含偏心起爆对EFP战斗部飞行特性的影响

刘健峰 龙源 纪冲 赵长啸 姜楠

刘健峰, 龙源, 纪冲, 赵长啸, 姜楠. 含偏心起爆对EFP战斗部飞行特性的影响[J]. 爆炸与冲击, 2015, 35(3): 335-342. doi: 10.11883/1001-1455-(2015)03-0335-08
引用本文: 刘健峰, 龙源, 纪冲, 赵长啸, 姜楠. 含偏心起爆对EFP战斗部飞行特性的影响[J]. 爆炸与冲击, 2015, 35(3): 335-342. doi: 10.11883/1001-1455-(2015)03-0335-08
Liu Jian-feng, Long Yuan, Ji Chong, Zhao Chang-xiao, Jiang Nan. Effect of eccentric initiation on the flight characteristics and ballistic dispersion of EFP[J]. Explosion And Shock Waves, 2015, 35(3): 335-342. doi: 10.11883/1001-1455-(2015)03-0335-08
Citation: Liu Jian-feng, Long Yuan, Ji Chong, Zhao Chang-xiao, Jiang Nan. Effect of eccentric initiation on the flight characteristics and ballistic dispersion of EFP[J]. Explosion And Shock Waves, 2015, 35(3): 335-342. doi: 10.11883/1001-1455-(2015)03-0335-08

含偏心起爆对EFP战斗部飞行特性的影响

doi: 10.11883/1001-1455-(2015)03-0335-08
基金项目: 北京理工大学爆炸科学与技术国家重点实验室开放基金项目(KFJJ10-2 M)
详细信息
    作者简介:

    刘健峰(1988—), 男, 博士研究生, 18260098162@163.com

  • 中图分类号: O383;TJ410.33

Effect of eccentric initiation on the flight characteristics and ballistic dispersion of EFP

  • 摘要: 为研究起爆不对称性对EFP战斗部飞行特性的影响, 对不同偏心量下⌀60 mm弧锥结合罩EFP战斗部进行飞行弹道实验。实验结果表明:偏心起爆条件下, 当相对偏心量小于3.3%时, EFP在网靶穿孔接近圆形, 弹丸飞行稳定; 起爆相对偏心量达到6.7%时, 弹丸飞行过程中摆动幅值增大, 降低了对目标的打击精度和毁伤效果。利用LS-DYNA及CFX非线性动力学有限元程序对不同起爆偏心量下成型EFP的空气动力学特性进行数值模拟, 描述了偏心起爆影响EFP成型对称性, 改变弹丸在飞行过程中流场的分布特征, 从而导致弹丸飞行过程中无规则运动的全过程。
  • 图  1  ⌀60 mm EFP战斗部实验照片图

    Figure  1.  Experimental picture of⌀60 mm EFP warhead

    图  2  不同偏心量设计方案

    Figure  2.  The design of different initiation eccentricity

    图  3  EFP战斗部偏心起爆飞行弹道实验布置示意图

    Figure  3.  Setup of EFP flight trajectory experiment

    图  4  实验所得EFP在飞行弹道不同距离上网靶穿孔照片

    Figure  4.  Experimental net target perforation photo of EFP at different distances on flight trajectory

    图  5  攻角随EFP飞行距离变化曲线

    Figure  5.  Attack angle varied with different distance on flight trajectory

    图  6  摆动角随EFP飞行距离变化曲线

    Figure  6.  Swinging angle varied with different distance on flight trajectory

    图  7  钢靶上弹丸穿孔分布图

    Figure  7.  Perforation distributions of 45 steel target

    图  8  1/2有限元计算模型

    Figure  8.  The 1/2 structure of the finite-element model

    图  9  不同相对起爆偏心量影响EFP成型

    Figure  9.  Influence of different relative initiation eccentricity on EFP forming

    图  10  不同相对偏心量对弹丸横向速度效应的影响

    Figure  10.  Influence of different relative initiation eccentricity on EFP lateral velocity

    图  11  偏心起爆获得EFP的飞行弹道流场分布

    Figure  11.  The distribution of EFP flow field on flight trajectory

    图  12  不同相对偏心量的弹丸的稳定储备量

    Figure  12.  The stabilization storage of projectile with different relative initiation eccentricity

    表  1  不同工况气动力初始计算状态及基本参数

    Table  1.   The initial calculation state and basic parameters of different aerodynamic conditions

    K/% v/(m·s-1) S/cm2 L/cm
    0.0 1 500.08 3.02 4.31
    3.3 1 496.89 3.53 4.14
    5.0 1 487.00 6.37 3.95
    6.7 1 475.08 9.15 3.73
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出版历程
  • 收稿日期:  2013-10-29
  • 修回日期:  2014-05-20
  • 刊出日期:  2015-05-25

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