Plasma Actuators for Hingeless Aerodynamic Control of an Unmanned Air Vehicle-Reference-Cited by-同舟云学术

Plasma Actuators for Hingeless Aerodynamic Control of an Unmanned Air Vehicle

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:3rd AIAA Flow Control Conference
language:
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Author:

Patel Mehul¹,Ng Terry¹,Vasudevan Srikanth¹,Corke Thomas²,He Chuan²

Affiliation:

1. Orbital Research Inc.

2. University of Notre Dame

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3495

Reference29 articles.

1. Mechanisms and Responses of a Dielectric Barrier Plasma Actuator: Geometric Effects

2. 3Corke, T. and Post, M. "Overview of Plasma Actuators: Concepts, Optimization, and Applications," AIAA Paper No. 2005-0563.

3. 4Wie, D. M. V., Risha, D. J., and Suchomel, C. F. "Research Issues Resulting from an Assessment of Technologies for Future Hypersonic Aerospace Systems," AIAA Paper No. 2004-1357.

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