Reynolds Number Effects on Shock-Wave Turbulent Boundary-Layer Interactions
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
2. Princeton University, Princeton, N.J.
3. NASA Ames Research Center, Moffett Field, Calif
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60766
Reference18 articles.
1. Numerical Study of Separated Turbulent Flows
2. Numerical Solution for Supersonic Turbulent Flow over a Compression Ramp
3. Numerical Simulation of Supersonic and Hypersonic Turbulent Compression Corner Flows
4. Computation of Separated Transonic Turbulent Flows
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