The flow structure near the windward side of V-shaped wings with an attached shock wave on the leading edges-Reference-Cited by-同舟云学术

The flow structure near the windward side of V-shaped wings with an attached shock wave on the leading edges

Published:1986 Issue:1 Volume:21 Page:104-112
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Zubin M. A.,Ostapenko N. A.

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/BF01051109.pdf

Reference9 articles.

1. V. V. Rusanov, ?Calculation of the interaction of unsteady shock waves with obstruc-tions,? Zh. Vychisl. Mat. Mat. Fiz., 1, 271 (1961).

2. V. I. Lapygin, ?Calculation of supersonic flow past V-shaped wings by the method of stabilization,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 180 (1971).

3. A. L. Gonor, N. A. Ostapenko, and V. I. Lapygin, ?The conical wing in hypersonic flow,? Lect. Notes Phys.,8, 320 (1971).

4. V. I. Lapygin and N. A. Ostapenko, ?Flow of supersonic gas past the windward side of a conical wing,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1, 112 (1973).

5. V. I. Lapygin, ?Solution of the problem of flow past a V-shaped wing with a strong shock on the leading edge,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 114 (1973).

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