Direct Numerical Simulation of Shockwave/Turbulent Boundary Layer Interaction
Author:
Affiliation:
1. Princeton University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2145
Reference25 articles.
1. Details of a Shock-Separated Turbulent Boundary Layer at a Compression Corner
2. Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow
3. Investigation of Three-Dimensional Shock/Boundary-Layer Interactions at Swept Compression Corners
4. Upstream influence scaling of 2D and 3D shock/turbulent boundary layer interactions at compression corners
5. Upstream influence scaling of sharp fin-induced shock wave turbulent boundary layer interactions
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