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Evaluation of a progressive failure analysis of unstiffened and stiffened composite panels

机译:对未加劲和加劲的复合板的渐进式破坏分析的评估

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摘要

Progressive failure analysis of laminated composite unstiffened and stiffened panels has been carried out in the present investigation. The laminated panels under transverse static loadings in linear and elastic range have been investigated using finite element method. In the finite element analysis of stiffened panels, eight noded isoparametric quadratic elements in association with the three noded curved beam elements has been considered and first order shear deformation theory utilised. An iterative method has been adopted using the various failure theories to predict the first ply failure load. After the first ply failure, the stiffness of failed lamina has been totally discarded from the laminate and remained laminae are considered for further analysis. The progressive failure analysis using Tsai-Wu failure criterion has been implemented into a general-purpose finite element code to predict the failure loading from initial to final stage.
机译:在目前的研究中已经进行了层压复合材料未加筋和加筋板的渐进破坏分析。使用有限元方法研究了在线性和弹性范围内的横向静态载荷下的层压板。在加筋板的有限元分析中,考虑了八个节点的等参二次元以及三个节点的弯曲梁单元,并采用了一阶剪切变形理论。已经采用了一种使用各种失效理论的迭代方法来预测第一层的失效载荷。第一次层破裂后,失效的层板的刚度已从层压板上完全丢弃,保留的层板被考虑作进一步分析。使用蔡-吴故障准则的渐进式故障分析已实施为通用有限元代码,以预测从初始阶段到最终阶段的故障负荷。

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