介质阻挡放电等离子体流动控制研究进展

聂万胜; 程钰锋; 车学科

doi:10.6052/1000-0992-11-161

介质阻挡放电等离子体流动控制研究进展

doi: 10.6052/1000-0992-11-161

1 装备学院航天装备系, 北京 101416
2 装备学院研究生院, 北京 101416

基金项目: 国家自然科学基金项目(11205244, 51076168) 资助

详细信息

作者简介:
聂万胜, 1969 年生, 装备学院航天装备系教授、博士生导师, 推进理论与工程教研室主任, 航空宇航科学与技术一级学科负责人, 1998 年获国防科技大学工学博士学位, 中国空气动力学会理事, 中国宇航学会液体火箭推进专委会委员, 总装航天运载技术专家组专家, 总装航天运载技术专业组特邀专家, 总装"双百计划" 科技领军人才培养对象. 近期主要研究方向为航空宇航推进与流动控制技术.

通讯作者:
聂万胜

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出版历程
- 收稿日期: 2012-11-23
- 修回日期: 2012-07-10
- 刊出日期: 2012-11-25

A REVIEW ON DIELECTRIC BARRIER DISCHARGE PLASMA FLOW CONTROL

1 Department of Space Equipment, Academy of Equipment, Beijing 101416, China
2 Department of Postgraduate, Academy of Equipment, Beijing 101416, China

Funds: The project was supported by the National Natural Science Foundation of China (11205244, 51076168).

More Information

Corresponding author: NIE Wansheng

摘要

摘要: 介质阻挡放电(DBD) 等离子体流动控制技术适用于低速工况, 具有结构简单、动态响应快等优点, 受到了国内外学术界及工业界的高度重视. 近20 年来, 很多学者对DBD 等离子体流动控制进行了研究, 在机理和应用上都取得了很多有意义的结论. 本文首先分析了介质阻挡放电及其气动激励基本原理; 然后分别对近年来DBD 等离子体流动控制机理和应用研究进展进行了综述, 并总结提出3 个主要气动激励机理; 最后对该领域今后的工作提出了几点建议.
- 介质阻挡放电, 等离子体气动激励, 流动控制
Abstract: Dielectric barrier discharge (DBD) plasma flow control is suited to the low velocity condition. It has a simple structure without mechanical parts, and has thus attracted much attention in research and industry institutions all over the world. DBD plasma flow control has been researched by many scholars in the recent 20 years, and there were a wealth of significant results on both plasma aerodynamic actuation mechanism and applications. In this paper, the physical process of dielectric barrier discharge and the essential mechanism of plasma aerodynamic actuation have been analyzed. Then the DBD plasma flow control, both the aerodynamic actuation mechanism and its applications in recent years, have been reviewed, and the plasma aerodynamic actuation mechanism was generalized in 3 main items. And the paper ends with a discussion about future development of the DBD plasma flow control.
- dielectric barrier discharge, plasma aerodynamic actuation, flow control

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