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

1191. NACA research memorandum RM (series). E53G24. Performance of annular turbojet combustor having reduced pressure losses and using propane fuel [with list of references]; by Carl T. Norgren and J. Howard Childs. Washington, Sept.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: 24, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1192. NACA research memorandum RM (series). A52J06. Correlation of predicted and experimental lateral oscillation characteristics for several airplanes [with list of references]; by Donovan R. Heinle and Walter E. McNeill.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 15, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1193. NACA research memorandum RM (series). L52K03. Flight test of radial-burning solid-fuel ram jet [with list of references]; by Walter A. Bartlett, jr., and H. Rudolph Dettwyler.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 10, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1194. NACA research memorandum RM (series). E52J10. Effects of internal corner fillets on pressure recovery-mass flow characteristics of scoop-type conical supersonic inlets [with list of references]; by Alfred S. Valerino.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 8, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1195. NACA research memorandum RM (series). A52I30. Comparison between prediction and experiment for all-movable wing and body combinations at supersonic speeds, drag due to lift and lift-drag ratio [with list of references]; by Elliott D. Katzen and William C. Pitts.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 5, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1196. NACA research memorandum RM (series). L52J02. Preliminary investigation of rectangular supersonic scoop inlet with swept sides designed for low drag at Mach number of 2.7 [with list of references]; by Raymond J. Comenzo and Ernest A. Mackley.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 26, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1197. NACA research memorandum RM (series). L52J15. Effective downwash characteristics at transonic speeds of 6-percentthick wing with 47° of sweepback in combination with cylindrical body as determined from force measurements of horizontal tail [with list of references]; by Domenic A. Coppolino.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 26, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1198. NACA research memorandum RM (series). L52I19. Evaluation of endand radial-burning solid fuels in ram jets mounted in free Jet at Mach numbers of 2.0, 2.2. and 2.3 [with list of references]; by Walter A. Bartlett, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 25, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1199. NACA research memorandum RM (series). E52H13. Investigation of turbines suitable for use in turbojet engine with high compressor pressure ratio and low compressor-tip speed: 4, Effect of increasing blade speed on velocity diagrams of turbine for engine operation at constant rotative speed [with list of references]; by Elmer H. Davison and Robert E. English.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 24, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1200. NACA research memorandum RM (series). E52G15. Investigation of turbines suitable for use in turbojet engine with high compressor pressure ratio and low compressor-tip speed: 3, Velocity diagram study of 2-stage and downstream-stator turbines for engine operation at constant rotative speed [with list of references]; by Robert E. English and Elmer H. Davison.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 21, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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