不同角度下EFP战斗部装药破坏规律的数值模拟与实验研究

IF 1.4 4区 工程技术 Q3 ENGINEERING, CIVIL Latin American Journal of Solids and Structures Pub Date : 2022-01-01 DOI:10.1590/1679-78256910
Kun Zhang, C. Zhao, C. Ji, Shaoguang Zhang, X. Wang, Tao Jiang, Gang Wu
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引用次数: 0

摘要

本文利用LS-dyna软件对不同角度EFP下圆柱壳的充装过程进行了数值模拟,发现了一些有趣的现象和规律。圆柱壳受EFP冲击时产生圆柱弹性波σ r。圆柱弹性波σ r与圆柱壳装药成功引爆所需的时间相关。当EFP战斗部侵彻角θ在0 ~ 10°范围内时,σ r随(cos θ) -1/2线性增加。随着θ的增大,切向速度v y对EFP对圆柱壳的冲击有明显的影响,弹性波σ r与(cos θ) -1/2之间的线性关系不变。当θ大于45°时,EFP不能成功撞击和起爆圆柱装药。采用测速法测量EFP速度,误差为1.3%。实验结果与仿真结果具有较强的相似性,表明数值模拟模型参数具有较好的可靠性。
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Numerical simulation and experimental study of the damage law of EFP warhead charging of cylindrical shells under different angles
In this paper, LS-dyna software was used to simulate the charging process of cylindrical shell when EFP has different angles, and some interesting phenomena and laws were found. Cylindrical elastic wave σ r was generated when the cylindrical shell was impacted by EFP. The cylindrical elastic wave σ r was correlated with the time required for the cylindrical shell charge to be successfully detonated. When the EFP warhead penetration Angle θ ranges from 0° to 10°, the σ r increases linearly with (cos θ ) -1/2 . With the increase of θ, the tangential velocity v y had an obvious effect on the impact of EFP on the cylindrical shell, and the linear relationship between the elastic wave σ r and (cos θ ) -1/2 does not change. When the θ was greater than 45°, EFP could not successfully impact and detonate the cylindrical shell charge. The EFP velocity was measured by velocity measurement method with an error of 1.3%. The experimental results have strong similarity with the simulation results, indicating that the parameters of the numerical simulation model have good reliability.
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来源期刊
CiteScore
2.80
自引率
8.30%
发文量
37
审稿时长
>12 weeks
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