Laminar/Transitional Fin-induced Shock Wave Boundary-Layer Interactions at Mach 5
Author:
Affiliation:
1. The University of Arizona College of Engineering
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1234
Reference37 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
2. Progress in shock wave/boundary layer interactions
3. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions
4. Experimental Study of Swept Impinging Oblique Shock/Boundary-Layer Interactions
5. Experimental study of the mean structure and quasi-conical scaling of a swept-compression-ramp interaction at Mach 2
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3. Experimental measurements and numerical investigations of boundary-layer instabilities on a Mach 5 hollow cylinder;AIAA SCITECH 2023 Forum;2023-01-19
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