Publish Year Decade: 1930 - 1939 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Publish Year Decade 1930 - 1939 Sudoc Stem Y 3.N 21/5

181. Airfoils. Turbulent boundary layer of airfoil [with list of references], by K. Fediaevsky; [translation by S. Reiss from Report 282 of] Central Aero-Hydrodynamical Institute [Moscow, 1936].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1937
SuDoc number:: Y 3.N 21/5:8/822

182. Airplanes. Charts expressing time, velocity, and altitude relations for airplane diving in standard atmosphere [with list of references]; by H. A. Pearson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1937
SuDoc number:: Y 3.N 21/5:6/599

183. Gyroplanes. Hafner A. R. 3 gyroplane. British; [from Flight, Feb. 18, 1937].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1937
SuDoc number:: Y 3.N 21/5:9/205

184. Strength of materials. Photoelastic investigation of 3-dimensional stress and strain conditions [with list of references], by G. Oppel; [translation by J. Vanier from] Forschung auf dem gebiete des ingenieurwesens, v. 7, no. 5. Sept.-Oct. 1936.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1937
SuDoc number:: Y 3.N 21/5:8/824

185. Surface roughness. Experimental investigation of problem of surface roughness [with list of references], by H. Schlichting; [translation by S. Reiss from] Ingenieur-archiv, v. 7, no. 1, Feb. 1936.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1937
SuDoc number:: Y 3.N 21/5:8/823

186. Tail (aircraft). Notes on calculation of minimum horizontal tail surface for airplanes equipped with wing flaps [with list of references]; by Hartley A. Soulé.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1937
SuDoc number:: Y 3.N 21/5:6/597

187. Wings. Wind-tunnel tests of Clark Y wing with Maxwell leading-edge slots [with list of references]; by William E. Gauvain.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1937
SuDoc number:: Y 3.N 21/5:6/598

188. Airplanes. Full-scale wind-tunnel and flight tests of Fairchild 22 airplane equipped with zap flap and zap ailerons [with list of references]; by C. H. Dearborn and H. A. Soulé.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Mar. 1937
SuDoc number:: Y 3.N 21/5:6/596

189. Aluminum alloy. Bending tests of circular cylinders of corrugated aluminum-alloy sheet [with list of references]; by Alfred S. Niles, John C. Buckwalter, and Warren D. Reed.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Mar. 1937
SuDoc number:: Y 3.N 21/5:6/595

190. Landing gears. On actual loads on airplane landing gears, by S. Shiskin; [translation by S. Reiss from Report 269 of] Central Aero-Hydrodynamical Institute [Moscow, 1936].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Mar. 1937
SuDoc number:: Y 3.N 21/5:8/821

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