Title:
翼
Document Type and Number:
Japanese Patent JP5060163
Kind Code:
B2
Inventors:
Motofumi Tanaka
Kazuo Hayashi
Yuyuki Yasui
Etsuo Noda
Matsuda Hisashi
Fumio Otomo
Naohiko Shimura
Kazuo Hayashi
Yuyuki Yasui
Etsuo Noda
Matsuda Hisashi
Fumio Otomo
Naohiko Shimura
Application Number:
JP2007120792A
Publication Date:
October 31, 2012
Filing Date:
May 01, 2007
Export Citation:
Assignee:
Toshiba Corporation
International Classes:
H01T23/00; B01J19/08; B64C23/00; F28F13/02; H01T19/00
Domestic Patent References:
| JP2009511360A |
Foreign References:
| US20070089795 | ||||
| US20040195462 |
Other References:
C.L. Enloe, Thomas E. McLaughlin, Robert D. VanDyken, and K.D.Kachner,Mechanism and Responses of a Single Dielectric Barrier Plasma Actuator: Geometric Effects,AIAA Journal,米国,American Institute of Aeronautics and Astronautics,2004年 3月,Vol.42, No.3,Page.595-604
Martiqua L. Post, Thomas C. Corke,Separation Control Using Plasma Actuator: Dynamic Stall Vortex Control on Oscillating Airfoil ,AIAA Journal,米国,American Institute of Aeronautics and Astronautics,2006年12月,Vol.44, No.12,Page. 3125-3135
Martiqua L. Post, Thomas C. Corke,Separation Control Using Plasma Actuator: Dynamic Stall Vortex Control on Oscillating Airfoil ,AIAA Journal,米国,American Institute of Aeronautics and Astronautics,2006年12月,Vol.44, No.12,Page. 3125-3135
Attorney, Agent or Firm:
Patent Business Corporation Sakura International Patent Office
Saichi Suyama
Yukio Kawahara
Satoshi Yamashita
Hideaki Suyama
Saichi Suyama
Yukio Kawahara
Satoshi Yamashita
Hideaki Suyama