2012 Fiscal Year Final Research Report
Development of High Power Plasma Actuator with a Novel Approach of Discharge Formation
| Project/Area Number |
23760771
|
|---|
| Research Category |
Grant-in-Aid for Young Scientists (B)
|
| Allocation Type | Multi-year Fund |
|---|
| Research Field |
Aerospace engineering
|
|---|
| Research Institution | Tottori University |
|---|
Principal Investigator |
MATSUNO Takashi 鳥取大学, 大学院・工学研究科, 講師 (90432608)
|
|---|
| Research Collaborator |
KANAZAKI Masahiro 首都大学東京, システムデザイン研究科, 准教授 (10392838)
|
|---|
| Project Period (FY) |
2011 – 2012
|
| Keywords | 航空宇宙流体力学 / 環境適合技術 / プラズマアクチュエータ |
|---|
| Research Abstract |
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.
|
