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Dynamic finite element analysis of stress and fracture in IM7/8552 monolithic composite laminates under impact loading conditions.

机译:IM7 / 8552整体复合材料层压板在冲击载荷条件下的应力和断裂动态有限元分析。

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摘要

This study used the finite element method to evaluate impact resistance and dynamic stress intensity factors (DSIFs) of the composite laminate, IM7/8552, using the FEA package, ANSYS, to find normalized von Mises stress as well as orthotropic SIFs for the 11 layer laminate. It was performed for six common carbon fibers for this material. An approach was taken to obtain an optimal design for the IM7/8552 composite and was based on the idea that the composition of the laminate such as the fiber orientations within each individual lamina, directly effects the physical properties of the laminate. The last part of this study focused on dynamic fracture analysis for the IM7/8552 multilayered composite laminate. The normalized mode-I DSIF was calculated using results from the ANSYS model. It was found that the higher values of fiber volume fraction yielded better results and that material composition does directly affect resistance to impact loading.
机译:这项研究使用有限元方法使用FEA软件包ANSYS对IM7 / 8552复合层压板的抗冲击性和动态应力强度因子(DSIF)进行了评估,以查找归一化的von Mises应力以及11层的正交各向异性SIF层压板。对于该材料,使用了六种常见的碳纤维。采取了一种方法来获得IM7 / 8552复合材料的最佳设计,该方法基于以下想法:层压板的组成(例如每个单独的薄片内的纤维方向)直接影响层压板的物理性能。本研究的最后一部分着重于IM7 / 8552多层复合层压板的动态断裂分析。使用来自ANSYS模型的结果来计算归一化模式I DSIF。发现较高的纤维体积分数值产生更好的结果,并且材料组成确实直接影响耐冲击负荷。

著录项

  • 作者

    Sampayo, Ines Elvira.;

  • 作者单位

    University of South Alabama.;

  • 授予单位 University of South Alabama.;
  • 学科 Engineering Aerospace.Engineering Mechanical.
  • 学位 M.S.
  • 年度 2010
  • 页码 86 p.
  • 总页数 86
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 药物化学;
  • 关键词

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