Unsteadiness in Shock Wave Boundary Layer Interactions across Multiple Interaction Configurations
Author:
Affiliation:
1. Imperial College London
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1977
Reference45 articles.
1. 1Dailey, C. L., Supersonic diffuser instability, Ph.D. thesis,California Institute of Technology, 1954.
2. Self-sustained shock oscillations on airfoils at transonic speeds
3. Unsteadiness in shock wave boundary layer interactions with separation
4. Relationship Between Upstream Turbulent Boundary-Layer Velocity Fluctuations and Separation Shock Unsteadiness
5. Effects of upstream boundary layer on the unsteadiness of shock-induced separation
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