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

681. NACA research memorandum RM (series). H56F08. Correlation of flight and analog investigations of roll coupling [with list of references]: by Joseph Well and Richard E. Day.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 24, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

682. NACA research memorandum RM (series). L56E04. Comparison of minimum drag of 2 versions of modified delta-wing fighter as obtained from flight tests of rocket-boosted models and equivalent bodies between Mach numbers of 0.80 and 1.64 [with list of references]; by Earl C. Hastings, jr., and Grady L. Mitcham.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 24, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

683. NACA research memorandum RM (series). L56G12. Additional results of investigation at transonic speeds to determine effects of heated propulsive jet on drag characteristics of series of related afterbodies [with list of references]; by Beverly Z. Henry Jr., and Maurice S. Cahn.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 24, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

684. NACA research memorandum RM (series). L56F06. Flight investigation of handling characteristics of fighter airplane controlled through rate type of automatic control system [with list of references]; by Walter R. Russell, S. A. Sjoberg, and William L. Alford.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 14, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

685. NACA research memorandum KM (series). L56F19. Wind-tunnel investigation at low speed of effects of sideslip on static longitudinal trim and static lateral stability characteristics of 3 lighter-type airplnne models [with list of references]; by Byron M. Jaquet and H. S. Fletcher.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 11, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

686. NACA research memorandum RM (series). L56E29. Investigation at high subsonic speeds of static lateral and directional stability and tail-loads characteristics of model having highly tapered swept wing of aspect ratio 3 and 2 horizontal-tail positions [with list of references]; by Albert G. Few, jr..

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington. Sept. 11, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

687. NACA research memorandum RM (series). L56F11a. Aerodynamic heating of wing as determined from free-flight rocket-model test to Mach number 3.64 [with list of references]; by Andrew G. Swanson and Charles B. Rumsey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 11, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

688. NACA research memorandum RM (series). A56F07. Simulator study of some longitudinal stability and control problems of piloted aircraft in flights to extreme altitude and high speed [with list of references]; by Howard F. Matthews and Robert B. Merrick.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 7, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

689. NACA research memorandum RM (series). L56F14a. Flutter investigation at low speed of 40° sweptback wing with pylon-mounted stores, tested as semispan cantilever wing and as full-span wing on towed airplane model [with list of references]; by Albert P. Martina.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 7, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

690. NACA research memorandum RM (series). L56E23. Static lateral and directional stability and effective sidewash characteristics of model of 35° swept-wing airplane at Mach number of 1.61 [with list of references]; by M. Leroy Spearman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 28, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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