Fatigue Life Prediction of Composite Laminate

被引：1

作者：

Liu Jun ^{[1
]}

Zhang Fengpeng ^{[2
]}

机构：

[1] Northeastern Univ, Sch Sci, Shenyang, Liaoning Provin, Peoples R China

[2] Northeastern Univ, Coll Resources & Civil Engn, Shenyang, Peoples R China

来源：

ADVANCED MANUFACTURING TECHNOLOGY, PTS 1-4 | 2012年 / 472-475卷

关键词：

composites; laminates; fatigue life; damage;

D O I：

10.4028/www.scientific.net/AMR.472-475.591

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Based on the accumulating fatigue damage model, with single ply plate theory and experiment data as the foundation, consider the interaction between adjacent layer and material degradation, a kind of fatigue life prediction method of fiber reinforced composite laminates is developed. The stiffness decline of each ply during cyclic loading is determined by the fatigue damage variable and the load amplitude and the fatigue life of any laminates can be predicted using the fatigue properties of single ply plate. Using this method a 3D Finite element model is established by ABAQUS software and the fatigue life and the fatigue damage evolution of a T300 / QY8911 laminats are analyzed, the results are more closer to the experimental results.

引用

页码：591 / +

页数：2

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