变截面爆炸成型弹丸垂直侵彻装甲钢板靶后破片质量模型

邢柏阳 刘荣忠 张东江 陈亮 侯云辉 郭锐

邢柏阳, 刘荣忠, 张东江, 陈亮, 侯云辉, 郭锐. 变截面爆炸成型弹丸垂直侵彻装甲钢板靶后破片质量模型[J]. 爆炸与冲击, 2019, 39(7): 074202. doi: 10.11883/bzycj-2018-0187
引用本文: 邢柏阳, 刘荣忠, 张东江, 陈亮, 侯云辉, 郭锐. 变截面爆炸成型弹丸垂直侵彻装甲钢板靶后破片质量模型[J]. 爆炸与冲击, 2019, 39(7): 074202. doi: 10.11883/bzycj-2018-0187
XING Boyang, LIU Rongzhong, ZHANG Dongjiang, CHEN Liang, HOU Yunhui, GUO Rui. A mass model for behind-armor debris generated by normal penetration of a variable cross-section explosively-formed projectile into an armor steel plate[J]. Explosion And Shock Waves, 2019, 39(7): 074202. doi: 10.11883/bzycj-2018-0187
Citation: XING Boyang, LIU Rongzhong, ZHANG Dongjiang, CHEN Liang, HOU Yunhui, GUO Rui. A mass model for behind-armor debris generated by normal penetration of a variable cross-section explosively-formed projectile into an armor steel plate[J]. Explosion And Shock Waves, 2019, 39(7): 074202. doi: 10.11883/bzycj-2018-0187

变截面爆炸成型弹丸垂直侵彻装甲钢板靶后破片质量模型

doi: 10.11883/bzycj-2018-0187
基金项目: 国家自然科学基金(11372136);中央高校基本科研业务费专项基金(30916011306)
详细信息
    作者简介:

    邢柏阳(1992- ),男,博士研究生,xing_boyang@163.com

    通讯作者:

    郭 锐(1980- ),男,博士,副教授,guorui@njust.edu.cn

  • 中图分类号: O385; TJ012.4; TJ413.+2

A mass model for behind-armor debris generated by normal penetration of a variable cross-section explosively-formed projectile into an armor steel plate

  • 摘要: 考虑爆炸成型弹丸(explosively-formed projectile,EFP)变截面的特性,基于流体力学Bernoulli方程和绝热剪切理论,改进了EFP垂直侵彻装甲钢板靶后破片质量模型,结合已有的试验数据和数值仿真方法检验了改进后模型的准确性。在此基础上,分析了靶板厚度和EFP着靶速度对靶板和EFP产生的靶后破片质量的影响规律。结果表明:相比于改进前的模型,改进后的模型能够更准确地解释靶板和EFP产生的靶后破片质量随靶板厚度和EFP着靶速度的变化规律;当EFP着靶速度为1 650 m/s时,随着靶板厚度从30 mm增大到70 mm,EFP变截面的特性对靶板和EFP产生靶后破片质量的影响不断增强;当靶板厚度为40 mm时,随着EFP着靶速度从1 650 m/s升高到1 860 m/s,EFP变截面的特性对靶板和EFP产生靶后破片质量的影响不断减弱。
  • 图  1  某典型爆炸成型弹丸的形状

    Figure  1.  The shape of a certain typical explosively-formed projectile

    图  2  爆炸成型弹丸(EFP)垂直侵彻靶板的过程

    Figure  2.  The process of an explosively-formed projectile (EFP) normally penetrating into a target

    图  3  冲塞体形成时刻

    Figure  3.  Forming time of a plug

    图  4  侵彻孔半径随时间变化关系

    Figure  4.  The time history of the crater radius

    图  5  依据文献[18-19]构建的EFP模型

    Figure  5.  The EFP model developed according to references [18-19]

    图  6  依据文献[18-19]构建的仿真模型

    Figure  6.  The simulation model developed by according to references [18-19]

    图  7  本文仿真所得的靶后破片云与文献[18]的对比

    Figure  7.  Behind-armor debris clouds obtained by this paper compared with that in reference [18]

    图  8  某典型EFP垂直侵彻靶板的出孔形状(单位:mm)

    Figure  8.  The exit hole shape of a target normally penetrated by a certain typical EFP (unit in mm)

    图  9  不同靶板厚度条件下的靶后破片质量

    Figure  9.  Mass of behind-armor debris for different thicknesses of targets

    图  10  不同EFP着靶速度条件下的靶后破片质量

    Figure  10.  Mass of behind-armor debris for different impact velocities of EFPs

    表  1  不同靶板厚度条件下靶后破片质量的偏差

    Table  1.   Mass deviations of behind-armor debris for different thicknesses of targets

    H0/mmεt,bjm/%εt,djm/%εp,bjm/% εp,djm/%
    304.113.53.532.0
    401.812.32.940.3
    500.825.94.145.4
    607.455.47.454.8
    706.070.110.464.3
    下载: 导出CSV

    表  2  不同EFP着靶速度条件下靶后破片质量的偏差

    Table  2.   Mass deviations of behind-armor debris for different impact velocities of EFPs

    v0/(m·s−1εt,bjm/%εt,djm/%εp,bjm/%εp,djm/%
    1 6501.812.32.940.3
    1 6803.911.22.438.6
    1 7404.99.61.237.1
    1 8002.75.01.236.1
    1 8602.22.30.434.1
    下载: 导出CSV
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出版历程
  • 收稿日期:  2018-05-29
  • 修回日期:  2018-06-28
  • 网络出版日期:  2019-06-25
  • 刊出日期:  2019-07-01

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