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

761. NACA research memorandum RM (series). E55H04a. Analysis of air-turborocket engine performance including effects of component changes [with list of references]; by Roger W. Luidens and Richard J. Weber.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 6, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

762. NACA research memorandum RM (series). L55L13. Investigation of jet effects on flat surface downstream of exit of simulated turbojet nacelle at free-stream Mach number of 1.39 [with list of references]; by Walter E. Bressette and Abraham Leiss.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 2, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

763. NACA research memorandum RM (series). (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]. E55L09. Experimental investigation of 0.4 hub tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers: 3, Effect of tip taper on over-all and blade-element performances [with list of references]: by John C. Montgomery and Frederick Glaser.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 30, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

764. NACA research memorandum RM (series). E05J11. Altitude performance evaluation of J71-A-11 turbojet engine [with one reference]; by James W. Useller and George E. Pappas.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 30, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

765. NACA research memorandum RM (series). A56A06. Preliminary investigation of static stability characteristics of 4 airplane-like configurations at Mach numbers from 3.00 to 6.28 [with list of references]; by Thomas J. Wong and Hermilo R. Gloria.

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

766. NACA research memorandum RM (series). L55L22. Experimental transonic flutter characteristics of untapered, 45° sweptback, aspect-ratio-4 wing [with list of references]; by Charles L. Ruhlin.

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

767. NACA research memorandum RM (series). E55E18. Temperature drops through liquid-cooled turbine blades with various cooling-passage geometries [with list of references]; by Edward R. Bartoo.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 23, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

768. NACA research memorandum RM (series). E55L09a. Effect of reduction in stator solidity on performance of transonic turbine [with list of references]; by James W. Miser, Warner L. Stewart, and Robert Y. Wong.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 23, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

769. NACA research memorandum RM (series). E55L13a. Dynamics of supersonic inlet with adjustable bypass in combination with J34 turbojet engine [with list of references]; by Fred Wilcox and Paul Whalen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 23, 1956
SuDoc number:: Y 3.N 21/5:15/E 55 L 13a

770. NACA research memorandum RM (series). L55H30. Transonic investigation of aerodynamic characteristics of swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches [with list or references]; by Charles F. Whitcomb and Harry T. Norton, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 19, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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