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

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361. NACA research memorandum RM (series). L57G03. Effect of full-span trniling-edge elevons on transonic longitudinal aerodynamic characteristics of wing-body combination having 3-percent-thick triangular wing with 60° leading-edge sweep [with list of references]; by Chris C. Critzos and Willard E. Foss, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 19, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

362. NACA research memorandum RM (series). L57G08a. Wind-tunnel investigation of effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered wings at transonic speeds [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:: Sept. 19, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

363. NACA research memorandum RM (series). L57G10a. Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers [with list of references]; by John A. Moore.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 19, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

364. NACA research memorandum RM (series). L57G22. Wind-tunnel investigation of static lateral and longitudinal stability characteristics of 1/62-scale model of X-1E airplane at combined angles of attack and sideslip at supersonic speeds [with list of references]; by Arthur Henderson, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 19, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

365. NACA research memorandum RM (series). E57D15. Aerodynamic performance of several techniques for spike-position control of blunt-lip nose inlet having internal contraction, Mach numbers of 0.63 and 1.5 to 2.0 [with list of references]; by Arthur A. Anderson and Maynard I. Weinstein.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 17, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

366. NACA research memorandum RM (series). E57F27. Flight investigation of pentaborane fuel in rocket boosted 9.75-inch-diameter ramjet engine with convergent-divergent exhaust nozzle [with list of references]; by John H. Disher.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 17, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

367. NACA research memorandum RM (series). E57G08. Investigation of 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study: 3, Experimental performance with 2 stator configurations designed to eliminate blade wakes and secondaryflow effects and conclusions from entire stator investigation [with list of references]; by Harold E. Rholik, William T. Wintucky, and Thomas P. Moffitt.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 17, 1957
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

368. NACA research memorandum RM (series). L57C19. Investigation at Mach numbers to 1.04 of blade-loading characteristics of 2 full-scale 3-blade superBonic propellers differing in blade-section camber [with list of references]; by Leland B. Salters, jr..

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

369. NACA research memorandum RM (series). L57F27. Temperature measurements from flight test of 2 wing-body combinations at 7° angle of attack for Mach numbers to 4.86 and Reynolds numbers to 19.2x10° [with one reference]; by Leo T. Chauvin.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

370. NACA research memorandum RM (series). L57G16. Effect of ground proximity on aerodynamic characteristics of 2 horizontal-altitude jet vertical-take-off-and-landing airplane models [with list of references]; by William A. Newsom, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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