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- Numerical procedures for the calculation of the stresses in monocoques IV : influence coefficients of curved bars for distortions in their own plane
- An analysis of the main spray characteristics of some full-size multi-engined flying boats
- Effect of small deviations from flatness on effective width and buckling of plates in compression
- Comparison of relative sensitivities of the knock limits of two fuels to six engine variables
- Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder
- Comparison of static strengths of machine countersunk riveted joints in 24S-T, X75S-T, and Alclad 75S-T sheet
- 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
- Flight investigation of the cooling characteristics of a two-row radial engine installation 3: engine temperature distribution
- Wake studies of eight model propellers
- An electron microscope study of used nitrated-steel piston rings
- High-speed investigation of skin wrinkles on two NACA airfoils
- 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
- Aerodynamic characteristics including scale effect of several wings and bodies alone and in combination at a Mach number of 1.53
- Altitude cooling investigation of the R-2800-21 engine in the P-47g airplane III : individual-cylinder temperature reduction by means of intake-pipe throttle and by coolant injection
- Altitude cooling investigation of the R-2800-21 engine in the P-47G airplane II : investigation of the engine & airplane variables affecting the cylinder temperature distribution
- Altitude-wind-tunnel investigations of thrust augmentation of a turbojet engine performance with tail-pipe burning
- Investigation of the performance of a 20-inch ram jet using preheated fuel
- Effect of Fuel Composition, Engine Operating Variables, and Spark-Plug Type and Condition on Preignition-Limited Performance of an R-2800 Cylinder
- An investigation of a thermal ice-prevention system for a twin-engine transport airplane
- The NACA high-speed motion-picture camera optical compensation at 40,000 photographs per second
- Determination of induced velocity in front of an inclined propeller by a magnetic-analogy method
- A correlation of loadings and afterbody length-beam ratios of various flying-boat hulls
- Critical combinations of longitudinal and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation
- Correlation of Wright Aeronautical Corporation cooling data on the R-3350-14 intermediate engine and comparison with data from the Langley 16-foot high-speed tunnel
- Critical Mach Numbers of Thin Airfoil Sections with Plain Flaps
- 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
- Analytical investigation of the use of regeneration in compressor-turbine-propeller systems
- Analysis of spark-ignition engine knock as seen in photographs taken at 200,000 frames per second
- Analysis of jet-propulsion-engine combustion-chamber pressure losses
- The effect of wall interference upon the aerodynamic characteristics of an airfoil spanning a closed-throat circular wind tunnel
- The effect of wall interference upon the aerodynamic characteristics of an airfoil spanning a closed-throat circular wind tunnel
- Experimental and theoretical studies of surging in continuous-flow compressors
- Knock-Limited Performance of Triptane and Xylidines Blended with 28-R Aviation Fuel at High Compression Ratios and Maximum-Economy Spark Setting
- Investigation of Three Design Modifications of the NACA Injection Impeller in an R-3350 Engine
- Effect of a low-loss air valve on performance of a 22-inch-diameter pulse-jet engine
- Stability and control force tests of four- and six-unit wing designs of low aspect ratio and 20 degree triangular plan form
- An analysis of the fatigue life of an airplane wing structure under overload conditions
- Aerodynamics of the carburetor air scoop and the engine cowling of a single-engine torpedo-bomber-type airplane
- The Knock-Limited Performance of Fuel Blends Containing Spiropentane, Methylenecyclobutane, Di-Tert-Butyl Ether, Methyl Tert-Butyl Ether, and Triptane
- Knock-limited performance tests of 2, 2, 3, 4-tetramethylpentane, 2, 3, 3, 4-tetramethylpentane, 3, 4, 4-trimethyl-2-pentane, and 2, 3, 4-trimethyl-2-pentane in small-scale and full-scale cylinders
- Tests of a 1/7-Scale Semispan Model of the XB-35 Airplane in the Langley 19-Foot Pressure Tunnel
- The Knock-Limited Performance of Fuel Blends Containing Aromatics 5: N-Propylbenzene, N-Butylbenzene, Isobutylbenzene, M-Xylene, and 1-Isopropyl-4-Methylbenzene
- Some Effects of Compressibility on the Flow Through Fans and Turbines
- An analysis of the skipping characteristics of some full-size flying boats
- Investigation of Operating Characteristics of an Engine Equipped with Modifications to Eliminate Fuel-Evaporation Icing
- Effects of external fuel tanks and bombs on critical speeds of aircraft
- Characteristics of a Hot Jet Discharged from a Jet-Propulsion Engine
- Altitude-wind-tunnel tests of power-plant installation in jet-propelled fighter
- Relation between spark-ignition engine knock, detonation waves, and autoignition as shown by high-speed photography
- Knock-limited performance of pure hydrocarbons blended with a base fuel in a full-scale aircraft-engine cylinder 3: four aromatics, six ethers