基于渐进损伤有限元的复材厚板连接分析
DOI:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:


A Study of Thick Composite Laminates Joints Based on Progressive Failure FEM Analysis
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    针对复合材料厚板连接件,建立三维累积损伤有限元模型预测复合材料厚板连接件的挤压性能。对复合材料层板中的纤维失效、基体失效和分层等损伤类型进行分析模拟,预测厚板连接件的破坏模式及损伤扩展过程,并分析尺寸参数与复材厚层合板连接强度的关系。

    Abstract:

    A three-dimensional progressive damage model was set up for predicting the bearing performance of thick composite laminates under tensile loading. Analyzing and simulating the fibre damage, matrix damage and delamination. The 3D model has the capability of assessing the ultimate bearing strength of joints and simulating the whole process of damage initiation, propagation and catastrophic failure of the structure. The finite element method could also be used to predict the relationship between structure design parameters and load carrying capabilities.

    参考文献
    相似文献
    引证文献
引用本文

匡国强、叶聪杰.基于渐进损伤有限元的复材厚板连接分析[J].民用飞机设计与研 究,2015(1):32-Kuang Guoqiang、Ye Congjie. A Study of Thick Composite Laminates Joints Based on Progressive Failure FEM Analysis[J]. Civil Aircraft Design and Research,2015,(1):32-. ( in Chinese)

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2015-04-16
  • 出版日期:

微信公众号二维码

手机版网站二维码

我要投稿 投稿指南 联系我们 二维码
TOP