三角翼DBD等离子体流动控制研究进展

doi:10.7527/S1000-6893.2019.22201

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三角翼DBD等离子体流动控制研究进展

牛中国¹, 赵光银¹, 梁华¹, 柳平²

1. 空军工程大学航空工程学院等离子体动力学重点实验室, 西安 710038;
2. 重庆交通大学航空学院, 重庆 400074

收稿日期:2018-04-16 修回日期:2018-05-04 出版日期:2019-03-15 发布日期:2019-03-28
通讯作者: 赵光银 E-mail:zym19860615@163.com
基金资助:
国家自然科学基金（11802341）

A review of vortical flow control over delta wings using DBD plasma actuation

NIU Zhongguo¹, ZHAO Guangyin¹, LIANG Hua¹, LIU Ping²

1. Key Laboratory of Plasma Dynamics, Aeronautical Engineering College, Air Force Engineering University, Xi'an 710038, China;
2. School of Aeronautics, Chongqing Jiaotong University, Chongqing 400074, China

Received:2018-04-16 Revised:2018-05-04 Online:2019-03-15 Published:2019-03-28
Supported by:
National Natural Science Foundation of China (11802341)

摘要/Abstract

摘要： 现代战机采用较多的三角翼，在大迎角绕流时存在前缘涡破裂等气动问题。作为新型主动流动控制技术，等离子体激励频带宽、响应快、结构简单、便于闭环控制，在解决三角翼气动问题上具有潜力。回顾了介质阻挡放电（DBD）等离子体气动激励的基本原理，及其用于三角翼前缘涡控制的研究进展。从来流条件、几何构型、激励参数等方面分析了DBD等离子体激励对流动控制效果的影响规律；结合不同激励频率下流场演化特性，分析了流动控制机理。最后，从理论研究和工程应用的角度，对三角翼前缘涡控制的发展进行总结展望。

关键词: 等离子体激励, 介质阻挡放电, 流动控制, 三角翼, 前缘涡

Abstract: Delta wings, being widely used in modern fighters, face aerodynamic problems such as vortex breakdown at large angles of attack. As a new type of active flow control technique, plasma aerodynamic actuation shows significant potential in the control of vortex flows of delta wings because of its fast response, simple structure, wide frequency band and convenience for closed loop control. In this paper, the principles of Dielectric Barrier Discharge (DBD) plasma aerodynamic actuation and its applications in the control of leading-edge vortices over delta wings are reviewed. The effect of DBD plasma actuation on flow control is analyzed in terms of the incoming flow condition, the geometry of experimental model and actuation parameters. Combining with the evolution characteristics of flow field at different actuation frequencies, the mechanism of flow control is analyzed. Finally, the future theoretical research and engineering application of delta wing vortex control are expounded.

Key words: plasma actuation, dielectric barrier discharge, flow control, delta wing, leading-edge vortex

中图分类号:

V211.74⁺5

牛中国, 赵光银, 梁华, 柳平. 三角翼DBD等离子体流动控制研究进展[J]. 航空学报, 2019, 40(3): 22201-022201.

NIU Zhongguo, ZHAO Guangyin, LIANG Hua, LIU Ping. A review of vortical flow control over delta wings using DBD plasma actuation[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(3): 22201-022201.

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三角翼DBD等离子体流动控制研究进展

A review of vortical flow control over delta wings using DBD plasma actuation

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