Review and Prospect of Missile Plasma Synthetic Jet Control Technology

Xiaobing ZHANG; Jinfeng LI

doi:10.12382/bgxb.2023.0894

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Review and Prospect of Missile Plasma Synthetic Jet Control Technology

更新时间：2025-08-18

- Review and Prospect of Missile Plasma Synthetic Jet Control Technology
- Acta Armamentarii Vol. 45, Issue 10, Pages: 3356-3370(2024)
- 作者机构：
  
  南京理工大学能源与动力工程学院, 江苏南京 210094
- 作者简介：
- 基金信息：
- DOI：10.12382/bgxb.2023.0894
  CLC：
- Received：07 September 2023，
  
  Published Online：30 October 2024，
  
  Published：31 October 2024
- 稿件说明：
移动端阅览
Xiaobing ZHANG, Jinfeng LI. Review and Prospect of Missile Plasma Synthetic Jet Control Technology[J]. Acta Armamentarii, 2024, 45(10): 3356-3370.
DOI：

Xiaobing ZHANG, Jinfeng LI. Review and Prospect of Missile Plasma Synthetic Jet Control Technology[J]. Acta Armamentarii, 2024, 45(10): 3356-3370. DOI： 10.12382/bgxb.2023.0894.

摘要

在反导技术不断发展的背景下

为提高导弹的命中率

需要对导弹的机动性、快响应性等提出更高的要求。近年来

由于响应时间短、无机械部件、工作频带宽等优势

基于等离子体合成射流激励器的主动流动控制技术成为兵器科学与技术以及航空航天领域的研究热点。该技术在导弹的快响应气动力控制、横向主流干扰控制、激波控制、激波/边界层干扰控制等流动控制领域均展现出巨大的应用前景

为减小导弹的阻力、提高导弹的机动性、快响应性等提供了技术保障。结合近二十年来国内外的相关文献资料

以及多年的研究经验

对导弹等离子体合成射流流动控制技术的原理内涵、发展状况、关键问题等进行阐述和总结

以便为相关研究人员提供帮助。

Abstract

In the context of the continuous development of anti-missile technology

higher requirements must be imposed on missile maneuverability and fast response to improve the missile hit rate. In recent years

due to the advantages of short response time

no mechanical parts and wide working frequency band

the active flow control technology based on plasma synthetic jet actuator has become a research hotspot in the weapons science and technology and the aerospace field. Great application prospects have been demonstrated in the flow control fields of missiles

such as fast response aerodynamic control

transverse mainstream interference control

shock wave control

shock wave/boundary layer interference control

etc.

which provides technical support for reducing the missile resistance and improving the maneuverability and fast response of missile. The principle

development and key problems of the missile plasma synthetic jet flow control technology are described and summarized based on the related literatures issued at home and abroad in the past 20 years and the research experience

hoping to provide help to the relevant researchers.

关键词

Keywords

references

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程林 , 孙姝 , 谭慧俊 , 等 . 斜孔式等离子体合成射流激励器静特性的实验 [J ] . 航空动力学报 , 2017 , 32 ( 11 ): 2784 - 2790 .

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吴云 , 李应红 . 等离子体流动控制研究进展与展望 [J ] . 航空学报 , 2015 , 36 ( 2 ): 381 - 405 . DOI: 10.7527/S1000-6893.2014.0246 http://doi.org/10.7527/S1000-6893.2014.0246 等离子体流动控制是基于等离子体气动激励的新型主动流动控制技术,具有响应时间短、激励频带宽等显著技术优势,在改善飞行器/发动机空气动力特性方面具有广阔的应用前景,已成为国际上等离子体动力学与空气动力学交叉领域的前沿研究热点。鉴于此,从介质阻挡放电(DBD)、电弧放电等离子体气动激励特性,等离子体气动激励抑制流动分离、控制附面层、控制激波与激波/附面层干扰、控制压气机与涡轮内部流动、控制管道流动和飞行控制等方面,综合评述了国际上等离子体流动控制的研究进展情况;从创新等离子体气动激励方式,揭示等离子体气动激励与复杂流动的非定常耦合机制,突破等离子体流动控制系统关键技术等方面,对未来的发展进行展望。

WU Y , LI Y H . Progress and outlook of plasma flow control [J ] . Acta Aeronautica et Astronautica Sinica , 2015 , 36 ( 2 ): 381 - 405 . (in Chinese) DOI: 10.7527/S1000-6893.2014.0246 http://doi.org/10.7527/S1000-6893.2014.0246 Plasma flow control is a new type of active flow control technology based on plasma aerodynamic actuation which is advantageous of short reactive time and broad bandwidth. The prospect of plasma flow control on improving aircraft/engine performance has made it a hot topic in the cross field of plasma dynamics and aerodynamics. This paper presents a review of the research progress from the aspects of dielectric barrier discharge (DBD) and arc discharge plasma aerodynamic actuation characteristics, boundary layer control, shock wave control and shock wave/boundary layer interaction control, compressor and turbine flow control, pipe flow and flight control. Also, future development of plasma flow control is looked forward in three aspects, i.e., innovation of plasma aerodynamic actuation, revealing the unsteady coupling mechanism of plasma aerodynamic actuation and complex flow, as well as breakthrough of the key technology of plasma flow control system.

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