Method for calculating aerodynamic characteristics of wings of complex planform with subsonic leading and trailing edges-Reference-Cited by-同舟云学术

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Method for calculating aerodynamic characteristics of wings of complex planform with subsonic leading and trailing edges

Published:1972 Issue:2 Volume:4 Page:88-91
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Belotserkovskii S. M.,Kudryavtseva N. A.,Fedotov B. N.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF01014980.pdf

Reference6 articles.

1. E. A. Krasil'shchikova, The Finite-Span Wing in Compressible Flow [in Russian], Gostekhizdat, Moscow-Leningrad, 1952.

2. M. K. Fursov, ?Calculation of the rotary derivative coefficients of wings at supersonic speeds?, Izv. AN SSSR, OTN, Mekhanika i mashinostroenie, no. 2, 1961.

3. M. N. Kogan, ?Some integral properties of supersonic flows?, Tr. TsAGI, no. 687, 1955.

4. H. Riber and F. Malvestuto, ?Stability derivatives of triangular wings at supersonic speeds?, NACA Techn. Repts., no. 908, 1948.

5. S. M. Belotserkovskii, The Thin Lifting Surface in Subsonic Gas Flow [in Russian], Nauka, Moscow, 1965.

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1. Action of a gust on a wing with subsonic leading and trailing edges;Fluid Dynamics;1970-03

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