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Academic article

Simulation Study on Penetration Performance of Linear Shaped Charge under Asymmetric Detonation

  • SHI Chenyi , 1 ,
  • XU Yongjie , 1, 2, * ,
  • ZHENG Nana 3 ,
  • ZHAO Xiongfei 4 ,
  • ZHANG Na 5
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  • 1 School of Mechatronic Engineering,North University of China,Taiyuan 030051,Shanxi,China
  • 2 Chongqing Hongyu Precision Industrial Co.,Ltd.,Chongqing 402760,China
  • 3 Changzhi Military Representative Office of Beijing Military Representative Bureau,Changzhi 046000,Shanxi China
  • 4 Chongqing Jialing Special Equipment Co.,Ltd.,Chongqing 400000,China
  • 5 Huaihai Industries Group Co.,Ltd.,Changzhi 046000,Shanxi China

Received date: 2025-03-26

  Online published: 2026-01-24

Abstract

In order to study the influence of detonation asymmetry on the penetration performance of linear shaped charges,the finite element software LS-DYNA was used and orthogonal design experiments were adopted.Three factors,namely detonation offset,liner thickness and charge height,were selected to simulate the process of linear shaped charge penetrating 45 steel target plates.The depth of penetrating the 45 steel target plate was taken as the evaluation basis.Through the analysis of the damage effect,the influence weights of three factors on the damage assessment criteria were obtained.Through the simulation analysis of the penetration process of linear shaped charge of different cross-sectional liner penetration into 45 steel target plates at the same level under different detonation offsets,the penetration performance and anti-eccentricity ability of arc top conical linear shaped charge,truncated top conical linear shaped charge and hemispherical linear shaped charge under the action of asymmetric detonation waves were further obtained.The research results can provide certain references for linear shaped charge in engineering applications.

Cite this article

SHI Chenyi , XU Yongjie , ZHENG Nana , ZHAO Xiongfei , ZHANG Na . Simulation Study on Penetration Performance of Linear Shaped Charge under Asymmetric Detonation[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2025 , 45(6) : 1268 -1275 . DOI: 10.15892/j.cnki.djzdxb.2025.06.038

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