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A Ballistic Material Model For Cross-plied Unidirectional Ultra-high Molecular-weight Polyethylene Fiber-reinforced Armor-grade Composites

机译:交叉单向超高分子量聚乙烯纤维增强铠装级复合材料的弹道材料模型

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摘要

The known fiber and polymeric-matrix material properties, unit-cell microstructural characteristics and unit-cell level finite-element analyses are used to construct a new ballistic material model for 0°/90° cross-plied oriented polyethylene fiber-based armor-grade composite laminates. The model is constructed in such a way that it can be readily integrated into commercial finite-element programs like ANSYS/Autodyn [ANSYS/Autodyn version 11.0, User Documentation, Century Dynamics Inc., a subsidiary of ANSYS Inc., 2007] and ABAQUS/Explicit [ABAQUS version 6.7, User Documentation, Dessault Systems, 2007] as a user material subroutine. To validate the model, a series of transient non-linear dynamics simulations of the transverse impact of armor-grade composite laminates with two types of bullets/projectiles is carried out. The results obtained are next compared with their experimental counterparts. This comparison revealed that a relatively good agreement is obtained between the experimental and the computational analysis relative to: (a) the success of the armor panels of different areal densities in defeating the bullets at different initial bullet velocities; (b) post-mortem spatial distribution of damage within the panels; (c) the temporal evolution of a bulge at the back-face of the armor; and (d) the existence of three distinct armor-penetration stages (i.e. an initial filament shearing/cutting dominated stage, an intermediate stage characterized by pronounced filament/matrix de-bonding/decohesion and the final stage associated with the extensive bulging of the armor panel).
机译:已知的纤维和聚合物基体材料性能,单位晶胞的微结构特征和单位晶胞水平的有限元分析被用于构建新的防弹材料模型,用于0°/ 90°交叉取向聚乙烯纤维基装甲等级复合层压板。该模型的构建方式使其可以轻松集成到商业有限元程序中,例如ANSYS / Autodyn [ANSYS / Autodyn 11.0版,用户文档,ANSYS Inc.的子公司Century Dynamics Inc.,2007年]和ABAQUS。 / Explicit [ABAQUS版本6.7,用户文档,Dessault系统,2007年]作为用户材料子例程。为了验证该模型,对装甲级复合材料层板与两种子弹/弹丸的横向冲击进行了一系列瞬态非线性动力学模拟。接下来将获得的结果与实验结果进行比较。这种比较表明,相对于以下方面,实验分析和计算分析之间获得了相对较好的一致性:(a)在不同的初始子弹速度下,不同面密度的装甲板在击败子弹方面的成功; (b)面板内损坏的验尸空间分布; (c)装甲背面凸起的时间变化; (d)存在三个不同的装甲穿透阶段(即初始的细丝剪切/切割为主阶段,以显着的细丝/基质解粘/解聚为特征的中间阶段以及与装甲的广泛膨胀相关的最后阶段)面板)。

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