Publish Year Decade: 1950 - 1959 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Publish Year Decade 1950 - 1959 Sudoc Stem Y 3.N 21/5

941. Technical notes. 3230. Errata [Investigation of distributed surface roughness on body of revolution at Mach number of 1.61]. by K. R. Czarnecki, Ross B. Robinson, and John H. Hilton, Jr., June 1954.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [Mar. 22, 1957.]
SuDoc number:: Y 3.N 21/5:6/(nos.)

942. NACA research memorandum RM (series). E57A21. Investigation of high-performance top inlet to Mach number of 2.0 and at angles of attack of 20° [with list of references]; by Donald J. Vargo, Philip N. Larks, and Owen H. Davis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 20, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

943. NACA research memorandum RM (series). L56D11. Some examples of applications of transonic and supersonic area rules to prediction of wave drag [with list of references]; by Robert L. Nelson and Clement J. Welsh.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 20, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

944. NACA research memorandum RM (series). A56K26. Investigation of symmetrical body indentations designed to reduce transonic zero-lift wave drag of 45° swept wing with NACA 64A006 section and with thickened leading-edge section [with list of references]; by George H. Holdaway and Elaine W. Hatfield.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 19, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

945. NACA research memorandum RM (series). L57A25. Supersonic aerodynamic characteristics of low-drag aircraft configuration having arrow wing of aspect ratio 1.86 and body of fineness ratio 20 [with list of references]: by Warren Gillespie, jr..

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 19, 1957
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

946. NACA research memorandum RM (series). L57B04. Experimental static aerodynamic forces and moments at high subsonic speeds on missile model during simulated launching from unswept-, sweptback and modified-delta-wing-fuselage combinations at zero sideslip [with list of references]; by William J. Alford, jr., and Thomas J. King, jr..

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 19, 1957
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

947. NACA research memorandum RM (series). E56K29. Investigation of mass-flow and pressure-recovery characteristics of several underslung scoop-type inlets at free-stream Mach numbers of 2.0, 1.8, 1.5, and 0.66 [with list of references]; by Alfred S. Valerino and Robert F. Zappa.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 13, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

948. NACA research memorandum RM (series). H57A02. Static-pressure error calibrations for nose-boom airspeed installations of 17 airplanes [with list of references]; by Terry J. Larson, Wendell H. Stillwell, and Katharine H. Armistead.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 13, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

949. NACA research memorandum RM (series). A56K19. Influence of imperfect radar space stabilization on final attack phase of automatic interceptor system [with list of references]; by William C. Triplett, John D. McLean, and John S. White.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 11, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

950. NACA research memorandum RM (series). H57A16. Flight-determined static lateral stability and control characteristics of swept-wing fighter airplane to Mach number of 1.39 [with list of references]; by Gene L. Matranga and James R. Peele.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 11, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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