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

651. NACA research memorandum RM (series). L56H13. Static stability characteristics of cambered-delta-wing model at high subsonic speeds [with list of references]; by William C. Moseley, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 31, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

652. NACA research memorandum RM (series). L56H21. Effect of increase in angle of dead rise on hydrodynamic qualities of seaplane configuration incorporating high wing loading [with list of references]; by Walter J. Kapryan and Irving Woinstoin.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 31, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

653. NACA research memorandum RM (series). L56H22a. Wind-tunnel investigation of 2 vertical-take-off-and-landing jet bomber airplane configurations at Mach numbers of 1.94 and 2.40 [with list of references]; by Robert A. Jones and Kobert W. Kainey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 31, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

654. NACA research memorandum RM (series). L56H24. Combined effects of wing taper ratio and low horizontal-tail position on longitudinal stability of 45° sweptback wing-body combination at transonic speeds [with list of references]; by Stanley H. Spooner.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 31, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

655. NACA research memorandum RM (series). E56D20. Analysis of ram-jet engine performance including effects of component changes [with list of references]; by Richard J. Weber and Roger W. Luidens.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 29, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

656. NACA research memorandum RM (series). E56H08. Experimental investigation of overriding control to effect recovery from surge and stall in turbojet engine [with list of references]; by Paul M. Stiglic and Herbert Heppler.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 29, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

657. NACA research memorandum RM (series). E56H14a. Investigation of turbines suitable for use in turbojet engine with high compressor pressure ratio and low compressor-tip speed: 7, Experimental performance of modified 2-stage turbine [with list of references]; by Elmer H. Davison, Donald A. Petrash, and Harold J. Schum.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 29, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

658. NACA research memorandum RM (series). L56H31. Low-speed investigation of high-lift lateral-control device consisting of spoiler-slot-deflector and trailing-edge flap on tapered 45° sweptback wing [with list of references]; by Alexander D. Hammond and Jarrett K. Huffman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 26, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

659. NACA research memorandum RM (series). L56H07. Experimental study of zero-angle-of attack transonic drag associated with vertical position of horizontal tail at zero incidence [with list of references]; by Robert R. Howell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 25, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

660. NACA research memorandum RM (series). E56G13a. Development of flow distortions in full-scale nacelle inlet at Mach numbers 0.63 and 1.6 to 2.0 [with list of references]: by Thomas G. Plercy and Bruce G. Chiccine.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 22, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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