Author: National Aeronautics and Space Administration / Publish Year Decade: 1950 - 1959 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Publish Year Decade 1950 - 1959

821. NACA research memorandum RM (series). L55G28a. Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drug to Mach number 6.9 of tin-stabilized cone-cylinder configuration [with list of references]; by Charles B. Rumsey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 7, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

822. NACA research memorandum RM (series). L65B16. Transonic flutter investigation of fighter-airplane wing model and comparison with systematic plan-form series [with list of references]; by Norman S. Land and Frank T. Abbott, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 7, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

823. NACA research memorandum RM (series). L55G06. Simulator studies of simple homing system [with list of references]; by Anthony L. Passera and H. Douglas Garner.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 6, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

824. NACA research memorandum RM (series). L55H15. Investigation of adaptation of transonic slotted tunnel to supersonic operation by enclosing slots with fairings [with list of references]; by Clarence W. Matthews.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 6, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

825. NACA research memorandum RM (series). E54K26. Inlet-air distortion effects on stall, surge, and acceleration margin of turbojet engine equipped with variable compressor inlet guide vanes [with list of references]; by David P. Harry, III, and Robert J. Lubick.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 4, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

826. NACA research memorandum RM (series). E54L23a. Investigation of performance of turbjoet engine with variable-position compressor inlet guide vanes [with list of references]; by Ray E. Budinger and Harold R. Kaufman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 4, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

827. NACA research memorandum RM (series). E55C25a. Effect of annular inlet baffles on rotating stall, blade vibration, and performance of axial-flow compressor in turbojet engine [with list of references]; by Donald F. Johnson, André J. Meyer, jr., and Morgan P. Hanson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 4, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

828. NACA research memorandum RM (series). A55F15. Drag and rolling-moment effectiveness of trailing-edge spoilers at Mach numbers 2.2 and 5.0 [with list of references]; by Thomas N. Canning and Charles E. DeRose.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 3, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

829. NACA research memorandum RM (series). A55G20. Temperature recovery factors on slender 12° cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45° [with list of references]: by John O. Reller, jr., and Frank M. Hamaker.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 3, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

830. NACA research memorandum RM (series). A55H09. Effects of boundary-layer separation on normal force and center of pressure of cone-cylinder model witii large base flare at Mach numbers from 3.00 to 6.28 [with list of references]; by David H. Dennis and Clarence A. Syvertson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 3, 1955
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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