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Chinese Journal of High Pressure Physics  > 2004  >  18(2): 116-122 .
BAI Jing-Song, HUA Jing-Song, Shen Qiang, DAI Cheng-Da, LI Ping, TAN Hua, ZHANG Lian-Meng. Numerical Simulation of the Experimental Hypervelocity Launcher[J]. Chinese Journal of High Pressure Physics, 2004, 18(2): 116-122 . doi: 10.11858/gywlxb.2004.02.004
Citation: BAI Jing-Song, HUA Jing-Song, Shen Qiang, DAI Cheng-Da, LI Ping, TAN Hua, ZHANG Lian-Meng. Numerical Simulation of the Experimental Hypervelocity Launcher[J]. Chinese Journal of High Pressure Physics, 2004, 18(2): 116-122 . doi: 10.11858/gywlxb.2004.02.004
shu

Numerical Simulation of the Experimental Hypervelocity Launcher

doi: 10.11858/gywlxb.2004.02.004
  • 1.

    Laboratory for Shock Wave and Detonation Physics Research, Institute of Fluid Physics, CAEP, Mianyang 621900, China;

  • 2.

    State Key Laboratory of Advanced Technology for Materials Synthesis and Processing, Wuhan University of Technology, Wuhan 430070, China

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  • Corresponding author: BAI Jing-Song
  • Received Date: 06 Jan 2004
  • Rev Recd Date: 15 Mar 2004
  • Publish Date: 05 Jun 2004
    Abstract
  • Based on multi-fluid VOF and PPM methods, we develop a MFPPM shock wave physics code to simulate the experiment configuration of the hypervelocity launcher and test the resolution of the algorithms in this code. By using the MFPPM, we simulate some experimental hypervelocity launchers from Sandia National Laboratories, and obtain the numerical results with maximal relative error 1% to 1D, 4.7% to 2D problems compared to that experiments and CTH simulations. Also, a designed model of hypervelocity launcher is simulated too, and some results are given in this paper.

     

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    • References(6)
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