期刊文献+

氩气微腔放电中特性参数的数值模拟研究 被引量:10

Numerical simulation study on characteristic parameters of microcavity discharge in argon
原文传递
导出
摘要 本文采用二维自洽完全流体模型,针对阳极为通孔的高气压微腔放电结构,研究了微腔放电的参数特性.数值计算得到了氩气压强为100Torr,放电稳态时的电势分布、电子数密度分布和电子温度分布等重要参数.模拟结果表明放电区存在显著的阴极鞘层结构,电子数密度的峰值达到1020m-3,电子温度的量级为几个eV至十几eV,该结论与实验结果相一致.数值模拟合理的解释了微腔放电的基本原理. The two-dimensional numerical model used is based on solutions of fluid equations in the drift-diffusion approximation for the electron and ion transport coupled with Poisson’s equation for electric field to simulate microcavity discharge qualities. The computation results show the potential profile,electron density distribution,ion density distribution,and electron temperature spatial distribution at the argon pressure of 100 Torr. The potential contour shows that the radial component of the electric field becomes very important as the forming of the cathode sheath. The results indicate the peak electron density is 1020m-3,and the electron temperature is on the order of several to tens of eV.
出处 《物理学报》 SCIE EI CAS CSCD 北大核心 2011年第1期397-402,共6页 Acta Physica Sinica
基金 中央高校基本科研业务费专项资金资助(批准号:3014-893309) 国家建设高水平大学公派研究生项目(批准号:[2006]3074,[2008]3039) 中国博士后科学基金(批准号:20100471633) 辽宁省博士科研启动基金(批准号:20101020)资助的课题~~
关键词 微腔放电 等离子体模拟 流体模型 microcavity discharge(MCD) plasma simulation fluid model
  • 相关文献

参考文献18

  • 1Kothnur P S, Yuan X, Raja L L 2003 Appl. Phys. Lett. 82 529.
  • 2Kothnur P S, Raja L L 2005 J. Appl. Phys. 97 043305.
  • 3Kushner M J 2004 J. Appl. Phys. 95 846.
  • 4Miclea M, Kunze K, Heitmann U, Florek S, Franzke J, Niemax K2005 J. Phys. D: Appl. Phys. 38 1709.
  • 5Munoz-Serrano E, Hagelaar G, Callegarl T, Boeuf J P, Pitchford L C 2006 Plasma Phys. Control. Fusion 48 391.
  • 6Deconinck T, Raja L L 2009 Plasma Process. Polym. 6 335.
  • 7姚细林,王新兵,赖建军.微空心阴极放电的Monte Carlo模拟研究[J].物理学报,2003,52(6):1450-1454. 被引量:16
  • 8周俐娜,王新兵.微空心阴极放电的流体模型模拟[J].物理学报,2004,53(10):3440-3446. 被引量:13
  • 9Boeuf J P, Pitchford L C 1995 Phys. Rev. E 51 1376.
  • 10Zhang H Y, Wang D Z, Wang X G 2007 Chin. Phys. 16 1089.

二级参考文献48

  • 1Schoenbach K H, Verhappen R and Tessnw T 1996 Appl. Phys.Lett. 68 13.
  • 2Ahmed EI-Habachl and Schoenbach K H 1998 Appl. Phys. Lett. 7222.
  • 3Stark R H and Schoenbach K H 1998 J. Appl. Phys. 85 2075.
  • 4J J, Yu J H, Huang J J and Wang X B 2001 Acta Phys. Sin.50 1528 (in Chinese).
  • 5Chen Y Z,Chen Q M,Li J,Lai J J and Qiu J L 1998 Acta Phys.Sin. 47 1665(in Chinese).
  • 6Seishim Hashiguchi and Mitugi Hasikuni 1998 J. Appl. Phys. 271010.
  • 7Fujii K, Miyazawa S, Takahashi T and Asami Y 1979 IEEE J.Quant. Electr. QE-I$ 35.
  • 8Bogaerts A, van Straaten M and Gijbels R 1995 Spectrachimica Acta. B50 179.
  • 9Bretagne J,Callede G, Legentil M and Puech V 1986 J.Phys. D:Appl . Phys. 19 761.
  • 10Carman R J 1989 J. Phys. D : Appl . Phys. 22 55.

共引文献31

同被引文献158

  • 1周俐娜,王新兵.微空心阴极放电的流体模型模拟[J].物理学报,2004,53(10):3440-3446. 被引量:13
  • 2曾庆化,刘建业,赖际舟,熊智.环形激光陀螺的最新发展[J].传感器技术,2004,23(11):1-4. 被引量:25
  • 3韩先伟,唐周强,陶文铨,张贵田,张恩昭.自由分子流微电热推力器工作特性和性能研究[J].固体火箭技术,2005,28(2):83-86. 被引量:4
  • 4岳明桥,王天泉.激光陀螺仪的分析及发展方向[J].飞航导弹,2005(12):46-48. 被引量:5
  • 5张连珠,傅凤清,王增波,刘俊红.氮气空心阴极辉光放电等离子体离子的蒙特卡罗模拟研究[J].核聚变与等离子体物理,2006,26(2):135-139. 被引量:8
  • 6Ahmed Z , Gimelshein S F, Ketsdever A. Numerical analysis of free- molecule micro-resistojet performance. Journal of Propulsion and Power,2006 ;22(4) :749 -756.
  • 7Ketsdever A, Green A, Muntz E P, et al. Fabrication and testing of the free molecule micro-resistojet : initial Results. Collection of Tech- nical Papers -- 36rd AIAA/ASME/SAE/ASEE Joint Propulsion Con- ference, 2000:3672.
  • 8Lee R H, Bauer A M, Killingsworth M D, et al. Performance charac- terization of the free molecule micro-resistojet utilizing water propel- lant. Collection of Technical Papers -- 43rd AIAA/ASME/SAE/AS- EE Joint Propulsion Conference, 2007:1748--1758.
  • 9Lee R H, Lilly T C, Muntz E P, et al. Free molecule micro-resisto- jet :nanosatellite propulsion. Collection of Technical Papers -- 41rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2005--4073.
  • 10Yukio H, Hideki Y, Yasushi O, et al. Thermally stress-free grid mounting with hinges for ion thrusters. 44th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference and Exhibit, AIAA 2008--4811.

引证文献10

二级引证文献15

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部