Flow field generated by a dielectric barrier discharge plasma actuator in quiescent air at initiation stage  

作　　者：Xin ZHANG Y.D.CUI Chien Ming Jonathan TAY B.C.KHOO 

机构地区：[1]State Key Laboratory of Aerodynamics,China Aerodynamics Research and Development Center,Mianyang 621000,China [2]National University of Singapore,Singapore 119260,Singapore

出　　处：《Chinese Journal of Aeronautics》2021年第3期13-24,共12页中国航空学报（英文版）

基　　金：financial support of the research project by the National University of Singapore;support by the National Natural Science Foundation of China (No. 11902336);State Key Laboratory of Aerodynamics Foundation of China (Nos. SKLA2019020201 and JBKYC190103);CARDC Fundamental and Frontier Technology Research Fund (No. PJD20180144);China Scholarship Council。

摘　　要：A single Dielectric Barrier Discharge(DBD) plasma actuator driven by Alternating Current(AC) power, capable of inducing a starting vortex and a wall jet in quiescent air, is suited for low-Reynolds-number flow control. However, the starting vortex and the wall jet are usually observed after the plasma actuator has been operated for dozens of and hundreds of cycles of the voltage, respectively. The detail of the induced flow field at the initiation stage of the plasma actuator has rarely been addressed. At the initiation stage, a thin jet that provides the impetus for the entrainment of the induced flow at the beginning of the plasma actuation is first observed by using a high-accuracy phase-lock Schlieren technique and a high-speed Particle Image Velocimetry(PIV) system. This is the initial form of the momentum transfer from the plasma to the fluid.Then, an arched type jet is created by the plasma actuator. In addition, the whole development process of the induced flow field from the starting point of the thin jet to the quasi-steady stage of wall jet is presented for providing a comprehensive understanding of the plasma actuator and proposing a relevant enhancement of the numerical simulation model.

关 键 词：Dielectric barrier discharge Particle image velocimetry Plasma actuator Schlieren technique Wall jet 

分 类 号：V211[航空宇航科学与技术—航空宇航推进理论与工程]