Advances in CFD prediction of shock wave turbulent boundary layer interactions-Reference-Cited by-同舟云学术

Advances in CFD prediction of shock wave turbulent boundary layer interactions

Published:2003-02 Issue:2-3 Volume:39 Page:121-184
ISSN:0376-0421
Container-title:Progress in Aerospace Sciences
language:en
Short-container-title:Progress in Aerospace Sciences

Author:

Knight Doyle,Yan Hong,Panaras Argyris G.,Zheltovodov Alexander

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference228 articles.

1. Knight D, Degrez G. Shock wave boundary layer interactions in high Mach number flows—a critical survey of current CFD prediction capabilities. AGARD AR-319, vol. 2, 1998.

2. The effect of the structure of swept shock wave turbulent boundary layer interactions on turbulence modeling;Panaras;J Fluid Mech,1997

3. Zheltovodov A. Shock waves/turbulent boundary layer interactions—fundamental studies and applications. AIAA Paper 96-1977, 1996.

4. Muylaert J, editor. Technologies for propelled hypersonic flight. EWP NR. 2122, European Space Agency, May 2001.

5. Knight D. Overview of NATO RTO WG 10 SG 3: CFD validation for propelled hypersonic flight. AIAA Paper 2002-0433, January 2002.

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