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弯曲电极下的等离子体介质阻挡放电激励器特性研究

娄雨晴 李美 郑贺 周德胜 唐井峰 魏立秋

航空科学技术2026,Vol.37Issue(1):31-37,7.
航空科学技术2026,Vol.37Issue(1):31-37,7.DOI:10.19452/j.issn1007-5453.2026.01.004

弯曲电极下的等离子体介质阻挡放电激励器特性研究

Study on the Characteristics of Plasma Dielectric Barrier Discharge Actuator under Curved Electrode

娄雨晴 1李美 2郑贺 1周德胜 1唐井峰 1魏立秋1

作者信息

  • 1. 哈尔滨工业大学,黑龙江哈尔滨 150001
  • 2. 中国电子科技集团第三十八研究所,安徽 合肥 230088
  • 折叠

摘要

Abstract

As a low-speed flow control method with perturbation,plasma dielectric barrier discharge(DBD)actuator is widely used in the field of flow control.Aiming at the limitations of traditional linear electrode structure in the field of turbulent flow control,this paper designs a curved electrode structure,and focuses on the variation of discharge,optical and flow characteristics of curved electrode and linear electrode under the same experimental conditions.The results show that under the same voltage conditions,compared with the linear electrode structure,the gas temperature,discharge intensity and other parameters of the curved electrode during the discharge process are enhanced to varying degrees,and the curved electrode will make the discharge more uniform.The bending electrode changes are used to increase the gas temperature and enhance the energy distribution of the electric field,resulting in better flow control characteristics during bending time.The research results of this paper will provide technical support for the application of variable geometry electrode plasma actuator in real flow control.

关键词

表面介质阻挡放电/等离子体/主动流动控制/柔性电极/诱导速度

Key words

surface dielectric barrier discharge/plasma/active flow control/flexible electrodes/induction speed

分类

数理科学

引用本文复制引用

娄雨晴,李美,郑贺,周德胜,唐井峰,魏立秋..弯曲电极下的等离子体介质阻挡放电激励器特性研究[J].航空科学技术,2026,37(1):31-37,7.

基金项目

航空科学基金(2022Z039077003) Aeronautical Science Foundation of China(2022Z039077003) (2022Z039077003)

航空科学技术

1007-5453

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