Delayed-Detached-Eddy Simulation of Shock Wave/Turbulent Boundary Layer Interaction
Author:
Affiliation:
1. University of Miami
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-109
Reference41 articles.
1. GENERAL CIRCULATION EXPERIMENTS WITH THE PRIMITIVE EQUATIONS
2. A dynamic subgrid‐scale eddy viscosity model
3. Subgrid‐scale backscatter in turbulent and transitional flows
4. A numerical study of three-dimensional turbulent channel flow at large Reynolds numbers
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