大着速范围长杆弹侵彻深度变化及其影响因素的数值模拟

徐晨阳 张先锋 刘闯 邓佳杰 郑应民

徐晨阳, 张先锋, 刘闯, 邓佳杰, 郑应民. 大着速范围长杆弹侵彻深度变化及其影响因素的数值模拟[J]. 高压物理学报, 2018, 32(2): 025103. doi: 10.11858/gywlxb.20170592
引用本文: 徐晨阳, 张先锋, 刘闯, 邓佳杰, 郑应民. 大着速范围长杆弹侵彻深度变化及其影响因素的数值模拟[J]. 高压物理学报, 2018, 32(2): 025103. doi: 10.11858/gywlxb.20170592
XU Chenyang, ZHANG Xianfeng, LIU Chuang, DENG Jiajie, ZHENG Yingmin. Depth of Penetration and Its Influence Factors of Long Rod Projectile Impacting on Semi Infinite Target with Elevated Velocity[J]. Chinese Journal of High Pressure Physics, 2018, 32(2): 025103. doi: 10.11858/gywlxb.20170592
Citation: XU Chenyang, ZHANG Xianfeng, LIU Chuang, DENG Jiajie, ZHENG Yingmin. Depth of Penetration and Its Influence Factors of Long Rod Projectile Impacting on Semi Infinite Target with Elevated Velocity[J]. Chinese Journal of High Pressure Physics, 2018, 32(2): 025103. doi: 10.11858/gywlxb.20170592

大着速范围长杆弹侵彻深度变化及其影响因素的数值模拟

doi: 10.11858/gywlxb.20170592
基金项目: 

中共中央组织部青年拔尖人才支持计划 2014

中央高校基本科研业务专项基金 30917011104

中央高校基本科研业务专项基金 30916011305

国家自然科学基金委员会与中国工程物理研究院联合基金 U1730101

详细信息
    作者简介:

    徐晨阳(1992—), 男,硕士研究生,主要从事冲击动力学研究.E-mail:xcynjust@126.com

    通讯作者:

    张先锋(1978—), 男,博士,教授,主要从事高效毁伤与防护研究.E-mail:lynx@njust.edu.cn

  • 中图分类号: O385

Depth of Penetration and Its Influence Factors of Long Rod Projectile Impacting on Semi Infinite Target with Elevated Velocity

  • 摘要: 高速/超高速侵彻问题一直是武器设计者和防护工程专家关注的焦点问题之一。随着撞击速度的提高,弹体可能进入流体侵彻阶段,侵彻深度不再随速度的增大单调上升。针对撞击速度增加侵彻深度可能出现增量逆转的现象,开展了大着速范围长杆弹侵彻深度变化的数值模拟研究,分析了弹体硬度、头部形状、弹体材料及靶体材料对侵彻转变点的影响。结果表明:随着长杆弹冲击速度的提升,侵彻深度先上升后下降;同时,弹体硬度提高,到达侵彻转变点对应的撞击速度提高;尖卵形头部弹体到达侵彻转变点的撞击速度比球形头部弹体高;此外,弹靶材料对侵彻深度转变也有较大的影响。

     

  • 图  长杆弹侵彻深度理论计算曲线

    Figure  1.  Theoretical DOP results of LRP at elevated impact velocity

    图  有限元模型

    Figure  2.  Finite element model

    图  撞击速度为967 m/s时弹靶变形过程

    Figure  3.  Simulation of normalized DOP and deformation at 967 m/s impact velocity

    图  模拟侵深与实验数据对比

    Figure  4.  Comparison between simulation normalized DOP and experimental data

    图  不同硬度弹体侵彻深度-速度曲线

    Figure  5.  Normalized DOP versus impact velocity for projectile with different hardnesses

    图  不同头部形状弹体侵彻深度-速度曲线

    Figure  6.  Normalized DOP versus impact velocity for projectile with different nose shapes

    图  不同靶体材料侵彻规律

    Figure  7.  Normalized DOP versus impact velocity for target with different materials

    图  不同材料弹体的侵彻规律

    Figure  8.  Normalized DOP versus impact velocity for projectiles with different materials

    表  1  弹体仿真模型主要参数

    Table  1.   Basic parameters of projectile

    A/MPa B/MPa n C D1 D2 D3 D4
    1 069 710.1 0.459 0.047 0.239 8.593 6.67 0.009
    下载: 导出CSV

    表  2  靶体仿真模型主要参数

    Table  2.   Basic parameters of target

    G/MPa Y/MPa β n Gp GT/(MPa·K-1) Yp T/K
    2 760 680 125 0.1 1.8 -17 0.018 1 220
    下载: 导出CSV

    表  3  30CrMnSiNi2A材料的J-C模型参数[20]

    Table  3.   J-C Parameters of 30CrMnSiNi2A materials[20]

    HRC A/MPa B/MPa n C D1 D2 D3 D4
    31 745 623.11 0.424 0.061 0.351 1.650 2.589 0.020
    36 814 643.57 0.446 0.055 0.348 2.673 4.333 0.012
    45 1 269 810.18 0.479 0.040 0.239 8.593 7.867 0.009
    55 1 516 1 537.97 0.610 0.017 0.014 0.015 3.251 0.007
    下载: 导出CSV

    表  4  不同硬度条件下侵彻转变阶段的弹体速度范围

    Table  4.   Range of projectile velocity in the transition stage with different hardnesses

    HRC Velocity range/(m·s-1)
    31 806-1 100
    36 832-1100
    45 967-1216
    下载: 导出CSV

    表  5  不同头部形状弹体参数

    Table  5.   Geometric size of rod with different nose

    Head shape R/mm L0/mm d/mm ρ/(g·cm-3) m/g
    Ball 3.5 71.00 3.5 7.83 21
    Ogive, φ=2 14.2 73.26 3.5 7.83 21
    Ogive, φ=3 21.3 73.61 3.5 7.83 21
    Ogive, φ=4 28.4 74.56 3.5 7.83 21
    下载: 导出CSV

    表  6  弹体材料参数

    Table  6.   Parameters of projectile material

    Material ρ/(g·cm-3) A/MPa B/MPa n C D1 D2 D3 D4
    30CrMnSiNi2A 7.83 745 623.11 0.424 0.061 0.351 1.650 2.589 0.020
    Tungalloy 17.70 631 1 258.00 0.092 0.014 0 0.330 -1.500 0
    下载: 导出CSV
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  • 收稿日期:  2017-06-15
  • 修回日期:  2017-06-25

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