RANS Simulations of Flows with Shock Wave-Boundary Layer Interaction
Author:
Affiliation:
1. Technological Institute of Aeronautics (ITA)
2. Aeronautics and Space Institute (IAE)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-985
Reference26 articles.
1. 1Délery, J. “Shock/Shock and Shock-Wave/Boundary-Layer Interactions in Hypersonic Flows,” Report 761, AGARD, 1989, pp.9.1-9.51.
2. Direct numerical simulation of hypersonic turbulent boundary layers. Part 1. Initialization and comparison with experiments
3. Analysis of shock motion in shockwave and turbulent boundary layer interaction using direct numerical simulation data
4. Direct Numerical Simulation of Supersonic Turbulent Boundary Layer over a Compression Ramp
5. Coherent structures in direct numerical simulation of turbulent boundary layers at Mach 3
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