Suggested Topics within your search.
Suggested Topics within your search.
- Charts, diagrams, etc 484
- Airplanes 447
- Wind tunnel testing 206
- Testing 121
- Motors 112
- Aerofoils 107
- Models 87
- Control 86
- Flaps (Airplanes) 79
- Wings 76
- Ailerons 71
- Mathematics 69
- Drag (Aerodynamics) 62
- Air flow 61
- Control surfaces 55
- Cooling 52
- Stability of airplanes 52
- Flight testing 51
- Fighter planes 47
- Seaplanes 45
- Propellers, Aerial 42
- Tail surfaces 42
- Aerodynamic load 40
- Ice prevention 40
- Performance 38
- Fuel 37
- Cylinders 32
- Pressure 32
- Elevators (Airplanes) 30
- Heat 29
-
261
Design criterions for the dimensions of the forebody of a long-range flying boat /
Published 1943Government Document Book -
262
Measurements of friction coefficients in a pipe for subsonic and supersonic flow of air /
Published 1943Government Document Book -
263
Foaming of aircraft-engine oils as a problem in colloid chemistry - I /
Published 1944Government Document Book -
264
Effects on low-speed spray characteristics of various modifications to a powered model of the Boeing XPBB-1 flying boat /
Published 1945Government Document Book -
265
Statistical analysis of the characteristics of repeated gusts in turbulent air /
Published 1945Government Document Book -
266
Effect of compressibility on pressure distribution over an airfoil with a slotted frise aileron /
Published 1944Government Document Book -
267
The effects of an increase in the concentration of ethylene dibromide in a leaded fuel on lead dposition, corrosion of exhaust valves, and knock-limited power /
Published 1945Government Document Book -
268
Full-scale wind-tunnel and flight tests of a Fairchild XR2K-1 airplane with a Zap flap and upper-surface aileron-wing installation /
Published 1942Government Document Book -
269
Drag measurements of a protruding .50-caliber machine gun with barrel jacket removed /
Published 1943Government Document Book -
270
Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 6 degrees and 9 degrees trim and a 22.5 degree angle of dead rise /
Published 1946Government Document Book -
271
Tank tests of a powered dynamic model of a flying boat having an afterbody length-beam ratio of 4.7-Langley tank model 203C-1 /
Published 1945Government Document Book -
272
Ditching tests of a 1/8-scale model of the Navy SB2C-1 airplane (Army A-25) in Langley tank number 2 and on an outdoor catapult /
Published 1946Government Document Book -
273
Performance of an exhaust-gas "blowdown" turbine on a nine-cylinder radial engine /
Published 1944Government Document Book -
274
Flight variables affecting fuel-vapor loss from a fuel tank /
Published 1944Government Document Book -
275
Elimination of rumble from the cooling ducts of a single-engine pursuit plane /
Published 1943“…NACA Wartime Reports. Series A.…”
Government Document Book -
276
High-speed wind-tunnel tests of a twin-fuselage pursuit airplane /
Published 1946“…NACA Wartime Reports. Series A.…”
Government Document Book -
277
Compressibility and heating effects on pressure loss and cooling of a baffled cylinder barrel /
Published 1944Government Document Book -
278
Wind-tunnel investigation of rounded horns and of guards on a horizontal tail surface /
Published 1944Government Document Book -
279
The knock-limited performance of several miscellaneous fuels blended with a base fuel /
Published 1944Government Document Book -
280
Cooling of a double-row radial engine by water injection to the individual cylinders /
Published 1945Government Document Book