A study on turbulence transportation and modification of Spalart–Allmaras model for shock-wave/turbulent boundary layer interaction flow-Reference-Cited by-同舟云学术

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A study on turbulence transportation and modification of Spalart–Allmaras model for shock-wave/turbulent boundary layer interaction flow

Published:2014-04 Issue:2 Volume:27 Page:200-209
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Ma Li,Lu Lipeng,Fang Jian,Wang Qiuhui

Funder

National Natural Science Foundation of China

National Basic Research Program of China

Aeronautical Science Foundation of China

Astronautical Technology Innovation Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference33 articles.

1. Fifty years of shock-wave/boundary-layer interaction research;Dolling;AIAA J,2001

2. Häberle J, Gülhan A. Investigation of the performance of a scramjet inlet at Mach 6 with boundary layer bleed. AIAA-2006-8139; 2006.

3. Häberle J, Gülhan A. Investigation of the flow field of a 2D SCRAM-Jet inlet at Mach 7 with optional boundary layer bleed. AIAA-2007-5068; 2007.

4. Details of a shock separated turbulent boundary layer at a compression corner;Settles;AIAA J,1976

5. Detailed study of attached and separated compression corner flowfields in high Reynolds number supersonic flow;Settles;AIAA J,1979

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