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Experimental and analytical study on fiber-kinking failure mode of laminated composites

机译:层状复合材料纤维扭结破坏模式的实验与分析研究

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摘要

Compressive behavior of composite materials has received significant attention in recent years. In the present work, a recently developed strain based fiber kinking model and stress based ones for unidirectional laminated composites are compared with experimental results. These models are implemented into a finite element code and the obtained results for glass/epoxy (Type C) ASNA 4197 unidirectional composites are presented and discussed in detail. Experimental investigations on compressive strength and kink band formation were also performed for several specimens with various dimensions and off-axis angles made of the same glass/epoxy prepreg composite material. A special compressive fixture was also fabricated in order to ensure that the specimens are in full contact with the loading machine elements and also to eliminate the potential bending moments. Comparison between the experimental and analytical results indicated that the proposed fiber kinking model and the developed code can be used to predict the compressive strength of laminated composites due to fiber kinking mode.
机译:近年来,复合材料的压缩性能受到了极大的关注。在当前的工作中,将最近开发的基于应变的纤维扭结模型和基于应力的单向层压复合材料模型与实验结果进行了比较。将这些模型实现为有限元代码,并详细介绍和讨论了玻璃/环氧树脂(C型)ASNA 4197单向复合材料的所得结果。还对由相同的玻璃/环氧树脂预浸料复合材料制成的具有不同尺寸和偏轴角的几个样品进行了抗压强度和扭结带形成的实验研究。还制造了一种特殊的压缩夹具,以确保样品与装载机元件完全接触,并消除潜在的弯矩。实验和分析结果的比较表明,所提出的纤维扭结模型和所开发的代码可用于预测由于纤维扭结模式引起的层压复合材料的抗压强度。

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