LES of Supersonic Turbulent Boundary Layers with µVG's-Reference-Cited by-同舟云学术

LES of Supersonic Turbulent Boundary Layers with µVG's

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA Applied Aerodynamics Conference
language:
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Author:

Lee S¹,Loth Eric¹,Wang C¹,Kim Sang²

Affiliation:

1. University of Illinois at Urbana-Champaign

2. Taegu University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-3916

Reference11 articles.

1. Optimal Control of Shock Wave Turbulent Boundary Layer Interactions Using Micro-Array Actuation

2. 2Urbin, G., Knight, D., and Zheltovodov, A.A. "Compressible Large-Eddy Simulationusing Unstructured Grid: Supersonic Turbulent Boundary LayerandCompression Corner,"AIAA Paper 99-0427.

3. 3Urbin, G., Knight, D., and Zheltovodov,A.A. "Large-Eddy Simulation of a Supersonic Compression Corner, Part I," AIAA Paper 2000-0398.

4. Large-Eddy Simulation of Supersonic Compression-Ramp Flow by High-Order Method

5. Large Eddy Simulation of Shock/Boundary-Layer Interaction

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