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基于物质点法不同头部形状弹体侵彻动靶过程的仿真研究
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  • 英文篇名:Numerical simulation on the projectile with different nose shapes penetrating moving target based on material point method
  • 作者:谢桂兰 ; 陈飞 ; 龚曙光 ; 陆文举
  • 英文作者:Xie Guilan;Chen Fei;Gong Shuguang;Lu Wenju;School of Mechanical Engineering, Xiangtan University;Key Laboratory of Welding Robot and Application Technology of Hunan Province, Xiangtan University;Engineering Research Center of Complex Trajectory Processing Technology and Equipment of Ministry of Education, Xiangtan University;
  • 关键词:数值模拟 ; 运动靶 ; 侵彻 ; 子弹头部形状 ; 物质点法
  • 英文关键词:numerical simulation;;moving-target;;penetration;;nose shape of projectile;;material point method
  • 中文刊名:YYLX
  • 英文刊名:Chinese Journal of Applied Mechanics
  • 机构:湘潭大学机械工程学院;湘潭大学焊接机器人及应用技术湖南省重点实验室;湘潭大学复杂轨迹加工工艺及装备教育部工程研究中心;
  • 出版日期:2019-02-01 16:56
  • 出版单位:应用力学学报
  • 年:2019
  • 期:v.36;No.157
  • 基金:国家自然科学基金(51475403)
  • 语种:中文;
  • 页:YYLX201903012
  • 页数:8
  • CN:03
  • ISSN:61-1112/O3
  • 分类号:79-85+264
摘要
为分析弹头形状对动靶侵彻性能的影响以及解决有限元法模拟子弹侵彻问题时存在的网格畸变问题,本文采用物质点法建立了弹体侵彻靶板的数值模型。利用编写的程序对卵形弹侵彻静靶过程进行了仿真,并将仿真结果与实验测试结果进行了对比分析。结果表明,利用物质点法仿真子弹侵彻过程是可行和有效的。通过对平头弹、球形弹、卵形弹侵彻动靶过程的模拟仿真,得到了弹体贯穿动靶后弹体的剩余速度、偏转角、扭转角、靶板的毁伤效果。所得结果显示:当靶板速度较低时,卵形弹侵彻动靶时靶板的毁伤面积最小;当靶板速度较高时,卵形弹侵彻动靶时靶板的毁伤面积最大;弹体偏转角和扭转角均随动靶速度的增加而逐渐增大,且卵形弹的偏转角和扭转角均大于平头弹和球形弹;当动靶初速度小于300m/s时,卵形弹的侵彻能力较强;当动靶初速度大于300m/s时,球形弹的侵彻能力较强。本文研究对弹丸侵彻和装甲防护等军工领域有一定的指导作用。
        In order to study the effects of projectile's nose shapes on projectile penetrating the moving-target and solve the problem of mesh distortion when simulating the projectile penetration by finite element method(FEM), the model of projectile with different nose shapes penetrating target are established based on material point method. The program is written to simulate the process of oval-nosed projectile penetrating fixed-target in this paper. By comparing the simulation results with the experiment tests and the finite element analysis, the results indicate that it is feasible to simulate projectile penetration based on material point method. The flat-nosed projectile, spherical-nosed projectile and oval-nosed projectile penetrating moving-target are simulated, respectively. The remaining kinetic energy, deflection angle, torsion angle of projectile and penetration effect of moving-target are computed and analyzed after different nosed projectiles penetrate moving-target. The research results show that the damage area of oval-nosed projectile is the smallest when the target velocity is low. And when the target velocity is high, the damage area of oval-nosed projectile is the largest, and the deflection angle and the torsion angle increase as moving-target velocity increases. The deflection angle and the torsion angle with oval-nosed projectile are larger than those of flat-nosed projectile and spherical-nosed projectile. The penetration capability of oval-nosed projectile is more intense when the initial velocity of moving target is less than 300 m/s. The penetration capability of spherical-nosed projectile is more intense when the initial velocity of moving target is larger than 300 m/s. The research has a certain guiding role in the field of military industry such as penetration and armor protection.
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