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Multiscale analysis of fatigue crack initiation life for unidirectional composite laminates

机译:单向复合材料层板疲劳裂纹萌生寿命的多尺度分析

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摘要

Three dimensional (3D) finite element analysis along with a damage model based on kinetic theory of fracture (KTF) are used to determine the onset of fatigue crack initiation in unidirectional carbon fiber reinforced composites. In addition, the Multicontinuum theory (MCT) and micromechanics are employed separately to enable the assessment of the stress state distribution at the length scale level of the constituents. While the MCT is implemented in the macroscale model formulation, micromechanical analysis of a representative unit cell has been also developed to capture the stress field in the micro length scale level. An ABAQUS (TM) user material (UMAT) subroutine has been developed and used for implementing the formulation. Numerical examples of various tests including tension, three point bending, four point bending, and short beam shear test of a unidirectional (UD) laminate are considered and the results are compared against actual test data. A detailed discussion, challenges and future plans on the applicability of the KTF are concluding this work.
机译:三维(3D)有限元分析以及基于断裂动力学理论(KTF)的损伤模型用于确定单向碳纤维增强复合材料疲劳裂纹萌生的开始。另外,多连续谱理论(MCT)和微力学被分开使用,以使得能够在构件的长度尺度水平上评估应力状态分布。虽然在宏观模型模型中实施了MCT,但也已经开发出具有代表性的晶胞的微机械分析,以捕获微观长度尺度水平的应力场。已经开发了ABAQUS(TM)用户资料(UMAT)子例程,并将其用于实施配方。考虑了各种测试的数值示例,包括单向(UD)层压板的拉伸,三点弯曲,四点弯曲和短梁剪切测试,并将结果与​​实际测试数据进行比较。关于KTF适用性的详细讨论,挑战和未来计划正在结束这项工作。

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