Plasma Actuation Effect on a MW class Wind Turbine
Author:
Affiliation:
1. Power and Industrial Systems R&D Center, TOSHIBA Corporation
2. Thermal & Hydro Power Systems & Services Division, TOSHIBA Corporation
3. Hokutaku Co.,LTD.
Publisher
Gas Turbine Society of Japan
Subject
Mechanical Engineering
Link
https://www.jstage.jst.go.jp/article/jgpp/9/1/9_47/_pdf
Reference17 articles.
1. Patel,M.P., Vasudevan,S., Nelson,R.C. and Corke,T.C., 2008, “Plasma Aerodynamic Control Effectors for Improved Wind Turbine Performance”, Phase I SBIR Final Report, Grant No. DE-FG02-07ER84781.
2. Post, M.L. and Corke, T.C., 2005, “Flow Control with Single Dielectric Barrier Plasma Actuators”, AIAA 2005-4630.
3. Göksel, B., Greenblatt, D., Rechenberg, I., Nayeri C.N. and Paschereit C.O. , 2006, “Steady and Unsteady Plasma Wall Jets for Separation and Circulation Control”, AIAA 2006-3686.
4. Matsuda,H., Otomo,F., Tanaka,M., Hayashi,K, Noda,S., Mizuno, S., Uchida,T., Aoki,K., Niizeki,Y. and Noda,E., 2008, “Experimental Study on Flow Control using Non-Thermal Plasma (Pulsed Modulation Control Effect on Separation Flow)”, Trans. of JSME, Ser. B, vol.74, No.744 (in Japanese).
5. Mitsuo.K., Watanabe.A., Atobe.T., Kato.H., Tanaka.M. and Uchida.T.,2013, “Lift Enhancement of a Pitching Airfoil in Dynamic Stall by DBD Plasma Actuators”, 51st AIAA Aerospace Sciences Meeting, AIAA 2013-1119, Texas.
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