复合材料易碎弹实验测试与仿真分析研究

doi:10.3969/j.issn.1000-1093.2013.09.001

摘要/Abstract

摘要：

基于分离式霍普金森压杆(SHPB) 实验获取复合材料易碎弹及航空有机玻璃的材料动态力学参数,选择合理描述易碎弹与有机玻璃材料的本构模型;采用显示动力学分析软件LS-DYNA中的光滑粒子流体动力学(SPH)方法对易碎弹侵彻靶板全过程进行仿真分析。通过仿真分析研究易碎弹着靶速度、入射角度对弹体破碎和靶板毁伤的影响规律,对比不同工况下子弹的破碎效果及毁伤性能,分析总结相关规律。结果表明:子弹的破碎效果及毁伤性能随着入射速度的增大提高明显;相同速度下,子弹垂直入射靶板其破碎与毁伤效果均要优于倾斜入射靶板。数值模拟方法及结果为易碎弹的研制提供了一定的理论参考依据。

关键词: 兵器科学与技术, 易碎弹, 侵彻, 数值模拟, 破碎

Abstract:

Dynamic mechanics parameters of composite fragile projectile and aviation organic glass areobtained by split Hopkinson press bar (SHPB) experiment. The reasonable material constitutive modelsare chosen to model the fragile projectile and organic glass based on LS-DYNA software. The simulationof the fragmentation process of fragile projectile penetrating target is carried out with smoothed particle hydrodynamics(SPH) method. The influence rule of projectile frangibility and damage performance is researched by analyzing the falling speed and impacting angle of projectile, and the relevant results aresummarized by comparing the fragile and damage performances. Simulation result shows that the perform-ances of fragmentation and penetration increase as the incident velocity increases, and at the same velocity, the performances of fragmentation and penetration under normal penetrating are superior to obliquepenetrating. Numerical simulation and analysis of results offer a theoretical reference for the study offragile projectile.

Key words: ordnance science and technology, fragile projectile, penetration, numerical simulation, fragmentation

中图分类号:

TJ012. 4

荣吉利, 李健, 刘先光, 林贤坤. 复合材料易碎弹实验测试与仿真分析研究[J]. 兵工学报, 2013, 34(9): 1057-1064.

RONG Ji-li, LI Jian, LIU Xian-guang, LIN Xian-kun. Simulative Analysis and Experimental Test of Composite Fragile Projectile Under Impact Dynamics[J]. Acta Armamentarii, 2013, 34(9): 1057-1064.

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