Characteristics of a Plasma Actuator in Mach 3 Flow
Author:
Affiliation:
1. The University of Texas at Austin
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-788
Reference23 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. 3Menart J., Shang J., Kimmel R., and Hayes J. "Effects of Magnetic Fields on Plasmas Generated in a Mach 5 Wind Tunnel,"AIAA-2003-4165, June2003.
4. 4Menart, J., Handerson, S., Atzbach, C., Shang, J., Kimmel, R., and Hayes, J. "Study of Surface and Volumetric Heating Effects in aMach 5 Flow,"AIAA-2004-2262,June2004.
5. 5Kimmel, R. L., Hayes, J. R., Menart, J. A., and Shang, J. "Effect of Surface Plasma Discharges on Boundary Layers at Mach 5,"42ndAIAAAerospaceSciencesMeetingandExhibit,AIAA-2004-509,January2004.
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