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

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16441. NACA research memorandum RM (series). L57G09a. Investigation at transonic speeds of loading over 30° sweptback wing of aspect ratio 3, taper ratio 0.2, and NACA 65A004 airfoil section mounted on body [with list of references]; by Donald D. Arabian.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 26, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16442. NACA research memorandum RM (series). L57G10. Comparison of low-lift drag at Mach numbers from 0.74 to 1.37 of rocket-boosted models having externally braced wings and cantilever wings [with list of references]; by Waldo L. Dickens and Earl C. Hastings, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 25, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16443. NACA research memorandum RM (series). L57G17. Transonic investigation of effects of spanwise and chordwise external store location and body contouring on aerodynamic characteristics of 45° sweptback wing-body configurations [with list of references]; by Albin O. Pearson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 25, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16444. NACA research memorandum RM (series). L57G19. Pressure measurements at transonic and low supersonic speeds on thin conical cambered low-aspect-ratio delta wing in combination with basic and indented bodies [with list of references]; by John P. Mugler, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 25, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16445. NACA research memorandum RM (series). L57G29. Free-flight investigation of drag of model of 60° delta-wing bomber with strut-mounted Siamese nacelles and indented fuselage at Mach numbers from 0.80 to 1.35 [with list of references] by Sherwood Hoffman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 25, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16446. 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.)

16447. 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.)

16448. 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.)

16449. 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.)

16450. 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.)

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