Effect of asymmetry of the boundary conditions on the boundary layer flow near a cone at an angle of attack-Reference-Cited by-同舟云学术

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Effect of asymmetry of the boundary conditions on the boundary layer flow near a cone at an angle of attack

Published:1989 Issue:1 Volume:24 Page:147-150
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Kornienko E. S.,Shuchinov V. M.

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/BF01051494.pdf

Reference5 articles.

1. A. N. Tikhonov and A. A. Samarskii, Equations of Mathematical Physics [in Russian], Nauka, Moscow (1953).

2. E. S. Kornienko and V. N. Shmanenkov, ?Effect of injection into the boundary layer on supersonic flow over an oscillating cone,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 42 (1983).

3. A. N. Pokrovskii, V. N. Shmanenkov, and V. M. Shuchinov, ?Determination of the param-eters of the boundary layer on rotating axisymmetric cones,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 34 (1984).

4. C. R. Illingworth, ?The laminar boundary layer of a rotating body of revolution,? Philos. Mag.,44, 389 (1953).

5. R. Sedney, ?Laminar boundary layer on a spinning cone at small angles of attack in a supersonic flow,? J. Aeronaut. Sci.,24, 430 (1957).

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