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

571. Landing gear. Dynamic and flight tests on rubber-cord and oleo-rubber-disk landing gears for F6C-4 airplane [with references and bibliography]; by William C. Peck.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1930 [published 1931]
SuDoc number:: Y 3.N 21/5:5/366

572. Maneuverability investigation of F6C-3 airplane with special flight instruments [with references and bibliography]; by C. H. Dearborn and H. W. Kirschbaum.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1930 [published 1931]
SuDoc number:: Y 3.N 21/5:5/369

573. Plates (metal). Strength of rectangular flat plates under edge compression; by Louis Schuman and Goldie Back.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1930.]
SuDoc number:: Y 3.N 21/5:5/356

574. Pressure distribution over horizontal and vertical tail surfaces of F6C-4 pursuit airplane in violent maneuvers [with references and bibliography]; by R. V. Rhode.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 2d reprint [1930]
SuDoc number:: Y 3.N 21/5:5/307-2

575. Pressure distribution over symmetrical airfoil section with trailing edge flap [with list of references]; by Eastman N. Jacobs and Robert M. Pinkerton.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1930
SuDoc number:: Y 3.N 21/5:5/360

576. Pressure distribution over thick, tapered and twisted monoplane wing model, N. A. C. A. 81-J [with list of references]; by Carl J. Wenzinger.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1930 [published 1931]
SuDoc number:: Y 3.N 21/5:5/367

577. Pressure distribution over wings and tail surfaces of PW-9 pursuit airplane in flight [with bibliography]; by Richard V. Rhode.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: 1930 [published 1931]
SuDoc number:: Y 3.N 21/5:5/364

578. Pressure distribution. Errata [to] Technical report 346, Water pressure distribution on flying boat hull.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1930.]
SuDoc number:: Y 3.N 21/5:5/346/errata

579. Pressure distribution. Proof of theorem regarding distribution of lift over span for minimum induced drag [with list of references]; by W. F. Durand.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1930.]
SuDoc number:: Y 3.N 21/5:5/349

580. Pressure distribution. Water pressure distribution on flying boat hull [with references and bibliography]; by F. L. Thompson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1930.]
SuDoc number:: Y 3.N 21/5:5/346

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