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Predicting the matrix cracking formation in symmetric composite laminates subjected to bending loads

机译:预测对称复合材料层合板在弯曲载荷下的基体裂纹形成情况

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摘要

The present study investigates analytically the effects of matrix crack formation on the properties of composite laminates subjected to bending loads, using a crack density-based model. For this purpose, by assuming that the plies prone for matrix cracking are sufficiently thin, the relationships of the stiffness reduction due to matrix cracking formation is applied. Then, by considering the equivalent damaged lamina and using the relationships of classical laminates theory (CLT), the variation of mechanical properties of symmetric laminates in the presence of matrix crack is calculated. In addition, a method is proposed to estimate the fracture toughness caused by the matrix crack in composite laminates by using the concept of finite fracture mechanics and calculating the energy release rate due to a matrix crack in a laminate under bending loading. Finally, the progressive growth of matrix crack in the cross-ply symmetric composite laminates is studied by applying the developed relationships into the nonlinear finite element code. The credibility of the proposed method is verified by comparing the obtained results with those achieved numerically and experimentally.
机译:本研究使用基于裂纹密度的模型,分析研究了基体裂纹形成对复合材料层合板弯曲特性的影响。为此,通过假定易于发生基体裂纹的层足够薄,应用了由于基体裂纹形成而导致的刚度降低的关系。然后,通过考虑等效的受损薄片并利用经典层压板理论(CLT)的关系,计算出存在基体裂纹时对称层压板的力学性能变化。此外,提出了一种利用有限断裂力学的概念来估计复合材料层合板中基体裂纹引起的断裂韧性的方法,并计算了弯曲载荷下层合板中基体裂纹引起的能量释放率。最后,通过将所建立的关系应用于非线性有限元代码中,研究了交叉对称复合层压板中基体裂纹的逐步增长。通过比较所获得的结果与在数值上和实验上获得的结果,验证了所提方法的可靠性。

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