张粲宇, 叶红霞, 付海洋, 何鸿飞, 梁子长. 非平行分层等离子体鞘套电波传播的复射线方法[J]. 电波科学学报, 2016, 31(4): 625-631. doi: 10.13443/j.cjors.2015090801
      引用本文: 张粲宇, 叶红霞, 付海洋, 何鸿飞, 梁子长. 非平行分层等离子体鞘套电波传播的复射线方法[J]. 电波科学学报, 2016, 31(4): 625-631. doi: 10.13443/j.cjors.2015090801
      ZHANG Canyu, YE Hongxia, FU Haiyang, HE Hongfei, LIANG Zichang. EM wave propagation in non-parallel plasma sheath using complex ray tracing algorithm[J]. CHINESE JOURNAL OF RADIO SCIENCE, 2016, 31(4): 625-631. doi: 10.13443/j.cjors.2015090801
      Citation: ZHANG Canyu, YE Hongxia, FU Haiyang, HE Hongfei, LIANG Zichang. EM wave propagation in non-parallel plasma sheath using complex ray tracing algorithm[J]. CHINESE JOURNAL OF RADIO SCIENCE, 2016, 31(4): 625-631. doi: 10.13443/j.cjors.2015090801

      非平行分层等离子体鞘套电波传播的复射线方法

      EM wave propagation in non-parallel plasma sheath using complex ray tracing algorithm

      • 摘要: 基于损耗媒质的复Snell定律提出采用复射线方法研究电磁波在非均匀且非平行分层的等离子体媒质中的传播特性.该方法考虑非均匀平面电磁波的复射线(包括等幅度面的传播射线和等相位面的传播射线), 追踪电磁波复射线在每层媒质中的传播路径以及它们透过媒质分界面时的折射射线, 同时根据复射线的传播方向计算电磁波在每层媒质中的传播衰减, 数值累计整个传播过程中的传播衰减即可获得电磁波穿过等离子体鞘套的总衰减.由钝锥体仿真流场数据简化出非平行分层几何模型并采用复射线方法进行计算分析.计算结果表明:飞行器头部至尾部的传播衰减相差巨大且呈现迅速减小趋势, 非平行分层非均匀等离子体媒质存在某特定入射角, 能使传播衰减达到最小值.

         

        Abstract: This paper introduces a complex ray tracing algorithm based on the complex Snell law to investigate the electromagnetic wave propagation in Reentry Plasma Sheath with non-uniform and non-parallel stratification. The algorithm takes the non-uniform electromagnetic complex rays (including propagation ray of equal-amplitude plane and equal-phase plane) into account, traces the path of complex rays in every layer and the refract rays in each interface. The attenuation is calculated along the direction of equal-amplitude plane in each layer and the total attenuation through the entire propagation path can be obtained by accumulate the attenuation in each layer. This paper further analyzes non-parallel stratified plasma sheath model with the complex ray tracing algorithm. Numerical results show that the attenuation sharp decreases from the top of aircraft to the tail. There exists a specific incident angle with minimum attenuation in non-parallel stratification layer.

         

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