基于ICP等离子装置的太赫兹波传输特性研究OA
Research on the Transmission Characteristics of Terahertz Waves Based on ICP Plasma Device
高超声速等离子体鞘套中的太赫兹波传输特性是开辟太赫兹通信、测控及导航的关键.为拓展相关研究,本文采用太赫兹时域光谱法(THz-TDS),基于电感耦合等离子体模拟装置,设计并实现了高超声速等离子体流场中的太赫兹波传输特性测量实验,获取并分析了腔体内等离子体介质对太赫兹波透射的影响,同时采用朗缪尔探针与理论仿真结合的方法建立腔体内的三维电子密度分布,在此模型的基础上通过电磁仿真算法得到太赫兹波的理论透射结果,将理论与实测值进行比对验证.结果表明:电感耦合等离子体设备产生的等离子体电子密度在1017 m-3左右时,实验所得结果与理论计算结果拟合度较高,论证了太赫兹时域光谱技术对研究动态、高温、高压的非均匀高超声速等离子体电磁特性具有可行性.
The propagation characteristics of terahertz waves within hypersonic plasma sheaths are pivotal to advancing terahertz communication,measurement and control,and navigation technologies.To extend relevant research,based on an inductively coupled plasma simulation device,this paper uses terahertz time-domain spectroscopy(THz-TDS)method to design and implement experimental measurements of terahertz wave propagation characteristics within hypersonic plasma flow fields.It acquires and analyses the influence of plasma medium within the cavity on terahertz wave transmis-sion.Meanwhile,a combined approach utilizing Langmuir probes and theoretical simulations is employed to establish the three-dimensional electron density distribution within the cavity.Based on this model,electromagnetic simulation algorithms are applied to derive theoretical transmission results of terahertz waves,and theoretical and measured values are compared and verified.The results indi-cate that the experimental findings exhibit a high degree of agreement with theoretical calculations,when the plasma electron density generated by the inductively coupled plasma device reaches approxi-mately 1017 m-3.This demonstrates the feasibility of THz-TDS for investigating the electromagnetic properties of dynamic,high-temperature,and high-pressure non-uniform hypersonic plasmas.
臧俊巍;郭琳静;李江挺;郭立新
西安电子科技大学,西安 710071西安电子科技大学,西安 710071西安电子科技大学,西安 710071西安电子科技大学,西安 710071
军事科技
电感耦合等离子体太赫兹波THz-TDS传输特性传输矩阵
inductively coupled plasmaterahertz waveTHz-TDStransmission characteristicstransmission matrix
《航空兵器》 2026 (1)
93-100,8
国家自然科学基金项目(U20B205962001344)航空科学基金项目(201901081001)中央高校基本科研业务费专项资金(20101236848)
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