Numerical Investigation of Transitional Shock-Wave/Boundary-Layer Interaction in Supersonic Regime
Author:
Affiliation:
1. University of Rome “La Sapienza,” 00184 Rome, Italy
Funder
Ministero dell'Istruzione, dell'Università e della Ricerca
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056650
Reference64 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
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5. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions
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