Control of a Shock/Boundary-Layer Interaction by Using a Pulsed-Plasma Jet Actuator
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051246
Reference18 articles.
1. Shock-wave-turbulent-boundary-layer interaction and its control: A survey of recent developments
2. Effects of plasma aerodynamic actuation on oblique shock wave in a cold supersonic flow
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