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Numerical investigation of matrix cracking propagation in cross-ply laminated composites subjected to three-point bending load using concurrent multiscale model

机译:用同时多尺度模型对三点弯曲载荷进行三分弯曲载荷的跨层叠层复合材料的数值研究

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摘要

The purpose of the present study is to analyze fiber-matrix debonding and induced matrix cracking formation as two major micromechanical damage modes in cross-ply composite laminates using a two-dimensional numerical approach. To this aim, the cross-ply laminates containing 90-degree layers are modeled, where the fibers are arranged randomly in transverse plies. Damage modes in this numerical model are simulated by the cohesive surface method. The performed analyses reveal that in the laminates with 90-degree layers located in the outer positions, the primary micro damage mode is micro matrix cracking which is initiated from the fiber-matrix debonding damage mode and will be followed by matrix cracking. The main benefit of the present study in comparison to other numerical methods is proposing a virtual test method for damage analysis of different cross-ply laminates in which, the matrix cracking formation will emerge physically in a random and antisymmetric pattern similar to the experimental observations.
机译:本研究的目的是分析纤维 - 基质剥离和诱导的基质裂化形成,以使用二维数值方法在交叉层复合层压板中的两个主要微机械损坏模式。为此目的,含有90度层的交叉层层叠层被建模,其中纤维在横向层中随机排列。通过粘性表面法模拟了该数值模型中的损坏模式。所执行的分析表明,在具有90度层的层压板中,主微损伤模式是从光纤矩阵剥离损伤模式启动的微矩阵裂缝,然后将是矩阵裂化。与其他数值方法相比,本研究的主要益处是提出了一种用于不同交叉层压板的损伤分析的虚拟试验方法,其中,基质开裂形成将以类似于实验观察的随机和反对称模式物理地出现。

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