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Numerical Approach to Damages in a Composite Laminated Plate under a Low-Velocity Impact

机译:低速冲击下复合材料层合板损伤的数值方法

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摘要

This paper presents a numerical analysis of damage evolution process of composite laminated plate under a low-velocity impact using the finite element method and the first-order shear deformation theory. Various types of damages including delamination, matrix cracking, fiber failure and their influences on the mechanical behavior of the plate are studied. A simulation technique is proposed to model the damage initiation and evolution, and a computer program is developed and successfully used for long-fiber reinforced carbon/epoxy composite laminated plate with arbitrary stack sequence and fiber orientation. Validations against experiment results show that the proposed approach is capable of giving accurate prediction of impact damage behavior.
机译:本文利用有限元法和一阶剪切变形理论对复合材料层合板在低速冲击下损伤演化过程进行了数值分析。研究了各种类型的损伤,包括分层,基体开裂,纤维破坏以及它们对板的机械性能的影响。提出了一种模拟技术,对损伤的发生和发展进行建模,并开发了计算机程序,并成功地将其用于具有任意堆叠顺序和纤维取向的长纤维增强碳/环氧树脂复合层压板。针对实验结果的验证表明,所提出的方法能够对冲击破坏行为做出准确的预测。

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