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Interaction of a surface glow discharge with a gas flow

机译:表面辉光放电与气流的相互作用

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A surface glow discharge in a gas flow is of particular interest as a possible tool for controlling the flow past hypersonic aircrafts. Using a hydrodynamic model of glow discharge, two-dimensional calculations for a kilovolt surface discharge in nitrogen at a pressure of 0.5 Torr are carried out in a stationary gas, as well as in a flow with a velocity of 1000 m/s. The discharge structure and plasma parameters are investigated near a charged electrode. It is shown that the electron energy in a cathode layer reaches 250-300 eV. Discharge is sustained by secondary electron emission. The influence of a high-speed gas flow on the discharge is considered. It is shown that the cathode layer configuration is flow-resistant. The distributions of the electric field and electron energy, as well as the ionization rate profile in the cathode layer, do not change qualitatively under the action of the flow. The basic effect of the flow's influence is a sharp decrease in the region of the quasi-neutral plasma surrounding the cathode layer due to fast convective transport of ions.
机译:气流中的表面辉光放电作为控制流过高超音速飞机的流量的一种可能的工具特别令人关注。使用辉光放电的流体动力学模型,在固定气体以及流速为1000 m / s的流动条件下,以0.5 Torr的压力对氮气中的千伏表面放电进行了二维计算。在带电电极附近研究放电结构和等离子体参数。结果表明,阴极层中的电子能量达到250-300 eV。二次电子发射可维持放电。考虑高速气流对放电的影响。示出了阴极层构造是耐流动的。阴极层中的电场和电子能量的分布以及电离速率分布在流动的作用下没有质的变化。流动影响的基本作用是由于离子的快速对流传输,围绕阴极层的准中性等离子体区域急剧减小。

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