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Postbuckling Analysis of Laminate with Delamination Based on the Improved Damage Model of 2-D

机译:基于改进的二维损伤模型的分层脱层后屈曲分析

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The paper presents the compatibility relation of displacement, strain energy expression, and the formulations of Finite Element Method in the transitional region for the improved damage model of 2-D delamination~[1]. The postbuckling behaviors of composite laminated plate with a circular delamination are analyzed. Results show that the model mainly improves computational results of energy release rates in the delamination front. The model should only be used in a narrow region near the crack-tip and the normal Mindlin model in other regions. It leads to little increase in the amount of computation, but significant improvement in the results.
机译:提出了改进的二维分层〜1损伤模型的过渡区域位移,应变能表达式的相容性关系以及有限元方法的公式。分析了圆形分层复合层压板的屈曲后行为。结果表明,该模型主要提高了分层前沿能量释放速率的计算结果。该模型仅应在裂纹尖端附近的狭窄区域中使用,而其他区域则应使用常规Mindlin模型。它导致计算量的增加很少,但是结果却有了明显的改善。

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