Notice on the organization of advanced research class on high-pressure science and new materials of engineering knowledge of professional and technical personnel Notice on the organization of advanced research class on high-pressure science and new materials of engineering knowledge of professional and technical personnel
Volume 37 Issue 6
Dec 2023
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Chinese Journal of High Pressure Physics  > 2023  >  37(6): 063401.
ZHAO Kanglin, WANG Qiming, ZHANG Youjun, JIANG Gang, PENG Fang, LI Yanchun. Physico-Mechanical Behavior and Size Effect of Nano-Tungsten under High Pressure[J]. Chinese Journal of High Pressure Physics, 2024, 38(3): 030103. doi: 10.11858/gywlxb.20230756
Citation: WU Xiao, ZHANG Le, MA Xiaojuan, ZHANG Mingjian, LIU Fusheng. Finite Element Simulation for Magnet Velocity Induction System[J]. Chinese Journal of High Pressure Physics, 2023, 37(6): 063401. doi: 10.11858/gywlxb.20230693
shu

Finite Element Simulation for Magnet Velocity Induction System

doi: 10.11858/gywlxb.20230693

  • School of Physical Science and Technology, Southwest Jiaotong University, Chengdu 610031, Sichuan, China

  • Received Date: 12 Jul 2023
  • Rev Recd Date: 29 Aug 2023
    • Available Online: 06 Dec 2023
  • Issue Publish Date: 15 Dec 2023
    Abstract
  • In shockwave experiments, the launch velocity of flyer is a crucial parameter for determining the physical quantities in sample under dynamic compression. Magnet velocity induction system is used to determine the velocity of flyer which can work under hypervelocity conditions. Based on finite element method, ANSYS Electromagnetics Suite module was used to establish a three-dimensional model and the launch process of flyer was simulated. The simulated results well reproduce the experimental signals. Comparing to the experimental results, the relative error of simulated amplitude of induced electromotive force (AIEMF) is 1.1%, lower than the system error of 2.0%. The relative error for flyer velocity determined by simulation is less than 0.4%, also lower than the measurement system error of 0.9%. The dependence of AIEMF with the thickness, radius, tilt angle, launch velocity of flyer and the diameter of pick-up coils is analyzed. The simulation result provides a reference for better signal acquisition in shockwave experiments.

     

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