Research on Plasma Synthetic Jet Actuator

被引:0
|
作者
Che, X. K. [1 ]
Nie, W. S. [1 ]
Hou, Z. Y. [1 ]
机构
[1] Acad Equipment Command & Technol, Dept Space Equipment, Beijing 101416, Peoples R China
关键词
dielectric barrier surface discharge; plasma synthetic jet; electrostatic body force; electrostatic shielding; FLOW-CONTROL;
D O I
暂无
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Circular dielectric barrier surface discharge (DBDs) actuator is a new concept of zero mass synthetic jet actuator. The characteristic of discharge and flow control effect of annular-circular plasma synthetic jet actuator has been studied by means of of numerical simulation and experiment. The discharge current density, electron density, electrostatic body force density and flowfield have been obtained. The results show annular-circular actuator can produce normal jet whose velocity will be greater than 2.0m/s. The jet will excite circumfluence. In order to insure the discharge is generated in the exposed electrode annular and produce centripetal and normal electrostatic body force, the width and annular diameter of exposed electrode must be big enough, or an opposite phase drove voltage potential should be applied between the two electrodes.
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页数:6
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