聚能射流侵彻径向扩孔的可压缩模型

李干 陈小伟

李干, 陈小伟. 聚能射流侵彻径向扩孔的可压缩模型[J]. 爆炸与冲击, 2022, 42(7): 073301. doi: 10.11883/bzycj-2021-0466
引用本文: 李干, 陈小伟. 聚能射流侵彻径向扩孔的可压缩模型[J]. 爆炸与冲击, 2022, 42(7): 073301. doi: 10.11883/bzycj-2021-0466
LI Gan, CHEN Xiaowei. A compressible model of radial crater growth by shaped-charge jet penetration[J]. Explosion And Shock Waves, 2022, 42(7): 073301. doi: 10.11883/bzycj-2021-0466
Citation: LI Gan, CHEN Xiaowei. A compressible model of radial crater growth by shaped-charge jet penetration[J]. Explosion And Shock Waves, 2022, 42(7): 073301. doi: 10.11883/bzycj-2021-0466

聚能射流侵彻径向扩孔的可压缩模型

doi: 10.11883/bzycj-2021-0466
基金项目: 国家自然科学基金(11872118,11627901)
详细信息
    作者简介:

    李 干(1991- ),男,博士研究生, xinren1210@163.com

    通讯作者:

    陈小伟(1967- ),男,博士,教授,博士生导师,chenxiaoweintu@bit.edu.cn

  • 中图分类号: O385

A compressible model of radial crater growth by shaped-charge jet penetration

  • 摘要: 聚能射流侵彻厚靶时,对靶材同时进行轴向和径向挤压进而发生轴向侵彻和径向扩孔。本文中基于聚能射流侵彻可压缩模型并结合Szendrei-Held扩孔方程,推导给出考虑弹/靶材料可压缩性的聚能射流扩孔方程。为简化完整可压缩模型繁琐的计算过程,又基于Murnaghan状态方程给出可压缩模型的近似解。与水中聚能射流扩孔的实验研究对比分析,表明该模型预测优于Szendrei-Held扩孔方程。模型分析表明,射流半径、驻点压力、靶材强度、驻点处靶材密度以及聚能射流速度是影响聚能射流扩孔的主要因素。本文模型可以更准确地预测聚能射流侵彻可压缩性较强的靶材的扩孔情况。相关工作可为含液密闭结构干扰聚能射流侵彻提供理论基础。
  • 图  1  侵彻速度与扩孔速度分布及侵彻过程中的流场

    Figure  1.  Distribution of penetration velocity and radial crater velocity, flow field during penetration

    图  2  不同方法获得的扩孔孔径随时间变化的比较

    Figure  2.  Comparison of crater radius varying with time among different methods

    图  3  靶材最大扩孔半径与水深度的关系

    Figure  3.  Relationship between the maximum target crater radius and the water depth

    图  4  靶材最大扩孔半径与射流半径的关系(h=10 m)

    Figure  4.  Relationship between the maximum target crater radius and the jet radius (h=10 m)

    图  5  水、铝和铜的Hugoniot压力曲线

    Figure  5.  Hugoniot pressure curves for water, aluminium and copper

    图  6  射流侵彻靶材的驻点压力随射流速度的变化

    Figure  6.  Stagnation point pressure of jets penetrating targets varying with jet velocity

    表  1  材料的Mie-Grüneisen状态方程和Murnaghan状态方程参数

    Table  1.   Material parameters of Mie-Grüneisen and Murnaghan equations of state

    材料ρ0/(kg·m−3)c0/(m·s−1)s1s2Γ0nD/(kg·m−1·s−2)
    [8]893039401.48901.994.9562.797×1010
    [18]100016471.92 00.1 6.68 4.061×108
    [19]275053281.33801.974.3521.794×1010
    下载: 导出CSV

    表  2  不同模型的相关参数和计算结果的比较

    Table  2.   Comparison of relevant parameters and calculation results among different models

    模型u/(m·s−1)A/(m4·s−2)B/(m2·s−2)rmax/mmtmax/μs
    Szendrei-Held模型[13]50006.295200056.11254
    可压缩模型48194.310113661.61827
    近似解48114.367126162.01850
    下载: 导出CSV

    表  3  不同方法获得的铜射流侵彻铝靶最大扩孔半径的比较

    Table  3.   Comparison of the maximum target crater radii for copper jets penetrating aluminum targets by different methods

    v/(m·s−1)最大扩孔半径/mm
    实验[20]Szendrei-Held模型[20]本文模型
    76007.507.67.9
    67507.256.67.0
    61006.006.06.2
    下载: 导出CSV
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出版历程
  • 收稿日期:  2021-11-10
  • 修回日期:  2022-05-12
  • 网络出版日期:  2022-05-30
  • 刊出日期:  2022-07-25

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