Numerical investigation of flow over two sweepback wedges at M = 4 and 6-Reference-Cited by-同舟云学术

Numerical investigation of flow over two sweepback wedges at M = 4 and 6

Published:2013-04 Issue:2 Volume:20 Page:179-193
ISSN:0869-8643
Container-title:Thermophysics and Aeromechanics
language:en
Short-container-title:Thermophys. Aeromech.

Author:

Gounko Yu. P.,Mazhul I. I.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Link

http://link.springer.com/content/pdf/10.1134/S0869864313020054.pdf

Reference11 articles.

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2. D.D. Knight and A.A. Zheltovodov, Ideal-gas shock wave-turbulent boundary-layer interactions (STBLIs) in supersonic flows and their modeling: Two-dimensional interactions, from book [1], P. 137–201.

3. A.A. Zheltovodov and D.D. Knight, Ideal-gas shock wave-turbulent boundary-layer interactions in supersonic flows and their modeling: Three-dimensional interactions, from book [1], P. 202–258.

4. A.V. Lokotko and A.M. Kharitonov, Special features of a supersonic flow in a step wise channel with different inlets, Thermophysics and Aeromechanics, 1999, Vol. 6, No. 3, P. 275–300.

5. A.A. Zheltovodov and A.M. Kharitonov, About analogy of 2D and 3D separation flows, Physical Gas Dynamics (Aerophysics Research), iss. 6, Novosibirsk, ITAM AS USSR, 1976, P. 130–133.

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