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行波管电子枪阴极组件的热计算
引用本文:姚列明,肖礼,杨中海.行波管电子枪阴极组件的热计算[J].强激光与粒子束,2004,16(10):1317-1320.
作者姓名:姚列明  肖礼  杨中海
作者单位:电子科技大学 物理电子学院,四川 成都 610054
基金项目:国防科技基础研究基金资助课题(AW010310),国防科技重点实验室基金资助课题(NKLC001)
摘    要: 使用ANSYS软件对行波管电子枪阴极组件进行了热分析和结构分析,计算了阴极组件的简化模型的温度和热形变。同时将热分析结果引入行波管设计软件TWTCAD中计算热形变前后电子束的射程、注腰半径、导流系数和面积压缩比的变化,使TWTCAD的计算结果与实验值更为接近。热形变导致电子束各项指标的变化对实际行波管的设计有参考价值。

关 键 词:热形变分析  电子枪  阴极  ANSYS软件  TWTCAD软件
文章编号:1001-4322(2004)10-1317-04
收稿时间:1900-01-01;
修稿时间:2004年3月1日

Thermal-stress analysis of the electron gun
SHI Jian-hua,JIANG Zong-fu,YUAN Sheng-fu,HUA Wei-hong.Thermal-stress analysis of the electron gun[J].High Power Laser and Particle Beams,2004,16(10):1317-1320.
Authors:SHI Jian-hua  JIANG Zong-fu  YUAN Sheng-fu  HUA Wei-hong
Institution:School of Physical Electronics, University of Electronics Science and Technology of China, Chengdu 610054,China
Abstract:The flowfield of hypersonic low temperature(HYLTE)nozzle in continuous wave DF/HF chemical lasers was visualized by laser induced iodine fluorescence(LIIF) and simulated by the CFD software FLUENT. The results from the two methods were compared and basically accord with each other. In the condition given in the article, the oxidant flow was drilled by the fuel. It was compressed first and expanded later.The two streams mixed enough at the plane 10m away from the exit plane. The experimental results show that the direction of the fuel stream changed slightly while the simulative result indicated that the fuel stream flowed almost along the x axis.
Keywords:Hypersonic low temperature(HYLTE) nozzle  Mixing performance  Laser induced iodine fluorescence(LIIF)  Fluorescence intensity  Numerical simulation  Molefraction
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