Author: National Advisory Committee for Aeronautics / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Author National Advisory Committee for Aeronautics Sudoc Stem Y 3.N 21/5

6401. Wings. Determination of profile drag of airplane wing in flight at high Reynolds numbers [with list of references]; by Joseph Bicknell.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1939
SuDoc number:: Y 3.N 21/5:5/667

6402. Wings. Interference of tail surfaces and wing and fuselage from tests of 17 combinations in N. A. C. A. variable-density tunnel [with list of references]; by Albert Sherman.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1939
SuDoc number:: Y 3.N 21/5:5/678

6403. Wings. Pressure-distribution measurements on tapered wing with full-span split flap in curved flight [with list of references]; by Th. Troller and F. Rokus.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Jan. 1939
SuDoc number:: Y 3.N 21/5:6/683

6404. Wings. Unsteady lift of finite wing [with list of references]; by Robert T. Jones.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Jan. 1939
SuDoc number:: Y 3.N 21/5:6/682

6405. Floats (aircraft). Aerodynamic drag of 5 models of side floats, N. A. C. A. models 51-E, 51-F, 51-G, 51-H, and 51-J [with list of references]; by R. O. House.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1938
SuDoc number:: Y 3.N 21/5:6/680

6406. Floats (aircraft). Hydrodynamic and aerodynamic tests of four models of outboard floats N. A. C. A. models 51-A, 51-B, 51-C, and 51-D [with list of references]; by John R. Dawson and Edwin P. Hartman.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1938
SuDoc number:: Y 3.N 21/5:6/678

6407. Propellers. Noise from propellers with symmetrical sections at zero blade angle, 2 [with list of references]; by A. F. Deming.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1938
SuDoc number:: Y 3.N 21/5:6/679

6408. Wings. Distribution of temperatures over airplane wing with reference to phenomena of ice formation, by Edmond Brun; [translation by J. Vanier from] Publications scientifiques et techniques du Ministere de l'Air, no. 119, 1938.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1938
SuDoc number:: Y 3.N 21/5:8/883

6409. Buckling (aircraft). Effective width of curved sheet after buckling [with list of references]; by W. A. Wenzek [translation by J. Vanier from] Luftfahrt-forschung, v. 15, no. 7, July 6, 1938.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Nov. 1938
SuDoc number:: Y 3.N 21/5:8/880

6410. Engines. Pressure available for ground cooling in front of cowling of aircooled airplane engines [with list of references]; by George W. Stickle and Upshur T. Joyner.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Nov. 1938
SuDoc number:: Y 3.N 21/5:6/673

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