Flowfield Measurements in a Mach 2 Fin-Generated Shock/Boundary-Layer Interaction
Author:
Affiliation:
1. Florida State University, Tallahassee, Florida
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056500
Reference31 articles.
1. Flowfield of a 3-D Swept Shock Boundary Layer Interaction in a Mach 2 Flow
2. DeleryJ. M.MarvinJ. G. “Shock-Wave Boundary-Layer Interactions,” AGARD, Paper 280, Neuilly-sur-Seine, France, Feb. 1986.
3. Shock-wave-turbulent-boundary-layer interaction and its control: A survey of recent developments
4. Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions
5. Progress in shock wave/boundary layer interactions
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