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A computational continuum damage mechanics model for predicting transverse cracking and splitting evolution in open hole cross-ply composite laminates

机译:用于预测裸眼交叉复合层合板的横向开裂和开裂发展的连续计算损伤力学模型

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摘要

The present study focuses on a computational constitutive model which predicts the matrix cracking evolution and fibre breakage in cross-ply composite laminates with open hole under in-plane loading. To consider the effects of matrix cracking on the nonlinear response of laminates, a simplified crack density based model is applied which evaluates the representative damage parameters of matrix cracking. Furthermore, a developed subroutine based on continuum damage mechanics concepts is applied in ANSYS code which is capable to consider the transverse cracking/splitting evolution and predict the final failure load of mentioned laminate under monotonic loading in a progressive damage analyses. It is shown that the obtained stress-strain behaviours and the damage evaluation of considered laminates are in good agreement with the available experimental results.
机译:本研究着重于计算本构模型,该模型可预测面内载荷作用下具有开孔的交叉复合层压板的基体开裂演变和纤维断裂。为了考虑基体开裂对层合板非线性响应的影响,采用简化的基于裂纹密度的模型来评估基体开裂的代表性损伤参数。此外,在ANSYS代码中应用了基于连续损伤力学概念的已开发子例程,该子例程能够在进行渐进式损伤分析时考虑横向开裂/分裂发展并预测单调载荷下所述层压板的最终破坏载荷。结果表明,所获得的应力-应变行为和所考虑层压板的损伤评估与可得的实验结果非常吻合。

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