Calculation of the length of the shock-boundary layer interaction zone-Reference-Cited by-同舟云学术

Calculation of the length of the shock-boundary layer interaction zone

Published:1987 Issue:2 Volume:22 Page:318-321
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Malik T. I.,Tagirov R. K.

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/BF01052272.pdf

Reference12 articles.

1. G. I. Petrov, V. Ya. Likhushin, I. P. Nekrasov, and L. I. Sorkin, ?Effect of viscosity on a supersonic flow with shock waves,? Tr. TsIAM, No. 224, 28 (1952).

2. D. A. Chapman, D. M. Kuehn, and H. K. Larson, ?Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition,? NACA, Rep. No. 1356 (1958).

3. F. W. Spaid and J. C. Frishett, ?Incipient separation of a supersonic turbulent boundary layer, including effects of heat transfer,? AIAA J.,10, 915 (1972).

4. G. S. Settles and S. M. Bogdonoff, ?Scaling of two- and three-dimensional shock/turbulent boundary-layer interactions at compression corners,? AIAA J.,20, 782 (1982).

5. R. K. Tagirov, ?Calculation of the critical pressure rise corresponding to boundary layer separation at a shock,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 38 (1985).

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