Author: National Aeronautics and Space Administration / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Sudoc Stem Y 3.N 21/5

531. NACA research memorandum RM (series). E57A30. Preliminary analysis of magnitude of shock losses in transonic compressors [with list of references]; by Francis C. Schwenk, George W. Lewis, and Melvin J. Hartmann.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 29, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

532. NACA research memorandum RM (series). L57A04. Some characteristics of roll controls having possible application to finstabilized ammunition (with list of references]; by Eugene D. Schult.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 27, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

533. NACA research memorandum RM (series). L57A15. Statistical approach to estimation of loads and pressures on seaplane hulls for routine operations [with list of references]; by Roy Steiner.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 27, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

534. NACA research memorandum RM (series). L57A31a. Stability of 2 rocket-propelled models having aspect-ratio, 5 unswept tails on long body for Mach number range of 1.7 to 2.4 [with list of references]; by Reginald R. Lundstrom.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 27, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

535. 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.)

536. 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.)

537. 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.)

538. 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.)

539. 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.)

540. 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.)

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