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弹药技术

尾翼型 EFP 形成的数值模拟研究

  • 张孝中 ,
  • 赵太勇 ,
  • 陈智刚 ,
  • 郭光全 ,
  • 李建飞
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  • 1 中北大学地下目标毁伤技术国防重点学科实验室,太原 030051
    2 晋西工业集团有限责任公司,太原 030051

张孝中(1989-),男,山西中阳人,硕士研究生,研究方向:弹箭控制与高效毁伤技术。

收稿日期: 2016-09-20

  网络出版日期: 2025-05-28

Numerical Simulation Research on the Formation of Fin Type EFP Explosively Formed Projectile

  • ZHANG Xiaozhong ,
  • ZHAO Taiyong ,
  • CHEN Zhigang ,
  • GUO Guangquan ,
  • LI Jianfei
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  • 1 National Defense Key Subject Laboratory of Underground Target Damage Technology, North University of China, Taiyuan 030051, China
    2 Jinxi Industries Group Co. Ltd, Taiyuan 030051, China

Received date: 2016-09-20

  Online published: 2025-05-28

摘要

为得到飞行稳定性较好的尾翼型爆炸成型弹丸。文中利用有限元分析软件,对三种药型罩结构的成翼过程进行数值模拟,对比计算结果得知,药型罩外表面周向对称刻槽且槽内有填充物时成翼效果较优。继而改变槽深、槽宽等参数,并以不同材料填充槽体进行计算。结果表明:槽深、槽宽等均对侵彻性能影响显著,且填充45钢,槽宽为0.048倍、槽深为0.038倍装药直径时,具有较大的侵彻速度和长径比,尾翼成形效果较好。

本文引用格式

张孝中 , 赵太勇 , 陈智刚 , 郭光全 , 李建飞 . 尾翼型 EFP 形成的数值模拟研究[J]. 弹箭与制导学报, 2017 , 37(4) : 47 -50 . DOI: 10.15892/j.cnki.djzdxb.2017.04.011

Abstract

In order to obtain the fin type explosively formed projectile with better flight stability, this thesis utilized finite element analysis software, and the numerical simulation of three kinds of wing formation process of liner structure was carried out. Comparing with the computing result, the forming fins effect was better when the outer surface of the liner was symmetrically cut and there were fillers in the tank. Then the parameters such as groove depth and groove width were changed, and the tank was filled with different materials for calculation. The conclusion indicated that the groove depth and groove width had remarkable influence on penetration performance, and it was filled with 45 steel. When the groove width was 0.048 times the charge diameter and the groove depth was 0.038 times the charge diameter, it had bigger penetration speed and aspect ratio, and the fin forming effect was better.

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参考文献

[1]
刘建青, 郭涛, 顾文彬,等. 三点起爆形成尾翼 EFP 的数值模拟和实验研究[J]. 爆炸与冲击, 2013. 33 1:38-46.
[2]
陆鸣, 井志胜, 张端平,等. 四点起爆形成带尾翼 EFP 的试验研究 弹箭与制导学报, 2009, 29 1:128-129.
[3]
于川, 董庆东, 孙承纬,等. 带尾翼翻转型爆炸成形弹丸试验研究[J]. 爆炸与冲击, 2003, 23 6:561-564.
[4]
BOUET T H,TARAYRE P,GUILLON J P. Study of a multi-point ignition EFP[C]//National Defence Research Establishment. 15th International Symposium on Ballistics. Israel:[s.n.]. 1995: 159-166.
[5]
林加剑,沈兆武,任辉启,等. 贴隔板法形成尾翼型 EFP 的试验研究及数值模拟[J]. 火炸药学报,2009, 32(1):74-78.
[6]
赵慧英,沈兆武,李成兵,等. 带尾翼爆炸成型弹丸的新技术[J]. 含能材料,2006,14(2):102-104.
[7]
WEIMANN K. Flight stability of EFP with star shaped tail[C]//National Defence Research Establishment. 14th International Symposium on Ballistics. Queber:[s.n.]. 1993:755-763.
[8]
唐平江,顾文彬,罗智伟. 变壁厚壳体对形成带尾翼 EFP 的影响[J]. 四川兵工学报,2009,30 (1 ):34-36.
[9]
门建兵,蒋建伟,万丽珍. 带尾翼EFP形成的三维数值模拟研究[J]. 北京理工大学学报,2002,22 (2 ):166-168.
[10]
李裕春,时党勇,赵远. LS-DYNA 基础理论与工程实践[M].北京: 中国水利水电出版社,2008: 264-282.
[11]
张先锋,陈惠武,赵有守.EFP 冲击引爆带壳炸药数值模拟研究[J]. 弹道学报,2006,18(1):90-92.
[12]
张钧,陈智刚,李小军,等. 变壁厚球缺罩杆式射流的形成与侵彻性能研究[J]. 爆破器材,2016,45(1):39-42.
[13]
MALEJKO G,KUHNLE W G. Aerodynamic predictions for explosively formed penetrators with thick fins using an inviscid cfd code[C]//AIAA. 32nd Aerospace Sciences Meeting & Exhibit.[S.l.:s.n.],1994:1-8.
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