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Onset of failure in finitely strained layered composites subjected to combined normal and shear loading

机译:法向和剪切载荷共同作用下有限应变层状复合材料的破坏开始

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摘要

A limiting factor in the design of fiber-reinforced composites is their failure under axial compression along the fiber direction. These critical axial stresses are significantly reduced in the presence of shear stresses. This investigation is motivated by the desire to study the onset of failure in fiber-reinforced composites under arbitrary multi-axial loading and in the absence of the experimentally inevitable imperfections and finite boundaries. By using a finite strain continuum mechanics formulation for the bifurcation (buckling) problem of a rate-independent, perfectly periodic (layered) solid of infinite extent, we are able to study the influence of load orientation, material properties and fiber volume fraction on the onset of instability in fiber-reinforced composites. Two applications of the general theory are presented in detail, one for a finitely strained elastic rubber composite and another for a graphite-epoxy composite, whose constitutive properties have been determined experimentally. For the latter case, extensive comparisons are made between the predictions of our general theory and the available experimental results as well as to the existing approximate structural theories. It is found that the load orientation, material properties and fiber volume fraction have substantial effects on the onset of failure stresses as well as on the type of the corresponding mode (local or global).
机译:纤维增强复合材料设计的一个限制因素是它们在沿纤维方向的轴向压缩下的破坏。在存在剪切应力的情况下,这些临界轴向应力会大大降低。这项研究的动机是希望研究在任意多轴载荷下并且在缺乏实验上不可避免的缺陷和有限边界的情况下纤维增强复合材料的破坏开始。通过使用有限应变连续介质力学公式来解决无限范围内与速率无关的完全周期性(分层)固体的分叉(屈曲)问题,我们能够研究载荷取向,材料特性和纤维体积分数对纤维的影响。纤维增强复合材料的不稳定性开始。详细介绍了通用理论的两种应用,一种用于有限应变的弹性橡胶复合材料,另一种用于石墨-环氧复合材料,其本构性质已通过实验确定。对于后一种情况,我们的一般理论的预测与可用的实验结果以及现有的近似结构理论之间进行了广泛的比较。发现载荷方向,材料特性和纤维体积分数对破坏应力的产生以及相应模式的类型(局部或整体)具有重大影响。

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