Catalog Issue Year Decade: 1960 - 1969 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Catalog Issue Year Decade 1960 - 1969 Sudoc Stem Y 3.N 21/5

171. NACA research memorandum RM (series). A57K05. Subsonic aerodynamic characteristics up to extreme angles of attack of airplane model having unswept wing and high horizontal tail [with list of references]; by Bruce B. Tinling.

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

172. NACA research memorandum RM (series). L57K08. Wind-tunnel investigation of effects of lip geometry on drag and pressure recovery of normal-shock nose inlet on body of revolution at Mach numbers of 1.41 and 1.81 [with list of references]; by A. Warner Robins.

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

173. NACA research memorandum RM (series). L57K14. Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over range of transonic and supersonic speeds [with list of references]; by Abraham Leiss and Walter L. Konyoumjian.

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

174. NACA research memorandum RM (series). L58A06. Heat transfer measured on flat-face cylinder-flare configuration in free flight at Mach numbers from 1.6 to 2.7 [with list of references]; by Dorothy B. Lee and Andrew G. Swanson.

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

175. NACA research memorandum RM (series). A57K07a. Heat transfer on afterbody immersed in separated wake of hemisphere [with list of references]; by Helmer V. Nielsen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 30, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

176. NACA research memorandum RM (series). A57H19. Effects of leading-edge slat and trailing-edge split flap on aerodynamic characteristics of wing-fuselage combination having nearly triangular wing of aspect ratio 2.9 at Mach numbers from 0.60 to 0.92 [with list of references]; by Fred A. Demele.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Jan. 24, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

177. NACA research memorandum RM (series). L57J28. Free-flight roll performance of steady-flow jet-spoiler control on 80° delta-wing missile between Mach numbers 0.6 and 1.8 [with list of references]; by Eugene D. Schult.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 24, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

178. NACA research memorandum RM (series). L57L03. Heat-transfer measurements in free flight at Mach numbers up to 14.6 on flat-faced conical nose with total angle of 29° [with list of references]; by Charles B. Rumsey and Dorothy B. Lee.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 24, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

179. NACA research memorandum RM (series). A57J15. Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22, longitudinal characteristics of triangular wing and canard [with list of references]: by John W. Boyd and Victor L. Peterson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 22, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

180. NACA research memorandum RM (series). H57J30. Simulator Investigation of factors affecting design and utilization of stick pusher for prevention of airplane pitch-up [with list of references]; by Euclid C. Holleman and David L. Boslaugh.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 22, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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