Simulation of the Effects of Force and Heat Produced by a Plasma Actuator on Neutral Flow Evolution-Reference-Cited by-同舟云学术

Simulation of the Effects of Force and Heat Produced by a Plasma Actuator on Neutral Flow Evolution

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Font Gabriel¹,Jung Suk²,Enloe C.¹,McLaughlin Thomas¹,Morgan W.³,Baughn James⁴

Affiliation:

1. U.S. Air Force Academy

2. Korean Agency for Defense Development

3. Kinema Research, L.L.C.

4. University of California, Davis

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-167

Reference23 articles.

1. 1Hultgren, L. S., and Ashpis, D. E. "Demonstration of Separation Delay with Glow-Discharge Plasma Actuators," AIAA Paper 2003-1025.

2. 2List, J., Byerley, A. R., McLaughlin, T. E., and Van Dyken, R. D. "Using a Plasma Actuator to Control Laminar Separation onaLinear CascadeTurbine Blade,"AIAA Paper 2003-1026.

3. 3Roth, J. R., Sherman, D. M., and Wilkinson, S. P. "Boundary Layer Flow Control with a One Atmosphere Uniform Glow Discharge Surface Plasma," AIAA paper98-0328.

4. Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators

5. 5Huang, J., Corke, T. and Thomas, F. "Plasma Actuator for Separation Controlof Low Pressure Turbine Blades," AIAA Paper 2003-1027.

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