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Simulation of Composite Laminate with Cohesive Interface Elements Under Low-Velocity Impact Loading

机译:低速冲击载荷下含粘性界面元件的复合材料层板的模拟

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摘要

In this paper, numerical model based on continuum damage mechanics is presented to predict the damage behavior in quasi-isotropic composite laminates under low-velocity impact conditions. Hashin criterion and a gradual degradation scheme are employed to trigger the intra-laminar damage initiation and growth. Additionally, an interface cohesive element is incorporated in the model to predict the inter-laminar delamination damages. A user-defined subroutine VUMAT comprising these constitutive models of intra-laminar and inter-laminar damage is written in FORTRAN and implemented into explicit finite element package ABAQUS. Parametric analysis is performed on quasi-isotropic composite model with different impact energy levels to study the impact velocity-time, velocity-displacement, acceleration-time and acceleration-displacement curves of full and reduced models as well as the damage development of intra-laminar matrix cracking and inter-laminar delamination. Reasonable accord between the numerical simulations and experimental test indicates good prediction of impact damage behavior of the proposed model at low-velocity impact conditions.
机译:本文提出了基于连续损伤力学的数值模型,以预测低速冲击条件下准各向同性复合材料层合板的损伤行为。采用Hashin准则和逐步退化方案来触发层内损伤的引发和生长。另外,在模型中结合了界面粘结元件以预测层间分层损伤。包含这些层内和层间损伤本构模型的用户定义子例程VUMAT用FORTRAN编写,并实现为显式有限元封装ABAQUS。对具有不同冲击能级的准各向同性复合材料模型进行参数分析,以研究完整模型和简化模型的冲击速度-时间,速度-位移,加速度-时间和加速度-位移曲线以及层内损伤的发展。基质开裂和层间分层。数值模拟与实验测试之间的合理吻合表明,该模型在低速冲击条件下的冲击损伤行为的良好预测。

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