Straight and curved type micro dielectric barrier discharge plasma actuators for active flow control

被引:18
|
作者
Aono, Hikaru [1 ]
Yamakawa, Shota [2 ]
Iwamura, Koh [1 ]
Honami, Shinji [1 ]
Ishikawa, Hitoshi [1 ]
机构
[1] Tokyo Univ Sci, Dept Mech Engn, Katsushika Ku, 6-3-1 Niijyuku, Tokyo, Japan
[2] Tokyo Univ Sci, Grad Sch Engn, Katsushika Ku, 6-3-1 Niijyuku, Tokyo, Japan
关键词
Micro dielectric barrier discharge plasma actuator; Induced flow structure; Flow control; Low Reynolds number flow; Particle image velocimetry; LOW-REYNOLDS-NUMBER; TURBINE;
D O I
10.1016/j.expthermflusci.2017.05.005
中图分类号
O414.1 [热力学];
学科分类号
摘要
We develop micro dielectric barrier discharge plasma actuators (DBD-PAs) for active flow control under low external flow conditions. Our micro DBD-PA consists of thin dielectric material and electrodes having a small width and shape variation in the span-wise direction. The fundamental characteristics of the induced flow structures and the effectiveness of the micro DBD-PAs for separated flow over an airfoil are experimentally studied. The flow structures induced by a straight and a curved type micro DBD-PAs in quiescent air are visualized by the tracer method and processed by particle image velocimetry technique. It is found that the curved type DBD-PA produces three-dimensional flow structures as the results of counter flows that impinge each other. For the separation control of the airfoil flow, the angle of attack and free-stream velocities are set to 7.5 degrees and 2 and 3 m/s, respectively. Results present that the separation is successfully suppressed by the use of the curved type micro DBD-PA and the curved type micro DBD-PA shows better capability in comparison with that of the straight type micro DBD-PA due to the induced flow structures. (C) 2017 Elsevier Inc. All rights reserved.
引用
收藏
页码:16 / 23
页数:8
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