MISSILES AND GUIDANCE TECHNOLOGY

Numerical Simulation on Shock Initiation of Composition Explosive of Cover Board Subjected to Multi-fragment

  • LIANG Bin ,
  • FENG Gaopeng ,
  • WEI Xueting
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  • Institute of Systems of Engineering, China Academy of Engineering Physics, Sichuan Mianyang 621900, China

Received date: 2013-03-19

  Online published: 2025-05-26

Abstract

The numerical simulation results of shock initiation performance of composition B explosive with cover board subjected to tungsten fragments with different number and distribution were presented. In order to study the fragment parameter effect on shock initiation of composition B explosive. Numerical simulation of different number and distribution tungsten fragments which impact on cover board and composition B explosive were conducted with AUTODYN software. The critical detonation velocity of composition B explosive was obtained by the "up-down" method. It is indicated the superposition of shock wave caused by that multi-fragments impact on composition B explosive at the same time or not has an obvious effect on the critical detonation velocity and detonation time. When multi-fragments impact on composition B explosive at the same time, the critical detonation velocity of shock initiation decrease with the fragment number increase. The initiation detonation velocity of composition B explosive impacted by six fragments at the same time is about of 65% comparer to the situation that the explosive is impacted by single fragment. While the explosive is impacted by multi-fragments at the same time, the initiation detonation velocity increases gradually with the distance of horizontal and uptightness orientation increase, and tends to a critical value of one fragment.

Cite this article

LIANG Bin , FENG Gaopeng , WEI Xueting . Numerical Simulation on Shock Initiation of Composition Explosive of Cover Board Subjected to Multi-fragment[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(6) : 62 -66,69 . DOI: 10.15892/j.cnki.djzdxb.2013.06.029

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