Ballistic impact wave and bulge profile propagation characteristics and blunt injury assessment of UHMWPE laminate composite

Yihui Zhu, Yang Song, Wei Wu, Weilong Niu, Zhuangqing Fan, Yaoke Wen, Cheng Xu, Min Xia
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Abstract

Amid escalating localized conflicts worldwide, the elucidation of the mechanisms and quantification blunt trauma the emergency services and military personnel confronted becomes imperatively. However, the understanding of bullet-induced bulge formation on the laminate's back face, impact wave propagation, and consequent trauma assessment methods remains incomplete. This study applies 3-dimension digital image correlation (3D-DIC) method to reveals these phenomena by utilizing a lead-core bullet traveling at 334.93 m/s to impact an ultra-high molecular weight polyethylene (UHMWPE) laminate. The results show that the initial transverse propagation velocity of bulge profile is 24.79% smaller than the theoretical calculation, which indicates the reduction caused by cohesive matrix. The transverse wave demonstrates a double exponential attenuation pattern, which could be decomposed into two single exponential attenuation curves. The bulge profile shows hyperbolic pattern, which reveals the stability of the bulge shape and the temporal evolution pattern. Increasing the laminate-body gap leads to a decline in Blunt Criterion (BC) and the Abbreviated Injury Scale (AIS) values reduce from 2 to 0 correspondingly. The numerical model confirms the compression wave velocity as 1447.77 ± 123.10 m/s in the thickness direction and 9542.86 ± 3087.75 m/s in the fiber direction. These findings reveals and quantified the propagation patterns of back bulge and compressive wave, and thus could provide data-driven insights to improve body armor performance and blunt trauma assessment for individual soldiers.
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超高分子量聚乙烯层压复合材料的弹道冲击波和隆起剖面传播特性以及钝伤评估
在全球局部冲突不断升级的情况下,阐明应急服务和军事人员所面临的钝性创伤的机制并对其进行量化已成为当务之急。然而,人们对子弹在层压板背面引起的隆起形成、冲击波传播以及由此产生的创伤评估方法的了解仍不全面。本研究采用三维数字图像相关(3D-DIC)方法,利用一颗速度为 334.93 米/秒的铅芯子弹撞击超高分子量聚乙烯(UHMWPE)层压板来揭示这些现象。结果表明,隆起剖面的初始横向传播速度比理论计算小 24.79%,这表明内聚基质导致了传播速度的降低。横波呈现双指数衰减模式,可分解为两条单指数衰减曲线。凸起轮廓呈现双曲线模式,揭示了凸起形状的稳定性和时间演化模式。增大层压体间隙会导致钝性标准(BC)下降,缩写损伤量表(AIS)值也会相应地从 2 降至 0。数值模型证实压缩波速度在厚度方向为 1447.77 ± 123.10 m/s,在纤维方向为 9542.86 ± 3087.75 m/s。这些发现揭示并量化了背部隆起和压缩波的传播模式,从而为改善防弹衣性能和评估士兵钝伤提供了数据驱动的见解。
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