头部对称刻槽弹体侵彻半无限厚铝合金靶实验与理论模型

邓佳杰 张先锋 刘闯 王文杰 徐晨阳

邓佳杰, 张先锋, 刘闯, 王文杰, 徐晨阳. 头部对称刻槽弹体侵彻半无限厚铝合金靶实验与理论模型[J]. 爆炸与冲击, 2018, 38(6): 1231-1240. doi: 10.11883/bzycj-2017-0413
引用本文: 邓佳杰, 张先锋, 刘闯, 王文杰, 徐晨阳. 头部对称刻槽弹体侵彻半无限厚铝合金靶实验与理论模型[J]. 爆炸与冲击, 2018, 38(6): 1231-1240. doi: 10.11883/bzycj-2017-0413
DENG Jiajie, ZHANG Xianfeng, LIU Chuang, WANG Wenjie, XU Chenyang. Experimental and theoretical study of symmetrical grooved-nose projectile penetrating into semi-infinite aluminum target[J]. Explosion And Shock Waves, 2018, 38(6): 1231-1240. doi: 10.11883/bzycj-2017-0413
Citation: DENG Jiajie, ZHANG Xianfeng, LIU Chuang, WANG Wenjie, XU Chenyang. Experimental and theoretical study of symmetrical grooved-nose projectile penetrating into semi-infinite aluminum target[J]. Explosion And Shock Waves, 2018, 38(6): 1231-1240. doi: 10.11883/bzycj-2017-0413

头部对称刻槽弹体侵彻半无限厚铝合金靶实验与理论模型

doi: 10.11883/bzycj-2017-0413
基金项目: 

国家自然科学基金项目 U1730101

中组部青年拔尖人才支持计划 2014

武器装备预研基金项目 6140657010116BQ02001

详细信息
    作者简介:

    邓佳杰(1990-), 男, 博士研究生

    通讯作者:

    张先锋, lynx@njust.edu.cn

  • 中图分类号: O385

Experimental and theoretical study of symmetrical grooved-nose projectile penetrating into semi-infinite aluminum target

  • 摘要: 在综合考虑弹体结构稳定性及截面比动能的前提下, 提出一种介于尖卵形弹体及尖锥形弹体间的头部对称刻槽弹体, 以期达到提高侵彻深度的目的。以尖卵形弹体侵彻深度为基准, 开展头部对称刻槽弹体侵彻半无限厚铝合金靶实验。在此基础上, 推导得到可描述头部对称刻槽弹体侵彻2A12铝合金靶过程的局部相互作用模型。同时, 结合头部对称刻槽弹体侵彻后靶体破坏现象, 提出适用于头部对称刻槽弹体的靶体响应力, 进而确立头部对称刻槽弹体的侵彻深度模型。实验结果与理论计算表明, 头部对称刻槽弹体具有相对于尖卵形弹体更好的侵彻能力。头部对称刻槽弹体侵彻深度提高的原因是弹体头部结构截面比动能增加及其侵彻过程中的靶体弱化效应, 其中弱化效应是侵彻深度提高的主控因素。
  • 图  1  尖卵形弹体和头部对称刻槽弹体结构工程图

    Figure  1.  Schemes of ogive-nose projectile and symmetrical grooved-nose projectile

    图  2  尖卵形弹体和头部对称刻槽弹体实物图

    Figure  2.  Photograph of ogive-nose projectile and symmetrical grooved-nose projectile

    图  3  侵彻实验布局

    Figure  3.  Sketch of projectile penetration test

    图  4  侵彻深度实验结果及其二次多项式拟合曲线

    Figure  4.  Experimental data and fitting curves of penetration depth

    图  5  回收弹体情况

    Projectiles after penetration tests

    图  6  侵彻后靶体破坏情况

    Figure  6.  Damages of targets after penetration tests

    图  7  侵彻后靶体材料挤出现象

    Figure  7.  Phenomenon of target material extrusion

    图  8  笛卡尔坐标系下头部对称刻槽弹体结构示意图

    Figure  8.  Schematic diagram of symmetrical grooved-nose projectile in Cartesian coordinate

    图  9  头部对称刻槽弹体剖面示意图

    Figure  9.  Sectional view of symmetrical grooved-nose projectile

    图  10  对称槽区域的靶体裂纹示意图

    Figure  10.  Crack of symmetrical grooved-nose area

    图  11  理论计算与实验侵彻深度结果对比

    Figure  11.  Comparison of penetration depth between theoretical and experimental results

    表  1  尖卵形弹体和头部对称刻槽弹体侵彻深度实验对比

    Table  1.   Experiment data of DOP between ogive-nose projectile and symmetrical grooved-nose projectile

    实验号 尖卵形弹体 头部对称刻槽弹体
    侵彻速度v0/(m·s-1) 质量m/g 侵彻深度P/mm 侵彻速度v0/(m·s-1) 质量m/g 侵彻深度P/mm
    1 417 65.5 35.6 373 66.3 36.2
    2 501 66.3 41.2 453 66.0 45.1
    3 615 66.4 59.8 615 66.3 67.2
    4 676 65.7 63.5 648 66.2 71.2
    5 719 65.6 73.0 691 66.4 79.2
    6 742 65.6 77.8 745 66.0 89.0
    7 793 65.9 86.4 768 65.7 95.2
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出版历程
  • 收稿日期:  2017-11-17
  • 修回日期:  2018-02-09
  • 刊出日期:  2018-11-25

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