首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于损伤力学的疲劳全寿命数值预估方法
引用本文:石欣桐,杨宇,肖迎春,黄博,冯威.基于损伤力学的疲劳全寿命数值预估方法[J].科学技术与工程,2024,24(11):4776-4783.
作者姓名:石欣桐  杨宇  肖迎春  黄博  冯威
作者单位:中国飞机强度研究所;西北工业大学
基金项目:国家自然科学基金(12202336)
摘    要:疲劳失效是影响结构件使用安全的主要问题,对疲劳寿命进行准确预测具有重要的工程意义。基于采用平均应力修正的损伤力学演化模型,结合有限元法建立了同时考虑裂纹萌生与扩展的疲劳全寿命数值预估方法。为了验证该方法,开展了不同应力水平下铝合金开孔板试样疲劳试验与疲劳数值模拟。结果表明,基于所建立的疲劳数值分析方法能够有效预测开孔板裂纹扩展过程及疲劳全寿命,预测寿命误差带在两倍以内。

关 键 词:损伤力学    疲劳  ?  寿命预估  ?  平均应力
收稿时间:2023/4/17 0:00:00
修稿时间:2024/4/7 0:00:00

Numerical Method of Fatigue Life Prediction Based on Damage Mechanics
Shi Xintong,Yang Yu,Xiao Yingchun,Huang Bo,Feng Wei.Numerical Method of Fatigue Life Prediction Based on Damage Mechanics[J].Science Technology and Engineering,2024,24(11):4776-4783.
Authors:Shi Xintong  Yang Yu  Xiao Yingchun  Huang Bo  Feng Wei
Institution:Aircraft Strength Research Institute of China
Abstract:Fatigue failure is the main problem affecting the safety of structural members. It is of great engineering significance to predict the fatigue life accurately. Based on the damage evolution model with mean stress correction, a numerical method for fatigue life prediction considering both crack initiation and propagation was established combined with finite element method. To verify this method, fatigue tests and numerical simulations of aluminum alloy plates with holes under different stress levels were carried out. The results show that the crack propagation process and the fatigue lives can be effectively predicted by the proposed fatigue numerical method, and the error band of the predicted lives is less than two times.
Keywords:Damage mechanics  ?  Fatigue  ?  Life prediction  ? ? Mean stress
点击此处可从《科学技术与工程》浏览原始摘要信息
点击此处可从《科学技术与工程》下载免费的PDF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