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Progressive Axial Crushing of Composite Laminates: A Comparison Between LS-DYNA Continuum Damage Models

机译:复合材料层板的渐进轴向压碎:LS-DYNA连续体损伤模型之间的比较

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We are presenting a detailed comparison of well-established intra-laminar materialdamage models to assess predictive capabilities and the influence of additional nonphysicalparameters with regards to compressive damage behavior and axial crushingof Carbon Fiber Reinforced Polymers (CFRPs) structures. Implemented in thecommercial explicit Finite Element (FE) software LS-DYNA, three material modelsMAT058, MAT219 and MAT261 are applied to a range of characteristic tests thatlead towards the axial crushing of quasi-isotropic IM7/8552 CFRP laminates. Thefindings of this study aid in fully understanding the efficient use of built-in intralaminardamage models for CFRP structures under compressive loading. It furtherleads towards robust and reliable calibration schemes to determine typically usedparameters in crashworthiness simulations.
机译:我们将对成熟的层内材料进行详细的比较 损害模型以评估预测能力和其他非物质因素的影响 关于压缩破坏行为和轴向压溃的参数 碳纤维增强聚合物(CFRP)结构的研究。实施于 商业显式有限元(FE)软件LS-DYNA,三种材料模型 MAT058,MAT219和MAT261适用于一系列特性测试,这些测试 导致准各向同性的IM7 / 8552 CFRP层压板的轴向破碎。这 这项研究的发现有助于充分了解内置椎板的有效使用 压缩荷载下CFRP结构的损伤模型。它进一步 导致强大而可靠的校准方案来确定通常使用的 耐撞性仿真中的参数。

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