...
首页> 外文期刊>Computational Materials Science >Analysis of microstructure damage in carbon/epoxy composites using FEM
【24h】

Analysis of microstructure damage in carbon/epoxy composites using FEM

机译:碳/环氧复合材料微观结构损伤的有限元分析

获取原文
获取原文并翻译 | 示例

摘要

This work presents a numerical analysis of damage of composite materials with polymeric matrix reinforced with carbon fibres subject to static tension. Verification of numerical analyses was conducted with experimental methods - strength tests and microstructural observations. The methodologies applied were: the material damage modelling methodology based on XFEM (eXtended Finite Element Method) and contact interactions in a fibre-matrix connection layer using the CZM method (Cohesive Zone Method - Surface-based Cohesive Behaviour). ABAQUS/Standard software was the applied numerical tool. Microstructural analysis and numerical simulations indicate the fact that initiation of composite material damage takes place at the interface as a result of cracking and loss of fibre/matrix connection. This results in weakening of the composite microstructure in this area through the initiation of a reinforcement cracking process, which leads to further structural degradation, consisting in propagation of matrix cracking and, as a result, complete damage of the composite structure. The presented research of carbon/epoxy composite damage confirmed the adequacy of the prepared numerical model.
机译:这项工作提出了对碳纤维增强的聚合物基体承受静态张力的复合材料的损伤的数值分析。数值分析的验证是通过实验方法进行的-强度测试和微观结构观察。应用的方法是:基于XFEM(扩展有限元法)的材料损伤建模方法,以及使用CZM方法(内聚区方法-基于表面的内聚行为)在纤维-基体连接层中的接触相互作用。 ABAQUS / Standard软件是应用的数值工具。微观结构分析和数值模拟表明,由于开裂和纤维/基体连接的损失,复合材料的破坏始于界面。这会通过启动增强裂纹过程而导致该区域复合材料微结构的削弱,从而导致进一步的结构退化,包括基体裂纹的扩展,从而完全破坏复合结构。提出的碳/环氧复合材料损伤的研究证实了所制备数值模型的适当性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号