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Prediction of the Failure Locus of C/PEEK Composites under Transverse Compression and Longitudinal Shear Through Computational Micromechanics

机译:通过计算微力学预测C / PEEK复合材料在横向压缩和纵向剪切作用下的破坏轨迹

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摘要

The potential of computational micromechanics to predict the failure locus of a unidirectional C/PEEK composite subjected to transverse compression and longitudinal shear was established. Numerical simulations were compared with the experimental results of Vogler and Kyriakides [Vogler TJ, Kyriakides S. Inelastic behavior of an AS4/PEEK composite under combined transverse compression and shear. Part I: Experiments. Int J Plasticity 1999;15:783–806], which contain detailed information of the matrix and fiber properties as well as the failure micromechanisms during multiaxial loading. Analyses were based in the finite element analysis of a three-dimensional representative volume element of the lamina microstructure and included the main deformation and failure mechanisms observed experimentally, namely matrix shear yielding and interface decohesion. In addition, the numerical predictions of the failure locus for composites with strong and weak interfaces were compared with those obtained by current phenomenological failure models to establish the accuracy and range of validity of these criteria.
机译:建立了计算微力学预测单向C / PEEK复合材料在横向压缩和纵向剪切作用下的破坏轨迹的潜力。将数值模拟与Vogler和Kyriakides [Vogler TJ,Kyriakides S. AS4 / PEEK复合材料在组合的横向压缩和剪切作用下的非弹性行为进行了比较。第一部分:实验。 Int J Plasticity 1999; 15:783–806],其中包含有关基体和纤维特性以及多轴加载过程中的破坏微观机制的详细信息。分析是基于层状微结构的三维代表性体积元的有限元分析,并包括实验观察到的主要变形和破坏机理,即基体剪切屈服和界面脱粘。另外,将具有强界面和弱界面的复合材料的失效轨迹的数值预测与通过当前现象学失效模型获得的数值进行了比较,以建立这些标准的准确性和有效性范围。

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