Research Project
Grant-in-Aid for Young Scientists (B)
A high power plasma actuator with a novel approach of discharge formation was developed and evaluated as an aerodynamic control device. Trielectrode (TED) plasma actuator which utilizes sliding discharge was designed and analyzed. The researches show that the thrust generated by the TED actuator is greatly improved from SDBD actuator mode than twice. By applying high DC voltage, the induced flow can be vectored to vertical jet. The superiority of the TED actuator in the aerodynamic control was also confirmed by the wind tunnel test.
All 2012 2011
All Journal Article (5 results) Presentation (12 results)
AIAA paper
Pages: 2012-3238
Proceedings of the 28th ISTS
Volume: No. 2011-e-28
Pages: 2011-3514
Volume: 電子版
Volume: 電子版 Pages: 2011-3514