A simulation method for high-cycle fatigue-driven delamination using a cohesive zone model

被引:70
|
作者
Bak, Brian L. V. [1 ,2 ]
Turon, Albert [3 ]
Lindgaard, Esben [2 ]
Lund, Erik [2 ]
机构
[1] Aalborg Univ, Dept Mech & Mfg Engn, Fibigerstr 16, DK-9220 Aalborg, Denmark
[2] Siemens Wind Power AS, Assensvej 11, DK-9220 Aalborg, Denmark
[3] Univ Girona, Polytech Sch, AMADE, Campus Montilivi S-N, Girona 17071, Spain
关键词
laminated composite structures; fatigue; cohesive zone model; interface elements; delamination; crack propagation simulation; CRACK GROWTH; ELEMENT-ANALYSIS; DAMAGE MODEL; COMPOSITES; DECOMPOSITION; PREDICTION; MESH;
D O I
10.1002/nme.5117
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A novel computational method for simulating fatigue-driven mixed-mode delamination cracks in laminated structures under cyclic loading is presented. The proposed fatigue method is based on linking a cohesive zone model for quasi-static crack growth and a Paris' law-like model described as a function of the energy release rate for the crack growth rate during cyclic loading. The J-integral has been applied to determine the energy release rate. Unlike other cohesive fatigue methods, the proposed method depends only on quasi-static properties and Paris' law parameters without relying on parameter fitting of any kind. The method has been implemented as a zero-thickness eight-node interface element for Abaqus and as a spring element for a simple finite element model in MATLAB. The method has been validated in simulations of mode I, mode II, and mixed-mode crack loading for both self-similar and non-self-similar crack propagation. The method produces highly accurate results compared with currently available methods and is capable of simulating general mixed-mode non-self-similar crack growth problems. Copyright (C) 2015 John Wiley & Sons, Ltd.
引用
收藏
页码:163 / 191
页数:29
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