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

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16501. NACA research memorandum RM (series). H57C22. Flight-determined induction-system and surge characteristics of TF-102 airplane with 2-spool turbo-jet engine [with list of references]; by Edwin J. Saltzman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 28, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16502. NACA research memorandum RM (series). L57D29a. Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over thin 45° sweptback highly tapered wing in combination with basic and indented bodies [with list of references]; by Thomas L. Fischetti.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 28, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16503. NACA research memorandum RM (series). L57F24. Flutter and divergence of rectangular wings of very low aspect ratio [with one reference]; by Robert W. Fralich, John M. Hedgepeth, and W. J. Tuovila.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 28, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16504. NACA research memorandum RM (series). E57D01. Some Reynolds number phenomena in turbojet compressor [with list of references]; by Harold R. Kaufman.

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

16505. NACA research memorandum RM (series). E57D29. Design and engine evaluation of semistrut corrugated air-cooled turbine blade for operation at tip speed of 1300 feet per second [with list of references]; by Andre J. Meyer, jr., Richard H. Kemp, and William C. Morgan.

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

16506. NACA research memorandum RM (series). L57D09. Investigation of low-speed stability and control characteristics of 1/7-scale model of North American X-15 airplane [with list of references]; by Peter C. Boisseau. Washington.

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

16507. NACA research memorandum RM (series). L57D19. Aerodynamic characteristics of missile configurations with wings of low aspect ratio for various combinations of forebodies, afterbodies, and nose shapes for combined angles of attack and sideslip at Mach number of 2.01 [with list of references]; by Ross B. Robinson.

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

16508. NACA research memorandum RM (series). A57D30. Comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies [with one reference]; by Maurice D. White and Fred J. Drinkwater III.

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

16509. NACA research memorandum RM (series). L57D19c. Heat transfer to bodies at angles of attack [with list of references]; by William V. Feller.

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

16510. NACA research memorandum RM (series). L57D29. Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers 1.0 to 2.3 of rocket-propelled free-flight model with 52.5° sweptback wing of aspect ratio 3 [with list of references]; by Allen B. Henning.

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

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