Theory of the interaction of a shock wave with a boundary layer on a moving surface

Author:

Khokhlov A. P.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference7 articles.

1. V. Ya. Neiland, ?Theory of the separation of a laminar boundary layer in supersonic flow,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4 (1969).

2. K. Stewartson and P. G. Williams, ?Self-induced separation,? Proc. R. Soc. London, Ser. A,312, No. 1509 (1969).

3. P. L. Krapivskii and V. Ya. Neiland, ?Boundary-layer separation from the stationary surface of a body in a supersonic gas flow,? Uch. Zap. Tsentr. Aérogidrodin. Inst.,13, No. 3 (1982).

4. V. I. Zhuk and O. S. Ryzhov, ?Locally inviscid disturbances in a boundary layer with self-induced pressure,? Dokl. Akad. Nauk SSSR,263, No. 1 (1982).

5. Vik. V. Sychev, ?Asymptotic theory of transient separation,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 6 (1979).

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