Experimental study for momentum transfer in a dielectric barrier discharge plasma actuator

被引:93
作者
Abe, Takashi [1 ]
Takizawa, Yuji [1 ]
Sato, Shunichi [1 ]
Kimura, Nobara [2 ]
机构
[1] Inst Space & Astronaut Sci, Div Space Transportat Engn, Sagamihara, Kanagawa 2298510, Japan
[2] Tokai Univ, Dept Aerodynam & Astronaut, Kanagawa 2591292, Japan
关键词
D O I
10.2514/1.30985
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The momentum-transfer performance of a plasma actuator was investigated experimentally for the effects of ambient-gas pressure, ambient-gas species, and electrode configuration. For measurement of the momentum-transfer performance, the force exerted by the actuator, in addition to the induced velocity, was measured; the consistency between both measurement methods was demonstrated. Results showed that the ambient-gas pressure under which a plasma actuator operates has a considerable effect on the momentum-transfer performance. In fact, the performance does not decrease in a linear manner with decreasing ambient-gas pressure; rather, it initially increases and then decreases. The chemical species of the ambient gas also has a considerable effect on the momentum-transfer performance. The momentum transfer in air is greater than that in nitrogen gas at pressures of less than 1 atm, which suggests a considerable contribution of oxygen molecules in the air. The momentum-transfer performance in carbon dioxide gas is slightly greater than that in nitrogen gas for pressures of less than 1 atm, although they are comparable at 1-atm pressure. Furthermore, the electrode configuration was found to strongly affect the momentum-transfer performance of the plasma actuator. In particular, a mesh-type electrode can improve the performance markedly, compared with the performance of a tape electrode with similar thickness, in an ambient-gas pressure of I atm. However, the performance difference attributable to the electrode configuration is greatly reduced with a decrease in the ambient-gas pressure; for example, it almost disappears at pressures of less than approximately 50 kPa.
引用
收藏
页码:2248 / 2256
页数:9
相关论文
共 43 条
[1]  
Abe T., 2007, 2007187 AIAA
[2]  
[Anonymous], 20050563 AIAA
[3]  
[Anonymous], 2006104 AIAA
[4]  
Baughn J., 2006, 44 AIAA AER SCI M EX
[5]  
BOEUF JP, 2005, J APPL PHYS, V97
[6]  
BOEUF JP, 2006, 20063574 AIAA
[7]  
CORKE T, 2004, 20042127 AIAA
[8]  
CORKE TC, 2006, 20061280 AIAA
[9]   Parameterization of temporal structure in the single-dielectric-barrier aerodynamic plasma actuator [J].
Enloe, C. L. ;
McLaughlin, T. E. ;
Font, G. I. ;
Baughn, J. W. .
AIAA JOURNAL, 2006, 44 (06) :1127-1136
[10]   Mechanisms and responses of a single dielectric barrier plasma actuator: Plasma morphology [J].
Enloe, CL ;
McLaughlin, TE ;
VanDyken, RD ;
Kachner, KD ;
Jumper, EJ ;
Corke, TC .
AIAA JOURNAL, 2004, 42 (03) :589-594