Author: National Advisory Committee for Aeronautics / Publish Year Decade: 1930 - 1939 - Blacklight Search Results

Start Over Author National Advisory Committee for Aeronautics Publish Year Decade 1930 - 1939

241. Wings. Span load distribution for tapered wings with partial-span flaps [with list of references]; by H. A. Pearson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1937
SuDoc number:: Y 3.N 21/5:5/585

242. Wings. Theoretical span loading and moments of tapered wings produced by aileron deflection [with list of references]; by H. A. Pearson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Jan. 1937
SuDoc number:: Y 3.N 21/5:6/589

243. Wings. Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps [with list of references]; by Carl J. Wenzinger.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1937
SuDoc number:: Y 3.N 21/5:5/611

244. Wings. Wind-tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps [with list of references]; by Robert C. Piatt and Joseph A. Shortal.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1937
SuDoc number:: Y 3.N 21/5:5/603

245. Ailerons. Reduction of aileron operating force by differential linkage [with list of references]; by Robert T. Jones and Albert I. Nerken.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1936
SuDoc number:: Y 3.N 21/5:6/586

246. Engines. Forces and moments on airplane engine mounts [with list of references]; by Philip Donely.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1936
SuDoc number:: Y 3.N 21/5:6/587

247. Fuels. Cetene scale and induction period preceding spontaneous ignition of Diesel fuels in bombs [with list of references], by M. N. Michailova and M. B. Neumann; [translation from] Comptes rendus, Doklady, de l'Academie des Sciences de l'URSS, 1936, v. 2 (11), no. 4 (90).

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1936
SuDoc number:: Y 3.N 21/5:8/813

248. Seaplanes. Short Empire commercial flying boat, British, all-metal cantilever monoplane; [from Flight, Oct. 29, 1936, and the Aeroplane, Oct. 28, 1936].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1936
SuDoc number:: Y 3.N 21/5:9/204

249. Stability. Automatic Stabilization, by Fr. Haus; [translation by J. Vanier from] l'Aéronautique, Mar. 1936.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1936
SuDoc number:: Y 3.N 21/5:8/815

250. Strength of materials. Experimental studies of effective width of buckled sheets [with one reference], by R. Lahde and H. Wagner; [translation by J. Vanier from] Luftfahrtforschung, v. 13, no. 7, July 20, 1936.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1936
SuDoc number:: Y 3.N 21/5:8/814

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