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Comparison between calculated and measured loads on wing and horizontal tail in pull-up maneuvers

Comparison of wind-tunnel and flight measurements of stability and control characteristics of a Douglas A-26 airplane

The effect of high loading on landing technique and distance, with experimental data for the B-26 airplane

Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

Wind-Tunnel Investigation of the Stability of the Jettisonable Nose Section of the X-3 Airplane

An Estimation of the Flying Qualities of the Kaiser Fleetwing All-Wing Airplane from Tests of a 1/7-Scale Model, TED No. NACA 2340

An Analytical Investigation of the Heat Losses from a U.S. Navy K-Type Airship

Flight Investigation of the Knock-Limited Performance of a Triptane Blend, a Toluene Blend, and 28-R Fuel in an R-1830-75 Engine

Plane and Three-Dimensional Flow at High Subsonic Speeds

Paths of Target Seeking Missiles in Two Dimensions

Preliminary Tests of a Buffet Stall-Warning Device on a 1/5-Scale Model of the Republic XP-84 Airplane

Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loading, 1, Aeroproducts H20C-162-X11M2 Four-Blade Propeller

Flight investigation at high speeds of profile drag of wing of a P-47D airplane having production surfaces covered with camouflage paint

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

Analysis of cooling limitations and effect of engine-cooling improvements on level-flight cruising performance of four-engine heavy bomber

Measurement of the arithmetic mean velocity of a pulsating flow of high velocity by the hot-wire method

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


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