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

161. NACA research memorandum RM (series). H58D21. Operational problems of manned orbital vehicles; by Hubert M. Drake, Donald R. Bellman, and Joseph A. Walker.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 21, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

162. NACA research memorandum RM (series). L58C27. Investigation of aerodynamic characteristics of model of supersonic bomber configuration with swept and unswept wing at Mach numbers from 1.79 to 2.67; by H. Norman Silvers and Raymond L. Zedekar.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 21, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

163. NACA research memorandum RM (series). L58E06. Effects of wing sweep, horizontal-tail configuration, and ventral fin on static stability characteristics of model with wing of aspect ratio 3 at Mach nos. from 2.29 to 4.65 [with list of references]; by Byron M. Jaquet and Roger H. Fournier.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, July 21, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

164. NACA research memorandum RM (series). L58E12. Wind-tunnel investigation of wing loads due to deflected Inboard ailerons on 45° sweptback wing at transonic speeds [with list of references]; by Atwood R. Heath, jr., and Ann W. Igoe.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 21, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

165. NACA research memorandum RM (series). H58D22. Simulator investigation of command reaction controls; by Euclid C. Holleman and Wendell H. Stlllwell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 17, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

166. NACA research memorandum RM (series). L58C14a. Heat transfer and pressure measurement on 5-inch hemispherical concave nose at Mach number of 2.0 [with list of references]; by J. Thomas Markley.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 17, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

167. NACA research memorandum RM (series). L58E08a. Simulation study of high-performance aircraft including effect on pilot control of large accelerations during exist and reentry flight [with list of references]; by C. H. Woodling [and others].

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington. July 17, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

168. NACA research memorandum RM (series). A58C24. Investigation of performance and internal flow of variable-area, variable-internal-contraction inlet at Mach nos. 2.00, 2.50, and 2.92 [with list of references]; by Richard Scherrer and Warren E. Anderson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 15, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

169. NACA research memorandum RM (series). E58C19. Effect of screens in reducing distortion and diffusion length for dump diffuser at Mach number of 3.85 [with list of references]; by Joseph F. Wasserbauer.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 15, 1958
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

170. NACA research memorandum RM (series). H58D29. Effect of leading-edge-flap deflection on wing loads, load distributions, and flap hinge moments of Douglas X-3 research airplane at transonic speeds [with list of references]; by Earl R. Keener, Norman J. McLeod, and Norman V. Taillon.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 15, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

« Previous
Next »
1
2
…
13
14
15
16
17 Current Page, Page 17
18
19
20
21
…
126
127