Author: National Aeronautics and Space Administration / Publish Year Decade: 1950 - 1959 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Publish Year Decade 1950 - 1959

931. NACA research memorandum RM (series). L55A05. Investigation of high-performance axial-flow compressor transonic inlet rotor designed for 87.5 pounds per second per square foot of frontal area, aerodynamic design and overall performance [with list of references]; by Melvyn Savage and A. Richard Felix.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 24, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

932. NACA research memorandum RM (series). A54J14. Flight and analog computer study of some stabilization and command networks for automatically controlled interceptor during final attack phase [with list of references]; by Howard L. Turner, William C. Triplett, and John S. White.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 23, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

933. NACA research memorandum RM (series). L54L31a. Experimental study of method of designing sweptback-wing-fuselage juncture for reducing drag at transonic speeds [with list of references]; by Robert R. Howell and Albert L. Braslow

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 23, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

934. NACA research memorandum RM (series). E54K23a. Effect of free-stream Mach number on gross-force and pumping characteristics of several electors [with list of references]; by Leonard E. Stitt and Alfred S. Valerino.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

935. NACA research memorandum RM (series). E54K29a. Experimental investigation of external water-spray cooling in turbojet engine utilizing several injection configurations including orifices in rotor-blade bases [with list of references]; by Roy A. McKinnon and John C. Freche.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

936. NACA research memorandum RM (series). E54L21a. Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight, I, U-shaped channel walls for secondary-air entry [with list of references]; by Eugene V. Zettle and Robert Friedman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

937. NACA research memorandum RM (series). E54L28a. Static sea-level performance of axial-flow compressor turbojet engine with air-cooled turbine [with list of references]; by Reeves P. Cochran and Robert P. Dengler.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

938. NACA research memorandum RM (series). L54L29a. Performance measurements from rocket-powered exploratory research missile flown to Mach number of 10.4 [with one reference]; by Robert O. Piland.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 15, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

939. NACA research memorandum RM (series). L55A13a. Origin and distribution of supersonic store interference from measurement of individual forces on several wing-fuselage-store configurations: 1, Swept-wing heavy-bomber configuration with large store (nacelle), lift and drag, Mach number, 1.61 [with list of references]; by Norman F. Smith and Harry W. Carlson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 11, 1955
SuDoc number:: Y 3.N 21/5:15/L 55 A 13a

940. NACA research memorandum RM (series). L55A14a. Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 [with list of references]; by Charles B. Rumsey, Robert O. Piland, and Russell N. Hopko.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 11, 1955
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

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