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A combined elastoplastic damage model for progressive failure analysis of composite materials and structures

机译:组合弹塑性损伤模型用于复合材料和结构的渐进式破坏分析

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The paper is concerned with the development and verification of a combined elastoplastic damage model for the progressive failure analysis of composite materials and structures. The model accounts for the irreversible strains caused by plasticity effects and material properties degradation due to the damage initiation and development. The strain-driven implicit integration procedure is developed using equations of continuum damage mechanics, plasticity theory and includes the return mapping algorithm. A tangent operator consistent with the integration procedure is derived to ensure a computational efficiency of the Newton-Raphson method in the finite element analysis. The algorithm is implemented in Abaqus as a user-defined subroutine. The efficiency of the constitutive model and computational procedure is demonstrated using the analysis of the progressive failure of composite laminates containing through holes and subjected to in-plane uniaxial tensile loading. It has been shown that the predicted results agree well with the experimental data reported in the literature.
机译:本文涉及用于复合材料和结构的渐进式失效分析的组合弹塑性损伤模型的开发和验证。该模型说明了由于损伤的产生和发展而导致的塑性效应和材料性能退化所引起的不可逆应变。应变驱动的隐式积分程序是使用连续损伤力学方程,可塑性理论开发的,并包括返回映射算法。得出与积分过程一致的切线算子,以确保牛顿-拉夫森法在有限元分析中的计算效率。该算法在Abaqus中作为用户定义的子例程实现。本构模型和计算程序的效率通过对包含通孔并承受面内单轴拉伸载荷的复合材料层板的渐进破坏进行分析来证明。结果表明,预测结果与文献报道的实验数据吻合良好。

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