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

191. Propellers. Experimental apparatus for study of propellers [with one reference], by M. Panetti; [translation by S. Reiss from experimental reports by] Aeronautical Laboratory of Royal Engineering Institute of Turin.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Mar. 1937
SuDoc number:: Y 3.N 21/5:8/819

192. Propellers. Some experiments on slipstream effect [with list of references], by C. Ferrari; [translation by S. Reiss from experimental reports by] Aeronautical Laboratory of Royal Engineering Institute of Turin.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Mar. 1937
SuDoc number:: Y 3.N 21/5:8/820

193. Valve-spring surge [with list of references], by Willy Marti; [translation by S. Reiss of thesis submitted in partial fulfillment of requirements for degree of engineer in mechanical engineering aeronautics] Federal Polytechnic Institute [of Zurich, 1935].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Mar. 1937
SuDoc number:: Y 3.N 21/5:8/818

194. Airplanes. Study of factors affecting range of airplanes [with list of references]; by David Biermann.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Feb. 1937
SuDoc number:: Y 3.N 21/5:6/592

195. Hulls (aircraft). Tank tests of 2 models of flying-boat hulls to determine effect of ventilating the step [with list of references]; by John R. Dawson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Feb. 1937
SuDoc number:: Y 3.N 21/5:6/594

196. Pressure drop' in tubing in aircraft instrument installations [with list of references]; by W. A. Wildhack.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Feb. 1937
SuDoc number:: Y 3.N 21/5:6/593

197. Stress distribution in shell bodies and wings as equilibrium problem [with list of references]; by H. Wagner; [translation by J. Vanier from] Luftfahrtforschung, v. 13, no. 9, Sept. 20, 1936.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Feb. 1937
SuDoc number:: Y 3.N 21/5:8/817

198. Wings. Full-scale span load distribution on tapered wing with split flaps of various spans [with list of references]; by John F. Parsons and Abe Silverstein.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Feb. 1937
SuDoc number:: Y 3.N 21/5:6/591

199. Aeronautical symbols. Aeronautic symbols.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1937.]
SuDoc number:: Y 3.N 21/5:2 Sy 6/937

200. Ailerons. Wind-tunnel and flight tests of slot-lip ailerons [with list of references]; by Joseph A. Shortal.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1937
SuDoc number:: Y 3.N 21/5:5/602

« Previous
Next »
1
2
…
16
17
18
19
20 Current Page, Page 20
21
22
23
24
…
59
60