首页 | 本学科首页   官方微博 | 高级检索  
     

一种可用于复合材料寿命预测的非线性疲劳损伤累积模型
引用本文:穆朋刚,万小朋,赵美英. 一种可用于复合材料寿命预测的非线性疲劳损伤累积模型[J]. 机械科学与技术, 2010, 0(4)
作者姓名:穆朋刚  万小朋  赵美英
作者单位:西北工业大学航空学院;
摘    要:结合试验数据,提出了一种含有3个待定参数的非线性疲劳损伤累积模型,该模型能够描述复合材料结构疲劳损伤扩展3个阶段,即可以模拟初始循环载荷的损伤快速增长阶段、达到特征损伤状态时的缓慢增长阶段及断裂前损伤快速扩展的阶段。通过算例验证:本文模型与试验数据吻合性较好,可用于对复合材料结构疲劳寿命进行预测及损伤评估。

关 键 词:复合材料  寿命预测  疲劳  损伤累积

A Nonlinear Fatigue Damage Model for Life Prediction of Composite Laminates
Mu Penggang,Wan Xiaopeng,Zhao Meiying. A Nonlinear Fatigue Damage Model for Life Prediction of Composite Laminates[J]. Mechanical Science and Technology for Aerospace Engineering, 2010, 0(4)
Authors:Mu Penggang  Wan Xiaopeng  Zhao Meiying
Affiliation:Mu Penggang,Wan Xiaopeng,Zhao Meiying
Abstract:A nonlinear cumulative damage model based on fatigue data for composite laminates is presented.Using residual strength or residual stiffness,the proposed model with three unknown parameters can simulate the three stages of a characteristic of fatigue damage growth,i.e.the quick growth in early life,the damage growing steadily in the middle of the life and the damage growing rapidly near the fracture.Several experimental data are used to verify this model,and the results indicate that the model describes the...
Keywords:fatigue  cumulative damage  composite laminates  life prediction  
本文献已被 CNKI 等数据库收录!
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