Control of Amplitude and Position of Reflected Shock Wave by Stripwise Plasma
Author:
Affiliation:
1. University of Notre Dame
2. Air Force Research Laboratory
3. Russian Academy of Sciences (RAS)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0683
Reference26 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
2. Control of mean separation in shock boundary layer interaction using pulsed plasma jets
3. On factors influencing arc filament plasma actuator performance in control of high speed jets
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