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

161. Spin (aircraft). Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails: 1, Basic loading condition [with list of references]: by Oscar Seidman and A. I. Neihouse.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:6/608

162. Wings. Empirical corrections to span load distribution at tip [with list of references]; by H. A. Pearson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:6/606

163. Wings. Pressure distribution on wing section with slotted flap in free flight tests [with one reference], by Georg Kiel: [translation by J. Vanier from] Luftfahrtforschung, v. 14, no. 2, Feb. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:8/835

164. Airplanes. Full-scale wind-tunnel and flight tests of Fairchild 22 airplane equipped with external-airfoil flaps [with list of references]; by Warren D. Reed and William C. Clay.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1937
SuDoc number:: Y 3.N 21/5:6/604

165. Cylinders. Stability of orthotopic elliptic cylinders in pure bending [with list of references], by O. S. Heck; [translation by J. Vanier from] Luftfahrtforschung, v. 14, no. 3, Mar. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1937
SuDoc number:: Y 3.N 21/5:8/834

166. Plates (metal). Apparent width of plate in compression [with list of references], by Karl Margnerre; [translation by J. Vanier from] Luftfahrtforschung, v. 14, no. 3, Mar. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1937
SuDoc number:: Y 3.N 21/5:8/833

167. Propellers. Noise from propellers with symmetrical sections at zero blade angle [with list of references]; by A. F. Deming.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1937
SuDoc number:: Y 3.N 21/5:6/605

168. Stresses. Contributions to theory of incomplete tension bay [with list of references], by E. Schapitz; [translation by J. Vanier from] Luftfahrtforschung, v. 14, no. 3, Mar. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1937
SuDoc number:: Y 3.N 21/5:8/831

169. Velocity. Critical velocity of body towed by cable from airplane [with one reference], by C. Koning and T. P. DeHaas; [translation by S. Reiss from Rapport A 367 of] Rijks-Studiedienst voor de Luchtvaart, Amsterdam.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1937
SuDoc number:: Y 3.N 21/5:8/832

170. Airplanes. Baynes Bee light airplane, British, 2-seat high-wing monoplane; [from the Aeroplane, Mar. 17, 1937, and Flight, Mar. 11 and 18, 1937].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: June 1937
SuDoc number:: Y 3.N 21/5:9/207

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