Mach 3 Shock Wave Unsteadiness Alleviation Using a Negative Corona Discharge
Author:
Affiliation:
1. Ecole Centrale Paris, 92290 Chatenay–Malabry, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34674
Reference21 articles.
1. Flow control using various plasma and aerodynamic approaches (Short review)
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5. Aerodynamic Modification of Supersonic Flow Around Truncated Cone Using a Pulsed Electrical Discharges
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4. DC negative corona discharge in atmospheric pressure helium: transition from the corona to the ‘normal’ glow regime;Plasma Sources Science and Technology;2014-05-19
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