Transitional Shock Boundary Layer Interactions on a Compression Ramp at Mach 4
Author:
Affiliation:
1. University of Arizona, Tucson, Arizona 85721
2. Raytheon Missiles and Defense, Tucson, Arizona 85756
Funder
Raytheon Technologies
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059981
Reference50 articles.
1. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions
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5. On the mechanism of unsteady shock oscillation in shock wave/turbulent boundary layer interactions
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