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- Fuel consumption corrected for cooling drag of an air-cooled radial aircraft engine at low fuel-air ratios and with variable spark advance
- An investigation of a thermal ice-prevention system for a C-46 cargo airplane VII : effect of the thermal system on the wing-structure stresses as established in flight
- Investigation of a method of comparison of metallic surface contours by means of stereoscopic electron micrographs
- Infrared-spectrophotometric analysis of binary and ternary mixtures of liquid hydrocarbons
- An infrared cloud indicator I : analysis of infrared-radiation exchange with tables and chart for calibration of the cloud indicator
- The influence of vertical-tail design and direction of propeller rotation on trim characteristics of a twin-engine-airplane model with one engine inoperative
- Measurements in flight of the pressure distribution on the right wing of a P-39N-1 airplane at several values of Mach number
- A method for studying the longitudinal dynamic stability of flying-boat-hull models at high planing speeds and during landing
- Quantitative analysis for aromatic amines in aviation fuels by ultraviolet spectrophotometry
- The oxidation of exhaust gases at room temperature
- Note on compressibility effects on downwash at the tail at subcritical speeds
- Preliminary investigation of deep inducers as separate supercharger components
- Langley full-scale-tunnel stability and control tests of the Bell YP-59A airplane
- Low-pressure boundary-layer control in diffusers and bends
- Measurement of operating stresses in an aircraft engine crankshaft under power
- Frequency of occurrence of critical gust loads on overloaded airplanes
- Heat-transfer tests of several engine coolants
- Operating stresses in aircraft-engine crankshafts and connecting rods 2: instrumentation and test results
- The Effect of Compression Ratio on Knock Limits of High-Performance Fuels in a CFR Engine II : Blends of 2,2,3-Trimethylpentane with 28-R
- Effect of changing the stroke on air capacity, power output and detonation of a single-cylinder engine
- A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine 1
- Correlation of the drag characteristics of a P-51B airplane obtained from high-speed wind-tunnel and flight tests
- Ditching tests with 1/16-size models of the Army B-17 airplane in Langley tank number 2 and on an outdoor catapult
- Knock-limited power outputs from a CFR engine using internal coolants 2: six aliphatic amines
- A relation between knock-limited or preignition-limited air-fuel ratio at lean mixtures and fuel-air ratio at rich mixtures
- Effect of oil flow to piston on piston-ring sticking and oil consumption in a single-cylinder engine
- Analytical investigation of the stability of an F8F dropping model with automatic stabilization
- Comparative drag measurements at transonic speeds of rectangular sweptback NACA 65-009 airfoils mounted on a freely falling body
- A comparison of analytically and experimentally determined isothermal pressure losses in a heat-exchanger installation
- An analysis of life expectancy of airplane wings in normal cruising flight
- An analysis of life expectancy of airplane wings in normal cruising flight
- Analysis and modification of theory for impact of seaplanes on water
- Effect of various carburetor throttle settings on the flow characteristics at the outlet of a supercharger inlet elbow
- Effect of progressive ring failure on piston destruction
- Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics
- An experimental investigation of rectangular exhaust-gas ejectors applicable for engine cooling
- Aerodynamic characteristics of a 1/8-scale powered model of a high-speed bomber with a dual pusher propeller aft of the empennage
- Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds
- Supersonic-tunnel tests of projectiles in Germany and Italy
- Propellers in yaw
- Summary report on the high-speed characteristics of six model wings having NACA 65(sub1)-series sections
- A systematic investigation of pressure distributions at high speeds over five representative NACA low-drag and conventional airfoil sections
- Some Basic Laws of Isotropic Turbulent Flow
- An Experimental Investigation of Several Low-Drag Wing-Nacelle Combinations with Internal Air Flow
- Cooling of Gas Turbines, 2, Effectiveness of Rim Cooling of Blades
- Economy of internally cooling only the overheated cylinders of aircraft engines
- Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a fighter-type airplane
- General theory of airfoil sections having arbitrary shape or pressure distribution
- In-line aircraft-engine bearing loads 2: blade-bearing loads
- An investigation of aircraft heaters XX : measured and predicted performance of a finned-type cast-aluminum crossflow exhaust gas and air heat exchanger