Flow Control of Swept Shock-Wave/Boundary-Layer Interaction Using Plasma Actuators
Author:
Affiliation:
1. Purdue University, West Lafayette, Indiana 47907-2045
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.A34114
Reference38 articles.
1. Interactions between shock waves and turbulent boundary layers
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5. Swept shock/boundary-layer interactions - Tutorial and update
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