Effect of Impulsive Plasma Discharge in Hypersonic Boundary Layer over Flat Plate
Author:
Affiliation:
1. University of Tokyo
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3736
Reference16 articles.
1. Mechanisms of plasma actuators for hypersonic flow control
2. Flow control using various plasma and aerodynamic approaches (Short review)
3. Hypersonic Flow over a Blunt Body with Plasma Injection
4. Computational Study of Shock Mitigation and Drag Reduction by Pulsed Energy Lines
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