Investigating Unsteady Dynamics of Cylinder-Induced Shock-Wave/Transitional Boundary-Layer Interactions
Author:
Affiliation:
1. University of Tennessee Space Institute, Tullahoma, Tennessee 37388
Funder
Office of Naval Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J056553
Reference33 articles.
1. KnightD. D.DegrezG. “Shock Wave Boundary Layer Interactions in High Mach Number Flows: A Critical Survey of Current Numerical Prediction Capabilities,” AGARD, Advisory Rept. 319, Vol. 2, 1998, pp. 1.1–1.35.
2. A review of aerothermal problems associated with hypersonic flight
3. Progress in shock wave/boundary layer interactions
4. Shock wave boundary layer interaction
5. Interactions between shock waves and turbulent boundary layers
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