航空学报 > 2008, Vol. 29 Issue (2): 304-308

等离子体涡电磁散射特性及隐身性能

常雨,陈伟芳,孙明波,吴其芬   

  1. 国防科学技术大学 航天与材料工程学院
  • 收稿日期:2007-04-27 修回日期:2007-09-17 出版日期:2008-03-15 发布日期:2008-03-15
  • 通讯作者: 常雨

Scattering and Stealth of Plasma Vortex

Chang Yu,Chen Weifang,Sun Mingbo,Wu Qifen   

  1. College of Aerospace and Material Engineering, National University of Defense Technology
  • Received:2007-04-27 Revised:2007-09-17 Online:2008-03-15 Published:2008-03-15
  • Contact: Chang Yu

摘要:

针对非均匀等离子体在飞行器隐身中的应用,采用分段线性电流密度递归卷积时域有限差分(PLJERC-FDTD)方法计算等离子体涡及涡串电磁散射特性,分析等离子体涡对飞行器隐身性能影响。计算表明,等离子体涡在很大频率区间对电磁波吸收效果显著,RCS降低很大,具有明显的隐身效果。等离子体涡表现出一定规律性的极化特性,对L,S和C波段电磁波具有不同的吸收、反射特性。

关键词: 时域有限差分, 电磁波, 等离子体, 涡, 雷达散射截面, 隐身

Abstract:

Aiming at the non-uniform plasma application in aircraft stealth, a piecewise linear current density recursive convolution finitedifferent time-domain (PLJERC-FDTD) algorithm is applied to the study on the scattering for the plasma vortex and plasma vortex cluster. The effects of plasma vortex on the aircraft stealth are analyzed. The results illustrate that the plasma vortex can absorb electromagnetic waves obviously, and the smaller radar cross section (RCS) is obtained comparing with RCS without plasma vortex. The stealth performance of vortex is remarkable.

Key words: FDTD, electromagnetic , wave,  , plasma, vortex, RCS, stealth

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