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电磁轨道发射器数值模拟与速度测量
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  • 英文篇名:Numerical Simulation and Velocity Measurement of Augmented Electromagnetic Rail Launcher
  • 作者:贺景瑞 ; 李小将 ; 万敏
  • 英文作者:HE Jingrui;LI Xiaojiang;WAN Min;Department of Aerospace Science and Technology, Space Engineering University;
  • 关键词:电磁轨道发射器 ; 数值模拟 ; 速度趋肤效应 ; 发射试验
  • 英文关键词:electromagnetic rail launcher;;numerical simulation;;velocity skin effect;;launching experiments
  • 中文刊名:HPFS
  • 英文刊名:Journal of Gun Launch & Control
  • 机构:航天工程大学宇航科学与技术系;
  • 出版日期:2019-01-30 08:42
  • 出版单位:火炮发射与控制学报
  • 年:2019
  • 期:v.40;No.154
  • 语种:中文;
  • 页:HPFS201902008
  • 页数:7
  • CN:02
  • ISSN:61-1280/TJ
  • 分类号:39-45
摘要
为研究电磁轨道发射器电磁场、温度场特性并且预测发射器性能,建立电磁轨道发射器计算模型,针对矩形电枢普通发射器、C形电枢普通发射器和增强型发射器,采用有限元方法进行求解得到电磁场、温度场和电枢运动过程,并讨论了电枢快速运动产生的速度趋肤效应和发射器结构对磁通密度、电流密度、温度和出口速度的影响。使用增强型电磁轨道发射器进行发射试验,利用高速相机测量电枢出口速度,与数值模拟结果进行对比,验证了计算模型的准确性。
        An electromagnetic launcher mathematical model was established for the purposes of studying the characteristics of electromagnetic field and temperature field of the electromagnetic launcher and predicting the performance of the electromagnetic launcher. The finite element method was used to solve the electromagnetic field, the temperature field and the armature movement process of the rectangular armature electromagnetic launcher, the C-shaped armature electromagnetic launcher and the augmented electromagnetic launcher, with the velocity skin effect caused by fast moving armature and the influence of launcher's structure on magnetic field intensity, current density, temperature and muzzle velocity discussed. The augmented electromagnetic rail launcher was used in the launch experiment. Experimental results were compared with the numerical simulation results, with the accuracy of the calculation model verified.
引文
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