Effect of energy release in the shock layer on supersonic flight-Reference-Cited by-同舟云学术

Effect of energy release in the shock layer on supersonic flight

Published:1988 Issue:4 Volume:22 Page:645-648
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Arafailov S. I.

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/BF01051435.pdf

Reference7 articles.

1. K. V. Krasnobaev and R. A. Syunyaev, ?Calculation of the flow of stellar wind past an x-ray source,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 106 (1983).

2. K. V. Krasnobaev, ?Supersonic flow past weak radiation sources,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 133 (1984).

3. R. W. McCormack, ?The effect of viscosity in hypervelocity impact cratering,? AIAA Pap., No. 354, 6 (1969).

4. P. D. Thomas, M. Vinokur, R. A. Bastianon, and R. J. Conti, ?Numerical solution for three-dimensional inviscid supersonic flow,? AIAA J.,10, 887 (1972).

5. A. P. Lyubimov and V. V. Rusanov, Gas Flow Past Blunt Bodies, Part 2 [in Russian], Nauka, Moscow (1970).

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