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Failure mechanisms of cross-ply carbon fiber reinforced polymer laminates under longitudinal compression with experimental and computational analyses

机译:交叉层碳纤维增强聚合物层压板在纵向压缩下的破坏机理及实验和计算分析

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摘要

This study investigates the failure mechanisms of cross-ply laminates subjected to longitudinal compressive loading. A sequence of failure initiation and propagation process is observed based on optical microscopy images of failed specimens. Specifically, the failure process in the cross-ply laminates involves a combination of four failure mechanisms: fiber kinking, delamination, matrix cracking, and fiber/matrix splitting. We find that the kink-bands in the middle 0 degrees plies of the cross-ply laminates most often show a wedge shape and the angle of matrix cracks in the 90 degrees plies is slightly larger than that of pure 90 degrees plies. The reason has been attributed to the constraining effects by the adjacent plies. The next focus of this study is to propose hybrid micro-macro models to more systematically study the failure mechanisms of the cross-ply laminates. We show that these models accurately predict the combined failure modes of the cross-ply laminates and enable us to closely investigate the interactions of different failure mechanisms. More importantly, the hybrid models achieve great computational efficiency compared to full-scale microstructural models. The combined experimental and computational analyses presented here provide a new level of understanding of the kink-band morphology and damage mechanisms in the cross-ply laminates.
机译:这项研究调查了承受纵向压缩载荷的交叉层压板的破坏机理。基于失败的标本的光学显微镜图像,观察到一系列的失败开始和传播过程。具体而言,交叉层压板的破坏过程涉及四种破坏机制的组合:纤维扭结,分层,基体开裂和纤维/基体分裂。我们发现,交叉铺层层压板中间0度层的扭结带通常呈楔形,并且90度层的基体裂纹夹角略大于纯90度层。原因归因于相邻层的约束作用。这项研究的下一个重点是提出混合微宏模型,以更系统地研究交叉层压板的破坏机理。我们表明,这些模型可以准确预测交叉层压板的组合破坏模式,并使我们能够密切研究不同破坏机制的相互作用。更重要的是,与全尺寸微观结构模型相比,混合模型实现了很高的计算效率。本文介绍的实验和计算分析相结合,使人们对交叉层压板的扭结带形态和损伤机理有了新的认识。

著录项

  • 来源
    《Composites》 |2019年第15期|147-160|共14页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Coll Energy & Power Engn, Nanjing, Jiangsu, Peoples R China|Ford Motor Co, Dept Mat Mfg, Dearborn, MI 48124 USA;

    Ohio State Univ, Coll Engn, Columbus, OH 43212 USA|Ford Motor Co, Dept Mat Mfg, Dearborn, MI 48124 USA;

    Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Coll Energy & Power Engn, Nanjing, Jiangsu, Peoples R China;

    Northwestern Univ, Dept Civil & Environm Engn, 2145 Sheridan Rd, Evanston, IL 60208 USA;

    Chongqing Univ, State Key Lab Mech Transmiss, Chongqing, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, Jiangsu Prov Key Lab Aerosp Power Syst, Coll Energy & Power Engn, Nanjing, Jiangsu, Peoples R China;

    Univ Michigan, Coll Engn & Comp Sci, Dearborn, MI 48128 USA;

    Ford Motor Co, Dept Mat Mfg, Dearborn, MI 48124 USA;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Cross-ply laminates; Longitudinal compression; Kink band; Constraining effect; Hybrid micro-macro model;

    机译:交叉层压板;纵向压缩;扭结带;约束效果;混合微宏模型;

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