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

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

1181. NACA research memorandum RM (series). E52J22. Characteristics of canard-type missile configuration with underslung scoop inlet at Mach numbers from 1.5 to 2.0 [with list of references]; by Evan A. Fredenburgh and Robert C. Campbell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 30, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1182. NACA research memorandum RM (series). A52K07. Experimental investigation of applicability of hypersonic similarity law to bodies of revolution [with list of references]: by Stanford E. Neice and Thomas J. Wong.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 27, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1183. NACA research memorandum RM (series). L52K20. Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds [with list of references]; by Clarence L. Gillis and Rowe Chapman, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 22, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1184. NACA research memorandum RM (series). L52K24. Wind-tunnel investigation to determine aerodynamic characteristics in steady roll of model at high subsonic speeds [with list of references]; by Richard E. Kuhn and James W. Wiggins.

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

1185. NACA research memorandum RM (series). E52E23. Effect of engine and control limits on steady-state and transient performance of turbojet engine with variable-area exhaust nozzle [with list of references]; by George Vasu and William L. Hinde.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 16, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1186. NACA research memorandum RM (series). A52.T31. Wind-tunnel investigation at subsonic and supersonic speeds of model of tailless fighter airplane employing low-aspect-ratio swept-baek wing-effects of external fuel tanks and rocket packets on drag characteristics [with list of references]; by Willard G. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Jan. 12, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1187. NACA research memorandum RM (series). A52J30. Wind-tunnel investigation at subsonic and supersonic speeds of model of tailless fighter airplane employing low-aspect-ratio swept-back wing-stability and control [with list of references]; by Willard G. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 12, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1188. NACA research memorandum RM (series). E52J14. Effects of fuel temperature and fuel distribution on combustion efficiency of 16-inch ram-jet engine at simulated flight Mach number of 2.9 [with list of references]; by E. E. Dangle, A. J. Cervenka, and D. W. Bahr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 8, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1189. NACA research memorandum RM (series). L52K10. Preliminary investigation of total-pressure-recovery characteristics of 15° semiangle movable-cone variable-geometry ram-jet inlet at free-jet Mach numbers of 1.62, 2.00, 2.53, and 3.05 [with list of references]; by Arthur H. Hinners, jr., and John B. Lee.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 8, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1190. NACA research memorandum RM (series). E53B03. Aerodynamics of slender bodies at Mach number 3.12 and Reynolds numbers from 2×106 to 15×10s: 3, Boundary layer and force measurements on slender cone-cylinder body of revolution [with list of references]; by John R. Jack. Washington, Apr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: 6, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

« Previous
Next »
1
2
…
115
116
117
118
119 Current Page, Page 119
120
121
122
123
…
126
127