Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing / by Lindsey, W. F.

The influence of vertical-tail design and direction of propeller rotation on trim characteristics of a twin-engine-airplane model with one engine inoperative / by Pitkin, Marvin

Ditching tests with a 1/16-size dynamic model of the Army B-24 airplane in Langley tank no. 2 and on an outdoor catapult / by Fisher, Lloyd J.

High-speed photographs of a YR-4B production rotor blade for simulated flight conditions in the Langley full-scale tunnel / by Dingeldein, Richard C.

An investigation of a thermal ice-prevention system for a C-46 cargo airplane. : 1 - Analysis of the thermal design for wings, empennage, and windshield / by Neel, Carr B.

“…NACA Wartime Reports. Series A.…”
Search for the full-text version of this title in HathiTrust

Shear-lag tests of a box beam with a highly cambered cover in tension / by Peterson, James P.

Search for the full-text version of this title in HathiTrust

The influence of exhaust pressure on knock-limited perfornance / by Cook, Harvey A.

Gasoline-water distribution coefficients of 27 aromatic amines / by Olson, W. T. (Walter T.)

An analysis of the fatigue life of an airplane wing structure under overload conditions / by Putnam, Abbott A.

Correlation of exhaust-valve temperatures with engine operating conditions and valve design / by Zipkin, M. A.

Development of thermal ice-prevention equipment for the B-24D airplane / by Jones, Alun R.

“…NACA Wartime Reports. Series A.…”

Critical Mach numbers of thin airfoil sections with plain flaps / by Heaslet, M. A. (Maxwell Alfred), 1907-

Flight measurements by various methods of the drag characteristics of the XP-51 airplane / by Pearson, Henry A. (Henry Adolph), 1906-

Condensation trails. : Where they occur and what can be done about them / by Rhode, Richard V.

Formulas for use in boundary-layer calculations on low-drag wings / by Jacobs, Eastman N. (Eastman Nixon), 1902-1987

Fatigue strength of flush-riveted joints for aircraft manufactured by various riveting methods / by Maney, George Alfred, 1888-1947

Porpoising. : A comparison of theory with experiment / by Davidson, Kenneth S. M.

The effect of inlet pressure and temperature on the efficiency of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel / by Gabriel, David S.

Efficiency tests of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with air as the driving fluid / by Gabriel, David S.

Effect of water-alcohol injection and maximum-economy spark advance on knock-limited performance and fuel economy of a large air-cooled cylinder / by Vandeman, Jack E.