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Mixed-mode translaminar fracture of CFRP: Failure analysis and fractography

机译:CFRP混合模式跨板层骨折:失效分析和断口扫描

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摘要

The translaminar fracture behaviour of an IM7/8552 carbon/epoxy material system was investigated under mixed mode loading conditions of G_(II)/G_(total)=0.12, 0.24, 0.46 and 1.00. Fracture tests were performed on cross-ply specimens using a modified compact tension configuration and a specially developed fixture. SEM of the fracture surfaces of failed specimens revealed damage mechanisms specifically caused by the introduction of a mode II component that accompanied a significant increase in the damage zone size. In order to quantify the effect that these mechanisms had on the energy dissipation process, R-curves were generated which suggested that the specimen configuration used here is appropriate for characterising fracture toughness at low proportions of mode II.
机译:在G_(II)/ G_(total)= 0.12、0.24、0.46和1.00的混合模式载荷条件下研究了IM7 / 8552碳/环氧树脂材料系统的层间断裂行为。使用改良的紧凑型张力配置和专门开发的夹具,对交叉层样本进行了断裂测试。失效样品断裂表面的SEM揭示了损伤机理,具体是由于引入了II型组分而引起的,该组分伴随着损伤区大小的显着增加。为了量化这些机制对能量耗散过程的影响,生成了R曲线,这表明此处使用的样本配置适合表征II型低比例断裂韧性。

著录项

  • 来源
    《Composite Structures 》 |2013年第1期| 135-141| 共7页
  • 作者单位

    Department of Aeronautics, Imperial College London, London SW7 2AZ, UK;

    Department of Aeronautics, Imperial College London, London SW7 2AZ, UK;

    Department of Aeronautics, Imperial College London, London SW7 2AZ, UK;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    fracture toughness; notch; damage; fractography;

    机译:断裂韧性缺口;损伤;断层扫描;

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