Characterization of a Direct-Current Glow Discharge Plasma Actuator in Low-Pressure Supersonic Flow
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/10.2514/1.27197
Reference31 articles.
1. Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology
2. Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a One Atmosphere Uniform Glow Discharge Plasma
3. Effects of Magnetic Fields on Plasmas Generated in a Mach 5 Wind Tunnel
4. Study of Surface and Volumetric Heating Effects in a Mach 5 Flow
5. Effect of Surface Plasma Discharges on Boundary Layers at Mach 5
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