Large Eddy/Reynolds-Averaged Navier-Stokes Simulation of a Mach 5 Compression-Corner Interaction-Reference-Cited by-同舟云学术

Large Eddy/Reynolds-Averaged Navier-Stokes Simulation of a Mach 5 Compression-Corner Interaction

Published:2008-04 Issue:4 Volume:46 Page:977-991
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Edwards Jack R.¹,Choi Jung-Il¹,Boles John A.¹

Affiliation:

1. North Carolina State University, Raleigh, North Carolina 27695

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.32240

Reference40 articles.

1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?

2. Computation of turbulent, separated, unswept compression ramp interactions

3. High-Speed Turbulent Separated Flows: Consistency of Mathematical Models and Flow Physics

4. Gramann, R. A. "Dynamics of Separation and Reattachment in a Mach 5 Unswept Compression Ramp Flow," Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics,Univ. of Texas, Austin, TX,1989.

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