Flow Similarity in Strong Swept-Shock/Turbulent-Boundary-Layer Interactions
Author:
Affiliation:
1. The Ohio State University, Columbus, Ohio 43210
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057534
Reference73 articles.
1. Supersonic Combustion in Air-Breathing Propulsion Systems for Hypersonic Flight
2. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions
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4. Space and time organization in a shock-induced separated boundary layer
5. A simple model for low-frequency unsteadiness in shock-induced separation
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