...
首页> 外文期刊>Frontiers in Physics >Simulation of main plasma parameters of a cylindrical asymmetric capacitively coupled plasma micro-thruster using computational fluid dynamics
【24h】

Simulation of main plasma parameters of a cylindrical asymmetric capacitively coupled plasma micro-thruster using computational fluid dynamics

机译:利用计算流体力学模拟圆柱非对称电容耦合等离子体微推力器的主要等离子体参数

获取原文
           

摘要

Computational fluid dynamics (CFD) simulations of a radio-frequency (13.56 MHz) electro-thermal capacitively coupled plasma (CCP) micro-thruster have been performed using the commercial CFD-ACE+ package. Standard operating conditions of a 10 W, 1.5 Torr argon discharge were used to compare with previously obtained experimental results for validation. Results show that the driving force behind plasma production within the thruster is ion-induced secondary electrons ejected from the surface of the discharge tube, accelerated through the sheath to electron temperatures up to 33.5 eV. The secondary electron coefficient was varied to determine the effect on the discharge, with results showing that full breakdown of the discharge did not occur for coefficients coefficients less than or equal to 0.01.
机译:射频(13.56 MHz)电热电容耦合等离子体(CCP)微型推进器的计算流体动力学(CFD)模拟已使用商用CFD-ACE +套件进行了。使用10 W,1.5 Torr氩气放电的标准操作条件与先前获得的实验结果进行比较以进行验证。结果表明,推进器内部产生等离子体的驱动力是从放电管表面喷出的离子感应二次电子,通过鞘层加速至电子温度高达33.5 eV。改变二次电子系数以确定对放电的影响,结果表明,当系数系数小于或等于0.01时,不会发生完全放电。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号