A study of plasma flow field around dielectric barrier discharge plasma actuator for high velocity flow condition

Research Project

Project/Area Number	23860077
Research Category	Grant-in-Aid for Research Activity Start-up
Allocation Type	Single-year Grants
Research Field	Aerospace engineering
Research Institution	Hokkaido University (2012) Japan Aerospace Exploration Agency (2011)
Principal Investigator	TAKAHASHI Yusuke 北海道大学, 大学院・工学研究院, 助教 (40611132)
Project Period (FY)	2011 – 2012
Project Status	Completed (Fiscal Year 2012)
Budget Amount *help	¥2,860,000 (Direct Cost: ¥2,200,000、Indirect Cost: ¥660,000) Fiscal Year 2012: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000) Fiscal Year 2011: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
Keywords	プラズマ流 / 数値解析 / 熱化学的非平衡流 / 熱化学非平衡
Research Abstract	Final goal of the present research is to develop a high-performance plasma actuator which is applicable for a condition of high-velocity flow. In the present study, to describe plasma flow behavior and potential drop by cathode sheath, numerical simulation models of plasma flow generated by dielectric barrier discharge plasma actuator and plasma near an electrode has been suggested and developed.

Report

(3 results)