Problem of the interaction of a wedge moving with supersonic velocity when it encounters an interface between two gases

Author:

Tugazakov R. Ya.

Publisher

Springer Science and Business Media LLC

Subject

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

Reference7 articles.

1. S. M. Ter-Minosyants, ?Supersonic flow past the lower surface of a delta wing,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 6, 147 (1966).

2. N. L. Arora, ?An integral-transform method for shock-shock interaction studies,? J. Fluid Mech.,34, 209 (1968).

3. R. Ya. Tugazakov, ?Diffraction of a shock wave by a moving wedge,? Uch. Zap. TsAGI,6, 80 (1975).

4. R. Ya. Tugazakov, ?Numerical solution to the problem of the penetration of a body moving supersonically into a gas of different density,? Uch. Zap. TsAGI,11, 139 (1980).

5. A. I. Golubinskii, ?Interaction between a shock wave and a wedge moving supersonically,? Prikl. Mat. Mekh.,28, 778 (1964).

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