Effective Layout of Plasma Actuators for a Flow Separation Control on a Wing
Author:
Affiliation:
1. University of Tokyo
2. Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-474
Reference21 articles.
1. 1Van Ness II, D. K., Corke, T. C., and Morrisz, S. C. “Turbine Tip Clearance Flow Control using Plasma Actuators,” AIAA Paper 2006-21.
2. 2Corke, T. C., Mertz, B., and Patel, M. P. “Plasma Flow Control Optimazed Airfoil,” AIAA Paper 2006-1208.
3. 3Visbal, M. R. and Gaitonde, D. V. “Control of Vortical Flows Using Simulated Plasma Actuators,” AIAA Paper 2006-505.
4. 4Visbal, M. R., Gaitonde, D. V., and Roy, S. “A Coupled Approach for Plasma-Based Flow Control Simulations of Wing Section,” AIAA Paper 2006-1205.
5. 5Corke, T. C. and Post, M. L. “Overview of Plasma Flow Control: Concepts, Optimization, and Applications,” AIAA Paper 2005-563.
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