Author: National Aeronautics and Space Administration / Publisher: National Aeronautics and Space Administration - Blacklight Search Results

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16711. NACA research memorandum RM (series). L56F14. Experimental investigation of transonic axial-flow-compressor rotor designed for sonic inlet velocity with inlet hub-tip radius ratio of 0.35 [with list of references]; by Emanuel Boxer and Peter T. Bernot.

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

16712. NACA research memorandum RM (series). L56F20. Wind-tunnel investigation of effect of aspect ratio and chordwise location on effectiveness of plain spoilers on thin untapered wings at transonic speeds [with list of references]; by Alexander D. Hammond.

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

16713. NACA research memorandum RM (series). L56G05. Aerodynamic heat transfer and zero-lift drag of flat windshield canopy on NACA RM-10 research vehicle at high Reynolds numbers for flight Mach number range from 1.5 to 3.0 [with list of references]; by Sherwood Hoffman and Leo T. Chauvin.

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

16714. 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.)

16715. 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.)

16716. 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.)

16717. 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.)

16718. 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.)

16719. 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.)

16720. 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.)

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