NACA UK Archive results page

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;