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Characterization of Composite Laminate Lightning Strike Thermal-Mechanical Coupling Damage Based on Progressive Damage Model

机译:基于渐进式损伤模型的复合层压雷击热机械耦合损伤的表征

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For the sake of characterizing composite lightning strike coupling damage, based on the method of continuum damage mechanics (CDM) and phenomenological analysis, stiffness matrix progressive damage degradation model of composite laminate structure with lightning strike ablation damage and mechanical impact damage was constructed in this paper. An effective three-dimensional finite element model (FEM) of composite laminate structure with lightning strike coupling damage has been established based on ABAQUS software, and combine UMAT subroutine, which was coded by stiffness matrix progressive damage degradation model, strength prediction and failure process analysis were accomplished under tensile load. Excellent agreement between experimental data and numerical results is observed. The results indicate that models constructed in this paper can characterize the lightning strike coupling damage well, and have the abilities to predict the residual strength and failure process of composite laminate with lightning strike coupling damage.
机译:为了表征复合雷击耦合耦合损坏,基于连续损伤力学(CDM)和现象学分析,在本文中构建了具有雷击烧灼损坏的复合层压板结构的刚度矩阵逐行损伤损伤和机械冲击损坏。基于ABAQUS软件建立了一种具有雷击耦合耦合损坏的复合层压板结构的有效三维有限元模型(FEM),并结合Umat子程序,由刚度矩阵逐行损伤降解模型,强度预测和故障过程分析进行编码在拉伸载荷下完成。观察到实验数据与数值结果之间的良好协议。结果表明,本文构建的模型可以呈现雷击耦合损坏良好,并且具有预测复合层压板的容量强度和故障过程,具有雷击耦合损坏。

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