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首页> 外文期刊>Fatigue & fracture of engineering materials and structures >Progressive damage analyses of angle-ply laminates exhibiting free edge effects using continuum damage mechanics with layer-wise finite element method
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Progressive damage analyses of angle-ply laminates exhibiting free edge effects using continuum damage mechanics with layer-wise finite element method

机译:使用连续损伤力学的分层有限元方法,对表现出自由边缘效应的角膜层板进行渐进式损伤分析

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摘要

Capability of continuum damage mechanics (CDM) to predict the damage mechanism evolution of composite laminates has rarely been carried out, and most of the previous CDM works mainly focused on the overall response of the laminates. In this paper, progressive damage and overall response of the composite laminates under quasi-static, monotonic increasing loading are investigated using three-dimensional (3D) CDM implementation in a finite element method that is based on the layer-wise laminate plate theory. In the damage formulation, each composite ply is treated as a homogeneous or-thotropic material exhibiting orthotropic damage in the form of distributed microscopic cracks that are normal to the three principal material directions. The progressive damage of different angle-ply composite laminates under quasi-static loading that exhibit free edge effects is investigated. It is shown that using CDM global behaviour and various damage mechanisms affected by the complex nature of free edges can be qualitatively well predicted.
机译:连续损伤力学(CDM)预测复合材料层压板损伤机理演变的能力很少得到实现,并且以前的大多数CDM工作主要集中在层压板的整体响应上。在本文中,在基于层状层压板理论的有限元方法中,使用三维(3D)CDM实现,研究了复合层压板在准静态,单调增加载荷下的渐进式损伤和整体响应。在损伤配方中,将每个复合层视为均质的正交异性材料,以正交于三个主要材料方向的分布的微观裂纹的形式表现出正交异性损伤。研究了在表现出自由边缘效应的准静态载荷下不同角度层合复合材料层压板的渐进损伤。结果表明,使用CDM的整体行为和受自由边缘复杂性影响的各种破坏机制可以在质量上得到很好的预测。

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