Catalog Issue Year Decade: 1940 - 1949 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Catalog Issue Year Decade 1940 - 1949 Sudoc Stem Y 3.N 21/5

601. Combustors. Effect of combustor-inlet conditions on performance of annular turbojet conibustor; by J. Howard Childs. Richard J. McCafferty and Oakley W. Surine.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1947
SuDoc number:: Y 3.N 21/5:6/1357

602. Condensation shock. Analytical treatment of normal condensation shock, by Heybey; translation [by Edward S. Shafer].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1947
SuDoc number:: Y 3.N 21/5:8/1174

603. Cylinders. Charts for stress analysis of reinforced circular cylinders under lateral loads [with list of references]; by Joseph Kempner and John E. Duberg. Washington, May 1947.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [July 1947]
SuDoc number:: Y 3.N 21/5:6/1310

604. Drag. Drag reduction by suction of boundary layer sepa fitted behind shock wave formation at high Mach numbers [with list of references], by B. Regenscheit; translation [by N. S. Medvedeff].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1947
SuDoc number:: Y 3.N 21/5:8/1168

605. Engines. Effect of exhaust pressure on performance of 12-cylinder liquid-cooled engine [with list of references]; by Leland G. Desmon and Ronald B. Doyle.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1947
SuDoc number:: Y 3.N 21/5:6/1367

606. Flaps (aircraft). Wind-tunnel investigation of split trailing-edge lift and trim flaps on tapered wing with 23° sweepback [with list of references]; by William Letko and David Feigenbaum.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1947
SuDoc number:: Y 3.N 21/5:6/1352

607. Flow. Laboratory report on investigation of flow around 2 turbine-blade profiles using interferometer method [with one reference], by K. von Yietinghoff-Scheel; [translation by Edward S. Shafer].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1947
SuDoc number:: Y 3.N 21/5:8/1171

608. Flow. One-demensional theory of steady compressible fluid flow in ducts with friction and heat addition [with list of references]; by Bruce L. Hicks, Donald J. Montgomery and Robert H. Wasserman.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1947
SuDoc number:: Y 3.N 21/5:6/1336

609. Heat. Tests to determine effect of heat on pressure drop through radiator tubes [with list of references]: by Louis W. Habel and James J. Gallagher.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1947
SuDoc number:: Y 3.N 21/5:6/1362

610. Hulls (aircraft). Investigation of effects of reversed-type longitudinal steps on resistance and spray characteristics of flying-boat hull [with list of references]; by Arthur W. Carter, Eugene P. Clement, and Alvin H. Morewitz.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1947
SuDoc number:: Y 3.N 21/5:6/1356

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