首页 | 本学科首页   官方微博 | 高级检索  
     

无网格法模拟复合型疲劳裂纹的扩展
引用本文:袁振, 李子然, 吴长春. 无网格法模拟复合型疲劳裂纹的扩展[J]. 工程力学, 2002, 19(1): 25-28.
作者姓名:袁振  李子然  吴长春
作者单位:中国科技大学力学与机械工程系,安徽,合肥,230026;中国科技大学力学与机械工程系,安徽,合肥,230026;中国科技大学力学与机械工程系,安徽,合肥,230026
基金项目:国家自然科学基金资助项目(19772051)
摘    要:本文提出了用无网格Galerkin法模拟构件在复合变形作用下疲劳裂纹扩展路径并预估其疲劳寿命的方法。该法能够自然模拟疲劳裂纹的扩展,不需要网格重构,避免了裂纹扩展过程中的精度受损。应用无网格数值结果计算了J积分和应力强度因子KIK;按照最大周向应力理论获得了裂纹扩展偏斜角。基于最小应变能密度因子理论,确定了裂纹扩展量Δa,并能获得疲劳载荷的循环周数ΔN。文末对数值模拟结果和实验拟合结果进行了对照。

关 键 词:无网格Galerkin法  疲劳裂纹  裂纹扩展
文章编号:1000-4750(2002)01-025-04
收稿时间:2000-07-10
修稿时间:2001-03-09

SIMULATION OF MIXED MODE FATIGUE CRACK GROWTH BY EFG METHOD
YUAN Zhen, LI Zi-ran, WU Chang-chun. SIMULATION OF MIXED MODE FATIGUE CRACK GROWTH BY EFG METHOD[J]. Engineering Mechanics, 2002, 19(1): 25-28.
Authors:YUAN Zhen  LI Zi-ran  WU Chang-chun
Affiliation:University of Science and Technology of China, Hefei, 230026
Abstract:The element-free Galerkin method for predicting fatigue crack propagation path and structure lifetime under mixed mode loading is presented in this paper. This method is used in order to allow for crack growth without remeshing and the degradation in accuracy with crack propagation in simulation process is overcome successfully. Using the results of a EFG method analysis, the J-integral and stress intensity factors IKand IIK are computed. The crack deflection angle 0F is determined by the criterion of maximum stress in tangential direction. An assumed crack incrementaD, for each computing cycle delivers an estimation for the number of load cycles, ND, using the strain energy density factor theory. Numerical results for a CGS-04-specimen made of Ti-6Al-4V are presented and compared with experimental data.
Keywords:EFG method  fatigue crack  crack growth  
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《工程力学》浏览原始摘要信息
点击此处可从《工程力学》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号