investigation
of a flow deflector and an auxiliary scoop for improving off-design
performance of nose inlets; naca-rm-a54e06; July 20, 1954
- White, Maurice D; A flight
investigation at transonic speeds of the aerodynamic characteristics of a
model having a thin unswept wing of aspect ratio 3.1; naca-rm-a54e12;
August 04, 1954
- Nelson, Warren H Frank,
Joseph L; The effect of
wing profile on the transonic characteristics of rectangular and triangular
wings having aspect ratios of 3 : transonic bump technique;
naca-rm-a54h12a; October 27, 1954
- Canning, Thomas N; Investigation
of the lift, center of pressure, and drag of a projectile at a Mach number of
8.6 and a Reynolds number of 17 million; naca-rm-a54h23a; November 19,
1954
- Holdaway, George H; A flight
investigation at transonic speeds and small angles of attack of the
aerodynamic characteristics of a model having a 45 degree sweptback wing of
aspect ratio 3 with an Naca 64A006 airfoil section; naca-rm-a54i17;
January 25, 1954
- Conners, James F
Woollett, Richard R; Force,
moment, and pressure characteristics of several annular nose inlets at Mach
number 3.85; naca-rm-e53j09; February 03, 1954
- Huntley, S C Yanowitz,
Herbert; Pumping and
thrust characteristics of several divergent cooling-air ejectors and
comparison of performance with conical and cylindrical ejectors;
naca-rm-e53j13; January 20, 1954
- Sivo, Joseph N Fenn,
David B; A
method of measuring jet thrust of turbojet engines in flight
installations; naca-rm-e53j15; January 21, 1954
- Rothenberg, Edward A
Ordin, Paul M; Preliminary
investigation of performance and starting characteristics of liquid fluorine :
liquid oxygen mixtures with jet fuel; naca-rm-e53j20; January 06,
1954
- Jack, John R Moskowitz,
Barry; Aerodynamics of
slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6)
to 15 x 10(exp 6) IV : aerodynamic characteristics of series of four bodies
having near-parabolic noses and cylindrical afterbodies; naca-rm-e53j27;
January 25, 1954
- Dangle, E E Friedman,
Robert Cervenka, Adolph J; Analytical
and experimental studies of a divided-flow ram-jet combustor;
naca-rm-e53k04; January 11, 1954
- Gibbs, James B; Starting
characteristics and combustion performance of magnesium slurry in
6.5-inch-diameter ram-jet engine mounted in connected-pipe facility;
naca-rm-e53k05; January 28, 1954
- North, Warren J; Summary of
free-flight performance of a series of ram-jet engines at Mach numbers from
0.80 to 2.20; naca-rm-e53k17; February 11, 1954
- Ziemer, Robert R
Schafer, Louis J JR Heaton, Thomas R; Performance
of two air-cooled turbojet engines determined analytically from engine
component performance for a range of cooling-air weight flows;
naca-rm-e53k19; February 17, 1954
- Witzke, Walter R Prok,
George M Walsh, Thomas J; A
preliminary study of the preparation of slurry fuels from vaporized
magnesium; naca-rm-e53k23; February 04, 1954
- Donoughe, Patrick L
Diaguila, Anthony J; Exploratory
engine test of transpiration-cooled turbine-rotor blade with wire-cloth
shell; naca-rm-e53k27; 1954
- Hamrick, Joseph T
Beede, William L Withee, Joseph R JR; Design
and test of mixed-flow impellers IV : experimental results for impeller models
MF-1 and MF-2 with changes in blade height; naca-rm-e53l02; February 11,
1954
- Jack, John R Moskowitz,
Barry; Aerodynamic
characteristics of two flat-bottomed bodies at Mach number of 3.12;
naca-rm-e53l11b; April 02, 1954
- Mckeown, A B Belles,
Frank E; Vapor pressures
and calculated heats of vaporization of concentrated nitric acid solutions in
the composition range 71 to 89 percent nitrogen dioxide, 1 to 10 percent
water, and in the temperature range 10 to 60 degrees C; naca-rm-e53l14;
February 05, 1954
- Farley, John M Welna,
Henry J; Investigation
of conical subsonic diffusers for ram-jet engines; naca-rm-e53l15; March
15, 1954
- Hearth, Donald P
Gorton, Gerald C; Investigation
of thrust and drag characteristics of a plug-type exhaust nozzle;
naca-rm-e53l16; February 19, 1954
- Maxwell, W A Gurnick, R
S Francisco, A C; Preliminary
investigation of the 'freeze-casting' method for forming refractory
powders; naca-rm-e53l21; March 09, 1954
- Schwenk, Francis C
Servory, George K Lewis, George W; Experimental
investigation of a transonic axial-flow-compressor rotor with
double-circular-arc airfoil blade sections I : design, over-all performance
and stall characteristics; naca-rm-e53l21a; April 05, 1954
- Shum, Eugene F Stepka,
Francis S; Analytical and
experimental investigation of a forced-convection air-cooled internal
strut-supported turbine blade; naca-rm-e53l22a; March 12, 1954
- Morse, C R Kemp, R H;
Evaluation
of a compressor bleed system for RIM cooling the turbine wheel of a turbojet
engine; naca-rm-e53l22b; March 22, 1954
- Fradenburgh, Evan A
Gorton, Gerald C Beke, Andrew; Thrust
characteristics of a series of convergent-divergent exhaust nozzles at
subsonic and supersonic flight speeds; naca-rm-e53l23; March 12,
1954
- Hearth, Donald P
Wilcox, Fred A; Thrust
and drag characteristics of a convergent-divergent nozzle with various exhaust
jet temperatures; naca-rm-e53l23b; March 11, 1954
- Stewart, Warner L Wong,
Robert Y Evans, David G; Design
and experimental investigation of transonic turbine with slight negative
reaction across rotor hub; naca-rm-e53l29a; March 12, 1954
- Rabb, Leonard Messing,
Wesley E; Force
measurements on cone-cylinder body of revolution with various nose and fin
configurations at Mach number 4.0; naca-rm-e53l29b; March 12, 1954
- Hunczak, Henry R; Pressure,
recovery and mass-flow performance of four annular nose inlets operating in
Mach number region of 3.1 and Reynolds number range of approximately 0.45 x
10(exp 6) to 2.20 x 10(exp 6); naca-rm-e54a07; March 26, 1954
- Seashore, Ferris, L
Hurrell, Herbert G; Starting
and performance characteristics of a large asymmetric supersonic free-jet
facility; naca-rm-e54a19; April 1954
- Male, Theodore
Kerslake, William R Tischler, Adelbert O; Photographic
study of rotary screaming and other oscillations in a rocket engine;
naca-rm-e54a29; 1954
- Moskowitz, Barry Jack,
John R; Aerodynamics of
slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6)
to 15 x 10(exp 6) V : aerodynamic load distributions for a series of four
boattailed bodies; naca-rm-e54b11; May 06, 1954
- Englert, Gerald W
Vargo, Donald J Cubbison, Robert W; Effect
of jet-nozzle-expansion ratio on drag of parabolic afterbodies;
naca-rm-e54b12; April 19, 1954
- Sterbentz, William H
Leissler, L Abbott; Investigation
of a translating-cone inlet at Mach numbers from 1.5 to 2.0;
naca-rm-e54b23; May 11, 1954
- Kremzier, Emil J
Campbell, Robert C; Angle-of-attack-supersonic
performance of a configuration consisting of a ramp-type scoop inlet located
either on top or bottom of a body of revolution; naca-rm-e54c09; May 13,
1954
- Douglass, Howard W; Experimental
performance of liquid fluorine-liquid ammonia propellant combination in
1000-pound-thrust rocket engines; naca-rm-e54c17; May 13, 1954
- Campbell, Robert C
Kremzier, Emil J; Performance
of wedge-type boundary layer diverters for side inlets at supersonic
speeds; naca-rm-e54c23; May 13, 1954
- Valerino, Alfred S; Jet effects on
pressure loading of all-movable horizontal stabilizer; naca-rm-e54c24;
October 10, 1954
- Reynolds, Thaine W
Male, Donald W; Effect
of immersed surfaces in combustion zone on efficiency and stability of 5-inch
diameter ram-jet combustor; naca-rm-e54c25; June 21, 1954
- Dangle, E E Cervenka, A
J Perchonok, Eugene; Effect
of mechanically induced sinusoidal air-foil oscillations on operation of a
ram-jet engine; naca-rm-e54d01; June 16, 1954
- Vargo, Donald J
Englert, Gerald W; Effect
of nozzle contour on drag of parabolic afterbodies; naca-rm-e54d02; June
21, 1954
- Reynolds, Thaine W
Haas, Donald P; Performance
of slurries of 50 percent boron in JP-4 fuel in 5-inch ram-jet burner;
naca-rm-e54d07; June 10, 1954
- Osborn, Walter M; Performance of
mixed-flow impeller, model MFI-1B, with diffuser vanes at equivalent impeller
speeds from 1100 to 1700 feet per second; naca-rm-e54d23; June 16,
1954
- Freche, John C
Mckinnon, Roy A; Design
and experimental investigation of light-weight bases for air-cooled turbine
rotor blades; naca-rm-e54e10; July 02, 1954
- Johnson, Harry W
Piercy, Thomas G; Effect
of wedge-type boundary-layer diverters on performance of half-conical side
inlets at Mach number 2.96; naca-rm-e54e20; August 1954
- Englert, Gerald W
Leissler, L Abbott; Preliminary
wind tunnel investigation of two types of jet-exit configurations for control
of aircraft; naca-rm-e54e27; August 06, 1954
- Goodman, Irving A Fenn,
Virginia O; Preparation and
properties of concentrated boronhydrocarbon slurry fuels; naca-rm-e54f18a;
August 06, 1954
- Harp, James L , Jr
Velie, Wallaace W Mallett, William; An
evaluation of turbojet engine thrust control by exhaust-nozzle-area modulation
and compressor-inlet throttling; naca-rm-e54f21; August 02, 1954
- Male, Theodore
Kerslake, William R; A
method for prevention of screaming in rocket engines; naca-rm-e54f28a;
August 19, 1954
- Henzel, James G Trout,
Arthur M; Altitude
investigation of 20-inch-diameter ram-jet engine with annular-piloted
combustor; naca-rm-e54g12; August 27, 1954
- Hearth, Donald P
Perchonok, Eugene; Performance
of a 16-inch ram-jet engine with a can-type combustor at Mach numbers of 1.5
to 2.16; naca-rm-e54g13; August 27, 1954
- Jones, Merle L Rabb,
Leonard Simpkins, Scott H; Drag
data for 16-inch-diameter ram-jet engine with double-cone inlet in free flight
at Mach numbers from 0.7 to 1.8; naca-rm-e54h02; October 25, 1954
- Gordon, Sanford
Wilkins, Roger L; Theoretical
maximum performance of liquid fluorine - liquid oxygen mixtures with JP-4 fuel
as rocket propellants; naca-rm-e54h09; October 11, 1954
- Vasu, G Wilcox, F A
Himmel, S C; Preliminary
report of experimental investigation of ram-jet controls and engine
dynamics; naca-rm-e54h10; October 25, 1954
- Wentworth, Carl B; Performance of
five low-temperature-ratio ram-jet combustors over range of simulated
altitudes; naca-rm-e54h13; November 1954
- Steffen, Fred W Krull,
H George Schmiedlin, Ralph F; Effect
of divergence angle on the internal performance characteristics of several
conical convergent-divergent nozzles.; naca-rm-e54h25; November 29,
1954
- Salmi, Reino J; Experimental
investigation of drag of afterbodies with exiting jet at high subsonic Mach
numbers; naca-rm-e54i13; November 29, 1954
- Leissler, L Abbott
Nettles, J Cary; Investigation
to Mach number 2.0 of shock-positioning control systems for a
variable-geometry inlet in combination with a J34 turbojet engine;
naca-rm-e54i27; December 20, 1954
- Seaberg, Ernest C
Geller, Edward S; Flight
investigation of the aerodynamic derivatives and performance of control
systems of two full-scale guided bombs; naca-rm-l53e22; June 17,
1954
- Arbic, Richard G
Gillespie, Warren, Jr; Summary
of rocket-model tests at zero lift of an arrow-wing missile configuration from
Mach numbers of 0.9 to 1.8; naca-rm-l53j02; January 14, 1954
- Wiley, Harleth G
Taylor, Robert T; Investigation
at transonic speeds of the lateral-control and hinge-moment characteristics of
a flap-type spoiler aileron on a 60 degree delta wing; naca-rm-l53j05;
January 11, 1954
- Burrows, Dale L Newman,
Ernest E; Wind-tunnel
tests of a model of a wingless fin-controlled missile to obtain static
stability and control characteristics through a range of Mach numbers from 0.5
to 0.88; naca-rm-l53j06; April 12, 1954
- Walters, Richard E; Application of
transonic area rule to a sharp-lipped ducted nacelle; naca-rm-l53j09b;
January 05, 1954
- Hammond, Alexander D
Graven, Jean C JR; The
twisting effect at transonic speeds of spoiler ailerons on a 45 degree
sweptback, aspect-ratio-4, tapered wing; naca-rm-l53k03a; January 07,
1954
- Sevier, John R , Jr; Effects of a
series of inboard plan-form modifications on the longitudinal characteristics
of two unswept wings of aspect ratio 3.5, taper ratio 0.2, and different
thickness distributions at Mach numbers of 1.61 and 2.01; naca-rm-l53k11;
February 05, 1954
- Love, Eugene S; A summary of
information on support interference at transonic and supersonic speeds;
naca-rm-l53k12; January 12, 1954
- Dettwyler, H Rudolph
Trout, Otto F JR; Flight
and preflight evaluation of an automatic thrust-coefficient control system in
a twin-engine ram-jet missile; naca-rm-l53k13; January 22, 1954
- Ikard, Wallace L; An
air-flow-direction pickup suitable for telemetering use on pilotless
Aircraft; naca-rm-l53k16; March 10, 1954
- Stoney, William E JR;
Transonic
drag measurements of eight body-nose shapes; naca-rm-l53k17; February 05,
1954
- Clevenson, Sherman A
Tomassoni, John E; Experimental
investigation of the oscillating forces and moments on a two-dimensional wing
equipped with an oscillating circular-arc spoiler; naca-rm-l53k18; January
12, 1954
- Church, James D; Flight
investigation of the rolling effectiveness of fingered semaphore spoilers on a
tapered 45 sweptback wing between Mach numbers 0.6 and 1.3;
naca-rm-l53k20; January 14, 1954
- Wiley, Harleth G Hayes,
William C JR; Wind-tunnel
investigation at low and transonic speeds of the feasibility of self-actuating
spoilers as a lateral-control device for a missile; naca-rm-l53k27;
January 28, 1954
- Chauvin, Leo T Maloney,
Joseph P; Experimental
convective heat transfer to a 4-inch and 6-inch hemisphere at Mach numbers
from 1.62 to 3.04; naca-rm-l53l08a; February 03, 1954
- Alford, William J , Jr
Pasteur, Thomas B , Jr; The
effects of changes in aspect ratio and tail height on the longitudinal
stability characteristics at high subsonic speeds of a model with a wing
having 32.6 degree sweepback; naca-rm-l53l09; February 02, 1954
- Strass, H Kurt; Summary of some
rocket-model investigations of effects of wing aspect ratio and thickness on
aileron rolling effectiveness including some effects of spanwise aileron
location for sweptback wings with aspect ratio of 8; naca-rm-l53l11;
February 17, 1954
- Schult, Eugene, D
Fields, E M; Free-flight
measurements of the rolling effectiveness and drag of trailing-edge spoilers
on a tapered sweptback wing at Mach numbers 0.6 and 1.4; naca-rm-l53l14a;
February 18, 1954
- Lord, Douglas R
Czarnecki, K R; Aerodynamic
characteristics of a full-span trailing-edge control on a 60 degree delta wing
with and without a spoiler at Mach number 1.61; naca-rm-l53l17; March 10,
1954
- Wiggins, James W; Wind-tunnel
investigation at high subsonic speeds to determine the rolling derivatives of
two wing-fuselage combinations having triangular wings, including a
semiempirical method of estimating the rolling derivatives;
naca-rm-l53l18a; February 08, 1954
- Stoney, William E
Sandahl, Carl A; Effect
of some section modifications and protuberances on the zero-lift drag of delta
wings at transonic and supersonic speeds; naca-rm-l53l24a; February 18,
1954
- Robinson, Harold L; Pressures and
associated aerodynamic and load characteristics for two bodies of revolution
at transonic speeds; naca-rm-l53l28a; March 11, 1954
- Kehlet, Alan B; Aerodynamic
characteristics at transonic and supersonic speeds of a rocket-propelled
airplane configuration having a 52.5 degree delta wing and a low, swept
horizontal tail; naca-rm-l54a20; March 29, 1954
- Silvers, H Norman King,
Thomas J , Jr; Wind-tunnel
investigation at high subsonic speeds of the effects of wing-mounted external
stores on the loading and aerodynamic characteristics in pitch of a 45 degree
sweptback wing combined with a fuselage; naca-rm-l54a21; March 23,
1954
- Thompson, Robert F; Hinge-moment,
lift, and pitching-moment characteristics of a flap-type control surface
having various hinge-line locations on a 4-percent-thick 60 degree delta wing
: transonic bump method; naca-rm-l54b08; March 24, 1954
- Henderson, James H
Swihart, John M Heiser, Gerald; Transonic
aerodynamic and loads characteristics of a 4-percent-thick
unswept-wing--fuselage combination; naca-rm-l54b24; May 24, 1954
- Kuehnel, Helmut A
Phillips, William H; Theoretical
investigation of some discontinuous yaw dampers; naca-rm-l54b24a; April
05, 1954
- Fournier, Paul G Few,
Albert G , Jr; Effects
of sweep and thickness on the static longitudinal aerodynamic characteristics
of a series of thin, low-aspect-ratio, highly tapered wings at transonic
speeds : transonic-bump method; naca-rm-l54b25; April 08, 1954
- Gillespie, Warren, Jr
Dietz, Albert E; Rocket-powered
model investigation of lift, drag, and stability of a body-tail configuration
at Mach numbers from 0.8 to 2.3 and angles of attack between plus or minus 6.5
degrees; naca-rm-l54c04; April 15, 1954
- Coletti, Donald E; Measurements
and predictions of flow conditions on a two-dimensional base separating a Mach
number 3.36 jet and a Mach number 1.55 outer stream; naca-rm-l54c08; May
07, 1954
- Church, James D; Rocket-powered-model
investigation of the hinge-moment and normal-force characteristics of a
half-diamond tip control on a 60 degree sweptback diamond wind between Mach
numbers of 0.5 and 1.3; naca-rm-l54c10; April 26, 1954
- De Moraes, Carlos A
Nowitzky, Albin M; Experimental
effects of propulsive jets and afterbody configurations on the zero-lift drag
of bodies of revolution at a Mach number of 1.59; naca-rm-l54c16; April
22, 1954
- Wiley, Harleth G; A wind-tunnel
investigation at high subsonic speeds of the lateral control characteristics
of various plain spoiler configurations on a 3-percent-thick 60 degree delta
wing; naca-rm-l54d01; May 26, 1954
- Maloney, Joseph P; Drag and heat
transfer on a parabolic body of revolution (NACA RM-10) in free flight to Mach
number 2 with both constant and varying Reynolds number and heating effects on
turbulent skin friction; naca-rm-l54d06; June 17, 1954
- Comenzo, Raymond J; A preliminary
investigation of the pressure recovery of several two-dimensional supersonic
inlets at Mach number of 2.01; naca-rm-l54d14; June 23, 1954
- Burrows, Dale L; Large-scale
low-speed wind-tunnel tests of a model having a 60 degree delta horizontal
canard control surface and wing to obtain static-longitudinal-stability and
canard surface hinge-moment data; naca-rm-l54d16a; June 17, 1954
- Lord, Douglas R
Czarnecki, K R; Aerodynamic
characteristics of several flap-type trailing-edge controls on a trapezoidal
wing at Mach numbers of 1.61 and 2.01; naca-rm-l54d19; June 14,
1954
- English, Roland D; Flight
investigation of an aileron and a spoiler on a wing of the X-3 airplane plan
form at Mach numbers from 0.5 to 1.6; naca-rm-l54d26a; June 18,
1954
- Demoraes, Carlos, A; Transonic
flight test of a rocket-powered model to determine propulsive jet influence on
the configuration drag; naca-rm-l54d27; June 18, 1954
- Gammal, Abraham A
Kennedy, Thomas L; Flight
investigation to determine lift and drag characteristics of a canard ram-jet
missile configuration in the Mach number range of 0.8 to 2.0;
naca-rm-l54d28; June 17, 1954
- D'Aiutolo, Charles T;
Low-amplitude
damping-in-pitch characteristics of tailless delta-wing-body combinations at
Mach numbers from 0.80 to 1.35 as obtained with rocket-powered models;
naca-rm-l54d29; June 24, 1954
- Ulmann, Edward F
Dunning, Robert W; Normal
force, center of pressure, and zero lift drag of several ballistic-type
missiles at Mach numbers of 4.05; naca-rm-l54d30a; July 06, 1954
- Grigsby, Carl E; An
investigation of the effects of jet exhaust and Reynolds number upon the flow
over the vertical stabilizer and rudder of the Douglas D-558-II research
airplane at Mach numbers of 1.62, 1.93, and 2.41; naca-rm-l54e03; June 17,
1954
- Bland, William M , Jr;
Effect of
wing flexibility on the damping roll of a notched delta-wing body combination
between Mach numbers 0.6 and approximately 2.2 as determined with
rocket-propelled models; naca-rm-l54e04; June 18, 1954
- Fletcher, Herman S; A wind-tunnel
investigation of the use of spoilers for obtaining static longitudinal
stability of a canard-missile model in reverse flight; naca-rm-l54e05;
June 21, 1954
- Kurbjun, Max C; Longitudinal
stability and drag characteristics of a fin stabilized body of revolution with
a fineness ratio of 12 as measured by the free-fall method;
naca-rm-l54e13; June 24, 1954
- Offenhartz, Edward; An experimental
investigation of two-dimensional, supersonic cascade-type inlets at a Mach
number of 3.11; naca-rm-l54e17; August 25, 1954
- Grigsby, Carl E; Investigation
of a canard missile configuration (NACA RM-4) in the Langley 9-inch supersonic
tunnel at Mach numbers of 1.62 and 1.93; naca-rm-l54e20; June 24,
1954
- Lord, Douglas R
Czarnecki, K R; Aerodynamic
characteristics of several tip controls on a 60 degree wing at a Mach number
of 1.61; naca-rm-l54e25; August 05, 1954
- Mathews, Charles W; Study of the
attack of an automatically controlled interceptor on a maneuvering bomber with
emphasis on proper coordination of lift-acceleration and roll-angle commands
during rolling maneuvers; naca-rm-l54e27; August 04, 1954
- Seaberg, Ernest C
Willoughby, William W Geller, Edward S; Theoretical
investigation based on experimental frequency-response measurements of an
automatic altitude control in combination with supersonic missile
configuration; naca-rm-l54f04; August 03, 1954
- Spearman, M Leroy
CORNELIUS DRIVER; Wind-tunnel
investigation at a Mach number of 2.01 of the aerodynamic characteristics in
combined pitch and sideslip of some canard-type missiles having cruciform
wings and canard surfaces with 70 degree delta plan forms; naca-rm-l54f09;
August 23, 1954
- Donlan, Charles J; An assessment
of the airplane drag problem at transonic and supersonic speeds;
naca-rm-l54f16; July 15, 1954
- Mclellan, Charles H; A method for
increasing the effectiveness of stabilizing surfaces at high supersonic Mach
numbers; naca-rm-l54f21; August 03, 1954
- Driver, Cornelius Lord,
Douglas R; Investigation
of the effect of balancing tabs on the hinge-moment characteristics of a
trailing-edge flap-type control on a trapezoidal wing at a Mach number of
1.61; naca-rm-l54f22; August 05, 1954
- Kell, Robert J
Hedgepeth, John M; Comparison
between theoretical and experimental rates of roll of two models with flexible
rectangular wings at supersonic speeds; naca-rm-l54f23; August 05,
1954
- Guy, Lawrence D; Effects of
overhang balance on the hinge-moment and effectiveness characteristics of an
unswept trailing-edge control on a 60 degree delta wing; naca-rm-l54g12a;
September 14, 1954
- Strass, H Kurt Tucker,
Warren A; Some effects of
aileron span, aileron chord, and wing twist on rolling effectiveness as
determined by rocket-powered model tests and theoretical estimates;
naca-rm-l54g13; September 14, 1954
- Spearman, M Leroy
Robinson, Ross B; Aerodynamic
characteristics at Mach number of 2.01 of two cruciform missile configurations
having 70 degree delta wings with length-diameter ratios of 14.8 and 17.7 with
several canard controls; naca-rm-l54g20; August 30, 1954
- Merlet, Charles, F
Putland, Leonard W; Flight
determination of the drag of conical-shock nose inlets with various cowling
shapes and axial positions of the center body at Mach numbers from 0.8 to
2.0; naca-rm-l54g21a; September 10, 1954
- Comenzo, Raymond J
Mackley, Ernest A; Effect
of yaw and angle of attack pressure recovery and mass-flow characteristics of
a rectangular supersonic scoop inlet at a Mach number of 2.71;
naca-rm-l54g22; September 10, 1954
- Kehlet, Alan B; Aerodynamic
characteristics at transonic and supersonic speeds of a rocket-propelled
airplane configuration having a diamond-plan-form wing of aspect ratio 3.08
and a low, swept horizontal tail; naca-rm-l54g27a; September 10,
1954
- Piland, Robert O; Drag
measurements on a 1/6-scale, finless, sting-mounted NACA RM-10 missile in
flight at Mach numbers from 1.1 to 4.04 showing some Reynolds number and
heating effects; naca-rm-l54h09; October 27, 1954
- Sleeman, William C ,
Jr; Experimental
investigation at high subsonic speeds to determine the rolling-stability
derivatives of three wing-fuselage configurations; naca-rm-l54h11; October
27, 1954
- Fetterman, David E
Ridyard, Herbert W; The
effect of a change in airfoil section on the hinge-moment characteristics of a
half-delta tip control with a 60 degree sweep angle at a Mach number of
6.9; naca-rm-l54h16a; October 15, 1954
- Schult, Eugene D; Free-flight
measurements of the rolling effectiveness and operating characteristics of a
bellows-actuated split-flap aileron on a 60 degree delta wing at Mach numbers
between 0.8 and 1.8; naca-rm-l54h17; October 18, 1954
- Spearman, M Leroy
Plazzo, Edward B; An
investigation of a supersonic aircraft configuration having a tapered wing
with circular-arc sections and 40 degree sweepback : aerodynamic
characteristics of the configuration equipped with a canard control surface at
a Mach number of 1.89; naca-rm-l54h19; October 18, 1954
- Wiley, Harleth G
Moseley, William C , Jr; An
investigation at high subsonic speeds of the pressure distributions on a 45
degree sweptback vertical tail in sideslip with and without a 45 degree
sweptback horizontal tail located on the fuselage center line;
naca-rm-l54h23; November 02, 1954
- Vitale, A James Mcfall,
John C , Jr; Longitudinal
stability characteristics at transonic speeds of a canard configuration having
a 45 degree sweptback wing of aspect ratio 6.0 and NACA 65A009 airfoil
section; naca-rm-l54i01; November 15, 1954
- Macauley, William D
Feller, William V; An
investigation of the characteristics of the NACA RM-10 (with and without fins)
in the Langley 11-inch hypersonic tunnel at a Mach number of 6.9;
naca-rm-l54i03; November 26, 1954
- Thompson, Robert F
Taylor, Robert T; Effect
of a wing leading-edge flap and chord-extension on the high subsonic control
characteristics of a spoiler-slot-deflector control located at two spanwise
positions; naca-rm-l54i09; November 19, 1954
- D'Aiutolo, Charles T;
Low-amplitude
damping-in pitch characteristics of four tailless swept wing-body combinations
at Mach numbers from 0.85 to 1.30 as obtained with rocket-powered models;
naca-rm-l54i10; November 24, 1954
- Bromm, August F
O'Donnell, Robert M; Investigation
at supersonic speeds of the effect of jet Mach number and divergence angle of
the nozzle upon the pressure of the base annulus of a body of revolution;
naca-rm-l54i16; December 17, 1954
- Hopko, Russell N; The effect of
some surface roughness elements on the drag of a body of revolution at
supersonic speeds; naca-rm-l54i21; November 24, 1954
- O'Donnell, Robert M
Mcdearmon, Russell W; Experimental
investigation of effects of primary jet flow and secondary flow through a
zero-length ejector on base and boattail pressures of a body of revolution at
free-stream Mach numbers of 1.62, 1.93, and 2.41; naca-rm-l54i22; December
06, 1954
- Piland, Robert O
Putland, Leonard W; Zero-lift
drag of several conical and blunt nose shapes obtained in free flight at Mach
numbers of 0.7 to 1.3; naca-rm-l54a27; March 23, 1954
- Amer, Kenneth B Gessow,
Alfred; Charts for
estimating tail-rotor contribution to helicopter directional stability and
control in low-speed flight; naca-tn-3156; May 1954
- (Author(s) Not
Available); Manual of the
ICAO standard atmosphere calculations by the NACA; naca-tn-3182; May
1954
- Lassiter, Leslie W
Hubbard, Harvey H; The
near noise field of static jets and some model studies of devices for noise
reduction; naca-tn-3187; July 1954
- Silsby, Norman S; Statistical
measurements of contact conditions of 478 transport-airplane landings during
routine daytime operations; naca-tn-3194; June 1954
- Mccomb, Harvey G , Jr;
Stress
distributions caused by three types of loading on a circular semimonocoque
cylinder with flexible rings; naca-tn-3199; September 1954
- Mccomb, Harvey G , Jr;
Stress
analysis of circular semimonocoque cylinders with cutouts by a perturbation
load technique; naca-tn-3200; September 1954
- Shinbrot, Marvin; On the analysis
of linear and nonlinear dynamical systems from transient-response data;
naca-tn-3288; December 1954
- Draper, John W Kuhn,
Richard E; Investigation
of the aerodynamic characteristics of a model wing-propeller combination and
of the wing and propeller separately at angles of attack up to 90 degrees;
naca-tn-3304; November 1954
- Eaton, I D (Aluminum
Company of America) Youra, John A (Aluminum Company of America); Additional
fatigue tests on effects of design details in 355-T6 sand-cast aluminum
alloy; naca-rm-53l22; March 10, 1954
- Wolock, I (National
Bureau of Standards) Sherman, M A (National Bureau of Standards) Axilrod, B M
(National Bureau of Standards); Effects
of molecular weight on crazing and tensile properties of polymethyl
methacrylate; naca-rm-54a04; February 17, 1954
- Black, John M (Forest
Products Laboratory) Blomquist, R F (Forest Products Laboratory.); Development
of metal-bonding adhesives with improved heat-resistant properties;
naca-rm-54d01; May 14, 1954
- Kistler, A L (Johns
Hopkins University) O'Brien, V (Johns Hopkins University) Corrsin, S (Johns
Hopkins University); Preliminary
measurements of turbulence and temperature fluctuations behind a heated
grid; naca-rm-54d19; June 10, 1954
- Wolock, Irvin (National
Bureau of Standards) George, Desmond A (National Bureau of Standards); Effects of
multiaxial stretching on crazing and other properties of transparent
plastics; naca-rm-54f22; October 20, 1954
- Sutton, Fred B Buell,
Donald A; The effect of
an operating propeller on the aerodynamic characteristics at high subsonic
speeds of a model of a vertical-rising airplane having an unswept wing of
aspect ratio 3; naca-rm-a52e06; November 15, 1954
- Bandettini, Angelo
Selan, Ralph; The
effects of horizontal-tail height and a partial-span leading-edge extension on
the static longitudinal stability of a wing-fuselage-tail combination having a
sweptback wing; naca-rm-a53j07; March 09, 1954
- Wetzel, Benton E Pfyl,
Frank A; Effects of
leading-edge chord extensions and an all-movable horizontal tail on the
aerodynamic characteristics of a wing-body combination employing a triangular
wing of aspect ratio 3 mounted in a high position at subsonic and supersonic
speeds; naca-rm-a53j14a; January 06, 1954
- Sutton, Fred B Demele,
Fred A; The
effects of operating propellers on the longitudinal characteristics at high
subsonic speeds of a four-engine tractor airplane configuration having a wing
with 40 degrees of sweepback and an aspect ratio of 10; naca-rm-a53j23;
January 07, 1954
- Ball, Louis H; Investigation
of a trailing-edge paddle-control surface on a triangular wing of aspect ratio
2 at subsonic and supersonic speeds; naca-rm-a53k20; February 02,
1954
- Coe, Charles F
Mellenthin, Jack A; Buffeting
forces on two-dimensional airfoils as affected by thickness and thickness
distribution; naca-rm-a53k24; February 04, 1954
- Nelson, Warren H; The transonic
characteristics of unswept wings having aspect ratios of 4, spanwise
variations in thickness ratio, and variations in plan-form taper-transonic
-bump technique; naca-rm-a53l17; March 12, 1954
- Boltz, Frederick W
Kolbe, Carl D; Effects
of operating propellers on the wing-surface pressures of a four-engine tractor
airplane configuration having a wing with 40 degrees of sweepback;
naca-rm-a53l29; April 23, 1954
- Reynolds, Robert M
Molk, Ashley J; Effects
of two spinner shapes on the pressure recovery in an NACA 1-series D-type cowl
behind a three-blade propeller at Mach numbers up to 0.80;
naca-rm-a53l29a; March 19, 1954
- Kelly, Mark W Tolhurst,
William H , Jr; The
use of area suction to increase the effectiveness of a trailing-edge flap on a
triangular wing of aspect ratio 2; naca-rm-a54a25; April 1954
- Herrera, Raymond
Barnes, Robert H; An
experimental investigation of the flutter of several wings of varying aspect
ratio, density, and thickness ratio at Mach numbers from 0.60 to 1.10;
naca-rm-a54a29; April 07, 1954
- Mossman, Emmet A
Anderson, Warren E; The
effect of lip shape on a nose-inlet installation at Mach numbers from 0 to 1.5
and a method for optimizing engine-inlet combinations; naca-rm-a54b08; May
07, 1954
- Koenig, David G; Tests in the
Ames 40- by 80-foot wind tunnel of the effects of varying wing modifications
on the longitudinal characteristics of two-triangular wing airplane models
with and without horizontal tails; naca-rm-a54b09; April 15, 1954
- Heitmeyer, John C; Effect of a
leading-edge flap upon the lift, drag, and pitching moment of an airplane
employing a thin, unswept wing; naca-rm-a54b16; October 20, 1954
- Cleary, Joseph W; The transonic
aerodynamic characteristics of structurally related wings of low aspect ratio
having a spanwise variation in thickness ratio-transonic bump technique;
naca-rm-a54b18; April 12, 1954
- Van Dyke, Rudolph D ,
Jr Matteson, Frederick H; Flight
investigation of the effects of a partial-span leading-edge chord extension on
the aerodynamic characteristics of a 35 degree swept-wing fighter
airplane; naca-rm-a54b26; April 23, 1954
- Neice, Stanford E; Experimental
investigation of the aerodynamic characteristics of a ballistic-type
missile; naca-rm-a54c04; April 23, 1954
- Demele, Fred A Otey,
William R; Investigation
of the normal force accompanying thrust-axis inclination of the NACA
1.167-(0)(03)-058 and the NACA 1.167-(0)(05)-058 three-blade propellers at
forward Mach numbers to 0.90; naca-rm-a54d22; June 23, 1954
- Maki, Ralph L Embry,
Ursel R; Effects of
high-lift devices and horizontal-tail location on the low-speed
characteristics of a large-scale 45 degree swept-wing airplane
configuration; naca-rm-a54e10; August 18, 1954
- Sutton, Fred B Dickson,
Jerald K; A
comparison of the longitudinal aerodynamic characteristics at mach numbers up
to 0.94 of swept back wings having NACA 4-digit or NACA 64A thickness
distributions; naca-rm-a54f18; August 23, 1954
- Mcfadden, Norman M
Heinle, Donovan R; Flight
investigation of the effects of horizontal-tail height, moment of inertia, and
control effectiveness on the pitch-up characteristics of a 35 degree
swept-wing fighter airplane at high subsonic speeds; naca-rm-a54f21;
January 18, 1954
- Holdaway, George H; An experimental
investigation of reduction in transonic drag rise at zero lift by the addition
of volume to the fuselage of a wing-body-tail configuration and a comparison
with theory; naca-rm-a54f22; August 18, 1954
- Reynolds, Robert M
Walker, John H; Investigation
of the NACA 4-(5)(05)-037 six- and eight-blade, dual-rotation propellers at
positive and negative thrust at Mach numbers up to 0.90, including some
aerodynamic characteristics of the NACA 4-(5)(05)-041 two- and four-blade,
single-rotat; naca-rm-a54g13; October 08, 1954
- Sammonds, Robert I
Reynolds, Robert M; Effect
of rotation of a NACA 1-series E-type cowling on the internal flow and force
characteristics of the cowling at Mach numbers up to 0.84 and at an angle of
attack of 0 degrees; naca-rm-a54g14; October 27, 1954
- Wyss, John A Herrera,
Raymond; Effects of
angle of attack and airfoil profile on the two-dimensional flutter derivatives
for airfoils oscillating in pitch at high subsonic speeds; naca-rm-a54h12;
October 15, 1954
- Franks, Ralph W; Tests in the
Ames 40- by 80-foot wind tunnel of the aerodynamic characteristics of airplane
models with plain spoiler ailerons; naca-rm-a54h26; December 06,
1954
- Franks, Ralph W; The application
of a simplified lifting-surface theory to the prediction of the rolling
effectiveness of plain spoiler ailerons at subsonic speeds;
naca-rm-a54h26a; December 06, 1954
- Spahr, J Richard; Longitudinal
aerodynamic characteristics to large angles of attack of a cruciform missile
configuration at a Mach number of 2; naca-rm-a54h27; December 06,
1954
- Cook, Woodrow L
Griffin, Roy N JR Hickey, David H; A
preliminary investigation of the use of circulation control to increase the
lift of a 45 degree sweptback wing by suction through trailing-edge slots;
naca-rm-a54i21; December 14, 1954
- Monfort, James C Wyss,
John A; Effects of
rigid spoilers on the two-dimensional flutter derivatives of airfoils
oscillating in pitch at high subsonic speeds; naca-rm-a54i22; December 17,
1954
- Abramovitz, Marvin Van
Dyke, Rudolph D , Jr; The
effect of stick-force gradient and stick gearing on the tracking accuracy of a
fighter airplane; naca-rm-a54i28; December 17, 1954
- Gillespie, Warren, Jr;
Free-flight
determination of force and stability characteristics of an inclined body of
fineness ratio 16.9 at a Mach number of 1.74; naca-rm-l54g28a; November
15, 1954
- Aladyev, I. T.; Experimental
determination of local and mean coefficients of heat transfer for turbulent
flow in pipes; naca-tm-1356; 1954
- Ferrari, Carlo.; On the
determination of certain basic types of supersonic flow fields;
naca-tm-1381; 1954
- Loposer, J. Dan,
Rumsey, Charles B.; Flight
measurements of average skin-friction coefficients on a parabolic body of
revolution (NACA-RM-10) at mach numbers from 1.0 to 3.7; naca-rm-l54g14;
1954
- Stiver, Louis S. Jr.;
Effects of
subsonic Mach number on the forces and pressure distributions on four NACA
64a-series airfoil sections at angles of attack as high as 28 degrees;
naca-tn-3162; 1954
- McCafferty, Richard J.;
Performance
comparisons of Navy jet mix and MIL-F-5624A (JP-3) fuels in tubular and
annular combustors / Richard J. McCafferty; naca-rm-e51j17; 1954
- Nussdorfer, Theodore
J.; Some
observations of shock-induced turbulent separation on supersonic
diffusers; naca-rm-e51l26; 1954
- Reynolds, Robert M.,
Kenyon, George C.; Investigation
of a three-blade propeller in combination with two different spinners and an
NACA D-type cowl at Mach numbers up to 0.80; naca-rm-a54b18a; 1954
- Wyss, John A., Monfort,
James C.; Effects of
airfoil profile on the two-dimensional flutter derivatives for wings
oscillating in pitch at high subsonic speeds; naca-rm-a54c24; 1954
- Rogallo, Vernon L.,
McCloud, John L., Yaggy, Paul F.; Note
on the effects of first-order aerodynamic loads on propeller shaft loads with
emphasis on counterrotating propellers; naca-rm-a54c30; 1954
- Sadoff, Melvin.,
Matterson, Frederick H., Van Dyke, Rudolph D. Jr.; The
effect of blunt-trailing-edge modifications on the high-speed stability and
control characteristics of a swept-wing fighter airplane; naca-rm-a54c31;
1954
- Smith, Willard G.; Wind-tunnel
investigation at subsonic and supersonic speeds of a fighter model employing a
low-aspect-ratio unswept wing and a horizontal tail mounted well above the
wing plane - longitudinal stability and control; naca-rm-a54d05;
1954
- Niewald, Roy J.,
Brewer, Jack D.; Bibliography
of NACA reports related to aircraft control and guidance systems January 1949
- April 1954; naca-rm-54f01; 1954
- B.M. Axilrod, J.E.
Wier, and J. Mandel (National Bureau of Standards); Effects
of Resin Coating Methods and Other Variables on Physical Properties of
Glass-Fabric Reinforce Polyesters; naca-rm-54g26; 1954
- William R. Winbrow
(Ames Aeroanutical Laboratory, Moffett Field Calif.); Effects
of Base Bleed on the Base Pressure of Blunt-Trailing Edge Airfoils at
Supersonic Speeds; naca-rm-a54a07; 1954
- Joseph H. Judd (Langley
Aeronautical Laboratory, Langley Field, Va.); Flight
Investigation of Engine Nacelles and Wing Vertical Position on the Drag of a
Delta-Wing Airplane Configuration from Mach Number 0.8 to 2.0;
naca-rm-l53l21; 1954
- Anatol Roshko; On
the Development of Turbulent Wakes from Vortex Streets; naca-report-1191;
1954
- Don D. Davis, Jr.,
George M. Stokes, Dewey Moore, George L. Stevens, Jr.; Theoretical
and Experimental Investigation of Mufflers with Comment on Engine-Exhaust
Muffler Design; naca-report-1192; 1954
- Robert G. Deissler; Analysis of
turbulent heat transfer, mass transfer, and friction in smooth tubes at high
Prandtl and Schmidt numbers; naca-report-1210; 1955
- E. R. G. Eckert, A. J.
Diaguila; Experimental
investigation of free-convection heat transfer in vertical tube at large
Grashof numbers; naca-report-1211; 1955
- George J. Pack, W. E.
Phillips, Jr.; Analog
study of interacting and noninteracting multiple-loop control systems for
turbojet engines; naca-report-1212; 1955
- Hermon M. Parker; Minimum-drag
ducted and pointed bodies of revolution based on linearized supersonic
theory; naca-report-1213; 1955
- Norman S. Silsby; Statistical
measurements of contact conditions of 478 transport-airplane landings during
routine daytime operations; naca-report-1214; 1955
- R. J. Brun, W. Lewis,
P. L. Perkins, J. S. Serafin; Impingement
of cloud droplets on a cylinder and procedure for measuring liquid-water
content and droplet sizes in supercooled clouds by rotating multicylinder
method; naca-report-1215; 1955
- Kenneth B. Amer, Alfred
Gessow; Charts for
estimating tail-rotor contribution to helicopter directional stability and
control in low-speed flight; naca-report-1216; 1955
- John R. Spreiter,
Alberta Alksne; Theoretical
prediction of pressure distributions on nonlifting airfoils at high subsonic
speeds; naca-report-1217; 1955
- G. Chester Furlong,
Thomas V. Bollech; Effect
of ground interference on the aerodynamic and flow characteristics of a 42
degree sweptback wing at Reynolds numbers up to 6.8 x 10(6);
naca-report-1218; 1955
- Wilber B. Huston, T. H.
Skopinski; Measurement and
analysis of wing and tail buffeting loads on a fighter airplane;
naca-report-1219; 1955
- E. R. G. Eckert, J. N.
B. Livingood; Calculations
of laminar heat transfer around cylinders of arbitrary cross section and
transpiration-cooled walls with application to turbine blade cooling;
naca-report-1220; 1955
- Clarence W. Matthews;
Theoretical
study of the tunnel-boundary lift interference due to slotted walls in the
presence of the trailing-vortex system of a lifting model;
naca-report-1221; 1955
- Alvin Seiff; A
free-flight wind tunnel for aerodynamic testing at hypersonic speeds;
naca-report-1222; 1955
- A. F. Lietzke; Theoretical
and experimental investigation of heat transfer by laminar natural convection
between parallel plates; naca-report-1223; 1955
- Alex Goodman, David T.
Thomas, Jr.; Effects of wing
position and fuselage size on the low-speed static rolling stability
characteristics of a delta-wing model; naca-report-1224; 1955
- James J. Donegan,
Samuel W. Robinson, Jr., Ordway B. Gates, Jr.; Determination
of lateral-stability derivatives and transfer-function coefficients from
frequency-response data for lateral motions; naca-report-1225; 1955
- Warren A. Tucker; A method for
the design of sweptback wings warped to produce specified flight
characteristics at supersonic speeds; naca-report-1226; 1955
- James J. Gallagher,
James N. Mueller; An
investigation of the maximum lift of wings at supersonic speeds;
naca-report-1227; 1955
- Franklin W. Diederich,
Martin Zlotnick; Calculated
spanwise lift distributions, influence functions, and influence coefficients
for unswept wings in subsonic flow; naca-report-1228; 1955
- Patrick L. Donoughe,
John N. B. Livingood; Exact
solutions of laminar-boundary-layer equations with constant property values
for porous wall with variable temperaturE; naca-report-1229; 1955
- Harvard Lomax, Franklyn
B. Fuller, Loma Sluder; Generalized
indical forces on deforming rectangular wings in supersonic flight;
naca-report-1230; 1955
- Ray H. Wright, Vernon
G. Ward; NACA transonic
wind-tunnel test sections; naca-report-1231; 1955
- Kenneth L. Wadlin,
Charles L. Shuford, Jr., John McGehee; A
theoretical and experimental investigation of the lift and drag
characteristics of hydrofoils at subcritical and supercritical speeds;
naca-report-1232; 1955
- H. S. Ribner; Shock-turbulence
interaction and the generation of noise; naca-report-1233; 1955
- Charles E. Watkins,
Harry L. Runyan, Donald S. Woolston; On
the Kernel function of the integral equation relating the lift and downwash
distributions of oscillating finite wings in subsonic flow;
naca-report-1234; 1955
- ; Standard
atmosphere - tables and data for altitudes to 65,800 feet;
naca-report-1235; 1955
- Morris D. Friedman,
Doris Cohn; Arrangement of
fusiform bodies to reduce the wave drag at supersonic speeds;
naca-report-1236; 1955
- Seth B. Anderson,
Richard S. Bray; A
flight evaluation of the longitudinal stability characteristics associated
with the pitch-up of a swept-wing airplane in maneuvering flight at transonic
speeds; naca-report-1237; 1955
- Eugene S. Love; Investigations
at supersonic speeds of 22 triangular wings representing two airfoil sections
for each of 11 apex angles; naca-report-1238; 1955
- Thomas C. O'Bryan,
Edward C. B. Danforth, J. Ford Johnston; Error
in airspeed measurement due to the static-pressure field ahead of an airplane
at transonic speeds; naca-report-1239; 1955
- K. R. Czarnecki,
Archibald R. Sinclair; An
investigation of the effects of heat transfer on boundary-layer transition on
a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61;
naca-report-1240; 1955
- Howard J. Curfman, Jr.;
Theoretical
and analog studies of the effects of nonlinear stability derivatives on the
longitudinal motions of an aircraft in response to step control deflections
and to the influence of proportional automatic control; naca-report-1241;
1955
- George E. Solomon; Transonic flow
past cone cylinders; naca-report-1242; 1955
- George C. Towe, Henry
J. Gomberg, J. W. Freemen; High-resolution
autoradiography; naca-report-1243; 1955
- Stanley Corrsin, Alan
L. Kistler; Free-stream
boundaries of turbulent flows; naca-report-1244; 1955
- Morris Morduchow; Analysis and
calculation by integral methods of laminar compressible boundary-layer with
heat transfer and with and without pressure gradient; naca-report-1245;
1955
- Kenneth L. Wadlin, John
A. Ramsen, Victor L. Vaughn, Jr.; The
hydrodynamic characteristics of modified rectangular flat plates having aspect
ratios of 1.00, 0.25, and 0.125 and operating near a free water surface;
naca-report-1246; 1955
- P. S. Klebanoff; Characteristics
of turbulence in boundary layer with zero pressure gradient;
naca-report-1247; 1955
- Benjamin Milwitzky,
Dean C. Lindquist, Dexter M. Potter; An
experimental study of applied ground loads in landing; naca-report-1248;
1955
- A. J. Eggers, Jr.,
Raymond C. Savin; A
unified two-dimensional approach to the calculation of three-dimensional
hypersonic flows, with application to bodies of revolution;
naca-report-1249; 1955
- William C. Triplett,
Stuart C. Brown, G. Allan Smith; The
dynamic-response characteristics of a 35 degree swept-wing airplane as
determined from flight measurements; naca-report-1250; 1955
- Harvey G. McComb, Jr.;
Stress
analysis of circular semimonocoque cylinders with cutouts;
naca-report-1251; 1955
- Jack N. Nielsen; Quasi-cylindrical
theory of wing-body interference at supersonic speeds and comparison with
experiment; naca-report-1252; 1955
- John B. McDevitt; A correlation
by means of transonic similarity rules of experimentally determined
characteristics of a series of symmetrical and cambered wings of rectangular
plan form; naca-report-1253; 1955
- Jack D. Brewer; Description and
bibliography of NACA research on wing controls - January 1946 - February
1955; naca-rm-54k24; Mar 1955
- Joseph W. Semonian,
James P. Peterson; An
analysis of the stability and ultimate compressive strength of short
sheet-stringer panels with special reference to the influence of the riveted
connection between sheet and stringer; naca-report-1255; Jan 1955
- Ivan E. Beckwith, John
A. Moore; An
accurate and rapid method for the design of supersonic nozzles;
naca-tn-3322; Feb 1955
- Allen R. Vick, Paul E.
Dewey; An
investigation of the discharge and drag characteristics of auxiliary-air
outlets discharging into a transonic stream; naca-tn-3466; Jul 1955
- Paul E. Dewey; A
preliminary investigation of aerodynamic characteristics of small inclined air
outlets at transonic Mach numbers; naca-tn-3442; May 1955
- William H. Sterbentz,
John C. Evvard; Criterions
for prediction and control of ram-jet flow pulsations; naca-tn-3506; Aug
1955
- Virgil A. Sandborn; Study of the
momentum distribution of turbulent boundary layers in adverse pressure
gradients; naca-tn-3264; Jan 1955
- Virgil A. Sandborn; Experimental
evaluation of momentum terms in turbulent pipe flow; naca-tn-3266; Jan
1955
- Harold W. Woolley; Effect of
dissociation on thermodynamic properties of pure diatomic gases;
naca-tn-3270; Apr 1955
- M. Metzger, J.
Intrater; Intergranular
corrosion of high-purity aluminum in hydrochloric acid II : grain-boundary
segregation of impurity atoms; naca-tn-3282; Apr 1955
- F. S. Sherman; A
low-density wind-tunnel study of shock-wave structure and relaxation phenomena
in gases; naca-tn-3298; Jul 1955
- H. J. Cunningham, R. R.
Lundstrom; Description and
analysis of a rocket-vehicle experiment on flutter involving wing deformation
and body motions; naca-tn-3311; Jan 1955
- William M. Bland, Jr.,
Carl A. Sandhal; A
technique utilizing rocket-propelled test vehicles for the measurement of the
damping in roll of sting-mounted models and some initial results for delta and
unswept tapered wings; naca-tn-3314; May 1955
- John DeYoung, Walter H.
Barling, Jr.; Prediction
of downwash behind swept-wing airplanes at subsonic speed; naca-tn-3346;
Jan 1955
- Raymond C. Savin; Application of
the generalized shock-expansion method to inclined bodies of revolution
traveling at high supersonic airspeeds; naca-tn-3349; Apr 1955
- A. C. Charters; The linearized
equations of motion underlying the dynamic stability of aircraft, spinning
projectiles, and symmetrical missiles; naca-tn-3350; Jan 1955
- R. D. Johnson, A. P.
Young, A. D. Schwope; Plastic
deformation of aluminum single crystals at elevated temperatures;
naca-tn-3351; Apr 1955
- G. B. Dubois, F. W.
Ocvirk, R. L. Wehe; Experimental
investigation of misaligning couples and eccentricity at ends of misaligned
plain bearings; naca-tn-3352; Feb 1955
- James R. Reese, John L.
Sewall; Effective
moment of inertia of fluid in offset, inclined, and swept-wing tanks
undergoing pitching oscillations; naca-tn-3353; Jan 1955
- James P. Trant, Jr.; Preliminary
investigation of a stick shaker as a lift-margin indicator; naca-tn-3355;
Feb 1955
- J. Mayers, Bernard
Budiansky; Analysis of
behavior of simply supported flat plates compressed beyond the buckling load
into the plastic range; naca-tn-3368; Feb 1955
- Conrad Rennemann, Jr.;
Minimum-drag
bodies of revolution in a nonuniform supersonic flow field; naca-tn-3369;
Feb 1955
- John M. Hedgepeth, Paul
G. Waner, Jr., Robert J. Kell; A
simplified method for calculating aeroelastic effects on the roll of
aircraft; naca-tn-3370; Mar 1955
- Robert F. Peck; Flight
measurements of base pressure on bodies of revolution with and without
simulated rocket chambers; naca-tn-3372; Apr 1955
- Kenneth Margolis; Theoretical
calculations of the pressures, forces, and moments due to various lateral
motions acting on thin isolated vertical tails with supersonic leading and
trailing edges; naca-tn-3373; Mar 1955
- Maurice J. Brevoort,
Bernard Rashis; Turbulent-heat-transfer
measurements at a Mach number of 2.06; naca-tn-3374; Mar 1955
- Robert L. Trimpi,
Nathaniel B. Cohen; A
theory for predicting the flow of real gases in shock tubes with experimental
verification; naca-tn-3375; Mar 1955
- James H. Walls; An experimental
study of orifice coefficients, internal strut pressures, and loads on a small
oleo-pneumatic shock strut; naca-tn-3426; Apr 1955
- Keith C. Harder, Conrad
Rennemann, Jr.; On
boattail bodies revolution having minimum wave drag; naca-tn-3478; Aug
1955
- William S. Aiken,
Bernard Wiener; Analysis
of the horizontal-tail loads measured in flight on a multiengine jet
bomber; naca-tn-3479; Sep 1955
- James J. Kramer, John
D. Stanitz; Prediction of
losses induced by angle of attack in cascades of sharp-nosed blades for
incompressible and subsonic compressible flow; naca-tn-3149; Jan
1955
- Kaattari, George E; Pressure
distributions on triangular and rectangular wings to high angles of attack
Mach numbers 2.46 and 3.36; naca-rm-a54j12; January 18, 1955
- Eggers, A J , Jr
Hermach, C A; Initial
experiments on the aerodynamic cooling associated with large-scale vortical
motions in supersonic flow; naca-rm-a54l13; March 08, 1955
- Mellenthin, Jack A; The effect of a
4-percent-high spoiler on buffeting forces on a naca 65(sub 06)A004
two-dimensional airfoil at subsonic Mach numbers; naca-rm-a54l22; March
23, 1955
- Bright, Loren G; A flight
investigation at transonic speeds of a model having a triangular wing of
aspect ratio 4; naca-rm-a54l27; March 24, 1955
- Hunton, Lynn W; A study of the
application of airfoil section data to the estimation of the
high-subsonic-speed characteristics of swept wings; naca-rm-a55c23; June
24, 1955
- Delany, Noel K; Exploratory
investigation of the low-speed static stability of a configuration employing
three identical triangular wing panels and a body of equal length;
naca-rm-a55c28; April 29, 1955
- Dugan, Duane W; Experimental
investigation of some aerodynamic effects of a gap between wing and body of a
moderately slender wing-body combination at a Mach number of 1.4;
naca-rm-a55d08; May 27, 1955
- Kaattari, George E
Hill, William A , Jr Nielsen, Jack N; Controls
for supersonic missiles; naca-rm-a55d12; May 27, 1955
- Triplett, William C; Considerations
involved in the design of a roll-angle computer for a bank-to-turn
interceptor; naca-rm-a55d18a; June 1955
- Eggers, A J , Jr
Hansen, Frederick Cunningham, Bernard E; Theoretical
and experimental investigation of the effect of yaw on heat transfer to
circular cylinders in hypersonic flow; naca-rm-a55e02; July 25,
1955
- Katzen, Elliott D
Pitts, William C; Load
distributions on wings and wing-body combinations at high angles of attack and
supersonic speeds; naca-rm-a55e17; July 21, 1955
- Seiff, Alvin Allen, H
Julian; Some
aspects of the design of hypersonic boost-glide aircraft; naca-rm-a55e26;
August 15, 1955
- Jorgensen, Leland H
Perkins, Edward W; Investigation
of some wake vortex characteristics of an inclined ogive-cylinder body at Mach
number 1.98; naca-rm-a55e31; August 23, 1955
- Reese, David E , Jr; An experimental
investigation of the unsteady lift induced on a wing in the downwash field of
an oscillating canard control surface; naca-rm-a55f01; August 15,
1955
- Canning, Thomas N
Derose, Charles E; Drag
and rolling-moment effectiveness of trailing-edge spoilers at Mach numbers 2.2
and 5.0; naca-rm-a55f15; October 03, 1955
- Eggers, A J , Jr; A discussion of
methods for reducing aerodynamic heating in supersonic flight;
naca-rm-a55f21a; September 1955
- Pfyl, Frank A; An
investigation of the effects of nose and lip shapes for an underslung scoop
inlet at Mach numbers from 0 to 1.9; naca-rm-a55g13; November 18,
1955
- Reller, John O Hamaker,
Frank M; Temperature
recovery factors on a slender 12 degree cone-cylinder at Mach numbers from 3.0
to 6.3 and angles of attack up to 45 degrees; naca-rm-a55g20; October 03,
1955
- Dennis, David H
Syvertson, Clarence A; Effects
of boundary-layer separation on normal force and center of pressure of a
cone-cylinder model with a large base flare at Mach numbers from 3.00 to
6.28; naca-rm-a55h09; October 03, 1955
- Eggers, A J , Jr; A method for
simulating the atmospheric entry of long-range ballistic missiles;
naca-rm-a55i15; December 28, 1955
- Rubesin, Morris W
Pappas, Constantine C Okuno, Arthur F; The
effect of fluid injection on the compressible turbulent boundary layer :
preliminary tests on transpiration cooling of a flat plate;
naca-rm-a55i19; December 21, 1955
- Reese, David E JR
Carlson, William C A; An
experimental investigation of the hinge-moment characteristics of a
constant-chord control surface oscillating at high frequency;
naca-rm-a55j24; December 1955
- Conrad, E William; Preliminary
analysis of performance of turbojet engines used as pumps for boundary-layer
control; naca-rm-e55e20a; August 16, 1955
- Childs, J Howard
Friedman, Robert Kochendorfer, Fred D Lubick, Robert J; Stall
and flame-out resulting from firing of armament; naca-rm-e55e25; August
05, 1955
- Dorsch, Robert G
Serafini, John S Fletcher, Edward A; A
preliminary investigation of static-pressure changes associated with
combustion of aluminum borohydride in a supersonic wind tunnel;
naca-rm-e55f07; August 18, 1955
- Henzel, James G , Jr
Mcardle, Jack G; Preliminary
performance data of several tail-pipe-cascade-type model thrust reversers;
naca-rm-e55f09; August 29, 1955
- Hurrell, Herbert G
Vasu, George Dunbar, William R; Experimental
study of shock-positioning method of ram-jet-engine control;
naca-rm-e55f21; August 29, 1955
- Reynolds, T W; Aircraft-fuel-tank
design for liquid hydrogen; naca-rm-e55f22; August 09, 1955
- Smith, Kenneth J
Osborn, Walter M; Design
and test of mixed-flow impellers VI : performance and parabolic-bladed
impeller with shroud redesigned by rapid approximate method;
naca-rm-e55f23; September 07, 1955
- Piercy, Thomas G Klann,
John L; Experimental
investigation of methods of improving diffuser-exit total-pressure profiles
for side-inlet model at Mach number 3.05; naca-rm-e55f24; August 29,
1955
- Rabb, Leonard
Simpkinson, Scott H; Free-flight
heat-transfer measurements on two 20 degree-cone-cylinders at Mach numbers
from 1.3 to 4.9; naca-rm-e55f27; July 18, 1955
- Perkins, Porter J; Statistical
survey of icing data measured on scheduled airline flights over the United
States and Canada from November 1951 to June 1952; naca-rm-e55f28a;
September 08, 1955
- Conners, James F Meyer,
Rudolph C; Performance
characteristics of axisymmetric two-cone and isentropic nose inlets at Mach
number 1.90; naca-rm-e55f29; December 07, 1955
- Englert, Gerald W
Wasserbauer, Joseph F Whalen, Paul; Interaction
of a jet and flat plate located in an airstream; naca-rm-e55g19; September
08, 1955
- Altschuller, Aubrey P;
Calculated
heats of formation and combustion of boron compounds (boron, hydrogen, carbon,
silicon); naca-rm-e55g26; October 04, 1955
- Esgar, Jack B Ziemer,
Robert R; Review of
status, methods and potentials of gas-turbine air-cooling; naca-rm-e54i23;
February 23, 1955
- Piercy, Thomas G; Preliminary
investigation of some internal boundary-layer-control systems on a side inlet
at Mach number 2.96; naca-rm-e54k01; February 18, 1955
- Foster, Hampton H
Fletcher, Edward A Straight, David M; Aluminum
borohydride - hydrocarbon mixtures as a source of ignition for a turbojet
combustor; naca-rm-e54k12; February 23, 1955
- Morgan, W C Kemp, R H;
An
experimental evaluation of several design variations of hollow turbine blades
for expendable engine application; naca-rm-e54k23; February 23,
1955
- Harry, David P , III
Lubick, Robert J; Inlet-air
distortion effects on stall, surge, and acceleration margin of a turbojet
engine equipped with variable compressor inlet guide vanes;
naca-rm-e54k26; October 04, 1955
- Steffen, Fred W Krull,
H George Schmiedlin, Ralph F; Effects
of several geometric variables on internal performance of short
convergent-divergent exhaust nozzles; naca-rm-e54l09; February 18,
1955
- Baughman, L Eugene; Wind-tunnel
investigation at Mach 1.9 of multijet-missile base pressures;
naca-rm-e54l14; March 1955
- Wise, G A Campbell, R
C; Investigation
of a ramp-type inlet designed for improved angle-of-attack performance at Mach
number 2.0; naca-rm-e54l17; February 23, 1955
- Wilcox, Fred A Hearth,
Donald P; Application of
oblique-shock sensing system to ram-jet-engine flight Mach number control;
naca-rm-e54l22a; March 03, 1955
- Morris, James F Caves,
Robert M Lord, Albert M; Blow-out
velocities of several slurry and liquid fuels in a 1 7/8 inch-diameter
combustor; naca-rm-e54l27a; February 23, 1955
- Olson, Walter T
Breitwieser, Roland; NACA
research on slurry fuels through 1954; naca-rm-e55b14; April 21,
1955
- Kerslake, William R
Dangle, E E Cervenka, A J; Experimental
evaluation of boron-hydrocarbon slurry in a 16-inch ram-jet combustor;
naca-rm-e55c07; July 1955
- Silverstein, Abe Hall,
Eldon W; Liquid hydrogen
as a jet fuel for high-altitude aircraft; naca-rm-e55c28a; April 15,
1955
- Hearth, Donald P
Englert, Gerald W Kowalski, Kenneth L; Matching
of auxiliary inlets to secondary-air requirements of aircraft ejector exhaust
nozzles; naca-rm-e55d21; August 16, 1955
- Hamrick, Joseph T
Osborn, Walter M; Design
and test of mixed-flow impellers V : design procedure and performance results
for two vaned diffusers tested with impeller model MFI-1B; naca-rm-e55e13;
July 07, 1955
- Chiarito, Patrick T; Effectiveness
of a turbojet tubular combustor in screening the turbine from foreign
objects; naca-rm-e55e16; July 18, 1955
- Kremzier, Emil J Wise,
George A; Effect of
centerbody boundary-layer removal near the throat of three coniccal nose
inlets at Mach 1.6 to 2.0; naca-rm-e55h16a; November 15, 1955
- Rabb, Leaonard Disher,
John H; Boundary-layer
transition at high Reynolds numbers as obtained in flight of a 20 degree
cone-cylinder with wall to local stream temperature ratios near 1.0;
naca-rm-e55i15; November 03, 1955
- Witzke, Walter R Prok,
George M Keller, Thomas A; Design
considerations of a condensing system for vaporized magnesium;
naca-rm-e55i20; November 30, 1955
- Ordin, Paul M; Transportation
of liquid fluorine; naca-rm-e55i23; November 08, 1955
- Allen, John L; Preliminary
investigation of effect on performance of dividing conical-spike nose inlets
into halves at Mach numbers 1.5 to 2.0; naca-rm-e55i26; December 19,
1955
- Pinkel, Benjamin
Deutsch, George C Morgan, William C; Preliminary
investigation of several root designs for cermet turbine blades in turbojet
engine III : curved-root design; naca-rm-e55j04; December 28, 1955
- Tomazic, William A; Rocket-engine
throttling; naca-rm-e55j20; 1955
- Lindsey, Walter F
Landrum, Emma Jean; Flow
and force characteristics of 2-percent-thick airfoils at transonic speeds;
naca-rm-l54i30; January 18, 1955
- Peck, Robert F; Jet effects on
longitudinal trim of an airplane configuration measured at Mach numbers
between 1.2 and 1.8; naca-rm-l54j29a; January 18, 1955
- Welsh, Clement J
Wallskog, Harvey A Sandahl, Carl A; Effects
of some leading-edge modifications, section and plan-form variations, and
vertical position on low-lift wing drag at transonic speeds;
naca-rm-l54k01; January 18, 1955
- Alford, William J
Silvers, H Norman King, Thomas, J , jr; Experimental
aerodynamic forces and moments at low speed of a missile model during
simulated launching from the midsemispan location of a 45 degree sweptback
wing-fuselage combination; naca-rm-l54k11a; February 04, 1955
- Parks, James H; Transonic
longitudinal aerodynamic effects of sweeping up the rear of the fuselage of a
rocket-propelled airplane model having no horizontal tail; naca-rm-l54k12;
January 20, 1955
- Kuhn, Richard E Byrnes,
Andrew L , Jr; Aerodynamic
loading characteristics in sideslip of a 45 degree sweptback wing with and
without a fence at high subsonic speeds; naca-rm-l54k15; January 28,
1955
- Bridgland, T F , Jr; A theoretical
investigation of the effect of auxiliary damping on the longitudinal response
of a transonic bomber configuration in flight through continuous
turbulence; naca-rm-l54k15a; March 1955
- English, Roland D; Free-flight
investigation, including some effects of wing aeroelasticity, of the rolling
effectiveness of an all-movable horizontal tail with differential incidence at
Mach numbers from 0.6 to 1.5; naca-rm-l54k30; January 25, 1955
- Curfman, Howard J , Jr;
Application
of nonlinear aerodynamic stability characteristics to simplify missile control
and guidance systems; naca-rm-l54l06a; February 15, 1955
- Chauvin, Leo T Maloney,
Joseph P; Turbulent
convective heat-transfer coefficients measured from flight tests of four
research models (NACA RM-10) at Mach numbers from 1.0 to 3.6;
naca-rm-l54l15; March 11, 1955
- Vitale, A James; Characteristics
of loads in rough air at transonic speeds of rocket-powered models of a canard
and a conventional-tail configuration; naca-rm-l54l17; March 1955
- Piland, Robert O; Performance
measurements from a rocket-powered exploratory research missile flown to a
Mach number of 10.4; naca-rm-l54l29a; March 15, 1955
- Fischetti, Thomas L
Loving, Donald L; Effect
of an all-movable wing-tip control on the longitudinal stability of 60 degree
sweptback-wing-indented-body configuration equipped with fences at transonic
speeds; naca-rm-l54l30; April 04, 1955
- Platt, Robert J , Jr
Brooks, Joseph D; Transonic
wind-tunnel investigation of the effects of sweepback and thickness ratio on
the wing loads of a wing-body combination of aspect ratio 4 and taper ratio
0.6; naca-rm-l54l31b; April 04, 1955
- Palmer, William E
Burrows, Dale L; A
transonic wind-tunnel investigation of the longitudinal force and moment
characteristics of two delta wings and one clipped-tip delta wing of 4 percent
thickness on a slender body; naca-rm-l55a07a; April 04, 1955
- Alford, William J , Jr;
Experimental
static aerodynamic forces and moments at low speed on a canard missle during
simulated launching from the midsemispan and wing-tip locations of a 45 degree
sweptback wing-fuselage combination; naca-rm-l55a12; April 06, 1955
- Wallskog, Harvey A; Flutter
experiences with thin pointed-tip wings during flight tests of
rocket-propelled models at Mach numbers from 0.8 to 1.95; naca-rm-l55a14;
April 04, 1955
- Rumsey, Charles B
Piland, Robert O Hopko, Russell N; Aerodynamic-heating
data obtained from free-flight tests between Mach numbers of 1 and 5;
naca-rm-l55a14a; March 11, 1955
- Ulmann, Edward F Smith,
Fred M; Aerodynamic
characteristics of a 60 degree delta wing having a half-delta tip control at a
Mach number of 4.04; naca-rm-l55a19; April 25, 1955
- Bartlett, Walter, A ,
jr Hagginbotham, William K , Jr; Flight
and preflight tests of a ram jet burning magnesium slurry fuel and utilizing a
solid-propellant gas generator for fuel expulsion; naca-rm-l55a24; April
06, 1955
- Henry, Beverly Z , Jr
Cahn, Maurice S; Preliminary
results of an investigation at transonic speeds to determine the effects of a
heated propulsive jet on the drag characteristics of a related series of
afterbodies; naca-rm-l55a24a; March 25, 1955
- Bertram, Mitchel H
Mccauley, William D; An
investigation of the aerodynamic characteristics of thin delta wings with a
symmetrical double-wedge section at a Mach number of 6.9; naca-rm-l55b14;
October 14, 1955
- Spearman, M Leroy; Investigation
of the aerodynamic characteristics in pitch and sideslip of a 45 degree
sweptback-wing airplane model with various vertical locations of the wing and
horizontal tail : effect of wing location and geometric dihedral for the
wing-body com; naca-rm-l55b18; April 06, 1955
- Thompson, Robert F
Taylor, Robert T; Effect
of a wing leading-edge flap and chord-extension on the high subsonic control
characteristics of an aileron located at two spanwise positions;
naca-rm-l55b18a; May 10, 1955
- Coletti, Donard E; Investigation
of interference lift, drag, and pitching moment of a series of triangular wing
and body combinations at a Mach number of 1.62; naca-rm-l55b25; May 27,
1955
- Nason, Martin L Rock,
Rupert S Brown, Clarence, Jr; An
evaluation of a rolleron-roll-rate-stabilization system for a canard missile
configuration at Mach numbers from 0.9 to 2.3; naca-rm-l55c22; September
15, 1955
- Chauvin, Leo T Carter,
Howard S; Exploratory
tests of transpiration cooling on a porous 8 degree cone at M = 2.05 using
nitrogen gas, helium gas, and water as the coolants; naca-rm-l55c29; June
03, 1955
- Dow, Norris F Peters,
Roger W; Preliminary
investigation of the failure of pressurized stiffened cylinders;
naca-rm-l55d15b; May 20, 1955
- Alford, William J , Jr
Silvers, H Norman King, Thomas J , Jr; Experimental
static aerodynamic forces and moments at low speed on a missile model during
simulated launching from the 25-percent-semispan and wing-tip location of a 45
degree sweptback wing-fuselage combination; naca-rm-l55d20; May 25,
1955
- Wiley, Harleth G
Moseley, William C , Jr; An
investigation at high subsonic speeds of the effects of horizontal-tail height
on the aerodynamic and loading characteristics in sideslip on a 45 degree
sweptback, untapered tail assembly as determined from force tests and
integrated vertical-tail; naca-rm-l55e04; June 28, 1955
- Smith, Norman F
Carlson, Harry W; Some
effects of configuration variables on store loads at supersonic speeds;
naca-rm-l55e05; July 06, 1955
- Bressette, Walter E
Faget, Maxime A; An
investigation of jet effects on adjacent surfaces; naca-rm-l55e06; June
28, 1955
- Jones, Jim J; Experimental
drag coefficients of round noses with conical windshields at Mach number
2.72; naca-rm-l55e10; June 28, 1955
- Davis, Don D , Jr
Hieser, Gerald; Loads
on thin wings at transonic speeds; naca-rm-l55e11c; June 28, 1955
- Czarnecki, K R Lord,
Douglas R; Simplified
procedures for estimating flap-control loads at supersonic speeds;
naca-rm-l55e12; May 27, 1955
- Lord, Douglas, R
Czarnecki, K R; Loads
associated with spoilers at supersonic speeds; naca-rm-l55e12a; June 14,
1955
- Runckel, Jack F Gray, W
H; An
investigation of loads on ailerons at transonic speeds; naca-rm-l55e13;
May 27, 1955
- Guy, Lawrence D; Loads on
external stores at transonic and supersonic speeds; naca-rm-l55e13b;
August 15, 1955
- Silsby, Norman S
Harrin, Eziaslav N; Landing
conditions for large airplanes in routine operations; naca-rm-l55e18c;
July 06, 1955
- Polhamus, Edward C; Some factors
affecting the variation of pitching moment with sideslip of aircraft
configurations; naca-rm-l55e20b; July 15, 1955
- Carlson, Harry W
Gapcynski, John P; An
experimental investigation at a Mach number of 2.01 of the effects of body
cross-section shape on the aerodynamic characteristics of bodies and wing-body
combinations; naca-rm-l55e23; July 21, 1955
- Feller, William V; Investigation
of equilibrium temperatures and average laminar heat-transfer coefficients for
the front half of swept circular cylinders at a Mach number of 6.9;
naca-rm-l55f08a; August 18, 1955
- Beckwith, Ivan E; Theoretical
investigation of laminar heat transfer on yawed infinite cylinders in
supersonic flow and a comparison with experimental data; naca-rm-l55f09;
August 09, 1955
- Falanga, Ralph A; A free-flight
investigation of the effects of simulated sonic turbojet exhaust on the drag
of a boattail body with various jet sizes from Mach number 0.87 to 1.50;
naca-rm-l55f09a; August 18, 1955
- Griffith, George E
Miltonberger, Georgene H Rosecrans, Richard; Tests
of aerodynamically heated multiweb wing structures in a free jet at Mach
number 2 : two aluminum-alloy models of 20-inch chord with 0.064- and
0.081-inch-thick skin; naca-rm-l55f13; August 09, 1955
- Strass, H Kurt
Stephens, Emily W Fields, E M Schult, Eugene D; Collection
and summary of flap-type-aileron rolling-effectiveness data at zero lift as
determined by rocket-powered model tests at Mach numbers between 0.6 and
1.6; naca-rm-l55f14; September 02, 1955
- Passera, Anthony L
Garner, H Douglas; Simulator
studies of a simple homing system; naca-rm-l55g06; October 06, 1955
- Schult, Eugene D; :A Free-flight
investigation at high subsonic and low supersonic speeds of the rolling
effectiveness and drag of three spoiler controls having potentially low
actuating-force requirements; naca-rm-l55g11a; September 20, 1955
- Rumsey, Charles B; Free-flight
measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to
Mach number 6.9 of a fin-stabilized cone-cylinder configuration;
naca-rm-l55g28a; October 07, 1955
- Seaberg, Ernest C
Sproull, Royce H Reid, H J E , Jr; Flight
investigation at supersonic Mach numbers of an automatic acceleration control
missile in which rate damping is obtained from a linear accelerometer placed
ahead of the missile center of gravity; naca-rm-l55g29; November 08,
1955
- Hoffman, Sherwood; Free-flight
tests to determine the power-on and power-off pressure distribution and drag
of the NACA RM-10 research vehicle at large Reynolds numbers between Mach
numbers 0.8 and 3.0; naca-rm-l55h02; September 20, 1955
- Guy, Lawrence D
Hadaway, William M; Aerodynamic
loads on an external store adjacent to a 45 degree sweptback wing at Mach
numbers from 0.70 to 1.96, including an evaluation of techniques used;
naca-rm-l55h12; November 15, 1955
- Turner, Thomas R
Vogler, Raymond D; Wind-tunnel
investigation at transonic speeds of a jet control on an 80 degree delta-wing
missile; naca-rm-l55h22; November 1955
- Gapcynski, John P; An experimental
investigation of the flow phenomena over bodies at high angles of attack at a
Mach number of 2.01; naca-rm-l55h29; October 27, 1955
- Clements, James E; A theoretical
analysis of a simple aerodynamic device to improve the longitudinal damping of
a cruciform missile configuration at supersonic speeds; naca-rm-l55h31;
October 27, 1955
- Purser, Paul E; Comparative
dispersion data from ground-launched 2.25-inch rockets equipped with cruciform
and monoplane fins; naca-rm-l55i06; November 1955
- Gillespie, Warren, Jr;
Lift, drag,
and longitudinal stability at Mach numbers from 1.4 to 2.3 of a rocket-powered
model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail
surfaces; naca-rm-l55i12; December 15, 1955
- Falanga, Ralph A Judd,
Joseph H; Flight
investigation of the effect of underwing propulsive jets on the lift, drag,
and longitudinal stability of a delta-wing configuration at Mach numbers from
1.23 to 1.62; naca-rm-l55i13; December 15, 1955
- Coletti, Donald E; Investigation
of interference lift, drag, and pitching moment of a series of triangular-wing
and body combinations at a Mach number of 1.94; naca-rm-l55i14; December
21, 1955
- Schmeer, James W; The effect of
leading-edge droop upon the pressure distribution and aerodynamic loading
characteristics of a 45 degree sweptback wing at transonic speeds;
naca-rm-l55i16; November 08, 1955
- Press, Harry Meadows,
May T Hadlock, Ivan; Estimates
of probability distribution of root-mean-square gust velocity of atmospheric
turbulence from operational gust-load data by random-process theory;
naca-tn-3362; March 1955
- Keith, Arvid L , Jr
Schiff, Jack; Low-speed
wind-tunnel investigation of a triangular sweptback air inlet in the root of a
45 degree sweptback wing; naca-tn-3363; 1955
- Reller, John O , Jr
Hamaker, Frank M; An
experimental investigation of the base pressure characteristics of nonlifting
bodies of revolution at Mach numbers from 2.73 to 4.98; naca-tn-3393;
March 17, 1955
- Daley, Bernard N Lord,
Douglas R; Aerodynamic
characteristics of several 6-percent-thick airfoils at angles of attack from 0
degrees to 20 degrees at high subsonic speeds; naca-tn-3424; May
1955
- Bird, John D; Some
calculations of the lateral response of two airplanes to atmospheric
turbulence with relation to the lateral snaking problem; naca-tn-3425; May
1955
- Seaberg, Ernest C; Theoretical
investigation of a proportional-plus-flicker automatic pilot;
naca-tn-3427; May 1955
- Pendley, Robert E
Robinson, Harold L; An
investigation of several NACA 1-series nose inlets with and without protruding
central bodies at high-subsonic Mach numbers and at a Mach number of 1.2;
naca-tn-3436; May 1955
- Nichols, Mark R
Pierpont, Kenneth P; Preliminary
investigation of a submerged air scoop utilizing boundary-layer suction to
obtain increased pressure recovery; naca-tn-3437; April 1955
- Watkins, Charles E
Berman, Julian H; On
the Kernel function of the integral equation relating lift and downwash
distributions of oscillating wings in supersonic flow; naca-tn-3438; May
1955
- Mccomb, Harvey G , Jr
Low, Emmet F , Jr; Tables
of coefficients for the analysis of stresses about cutouts in circular
semimonocoque cylinders with flexible rings; naca-tn-3460; July
1955
- Turner, Thomas R; Effects of
sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at
transonic speeds; naca-tn-3468; July 1955
- Gessow, Alfred
Tapscott, Robert J; Supplementary
charts for estimating performance of high-performance helicopters;
naca-tn-3482; July 1955
- Turner, Howard L White,
John S Van Dyke, Rudolph D , Jr; Flight
testing by radio remote control-flight evaluation of a beep-control
system; naca-tn-3496; March 1955
- Beck, Preston E (Naval
Air Test Center); Some
results of flight testing of ski-equipped aircraft at the Naval Air Test
Center; naca-rm-54j27; February 04, 1955
- (Author(s) Not
Available); Meteorological
problems associated with commercial turbojet-aircraft operation;
naca-rm-54l29; June 21, 1955
- Black, John M (Forest
Products Laboratory) Blomquist, R F (Forest Products Laboratory); Metal-bonding
adhesives for high-temperature service; naca-rm-55f08; July 28,
1955
- Cesaro, Richard S
Walker, Curtis L; Application
of non-afterburning turbojets to supersonic flight; naca-rm-55k16;
November 18, 1955
- Wetzel, Benton E; Wind-tunnel
investigation at subsonic and supersonic speeds of a fighter model employing a
low-aspect-ratio unswept wing and a horizontal tail mounted well above the
wing plane-lateral and directional stability; naca-rm-a54h26b; April 28,
1955
- Eggers, A J , Jr
Syverton, Clarence A; Experimental
investigation of a body flare for obtaining pitch stability and a body flap
for obtaining pitch control in hypersonic flight; naca-rm-a54j13; January
18, 1955
- Turner, Howard L
Triplett, William C White, John S; A
flight and analog computer study of some stabilization and command networks
for an automatically controlled interceptor during the final attack phase;
naca-rm-a54j14; March 23, 1955
- Baldwin, Barrett S , Jr
Dickey, Robert R; Application
of wing-body theory to drag reduction at low supersonic speeds;
naca-rm-a54j19; January 28, 1955
- Wetzel, Benton E; Effect of taper
ratio on lift, drag, and pitching-moment characteristics of thin wings of
aspect ratio 3 with 53.1 degrees sweepback of leading edge at subsonic and
supersonic speeds; naca-rm-a54j20; January 27, 1955
- Sammonds, Robert I
Reynolds, Robert M; The
pressure-recovery and propeller-force characteristics of a
propeller-spinner-cowling combination employing NACA 4-(5) (05)-037 six- and
eight-blade dual-rotation propellers with an NACA 1 series D-type cowl;
naca-rm-a54j22; January 27, 1955
- Tunnell, Phillips J; An
investigation of string support interference on base pressure and forebody
chord force at Mach numbers from 0.60 to 1.30; naca-rm-a54k16a; January
28, 1955
- Sutton, Fred B Dickson,
Jerald K; The
longitudinal characteristics at Mach numbers up to 0.92 of several
wing-fuselage-tail combinations having sweptback wings with NACA four-digit
thickness distributions; naca-rm-a54l08; March 24, 1955
- Eggers, Alfred J , Jr
Allen, H Julian Neice, Stanford E; A
comparative analysis of the performance of long-range hypervelocity
vehicles; naca-rm-a54l10; March 24, 1955
- Knechtel, Earl D
Summers, James L; Effects
of sweep and taper on the longitudinal characteristics of an aspect ratio 3
wing-body combination at Mach numbers from 0.6 to 1.4; naca-rm-a55a03;
March 23, 1955
- Sadoff, Melvin; Summary of the
flight conditions and maneuvers in which maximum wing and tail loads were
experienced on a swept-wing fighter airplane; naca-rm-a55a06; March 30,
1955
- Alksne, Alberta; A comparison of
two methods for computing the wave of wing-body combinations;
naca-rm-a55a06a; April 07, 1955
- Hopkins, Edward J
Sorensen, Norman E; Downwash
survey behind two low-aspect-ratio variable-incidence wings in combination
with three different size fuselages at a Mach number of 0.25;
naca-rm-a55a07; March 30, 1955
- Mossman, Emmet A
Lazzeroni, Frank A Pfyl, Frank A; An
experimental investigation of the air-flow of a scoop-type normal-shock
inlet; naca-rm-a55a13; April 28, 1955
- Lomax, Harvard; The wave drag
of arbitrary configurations in linearized flow as determined by areas and
forces in oblique planes; naca-rm-a55a18; March 24, 1955
- Beam, Benjamin H Reed,
Verlin D Lopez, Armando E; Wind-tunnel
measurements at subsonic speeds of the static and dynamic-rotary stability
derivatives of a triangular-wing airplane model having a triangular vertical
tail; naca-rm-a55a28; April 25, 1955
- Blackaby, James R; Wind-tunnel
investigation at low speed of a wing having 63 degree sweepback and a drooped
tip; naca-rm-a55b14; April 07, 1955
- Mcdevitt, John B; An experimental
investigation of two methods for reducing transonic drag of swept-wing and
body combinations; naca-rm-a55b21; April 29, 1955
- Polentz, Perry P Page,
William A Levy, Lionel L , Jr; The
unsteady normal-force characteristics of selected NACA profiles at high
subsonic Mach numbers; naca-rm-a55c02; May 27, 1955
- Walker, Harold J
Maillard, William C; A
correlation of airfoil section data with the aerodynamic loads measured on a
45 degree sweptback wing model at subsonic Mach numbers; naca-rm-a55c08;
May 27, 1955
- Neice, Stanford E Wong,
Thomas J Hermach, Charles A; Lift,
drag, and static longitudinal stability characteristics of four airplane-like
configurations at Mach numbers from 3.00 to 6.28; naca-rm-a55c24; April
25, 1955
- Dickson, Jerald K
Sutton, Fred B; The
effect of wing height on the longitudinal characteristics at high subsonic
speeds of a wing-fuselage-tail combination having a wing with 40 degrees of
sweepback and NACA four digit thickness distribution; naca-rm-a55c30; May
25, 1955
- Dickson, Gerald K
Sutton, Fred B; The
effect of wing fences on the longitudinal characteristics at Mach numbers up
to 0.92 of a wing-fuselage-tail combination having a 40 degree sweptback wing
with NACA 64A thickness distribution; naca-rm-a55c30a; May 27, 1955
- Graham, David Evans,
William T; Investigation
of the effects of an airfoil section modification on the aerodynamic
characteristics at subsonic and supersonic speeds of a thin swept wing of
aspect ratio 3 in combination with a body; naca-rm-a55d11; June 28,
1955
- Cole, Henry A , Jr
Brown, Stuart C Holleman, Euclid C; The
effects of flexibility on the longitudinal and lateral directional response of
a large airplane; naca-rm-a55d14; May 27, 1955
- White, Maurice D; A flight
investigation at transonic speeds of a model having a triangular wing of
aspect ratio 3; naca-rm-a55d18; June 24, 1955
- Mossman, Emmett A Pfyl,
Frank A Lazzeroni, Frank A; Experimental
investigation at Mach numbers from 0 to 1.9 of trapezoidal and circular side
inlets for a fighter-type airplane; naca-rm-a55d27; July 28, 1955
- Stephenson, Jack D
Selan, Ralph Bandettini, Angelo; A
comparison at Mach numbers up to 0.92 of the calculated and experimental
downwash and wake characteristics at various horizontal tail heights behind a
wing with 45 degree of sweepback; naca-rm-a55d27a; June 28, 1955
- Stewart, Elwood C; Application of
statistical theory to beam-rider guidance in the presence of noise I : Wiener
filter theory; naca-rm-a55e11; August 23, 1955
- Delany, Noel K; Additional
measurements of the low-speed static stability of a configuration employing
three triangular wing panels and a body of equal length; naca-rm-a55f02a;
July 25, 1955
- Holdaway, George H; Additional
comparisons between computed and measured transonic drag-rise coefficients at
zero lift for wing-body-tail configurations; naca-rm-a55f06; August 15,
1955
- Cooper, George E Innis,
Robert C; Effect of
area-suction-type boundary-layer control on the landing-approach
characteristics of a 35 degree swept-wing fighter; naca-rm-a55k14;
February 03, 1955
- Peterson, Victor L
Menees, Gene P; Static
stability and control of canard configurations at Mach numbers from 0.70 to
2.22 : lateral-directional characteristics of a triangular wing and
canard; naca-rm-a57l18; March 28, 1955
- Gillespie, Warren, Jr;
Lift, drag,
and longitudinal stability at Mach numbers from 0.8 to 2.1 of a rocket-powered
model having a tapered unswept wing of aspect ratio 3 and inline tail
surfaces; naca-rm-l55b10; April 25, 1955
- Cubbage, James M , Jr;
Effect of
convergent ejector nozzles on the boattail drag of a 16 degree conical
afterbody at Mach numbers of 0.6 to 1.26; naca-rm-l58g25; September 17,
1955
- Keune, Friedrich.; Lift on a bent,
flat plate; naca-tm-1340; 1955
- Vladimirov, A. N.; Approximate
hydrodynamic design of a finite span hydrofoil; naca-tm-1341; 1955
- Germain, Paul.; General theory
of conical flows and its application to supersonic aerodynamics;
naca-tm-1354; 1955
- Miele, Angelo.; General
solutions of optimum problems in nonstationary flight; naca-tm-1388;
1955
- Miele, Angelo.; Optimum flight
paths of turbojet aircraft; naca-tm-1389; 1955
- Loeb, Julian.; From
linear mechanics to nonlinear mechanics; naca-tm-1396; 1955
- Rothrock, Addison M.;
Turbojet
propulsion-system research and the resulting effects on airplane
performance; naca-rm-54h23; 1955
- Neel, Carr B., Jr.; A Heated-Wire
Liquid-Water-Content Instrument and Results of Initial Flight Tests in Icing
Conditions; naca-rm-a54i23; 1955
- Dods, Jules B. Jr.,
Tinling, Bruce E.; Summary
of results of a wind-tunnel investigation of nine related horizontal
tails; naca-tn-3497; 1955
- Deyoung, John Barling,
Walter H , Jr; Correction
of additional span loadings computed by the Weissinger seven-point method for
moderately tapered wings of high aspect ratio; naca-tn-3500; July
1955
- Sadoff, Melvin.,
Matteson, Frederick H., Havill, C. Dewey.; A
method for evaluating the loads and controllability aspects of the pitch-up
problem; naca-rm-a55d06; 1955
- Matthews, Howard F.,
Schmidt, Stanley F.; A
comparison of the maneuvering performance of a monowing versus a cruciform
missile; naca-rm-a55d13; 1955
- Rathert, George A , Jr
Abramovitz, Marvin Gadeberg, Burnett L; The
effects of powered controls and fire-control systems on tracking accuracy;
naca-rm-a55d12a; May 26, 1955
- Doolin, Brian F Smith,
G Allan Drinkwater, Fred J , III; An
air-borne target simulator for use in optical sight tracking studies;
naca-rm-a55f20; September 1955
- Scherrer, Richard.,
Gowen, Forrest E.; Preliminary
experimental investigation of a variable-area, variable-internal-contraction
air inlet at Mach numbers between 1.42 and 2.44; naca-rm-a55f23;
1955
- Warner Robert W.; Comparison
between analytical and wind-tunnel results on flutter of several
low-aspect-ratio, high-density, unswept wings at high subsonic speeds and zero
angle of attack; naca-rm-a55g08; 1955
- Boyd, John W.,
Migotsky, Eugene., Wetzel, Benton E.; A
study of conical camber for triangular and sweptback wings;
naca-rm-a55g19; 1955
- Wetzel, Benton E.; Effect of
leading-edge sweepback on lift, drag, and pitching-moment characteristics of
thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic
speeds; naca-rm-a55h04a; 1955
- Wong, Thomas J.,
Gloria, Hermilo R.; Aerodynamic
characteristics of two rectangular-plan-form, all moveable controls in
combination with a slender body of revolution at Mach numbers from 3.00 to
6.25; naca-rm-a55j07; 1955
- Coe, Charles F.; A study of
local-pressure fluctuations relative to static-pressure distributions on
two-dimensional airfoils at high subsonic Mach numbers; naca-rm-a55j11;
1955
- Jack D. Stephenson,
Angelo Bandettini, and Ralph Selan (Ames Aeroanutical Laboratory, Moffett
Field Calif.); Longitudinal
Stability Characteristics at Mach Numbers up to 0.92 of a Wing-Body-Tail
Combination Having a Wing with 45o of Sweepback and a Tail in Various Vertical
Positions; naca-rm-a54k09; 1955
- Richard R. Heldenfels,
Eldon E. Mathauser; A
summary of NACA research on the strength and creep of aircraft structures at
elevated temperatures; naca-rm-L56D06; May, 1956
- Edmond E. Bisson,
Robert L. Johnson, Max A Swikert, Douglas Godfrey; Friction,
wear, and surface damage of metals as affected by solid surface films;
naca-report-1254; Jan 1956
- Max A. Heaslet,
Franklyn B. Fuller; Axially
symmetric shapes with minimum wave drag; naca-report-1256; Jan 1956
- Charles E. Watkins,
Julian H. Berman; On
the Kernel function of the integral equation relating lift and downwash
distributions of oscillating wings in supersonic flow; naca-report-1257;
Jan 1956
- Benjamin H. Beam; A wind-tunnel
test technique for measuring the dynamic rotary stability derivatives at
subsonic and supersonic speeds; naca-report-1258; Jan 1956
- Dean R. Chapman; Some
possibilities of using gas mixtures other than air in aerodynamic
research; naca-report-1259; Jan 1956
- Robert J. Tapscott,
Kenneth B. Amer; Studies
of the speed stability of a tandem helicopter in forward flight;
naca-report-1260; Jan 1956
- Leslie W. Lassiter,
Harvey H. Hubbard; The
near noise field of static jets and some model studies of devices for noise
reduction; naca-report-1261; Jan 1956
- Harry L. Runyan, Donald
S. Woolston, Gerald A. Rainey; Theoretical
and experimental investigation of the effect of tunnel walls on the forces on
an oscillating airfoil in two-dimensional subsonic compressible flow;
naca-report-1262; Jan 1956
- Richard E. Kuhn, John
W. Draper; Investigation
of the aerodynamic characteristics of a model wing-propeller combination and
of the wing and propeller separately at angles of attack up to 90 degrees;
naca-report-1263; Jan 1956
- A. E. Potter, Jr., A.
I. Berlad; A
thermal equation for flame quenching; naca-report-1264; Jan 1956
- Robert L. Trimpi; A theory for
stability and buzz pulsation amplitude in ram jets and an experimental
investigation including scale effects; naca-report-1265; Jan 1956
- Alfred Gessow, Robert
J. Tapscott; Charts for
estimating performance of high-performance helicopters; naca-report-1266;
Jan 1956
- M. J. Queijo; Theoretical
span load distributions and rolling moments for sideslipping wings of
arbitrary plan form in incompressible flow; naca-report-1269; Jan
1956
- Bernard Lubarsky,
Samuel J. Kaufman; Review
of experimental investigations of liquid-metal heat transfer;
naca-report-1270; Jan 1956
- Keith C. Harder, Conrad
Renneman, Jr.; On
boattail bodies of revolution having minimum wave drag; naca-report-1271;
Jan 1956
- Harry Press, May T.
Meadows, Ivan Hadlock; A
reevaluaion of data on atmospheric turbulence and airplane gust loads for
application in spectral calculations; naca-report-1272; Jan 1956
- Richard T. Whitcomb; A study of the
zero-lift drag-rise characteristics of wing-body combinations near the speed
of sound; naca-report-1273; Jan 1956
- Milton D. Van Dyke; Second-order
subsonic airfoil theory including edge effects; naca-report-1274; Jan
1956
- Frederick C. Grant; The proper
combination of lift loadings for least drag on a supersonic wing;
naca-report-1275; Jan 1956
- Curt A. Holzhauser,
Richard S. Bray; Wind-tunnel
and flight investigations of the use of leading-edge area suction for the
purpose of increasing the maximum lift coefficient of a 35 degree swept-wing
airplane; naca-report-1276; Jan 1956
- Maurice Tucker; Interaction of
a free flame front with a turbulence field; naca-report-1277; Jan
1956
- Francis E. Cook,
Benjamin Milwitzky; Effect
of interaction on landing-gear behavior and dynamic loads in a flexible
airplane structure; naca-report-1278; Jan 1956
- James J. Kramer, Vasily
D. Prian, Chung-Hua Wu; Theoretical
analysis of incompressible flow through a radial-inlet centrifugal impeller at
various weight flows; naca-report-1279; jan 1956
- Herbert C. Nelson,
Herbert J. Cunningham; Theoretical
investigation of flutter of two-dimensional flat panels with one surface
exposed to supersonic potential flow; naca-report-1280; Jan 1956
- R. I. Sears, C. F.
Merlet, L. W. Putland; Flight
determination of drag of normal-shock nose inlets with various cowling
profiles at Mach numbers from 0.9 to 1.5; naca-report-1281; Jan
1956
- Harvard Lomax, Max A.
Heaslet; A
special method for finding body distortions that reduce the wave drag of wing
and body combinations at supersonic speeds; naca-report-1282; Jan
1956
- Robert R. McCready; Extrapolation
techniques applied to matrix methods in neutron diffusion problems;
naca-report-1283; Jan 1956
- Robert T. Jones; Theory of
wing-body drag at supersonic speeds; naca-report-1284; Jan 1956
- H. B. Tolefson; Summary of
derived gust velocities obtained from measurements within thunderstorms;
naca-report-1285; Jan 1956
- Clyde C. Swett, Jr.; Spark ignition
of flowing gases; naca-report-1287; jan 1956
- NACA Subcommittee on
Power-Plant Materials; Cooperative
investigation of relationship between static and fatigue properties of wrought
n-155 alloy at elevated temperatures; naca-report-1288; Jan 1956
- G. B. Schubauer, P. S.
Klebanoff; Contributions
on the mechanics of boundary-layer transition; naca-report-1289; Jan
1956
- R. D. Johnson, A. P.
Young, A. D. Schwope; Plastic
deformation of aluminum single crystals at elevated temperatures;
naca-report-1267; Jan 1956
- G. M. Kline, I. Wolock,
B. M. Axilrod, M. A. Sherman, D. A. George, V. Cohen; Development
of craze and impact resistance in glazing plastics by multiaxial
stretching; naca-report-1290; Jan 1956
- Franklin K. Moore; Lift hysteresis
at stall as an unsteady boundary-layer phenomenon; naca-report-1291; Jan
1956
- James C. Laurence; Intensity,
scale, and spectra of turbulence in mixing region of free subsonic jet;
naca-report-1292; Jan 1956
- Clarence B. Cohen, Eli
Reshotko; Similar
solutions for the compressible laminar boundary layer with heat transfer and
pressure gradient; naca-report-1293; Jan 1956
- Clarence B. Cohen, Eli
Reshotko; The
compressible laminar boundary layer with heat transfer and arbitrary pressure
gradient; naca-report-1294; Jan 1956
- Vernon L. Rogallo, Paul
F. Yaggy, John L. McCloud, III; An
analysis of once-per-revolution oscillating aerodynamic thrust loads on
single-rotation propellers on tractor airplanes at zero yaw;
naca-report-1295; Jan 1956
- William R. Mickelsen,
Norman E. Ernstein; Propagation
of a free flame in a turbulent gas stream; naca-report-1286; Jan
1956
- Robert H. Kirby; Exploratory
investigation of the effectiveness of biplane wings with large-chord double
slotted flaps in redirecting a propeller slipstream downward for vertical
take-off; naca-tn-3800; Oct 1956
- Allister F. Fraser; Experimental
investigation of the strength of multiweb beams with corrugated webs;
naca-tn-3801; Oct 1956
- James C. Dunavant, John
R. Erwin; Investigation
of a related series of turbine-blade profiles in cascade; naca-tn-3802;
Oct 1956
- George P. Wood, Paul B.
Gooderum; A
factor affecting transonic leading-edge flow separation; naca-tn-3804; Oct
1956
- Emanuel Schnitzer; Band-pass shock
and vibration absorbers for application to aircraft landing gear;
naca-tn-3803; Oct 1956
- John M. Eggleston; Calculation of
the forces and moments on a slender fuselage and vertical fin penetrating
lateral gusts; naca-tn-3805; Oct 1956
- Eugene S. Love; Initial
inclination of the mixing boundary separating an exhausting supersonic jet
from a supersonic ambient stream; naca-rm-l55j14; Jan 1956
- Archibald R. Sinclair,
William D. Mace; Wind-tunnel
calibration of a combined pitot-static tube and vane-type flow-angularity
indicator at Mach numbers of 1.61 and 2.01; naca-tn-3808; Oct 1956
- Charles E. Watkins,
Barbara J. Durling; A
method for calculation of free-space sound pressures near a propeller in
flight including considerations of the chordwise blade loading;
naca-tn-3809; Nov 1956
- Robert A. Makofski; Charts for
estimating the hovering endurance of a helicopter; naca-tn-3810; Oct
1956
- Dorothy B. Lee, Maxime
A. Faget; Charts adapted
from Van Driest's turbulent flat-plate theory for determining values of
turbulent aerodynamic friction and heat-transfer coefficients;
naca-tn-3811; Oct 1956
- Robert H. Kirby; Flight
investigation of the stability and control characteristics of vertically
rising airplane research model with swept or unswept wings and x- or
+-tails; naca-tn-3812; Oct 1956
- George W. Zender; Comparison of
theoretical stresses and deflections of multicell wings with experimental
results obtained from plastic models; naca-tn-3813; Nov 1956
- M. J. Queijo, Evalyn G.
Wells; Effects of
vertical fins near the nose of the fuselage on the directional and
damping-in-yaw stability derivatives of an airplane model under steady-state
and oscillatory conditions; naca-tn-3814; Dec 1956
- Keith C. Harder, E. B.
Klunker; On
slender-body theory and the area rule at transonic speeds; naca-tn-3815;
Nov 1956
- Arthur J. McEvily, Jr.,
Walter Illg, Herbert F. Hardrath; Static
strength of aluminum-alloy specimens containing fatigue cracks;
naca-tn-3816; Oct 1956
- John R. Erwin, Melvyn
Savage, James C. Emery; Two-dimensional
low-speed cascade investigation of NACA compressor blade sections having a
systematic variation in mean-line loading; naca-tn-3817; Nov 1956
- James W. Wiggins,
Richard E. Kahn, Paul G. Fournier; Wind-tunnel
investigation to determine the horizontal- and vertical-tail contributions to
the static lateral stability characteristics of a complete-model swept-wing
configuration at high subsonic speeds; naca-tn-3818; Nov 1956
- De E. Beeler, Donald R.
Bellman, Edwin J. Saltzman; Flight
techniques for determining airplane drag at high Mach numbers;
naca-tn-3821; Aug 1956
- Walter F. Lindsey,
Patrick J. Johnston; Some
observations on maximum pressure rise across shocks without boundary-layer
separation on airfoils at transonic speeds; naca-tn-3820; Nov 1956
- Sherman A. Clevenson,
Sumner A. Leadbetter; Some
measurements of aerodynamic forces and moments at subsonic speeds on a
wing-tank configuration oscillating in pitch about the wing midchord;
naca-tn-3822; Dec 1956
- Harold W. Woolley; Thermodynamic
properties of gaseous nitrogen; naca-tn-3271; Mar 1956
- Harold W. Woolley,
William S. Benedict; Generalized
tables of corrections to thermodynamic properties for nonpolar gases;
naca-tn-3272; Mar 1956
- Lilla Fano, John H.
Hubbell, Charles W. Beckett; Compressibility
factor, density, specific heat, enthalpy, entropy, free-energy function,
viscosity, and thermal conductivity of steam; naca-tn-3273; Aug
1956
- John E. Dalgleish,
Adelbert O. Tischler; Experimental
investigation of a lightweight rocket chamber; naca-tn-3827; Oct
1956
- David Novik; Some
linear dynamics of two-spool turbojet engines; naca-tn-3274; Jun
1956
- Cleveland O'Neal, Jr.;
Effect of
pressure on the spontaneous ignition temperature of liquid fuels;
naca-tn-3829; Oct 1956
- Perry L. Blackshear,
Jr.; Growth
of disturbances in a flame-generated shear region; naca-tn-3830; Nov
1956
- Albert Kaufman, Andre
J. Meyer, Jr.; Investigation
of the effect of impact damage on fatigue strength of jet-engine compressor
rotor blades; naca-tn-3275; Jun 1956
- Henry C. Barnett,
Robert R. Hibbard; Properties
of aircraft fuels; naca-tn-3276; Aug 1956
- Burton D. Fine, Paul
Wagner; Space heating
rates for some premixed turbulent propane-air flames; naca-tn-3277; Jun
1956
- George C. Fryburg,
Norman H. Katz, Sidney L. Simon; Effect
of phosphate coatings on temperature of metal parts exposed to flame
environments; naca-tn-3279; Jul 1956
- Alexander P. Sabol,
John S. Evans; Investigation
of the use of the thermal decomposition of nitrous oxide to produce hypersonic
flow of a gas closely resembling air; naca-tn-3624; Mar 1956
- James N. Mueller; Conversion of
inviscid normal-force coefficients in helium to equivalent coefficients in air
for simple shapes at hypersonic speeds; naca-tn-3807; Oct 1956
- Morris D. Rousso,
Eugene L. Baughman; Spreading
characteristics of a jet expanding from choked nozzles at mach 1.91;
naca-tn-3836; Dec 1956
- Holdaway, George H
Mersman, William A; Application
of Tchebichef form of harmonic analysis to the calculation of zero-lift wave
drag of wing-body-tail combinations; naca-rm-a55j28; February 13,
1956
- Gloria, Hermilo R Wong,
Thomas J; Effects of two
trailing-edge controls on the aerodynamic characteristics of a rectangular
wing and body combination at Mach numbers from 3.00 and 5.05;
naca-rm-a55k07; February 1956
- Pitts, William C; Force, moment,
and pressure-distribution characteristics of rectangular wings at high angles
of attack and supersonic speeds; naca-rm-a55k09; February 13, 1956
- Page, William A; Influence of
the body flow field on the zero-lift wave drag of wing-body combinations
modified in accordance with the transonic area rule; naca-rm-a55k10;
February 07, 1956
- Savin, Raymond C Wong,
Thomas J; Lift, drag, and
static longitudinal stability characteristics of configurations consisting of
three triangular wing panels and a body of equal length at Mach numbers from
3.00 to 6.28; naca-rm-a55k21; February 07, 1956
- Hopkins, Edward J
Sorensen, Norman E; A
study of a missile designed to fly at low speed with its longitudinal axis
aligned with the flight path; naca-rm-a55k30; February 07, 1956
- Eggers, A J , Jr
Syverton, Clarence A; Aircraft
configurations developing high lift-drag ratios at high supersonic speeds;
naca-rm-a55l05; March 05, 1956
- Lessing, Henry C Reese,
David E , Jr; A
simulation study of a wingless missile; naca-rm-a55l06; February 08,
1956
- Rossow, Vernon J; A theoretical
study of the lifting efficiency at supersonic speeds of wings utilizing
indirect lift induced by vertical surfaces; naca-rm-a55l08; March 26,
1956
- Hikido, Katsumi
Hayashi, Paul H Lessing, Henry C; Investigation
of the possibility of simplifying missile guidance systems by the use of
free-floating flaps and spring-mounted control surfaces; naca-rm-a55l09;
May 17, 1956
- Rubesin, Morris W; The influence
of surface injection on heat-transfer and skin friction associated with the
high-speed turbulent boundary layer; naca-rm-a55l13; February 20,
1956
- Goodwin, Glen; Heat-transfer
characteristics of blunt two-and three-dimensional bodies at supersonic
speeds; naca-rm-a55l13a; February 16, 1956
- Nielsen, Jack N Spahr,
J Richard Centolanzi, Frank; Aerodynamics
of bodies, wings, and wing-body combinations at high angles of attack and
supersonic speeds; naca-rm-a55l13c; February 13, 1956
- Chapman, Dean R Kuehn,
Donald M Larson, Howard K; Preliminary
report on a study of separated flows in supersonic and subsonic streams;
naca-rm-a55l14; June 12, 1956
- Levy, Lionel L JR
Dickey, Robert R; External-store
drag reduction at transonic and low supersonic Mach numbers by application of
Baldwin's moment-of-area rule; naca-rm-a55l14a; March 05, 1956
- Allen, H Julian Neice,
Stanford E; Problems of
performance and heating of hypersonic vehicles; naca-rm-a55l15; March 05,
1956
- Mossman, Emmet A Pfyl,
Frank A; A
study of a symmetrical, circular, internal, compression inlet;
naca-rm-a55l16; February 13, 1956
- Seiff, Alvin; A
review of recent information on boundary-layer transition at supersonic
speeds; naca-rm-a55l21; March 05, 1956
- Wong, Thomas J Gloria,
Hermilo R; A
preliminary investigation of the static stability characteristics of four
airplane-like configurations at Mach numbers from 3.00 to 6.28;
naca-rm-a56a06; March 26, 1956
- Pitts, William C; Reduction of
wave drag of wing-body combinations at supersonic speeds through body
distortions; naca-rm-a56b10; April 13, 1956
- Carros, Robert J; Effect of Mach
number on boundary-layer transition in the presence of pressure rise and
surface roughness on an ogive-cylinder body with cold wall conditions;
naca-rm-a56b15; April 20, 1956
- Stine, Howard A
Winovich, Warren; Light
diffusion through high-speed turbulent boundary layers; naca-rm-a56b21;
May 26, 1956
- Stalder, Jackson R
Inouye, Momoru; A
method of reducing heat transfer to blunt bodies by air injection;
naca-rm-a56b27a; May 17, 1956
- Davis, Wallace F Gowen,
Forrest E; The change with
mass-flow ratio of the cowl pressure drag of normal-shock inlets at supersonic
speeds; naca-rm-a56c06; June 22, 1956
- Sammonds, Robert I
Reynolds, Robert M; The
effect of conical camber on the static longitudinal, lateral, and directional
characteristics of a 45-degree sweptback wing at Mach numbers up to 0.96;
naca-rm-a56d02; July 03, 1956
- Tendeland, Thorval
Okuno, Arthur F; The
effect of fluid injection on the compressible turbulent boundary layer : the
effect of skin friction of air injected into the boundary layer of a cone at M
= 2.7; naca-rm-a56d05; June 19, 1956
- Dickey, Robert R; Effect of
camber on the drag of a body of revolution; naca-rm-a56e23; October 19,
1956
- Mossman, Emmett A Pfyl,
Frank A; An
experimental investigation at Mach numbers from 2.1 to 3.0 of
circular-internal-contraction inlets with translating centerbodies;
naca-rm-a56g06; October 31, 1956
- Gloria, Hermilo R; An
investigation of the lift, drag, and static-stability characteristics of a
triangular-wing airplane configuration at Mach numbers from 3.00 to 6.28;
naca-rm-a56h27; December 19, 1956
- Knechtel, Earl D
Andrea, Arvid N; Aerodynamic
characteristics in pitch of several triple-body missile configurations at Mach
numbers 0.6 to 1.4; naca-rm-a56h31; November 02, 1956
- Morrell, Virginia E; Effect of
combustion-chamber pressure and nozzle expansion ratio on theoretical
performance of several rocket propellant systems; naca-rm-e50c30; May 25,
1956
- Lezberg, Erwin A Lord,
Albert M; Spontaneous
ignition of pentaborane sprays in a hot-air stream; naca-rm-e55f29a;
November 23, 1956
- Weber, Richard J
Luidens, Roger W; A
simplified method for evaluating jet-propulsion-system components in terms of
airplane performance; naca-rm-e56j26; December 06, 1956
- Mcdonald, Glen E; Thermal
stability of pentaborane in the range 329 to 419 F; naca-rm-e54g16;
December 19, 1956
- (Author(s) Not
Available); Factors that
affect operational reliability of turbojet engines; naca-rm-e55h02;
January 31, 1956
- Hearth, Donald P
Cubbison, Robert W; Investigation
at supersonic and subsonic Mach numbers of auxiliary inlets supplying
secondary air flow to ejector exhaust nozzles; naca-rm-e55j12a; January
25, 1956
- Salmi, Reino J Klann,
John L; Interference
effects at Mach 1.9 on a horizontal tail due to trailing shock waves from an
axisymmetric body with an exiting jet; naca-rm-e55j13a; January 25,
1956
- Foster, Hampton H
Ingebo, Robert D; Evaporation
of JP-5 fuel sprays in air streams; naca-rm-e55k02; February 21,
1956
- Mull, Harold R
Algranti, Joseph S; Preliminary
flight survey of aerodynamic noise on an airplane wing; naca-rm-e55k07;
March 02, 1956
- Lubick, Robert J
Chelko, Louis J Wallner, Lewis E; Effect
of inlet-duct length in uniform-flow field on turbojet-engine operation;
naca-rm-e55k15; April 11, 1956
- Lezberg, Erwin A
Blackshear, Perry L , Jr Rayle, Warren D; Weight-flow
and thrust limitations due to use of rotating combustors in a turbojet
engine; naca-rm-e55k16; August 17, 1956
- Beheim, Milton, A
Evans, Phillip J; Effects
of rocket-armament exhaust gas on the performance of a supersonic-inlet
J34-turbojet-engine installation at Mach 2.0; naca-rm-e55k22; February 20,
1956
- Wilcox, Fred Whalen,
Paul; Dynamics of a
supersonic inlet with adjustable bypass in combination with a J34 turbojet
engine; naca-rm-e55l13a; March 23, 1956
- Wilcox, Fred A
Perchonok, Eugene; Aerodynamic
control of supersonic inlets for optimum performance; naca-rm-e55l14;
February 20, 1956
- Connors, James F; Some aspects of
supersonic inlet stability; naca-rm-e55l16a; February 29, 1956
- Obery, Leonard J
Schueller, Carl F; Effects
of internal boundary-layer control on the performance of supersonic aft
inlets; naca-rm-e55l17; March 02, 1956
- Gordon, Sanford Huff,
Vearl N; Theoretical
performance of JP-4 fuel with a 70-percent-flourine -30-percent-oxygen mixture
as a rocket propellant I : frozen composition; naca-rm-e56a13a; April 11,
1956
- Wasserbauer, Joseph F
Englert, Gerald W; Interaction
of an exhaust jet and elementary contoured surfaces located in a supersonic
air stream; naca-rm-e56a16; April 06, 1956
- Huff, Vearl N Fortini,
Anthony; Theoretical
performance of JP-4 fuel and liquid oxygen as a rocket propellant I : frozen
composition; naca-rm-e56a27; April 17, 1956
- Gray, Vernon H Von
Glahn, Uwe H; Heat-requirements
for ice protection of a cyclically gas-heated, 36 degree swept airfoil with
partial-span leading-edge slat; naca-rm-e56b23; May 14, 1956
- Hall, Eldon W Weber,
Richard J; Tables and
charts for thermodynamic calculations involving air and fuels containing
boron, carbon, hydrogen, and oxygen; naca-rm-e56b27; July 13, 1956
- Pass, Isaac Tischler,
Adelbert O; Effect of fuels
on screaming in 200-pound-thrust liquid-oxygen - fuel rocket engine;
naca-rm-e56c10; June 22, 1956
- Valerino, Alfred S
Yeager, Richard A; External-stream
effects on gross thrust and pumping characteristics of ejectors operating at
off-design Mach numbers; naca-rm-e56c14; June 26, 1956
- Klann, John L Huff,
Ronald G; Experimental
investigation of interference effects of lateral-support struts on afterbody
pressures at Mach 1.9; naca-rm-e56c16; May 14, 1956
- Heidmann, Marcus F; Injection
principles for liquid oxygen and heptane using two-element injectors;
naca-rm-e56d04; June 26, 1956
- Kowalski, K Piercy,
Thomas G; Stability of
supersonic inlets at Mach 1.91 with air injection and suction;
naca-rm-e56d12; June 28, 1956
- Huff, Vearl N Fortini,
Anthony Gordon, Sanford; Theoretical
performance of JP-4 fuel and liquid oxygen as a rocket propellant II :
equilibrium composition; naca-rm-e56d23; September 07, 1956
- Nettles, J C; Investigation
of the air-flow regulation characteristics of a translating-spike inlet with
two oblique shocks from Mach 1.6 to 2.0; naca-rm-e56d23b; July 24,
1956
- Krull, H George Beale,
William T; Internal
performance characteristics of short convergent-divergent exhaust nozzles
designed by the method of characteristics; naca-rm-e56d27a; July 24,
1956
- Low, George M; Boundary-layer
transition at supersonic speeds; naca-rm-e56e10; August 03, 1956
- Huntley, S C
Braithwaite, Willis M; Effect
of variable-position inlet guide vanes and interstage bleed on compressor
performance of a high-pressure-ratio turbojet engine; naca-rm-e56e23a;
December 28, 1956
- Gordon, Sanford Huff,
Vearl N; Theoretical
performance of JP-4 fuel with a 70-30 mixture of fluorine and oxygen as a
rocket propellant : equilibrium composition; naca-rm-e56f04; October 02,
1956
- Whalen, Paul P Wilcox,
Fred A; Use
of a diffuser Mach number as a supersonic-inlet control parameter;
naca-rm-e56f05; September 14, 1956
- Salmi, R J Cortright, E
M , Jr; Effects of
external stream flow and afterbody variations on the performance of a plug
nozzle; naca-rm-e56f11a; October 02, 1956
- Ladanyi, Dezso J; Effects of
variations in combustion-chamber configuration on ignition delay in a
50-pound-thrust rocket; naca-rm-e56f22; October 05, 1956
- Krull, H George Beale,
William T Schmiedlin, Ralph F; Effect
of several design variables on internal performance of convergent-plug exhaust
nozzles; naca-rm-e56g20; October 29, 1956
- Disher, John H Rabb,
Leonard; Observation of
laminar flow on a blunted 15 degree cone-cylinder in free flight at high
reynolds numbers and free-stream mach numbers to 8.17; naca-rm-e56g23;
October 15, 1956
- Cavicchi, Richard H; Analysis of
limitations imposed on one-spool turboprop-engine designs by compressors and
turbines at flight mach numbers of 0.06, and 0.8; naca-rm-e56i05; December
06, 1956
- Signorelli, R A
Johnston, J R Weeton, J W; Preliminary
investigation of Guy alloy as a turbojet-engine bucket material for use at
1650 degrees F; naca-rm-e56i19; November 29, 1956
- Salmi, Reino J; Preliminary
investigation of methods to increase base pressure of plug nozzles at Mach
0.9; naca-rm-e56j05; December 19, 1956
- Hall, James Rudyard; Effect of wing
size and amount of indentation on applicability of transonic area rule to
swept-wing configurations; naca-rm-l55f03; July 20, 1956
- Putland, Leonard W; Flight
determination of drag and pressure recovery of two scoop inlets located at
maximum-body-diameter station at Mach numbers from 0.8 to 1.8;
naca-rm-l55h22a; January 10, 1956
- Platt, Robert J , Jr;
Transonic
wind-tunnel investigation of the effects of indentation on the wing loads of a
45 degree sweptback wing-body combination; naca-rm-l55h26; January 11,
1956
- Unangst, John R Jones,
George W , Jr; Some
effects of sweep and aspect ratio on the transonic flutter characteristics of
a series of thin cantilever wings having a taper ratio of 0.6;
naca-rm-l55i13a; January 24, 1956
- Lord, Douglas R
Czarnecki, K R; Pressure
distribution and aerodynamic loadings for several-flap-type trailing-edge
controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01;
naca-rm-l55j03; March 12, 1956
- Lord, Douglas R
Czarnecki, K R; Tabulated
pressure data for several flap-type trailing edge controls on a trapezoidal
wing at Mach numbers of 1.61 and 2.01; naca-rm-l55j04; February 27,
1956
- Loving, Donald L; A transonic
investigation of changing indentation design Mach number on the aerodynamic
characteristics of a 45 degree sweptback-wing-body combination designed for
high performance; naca-rm-l55j07; January 10, 1956
- Few, Albert G , Jr; Some effects of
sweep and thickness on the experimental downwash characteristics at transonic
speeds of a series of highly tapered wings with an aspect ratio of 3 :
transonic bump method; naca-rm-l55j12; February 16, 1956
- Hall, James Rudyard; Preliminary
free-flight study of the drag and stability of a series of short-span missiles
at Mach numbers from 0.9 to 1.3; naca-rm-l55j13; February 08, 1956
- Stokes, George M; A method for
the design of porous-wall wind tunnels; naca-rm-l55j13a; January 20,
1956
- Brooks, Joseph D; Transonic
wind-tunnel investigation of the aerodynamic loading characteristics of a
highly tapered upswept wing in the presence of a body with and without
indentation; naca-rm-l55j20; February 1956
- Lauten, William T , Jr
O'Kelly, Burke R; Free-flight
flutter tests in the transonic and low supersonic speed range of three
low-aspect-ratio swept, tapered wings on rocket-propelled vehicles;
naca-rm-l55j21; March 19, 1956
- Gardiner, Robert A
Gillis, Clarence L Graves, G B , Jr; Analysis
of a flight investigation at supersonic speeds of a simple homing system;
naca-rm-l55j28; January 10, 1956
- Penland, Jim A
Fetterman, David E , Jr; The
effects at a Mach number of 6.86 of drag brakes on the lift, drag, and
pitching moment of an ogive cylinder; naca-rm-l55k23; March 19,
1956
- Jones, George W , Jr
Unangst, John R; Investigation
to determine effects of center-of-gravity location on the transonic flutter
characteristics of a 45 degree sweptback wing; naca-rm-l55k30; February
20, 1956
- Lord, Douglas R
Czarnecki, K R; Aerodynamic
loadings associated with swept and unswept spoilers on a flat-plate at Mach
numbers of 1.61 and 2.01; naca-rm-l55l12; March 12, 1956
- Bressette, Walter E
Leiss, Abraham; Investigation
of jet effects on a flat surface downstream of the exit of a simulated
turbojet nacelle at a free-stream Mach number of 1.39; naca-rm-l55l13;
April 02, 1956
- Mclellan, Charles H
Dunning, Robert W; Factors
affecting the maximum lift-drag ratio at high supersonic speeds;
naca-rm-l55l20a; February 13, 1956
- Falanga, Ralph A; A free-flight
investigation of the effects of a sonic jet on the total-drag and
base-pressure coefficients of a boattail body of revolution from Mach number
0.83 to 1.70; naca-rm-l55l21; March 08, 1956
- Riebe, John M Moseley,
William C , Jr; Low-speed
stability characteristics of a cambered-delta-wing model; naca-rm-l55l21a;
March 08, 1956
- Lowry, John G; Recent
control studies; naca-rm-l55l22a; February 16, 1956
- Malvestuto, Frank S ,
Jr Alford, William J , Jr; Effects
of wing-body geometry on the lateral-flow angularities at subsonic speeds;
naca-rm-l55l26a; February 21, 1956
- Vitale, A James
Mitchell, Jesse L; Experimental
results from a test in rough air at high subsonic speeds of a tailless rocket
model having cruciform triangular wings, and a note on the calculation of mean
square loads of aircraft in continuous rough air; naca-rm-l55l28; April
13, 1956
- Bobbitt, Percy J
Malvestuto, Frank S , Jr Margolis, Kenneth; Theoretical
prediction of the side force on stores attached to configurations traveling at
supersonic speeds; naca-rm-l55l30b; March 12, 1956
- Syvertson, Clarence A
Dennis, David H; A
second-order shock-expansion method applicable to bodies of revolution near
zero lift; naca-tn-3527; 1956
- Connors, James F
Meyers, Rudolph C; Design
criteria for axisymmetric and two-dimensional supersonic inlets and exits;
naca-tn-3589; 1956
- Anderson, Roger A
Anderson, Melvin S; Correlation
of crippling strength of plate structures with material properties;
naca-tn-3600; 1956
- Peterson, Marshall B
Johnson, Robert L; Friction
studies of graphite and mixtures of graphite with several metallic oxides and
salts at temperatures to 1000 F; naca-tn-3657; February 1956
- Heyson, Harry H
Katzoff, S; Normal
component of induced velocity in the vicinity of a lifting rotor with a
nonuniform disk loading; naca-tn-3690; April 1956
- Whitney, Warren J; Tabulation of
mass-flow parameters for use in design of turbomachine blade rows for ratios
of specific heats of 1.3 and 1.4; naca-tn-3831; October 1956
- Herzig, Howard Z
Hansen, Arthur G; On
possible similarity solutions for three-dimensional incompressible laminar
boundary layers II : similarity with respect to stationary polar
coordinates; naca-tn-3832; November 1956
- Fine, Burton; Stability
limits and burning velocities of laminar hydrogen-air flames at reduced
pressure; naca-tn-3833; November 1956
- Leiws, James P Ruggeri,
Robert S; Investigation
of heat transfer from a stationary and rotating ellipsoidal forebody of
fineness ratio 3; naca-tn-3837; November 1956
- Mcardle, Jack G; Performance
characteristics of ring-cascade-type thrust reversers; naca-tn-3838;
November 1956
- Gelder, Thomas, F
Smyers, William H , Jr Von Glahn, Uwe; Experimental
droplet impingement on several two-dimensional airfoils with thickness ratios
of 6 to 16 percent; naca-tn-3839; December 1956
- Hansen, Arthur G
Herzig, Howard Z; Analysis
of particle motions for a class of three-dimensional incompressible laminar
boundary layers; naca-tn-3840; November 1956
- Castles, Walter, Jr
(Georgia Institute of Technology) Durham, Howard L , Jr (Georgia Institute of
Technology); Distribution of
normal component of induced velocity in lateral plane of a lifting rotor;
naca-tn-3841; December 1956
- Jaquet, Byron M
Fletcher, Herman S; Experimental
steady-state yawing derivatives of a 60 degree delta-wing model as affected by
changes in vertical position of the wing and in ratio of fuselage diameter to
wing span; naca-tn-3843; October 1956
- Whaley, Richard E
Mcguigan, M J , Jr Bryan, D F; Fatigue-crack-propagation
and residual-static-strength results on full-scale transport-airplane
wings; naca-tn-3847; December 1956
- Foster, Gerald V
Griner, Roland F; A
study of several factors affecting the stability contributed by a horizontal
tail at various vertical positions on a sweptback-wing airplane model;
naca-tn-3848; November 1956
- Shivers, James P
Carpenter, Paul J; Experimental
investigation on the Langley helicopter test tower of compressibility effects
on a rotor having NACA 63(sub 2)-015 airfoil sections; naca-tn-3850;
December 1956
- Potter, A E , Jr
Berlad, A L; A relation
between burning velocity and quenching distance; naca-tn-3882; November
1956
- Anagnostou, E Brokaw, R
S Butler, J N; Effect
of concentration on ignition delays for various fuel-oxygen-nitrogen mixtures
at elevated temperatures; naca-tn-3887; December 1956
- Donegan, James J Huss,
Carl R; Incomplete time
response to a unit impulse and its application to lightly damped linear
systems; naca-tn-3897; December 1956
- Dewalt, W J (Aluminum
Company of America) Bogardus, K O (Aluminum Company of America); Static
shear strength of 2117-T4 (A17S-T4) aluminum-alloy rivets at elevated
temperatures; naca-rm-55i30; January 04, 1956
- Rey, William K
(University of Alabama); Elevated-temperature
fatigue properties of two titanium alloys; naca-rm-56b07; April 24,
1956
- Patel, Sharad A
(Polytechnic Institute of Brooklyn) Kempner, Joseph (Polytechnic Institute of
Brooklyn) Erickson, Burton (Polytechnic Institute of Brooklyn) Mobassery, Abol
H (Polytechnic Institute of Brooklyn); Correlation
of creep-buckling tests with theory; naca-rm-56c20; May 23, 1956
- Chu, Boa-Teh (Johns
Hopkins University); Stability
of systems containing a heat source : the Rayleigh criterion;
naca-rm-56d27; June 26, 1956
- (Author(s) Not
Available); A survey and
evaluation of flutter research and engineering; naca-rm-56i12; October 05,
1956
- Margolis, Kenneth
Bobbitt, Percy J; Theoretical
calculations of the pressure, forces, and moments at supersonic speeds due to
various lateral motions acting on thin isolated vertical tails;
naca-report-1268; 1956
- Davis, Wallace F
Scherrer, Richard; Aerodynamic
principles for the design of jet-engine induction systems; naca-rm-a55f16;
February 27, 1956
- Mossman, Emmet A Pfyl,
Frank A Lazzeroni, Frank A; Fuselage
side inlets : a study of some factors affecting their performance and a
comparison with nose inlets; naca-rm-a55f29; April 02, 1956
- Goodwin, Glen Creager,
Marcus O Winkler, Ernest L; Investigation
of local heat-transfer and pressure drag characteristics of a yawed circular
cylinder at supersonic speeds; naca-rm-a55h31; January 24, 1956
- Rolls, L Stewart Innis,
Robert C; A
flight evaluation of a wing-shroud-blowing boundary-layer control system
applied to the flaps of an F9F-4 airplane; naca-rm-a55k01; February 14,
1956
- Anderson, Seth B
Quigley, Hervey C; Flight
measurements of the low-speed characteristics of a 35 degree swept-wing
airplane with area suction boundary-layer control on the flaps;
naca-rm-a55k29; February 03, 1956
- LAZZERONI FRANK A Pfyl,
Frank A; Effect of
boundary-layer control and inlet lip shape on the performance of a twin-scoop
air-induction system at Mach numbers from 0 to 1.9; naca-rm-a55l02;
February 14, 1956
- Dods, Jules B , Jr
Watson, Earl C; The
effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil
section, comparisons with various types of flaps on other airfoil sections,
and an analysis of flow and power relationships for blowing systems;
naca-rm-a56c01; June 12, 1956
- Hill, William A
Kaattari, George E; Force
and pressure-distribution investigation to high angles of attack on
all-movable triangular and rectangular wings in combination with a body at
supersonic speeds; naca-rm-a56c12; July 10, 1956
- Edwards, George G
Savage, Howard F; A
horizontal-tail arrangement for counteracting static longitudinal instability
of sweptback wings; naca-rm-a56d06; May 25, 1956
- Koenig, David G; The use of area
suction for improving the longitudinal characteristics of a thin unswept
wing-fuselage model with leading- and trailing-edge flaps; naca-rm-a56d23;
July 10, 1956
- Summers, James L Treon,
Stuart L Graham, Lawrence A; Wind-tunnel
investigation at Mach numbers from 0.8 to 1.4 of static longitudinal and
lateral-directional characteristics of an unswept-wing airplane model;
naca-rm-a56e22; December 13, 1956
- Tolhurst, William H ,
Jr Kelly, Mark W; Full-scale
wind-tunnel tests of a 35 degree sweptback-wing airplane with high-velocity
blowing over the trailing-edge flaps : longitudinal and lateral stability and
control; naca-rm-a56e24; October 05, 1956
- Holzhauser, Curt A
Martin, Robert K Page, V Robert; Application
of area suction to leading-edge and trailing-edge flaps on a 44 degree
swept-wing model; naca-rm-a56f01; September 26, 1956
- Matthews, Howard F
Merrick, Robert B; A
simulator study of some longitudinal stability and control problems of a
piloted aircraft in flights to extreme altitude and high speed;
naca-rm-a56f07; September 07, 1956
- Kelly, Mark W; Analysis
of some parameters used in correlating blowing-type boundary-layer control
data; naca-rm-a56f12; September 26, 1956
- Jorgenson, Leland H
Katzen, Eliott D; Wing-body
combinations with wings of very low aspect ratio at supersonic speeds;
naca-rm-a56g16; October 26, 1956
- Boltz, Frederick W
Kenyon, George C Allen, Clyde Q; Measurements
of boundary-layer transition at low speed on two bodies of revolution in a
low-turbulence wind tunnel; naca-rm-a56g17; September 26, 1956
- Kelly, Mark W Tucker,
Jeffrey H; Wind-tunnel
tests of blowing boundary-layer control with jet pressure ratios up to 9.5 on
the trailing-edge flaps of a 35 degree sweptback wing airplane;
naca-rm-a56g19; October 26, 1956
- Anderson, Seth B
Quigley, Hervey C Innis, Robert C; Flight
measurements of the low-speed characteristics of a 35 degree swept-wing
airplane with blowing-type boundary-layer control in the trailing-edge
flaps; naca-rm-a56g30; October 25, 1956
- Buell, Donald A
Tinling, Bruce E; The
subsonic lateral and longitudinal static stability characteristics up to large
angles of sideslip for a triangular-wing airplane model having a ventral
fin; naca-rm-a56h06; October 25, 1956
- Koenig, David G Aoyagi,
Kiyoshi; Large-scale
wind-tunnel tests of an airplane model with a 45 degree sweptback wing of
aspect ratio 2.8 with area suction applied to trailing-edge flaps and with
several wing leading-edge modifications; naca-rm-a56h08; November 02,
1956
- Bland, William M , Jr
Collie, Katherine A; Free-flight
aerodynamic-heating data to Mach number 10.4 for a modified Von Karman nose
shape; naca-rm-l56d25; July 10, 1956
- Weber, Richard J
Luidens, Roger W; Analysis
of ram-jet engine performance including effects of component changes;
naca-rm-e56d20; October 29, 1956
- Allen, John L; Performance
of a blunt-lip side inlet with ramp bleed, bypass, and a long constant-area
duct ahead of the engine : Mach number 0.66 and 1.5 to 2.1;
naca-rm-e56j01; December 28, 1956
- Sevier, John R , Jr; Investigation
of the effects of body camber and body indentation on the longitudinal
characteristics of a 60 degree delta-wing-body combination at a Mach number of
1.61; naca-rm-l56a03; April 20, 1956
- Judd, Joseph H Falanga,
Ralph A; Flight
investigation of the effect of a propulsive jet positioned according to the
transonic area rule on the drag coefficients of a single-engine delta-wing
configuration at Mach numbers from 0.83 to 1.36; naca-rm-l56a16; April 13,
1956
- Hall, James Rudyard; Two experiments
on applications of the transonic area rule to asymmetric configurations;
naca-rm-l56a25; April 20, 1956
- Tuovila, W J Hess,
Robert W; Aerodynamic
damping at Mach numbers of 1.3 and 1.6 of a control surface on a
two-dimensional wing by a free-oscillation method; naca-rm-l56a26a; May
1956
- Nason, Martin L; An evaluation
of an aeromechanical method of minimizing servo- missile transfer function
variations with flight condition; naca-rm-l56a31; April 18, 1956
- Rumsey, Charles B Lee,
Dorothy B; Measurements of
aerodynamic heat transfer and boundary-layer transition on a 10 degree cone in
free flight at supersonic Mach numbers up to 5.9; naca-rm-l56b07; April
26, 1956
- Driver, Cornelius
Hamilton, Clyde V; Wind-tunnel
investigation of a ram-jet model having a wing and canard surfaces of delta
plan form with 70 degrees swept leading edges : force and moment
characteristics at combined angles of pitch and sideslip for Mach number
2.01; naca-rm-l56b21; April 26, 1956
- Ridyard, Herbert W
Fetterman, David E , Jr; Aerodynamic
characteristics of a 6-percent-thick symmetrical circular-arc airfoil having a
30-percent-chord trailing-edge flap at a Mach number of 6.9;
naca-rm-l56b24; May 05, 1956
- Hoffman, Sherwood; Supersonic-area-rule
design and rocket-propelled flight investigation of a zero-lift
straight-wing-body-nacelle configuration between Mach numbers 0.8 and
1.53; naca-rm-l56b27; April 26, 1956
- Piland, Robert O
Collie, Katherine A Stoney, William E; Turbulent
and laminar heat-transfer measurements on a 1/6-scale NACA RM-10 missile in
free fight to Mach number of 4.2 and to a wall temperature of 1400 R;
naca-rm-l56c05; July 03, 1956
- Jackson, H Herbert; Free-flight
measurements of the zero-lift drag of several wings at Mach numbers from 1.4
to 3.8; naca-rm-l56c13; June 22, 1956
- Schmeer, James W; Effect of
leading-edge droop on the aerodynamic and loading characteristics of a
4-percent-thick unswept-wing-fuselage combination at transonic speeds;
naca-rm-l56c14; May 23, 1956
- Gillespie, Warren, Jr;
Effect of
wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and
longitudinal stability of a rocket-powered model having a 52.5 degree
sweptback wing of aspect ratio 3 and inline tail surfaces; naca-rm-l56c16;
May 07, 1956
- Cubbage, James M , Jr;
Jet effects
on base and afterbody pressures of a cylindrical afterbody at transonic
speeds; naca-rm-l56c21; May 23, 1956
- Carter, Howard S; Heat transfer
on the lifting surfaces of a 60 degree delta wing at angle of attack for Mach
number 1.98; naca-rm-l56c23; May 31, 1956
- Brown, Clarence, A ,
jr; Longitudinal
stability characteristics of a simple infrared homing missile configuration at
Mach numbers of 0.7 to 1.4; naca-rm-l56d10; June 12, 1956
- Palmer, William E
Howell, Robert R Braslow, Albert L; Transonic
investigation at lifting conditions of streamline contouring in the
sweptback-wing-fuselage juncture in combination with the transonic area
rule; naca-rm-l56d11a; July 20, 1956
- Riley, Donald R; Some effects of
wing fences on the lateral stability derivatives of a 60 degree delta wing
oscillating continuously in yaw; naca-rm-l56d13; July 11, 1956
- Stoney, William E, Jr
Royall, John F; Zero-lift
drag of a series of bomb shapes at Mach numbers from 0.60 to 1.10;
naca-rm-l56d16; July 26, 1956
- Lange, Roy H Wittliff,
Charles E; Force and
pressure-distribution measurements at a Mach number of 3.12 of slender bodies
having circular, elliptical, and triangular cross sections and the same
longitudinal distribution of cross-sectional area; naca-rm-l56d17; July
13, 1956
- Stephens, Emily W; The effect of
external stiffening ribs on the rolling power of ailerons on a swept wing;
naca-rm-l56d19; October 25, 1956
- Leiss, Abraham; Free-flight
investigation of effects of simulated sonic turbojet exhaust on the drag of
twin-jet boattail bodies at transonic speeds; naca-rm-l56d30; July 20,
1956
- Beckwith, Ivan E
Gallagher, James J; Experimental
investigation of the effect of boundary-layer transition on the average heat
transfer to a yawed cylinder in supersonic flow; naca-rm-l56e09; July 13,
1956
- Lowry, John G Taylor,
Robert T; The variation
with wing aspect ratio of flap effectiveness on thin rectangular wings at
transonic speeds; naca-rm-l56e18; August 23, 1956
- Faber, Stanley
Cheatham, Donald C Champine, Robert A; Flight
investigation of factors affecting pilots' ability to utilize a radarscope
display of steering information; naca-rm-l56e21; November 23, 1956
- Aiken, William S , Jr
Fisher, Raymond A; Lift-curve
slopes determined in flight on a flexible swept-wing jet bomber;
naca-rm-l56e21a; December 19, 1956
- Guy, Lawrence D; Hinge moment
and effectiveness of an unswept constant-chord control and an
overhang-balanced, swept hinge-line control on an 80 degree swept pointed wing
at Mach numbers from 0.75 to 1.96; naca-rm-l56f11; August 28, 1956
- Swanson, Andrew G
Rumsey, Charles B; Aerodynamic
heating of a wing as determined from a free-flight rocket-model test to Mach
number 3.64; naca-rm-l56f11a; September 11, 1956
- Mcdearmon, Russell W
Jones, Robert A; Wind-tunnel
investigation of damping in roll at supersonic speeds of triangular wings at
angles of attack; naca-rm-l56f13a; September 14, 1956
- Foster, Gerald V
Driver, Cornelius; Effects
of external stores on the static longitudinal aerodynamic characteristics of a
model of a 45 degree swept-wing fighter airplane at Mach numbers of 1.61 and
2.01; naca-rm-l56f15a; August 23, 1956
- Hammond, Alexander D;
Wind-tunnel
investigation of the effect of aspect ratio and chordwise location on
effectiveness of plain spoilers on thin untapered wings at transonic
speeds; naca-rm-l56f20; September 26, 1956
- Burrows, Dale L; Transonic
wind-tunnel investigation of static longitudinal force and moment
characteristics of two wing-body combinations with clipped-tip and full delta
wings of aspect ratio 1.73; naca-rm-l56f21; September 14, 1956
- Becker, John V
Korycinski, Peter F; Heat
transfer and pressure distribution at a Mach number of 6.8 on bodies with
conical flares and extensive flow separation; naca-rm-l56f22; July 20,
1956
- Rumsey, Charles B Lee,
Dorothy B; Measurements of
aerodynamic heat transfer and boundary-layer transition on a 15 degree cone in
free flight at supersonic Mach numbers up to 5.2; naca-rm-l56f26; October
15, 1956
- Thomson, William C; Model ditching
investigation of a jet transport airplane with various engine
installations; naca-rm-l56g10; August 20, 1956
- Henry, Beverly Z JR
Cahn, Maurice S; Additional
results of an investigation at transonic speeds to determine the effects of a
heated propulsive jet on the drag characteristics of a series of related
afterbodies; naca-rm-l56g12; September 24, 1956
- Mugler, John P , Jr; Effects of two
leading-edge modifications on the aerodynamic characteristics of a thin
low-aspect-ratio delta wing at transonic speeds; naca-rm-l56g12a; October
12, 1956
- Love, Eugene S
Woodling, Mildred J Lee, Louise P; Boundaries
of supersonic axisymmetric free jets; naca-rm-l56g18; October 05,
1956
- Martz, C William; Experimental
hinge moments on freely oscillating flap-type control surfaces;
naca-rm-l56g20; October 12, 1956
- Rainey, Robert W; Investigation
at supersonic speeds of the effects of bomb-bay configuration upon the
aerodynamic characteristics of fuselages with noncircular cross sections;
naca-rm-l56h20; November 29, 1956
- Falanga, Ralph A Leiss,
Abraham; Free-flight
investigation at transonic speeds of drag coefficients of a boattail body of
revolution with a simulated turbojet exhaust issuing at the base from conical
short-length ejectors; naca-rm-l56h23; December 13, 1956
- Turner, Thomas R; A wind-tunnel
investigation of the development of lift on wings in accelerated longitudinal
motion; naca-rm-l56h28a; November 02, 1956
- Schult, Eugene D; Free-flight
investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling
effectiveness and drag of various surface, spoiler, and jet controls on an 80
degree delta-wing missile; naca-rm-l56h29; November 29, 1956
- Kliner, Walter J
Wilkes, L Faye; Dynamic
model investigation of two tail-sitter vertically rising airplanes to
determine the altitude required to approach normal flight conditions under
power failure in hovering flight; naca-rm-l56h29a; November 09,
1956
- Klunker, E B Harder,
Keith C; Some
considerations of the influence of body cross-sectional shape on the lifting
efficiency of wing-body combinations at supersonic speeds; naca-rm-l56h30;
October 19, 1956
- Croom, Delwin R
Huffman, Jarrett K; Low-speed
pressure-distribution investigation of a thin-delta-wing-fuselage model with
double slotted flap, extended double slotted flap, and canard;
naca-rm-l56i11; November 23, 1956
- Nason, Martin L; A semigraphical
method for the determination of the rolling characteristics of
rolleron-equipped missiles; naca-rm-l56i12; November 29, 1956
- Boatright, William B;
Experimental
study and analysis of loading and pressure distributions on delta wings due to
thickness and to angle of attack at supersonic speeds; naca-rm-l56i14;
December 26, 1956
- Purser, Paul E Hopho,
Russell N; Exploratory
materials and missile-nose-shape tests in a 4,000 F supersonic air jet;
naca-rm-l56j09; December 13, 1956
- El Badrawy, Rashad M.;
Flat plate
cascades at supersonic speed; naca-tm-1369; 1956
- Krasilschchikova, E.
A.; Finite
span wings in compressible flow; naca-tm-1383; 1956
- Busemann, Adolf.; On the gas
dynamics of a rotating impeller; naca-tm-1385; 1956
- Benthem, J. P.; On the buckling
of bars and plates in the plastic range. Part II; naca-tm-1392;
1956
- Deich, M. E.; Flow
of gas through turbine lattices; naca-tm-1393; 1956
- Donov, A. E.; A
flat wing with sharp edges in a supersonic stream; naca-tm-1394;
1956
- Schijve, J.; The
fatigue strength of riveted joints and lugs; naca-tm-1395; 1956
- Kepert, J. L., Payne,
A. O.; Interim report
on fatigue characteristics of a typical metal wing; naca-tm-1397;
1956
- Anton, Leo.; Formation
of a vortex at the edge of a plate; naca-tm-1398; 1956
- ; Aeroelastic
problems of airplane design; naca-tm-1402; 1956
- ; On
the instability of methods for the integration of ordinary differential
equations; naca-tm-1403; 1956
- Anderson, H.L.; Effects of
intermittent versus continuous heating upon the tensile properties of 2024-T4,
6061-T6, and 7075-T6 aluminum alloys; naca-tm-1419; 1956
- Liepmann, H.W.; On the
contribution of turbulent boundary layers to the noise inside a fuselage;
naca-tm-1420; 1956
- ; On
landing gear stresses; naca-tm-1422; 1956
- ; Safegaurds
against flutter of airplanes; naca-tm-1423; 1956
- ; On
the theory of anisotropic shallow shells; naca-tm-1424; 1956
- ; On
the calculation of shallow shells; naca-tm-1425; 1956
- ; On
the theory of thin shallow shells; naca-tm-1426; 1956
- Weick, Fred E.,
Abramson, Norman; Investigation
of lateral control near the stall analysis for required longitudinal trim
characteristics and discussion of design variables; naca-tn-3677;
1956
- Klawans, Bernard B.; A simple method
for calculating the characteristics of the Dutch roll motion of an
airplane; naca-tn-3754; 1956
- Weick, Fred E
(Agricultural and Mechanical College of Texas) Abramson, H Norman
(Agricultural and Mechanical College of Texas); Investigation
of lateral control near the stall flight tests with high-wing and low-wing
monoplanes of various configurations; naca-tn-3676; June 1956
- Edwards, S. Sherman.;
Some
interference effects that influence vertical-tail loads at supersonic
speeds; naca-rm-a55h30; 1956
- Spiegel, Joseph M.,
Lawrence, Leslie F.; A
description of the Ames 2- by 2-foot transonic wind tunnel and preliminary
evaluation of wall interference; naca-rm-a55i21; 1956
- Smith, Willard G.,
Ball, Louis H.; Static
lateral-directional stability characteristics of five contemporary airplane
models from wind-tunnel tests at high subsonic and supersonic speeds;
naca-rm-a55j03; 1956
- Demele, Fred A., Kolbe,
Carl D.; The
effect of trailing-edge bluntness on the performance of a small-scale
supersonic propeller at forward Mach numbers to 0.92; naca-rm-a55j12;
1956
- Hickey, David H.; Full-scale
wind-tunnel tests of the longitudinal stability and control characteristics of
the XV-1 convertiplane in the autorotating flight range; naca-rm-a55k21a;
1956
- Katzen, Elliot D.,
Jorgensen, Leland H.; Aerodynamics
of missiles employing wings of very low aspect ratio; naca-rm-a55l13b;
1956
- Phelps, E. Ray.; Pressure
distributions at Mach numbers of 1.6 and 1.9 of a conically cambered wing of
triangular plan form with and without pylon-mounted engine nacelles;
naca-rm-a56b03; 1956
- Evans, William T.; Data from
large-scale low-speed tests of airplane configurations with a thin 45 degree
swept-wing incorporating several leading-edge contour modifications;
naca-rm-a56b17; 1956
- Sutton, Fred B; The effect of
leading-edge extensions on the longitudinal characteristics at Mach numbers up
to 0.92 of a wing-fuselage-tail combination having a 40 degree sweptback wing
with NACA 64A thickness distribution; naca-rm-a55i29; January 20,
1956
- Griffin, Roy N , Jr
Hickey, David H; Investigation
of the use of area suction to increase the effectiveness of trailing-edge
flaps of various spans on a wing of 45 degree sweepback and aspect ratio
6; naca-rm-a56b27; June 22, 1956
- L. G. Loitsianskii; Boundary
Layer; naca-tm-1400; 1956
- Jacob Zarovsky, Robert
A. Gardiner; Flight
investigation of a roll-stabilized missile configuration at varying angles of
attack at Mach numbers between 0.8 and 1.79; naca-tn-3915; Jan 1957
- Franklin W. Diederich,
Joseph A. Drischler; Effect
of spanwise variations in gust intensity on the lift due to atmospheric
turbulence; naca-tn-3920; Apr 1957
- Andrew Beke; Analytical
investigation of the effect of water injection on supersonic
turbojet-engine-inlet matching and thrust augmentation; naca-tn-3922; Jan
1957
- N. S. Diaconis, John R.
Jack, Richard J. Wisniewski; Boundary-layer
transition at Mach 3.12 as affected by cooling and nose blunting;
naca-tn-3928; Jan 1957
- Kenneth P. Coffin,
Richard S. Brokaw; A
general system for calculating burning rates of particles and drops and
comparison of calculated rates for carbon, boron, magnesium, and
isooctane; naca-tn-3929; Feb 1957
- George E. Glawe, Robert
C. Johnson; Experimental
study of heat transfer to small cylinders in a subsonic, high-temperature gas
stream; naca-tn-3934; May 1957
- Paul M. Ordin; Hydrogen-oxygen
explosions in exhaust ducting; naca-tn-3935; Apr 1957
- Percy J. Bobbitt, Peter
J. Maxie , Jr.; Sidewash
in the vicinity of lifting swept wings at supersonic speeds; naca-tn-3938;
Feb 1957
- John L. Crigler; Comparison of
calculated and experimental load distributions on thin wings at high subsonic
and sonic speeds; naca-tn-3941; Jan 1957
- Vernon Van Hise; Investigation
of variation in base pressure over the Reynolds number range in which wake
transition occurs for nonlifting bodies of revolution at Mach numbers from
1.62 to 2.62; naca-tn-3942; Jan 1957
- Nathaniel B. Cohen; A power-series
solution for the unsteady laminar boundary-layer flow in an expansion wave of
finite width moving through a gas initially at rest; naca-tn-3943; Jun
1957
- Robert L. Trimpi,
Nathaniel B. Cohen; An
integral solution to the flat-plate laminar boundary-layer flow existing
inside and after expansion waves and after shock waves moving into quiescent
fluid with particular application to the complete shock-tube flow;
naca-tn-3944; Jun 1957
- Lloyd J. Fisher, Edward
L. Hoffman; Ditching
investigations of dynamic models and effects of design parameters on ditching
characteristics; naca-tn-3946; Feb 1957
- Homer P. Mason, William
N. Gardner; A limited
correlation of atmospheric sounding data and turbulence experienced by
rocket-powered models; naca-tn-3953; Apr 1957
- John M. Eggleston; A theory for
the lateral response of airplanes to random atmospheric turbulence;
naca-tn-3954; May 1957
- David G. Stone; A collection of
data for zero-lift damping in roll of wing-body combinations as determined
with rocket-powered models equipped with roll-torque nozzles;
naca-tn-3955; Apr 1957
- Joseph A. Drischler,
Franklin W. Diederich; Lift
and moment responses to penetration of sharp-edged traveling gusts, with
application to penetration of weak blast waves; naca-tn-3956; May
1957
- Albert G. Few, Jr.,
Thomas J. King, Jr.; Some
effects of tail height and wing plan form on the static longitudinal stability
characteristics of a small-scale model at high subsonic speeds;
naca-tn-3957; May 1957
- James C. Dunavant; Cascade
investigation of a related series of 6-percent-thick guide-vane profiles and
design charts; naca-tn-3959; May 1957
- C. Frederick Hansen; The erosion of
meteors and high-speed vehicles in the upper atmosphere; naca-tn-3962; Mar
1957
- Donald E. Gault; A correlation
of low-speed, airfoil-section stalling characteristics with Reynolds number
and airfoil geometry; naca-tn-3963; Mar 1957
- John B. Mcdevitt; The linearized
subsonic flow about symmetrical nonlifting wing-body combinations;
naca-tn-3964; Apr 1957
- Warren Winovich, Howard
A. Stine; Measurements of
the nonlinear variation with temperature of heat-transfer rate from hot wires
in transonic and supersonic flow; naca-tn-3965; Apr 1957
- J. Richard Spahr; Theoretical
investigation of the effects of configuration changes on the
center-of-pressure shift of a body-wing-tail combination due to angle of
attack and mach number at transonic speeds; naca-tn-3966; May 1957
- Frank J. Centolanzi; Characteristics
of a 40 degree cone for measuring Mach number, total pressure, and flow angles
at supersonic speeds; naca-tn-3967; May 1957
- Brian F. Doolin; The application
of matrix methods to coordinate transformations occurring in systems studies
involving large motions of aircraft; naca-tn-3968; May 1957
- Morris W. Rubesin,
Mamoru Inouye; A
theoretical study of the effect of upstream transpiration cooling on the
heat-transfer and skin-friction characteristics of a compressible, laminar
boundary layer; naca-tn-3969; May 1957
- John R. Spreiter,
Alberta Y. Alksne; Thin
airfoil theory based on approximate solution of the transonic flow
equation; naca-tn-3970; May 1957
- Vernon J. Rossow; On flow of
electrically conducting fluids over a flat plate in the presence of a
transverse magnetic field; naca-tn-3971; May 1957
- I. Irving Pinkel,
Solomon Weiss, G. Merritt Preston, Gerard J. Pesman; Origin
and prevention of crash fires in turbojet aircraft; naca-tn-3973; May
1957
- Robert C. Kohl, Joseph
S. Algranti; Investigation
of a full-scale, cascade-type thrust reverser; naca-tn-3975; Apr
1957
- Harold R. Mull, John C.
Erickson, Jr.; Survey
of the acoustic near field of three nozzles at a pressure ratio of 30;
naca-tn-3978; Apr 1957
- Paul F. Brinich, Norman
Sands; Effect of
bluntness on transition for a cone and a hollow cylinder at Mach 3.1;
naca-tn-3979; May 1957
- Harold E. Rohlik,
William T. Wintucky; Investigation
of semivaneless turbine stator designed to produce axially symmetrical
free-vortex flow; naca-tn-3980; Apr 1957
- Lewis Laboratory
Computing Staff; Tables
of various Mach number functions for specific-heat ratios from 1.28 to
1.38; naca-tn-3981; Apr 1957
- William R. Mickelsen;
Effect of
standing transverse acoustic oscillations on fuel-oxidant mixing in
cylindrical combustion chambers; naca-tn-3983; May 1957
- Porter J. Perkins,
William Lewis, Donald R. Mulholland; Statistical
study of aircraft icing probabilities at the 700- and 500-millibar levels over
ocean areas in the northern hemisphere; naca-tn-3984; May 1957
- Richard J. Priem; Propellant
vaporization as a criterion for rocket engine design : calculations of chamber
length to vaporize a single n-heptane drop; naca-tn-3985; Jul 1957
- Eli Reshotko, Ivan E.
Beckwith; Compressible
laminar boundary layer over a yawed infinite cylinder with heat transfer and
arbitrary Prandtl number; naca-tn-3986; Jun 1957
- Howard T. Mchenry, H.
B. Probst; Effect of
environments of sodium hydroxide, air, and argon on the stress-rupture
properties of nickel at 1500 F; naca-tn-3987; Jan 1958
- R. J. Priem, G. L.
Borman, M. M. El Wakil, O. A. Uyehara, P. S. Myers; Experimental
and calculated histories of vaporizing fuel drops; naca-tn-3988; Aug
1957
- Donald H. Desy, J. O.
Brittain, M. Gensamer; Strength
and ductility of bainitic steels; naca-tn-3989; Aug 1957
- J. G. Weinberg, J. A.
Bennett; Effect of
crystal orientation on fatigue-crack initiation in polycrystalline aluminum
alloys; naca-tn-3990; Aug 1957
- Martin E. Barzelay,
George F. Holloway; Interface
thermal conductance of twenty-seven riveted aircraft joints; naca-tn-3991;
Jul 1957
- Kermit G. Pratt, Floyd
V. Bennett; Charts for
estimating the effects of short-period stability characteristics on airplane
vertical-acceleration and pitch-angle response in continuous atmospheric
turbulence; naca-tn-3992; Jun 1957
- Stafford W. Wilbur; An
investigation of flow in circular and annular 90 degrees bends with a
transition in cross section; naca-tn-3995; Aug 1957
- Stafford W. Wilbur,
James T. Higginbotham; Investigation
of a short-annular-diffuser configuration utilizing suction as a means of
boundary-layer control; naca-tn-3996; Jun 1957
- K. R. Czarnecki,
Archibald R. Sinclair; A
note on the effect of heat transfer on peak pressure rise associated with
separation of turbulent boundary layer on a body of revolution (NACA RM-10) at
a Mach number of 1.61; naca-tn-3997; Apr 1957
- George W. Brooks, John
E. Baker; An
experimental investigation of the effect of various; naca-tn-4005; Sept
1958
- William A. Brooks, Jr,
George E. Griffith, Kurt H. Strass; Two
factors influencing temperature distributions and thermal stresses in
structures; naca-tn-4052; Jun 1957
- George W. Zender,
Richard A. Pride; The
combinations of thermal and load stresses for the onset of permanent buckling
in plates; naca-tn-4053; Jun 1957
- Louis F. Vosteen,
Robert R. Mcwithey, Robert G. Thomson; Effect
of transient heating on vibration frequencies of some simple wing
structures; naca-tn-4054; Jun 1957
- Thomas L. Coleman,
Harry Press, C. C. Shufflebarger; Effects
of airplane flexibility on wing bending strains in rough air;
naca-tn-4055; Jul 1957
- William H. Phillips; Loads
implications of gust-alleviation systems; naca-tn-4056; Jun 1957
- Delwin R. Croom,
Jarrett K. Huffman; Investigation
at low speeds of deflectors and spoilers as gust alleviators on a model of the
Bell X-5 airplane with 35 degree swept wings and on a high-aspect-ratio 35
degree swept-wing-fuselage model; naca-tn-4057; Jun 1957
- John A. Zalovik; Calculated
effect of some airplane handling techniques on the ground-run distance in
landing on slippery runways; naca-tn-4058; Jul 1957
- Max C. Kurbjun; Noise survey of
a full-scale supersonic turbine-driven propeller under static conditions;
naca-tn-4059; Jul 1957
- Robert W. Herr; A
wide-frequency-range air-jet shaker; naca-tn-4060; Jun 1957
- Andrew G. Swanson,
James J. Buglia, Leo T. Chauvin; Flight
measurements of boundary-layer temperature profiles on a body of revolution
(NACA RM-10) at Mach numbers from 1.2 to 3.5; naca-tn-4061; Jul
1957
- Godwin, William R; Effect of sweep
on performance of compressor blade sections as indicated by swept-blade rotor,
unswept-blade rotor, and cascade tests; naca-tn-4062; Jul 1957
- James N. Mueller; Equations,
tables, and figures for use in the analysis of helium flow at supersonic and
hypersonic speeds; naca-tn-4063; Sep 1957
- William H. Phillips, B.
Porter Brown, James T. Matthews, Jr; Review
and investigation of unsatisfactory control characteristics involving
instability of pilot-airplane combination and methods for predicting these
difficulties from ground tests; naca-tn-4064; Aug 1957
- Ivo M. Kurg; Tensile
properties of Inconel X sheet under rapid-heating and constant-temperature
conditions; naca-tn-4065; Aug 1957
- Bernard B. Klawans,
Jack A. White; A
method utilizing data on the spiral, roll-subsidence, and dutch roll modes for
determining lateral stability derivatives from flight measurements;
naca-tn-4066; Aug 1957
- Richard R. Heldenfels,
Louis F. Vosteen; Approximate
analysis of effects of large deflections and initial twist on torsional
stiffness of a cantilever plate subjected to thermal stresses;
naca-tn-4067; Aug 1957
- Max C. Kurbjun; Effects of
blade plan form on free-space oscillating pressures near propellers at flight
Mach numbers to 0.72; naca-tn-4068; Aug 1957
- Robert O. Schade; Flight-test
investigation on the Langley control-line facility of a model of a
propeller-driven tail-sitter-type vertical-take-off airplane with delta wing
during rapid transitions; naca-tn-4070; Aug 1957
- C. C. Shufflebarger,
Chester B. Payne, George L. Cahen; A
correlation of results of a flight investigation with results of an analytical
study of effects of wing flexibility on wing strains due to gusts;
naca-tn-4071; Aug 1957
- Carl R. Huss, James J.
Donegan; Tables for the
numerical determination of the Fourier transform of a function of time and the
inverse Fourier transform of a function of frequency, with some applications
to operational calculus methods; naca-tn-4073; Oct 1957
- Ivo M. Kurg; Tensile
stress-strain properties of 17-7 PH and AM 350 stainless-steel sheet at
elevated temperatures; naca-tn-4075; Sep 1957
- Leslie W. Lassiter,
Robert W. Hess; Calculated
and measured stresses in simple panels subject to intense random acoustic
loading including the near noise field of a turbojet engine; naca-tn-4076;
Sep 1957
- David F. Thomas, Jr,
Walter D. Wolhart; Static
longitudinal and lateral stability characteristics at low speed of 45 degree
sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6;
naca-tn-4077; Sep 1957
- Neal Tetervin; A
discussion of cone and flat-plate Reynolds numbers for equal ratios of the
laminar shear to the shear caused by small velocity fluctuations in a laminar
boundary layer; naca-tn-4078; Aug 1957
- Edwin E. Davenport; Wind-tunnel
investigation of external-flow jet-augmented double slotted flaps on a
rectangular wing at an angle of attack of 0 degree to high momentum
coefficients; naca-tn-4079; Sep 1957
- John P. Rowe, J. W.
Freeman; Effect of
overheating on creep-rupture properties of S-816 alloy at 1,500 F;
naca-tn-4081; Dec 1957
- R. F. Decker, A. I.
Rush, A. G. Dano, A. G. Freeman; Abnormal
grain growth in nickel-base heat-resistant alloys; naca-tn-4082; Dec
1957
- John P. Rowe, J. W.
Freeman; Effect of
overheating on creep-rupture properties of HS-31 alloy at 1,500 F;
naca-tn-4083; Dec 1957
- R. F. Decker, A. I.
Rush, A. G. Dano, J. W. Freeman; Abnormal
grain growth in M-252 and S-816 alloys; naca-tn-4084; Nov 1957
- Robert D. Ingebo,
Hampton H. Foster; Drop-size
distribution for cross current breakup of liquid jets in airstreams;
naca-tn-4087; Oct 1957
- A. Mendelson, S.
Manson; Practical
solution of plastic deformation problems in elastic-plastic range;
naca-tn-4088; Sep 1957
- Charles E. May; The mechanism
of thermal-gradient mass transfer in the sodium hydroxide-nickel system;
naca-tn-4089; Sep 1957
- Herbert G. Hurrell; Analysis of
shock motion in ducts during disturbances in downstream pressure;
naca-tn-4090; Sep 1957
- William E. Brunk; Experimental
investigation of transpiration cooling for a turbulent boundary layer in
subsonic flow using air as a coolant; naca-tn-4091; Oct 1957
- James P. Lewis, Robert
S. Ruggeri; Experimental
droplet impingement on four bodies of revolution; naca-tn-4092; Dec
1957
- Robert S. Ruggeri,
James P. Lewis; Investigation
of heat transfer from a stationary and rotating conical forebody;
naca-tn-4093; Oct 1957
- John R. Jack, Richard
J. Wisniewski, N. S. Diaconis; Effects
of extreme surface cooling on boundary-layer transition; naca-tn-4094; Oct
1957
- William H. Roudebush;
An analysis
of the effect of several parameters on the stability of an air-lubricated
hydrostatic thrust bearing; naca-tn-4095; Oct 1957
- Rudolph C. Meyer; Flow-turning
losses associated with zero-drag external-compression supersonic inlets;
naca-tn-4096; Oct 1957
- Johnson, Donald F.; Investigation
of some mechanical properties of thermenol compressor blades;
naca-tn-4097; Oct 1957
- Richard J. Priem; Propellant
vaporization as a criterion for rocket-engine design : calculations using
various log-probability distributions of heptane drops; naca-tn-4098; Oct
1957
- Thomas L. Carter; Effect of
lubricant viscosity on rolling-contact fatigue life; naca-tn-4101; Oct
1957
- E. R. G. Eckert,
Patrick L. Donoughe, Betty JO Moore; Velocity
and friction characteristics of laminar viscous boundary-layer and channel
flow over surfaces with ejection or suction; naca-tn-4102; Dec 1957
- Philip M. Edge, Jr; Impact-loads
investigation of chine-immersed model having a circular-arc transverse
shape; naca-tn-4103; Sep 1957
- Frederick C. Grant; The use of pure
twist for drag reduction on arrow wings with subsonic leading edges;
naca-tn-4104; Aug 1957
- P. R. Hill; A
method of computing the transient temperature of thick walls from arbitrary
variation of adiabatic-wall temperature and heat-transfer coefficient;
naca-tn-4105; Oct 1957
- Philip M. Edge, Jr,
John S. Mixson; Impact-loads
investigation of a chine-immersed model having a longitudinally curved bow and
a V-bottom with a dead-rise angle of 30 degrees; naca-tn-4106; Sep
1957
- Richard H. Rhyne,
Harold N. Murrow; Effects
of airplane flexibility on wing strains in rough air at 5,000 feet as
determined by flight tests of a large swept-wing airplane; naca-tn-4107;
Sep 1957
- Norman R. Richardson,
Elmer A. Horton; A
thermal system for continuous monitoring of laminar and turbulent
boundary-layer flows during routine flight; naca-tn-4108; Sep 1957
- William D. Deveikis; Investigation
of the compressive strength and creep of 7075-T6 aluminum-alloy plates at
elevated temperatures; naca-tn-4111; Nov 1957
- George J. Heimerl,
Arthur J. Mcevily, Jr; Generalized
master curves for creep and rupture; naca-tn-4112; Oct 1957
- Wayne D. Erickson; Study of
pressure distributions on simple sharp-nosed models at Mach numbers from 16 to
18 in helium flow; naca-tn-4113; Oct 1957
- James P. Peterson; Weight-strength
studies of structures representative of fuselage construction;
naca-tn-4114; Oct 1957
- William J. O'Sullivan,
Jr; Theory
of aircraft structural models subject to aerodynamic heating and external
loads; naca-tn-4115; Sep 1957
- Raymond D. Vogler,
Thomas R. Turner; Wind-tunnel
investigation at low speeds to determine flow-field characteristics and ground
influence on a model with jet-augmented flaps; naca-tn-4116; Sep
1957
- Herman S. Fletcher; Experimental
investigation of lift, drag, and pitching moment of five annular airfoils;
naca-tn-4117; Oct 1957
- Byron M. Jaquet; Wind-tunnel
investigation of effects of ground proximity and of split flaps on the lateral
stability derivatives of a 60 degree delta-wing model oscillating in yaw;
naca-tn-4119; Sep 1957
- William J. O'Sullivan,
Jr, William R. Wade; Theory
and apparatus for measurement of emissivity for radiative cooling of
hypersonic aircraft with data for Inconel and Inconel X; naca-tn-4121; Oct
1957
- Norman S. Silsby; External
interference effects of a flow through static-pressure orifices of a NACA
airspeed head at a Mach number of 3; naca-tn-4122; Oct 1957
- Melvin F. Markey,
Thomas D. Carpini; Rough-water
impact-load investigation of a chine-immersed V-bottom model having a
dead-rise angle of 10 degrees; naca-tn-4123; Oct 1957
- William A. Newsom, Jr;
Effect of
ground proximity on the aerodynamic characteristics of a four-engine
vertical-take-off-and-landing transport-airplane model with tilting wing and
propellers; naca-tn-4124; Oct 1957
- Ivan E. Beckwith, James
J. Gallagher; Heat
transfer and recovery temperatures on a sphere with laminar, transitional, and
turbulent boundary layers at Mach numbers of 2.00 and 4.15; naca-tn-4125;
Dec 1957
- William Gracey; The measurement
of pressure altitude on aircraft; naca-tn-4127; Oct 1957
- Clifford L. Fricke; A thermocouple
subcarrier oscillator for telemetering temperatures from pilotless
aircraft; naca-tn-4128; Dec 1957
- Martin R. Copp, Walter
G. Walker; Analysis of
operational airline data to show the effects of airborne weather radar on the
gust loads and operating practices of twin-engine short-haul transport
airplanes; naca-tn-4129; Nov 1957
- George C. Ashby, Jr,
John R. Erwin, Wallace M. Schulze; NACA
65-series compressor rotor performance with varying annulus-area ratio,
solidity, blade angle, and Reynolds number and comparison with cascade
results; naca-tn-4130; Oct 1057
- Louis P. Tosti; Transition-flight
investigation of a four-engine-transport vertical-take-off airplane model
utilizing a large flap and extensible vanes for redirecting the propeller
slipstream; naca-tn-4131; Dec 1957
- Richard E. Whaley; Fatigue
investigation of full-scale transport-airplane wings : variable-amplitude
tests with a gust-loads spectrum; naca-tn-4132; Nov 1957
- John R. Spreiter, Alvin
H. Sacks; A
theoretical study of the aerodynamics of slender cruciform-wing arrangements
and their wakes; naca-report-1296; Jan 1957
- Harvard Lomax; Nonlifting
wing-body combinations with certain geometric restraints having minimum wave
drag at low supersonic speeds; naca-report-1297; Jan 1957
- Henry C. Barnett,
Robert R. Hibbard; Basic
considerations in the combustion of hydrocarbon fuels with air;
naca-report-1300; Jan 1957
- Percy J. Bobbitt; Linearized
lifting-surface and lifting-line evaluations of sidewash behind rolling
triangular wings at supersonic speeds; naca-report-1301; jan 1957
- Robert W. Leonard, John
M. Hedgepeth; On
panel flutter and divergence of infinitely long unstiffened and ring-stiffened
thin-walled circular cylinders; naca-report-1302; Jan 1957
- William Gracey; Wind-tunnel
investigation of a number of total-pressure tubes at high angles of attack --
subsonic, transonic, and supersonic speeds; naca-report-1303; jan
1957
- Gerald A. Rainey; Measurement of
aerodynamic forces for various mean angles of attack on an airfoil oscillating
in pitch and on two finite-span wings oscillating in bending with emphasis on
damping in the stall; naca-report-1305; Jan 1957
- A. J. Eggers, Jr.,
Meyer M. Resnikoff; Bodies
of revolution having minimum drag at high supersonic airspeeds;
naca-report-1306; Jan 1957
- William C. Pitts, Jack
N. Nielsen, George E. Kaattari; Lift
and center of pressure of wing-body-tail combinations at subsonic, transonic,
and supersonic speeds; naca-report-1307; Jan 1957
- Eldon E. Mathauser,
William D. Deveikis; Investigation
of the compressive strength and creep lifetime of 2024-T3 aluminum-alloy
plates at elevated temperatures; naca-report-1308; Jan 1957
- Julian D. Maynard,
Leland B. Salters, Jr.; Aerodynamic
characteristics at high speeds of related full-scale propellers having
different blade-section cambers; naca-report-1309; Jan 1957
- Charles H. McLellan,
Mitchel H. Bertram, John A. Moore; An
investigation of four wings of square plan form at a Mach number of 6.9 in the
Langley 11-inch hypersonic tunnel; naca-report-1310; Jan 1957
- Alberta Y. Alksne; Determination
of vortex paths by series expansion technique with application to cruciform
wings; naca-report-1311; Jan 1957
- W. E. Moeckel; Some
effects of bluntness on boundary-layer transition and heat transfer at
supersonic speeds; naca-report-1312; Jan 1957
- Mitchel H. Bertram; Exploratory
investigation of boundary-layer transition on a hollow cylinder at a Mach
number of 6.9; naca-report-1313; Jan 1957
- John H. Povolny, Fred
W. Steffen, Jack G. McArdle; Summary
of scale-model thrust-reverser investigation; naca-report-1314; Jan
1957
- Keith C. Harder, E. B.
Klunker; On
slender-body theory at transonic speeds; naca-report-1315; Jan 1957
- Harvey G. McComb, Jr.;
Torsional
stiffness of thin-walled shells having reinforcing cores and rectangular,
triangular, or diamond cross section; naca-report-1316; Jan 1957
- Rinaldo J. Brun; Cloud-droplet
ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7;
naca-report-1317; Jan 1957
- Max A. Heaslet, John R.
Spreiter; Three-dimensional
transonic flow theory applied to slender wings and bodies;
naca-report-1318; Jan 1957
- Harry H. Heyson, S.
Katzoff; Induced
velocities near a lifting rotor with nonuniform disk loading;
naca-report-1319; Jan 1957
- George J. Nothwang; An evaluation
of four experimental methods for measuring mean properties of a supersonic
turbulent boundary layer; naca-report-1320; Jan 1957
- John M. Eggleston,
Franklin W. Diederich; Theoretical
calculation of the power spectra of the rolling and yawing moments on a wing
in random turbulence; naca-report-1321; Jan 1957
- Harry L. Runyan, Donald
S. Woolston; Method for
calculating the aerodynamic loading on an oscillating finite wing in subsonic
and sonic flow; naca-report-1322; Jan 1957
- Davis H. Crawford,
William D. McCauley; Investigation
of the laminar aerodynamic heat-transfer characteristics of a
hemisphere-cylinder in the Langley 11-inch hypersonic tunnel at a Mach number
of 6.8; naca-report-1323; Jan 1957
- James J. Donegan, Carl
R. Huss; Comparison of
several methods for obtaining the time response of linear systems to either a
unit impulse or arbitrary input from frequency-response data;
naca-report-1324; Jan 1957
- Franklin K. Moore,
Simon Ostrach; Average
properties of compressible laminar boundary layer on flat plate with unsteady
flight velocity; naca-report-1325; Jan 1957
- John E. Yeates, Jr.,
George W. Brooks, John C. Houbolt; Flight
and analytical methods for determining the coupled vibration response of
tandem helicopters; naca-report-1326; Jan 1957
- William J. Alford, Jr.;
Theoretical
and experimental investigation of the subsonic-flow fields beneath swept and
unswept wings with tables or vortex-induced velocities; naca-report-1327;
Jan 1957
- Clarence A. Syvertson,
David H. Dennis; A
second-order shock-expansion method applicable to bodies of revolution near
zero lift; naca-report-1328; Jan 1957
- Edmund E. Callaghan,
Willard D. Coles; Far
noise field of air jets and jet engines; naca-report-1329; Jan 1957
- Henry A. Cole, Jr.,
Stuart C. Brown, Euclid C. Holleman; Experimental
and predicted longitudinal and lateral-directional response characteristics of
a large flexible 35 degree swept-wing airplane at an altitude of 35,000
feet; naca-report-1330; Jan 1957
- F. N. Rhines, W. W.
Bond, M. A. Kissel; Influence
of alloying upon grain-boundary creep; naca-report-1331; Jan 1957
- Irving I. Pinkel,
Edmund G. Rosenberg; Seat
design for crash worthiness; naca-report-1332; Jan 1957
- Harold Mirels; Attenuation
in a shock tube due to unsteady-boundary-layer action; naca-report-1333;
Jan 1957
- Howard J. Childs,
Thaine W. Reynolds, Charles C. Graves; Relation
of turbojet and ramjet combustion efficiency to second-order reaction kinetics
and fundamental flame speed; naca-report-1334; Jan 1957
- Robert T. Jones; Minimum wave
drag for arbitrary arrangements of wings and bodies; naca-report-1335; Jan
1957
- Robert M. Reynolds,
Robert I. Samonds, John H. Walker; An
investigation of single- and dual-rotation propellers at positive and negative
thrust, and in combination with an NACA 1-series D-type cowling at Mach
numbers up to 0.84; naca-report-1336; Jan 1957
- Robert E. Street; Problem of slip
flow in aerodynamics; naca-rm-57a30; Mar 1957
- Richard B. Skoog; An analysis of
the effects of aeroelasticity on static longitudinal stability and control of
a swept-wing airplane; naca-report-1298; Jan 1957
- Robert F. Smiley; Correlation,
evaluation, and extension of linearized theories for tire motion and wheel
shimmy; naca-report-1299; Jan 1957
- Paul C. Simon, Dennis
W. Brown, Ronald G. Huff; Performance
of external-compression bump inlet at Mach numbers of 1.5 and 2.0;
naca-rm-e56l19; Apr 1957
- Fred W. Steffen, Lewis
A. Rodert; Foreign-object
retention and flow characteristics of retractable engine-inlet screens;
naca-rm-e57a15; Jul 1957
- Donald J. Vargo, Philip
N. Parks, Owen H. Davis; Investigation
of a high-performance top inlet to Mach number of 2.0 and at angles of attack
to 20 degrees; naca-rm-e57a21; Mar 1957
- John E. McAulay; Full-scale
free-jet investigation of a two-shock side-inlet diffuser at Mach 2.75 and a
comparison with a single-shock diffuser; naca-rm-e57a31; Apr 1957
- Henry O. Slone, Patrick
L. Donoughe; Analysis of
coolant flow and pressure requirements for a return-flow turbine rotor blade
design using hydrogen, helium, or air as coolant; naca-rm-e57b18; May
1957
- Leonard K. Tower; Thermal
relations for two-phase expansion with phase equilibrium and example for
combustion products of boron-containing fuel; naca-rm-e57c11; may
1957
- Elmer H. Davison; Analysis of
two-spool turboprop-engine characteristics; naca-rm-e57c21; Jun
1957
- Robert E. English,
Peggy L. Yohner; Theoretical
analysis of one-stage windmills for reducing flow distortion;
naca-rm-e57d05; Jun 1957
- Arthur A. Anderson,
Maynard I. Weinstein; Aerodynamic
performance of several techniques for spike-position control of a blunt-lip
nose inlet having internal contraction; Mach numbers of 0.63 and 1.5 to
2.0; naca-rm-e57d15; Sep 1957
- W. E. Moeckel; Oblique-shock
relations at hypersonic speeds for air in chemical equilibrium;
naca-tn-3895; Jan 1957
- Julian H. Allen, A. J.
Eggers, Jr.; A study of the
motion and aerodynamic heating of missiles entering the earth's atmosphere at
high supersonic speeds; naca-tn-4047; Oct 1957
- Julian H. Allen; Motion of a
ballistic missile angularly misaligned with the flight path upon entering the
atmosphere and its effect upon aerodynamic heating, aerodynamic loads, and
miss distance; naca-tn-4048; Oct 1957
- R. F. Decker, John P.
Rowe, J. W. Freeman; Influence
of crucible materials on high-temperature properties of vacuum-melted
nickel-chromium-cobalt alloy; naca-tn-4049; Jun 1957
- Jim J. Jones; Experimental
investigation of attenuation of strong shock waves in a shock tube with
hydrogen and helium as driver gases; naca-tn-4072; Jul 1957
- Bland A. Stein; Compressive
stress-strain properties of 17-7 PH and AM 350 stainless-steel sheet at
elevated temperatures; naca-tn-4074; Aug 1957
- N. S. Diaconis, Richard
J. Wisniewski, John R. Jack; Heat
transfer and boundary-layer transition on two blunt bodies at Mach numbers
3.12; naca-tn-4099; Oct 1957
- Robert W. Hess, Robert
W. Fralich, Harvey H. Hubbard; Studies
of structural failure due to acoustic loading; naca-tn-4050; Jul
1957
- Willard R. Westphal,
William R. Godwin; Comparison
of NACA 65-series compressor-blade pressure distributions and performance in a
rotor and in cascade; naca-tn-3806; Mar 1957
- S. R. Montgomery, J. J.
Braun; Investigation
of rotating stall in a single-stage axial compressor; naca-tn-3823; Jan
1957
- Martin E. Barzelay,
George F. Holloway; Effect
of an interface on transient temperature distribution in composite aircraft
joints; naca-tn-3824; Apr 1957
- I. Flugge-Lotz, C. F.
Taylor; Investigation
of a nonlinear control system; naca-tn-3826; Apr 1957
- Edward M. Grala; Investigation
of the NiAl phase of nickel-aluminum alloys; naca-tn-3828; Jan 1957
- George Gerard, Herbert
Becker; Handbook of
structural stability part III: buckling of curved plates and shells;
naca-tn-3783; Aug 1957
- Max A. Heaslet; The
minimization of wave drag for wings and bodies with given base area or
volume; naca-tn-3289; Jul 1957
- Murray Tobak; On
the minimization of airplane responses to random gusts; naca-tn-3290; Oct
1957
- George Gerard, Herbert
Becker; Handbook of
structural stability part I : buckling of flat plates; naca-tn-3781; Jul
1957
- Eugene Perchonok,
Donald P. Hearth; Effect
of ambient-temperature variation on the matching requirements of inlet-engine
combinations at supersonic speeds; naca-tn-3834; Jan 1957
- Marcus F. Heidmann,
Richard J. Priem, Jack C. Humphrey; A
study of sprays formed by two impinging jets; naca-tn-3835; Mar
1957
- Seiff, Alvin Sommer,
Simon C Canning, Thomas N; Some
experiments at high supersonic speeds on the aerodynamic and boundary-layer
transition characteristics of high-drag bodies of revolution;
naca-rm-a56i05; January 14, 1957
- Peterson, Robert B; Comparison of
experimental and theoretical zero-lift wave-drag results for various
wing-body-tail combinations at Mach numbers up to 1.9; naca-rm-a56i07;
March 27, 1957
- Barnett, Robert M
Kaufman, William M Fulcher, Elmer C; Application
of a windshield-display system to the low-altitude bombing problem;
naca-rm-a56i10; January 04, 1957
- Hickey, Daniel P; Experimental
investigation of a method of wave-drag reduction for combinations employing
quasicylindrical bodies and swept wings at supersonic speeds;
naca-rm-a56i18; February 19, 1957
- Holdaway, George H
Hatfield, Elaine W; Investigation
of symmetric body indentations designed to reduce the transonic zero-lift wave
drag of a 45 degree swept wing with an NACA 64A006 section and with a
thickened leading-edge section; naca-rm-a56k26; March 19, 1957
- Hermach, C A Kraus,
Samuel Reller, John O , Jr; Reductions
in temperature-recovery factor associated with pulsating flows generated by
spike-nosed cylinders at a Mach number of 3.50; naca-rm-a56l05; March 04,
1957
- Peterson, Victor, L
Boyd, John W; Effects
of conical camber on the lift, drag, and pitching-moment characteristics of a
triangular wing of aspect ratio 3.0; naca-rm-a56l18; February 19,
1957
- Mcdevitt, John B
Taylor, Robert A; An
investigation of wing-body juncture interference effects at transonic speeds
for several swept-wing and body combinations; naca-rm-a57a02; May 16,
1957
- Phelps, E Ray Boyd,
John W; A
wind-tunnel investigation of the effects of conical camber for an airplane
configuration having a triangular wing of aspect ratio 2.2;
naca-rm-a57a10; April 30, 1957
- Treon, Stuart L
Knechtel, Earl D; Lateral-directional
aerodynamic characteristics of several coplanar triple-body missile
configurations at Mach numbers from 0.6 to 1.4; naca-rm-a57a25; April 10,
1957
- Evans, William T; Leading-edge
contours for thin swept wings : an analysis of low-and high-speed data;
naca-rm-a57b11; March 29, 1957
- Foster, John V Fulcher,
Elmer C Heinle, Donovan R; An
air-borne target simulator for use with scope-presentation type fire-control
systems; naca-rm-a57c19; May 10, 1957
- Canning, Thomas N
Sommer, Simon C; Investigation
of boundary-layer transition on flat-faced bodies of revolution at high
supersonic speeds; naca-rm-a57c25; June 07, 1957
- Sadoff, Melvin Stewart,
John D Cooper, George E; Analytical
study of the comparative pitch-up behavior of several airplanes and
correlation with pilot opinion; naca-rm-a57d04; June 12, 1957
- Drinkwater, Fred J ,
III White, Maurice D; A
comparison of carrier approach speeds as determined from flight tests and from
pilot-operated simulator studies; naca-rm-a57d30; June 19, 1957
- Migotsky, Eugene Adams,
Gaynor, J; Some properties
of wing and half-body arrangements at supersonic speeds; naca-rm-a57e15;
July 22, 1957
- Spahr, J Richard
Polhamus, Edward C; Aerodynamic
loads on tails at high angles of attack and sideslip; naca-rm-a57e21; July
23, 1957
- Holdaway, George H
Wallace, Minor R , Jr; Investigation
of axially symmetric flow over steps at transonic speeds with comparisons of
estimated and experimental drag results; naca-rm-a57e24; July 22,
1957
- Reller, John O , Jr; Heat transfer
to blunt nose shapes with laminar boundary layers at high supersonic
speeds; naca-rm-a57f03a; August 16, 1957
- Sutton, Fred B
Lautenberger, J Walter, Jr; A
buffet investigation at high subsonic speeds of wing-fuselage-tail
combinations having sweptback wings with NACA 64A thickness distributions,
fences, a leading-edge extension, and body contouring; naca-rm-a57f06a;
August 1957
- Lee, George Summers,
James L; Effects of
string-support interference on the drag of an olgive-cylinder body with and
without a boatail at 0.6 to 1.4 Mach number; naca-rm-a57i09; December 03,
1957
- Hill, William A , Jr;
Experimental
lift of low-aspect-ratio triangular wings at large angles of attack and
supersonic speeds; naca-rm-a57i17; November 20, 1957
- Neice, Stanford E
Carson, James A Cunningham, Bernard E; Experimental
investigation of the simulation of atmospheric entry of ballistic
missiles; naca-rm-a57i26; December 12, 1957
- Dennis, David H; The effects of
boundary-layer separation over bodies of revolution with conical tail
flares; naca-rm-a57i30; December 12, 1957
- Nussdorfer, T J
Sederstrom, D C Perchonok, E; Investigation
of combustion in 16-inch ram jet under simulated conditions of high altitude
and high Mach number; naca-rm-e50d04; June 27, 1957
- Schafer, Louis J , Jr
Stepka, Francis S; Results
of turbojet engine operation tests using a 50-50 mixture of JP-4 and tributyl
borate as the fuel; naca-rm-e52l17a; January 16, 1957
- Heidmann, M F; A
study of injection processes for 15-percent fluorine - 85-percent oxygen and
heptane in a 200-pound-thrust rocket engine; naca-rm-e56j11; January 15,
1957
- Spakowski, A E Graab,
J; Identification
of foreign objects damaging compressor blades in turbojet engines;
naca-rm-e56j12; January 07, 1957
- Beke, Andrew; Experimental
investigation of water injection in subsonic diffuser of a conical inlet
operation at free-stream Mach number of 2.5; naca-rm-e56j15; January 15,
1957
- Huff, Ronald G
Anderson, Arthur R; Internal
performance of several auxiliary air inlets immersed in a turbulent boundary
layer at Mach numbers of 1.3, 1.5, and 2.0; naca-rm-e56j18; January 18,
1957
- Norgren, Carl T; Performance of
an experimental annular turbojet combustor with methane and propane;
naca-rm-e56j22; January 16, 1957
- Hearth, Donald P; Use of
main-inlet bypass to supply ejector exhaust nozzle at supersonic speeds;
naca-rm-e56k08; February 28, 1957
- Connors, James F Meyer,
Rudolph C; Investigation
of an asymmetric 'penshape' exit having circular projections and discharging
into quiescent air; naca-rm-e56k09a; January 24, 1957
- Huff, Vearl N Gordon,
Sanford; Theoretical
rocket performance of JP-4 fuel with mixtures of liquid ozone and
fluorine; naca-rm-e56k14; January 28, 1957
- Shillito, Thomas B
Koffel, William K; Experimental
investigation of ejector-nozzle metal temperatures; naca-rm-e56k20;
February 27, 1957
- Price, Harold G , Jr
Douglass, Howard W; Material
compatibility with gaseous fluorine; naca-rm-e56k21; January 23,
1957
- Musial, Norman T; Comparison of
effect of a turbojet engine and three cold-flow configurations on the
stability of a full-scale supersonicle inlet; naca-rm-e56k23; January 24,
1957
- Livingood, John N B
Diaguila, Anthony J; A
method for determining core dimensions of heat exchanger with one dominating
film resistance and verification with experimental data; naca-rm-e56k26a;
January 28, 1957
- Schueller, Carl F
Stitt, Leonard E; An
inlet design concept to reduce flow distortion at angle of attack;
naca-rm-e56k28b; February 26, 1957
- Valerino, Alfred S
Zappa, Robert F; Investigation
of mass-flow and pressure recovery characteristics of several underslung
scoop-type inlets at free-stream Mach numbers of 2.0, 1.8, 1.5, and 0.66;
naca-rm-e56k29; March 13, 1957
- Beale, William T
Povolny, John H; Internal
performance of two-dimensional wedge exhaust nozzles; naca-rm-e56k29b;
February 28, 1957
- Rabb, Leonard
Krasnican, Milan J; Observation
of laminar flow on an air-launched 15 degree cone-cylinder at local Reynolds
numbers to 50 x 10(exp 6) at peak Mach number of 6.75; naca-rm-e56l03;
March 04, 1957
- Luidens, Roger W; Arrangements of
jet engine and airframe for increased range; naca-rm-e56l04; July 26,
1957
- Osborn, Walter M Smith,
Kenneth J Hamrick, Joseph T; Design
and test of mixed-flow impellers VIII : comparison of experimental results for
three impellers with shroud redesigned by rapid approximate method;
naca-rm-e56l07; February 27, 1957
- Fortini, Anthony Huff,
Vearl N; Theoretical
performance of liquid hydrogen and liquid fluorine as a rocket propellant for
a chamber pressure of 600 pounds per square inch absolute;
naca-rm-e56l10a; January 25, 1957
- Wise, Paul H Lipschitz,
Abraham; Comparison of
combustion reactivity of ethyldecaborane fuels with typical hydrocarbon fuels
on basis of spray flammability limits of fuel-rich mists and calculated
lean-limit flame temperatures for fuel vapor-air systems; naca-rm-e56l12;
February 27, 1957
- Rosenblum, Louis; Thermal
decomposition of some group I, II, and III metal alkyls; naca-rm-e56l18;
February 15, 1957
- Tannenbaum, Stanley; The heat of
combustion of tetraethyldiborane; naca-rm-e53e11; January 16, 1957
- Fletcher, Edward A; Spontaneous
flammability of pentaborane and pentaborane-3-methylpentane blends;
naca-rm-e53i17; February 13, 1957
- Disher, John H Rabb,
Leonard; Initial
performance investigation of pentaborane fuel in free-flight ram-jet
engine; naca-rm-e54d28; January 24, 1957
- Setze, Paul C; A
study of liquid boric oxide particle growth rates in a gas stream from a
simulated jet engine combustor; naca-rm-e55i20a; April 30, 1957
- Curren, Arthur N
Cochran, Reeves P; A
balanced-pressure sliding seal used for transfer of pressurized air between
stationary and rotating parts; naca-rm-e56i11; January 09, 1957
- Mitchell, Glenn A
Campbell, Robert C; Performance
of a supersonic ramp-type side inlet with ram-scoop throat bleed and varying
fuselage boundary-layer removal : Mach number range 1.5 to 2.0 / Glenn A.
Mitchell and Robert C. Campbell; naca-rm-e56i26; January 17, 1957
- Wise, George A
Sterbentz, William H; Investigation
of shock-boundary-layer interaction on the spike of a conical-spike nose
inlet; naca-rm-e56i26a; January 09, 1957
- Mcaulay, John E Prince,
William R; Some operating
experience and problems encountered during operation of a free-jet
facility; naca-rm-e56j02; February 13, 1957
- Hearth, Donald P
Musial, Norman T; Investigation
of a supersonic-inlet - turbojet-engine combination at Mach 2.0 and angles of
attack up to 6 degrees; naca-rm-e57d18; July 1957
- Drell, Isadore L
Belles, Frank E; Survey
of hydrogen combustion properties; naca-rm-e57d24; July 26, 1957
- Schmidt, Harold W; Reaction of
fluorine with carbon as a means of fluorine disposal; naca-rm-e57e02; July
18, 1957
- Baughman, L Eugene
Kochendorfer, Fred D; Jet
effects on base pressures of conical afterbodies at Mach 1.91 and 3.12;
naca-rm-e57e06; August 12, 1957
- Rohlik, Harold E
Wintucky, William T Scribbe, Herbert W; Investigation
of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow
study II : design and experimental performance of turbine with
low-velocity-turning stator and standard rotor; naca-rm-e57e09; July 18,
1957
- Neu, Richard F; Injection
principles for liquid oxygen and heptane using nine-element injectors in an
1800-pound-thrust rocket engine; naca-rm-e57e13; July 18, 1957
- Dorsch, Robert G
Serafini, John S Fletcher, Edward A; Exploratory
investigation of aerodynamic effects of external combustion of aluminum
borohydride in airstream adjacent to flat plate in Mach 2.46 tunnel;
naca-rm-e57e16; July 29, 1957
- Krasnican, M J
Wisniewski, R J; Free-flight
determination of boundary-layer transition and heat transfer for a
hemisphere-cylinder at Mach numbers to 5.6; naca-rm-e57f10; October 21,
1957
- Trout, Arthur M Papell,
S Stephen Povolny, John H; Internal
performance of several divergent-shroud ejector nozzles with high divergence
angles; naca-rm-e57f13; October 02, 1957
- King, Charles R; A semiempirical
correlation of afterburner combustion efficiency and lean-blowout
fuel-air-ratio data with several afterburner-inlet variables and afterburner
lengths; naca-rm-e57f26; September 17, 1957
- Disher, John H; Flight
investigation of pentaborane fuel in rocket boosted 9.75-inch-diameter ramjet
engine with convergent-divergent exhaust nozzle; naca-rm-e57f27; September
17, 1957
- Gelder, Thomas F; Total-pressure
distortion and recovery of supersonic nose inlet with conical centerbody in
subsonic icing conditions; naca-rm-e57g09; September 17, 1957
- Gordon, Sanford
Drellishak, Kenneth S; Theoretical
rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming
frozen composition; naca-rm-e57g16a; November 13, 1957
- Price, Harold G , Jr
Douglass, Howard W; Nonmetallic
material compatibility with liquid fluorine; naca-rm-e57g18; October 02,
1957
- Morrell, Gerald; Summary of NACA
research on ignition lag of self-igniting fuel - nitric acid propellants;
naca-rm-e57g19; October 03, 1957
- Samanich, Nick E; Pressure drag
of axisymmetric cowls having large initial lip angles at Mach numbers from
1.90 to 3.88; naca-rm-e57g24; October 21, 1957
- Morrell, Gerald
Ladanyi, Dezso J; Chemical
igniters for starting jet fuel - nitric acid rockets; naca-rm-e57g26;
October 08, 1957
- Connors, James F Wise,
George A; Performance of
a translating-double-cone axisymmetric inlet with cowl bypass at Mach numbers
from 2.0 to 3.5; naca-rm-e57h07b; November 13, 1957
- Hurrell, Herbert G; Simplified
theory for dynamic relation of ramjet pressures and fuel flow;
naca-rm-e57i13; 1957
- Larson, Terry J
Stillwell, Wendell H Armistead, Katharine H; Static-pressure
error calibrations for nose-boom airspeed installations of 17 airplanes;
naca-rm-h57a02; March 13, 1957
- Saltzman, Edwin J; Flight-determined
induction-system and surge characteristics of the YF-102 airplane with a
two-spool turbojet engine; naca-rm-h57c22; June 28, 1957
- Purser, Paul E Fields,
E M; Some
research on the lift and stability of wing-body combinations;
naca-rm-l55g06a; July 02, 1957
- Pride, Richard A Hall,
John B , Jr Anderson, Melvin S; Effects
of rapid heating on strength of airframe components; naca-tn-4051; June
1957
- Love, Eugene S; A reexamination
of the use of simple concepts for predicting the shape and location of
detached shock waves; naca-tn-4170; December 1957
- Aiken, William S , Jr;
Analysis of
horizontal-tail loads in pitching maneuvers on a flexible swept-wing jet
bomber; naca-tn-4191; December 1957
- Houbolt, John C Brooks,
George W; Differential
equations of motion for combined flapwise bending, chordwise bending, and
torsion of twisted nonuniform rotor blades; naca-tn-3905; February
1957
- Vaughan, Victor L , Jr
Ramsen, John A; Hydrodynamic
characteristics over a range of speeds up to 80 feet per second of a
rectangular modified flat plate having an aspect ratio of 0.25 and operating
at several depths of submersion; naca-tn-3908; April 1957
- Smiley, Robert F Horne,
Walter B; Vertical
force-deflection characteristics of a pair of 56-inch-diameter aircraft tires
from static and drop tests with and without prerotation; naca-tn-3909;
February 1957
- Lovell, Powell M , Jr
Parlett, Lysle P; Flight
tests of a model of a high-wing transport vertical-take-off airplane with
tilting wing and propellers and with jet controls at the rear of the fuselage
for pitch and yaw control; naca-tn-3912; March 1957
- Sylvester, Maurice A
Baker, John E; Some
experimental studies of panel flutter at Mach number 1.3; naca-tn-3914;
February 1957
- Newsom, William A , Jr;
Effect of
propeller location and flap deflection on the aerodynamic characteristics of a
wing-propeller combination for angles of attack from 0 degrees to 80
degrees; naca-tn-3917; 1957
- Kuhn, Richard E Hayes,
William C , Jr; Wind-tunnel
investigation of effect of propeller slipstreams on aerodynamic
characteristics of a wing equipped with a 50-percent-chord sliding flap and a
30-percent-chord slotted flap; naca-tn-3918; February 1957
- Kuhn, Richard E; Investigation
of effectiveness of a wing equipped with a 50-percent-chord sliding flap, a
30-percent-chord slotted flap, and a 30-percent-chord slat in deflecting
propeller slipstreams downward for vertical take-off; naca-tn-3919;
1957
- Castles, Walter, Jr
(Georgia Institute of Technology); Approximate
solution for streamlines about a lifting rotor having uniform loading and
operating in hovering or low-speed vertical-ascent flight conditions;
naca-tn-3921; February 1957
- Wenzel, L M Hart, C E
Craig, R T; Experimental
comparison of speed : fuel-flow and speed-area controls on a turbojet engine
for small step disturbances; naca-tn-3926; March 1957
- Robins, Leonard Grala,
Edward M; Preliminary
investigation of the effect of surface treatment on the strength of a titanium
carbide - 30 percent nickel base cermet; naca-tn-3927; February
1957
- Probst, H B Mchenry,
Howard T; A
study of the "toss factor" in the impact testing of cermets by the Izod
pendulum test; naca-tn-3931; February 1957
- Russell, Walter E
Wisner, John P; An
investigation of high-temperature vacuum and hydrogen furnace brazing;
naca-tn-3932; March 1957
- Hart, C E Wenzel, L M
Craig, R T; Experimental
investigation of temperature feedback control systems applicable to
turbojet-engine control; naca-tn-3936; March 1957
- Felix, A Richard Emery,
James C; A
comparison of typical National Gas Turbine Establishment and NACA axial-flow
compressor blade sections in cascade at low speed; naca-tn-3937; March
1957
- Edge, Philip M , Jr; Impact-loads
investigation of chine-immersed models having concave-convex transverse shape
and straight or curved keel lines; naca-tn-3940; February 1957
- Gustafson, F B
Tapscott, Robert J; Methods
for obtaining desired helicopter stability characteristics and procedures for
stability predictions; naca-tn-3945; February 1957
- Salmirs, Seymour
Tapscott, Robert J; Instrument
flight trials with helicopter stabilized in attitude about each axis
individually; naca-tn-3947; 1957
- Clevenson, Sherman A
Tomassoni, John E; Experimental
investigation of the oscillating forces and moments on a two-dimensional wing
equipped with an oscillating circular-arc spoiler; naca-tn-3949; March
1957
- Christopher, Kenneth W;
Investigation
of the planing lift of a flat plate at speeds up to 170 feet per second;
naca-tn-3951; March 1957
- Hedgepeth, John M
Waner, Paul G , Jr; Analysis
of static aeroelastic behavior of low-aspect-ratio rectangular wings;
naca-tn-3958; April 1957
- Diederich, Franklin W;
Expected
numbers of maxima and minima of a stationary random process with non-Gaussian
frequency distribution; naca-tn-3960; April 1957
- Jaquet, Byron M
Fletcher, H S; Effect
of fuselage length and a canopy on the static longitudinal and lateral
stability characteristics of 45 degrees sweptback airplane models having
fuselages with square cross sections; naca-tn-3961; April 1957
- Valluri, S R
(California Institute of Technology); Effect
of frequency and temperature on fatigue of metals; naca-tn-3972; February
1957
- Coles, Willard D
Callaghan, Edmund E; Full-scale
investigation of several jet-engine noise-reduction nozzles; naca-tn-3974;
April 1957
- Dance, James H Clauss,
Francis J; Rupture
strength of several nickel-base alloys in sheet form; naca-tn-3976; April
1957
- Fine, Burton; Further
experiments on the stability of laminar and turbulent hydrogen-air flames at
reduced pressures; naca-tn-3977; April 1957
- Von Glahn, Uwe H; Exploratory
study of ground proximity effects on thrust of annular and circular
nozzles; naca-tn-3982; April 1957
- Peters, Roger W Kuhn,
Paul; Bursting
strength of unstiffened pressure cylinders with slits; naca-tn-3993; April
1957
- Illg, Walter Mcevily,
Arthur J , Jr; Static
strength of cross-grain 7075-T6 aluminum-alloy extruded bar containing fatigue
cracks; naca-tn-3994; April 1957
- LOVE EUGENE S; Base
pressure at supersonic speeds on two-dimensional airfoils and on bodies of
revolution with and without fins having turbulent boundary layers;
naca-tn-3819; 1957
- Reinhart, F W (National
Bureau of Standards) Good, C L (National Bureau of Standards) Turner, P S
(National Bureau of Standards) Wolock, I (National Bureau of Standards); Comparison of
mechanical properties of flat sheets, molded shapes, and postformed shapes of
cotton-fabric phenolic laminates; naca-tn-3825; 1957
- Mordfin, Leonard
(National Bureau of Standards) Legate, Alvin C (National Bureau of Standards);
Creep
behavior of structural joints of aircraft materials under constant loads and
temperatures; naca-tn-3842; 1957
- Coletti, Donald E; Experimental
investigation of the forces and moments due to sideslip of a series of
triangular vertical- and horizontal-tail combinations at Mach numbers of 1.62,
1.93, and 2.41; naca-tn-3846; March 1957
- Powell, Robert D , Jr;
The effect
of forward-flight speed on the propulsive characteristics of a pulse-jet
engine mounted on a helicopter rotor; naca-tn-3855; 1957
- Herzig, Howard Z
Hansen, Arthur G; On
possible similarity solutions for three-dimensional incompressible laminar
boundary layers III : similarity with respect to stationary polar coordinates
for small angle variation; naca-tn-3890; 1957
- Anderson, William J; Performance of
110-millimeter-bore M-1 tool steel ball bearings at high speeds, loads, and
temperatures; naca-tn-3892; 1957
- Probst, H B Mchenry,
Howard T; A
study of the impact behavior of high-temperature materials; naca-tn-3894;
March 1957
- Pridmore-Brown, David C
(Massachusetts Institute of Technology); Propagation
of sound into a wind-created shadow zone; naca-rm-57b25; April 22,
1957
- Erickson, Burton :
(Polytechnic Institute of Brooklyn) Patel, Sharad A : (Polytechnic Institute
of Brooklyn) French, Francis W : (Polytechnic Institute of Brooklyn) Lederman,
Samuel : (Polytechnic Institute of Brooklyn) Hoff, N J : (Polytechnic
Institute; Experimental
investigation of creep bending and buckling of thin circular cylindrical
shells; naca-rm-57e17; July 23, 1957
- Gillis, Clarence L
Mitchell, Jesse L; Determination
of longitudinal stability and control characteristics from free-flight model
tests with results at transonic speeds for three airplane configurations;
naca-report-1337; 1957
- Howes, Walton L
Callaghan, Edmund E Coles, Willard D Mull, Harold R; Near
noise field of a jet-engine exhaust; naca-report-1338; 1957
- Furlong, G Chester
Mchugh, James G; A
summary and analysis of the low-speed longitudinal characteristics of swept
wings at high Reynolds number; naca-report-1339; 1957
- Adamson, David
Boatright, William B; Investigation
of downwash, sidewash, and Mach number distribution behind a rectangular wing
at a Mach number of 2.41; naca-report-1340; 1957
- Ewing, John F Freeman,
J W; Influence of
hot-working conditions on high-temperature properties of a heat-resistant
alloy; naca-report-1341; 1957
- Creer, Brent Y; An analog
computer study of several stability augmentation schemes designed to alleviate
roll-induced instability; naca-rm-a56h30; February 19, 1957
- Buell, Donald A Reed,
Verlin D Lopez, Armando E; The
static and dynamic-rotary stability derivatives at subsonic speeds of an
airplane model with an unswept wing and a high horizontal tail;
naca-rm-a56i04; January 14, 1957
- James, Harry A Maki,
Ralph L; Wind-tunnel
tests of the static longitudinal characteristics at low speed of a swept-wing
airplane with blowing flaps and leading-edge slats; naca-rm-a57d11; July
05, 1957
- Buell, Donald A Kolbe,
Carl D; The
effects at subsonic speeds of wing fences and a tail on the longitudinal
characteristics of a 63 degree swept-wing fuselage combination;
naca-rm-a57e02; July 02, 1957
- Anderson, Seth B Faye,
Alan E , Jr; Flight
investigation of the low-speed characteristics of a 35 degree swept-wing
airplane equipped with an area-suction ejector flap and various wing
leading-edge devices; naca-rm-a57g10; September 26, 1957
- Holdaway, George H
Wallace, Minor R , Jr Hatfield, Elaine W; A
transonic investigation of the effects of semisubmerged-store cavities and of
slots on the zero-lift drag of a body of revolution; naca-rm-a57h19a;
October 28, 1957
- Koenig, David G Aoyagi,
Kiyoshi; The
use of a leading-edge area-suction flap and leading-edge modifications to
improve the high-lift characteristics of an airplane model with a wing of 45
degree sweep and aspect ratio 2.8; naca-rm-a57h21; November 04,
1957
- Mcfadden, Norman M
Pauli, Frank A Heinle, Frank A; A
flight study of longitudinal-control-system dynamic characteristics by the use
of a variable-control-system airplane; naca-rm-a57l10; 1957
- Chauvin, Leo T; Temperature
measurements from a flight test of two wing-body combinations at 7 degree
angle of attack for Mach numbers to 4.86 and Reynolds numbers to 19.2 X 10(exp
6); naca-rm-l57f27; September 12, 1957
- Nelson, Robert L Welsh,
Clement J; Some examples
of the applications of the transonic and supersonic area rules to the
prediction of wave drag; naca-rm-l56d11; March 20, 1957
- Leiss, Abraham
Bressette, Walter E; Pressure
distribution induced on a flat plate by a supersonic and sonic jet exhaust at
a free-stream Mach number of 1.80; naca-rm-l56i06; January 10, 1957
- Few, Albert G , Jr
Fournier, Paul G; Wind-tunnel
investigation of the aerodynamic characteristics of a series of swept, highly
tapered thin wings at transonic speeds : transonic bumb method;
naca-rm-l56i24; January 04, 1957
- Barlett, Walter A , Jr
Merlet, Charles F; Flight
investigation of a ram jet burning magnesium slurry fuel and having a conical
shock inlet designed for a Mach number of 4.1; naca-rm-l56i24a; January
22, 1957
- Morris, Odell A; Aerodynamic
forces and moments on a large ogive-cylinder store at various locations below
the fuselage center line of a swept-wing bomber configuration at a Mach number
of 1.61; naca-rm-l56i25; January 14, 1957
- Potter, Dexter M; Measurements of
runway roughness of four commercial airports; naca-rm-l56i26; January 07,
1957
- Alford, William J King,
Thomas, Jr; Experimental
static aerodynamic forces and moments at high subsonic speeds on a missile
model during simulated launching from the midsemispan location of a 45 degree
sweptback wing-fuselage-pylon combination; naca-rm-l56j05; January 10,
1957
- Mayer, John P Hamer,
Harold A; Applications of
power spectral analysis methods to maneuver loads obtained on jet fighter
airplanes during service operations; naca-rm-l56j15; January 15,
1957
- Guy, Lawrence D; Hinge-moment
and effectiveness characteristics of an aspect-ratio-8.2 flap-type control on
a 60 degree delta wing at Mach numbers from 0.72 to 1.96; naca-rm-l56j17;
January 07, 1957
- Howell, Robert R
Braslow, Albert L; Experimental
study of the effects of scale on the absolute values of zero-lift drag of
aircraft configurations at transonic speeds; naca-rm-l56j29; February 08,
1957
- Wood, Charles C; Basic
performance characteristics of several subsonic-diffuser-bypass-duct
combinations for use with supersonic inlets; naca-rm-l56j31; January 21,
1957
- Lee, Dorothy B; Flight
performance of a 2.8 KS 8100 Cajun solid-propellant rocket motor;
naca-rm-l56k01; January 21, 1957
- Henry, Beverly Z , Jr
Cahn, Maurice S; Pressure
distribution over a series of related afterbody shapes as affected by a
propulsive jet at transonic speeds; naca-rm-l56k05; January 22,
1957
- Brissenden, Roy F
Cheatham, Donald C Champine, Robert A; Tolerable
limits of oscillatory accelerations due to rolling motions experienced by one
pilot during automatic-interceptor flight tests; naca-rm-l56k20; January
25, 1957
- Silhan, Frank V
Cubbage, James M , Jr; Drag
of conical and circular-arc boattail afterbodies at Mach numbers from 0.6 to
1.3; naca-rm-l56k22; January 22, 1957
- Felix, A Richard
Savage, Melvyn; Investigation
of a high-performance axial-flow compressor transonic inlet rotor designed for
37.5 pounds per second per square foot of frontal area : detailed
blade-element performance; naca-rm-l56k23; April 12, 1957
- Croom, Delwin R
Huffman, Jarrett K; Low-speed
pressure-distribution investigation of a thin-delta-wing-fuselage model having
double slotted flaps and spoilers; naca-rm-l56l07; February 26,
1957
- Merlet, Charles F
Rumsey, Charles B; Supersonic
free-flight measurement of heat transfer and transition on a 10 degree cone
having a low temperature ratio; naca-rm-l56l10; January 31, 1957
- Lindsey, Walter F
Pitts, Robert G; Two-dimensional
transonic investigation of flows and forces on a 9-percent-thick airfoil with
30-percent-chord flap; naca-rm-l56l11; February 19, 1957
- Henning, Allen B
Wineman, Andrew R Rainey, Robert W; Some
data on body and jet reaction controls; naca-rm-l56l17; March 04,
1957
- Hoffman, Sherwood; Zero-lift drag
of a large fuselage cavity and a partially submerged store on a 52.5 degree
sweptback-wing-body configuration as determined from free-flight tests at Mach
numbers of 0.7 to 1.53; naca-rm-l56l21; February 26, 1957
- Schult, Eugene D; Some
characteristics of roll controls having possible application to fin-stabilized
ammunition; naca-rm-l57a04; March 27, 1957
- Gracey, William; Measurement of
static pressure on aircraft; naca-rm-l57a09; April 1957
- Gillespie, Warren JR;
Supersonic
aerodynamic characteristics of a low-drag aircraft configuration having an
arrow wing of aspect ratio 1.86 and a body of fineness ratio 20;
naca-rm-l57a25; March 19, 1957
- Letko, William; Experimental
determination at subsonic speeds of the oscillatory and static lateral
stability derivatives of a series of delta wings with leading-edge sweep from
30 to 86.5 degrees; naca-rm-l57a30; April 12, 1957
- Lundstrom, Reginald R;
Stability of
two rocket-propelled models having aspect-ratio-5 unswept tails on a long body
for the Mach number range of 1.7 to 2.4; naca-rm-l57a31a; March 27,
1957
- Lord, Douglas R
Czarnecki, K R; Hinge-moment
characteristics for a series of controls and balancing devices on a 60 degree
delta wing at Mach numbers of 1.61 and 2.01; naca-rm-l57b01; April 12,
1957
- Alford, William J King,
Thomas J , Jr; Experimental
static aerodynamic forces and moments at high subsonic speeds on a missile
model during simulated launching from unswept-, sweptback and
modified-delta-wing-fuselage combinations at zero sideslip;
naca-rm-l57b04; March 19, 1957
- Dennard, John S; A transonic
investigation of the mass-flow and pressure recovery characteristics of
several types of auxiliary air inlets; naca-rm-l57b07; April 10,
1957
- Chauvin, Leo T Buglia,
James J; Measurement of
aerodynamic heat transfer to a deflected trailing-edge flap on a delta fin in
free flight at Mach numbers from 1.5 to 2.6; naca-rm-l57b20; April 10,
1957
- Cubbage, James M , Jr;
Jet effects
on the drag of conical afterbodies for Mach numbers of 0.6 to 1.28;
naca-rm-l57b21; April 12, 1957
- Blanchard, Willard S ,
Jr Hoffman, Sherwood; A
flight investigation to determine the effectiveness of Mach number 1.0, 1.2,
and 1.41 fuselage indentations for reducing the pressure drag of a 45 degree
sweptback wing configuration at transonic and low supersonic speeds;
naca-rm-l57b27; May 16, 1957
- Bland, William M , Jr
Bressette, Walter E; Some
effects of heat transfer at Mach number 2.0 at stagnation temperatures between
2,310 and 3,500 R on a magnesium fin with several leading-edge
modifications; naca-rm-l57c14; April 18, 1957
- Carter, Howard S
Bressette, Walter E; Heat-transfer
and pressure distribution on six blunt noses at a Mach number of 2;
naca-rm-l57c18; April 18, 1957
- Schult, Eugene D; Free-flight
performance of a rotating-vane-spoiler roll control system with low actuating
forces; naca-rm-l57c21; May 10, 1957
- Buglia, James J; Heat transfer
and boundary-layer transition on a highly polished hemisphere-cone in free
flight at Mach numbers up to 3.14 and Reynolds numbers up to 24 x 10(exp
6); naca-rm-l57d05; April 18, 1957
- Swihart, John M Foss,
Willard E , Jr; Transonic
loads characteristics of a 3-percent-thick 60 degree delta-wing-body
combination; naca-rm-l57d12; May 28, 1957
- Penland, Jim A Carroll,
C Maria; Static
longitudinal and lateral stability parameters of three flared-skirt two-stage
missile configurations at a Mach number of 6.86; naca-rm-l57d15; June 05,
1957
- Hall, James R Speegle,
Katherine C Piland, Robert O; Preliminary
results from a free-flight investigation of boundary-layer transition and heat
transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach
numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x
10(exp; naca-rm-l57d18c; May 16, 1957
- Robinson, Ross B; Aerodynamic
characteristics of missile configurations with wings of low aspect ratio for
various combinations of forebodies, afterbodies, and nose shapes for combined
angles of attack and sideslip at a Mach number of 2.01; naca-rm-l57d19;
June 25, 1957
- Bressette, Walter E
Leiss, Abraham; Effects
on adjacent surfaces from the firing of rocket jets; naca-rm-l57d19a; June
12, 1957
- Feller, William V; Heat transfer
to bodies at angles of attack; naca-rm-l57d19c; June 19, 1957
- Faget, Maxime A; The sine-cosine
method for reducing the interference pressure drag of sweptback wings;
naca-rm-l57d24; July 02, 1957
- Grant, Frederick C
Mugler, John P , Jr; Span
loadings due to wing twist at transonic and supersonic speeds;
naca-rm-l57d24a; July 12, 1957
- Swihart, John M
Crabill, Norman L; Steady
loads due to jet interference on wings, tails, and fuselages at transonic
speeds; naca-rm-l57d24b; May 22, 1957
- Henning, Allen B; Effects of wing
inboard plan-form modifications on lift, drag, and longitudinal stability at
Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a
52.5 degree sweptback wing of aspect ratio 3; naca-rm-l57d29; June 19,
1957
- Fischetti, Thomas L; Investigation
at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a
thin 45 degree sweptback highly tapered wing in combination with basic and
indented bodies; naca-rm-l57d29a; June 28, 1957
- Smith, Fred M; Experimental
and theoretical aerodynamic characteristics of two low-aspect-ratio delta
wings at angles of attack to 50 degrees at a Mach number of 4.07;
naca-rm-l57e02; July 10, 1957
- Hall, James R Speegle,
Katherine C; Limited
heat-transfer, drag, and stability results from an investigation at Mach
numbers up to 9 of a large rocket-propelled 10 degree cone;
naca-rm-l57e08; July 22, 1957
- Leiss, Abraham; Design and
evaluation of a turbojet-exhaust simulator with a solid-propellant rocket
motor for free-flight research; naca-rm-l57e10a; July 05, 1957
- Gapcynski, John P
Carlson, Harry W; The
aerodynamic characteristics of a body in the two-dimensional flow field of a
circular-arc wing at a Mach number of 2.01; naca-rm-l57e14; July 02,
1957
- Garland, Benjamine J
Swanson, Andrew G Speegle, Katherine C; Aerodynamic
heating and boundary-layer transition on a 1/10-power nose shape in free
flight at Mach numbers up to 6.7 and free-stream Reynolds numbers up tp 16 x
10(exp 6); naca-rm-l57e14a; June 17, 1957
- Trescot, Charles D ,
Jr; Investigation
at transonic speeds of the effects of inlet-lip sweep on the internal-flow
characteristics of a semielliptical air inlet with an inlet-lip stagger of 30
degrees; naca-rm-l57e16; July 23, 1957
- Hopko, Russell N Trout,
Otto F , Jr; Exploratory
tests of the behavior of several materials in a supersonic air jet at 4,000
F; naca-rm-l57e24; July 29, 1957
- Martz, C William; Rocket-model
investigation of hinge-moments on a trailing-edge control on a 52.5 degree
swept wing between Mach numbers of 0.70 and 1.80; naca-rm-l57f04; August
12, 1957
- Ladson, Charles L; Two-dimensional
airfoil characteristics of four NACA 6A-series airfoils at transonic Mach
numbers up to 1.25; naca-rm-l57f05; August 06, 1957
- Strass, H Kurt
Stephens, Emily W; Aerodynamic
heating of a thin, unswept, untapered, multiweb, aluminum-alloy wing at Mach
numbers up to 2.67 as determined from a free-flight investigation of a
rocket-propelled model; naca-rm-l57f06; August 06, 1957
- Kehlet, Alan B; Free-flight
investigation of comparative zero-lift rolling effectiveness of a leading edge
and a trailing edge air-jet spoiler on an unswept wing; naca-rm-l57f10;
August 1957
- Rashis, Bernard; Exploratory
investigation of transpiration cooling of a 40 degree double wedge using
nitrogen and helium as coolants at stagnation temperatures of 1,295 to 2,910
F; naca-rm-l57f11; September 1957
- Modisette, Jerry L; Preliminary
investigation of lithium hydride as a high-temperature internal coolant;
naca-rm-l57f12a; October 03, 1957
- Love, Eugene S; The use of
cones as stabilizing and control surfaces at hypersonic speeds;
naca-rm-l57f14; August 12, 1957
- Polhamus, Edward C; Effect of nose
shape on subsonic aerodynamic characteristics of a body of revolution having a
fineness ratio of 10.94; naca-rm-l57f25; August 12, 1957
- Bland, William M , Jr
Rumsey, Charles B Lee, Dorothy B Kolenkiewicz, Ronald; Free-flight
aerodynamic-heating data to a Mach number of 15.5 on a blunted conical nose
with a total angle of 29 degrees; naca-rm-l57f28; August 1957
- Jones, George W , Jr;
Transonic
flutter investigation of a 64 degree delta wing constructed with spars along
constant-percent chord lines and streamwise ribs; naca-rm-l57g01; August
12, 1957
- Dickens, Waldo L
Hastings, Earl C , Jr; Comparison
of low-lift drag at Mach numbers from 0.74 to 1.37 of rocket-boosted models
having externally braced wings and cantilever wings; naca-rm-l57g10;
September 25, 1957
- Moore, John A; Experimental
determination of damping in pitch of swept and delta wings at supersonic Mach
numbers; naca-rm-l57g10a; September 19, 1957
- Gillespie, Warren, Jr;
Effects of
wing warp on the lift, drag, and static longitudinal stability characteristics
of an aircraft configuration having an arrow wing of aspect ratio 1.86 at Mach
numbers from 1.1 to 1.7; naca-rm-l57g12; August 30, 1957
- Thibodaux, Joseph G ,
Jr Swain, Robert L Wright, George; Analytical
and experimental studies of spherical solid-propellant rocket motors;
naca-rm-l57g12a; August 16, 1957
- Blanchard, Willard S;
Effect of
conical and flat sting-mounted windshields on the zero-lift drag of a
flare-stabilized bluff body at Mach numbers from 0.6 to 1.15;
naca-rm-l57g18; September 12, 1957
- Mugler, John P JR; Pressure
measurements at transonic and low supersonic speeds on a thin conical cambered
low-aspect-ratio delta wing in combination with basic and indented bodies;
naca-rm-l57g19; September 25, 1957
- Hoffman, Sherwood; Free-flight
investigation of the drag of a model of a 60 degree delta-wing bomber with
strut-mounted siamese nacelles and indented fuselage at Mach numbers from 0.80
to 1.35; naca-rm-l57g29; September 25, 1957
- Rashis, Bernard Bond,
Aleck C; Free-flight
skin-temperature and surface-pressure measurements on a highly polished nose
having a 100 degree total-angle cone and a 10 degree half-angle conical flare
section up to a Mach number of 4.08; naca-rm-l57g30; August 23,
1957
- Runckel, Jack F
Swihart, John M; A
hydrogen peroxide turbojet-engine simulator for wing-tunnel powered-model
investigations; naca-rm-l57h15; November 04, 1957
- Miltonberger, Georgene
H Davidson, John R Griffith, George E; Tests
of aerodynamically heated multiweb wing structures in a free jet at Mach
number 2 : two aluminum-alloy models of 20-inch chord with 0.064-inch-thick
skin at angles of attack of 0 degree and plus or minus 2 degrees;
naca-rm-l57h19; October 28, 1957
- Lord, Douglas R; Tabulated
pressure data for a series of controls on a 40 degree sweptback wing at Mach
numbers of 1.61 and 2.01; naca-rm-l57h30; November 08, 1957
- Rashis, Bernard; Preliminary
indications of the cooling achieved by ejecting water upstream from the
stagnation point of hemispherical, 80 degree conical, and flat-faced nose
shapes at a stagnation temperature of 4,000 F; naca-rm-l57i03; October 23,
1957
- Runckel, Jack F Hieser,
Gerald; Normal-force
and hinge-moment characteristics at transonic speeds of flap-type ailerons at
three spanwise locations on a 4-percent-thick sweptback-wing-body model and
pressure distribution measurements on an inboard aileron; naca-rm-l57i23;
December 05, 1957
- West, F E , Jr
Whitcomb, Charles F Schmeer, James W; Aerodynamic
load distribution over a 45 degree swept wing having a spoiler-slot-deflector
aileron and other spoiler ailerons for Mach numbers from 0.60 to 1.03;
naca-rm-l57j11; December 05, 1957
- ; The
principles of turbulent heat transfer; naca-tm-1408; 1957
- ; Reflection
and refraction of acoustic waves by a shock wave; naca-tm-1409;
1957
- ; Study
of the micro-nonuniformity of the plastic deformation of steel;
naca-tm-1411; 1957
- ; Aerodynamic
forces on a vibrating unstaggered cascade; naca-tm-1412; 1957
- ; On
the spectrum of natural oscillations of two-dimensional laminar flows;
naca-tm-1417; 1957
- Lagerstrom, P.A.,
Licher, R.M., Beane, B.J.; A
theoretical investigation of the drag of generalized aircraft configurations
in supersonic flow; naca-tm-1421; 1957
- ; Turbulence
in the wake of a thin airfoil at low speeds; naca-tm-1427; 1957
- Eaton, Ian D.; Effect
of fatigue crack on static strength; naca-tm-1428; 1957
- ; Wall
interference in a perforated wind tunnel; naca-tm-1429; 1957
- Eggers, Alfred J., Jr.,
Allen, Julian H., Neice, Stanford E.; A
comparative analysis of the performance of long-range hypervelocity
vehicles; naca-tn-4046; 1957
- Hastings, Earl C. Jr.,
Dickens, Waldo L.; Effects
of inlet modification and rocket-rack extension on the longitudinal trim and
low-lift drag of the Douglas F5D-1 airplane as abtained with a 0.125-scale
rocket-boosted model between mach numbers of 0.81 and 1.64;
naca-rm-sl57d30; 1957
- Phillips, William H.,
Kuehnel, Helmut A., Whitten, James B.; Flight
investigation of the effectiveness of an automatic aileron trim control device
for personal airplanes; naca-report-1304; 1957
- Lowry, John G.,
Polhamus, Edward C.; A
method for predicting lift increments due to flap deflection at low angles of
attack in incompressible flow; naca-tn-3911; 1957
- Berkey, William E.,
Rebeske, John J., Jr., Forrette, Robert E.; Performance
evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine
:over-all performance with standard rotor blading at inlet conditions of 35
inches of mercury absolute and 700 R; naca-rm-e52g31; 1957
- Sutton, Fred B.,
Lautenberger, J. Walter, Jr.; The
effect of body contouring on the longitudinal characteristics at Mach numbers
up to 0.92 of a wing-fuselage-tail and several wing-fuselage combinations
having sweptback wings of relatively high aspect ratio; naca-rm-a56j08;
1957
- Schmidt, Stanley F.,
Bergrun, Norman R., Merrick, Robert B., Matthews, Howard F.; A
simplified method for assessing the effect of steady rolling on angle of
attack and sideslip; naca-rm-a56k07; 1957
- Triplett, William C.,
McLean, John D., White, John S.; The
influence of imperfect radar space stabilization on the final attack phase of
an automatic interceptor system; naca-rm-a56k19; 1957
- Kaufman, Warner B.,
Gibbs, James B., Branstetter, J. Robert; Preliminary
investigation of combustion of diborane in a turbojet combustor;
naca-rm-e52l15; 1957
- Quigley, Hervey C.,
Hom, Francis W. K., Innis, Robert C.; A
flight investigation of area-suction and blowing boundary-layer control on the
trailing-edge flaps of a 35 degree swept-wing-carrier-type airplane;
naca-rm-a57b14; 1957
- Triplett, William C.,
Hom, Francis W. K.; Flight
tests of an automatic interceptor system with a tracking radar modified to
minimize the interaction between antenna and interceptor motions;
naca-rm-a57d09; 1957
- Hickey, David H.; Preliminary
investigation of the characteristics of a two dimensional wing and propeller
with the propeller plane of rotation in the wing-chord plane;
naca-rm-a57f03; 1957
- Knechtel, Earl D., Lee,
George.; Effects of
wing-tip droop on the longitudinal characteristics of two highly swept
wing-body combinations at Mach numbers from 0.6 to 1.4; naca-rm-a57f06b;
1957
- Stivers, Louis S., Jr.,
Lippmann, Garth W.; Effects
of vertical location of wing and horizontal tail on the aerodynamic
characteristics in pitch at Mach numbers from 0.60 to 1.40 of an airplane
configuration with an unswept wing; naca-rm-a57i10; 1957
- Wong, Norman D.; An
investigation of the control effectiveness of tip ailerons and spoilers on a
low-aspect-ratio trapezoidal-wing airplane model at Mach numbers from 1.55 to
2.35; naca-rm-a57i26a; 1957
- Garland, Benjamine J.,
Chauvin, Leo T.; Measurements
of Heat Transfer and Boundary-Layer Transition on an 8-inch-Diameter
Hemisphere-Cylinder in Free Flight for a Mach Number Range of 2.00 to
3.88.; naca-rm-l57d04a; April 1957
- Donald D. Arabian
(Langley Aeronautical Laboratory, Langley Field, Va.); Investigation
at Transonic Speeds of Loading Over a 30o Sweptback Wing of Aspect Ratio 3,
Taper Ratio 0.2, and NACA 65A004 Airfoil Mounted on a Body;
naca-rm-l57g09a; 1957
- J. Lyell Sanders, Jr.,
Harvey G. Mccomb, Jr., Floyd R. Schlechte; A
variational theorem for creep with applications to plates and columns;
naca-report-1342; 1958
- Elbridge Z. Stowell; A
phenomenological relation between stress, strain rate, and temperature for
metals at elevated temperatures; naca-report-1343; 1958
- Leonard Sternfield; A simplified
method for approximating the transient motion in angles of attack and sideslip
during a constant rolling maneuver; naca-report-1344; 1958
- Franklin W. Diederich;
The response
of an airplane to random atmospheric disturbances; naca-report-1345;
1958
- John C Houbolt, George
W Brooks; Differential
equations of motion for combined flapwise bending, chordwise bending, and
torsion of twisted nonuniform rotor blades; naca-report-1346; 1958
- Lloyd J Fisher, Edward
L Hoffman; Ditching
investigations of dynamic models and effects of design parameters on ditching
characteristics; naca-report-1347; 1958
- B Porter Brown; Ground
simulator studies of the effects of valve friction, stick friction,
flexibility, and backwash on power control system quality;
naca-report-1348; 1958
- Albert E. Von Doenhoff,
Elmer A Horton; A
low-speed experimental investigation of the effect of a sandpaper type of
roughness on boundary-layer transition; naca-report-1349; 1958
- F. B. Gustafson, Robert
J. Tapscott; Methods for
obtaining desired helicopter stability characteristics and procedures for
stability predictions; naca-report-1350; 1958
- Robert P. Coleman,
Arnold M. Feingold; Theory
of self-excited mechanical oscillations of helicopter rotors with hinged
blades; naca-report-1351; 1958
- Edmund R. Jonash,
Jerrold D. Wear, William P. Cook; Effect
of fuel variables on carbon formation in turbojet-engine combustors;
naca-report-1352; 1958
- Maurice S. Cahn; An experimental
investigation of sting-support effects on drag and a comparison with jet
effects at transonic speeds; naca-report-1353; 1958
- Jack B. Esgar, Eugene
F. Schum, Arthur N. Curren; Effect
of chord size on weight and cooling characteristics of air-cooled turbine
blades; naca-report-1354; 1958
- Charles L. Shuford,
Jr.; A
theoretical and experimental study of planing surfaces including effects of
cross section and plan form; naca-report-1355; 1958
- Dean R. Chapman, Donald
M. Kuehn, Howard K. Larson; Investigation
of separated flows in supersonic and subsonic streams with emphasis on the
effect of transition; naca-report-1356; 1958
- Lewis R Fisher; Experimental
determination of effects of frequency and amplitude on the lateral stability
derivatives for a delta, a swept, and unswept wing oscillating in yaw;
naca-report-1357; 1958
- Vernon J. Rossow; On flow of
electrically conducting fluids over a flat plate in the presence of a
transverse magnetic field; naca-report-1358; 1958
- John R. Spreiter,
Alberta Y. Alksne; Thin
airfoil theory based on approximate solution of the transonic flow
equation; naca-report-1359; 1958
- Perry L. Blackshear,
Jr.; Growth
of disturbances in a flame-generated shear region; naca-report-1360;
1958
- Richard R. Heldenfels,
Louis F. Vosteen; Approximate
analysis of effects of large deflections and initial twist on torsional
stiffness of a cantilever plate subjected to thermal stresses;
naca-report-1361; 1958
- Leonard K. Tower,
Roland Breitwieser, Benson E. Gammon; Theoretical
combustion performance of several high-energy fuels for ramjet engines;
naca-report-1362; 1958
- I. Irvin Pinkel,
Solomon Weiss, G. Merritt Preston, Gerard J. Pesman; Origin
and prevention of crash fires in turbojet aircraft; naca-report-1363;
1958
- William Gracey; Measurement of
static pressure on aircraft; naca-report-1364; 1958
- C. C. Shufflebarger,
Chester B. Payne, George L. Cohen; A
correlation of results of flight investigation with results of an analytical
study of effects of wing flexibility on wing strains due to gusts;
naca-report-1365; 1958
- Charles E. May; The mechanism
of thermal-gradient mass transfer in the sodium hydroxide-nickel system;
naca-report-1366; 1958
- Leslie W. Lassiter,
Robert W. Hess; Calculated
and measured stresses in simple panels subject to intense random acoustic
loading including the near noise field of a turbojet engine;
naca-report-1367; 1958
- James C. Emery, L.
Joseph Herrig, John R. Erwin, A. Richard Felix; Systematic
two-dimensional cascade tests of NACA 65-series compressor blades at low
speeds; naca-report-1368; 1958
- Mark W. Kelly, Seth B.
Anderson, Robert C. Innis; Blowing-type
boundary-layer control as applied to the trailing-edge flaps of a 35 degree
swept-wing airplane; naca-report-1369; 1958
- Woodrow L. Cook, Seth
B. Anderson, George E. Cooper; Area-suction
boundary-layer control as applied to the trailing-edge flaps of a 35 degree
swept-wing airplane; naca-report-1370; 1958
- Leland H. Jorgensen,
Edward W. Perkins; Investigation
of some wake vortex characteristics of an inclined ogive-cylinder body at Mach
number 2; naca-report-1371; 1958
- P. R. Hill; A
method of computing the transient temperature of thick walls from arbitrary
variation of adiabatic-wall temperature and heat-transfer coefficient;
naca-report-1372; 1958
- Charles C. Graves, Jack
S. Grobman; Theoretical
analysis of total-pressure loss and airflow distribution for tubular turbojet
combustors with constant annulus and liner cross-sectional areas;
naca-report-1373; 1958
- Milton D. Van Dyke; The similarity
rules for second-order subsonic and supersonic flow; naca-report-1374;
1958
- Albert J. Evans, George
Liner; A
wind-tunnel investigation of the aerodynamic characteristics of a full-scale
supersonic-type three-blade propeller at Mach numbers to 0.96;
naca-report-1375; 1958
- Leland H. Jorgensen; Elliptic cones
alone and with wings at supersonic speed; naca-report-1376; 1958
- Max C. Kurbjun, Arthur
W. Vogeley; Measurements of
free-space oscillating pressures near propellers at flight Mach numbers to
0.72; naca-report-1377; 1958
- A. J. Eggers, Jr.; A method for
simulating the atmospheric entry of long-range ballistic missiles;
naca-report-1378; 1958
- Eli Reshotko, Iavn E.
Beckwith; Compressible
laminar boundary layer over a yawed infinite cylinder with heat transfer and
arbitrary Prandtl number; naca-report-1379; 1958
- William B. Boatright;
An analysis
of pressure studies and experimental and theoretical downwash and sidewash
behind five pointed-tip wings at supersonic speeds; naca-report-1380;
1958
- H. Julian Allen, A. J.
Eggers, Jr.; A study of the
motion and aerodynamic heating of ballistic missiles entering the earth's
atmosphere at high supersonic speeds; naca-report-1381; 1958
- Alfred J. Eggers, Jr.,
H. Julian Allen, Stanford E. Neice; A
comparative analysis of the performance of long-range hypervelocity
vehicles; naca-report-1382; 1958
- Isadore L. Drell, Frank
E. Belles; Survey of
hydrogen combustion properties; naca-report-1383; 1958
- Lewis Laboratory Staff;
A summary of
preliminary investigations into the characteristics of combustion screech in
ducted burners; naca-report-1384; 1958
- Max A. Heaslet,
Franklyn B. Fuller; Drag
minimization for wings and bodies in supersonic flow; naca-report-1385;
1958
- Edward W. Perkins,
Leland H. Jorgensen, Simon C. Sommer; Investigation
of the drag of various axially symmetric nose shapes of fineness ratio 3 for
Mach numbers from 1.24 to 7.4; naca-report-1386; 1958
- Willard D. Coles,
Edmund E. Callaghan; Full-scale
investigation of several jet-engine noise-reduction nozzles;
naca-report-1387; 1958
- M. L. Pinns, W. T.
Olson, H. C. Barnett, R. Breitwieser; NACA
research on slurry fuels; naca-report-1388; 1958
- Ray H. Wright, Virgil
S. Wright, Virgil S. Ritchie, Albin O. Pearson; Characteristics
of the Langley 8-foot transonic tunnel with slotted test section;
naca-report-1389; 1958
- C. H. Wilts; Incompressible
flutter characteristics of representative aircraft wings;
naca-report-1390; 1958
- I. Flugge-Lotz, C. F.
Taylor, H. E. Lindberg; Investigation
of a nonlinear control system; naca-report-1391; 1958
- R. F. Decker, John P.
Rowe, J. W. Freeman; Boron
and zirconium from crucible refractories in a complex heat-resistant
alloy; naca-report-1392; 1993
- Ralph T. Dittrich; Discharge
coefficients for combustor-liner air-entry holes II : flush rectangular holes,
step louvers, and scoops; naca-tn-3924; Apr 1958
- Howard F. Calvert,
Gordon T. Smith; Vibration
survey of four representative types of air-cooled turbine blades;
naca-tn-4100; Jul 1958
- Mitchel H. Bertram; Boundary-layer
displacement effects in air at Mach numbers 6.8 and 9.6; naca-tn-4133; Feb
1958
- Kriebel, Anthony R
(Massachusetts Institute of Technology) Seidel, Barry S (Massachusetts
Institute of Technology) Schwind, Richard G; Stall
propagation in a cascade of airfoils; naca-tn-4134; Jul 1958
- E. G. Bodine, R. L.
Carlson, G. K. Manning; Creep
deformation patterns of joints under bearing and tensile loads;
naca-tn-4138; Dec 1957
- Willmarth, William W
(California Institute of Technology); Wall
pressure fluctuations in a turbulent boundary layer; naca-tn-4139; Mar
1958
- Ashkenas, Harry
(Cornell University); Turbulent
shearing stress in the boundary layer of yawed flat plates; naca-tn-4140;
Apr 1958
- Jackson R. Stalder; The useful heat
capacity of several materials for ballistic nose-cone construction;
naca-tn-4141; Nov 1957
- Creager, Marcus O; Effects of
leading-edge blunting on the local heat transfer and pressure distributions
over flat plates in supersonic flow; naca-tn-4142; Dec 1957
- A. C. Charters, B. Pat
Denardo, Vernon J. Rossow; Development
of a piston-compressor type light-gas gun for the launching of free-flight
models at high velocity; naca-tn-4143; Nov 1957
- Steve P. Heims; Effect of
oxygen recombination on one-dimensional flow at high Mach numbers;
naca-tn-4144; Jan 1958
- Marvin Shinbrot, Grace
C. Carpenter; An
analysis of the optimization of a beam rider missile system; naca-tn-4145;
Mar 1958
- J. Richard Spahr; Contribution of
the wing panels to the forces and moments of supersonic wing-body combinations
at combined angles; naca-tn-4146; Jan 1958
- Henry A. Cole, Jr.,
Euclid C. Holleman; Measured
and predicted dynamic response characteristics of a flexible airplane to
elevator control over a frequency range including three structural modes;
naca-tn-4147; Feb 1958
- John R. Spreiter,
Alberta Y. Alksne, B. Jeanne Hyett; Theoretical
pressure distribution for several related nonlifting airfoils at high subsonic
speeds; naca-tn-4148; Jan 1958
- Morris W. Rubesin,
Constantine C. Pappas; An
analysis of the turbulent boundary-layer characteristics on a flat plate with
distributed light-gas injection; naca-tn-4149; Feb 1958
- C. Frederick Hansen; Approximations
for the thermodynamic and transport properties of high-temperature air;
naca-tn-4150; Mar 1958
- Vernon H. Gray; Correlations
among ice measurements, impingement rates icing conditions, and drag
coefficients for unswept NACA 65A004 airfoil; naca-tn-4151; Feb
1958
- Eli Reshotko; Laminar
boundary layer with heat transfer on a cone at angle of attack in a supersonic
stream; naca-tn-4152; Dec 1957
- Andrew Beke; Effect
of wall cooling on inlet parameters of a scoop operating in a turbulent
boundary layer on a flat or conical surface for Mach numbers 2 to 10;
naca-tn-4153; Mar 1958
- Eli Reshotko, Maurice
Tucker; Approximate
calculation of the compressible turbulent boundary layer with heat transfer
and arbitrary pressure gradient; naca-tn-4154; Dec 1957
- Vernon H. Gray, Uwe H.
Von Glahn; Aerodynamic
effects caused by icing of an unswept NACA 65A004 airfoil; naca-tn-4155;
Feb 1958
- Sheldon Heimel; Effect of
initial mixture-temperature on burning velocity of hydrogen-air mixtures with
preheating and simulated preburning; naca-tn-4156; Oct 1957
- H. B. Probst, C. E.
May, Howard T. Mchenry; Corrosion
resistance of nickel alloys in molten sodium hydroxide; naca-tn-4157; Jan
1958
- G. Merritt Preston,
Gerard J. Pesman; Accelerations
in transport-airplane crashes; naca-tn-4158; Feb 1958
- Donald B. Kirsch, Leon
M. Wenzel, Clint E. Hart; Experimental
investigation of turbojet-engine multiple-loop controls for non-afterburning
and afterburning modes of engine operation; naca-tn-4159; Jan 1958
- Francis J. Clauss,
James W. Freeman; Thermal
fatigue of ductile materials I: effect of variations in the temperature cycle
on the thermal-fatigue of S-816 and Inconel 550; naca-tn-4160; Sep
1958
- Thomas L. Carter; Effect of
lubricant base stock on rolling-contact fatigue life; naca-tn-4161; Feb
1958
- Donald R. Boldman,
Perry L. Blackshear, Jr.; Study
of some burner cross-section changes that increase space-heating rates;
naca-tn-4162; Nov 1957
- Thomas L. Carter; Effect of
temperature on rolling-contact fatigue life with liquid and dry powder
lubricants; naca-tn-4163; Jan 1958
- Edward R. Gotsky, James
P. Cusick, Donald Bogart; Two-dimensional
diffusion theory analysis of reactivity effects of a fuel-plate-removal
experiment; naca-tn-4164; Jan 1958
- Francis J. Clauss,
James W. Freeman; Thermal
fatigue of ductile materials II : effect of cyclic thermal stressing on the
stress-rupture life and ductility of S-816 and Inconel 550.; naca-tn-4165;
Sep 1958
- John L. Sewall; An experimental
and theoretical study of the effect of fuel on pitching-translation
flutter; naca-tn-4166; Dec 1957
- Eugene S. Love, Ronald
H. Long; A
rapid method for predicting attached-shock shape; naca-tn-4167; Oct
1957
- Kenneth L. Wadlin,
Kenneth W. Christopher; A
method for calculation of hydrodynamic lift for submerged and planing
rectangular lifting surfaces; naca-tn-4168; Jan 1958
- H. B. Tolefson; Atmospheric
temperature observations to 100,000 feet for several climatological regions of
the Northern Hemisphere; naca-tn-4169; Nov 1957
- Roy F. Brissenden; Some ground
measurements of the forces applied by pilots to a side-located aircraft
controller; naca-tn-4171; Nov 1957
- Max C. Kurbjun; Noise survey
under static conditions of a turbine-driven full-scale modified supersonic
propeller with an advance ratio of 3.2; naca-tn-4172; Jan 1958
- Norman L. Crabill; An analytical
investigation of the gust-alleviating properties of a simple pitch damper;
naca-tn-4173; Dec 1957
- James W. Wiggins, Paul
G. Fournier; Wind-tunnel
investigation of the static lateral stability characteristics of wind-fuselage
combinations at high subsonic speeds : taper-ratio series; naca-tn-4174;
Oct 1957
- Delwin R. Croom,
Jarrett K. Huffman; Investigation
of deflectors as gust alleviators on a 0.09-scale model of the Bell X-5
airplane with various wing sweep angles from 20 degrees to 60 degrees at Mach
numbers from 0.40 to 0.90; naca-tn-4175; Nov 1957
- Joseph L. Johnson, Jr.;
Wind-tunnel
investigation of the static longitudinal stability and trim characteristics of
a sweptback-wing jet-transport model equipped with an external-flow jet
augmented flap; naca-tn-4177; Jan 1958
- James C. Emery; Low-speed
cascade investigation of compressor blades having loaded leading edges;
naca-tn-4178; Jan 1958
- James T. Matthews, Jr.;
Analytical
investigation of acceleration restriction in a fighter airplane with an
automatic control system; naca-tn-4179; Jan 1958
- James N. Mueller; Investigation
of spoilers at a Mach number of 1.93 to determine the effects of height and
chordwise location on the section aerodynamic characteristics of a
two-dimensional wing; naca-tn-4180; Feb 1958
- Kenneth P. Spreemann;
Investigation
of the effects of propeller diameter on the ability of a flapped wing, with
and without boundary-layer control, to deflect a propeller slipstream downward
for vertical take-off; naca-tn-4181; Dec 1957
- Roland D. English,
Abraham Spinak, Eldred H. Helton; Physical
characteristics and test conditions of an ethylene-heated high-temperature
jet; naca-tn-4182; Jan 1958
- John R. Sevier, Jr., K.
R. Czarnecki; Investigation
of effects of distributed surface roughness on a turbulent boundary layer over
a body of revolution at a mach number of 2.01; naca-tn-4183; Feb
1958
- William Gracey; Measurement of
static pressure on aircraft; naca-tn-4184; Nov 1957
- James W. Wiggins; Wind-tunnel
investigation of effect of sweep on rolling derivatives at angles of attack up
to 13 degrees and at high subsonic Mach numbers, including a semiempirical
method of estimating the rolling derivatives; naca-tn-4185; Jan
1958
- D. W. Dunn, W. H. Reid;
Heat
transfer in isotropic turbulence during the final period of decay;
naca-tn-4186; Jun 1958
- Daniel Savitsky, R. E.
Prowse, D. H. Lueders; High-speed
hydrodynamic characteristics of a flat plate and 20 degrees dead-rise surface
in unsymmetrical planing conditions; naca-tn-4187; Jun 1958
- Aldie E. Johnson; Charts relating
the compressive and shear buckling stresses of longitudinally supported plates
to the effective deflectional stiffness; naca-tn-4188; Feb 1958
- H. J. Cunningham; Lift and moment
on thin arrowhead wings with supersonic edges oscillating in symmetric
flapping and roll and application to the flutter of an all-movable control
surface; naca-tn-4189; Jan 1958
- William A. Newsom, Jr.;
Experimental
investigation of the lateral trim of a wing-propeller combination at angles of
attack up to 90 degrees with all propellers turning in the same direction;
naca-tn-4190; Jan 1958
- William S. Aiken, Jr.;
Analysis of
horizontal-tail loads in pitching maneuvers on a flexible swept-wing jet
bomber; naca-tn-4191; Dec 1957
- Seaberg, Ernest C; Three-degree-of
freedom evaluation of the longitudinal transfer functions of a supersonic
canard missile configuration including changes in forward speed;
naca-tn-4192; Dec 1957
- Robert W. Miller; Comparison of
hydrodynamic-impact acceleration and response for systems with single and with
multiple elastic modes; naca-tn-4194; Feb 1958
- Eugene S. Love, Louise
P. Lee; Shape of
initial portion of boundary of supersonic axisymmetric free jets at large jet
pressure ratios; naca-tn-4195; Jan 1958
- John M. Eggleston,
William H. Phillips; A
method for the calculation of the lateral response of airplanes to random
turbulence; naca-tn-4196; Feb 1958
- Dennis J. Martin; Summary of
flutter experiences as a guide to the preliminary design of lifting surfaces
on missiles; naca-tn-4197; Feb 1958
- Richard H. Rhyne; Effects of
airplane flexibility on wing strains in rough air at 35,000 feet as determined
by a flight investigation of a large swept-wing airplane; naca-tn-4198;
Jan 1958
- Helmut A. Kuehnel,
Arnold R. Beckhardt, Robert A. Champine; A
flight investigation of the effects of varied lateral damping on the
effectiveness of a fighter airplane as a gun platform; naca-tn-4199; Jan
1958
- Spreemann, Kenneth P;
Effectiveness
of boundary-layer control, obtained by blowing over a plain rear flap in
combination with a forward slotted flap, in deflecting a slipstream downward
for vertical take-off; naca-tn-4200; Feb 1958
- William E. Stoney, Jr.;
Collection
of zero-lift drag data on bodies of revolution from free-flight
investigations; naca-tn-4201; Jan 1958
- Stanley Faber; Qualitative
simulator study of longitudinal stick forces and displacements desirable
during tracking; naca-tn-4202; Feb 1958
- Leroy H. Ludi; Flight
investigation of effects of atmospheric turbulence and moderate maneuvers on
bending and torsional moments encountered by a helicopter rotor blade;
naca-tn-4203; Feb 1958
- Walter F. Lindsey, Emma
Jean Landrum; Compilation
of information on the transonic attachment of flows at the leading edges of
airfoils; naca-tn-4204; Feb 1958
- Richard A. Pride, John
B. Hall, Jr.; Transient
heating effects on the bending strength of integral aluminum-alloy box
beams; naca-tn-4205; Mar 1958
- William R. Wade; Measurements of
total hemispherical emissivity of various oxidized metals at high
temperature; naca-tn-4206; Mar 1958
- J. Lyell Sanders, Jr.;
Effect of a
stringer on the stress concentration due to a crack in a thin sheet;
naca-tn-4207; Mar 1958
- Willis H. Braun; Turbulent
boundary layer on a yawed cone in a supersonic stream; naca-tn-4208; Jan
1958
- Kenneth P. Coffin,
Cleveland O'Neal, Jr.; Experimental
thermal conductivities of the N2O4 is in equilibrium to 2NO2 system;
naca-tn-4209; Feb 1958
- A. E. Potter, Jr., E.
L. Wong, A. L. Berlad; Stability
of propane-air flames in vortex flow; naca-tn-4210; Feb 1958
- D. W. Wisander, W. F.
Hady, R. L. Johnson; Friction
studies of various materials in liquid nitrogen; naca-tn-4211; Feb
1958
- NACA Lewis Laboratory
Staff; Central
automatic data processing system; naca-tn-4212; Apr 1958
- Paul F. Brinich; Recovery
temperatures and heat transfer near two-dimensional roughness elements at Mach
3.1; naca-tn-4213; Feb 1958
- Paul F. Brinich; Boundary-layer
transition on an open-nose cone; naca-tn-4214; Feb 1958
- R. H. Kemp, C. R.
Morse, M. H. Hirschberg; Application
of a high-temperature static strain gage to the measurement of thermal
stresses in a turbine stator vane; naca-tn-4215; Mar 1958
- Vern G. Rollin; Effect of jet
temperature on jet-noise generation; naca-tn-4217; Mar 1958
- M. H. Hirschberg, A.
Mendelson; Analysis of
stresses and deflections in a disk subjected to gyroscopic forces;
naca-tn-4218; Mar 1958
- Marcus F. Heidmann,
Richard J. Priem; Propellant
vaporization as a criterion for rocket engine design : relation between
percentage of propellant vaporized and engine performance; naca-tn-4219;
Mar 1958
- M. Murdochow, A.
Muzyka; Analysis of
harmonic forces produced at hub by imbalances in helicopter rotor blades;
naca-tn-4226; Apr 1958
- Max A. Heaslet,
Franklyn B. Fuller; Drag
minimization for wings in supersonic flow, with various constraints;
naca-tn-4227; Feb 1958
- Paul W. Huber; Tables
and graphs of normal-shock parameters at hypersonic Mach numbers and selected
altitudes; naca-tn-4352; September 1958
- Arthur G. Hansen,
Howard Z. Herzig; Approximate
solutions of a class of similarity equations for three-dimensional, laminar,
incompressible boundary-layer flows; naca-tn-4375; Sep 1958
- W. F. Weiland, W. H.
Lowdermilk, R. G. Deissler; Analytical
and experimental investigation of temperature recovery factors for fully
developed flow of air in a tube; naca-tn-4376; Sep 1958
- Uwe H. Von Glahn; Use of the
Coanda effect for jet deflection and vertical lift with multiple-flat-plate
and curved-plate deflection surfaces; naca-tn-4377; Sep 1958
- Norman Sands, John R.
Jack; Preliminary
heat-transfer studies on two bodies of revolution at angle of attack at a Mach
number of 3.12; naca-tn-4378; Sep 1958
- Warner L. Stewart; Torque-speed
characteristics for high-specific-work turbines; naca-tn-4379; Sep
1958
- William E. Brunk; Approximate
method for calculation of laminar boundary layer with heat transfer on a cone
at large angle of attack in supersonic flow; naca-tn-4380; Sep 1958
- Andrew E. Potter, Jr.,
Edgar L. Wong; Effect
of pressure and duct geometry on bluff-body flame stabilization;
naca-tn-4381; Sep 1958
- Warren H. Lowdermilk,
Chester D. Lanzo, Byron L. Siegel; Investigation
of boiling burnout and flow stability for water flowing in tubes;
naca-tn-4382; Sep 1958
- Lloyd N. Krause, Robert
C. Johnson, George E. Glawe; A
cooled-gas pyrometer for use in high-temperature gas streams;
naca-tn-4383; Sep 1958
- Robert G. Deissler,
Maynard F. Taylor; Analysis
of turbulent flow and heat transfer in noncircular passages; naca-tn-4384;
Sep 1958
- Savin, Raymond C; Comparison of
shock-expansion theory with experiment for the lift, drag, and pitching-moment
characteristics of two wing-body combinations at M=5.0; naca-tn-4385; Sep
1958
- Richard J. Weber, John
S. Mackay; An analysis of
ramjet engines using supersonic combustion; naca-tn-4386; Sep 1958
- Emanuel Schnitzer; Experimental
evaluation of low-band-pass landing-gear shock absorber for pulse
loadings; naca-tn-4387; Sep 1958
- K. R. Czarnecki, Mary
W. Jackson; Effects of nose
angle and Mach number on transition on cones at supersonic speeds;
naca-tn-4388; Sep 1958
- Jerome B. Hammack,
Thomas C. O'Bryan; Effect
of advance ratio on flight performance of a modified supersonic propeller;
naca-tn-4389; Sep 1958
- William Letko, Herman
S. Fletcher; Effects of
frequency and amplitude on the yawing derivatives of triangular, swept, and
unswept wings and of a triangular-wing-fuselage combination with and without a
triangular tail performing sinusoidal yawing oscillations; naca-tn-4390;
SEP 1958
- Leonard Roberts; Mass transfer
cooling near the stagnation point; naca-tn-4391; SEP 1958
- Leonard Roberts; A theoretical
study of stagnation-point ablation; naca-tn-4392; SEP 1958
- Robert J. Tapscott; Some static
longitudinal stability characteristics of an overlapped-type tandem-rotor
helicopter at low airspeeds; naca-tn-4393; SEP 1958
- Arthur J. Mcevily, Jr.,
Walter Illg; The rate of
fatigue-crack propagation in two aluminum alloys; naca-tn-4394; SEP
1958
- Donald S. Woolston,
John L. Sewall; Use
of the Kernel function in a three-dimensional flutter analysis with
application to a flutter-tested delta-wing model; naca-tn-4395; SEP
1958
- Elbridge Z. Stowell; A
phenomenological theory for the transient creep of metals at elevated
temperatures; naca-tn-4396; SEP 1958
- Walter D. Wolhart,
David F. Thomas; Static
longitudinal and lateral stability characteristics at low speed of 60 degree
sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6;
naca-tn-4397; SEP 1958
- Harvey G. Mccomb, Jr.;
Analysis of
the creep behavior of a square plate loaded in edge compression;
naca-tn-4398; SEP 1958
- Richard Hord; Relative
motion in the terminal phase of interception of a satellite or a ballistic
missile; naca-tn-4399; SEP 1958
- James M. Mckay, Richard
H. Sawyer, Albert W. Hall; Measurements
of ground-reaction forces and vertical center-of-gravity accelerations of a
bomber airplane taxiing over obstacles; naca-tn-4400; SEP 1958
- Philip M. Edge, Jean P.
Mason; Hydrodynamic
impact loads on 30 degree and 60 degree V-step plan-form models with and
without dead rise; naca-tn-4401; SEP 1958
- Sherman A. Clevenson,
Sumner A. Leadbetter; Measurements
of aerodynamic forces and moments at subsonic speeds on a simplified T-tail
oscillating in yaw about the fin midchord; naca-tn-4402; SEP 1958
- James P. Peterson,
Richard G. Updegraff; Tests
of ring-stiffened circular cylinders subjected to a transverse shear load;
naca-tn-4403; SEP 1958
- William C. Hayes,
Richard E. Kuhn, Irving R. Sherman; Effects
of propeller position and overlap on the slipstream deflection characteristics
of a wing-propeller; naca-tn-4404; SEP 1958
- Walter L. Kouyoumjian,
Sherwood Hoffman; Free-flight
investigation to determine the drag of flat- and vee- windshield canopies on a
parabolic fuselage with and without transonic indentation between Mach numbers
of 0.75 and 1.35; naca-tn-4405; SEP 1958
- Eziaslav N. Harrin; Low tire
friction and cornering forces on a wet surface; naca-tn-4406; SEP
1958
- Kenneth P. Spreemann,
Irving R. Sherman; Effects
of ground proximity on the thrust of a simple downward-directed jet beneath a
flat surface; naca-tn-4407; SEP 1958
- Louis A. Girifalco,
Hubert H. Grimes; The
theory of diffusion in strained systems; naca-tn-4408; SEP 1958
- John E. Yeates; Flight
measurements of the vibration experienced by a tandem helicopter in
transition, vortex-ring state, landing, approach, and yawed flight;
naca-tn-4409; SEP 1958
- Thomas C. O'Bryan; Flight
measurements of the vibratory stresses on a propeller designed for an advance
ratio of 4.0 and a Mach number of 0.82; naca-tn-4410; SEP 1958
- Frank S. Malvestuto,
Jr, Julia M. Goodwin; Effect
of angle of attack and thickness on aerodynamic coefficients of a rigid wing
oscillating at very low frequencies in two-dimensional supersonic flow;
naca-tn-4069; Jan 1958
- Carl A. Moore, Jr,
Stephen J. Kline; Some
effects of vanes and of turbulence in two-dimensional wide-angle subsonic
diffusers; naca-tn-4080; Jun 1958
- P. P. Bijlaard; Method of split
rigidities and its application to various buckling problems; naca-tn-4085;
Jul 1958
- Charles Saltzer; Discrete
potential theory for two-dimensional Laplace and Poisson difference
equations; naca-tn-4086; Jan 1958
- W. E. Moeckel, Kenneth
C. Weston; Composition and
thermodynamic properties of air in chemical equilibrium; naca-tn-4265; Apr
1958
- Walter B. Horne, Robert
F. Smiley; Low-speed
yawed-rolling characteristics and other elastic properties of a pair of
40-inch-diameter, 14-ply-rating, type VII aircraft tires; naca-tn-4109;
Jan 1958
- Robert F. Smiley,
Walter B. Horne; Mechanical
properties of pneumatic tires with special reference to modern aircraft
tires; naca-tn-4110; Jan 1958
- William T. House,
Milton Orchin; Low-temperature,
vapor-phase oxidation of fuel-rich hydrocarbon mixtures; naca-tn-4118; Jan
1958
- Kenneth Margolis, Frank
S. Malvestuto, Jr, Peter J. Maxie, Jr; Theoretical
calculations of subsonic wave drag at zero lift for a particular store
arrangement; naca-tn-4120; Jan 1958
- Robert T. Taylor; Experimental
investigation of the effects of some shroud design variables on the static
thrust characteristics of a small-scale shrouded propeller submerged in a
wing; naca-tn-4126; Jan 1958
- Stanley Corrsin; Local isotropy
in turbulent shear flow; naca-rm-58b11; May 1958
- Stephen C. Traugott; Influence of
solid-body rotation on screen-produced turbulence; naca-tn-4135; Aug
1958
- Frank Lane, Manfred
Friedman; Theoretical
investigation of subsonic oscillatory blade-row aerodynamics;
naca-tn-4136; Feb 1958
- W. S. Hyler, H. G.
Popp, S. A. Gordon, H. J. Grover, D. N. Gideon; Fatigue
behavior of aircraft structural beams; naca-tn-4137; Jan 1958
- Edward C. Polhamus; Effect of flow
incidence and Reynolds number on low-speed aerodynamic characteristics of
several noncircular cylinders with applications to directional stability and
spinning; naca-tn-4176; Jan 1958
- Harold L. Crane, George
J. Hurt, Jr., John M. Elliott; Subsonic
flight investigation of methods to improve the damping of lateral oscillations
by means of a viscous damper in the rudder system in conjunction with adjusted
hinge-moment parameters; naca-tn-4193; Jan 1958
- Thomas L. Carter; Effect of fiber
orientation in races and balls under rolling-contact fatigue conditions;
naca-tn-4216; Feb 1958
- William Lewis, Porter
J. Perkins, Jr.; A
flight evaluation and analysis of the effect of icing conditions on the ZPG-2
airship; naca-tn-4220; Apr 1958
- Albert L. Loeffler,
Jr., Morris Perlmutter; Turbulent
flow through porous resistances slightly inclined to the flow direction;
naca-tn-4221; Feb 1958
- Robert D. Ingebo; Drop-size
distributions for impinging-jet breakup in airstreams simulating the velocity
conditions in rocket combustors; naca-tn-4222; mar 1958
- F. W. Ocvirk, G. B.
DuBois; Relation of
journal bearing performance to minimum oil-film thickness; naca-tn-4223;
Apr 1958
- B. S. Berry, A. S.
Nowick; Internal-friction
study of aluminum alloy containing 4 weight percent copper; naca-tn-4225;
Aug 1958
- Herbert Becker; General
instability of stiffened cylinders; naca-tn-4237; Jul 1958
- Walter Castles, Jr.,
Howard L. Durham, Jr., Jirair Kevorkian; Normal
component of induced velocity for entire field of a uniformly loaded lifting
rotor with highly swept wake as determined by electromagnetic analog;
naca-tn-4238; Jun 1958
- John W. McKee, Rodger
L. Naeseth; Experimental
investigation of the drag of flat plates and cylinders in the slipstream of a
hovering rotor; naca-tn-4239; Apr 1958
- Edward Widmayer, Jr.,
Sherman A. Clevenson, Sumner A. Leadbetter; Some
measurements of aerodynamic forces and moments at subsonic speeds on a
rectangular wing of aspect ratio 2 oscillating about the midchord;
naca-tn-4240; May 1958
- Floyd E. Valentine; An approximate
method for design or analysis of two-dimensional subsonic-flow passages;
naca-tn-4241; Apr 1958
- E. B. Klunker, Keith C.
Harder; General
solutions for flow past slender cambered wings with swept trailing edges and
calculation of additional loading due to control surfaces; naca-tn-4242;
May 1958
- Paul B. Gooderum; An experimental
study of the turbulent boundary layer on a shock-tube wall; naca-tn-4243;
Jun 1958
- Robert W. Leonard; On solutions
for the transient response of beams; naca-tn-4244; Jun 1958
- Robert W. Fralich, John
M. Hedgepeth; Flutter
analysis of rectangular wings of very low aspect ratio; naca-tn-4245; Jun
1958
- Herbert F. Hardrath,
Herbert A. Leybold; Further
investigation of fatigue-crack propagation in aluminum-alloy box beams;
naca-tn-4246; Jun 1958
- Albert W. Hall, Richard
H. Sawyer, James M. McKay; Study
of ground-reaction forces measured during landing impacts of a large
airplane; naca-tn-4247; May 1958
- S. Katzoff, Raymond L.
Barger; Boundary-induced
downwash due to lift in a two-dimensional slotted wind tunnel;
naca-tn-4289; Jun 1958
- Richard T. Whitcomb; A fuselage
addition to increase drag-rise Mach number of subsonic airplanes at lifting
conditions; naca-tn-4290; Jun 1958
- Thomas L. Coleman,
Harry Press, May T. Meadows; An
evaluation of the effects of flexibility on wing strains in rough air for a
large swept-wing airplane by means of experimentally determined
frequency-response functions with an assessment of random-process techniques
employed; naca-tn-4291; Jul 1958
- Melvin S. Anderson; Local
instability of the elements of a truss-core sandwich plate; naca-tn-4292;
Jul 1958
- Richard T. Whitcomb; Special bodies
added on a wing to reduce shock-induced boundary-layer separation at high
subsonic speeds; naca-tn-4293; Jun 1958
- John R. McGehee; Effects of nose
shape and spray control strips on emergence and planing spray of hydro-ski
models; naca-tn-4294; Jul 1958
- Raymond L. Barger; Reflection and
transmission of sound by a slotted wall separating two moving fluid
streams; naca-tn-4295; Jun 1958
- Bland A. Stein; Compressive
strength and creep of 17-7 PH stainless-steel plates at elevated
temperatures; naca-tn-4296; Jul 1958
- Helmut A. Kuehnel,
Robert W. Sommer; Flight
investigation of the acceptability of a small side-located controller used
with an irreversible hydraulic control system; naca-tn-4297; Jul
1958
- John M. Riebe, Edwin E.
Davenport; Exploratory
wind-tunnel investigation to determine the lift effects of blowing over flaps
from nacelles mounted above the wing; naca-tn-4298; Jun 1958
- K. R. Czarnecki, John
R. Sevier, Jr., Melvin M. Carmel; Effects
of fabrication-type roughness on turbulent skin friction at supersonic
speeds; naca-tn-4299; Jul 1958
- William E. Stoney, Jr.,
J. Thomas Markley; Heat-transfer
and pressure measurements on flat-faced cylinders at a Mach number of 2;
naca-tn-4300; Jul 1958
- Mitchel H. Bertram,
Arthur Henderson, Jr.; Effects
of boundary-layer displacement and leading-edge bluntness on pressure
distribution, skin friction, and heat transfer of bodies at hypersonic
speeds; naca-tn-4301; Jul 1958
- Donald S. Woolston,
Sherman A. Clevenson, Sumner A. Leadbetter; Analytical
and experimental investigation of aerodynamic forces and moments on
low-aspect-ratio wings undergoing flapping oscillations; naca-tn-4302; Aug
1958
- Wilbur E. Thompson; Measurements
and power spectra of runway roughness at airports in countries of the North
Atlantic Treaty Organization; naca-tn-4303; Jul 1958
- Alton P. Mayo; Matrix
method for obtaining spanwise moments and deflections of torsionally rigid
rotor blades with arbitrary loadings; naca-tn-4304; Aug 1958
- James L. Williams; Wind-tunnel
investigation of effects of spoiler location, spoiler size, and fuselage nose
shape on directional characteristics of a model of a tandem-rotor helicopter
fuselage; naca-tn-4305; Jul 1958
- William A. Brooks, Jr.;
Temperature
and thermal-stress distributions in some structural elements heated at a
constant rate; naca-tn-4306; Aug 1958
- Jerome N. Engel; Experimental
measurements of the effects of airplane motions on wing and tail angles of
attack of a swept-wing bomber in rough air; naca-tn-4307; Aug 1958
- Robert L. Trimpi,
Robert A. Jones; Transient
temperature distribution in a two-component semi-infinite composite slab
of; naca-tn-4308; Sep 1958
- D. L. Cochran, S. J.
Kline; Use
of short flat vanes for producing efficient wide-angle two-dimensional
subsonic diffusers; naca-tn-4309; Sep 1958
- E. M. Sparrow, J. L.
Gregg; Prandtl number
effects on unsteady forced-convection heat transfer; naca-tn-4311; Jun
1958
- Jack G. McArdle; Internal
characteristics and performance of an aerodynamically controlled,
variable-discharge convergent nozzle; naca-tn-4312; Jul 1958
- John R. Jack; Effect
of favorable pressure gradients on transition for several bodies of revolution
at Mach 3.12; naca-tn-4313; Jul 1958
- Porter J. Perkins; Icing
frequencies experienced during climb and descent by fighter-interceptor
aircraft; naca-tn-4314; Jul 1958
- Edmund E. Callaghan; An estimate of
the fluctuating surface pressures encountered in the reentry of a ballistic
missile; naca-tn-4315; Jul 1958
- Gordon P. Allen, Donald
H. Buckley, Robert L. Johnson; Friction
and wear with reactive gases at temperatures up to 1200 F; naca-tn-4316;
Sep 1958
- Willard D. Coles, John
A. Mihaloew, Edmund E. Callaghan; Turbojet
engine noise reduction with mixing nozzle-ejector combinations;
naca-tn-4317; Aug 1958
- Seymour Lieblein; Analytical
relation for wake momentum thickness and diffusion ratio for low-speed
compressor; naca-tn-4318; Aug 1958
- Stephen H. Maslen; On fully
developed channel flows: some solutions and limitations, and effects of
compressibility, variable properties, and body forces; naca-tn-4319; Sep
1958
- Simon Ostrach, Philip
R. Thornton; Compressible
laminar flow and heat transfer about a rotating isothermal disk;
naca-tn-4320; Aug 1958
- Walter Castles, Jr.; Flow induced by
a rotor in power-on vertical descent; naca-tn-4330; Jul 1958
- Herbert A. Leybold,
Herbert F. Hardrath, Robert L. Moore; An
investigation of the effects of atmospheric corrosion on the fatigue life of
aluminum alloys; naca-tn-4331; Sep 1958
- Harry Press, Roy
Steiner; An
approach to the problem of estimating severe and repeated gust loads for
missile operations; naca-tn-4332; Sep 1958
- Howard S. Carter; Effect of some
external crosswise stiffeners on the heat transfer and pressure distribution
on a flat plate at Mach numbers of 0.77, 1.39, and 1.98; naca-tn-4333; Sep
1958
- William T. Davis; Lag in pressure
systems at extremely low pressures; naca-tn-4334; Sep 1958
- Homer G. Morgan, Vera
Huckel, Harry L. Runyan; Procedure
for calculating flutter at high supersonic speed including camber deflections,
and comparison with experimental results; naca-tn-4335; Sep 1958
- David J. Carter, Jr.,
Allen R. Vick; Experimental
investigation of axial and normal force characteristics of skewed nozzles;
naca-tn-4336; Sep 1958
- Harvey H. Hubbard,
Domenic J. Maglieri; An
investigation of some phenomena relating to aural detection of airplanes;
naca-tn-4337; Sep 1958
- G. L. Borman, M. M. El
Wakil, O. A. Uyehara, P. S. Myers; Graphs
of reduced variables for computing histories of vaporizing fuel drops, and
drop histories under pressure; naca-tn-4338; Sep 1958
- Philip M. Edge, Jr.; Hydrodynamic
impact loads of a -20 degree dead-rise inverted-V model and comparisons with
loads of a flat-bottom model; naca-tn-4339; Aug 1958
- Paul G. Fournier; Wind-tunnel
investigation of the high-subsonic static longitudinal stability
characteristics of several wing-body configurations designed for high
lift-drag ratios at a Mach number of 1.4; naca-tn-4340; Jul 1958
- Herman S. Fletcher; Low-speed
experimental determination of the effects of leading-edge radius and profile
thickness on static and oscillatory lateral stability derivatives for a delta
wing with 60 degrees of leading-edge sweep; naca-tn-4341; Jul 1958
- Thomas C. O'Bryan; Flight
measurements of the vibratory bending and torsional stresses on a modified
supersonic propeller for forward Mach numbers up to 0.95; naca-tn-4342;
Jun 1958
- James J. Buglia, Helen
Brinkworth; A comparison of
two methods for calculating transient temperatures for thick walls;
naca-tn-4343; Aug 1958
- James C. Emery, Paul W.
Howard; Performance at
low speeds of compressor rotors having low-cambered NACA 65-series blades with
high inlet angles and low solities; naca-tn-4344; Aug 1958
- Ivan E. Beckwith; Similar
solutions for the compressible boundary layer on a yawed cylinder with
transpiration cooling; naca-tn-4345; Sep 1958
- Martin T. Moul, Teresa
R. Brennan; Approximate
method for calculating motions in angles of attack and sideslip due to step
pitching- and yawing-moment inputs during steady roll; naca-tn-4346; Sep
1958
- Robert L. Trimpi,
Nathaniel B. Cohen; A
nonlinear theory for predicting the effects of unsteady laminar, turbulent, or
transitional boundary layers on the attenuation of shock waves in a shock tube
with experimental comparison; naca-tn-4347; Sep 1958
- Louis F. Vosteen; Effect of
temperature on dynamic modulus of elasticity of some structural alloys;
naca-tn-4348; Aug 1958
- Robert T. Swann; Heat transfer
and thermal stresses in sandwich panels; naca-tn-4349; Sep 1958
- Neal Tetervin; Theoretical
distribution of laminar-boundary-layer thickness, boundary-layer Reynolds
number and stability limit, and roughness Reynolds number for a sphere and
disk in incompressible flow; naca-tn-4350; Sep 1958
- William Gracey; Summary of
methods of measuring angle of attack on aircraft; naca-tn-4351; Aug
1958
- Vernard E. Lockwood,
Raymond D. Vogler; Exploratory
wind-tunnel investigation at high subsonic and transonic speeds of jet flaps
on unswept rectangular wings; naca-tn-4353; Aug 1958
- Alexander P. Sabol; Measurements in
a shock tube of heat-transfer rates at the stagnation point of a
1.0-inch-diameter sphere for real-gas temperatures up to 7,900 R;
naca-tn-4354; Aug 1958
- Robert D. Powell, Jr.,
Paul J. Carpenter; Low
tip Mach number stall characteristics and high tip Mach number compressibility
effects on a helicopter rotor having an NACA 0009 tip airfoil section;
naca-tn-4355; Jul 1958
- James P. Shivers, Paul
J. Carpenter; Effects
of compressibility on rotor hovering performance and synthesized blade-section
characteristics derived from measured rotor performance of blades having NACA
0015 airfoil tip sections; naca-tn-4356; Sep 1958
- Paul J. Carpenter; Lift and
profile-drag characteristics of an NACA 0012 airfoil section as derived from
measured helicopter-rotor hovering performance; naca-tn-4357; Sep
1958
- Eugene S. Love; Supersonic wave
interference affecting stability; naca-tn-4358; Sep 1958
- Frederick C. Hansen,
Steve P. Heims; A
review of the thermodynamic, transport, and chemical reaction rate properties
of high-temperature air; naca-tn-4359; Jul 1958
- Joseph M. Spiegel,
Phillips J. Tunnell, Warren S. Wilson; Measurements
of the effects of wall outflow and porosity on wave attenuation in a transonic
wind tunnel with perforated walls; naca-tn-4360; Aug 1958
- Elliott D. Katzen; Idealized wings
and wing-bodies at a Mach number of 3; naca-tn-4361; Jul 1958
- John B. McDevitt,
Robert A. Taylor; Force
and pressure measurements at transonic speeds for several bodies having
elliptical cross sections; naca-tn-4362; Sep 1958
- Albert L. Braslow,
Eugene C. Knox; Simplified
method for determination of critical height of distributed roughness particles
for boundary-layer transition at Mach numbers from 0 to 5; naca-tn-4363;
Sep 1958
- Alvin Seiff, Barbara J.
Short; An
investigation of supersonic turbulent boundary layers on slender bodies of
revolution in free flight by use of a Mach-Zehnder interferometer and
shadowgraphs; naca-tn-4364; Sep 1958
- James A. Weiberg, Roy
N. Griffin, George L. Florman; Large-scale
wind-tunnel tests of an airplane model with an unswept, aspect-ratio-10 wing,
two propellers, and area-suction flaps; naca-tn-4365; Sep 1958
- Fred A. Demele, K.
Harmon Powell; The
effects of an inverse-taper leading-edge flap on the aerodynamic
characteristics in pitch of a wing-body combination having an aspect ratio of
3 to 45 degrees of sweepback at Mach numbers to 0.92; naca-tn-4366; Aug
1958
- John L. McCloud, III,
George B. McCullough; Wind-tunnel
tests of a full-scale helicopter rotor with symmetrical and with cambered
blade sections at advance ratios from 0.3 to 0.4; naca-tn-4367; Sep
1958
- Lionel V. Baldwin; Slip-flow heat
transfer from cylinders in subsonic airstreams; naca-tn-4369; Sep
1958
- Peggy L. Yohner, Arthur
G. Hansen; Some numerical
solutions of similarity equations for three-dimensional laminar incompressible
boundary-layer flows; naca-tn-4370; Sep 1958
- S. R. Valluri; Some
observations relating to recovery of internal friction during fatigue of
aluminum; naca-tn-4371; Sep 1958
- E. E. Underwood, L. L.
Marsh, G. K. Manning; Effect
of precipitate particles on creep of aluminum-copper alloys during age
hardening; naca-tn-4372; Sep 1958
- Richard H. Kemp, Marvin
H. Hirschberg, William C. Morgan; Theoretical
and experimental analysis of the reduction of rotor blade vibration in
turbomachinery through the use of modified stator vane spacing;
naca-tn-4373; Sep 1958
- Vernon A. Slabey,
Edward A. Fletcher; Rate
of reaction of gaseous fluorine with water vapor at 35 C; naca-tn-4374;
Sep 1958
- Leroy L. Presley, Emmet
A. Mossman; A study of
several theoretical methods for computing the zero-lift wave drag of a family
of open-nosed bodies of revolution in the Mach number range of 2.0 to 4.0;
naca-tn-4368; Sep 1958
- Stewart, Elwood C
Druding, Frank Nishiura, Togo; The
effects of target and missile characteristics on theoretical minimum miss
distance for a beam-rider guidance system in the presence of noise;
naca-rm-a57f26; February 10, 1958
- Nielsen, Helmer V; Heat transfer
on an afterbody immersed in the separated wake of a hemisphere;
naca-rm-a57k07a; January 30, 1958
- Jorgensen, Leland H; Experimental
lift-drag ratios for two families of wing-body combinations at supersonic
speeds; naca-rm-a58a08; March 10, 1958
- Gloria, Hermilo R; An experimental
investigation of the static longitudinal stability and control characteristics
of a wingless missile configuration at Mach numbers from 3.0 to 6.3;
naca-rm-a58c20; June 24, 1958
- Gambucci, Bruno J Wyss,
John A; Experimental
investigation of the drag due to wedges along the trailing edge of a swept
wing; naca-rm-a58d15; June 27, 1958
- Cunningham, Bernard E
Kraus, Samuel; Experimental
investigation of the effect of yaw on rates of heat transfer to transverse
circular cylinders in a 6500-foot-per-second hypersonic air stream;
naca-rm-a58e19; August 26, 1958
- Hopkins, Edward J
Keating, Stephen J , Jr Muhl, Richard R; Forces
and pitching moments on an aspect-ratio-3.1 wing-body combination at Mach
numbers from 2.5 to 3.5 and sublimation studies of the effect of
single-elements roughness on the boundary-layer flow; naca-rm-a58e21a;
August 26, 1958
- Savin, Raymond C; Approximate
solutions for the flow about flat-top wing-body configurations at high
supersonic airspeeds; naca-rm-a58f02; September 15, 1958
- Lazzeroni, Frank A; Investigation
of wingless missile configurations with folding controls and low-aspect-ratio
stabilizing surfaces; naca-rm-a58f30; September 17, 1958
- Priem, Richard J Clark,
Bruce J; Comparison of
injectors with a 200-pound-thrust ammonia-oxygen engine; naca-rm-e57h01;
September 04, 1958
- Bloomer, Harry E; Experimental
results of an investigation of two methods of inflight thrust measurement
applicable to afterburning turbojet engines with ejectors; naca-rm-e57h28;
May 02, 1958
- Valentine, Harold H
Beale, William T; Experimental
investigation of distortion removal characteristics of several free-wheeling
fans; naca-rm-e57i12; January 07, 1958
- Rabb, Leonard
Krasnican, Milan J; Effects
of surface roughness and extreme cooling on boundary-layer transition for 15
degrees cone-cylinder in free flight at Mach numbers to 7.6;
naca-rm-e57k19; March 05, 1958
- Brokaw, Richard S; Correlation of
turbulent heat transfer in a tube for the dissociating system N204 reversibly
yields 2N02; naca-rm-e57k19a; March 05, 1958
- Nettles, J Gary
Campbell, Robert C; Investigation
at supersonic speeds of the compressor stall and inlet buzz characteristics of
a J34 - spike-inlet combination; naca-rm-e57k19b; March 05, 1958
- Gordon, Sanford; Theoretical
rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming
equilibrium composition; naca-rm-e57k22; February 25, 1958
- Stewart, Warner L; Analytical
investigation of multistage-turbine efficiency characteristics in terms of
work and speed requirements; naca-rm-e57k22b; February 18, 1958
- Stewart, Warner L
Evans, David G Whitney, Warren J; A
method for determining turbine design characteristics for rocket turbodrive
applications; naca-rm-e57k25a; May 02, 1958
- Dryer, Murray Luidens,
Roger W; Aerodynamic and
inlet-flow-field characteristics at a free-stream Mach number of 3.0 for
airplanes with circular fuselage cross sections and for two engine
locations; naca-rm-e57k26; March 18, 1958
- Woolett, Richard R
Ferguson, Harold M; Performance
of a two-dimensional cascade inlet at a free-stream Mach number of 3.05 and at
angles of attack of -3 degrees, 0 degrees, 3 degrees, and 6 degrees;
naca-rm-e57l06; March 05, 1958
- Esgar, Jack B Hickel,
Robert O Stepka, Francis S; Preliminary
survey of possible methods for hypersonic aircraft; naca-rm-e57l19; May
12, 1958
- Gordon, Sanford Glueck,
Alan R; Theoretical
performance of liquid ammonia with liquid oxygen as a rocket propellant;
naca-rm-e58a21; May 12, 1958
- Campbell, Carl E; Performance of
basic XJ79-GE-1 turbojet engine and its components; naca-rm-e58c12; May
08, 1958
- Baker, Louis, Jr; A study of the
combustion rates of hydrocarbon fuels with red fuming nitric acid in a small
rocket engine; naca-rm-e58d03a; August 06, 1958
- Schmidt, Harold W; Compatibility
of metals with liquid fluorine at high pressures and flow velocities;
naca-rm-e58d11; July 15, 1958
- Baker, Louis, Jr
Steffen, Fred W; Screaming
tendency of the gaseous-hydrogen - liquid-oxygen propellant combination;
naca-rm-e58e09; September 30, 1958
- Heidmann, M F Baker,
Louis, Jr; Combustor
performance with various hydrogen-oxygen injection methods in a
200-pound-thrust rocket engine; naca-rm-e58e21; September 30, 1958
- Moffitt, Thomas P; Design and
experimental investigation of a single-stage turbine with a rotor entering
relative Mach number of 2; naca-rm-e58f20a; September 15, 1958
- Anderson, Bernhard H
Bowditch, David N; Investigation
of inlet control parameters for an external-internal-compression inlet from
Mach 2.1 to 3.0; naca-rm-e58g08; September 23, 1958
- Samanich, Nick E
Cubbison, Robert W; A
pivoting-cowl-and-spike technique for efficient angle-of-attack operation of
supersonic inlets; naca-rm-e58g11a; September 23, 1958
- Nettles, J Cary; Experimental
study of ballistic-missile base heating with operating rocket;
naca-rm-e58g17; September 23, 1958
- Johnson, Clinton T; Flight
investigation of the aerodynamic forces on a wing-mounted external-store
installation on the Douglas D-558-II research airplane; naca-rm-h58b24;
May 13, 1958
- Drake, Hubert M
Bellman, Donald R Walker, Joseph A; Operational
problems of manned orbital vehicles; naca-rm-h58d21; July 21, 1958
- Rowe, John P
(University of Michigan) Freeman, J W (University of Michigan); Effect
of overheating on creep-rupture properties of M-252 alloy; naca-tn-4224;
March 1958
- Stivers, Louis S , Jr
Lippmann, Garth W; Effects
of fixing boundary-layer transition for an unswept-wing model and an
evaluation of porous tunnel-wall interference for Mach numbers from 0.60 to
1.40; naca-tn-4228; April 1958
- Eggers, A J , Jr
Hansen, C Frederick Cunningham, Bernard E; Stagnation-point
heat transfer to blunt shapes in hypersonic flight, including effects of
yaw; naca-tn-4229; April 1958
- Heims, Steve P; Prandtl-Meyer
expansion of chemically reacting gases in local chemical and thermodynamic
equilibrium; naca-tn-4230; March 1958
- Smith, Donald W Walker,
John H; Skin-friction
measurements in incompressible flow; naca-tn-4231; March 1958
- Lomax, Harvard Sluder,
Loma; A
method for the calculation of wave drag on supersonic-edged wings and
biplanes; naca-tn-4232; March 1958
- Page, William A; Experimental
study of the equivalence of transonic flow about slender cone-cylinders of
circular and elliptic cross section; naca-tn-4233; April 1958
- Taylor, Robert A
Mcdevitt, John B; Pressure
distributions at transonic speeds for parabolic-arc bodies of revolution
having fineness ratios of 10, 12, and 14; naca-tn-4234; March 1958
- James, Carlton S; Observations of
turbulent-burst geometry and growth in supersonic flow; naca-tn-4235;
April 1958
- Tendeland, Thorval; Effects of Mach
number and wall-temperature ratio on turbulent heat transfer at Mach numbers
from 3 to 5; naca-tn-4236; April 1958
- Brevoort, Maurice J
Arabian, Barbara D; Summary
of experimental heat-transfer measurements in turbulent flow for a Mach number
range from 0.87 to 5.05; naca-tn-4248; May 1958
- Gates, Ordway B , Jr
Woodling, C H; A
theoretical analysis of the effect of engine angular momentum on longitudinal
and directional stability in steady rolling maneuvers; naca-tn-4249; April
1958
- Huss, Carl R Donegan,
James J; Effect of the
proximity of the wing first-bending frequency and the short-period frequency
on the airplane dynamic-response factor; naca-tn-4250; June 1958
- Mcbride, Ellis E
Fisher, Lloyd J; An
experimental investigation of wake effects on hydro-skis; naca-tn-4251;
May 1958
- Sterrett, James R; Experimental
investigation of an impulse-type supersonic compressor rotor having a turning
of 73 degrees at the mean radius; naca-tn-4252; June 1958
- Bland, William M , Jr
Kolenkiewicz, Ronald; Free-flight
pressure measurements over a flare-stabilized rocket model with a modified Von
Karman nose for Mach numbers up to 4.3; naca-rm-l57j24; January 13,
1958
- Ludi, Leroy H; Flight
investigation of effects of retreating-blade stall on bending and torsional
moments encountered by a helicopter rotor blade; naca-tn-4254; May
1958
- Johnson, Joseph L , Jr;
Wind-tunnel
investigation at low speeds of flight characteristics of a sweptback-wing
jet-transport airplane model equipped with an external-flow jet-augmented
slotted flap; naca-tn-4255; July 1958
- Schnitzer, Emanuel; Water-impact
theory for aircraft equipped with nontrimming hydro-skis mounted on shock
struts; naca-tn-4256; September 1958
- Silveira, Milton A
Maglieri, Domenic J Brooks, George W; Results
of an experimental investigation of small viscous dampers; naca-tn-4257;
June 1958
- Cahn, Maurice S Olstad,
Walter B; A
numerical method for evaluating wave drag; naca-tn-4258; June 1958
- Huntley, Sidney C; Temperature-pressure-time
relations in a closed cryogenic container; naca-tn-4259; February
1958
- Howes, Walton L; Ground
reflection of jet noise; naca-tn-4260; April 1958
- Ciepluch, Carl C North,
Warren J Coles, Willard D Antl, Robert J; Acoustic,
thrust, and drag characteristics of several full-scale noise suppressors for
turbojet engines; naca-tn-4261; April 1958
- Deissler, R G Loeffler,
A L , Jr; Analysis of
turbulent flow and heat transfer on a flat plate at high Mach numbers with
variable fluid properties; naca-tn-4262; April 1958
- Signorelli, Robert A
Johnston, James R Garrett, Floyd B; Effect
of prior air force over temperature operation on life of J47 buckets evaluated
in a sea-level cyclic engine test; naca-tn-4263; April 1958
- Mcardle, Jack G; Internal
characteristics and performance of several jet deflectors at primary-nozzle
pressure ratios up to 3.0; naca-tn-4264; June 1958
- Clark, Thomas P; Studies of OH,
CO, CH, and C(sub 2) radiation from laminar and turbulent propane-air and
ethylene-air flames; naca-tn-4266; June 1958
- Baldwin, Lionel V
Blackshear, Perry L; Preliminary
survey of propulsion using chemical energy stored in the upper atmosphere;
naca-tn-4267; May 1958
- Gelder, Thomas F; Droplet
impingement and ingestion by supersonic nose inlet in subsonic tunnel
conditions; naca-tn-4268; May 1958
- North, Warren J; Transonic drag
of several jet-noise suppressors; naca-tn-4269; April 1958
- Hearth, Donald P
Connors, James F; A
performance analysis of methods for handling excess inlet flow at supersonic
speeds; naca-tn-4270; May 1958
- Moffitt, Thomas P; Maximum
theoretical tangential velocity component possible from straight-back
converging and converging-diverging stators at supercritical pressure
ratios; naca-tn-4271; April 1958
- Von Glahn, Uwe H; Use of the
Coanda effect for obtaining jet deflection and lift with a single flat-plate
deflection surface; naca-tn-4272; June 1958
- Ostrach, Simon Albers,
Lynn U; On
pairs of solutions of a class of internal viscous flow problems with body
forces; naca-tn-4273; June 1958
- Bader, Michel Carlson,
William C A; Measurement of
the effect of an axial magnetic field on the Reynolds number of transition in
mercury flowing through a glass tube; naca-tn-4274; May 1958
- Tobak, Murray Allen, H
Julian; Dynamic
stability of vehicles traversing ascending or descending paths through the
atmosphere; naca-tn-4275; July 1958
- Chapman, Dean R; An approximate
analytical method for studying entry into planetary atmospheres;
naca-tn-4276; May 1958
- Pitts, William C
Nielsen, Jack N; A
body modification to reduce drag due to wedge angle of wing with unswept
trailing edge; naca-tn-4277; July 1958
- Stewart, Elwood C; Application of
statistical theory to beam-rider guidance in the presence of noise II :
modified Wiener filter theory; naca-tn-4278; June 1958
- Hunton, Lynn W; Effects of
fixing transition on the transonic aerodynamic characteristics of a wing-body
configuration at Reynolds numbers from 2.4 to 12 million; naca-tn-4279;
July 1958
- Mcdevitt, John B
Taylor, Robert A; Pressure
distributions at transonic speeds for slender bodies having various axial
locations of maximum diameter; naca-tn-4280; July 1958
- Van Dyke, Milton D; Second-order
slender-body theory : axisymmetric flow; naca-tn-4281; September
1958
- Rossow, Vernon J; Boundary-layer
stability diagrams for electrically conducting fluids in the presence of a
magnetic field; naca-tn-4282; August 1958
- Tolhurst, William H ,
Jr; Full-scale
wind-tunnel tests of a 35 degree sweptback-wing airplane with blowing from the
shroud ahead of the trailing-edge flaps; naca-tn-4283; July 1958
- Rey, William K
(University of Alabama); Cumulative
fatigue damage at elevated temperature; naca-tn-4284; September
1958
- Shepard, L A
(University of California, Berkeley) Giedt, W H (University of California,
Berkeley); Triangular and
intergranular fracture of ingot iron during creep; naca-tn-4285; August
1958
- Decker, R F (University
of Michigan) Freeman, J W (University of Michigan); Mechanism
of beneficial effects of boron and zirconium on creep-rupture properties of a
complex heat-resistant alloy; naca-tn-4286; August 1958
- Black, J M (Forest
Products Laboratory) Blomquist, R F (Forest Products Laboratory); Relationship
of metal surfaces to heat-aging properties of adhesive bonds;
naca-tn-4287; September 1958
- Mills, R R , Jr (Johns
Hopkins University) Kistler, A L (Johns Hopkins University) O'Brien, V (Johns
Hopkins University) Corrsin, S (Johns Hopkins University); Turbulence
and temperature fluctuations behind a heated grid; naca-tn-4288; August
1958
- Rhyne, Richard H; Measurements of
the motions of a large swept-wing airplane in rough air; naca-tn-4310;
September 1958
- Bittker, David A; An analytical
study of turbulent and molecular mixing in rocket combustion;
naca-tn-4321; September 1958
- Patterson, Elizabeth W
Braslow, Albert L; Ordinates
and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil
sections with thicknesses from 2 to 21 and from 2 to 15 percent chord,
respectively; naca-tn-4322; September 1958
- Ostrach, Simon Braun,
Willis H; Natural
convection inside a flat rotating container; naca-tn-4323; September
1958
- Kaufman, Albert; Method for
determining the need to rework or replace compressor rotor blades damaged by
foreign objects; naca-tn-4324; September 1958
- Graham, Robert W
Guentert, Eleanor Costilow Huff, Vearl N; A
Mach 4 rocket-powered supersonic tunnel using ammonia-oxygen as working
fluid; naca-tn-4325; September 1958
- Robb, J D (Lightning
and Transients Research Institute) Hill, E L (Lightning and Transients
Research Institute) Newman, M M (Lightning and Transients Research Institute)
Stahmann, J R (Lightning and Transients Research Institute); Lightning
hazards to aircraft fuel tanks; naca-tn-4326; September 1958
- Talbot, Lawrence
(University of California) Koga, Toyoki (University of California) Sherman,
Pauline M (University of California); Hypersonic
viscous flow over slender cones; naca-tn-4327; September 1958
- Maringer, R E (Battelle
Memorial Institute) Swetnam, E B (Battelle Memorial Institute) Marsh, L L
(Battelle Memorial Institute) Manning, G K (Battelle Memorial Institute); Study of
hydrogen embrittlement of iron by internal-friction methods; naca-tn-4328;
September 1958
- Decker, R F (University
of Michigan) Rowe, John P (University of Michigan) Bigelow, W C (University of
Michigan) Freeman, J W (University of Michigan); Influence
of heat treatment on microstructure and high-temperature properties of
nickel-base precipitation-hardening alloy; naca-tn-4329; July 1958
- White, Maurice D
Schlaff, Bernard A Drinkwater, Fred J , III; A
comparison of flight-measured carrier-approach speeds with values predicted by
several different criteria for 41 fighter-type airplane configurations;
naca-rm-a57l11; May 08, 1958
- Kelly, Mark W Anderson,
Seth B Innis, Robert C; Blowing-type
boundary-layer control as applied to the trailing-edge flaps of a 35 degree
swept-wing airplane; naca-rm-a55i09; 1958
- Demele, Fred A; Effects of
leading-edge slat and trailing-edge split flap on the aerodynamic
characteristics of a wing-fuselage combination having a nearly triangular wing
of aspect ratio 2.9 at Mach numbers from 0.60 to 0.92; naca-rm-a57h19;
January 12, 1958
- Axelson, John A; Transonic
lateral and longitudinal aerodynamic characteristics of a lateral-control
system employing rotatable airfoils mounted vertically at the wing tips of an
unswept wing-fuselage-tail combination; naca-rm-a57j16; January 07,
1958
- Boyd, John W Peterson,
Victor L; Static
stability and control of canard configurations at Mach numbers from 0.70 to
2.22 : triangular wing and canard on an extended body; naca-rm-a57k14;
February 10, 1958
- Gnos, A Vernon
Kurkowski, Richard L; Static
longitudinal and lateral stability and control characteristics of a model of a
swept-wing fighter-bomber-type airplane with a top inlet at Mach numbers from
1.6 to 2.35; naca-rm-a57k20; March 03, 1958
- Peterson, Victor L
Menees, Gene P; Static
stability and control of canard configurations at Mach numbers from 0.70 to
2.22longitudinal characteristics of a triangular wing and unswept canard;
naca-rm-a57k26; February 17, 1958
- Peterson, Victor L
Boyd, John W; Static
stability and control of canard configurations at Mach numbers from 0.70 to
2.22 : longitudinal characteristics of an unswept wing and canard;
naca-rm-a57k27; February 17, 1958
- Triplett, William C; The effects of
a modified roll-command system on the flight-path stability and tracking
accuracy of an automatic interceptor; naca-rm-a57l11a; March 04,
1958
- Nielsen, Jack N; The effects of
body vortices and the wing shock-expansion field on the pitch-up
characteristics of supersonic airplanes; naca-rm-a57l23; March 24,
1958
- Hickey, David H Aoyagi,
Kiyoshi; Large-scale
wind-tunnel tests of an airplane model with a 45 degree sweptback wing of
aspect ratio 2.8 employing high-velocity blowing over the leading- and
trailing-edge flaps; naca-rm-a58a09; May 26, 1958
- Beam, Benjamin H
Endicott, Kenneth C; Wind-tunnel
data on the longitudinal and lateral-directional rotary derivatives of a
straight-wing, research airplane configuration at Mach numbers from 2.5 to
3.5; naca-rm-a58a14; March 25, 1958
- Dickey, Robert R; The effect of
moment-of-area-rule modifications on the zero-lift drag of three wing-body
combinations; naca-rm-a58a31; May 02, 1958
- Wingrove, Rodney C; A flight-test
study of total-pressure distortion in a thick-lipped nose inlet;
naca-rm-a58b07; June 30, 1958
- Scherrer, Richard
Anderson, Warren E; Investigation
of the performance and internal flow of a variable-area,
variable-internal-contraction inlet at Mach numbers of 2.00, 2.50, and
2.92; naca-rm-a58c24; July 15, 1958
- Evans, William T; Data from
flow-field surveys behind a large-scale thin straight wing of aspect ratio
3; naca-rm-a58d17; June 23, 1958
- Scherrer, Richard
Lundell, John H Anderson, Lewis A; Viscous
flows in inlets; naca-rm-a58d17a; June 30, 1958
- Winovich, Warren
Higdon, Nancy S; Evaluation
of some aerodynamic controls for a low-aspect-ratio missile;
naca-rm-a58d17b; July 17, 1958
- Havill, C Dewey
Wingrove, Rodne C; Flight
investigation of a full-scale aircraft ejector with various spacing ratios and
correlation with small-scale tests; naca-rm-a58d21; August 26, 1958
- Hall, Charles F Boyd,
John W; Effects of
canards on airplane performance and stability; naca-rm-a58d24; July 07,
1958
- Summers, James L; Wind-tunnel
investigation at Mach numbers from 0.6 to 1.4 of several ejected pilot-seat
models; naca-rm-a58e02; September 10, 1958
- Quigley, Hervey C
Anderson, Seth B Innis, Robert C; Flight
investigation of the low-speed characteristics of a 45 degree swept-wing
fighter-type airplane with blowing boundary-layer control applied to the
trailing edge flaps; naca-rm-a58e05; August 04, 1958
- Turner, Howard L
Heinle, Donovan R; A
flight study of the effects of noise filtering in the attack display on the
pilot's tracking performance; naca-rm-a58e21; September 10, 1958
- Kelly, Mark W; Wind-tunnel
investigation of the low-speed aerodynamic characteristics of a hypersonic
glider configuration; naca-rm-a58f03; September 15, 1958
- Lopez, Armando E
Tinling, Bruce E; The
static and dynamic-rotary stability derivatives at subsonic speeds of a model
of the X-15 research airplane; naca-rm-a58f09; September 15, 1958
- Syvertson, Clarence A
Gloria, Hermilo R Sarabia, Michael F; Aerodynamic
performance and static stability and control of flat-top hypersonic gliders at
Mach numbers from 0.6 to 18; naca-rm-a58g17; September 17, 1958
- Aoyagi, Kiyoshi Hickey,
David H; Large-scale
wind-tunnel tests of a jet-transport-type model with leading- and
trailing-edge high-lift devices; naca-rm-a58h12; September 26, 1958
- Sadoff, Melvin Stewart,
John D; An
analytical evaluation of the effects of an aerodynamic modification and of
stability augmenters on the pitch behavior and probable pilot opinion of two
current fighter airplanes; naca-rm-a57k07; April 21, 1958
- Lampkin, Bedford A
Tunnell, Phillips J; Static
and dynamic-rotary stability derivatives of an airplane model with an unswept
wing and a high horizontal tail at Mach numbers of 2.5, 3.0, and 3.5;
naca-rm-a58f17; September 26, 1958
- Stitt, Leonard E Obery,
Leonard J; Performance of
an all-internal conical compression inlet with annular throat bleed at Mach
number 5.0; naca-rm-e58e14; August 06, 1958
- Banner, Richard D
Mctigue, John G Petty, Gilbert, Jr; Boundary-layer-transition
measurements in full-scale flight; naca-rm-h58e28; July 28, 1958
- Fields, E M Wakelyn, N
T; Limited
tests of molybdenum coated with molybdenum disilicide in a supersonic
heated-air jet and brief description of the coating facility;
naca-rm-l57i12; January 09, 1958
- Howell, Robert R; An initial
experimental study of the effect of variations in frequency and impulse on the
reduction in temperature recovery factor afforded by large-scale unsteady
flow; naca-rm-l57i27; January 22, 1958
- Mackley, Ernest A; Effect of inlet
aspect ratio on the starting and pressure recovery characteristics of a
rectangular swept scoop inlet tested at a Mach number of 3.1;
naca-rm-l57j07; January 13, 1958
- Rumsey, Charles B Lee,
Dorothy B; Measurements of
aerodynamic heat transfer on a 15 degree cone-cylinder-flare configuration in
free flight at Mach numbers up to 4.7; naca-rm-l57j10; January 22,
1958
- Swihert, John M; Effect of
target-type thrust reverser on transonic aerodynamic characteristics of a
single-engine fighter model; naca-rm-l57j16; January 13, 1958
- Bland, William M , Jr;
Effectiveness
of various protective coverings on magnesium fins at Mach number 2.0 and
stagnation temperatures up to 3,600 R; naca-rm-l57j17; January 09,
1958
- Schult, Eugene D; Free-flight
roll performance of a steady-flow jet-spoiler control on an 80 degree
delta-wing missile between Mach numbers of 0.6 and 1.8; naca-rm-l57j28;
January 24, 1958
- Mcfarland, Donald R
Huber, Paul W; Investigation
of vortex movements about a wing in steady subsonic flow undergoing a large
angle-of-attack change in a blast-induced gust; naca-rm-l57k04; January
22, 1958
- Robins, A Warner; Wind-tunnel
investigation of the effects of lip geometry on drag and pressure recovery of
a normal-shock nose inlet on a body of revolution at Mach numbers of 1.41 and
1.81; naca-rm-l57k08; February 03, 1958
- Bland, William M , Jr;
Some effects
of fin leading-edge shape on aerodynamic heating at Mach number 2.0 at a
stagnation temperature of about 2,600 R; naca-rm-l57k12; January 09,
1958
- Casey, Francis W , Jr
Hopko, Russell N; Preliminary
investigation of graphite, silicon carbide, and several polymer-glass-cloth
laminates in a Mach number 2 air jet at stagnation temperatures of 3,000 F and
4,000 F; naca-rm-l57k15; January 09, 1958
- Polhamus, Edward C
Spreemann, Kenneth P; Effect
at high subsonic speeds of fuselage forebody strakes on the static stability
and vertical-tail-load characteristics of a complete model having a delta
wing; naca-rm-l57k15a; February 10, 1958
- Morris, Odell A
Carlson, Harry W Geier, Douglas J; Experimental
and theoretical determination of forces and moments on a store and on a
store-pylon combination mounted on a 45 degree swept-wing-fuselage
configuration at a Mach number of 1.61; naca-rm-l57k18; January 30,
1958
- Kinard, William H; Feasibility of
nose-cone cooling by the upstream ejection of solid coolants at the stagnation
point; naca-rm-l57k22; March 24, 1958
- Fields, E M Hopko,
Russel N Swain, Robert L Trout, Otto F , Jr; Behavior
of some materials and shapes in supersonic free jets at stagnation
temperatures up to 4,210 F, and descriptions of the jets; naca-rm-l57k26;
February 24, 1958
- Bland, William M , Jr
Swanson, Andrew G Kolenkiewicz, Roland; Free-flight
aerodynamic-heating data at Mach numbers up to 10.9 on a flat-faced
cylinder; naca-rm-l57k29; January 13, 1958
- Garland, Benjamine J
Hall, James R; Measurements
of aerodynamic heat transfer in turbulent separated regions at a Mach number
of 1.8; naca-rm-l57l09; February 20, 1958
- Yates, E Carson, Jr; Calculation of
flutter characteristics for finite-span swept or unswept wings at subsonic and
supersonic speeds by a modified strip analysis; naca-rm-l57l10; March 18,
1958
- Clark, Frank L Edwards,
Clyde L W; An
investigation at Mach numbers 1.94 and 2.41 of jet effects upon the
longitudinal and directional stability of a general aircraft configuration
employing wing-tip-mounted nacelles; naca-rm-l57l18a; March 04,
1958
- Lee, Dorothy B Swanson,
Andrew G; Heat transfer
measured on a flat-face cylinder-flare configuration in free flight at Mach
numbers from 1.6 to 2.7; naca-rm-l58a06; February 03, 1958
- Foster, Gerald V; Effects of nose
and afterbody modifications on aerodynamic characteristics of a body with and
without a vertical tail at a Mach number of 2.01; naca-rm-l58a10; April
15, 1958
- O'Neal, Robert L Bond,
Aleck C; Heat transfer
to 0 degree and 75 degree swept blunt leading edges in free flight at Mach
numbers from 1.90 to 3.07; naca-rm-l58a13; March 24, 1958
- Braslow, Albert L; Effect of
distributed granular-type roughness on boundary-layer transition at supersonic
speeds with and without surface cooling; naca-rm-l58a17; March 10,
1958
- Robinson, Ross B; Wind-tunnel
investigation at a Mach number of 2.01 of the aerodynamic characteristics in
combined angles of attack and sideslip of several hypersonic missile
configurations with various canard controls; naca-rm-l58a21; March 10,
1958
- Nelson, William J
Scott, William R; Jet
effects on the base drag of a cylindrical afterbody with extended nozzles;
naca-rm-l58a27; April 15, 1958
- Speegle, Katherine C
Chauvin, Leo T Heberlig, Jack C; Heat
transfer for Mach numbers up to 2.2 and pressure distributions for Mach
numbers up to 4.7 from flight investigations of a flat-face-cone and a
hemisphere-cone; naca-rm-l58b18; May 08, 1958
- Markley, J Thomas; Heat transfer
and pressure measurement on a 5-inch hemispherical concave nose at a Mach
number of 2.0; naca-rm-l58c14a; July 17, 1958
- Presnell, John G , Jr;
Investigation
of control effectiveness and stability characteristics of a model of a
low-wing missile with interdigitated tail surfaces at Mach numbers of 2.29,
2.97, and 3.51; naca-rm-l58c19; July 14, 1958
- Hall, James R Garland,
Benjamine J; A feasibility
study of the flare-cylinder configuration as a reentry body shape for an
intermediate range ballistic missile; naca-rm-l58c21; May 28, 1958
- Griffith, George E
Miltonberger, Georgene H; Tests
of aerodynamically heated multiweb wing structures in a free jet at Mach
number 2 and aluminum-alloy model of 40-inch chord with 0.125-inch-thick
skin; naca-rm-l58c24; June 23, 1958
- Runyan, Harry L Jones,
Nan H; Effect of
aerodynamic heating on the flutter of a rectangular wing at a Mach number of
2; naca-rm-l58c31; June 23, 1958
- Burbank, Paige B
Strass, H Kurt; Heat
transfer to surfaces and protuberances in a supersonic turbulent boundary
layer; naca-rm-l58e01a; July 14, 1958
- Rainey, A Gerald
Hanson, Perry W Martin, Dennis J; Experimental
and analytical investigation of the transonic and supersonic divergence
characteristics of a delta-plan-form all-movable control; naca-rm-l58e07;
August 04, 1958
- Faget, Maxime A
Garland, Benjamine J Buglia, James J; Preliminary
studies of manned satellites : wingless configuration: nonlifting;
naca-rm-l58e07a; August 11, 1958
- Woodling, C H Whitten,
James B Champine, Robert A Andrews, Robert E; Simulation
study of a high-performance aircraft including the effect on pilot control of
large accelerations during exit and reentry flight; naca-rm-l58e08a; July
17, 1958
- Bond, Aleck C Rashis,
Bernard Levin, L Ross; Experimental
ablation cooling; naca-rm-l58e15a; July 15, 1958
- Smith, Fred M Ulmann,
Edwards F Dunning, Robert W; Longitudinal
and lateral aerodynamic characteristics at combined angles of attack and
sideslip of a generalized missile model having a rectangular wing at a Mach
number of 4.08; naca-rm-l58e26; August 14, 1958
- Phillips, William H; Analysis of
effects of interceptor roll performance and maneuverability on success of
collision-course attacks; naca-rm-l58e27; August 06, 1958
- Mugler, John P , Jr; Analysis of
pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered
delta wing-body combination; naca-rm-l58f24; September 26, 1958
- Rainey, A Gerald Igoe,
William B; Measurements of
the buffeting loads on the wing and horizontal tail of a 1/4-scale model of
the X-1E airplane; naca-rm-l58f25; September 17, 1958
- Swanson, Andrew; Free-flight
investigation of aerodynamic heat transfer to a simulated glide-rocket shape
at Mach numbers up to 10; naca-rm-l58g03; September 10, 1958
- Lee, Dorothy B Rumsey,
Charles B Bond, Aleck C; Heat
transfer measured in free flight on a slightly blunted 25 degree
cone-cylinder-flare configuration at Mach numbers up to 9.89;
naca-rm-l58g21; September 26, 1958
- Coltrane, Lucille C; Stability
investigation of a blunt cone and a blunt cylinder with a square base at Mach
numbers from 0.64 to 2.14; naca-rm-l58g24; September 17, 1958
- Martz, C William; Rocket-model
investigation to determine the lift and pitching effectiveness of small pulse
rockets exhausted from the fuselage over the surface of an adjacent wing at
Mach numbers from 0.9 to 1.8; naca-rm-l58g29; September 30, 1958
- ; Free
convection under the conditions of the internal problem; naca-tm-1407;
1958
- Fabri, J., Paulon, J.;
Theory and
experiments on supersonic air-to-air ejectors; naca-tm-1410; 1958
- ; Impact
on a compressible fluid; naca-tm-1413; 1958
- ; Aerodynamic
research on fuselages with rectangular cross section; naca-tm-1414;
1958
- ; The
interaction of a reflected shock wave with the boundary layer in a shock
tube; naca-tm-1418; 1958
- Heisenberg, W.; On the
statistical theory of turbulence; naca-tm-1431; 1958
- ; Stability
of cylindrical and conical shells of circular cross section, with simultaneous
action of axial compression and external normal pressure; naca-tm-1433;
1958
- ; Extreme
speeds and thermodynamic states in supersonic flight; naca-tm-1434;
1958
- ; Elliptic
functions and integrals with real modulus in fluid mechanics;
naca-tm-1435; 1958
- ; Statiscal
study of turbulence - spectral functions and correlation coefficients;
naca-tm-1436; 1958
- ; On
possible similarity solutions for three-dimensional incompressible laminar
boundary-layer flows over developable surfaces and with proportional
mainstream velocity components; naca-tm-1437; 1958
- ; On
the flutter of cylindrical shells and panels moving in a flow of gas;
naca-tm-1438; 1958
- ; Application
of the method of coordinate perturbation to unsteady duct flow;
naca-tm-1439; 1958
- ; The
turbulent boundary layer on a rough curvilinear surface; naca-tm-1440;
1958
- Sugawara, Sugao., Sato,
Takashi., Komatsu, Hiroyasu., Osaka, Hiroichi.; The
effect of free-stream turbulence on heat transfer from a flat plate;
naca-tm-1441; 1958
- Seiff, Alvin.; The
prospects for laminar flow on hypersonic airplanes; naca-rm-a58d25;
1958
- Matting, Fred W.,
Chapman, Dean R.; Turbulent
skin friction at high mach numbers and reynolds numbers; naca-rm-a58d28;
1958
- Turner, Howard L.,
Rathert, George A., Jr., Heinle, Donovan R.; Tracking
performance of a swept-wing fighter with a director-type radar fire-control
system and scope presentation; naca-rm-a57j01; 1958
- Boyd, John W.,
Peterson, Victor L.; Static
stability and control of canard configurations at Mach numbers from 0.70 to
2.22 :longitudinal characteristics of a triangular wing and canard;
naca-rm-a57j15; 1958
- Reese, David E., Jr.;
A
wind-tunnel investigation of several wingless missile configurations at
supersonic speeds; naca-rm-a57j22; 1958
- Holzhauser, Curt A.; Wind-tunnel
investigation of the use of leading-edge and trailing-edge area-suction flaps
on a 13-percent-thick straight wing and fuselage model; naca-rm-a57k01;
1958
- Tinling, Bruce E.; Subsonic
aerodynamic characteristics up to extreme angles of attack of an airplane
model having an unswept wing and a high horizontal tail; naca-rm-a57k05;
1958
- Wyss, John A.,
Sorenson, Robert M., Gambucci, Bruno J.; Effects
of modifications to a control surface on a 6-percent-thick unswept wing on the
transonic control-surface flutter derivatives; naca-rm-a58b04; 1958
- Holdaway, George H.,
Hatfield, Elaine W.; Transonic
investigation of yawed wings of aspect ratios 3 and 6 with a Sears-Haack body
and with symmetrical and asymmetrical bodies indented for a Mach number of
1.20; naca-rm-a58c03; 1958
- Sammonds, Robert I.,
Reynolds, Robert M.; The
static longitudinal characteristics of a twisted and cambered 45 degree
sweptback wing at Mach numbers up to 0.96; naca-rm-a58c21; 1958
- Marie Luise Exner; Investigation
of Aperiodic Time Processes with Autocorrelation and Fourier Analysis;
naca-tm-1404; 1958
- Nils Frossling; Evaporation,
Heat Transfer, and Velocity Distribution in Two-Dimensional and Rotationally
Symmetrical Laminar Boundary-Layer FLow; naca-tm-1432; 1958
- Sanford Gordon and
Michael E. Kastner (Lewis Flight Propulsion Laboratory, Cleveland, Ohio); Theoretical
Rocket Performance of Liquid Methane with Several Flourine-Oxygen Mixtures
Assuming Frozen Composition; naca-rm-e58b20; 1958
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9, 2006, 12:07 pm
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Paul A S
Needham