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Evaluation of the damaged area of glass-fiber-reinforced epoxy-matrix composite materials submitted to ballistic impacts

机译:评估玻璃纤维增​​强的环氧基复合材料受到弹道冲击的损坏区域

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摘要

Fiber-reinforced composites submitted to ballistic impact show large, and sometimes irregular, areas of delamination. The evaluation of these damaged areas is important to assess the effects of the laminate microstructure on the response of the material to the imposed loading. In this paper bulletproof laminates were obtained using 30 plies of glass-fiber reinforced-epoxy matrix composites. The ballistic performance of these laminates was varied by modifying the properties of the constituent laminate or by changing the laminate assemblage. An automated digital analysis procedure was developed in order to determine size and shape parameters that characterize the damaged areas. The procedure developed proved to be robust and sensible enough to cope with subtle variations on the damaged areas, which are due to the differences on the mechanical response of the composites caused by modifications on their microstructure. The results obtained show that not only the area of delamination is important to quantify the ballistic performance. The isotropy of the ballistic response, determined measuring the Feret Ratio or the Circular Shape Factor, is also important.
机译:经受弹道冲击的纤维增强复合材料表现出大的,有时是不规则的分层区域。这些受损区域的评估对于评估层压板微结构对材料对施加的载荷的响应的影响很重要。在本文中,使用30层玻璃纤维增​​强环氧树脂基复合材料获得了防弹层压板。这些叠层的弹道性能通过改变组成叠层的性能或改变叠层的组合来改变。为了确定表征受损区域的尺寸和形状参数,开发了一种自动数字分析程序。事实证明,所开发的程序既健壮又明智,足以应付受损区域的细微变化,这是由于复合材料的微观结构发生变化而导致的机械响应差异。获得的结果表明,不仅分层的面积对于量化弹道性能也很重要。弹道响应的各向同性(通过测量费雷特比或圆形形状因子确定)也很重要。

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