胡小飞

个人信息Personal Information

副教授

博士生导师

硕士生导师

主要任职:Associate Professor

性别:男

毕业院校:大连理工大学

学位:博士

所在单位:力学与航空航天学院

学科:固体力学. 计算力学. 工程力学

办公地点:力学系楼401-1

联系方式:hxf@dlut.edu.cn

电子邮箱:hxf@dlut.edu.cn

扫描关注

论文成果

当前位置: 胡小飞博士 >> 科学研究 >> 论文成果

Integrated XFEM-CE analysis of delamination migration in multi-directional composite laminates

点击次数:

论文类型:期刊论文

发表时间:2016-11-01

发表刊物:COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING

收录刊物:SCIE、EI、Scopus

卷号:90

页面范围:161-173

ISSN号:1359-835X

关键字:Delamination migration; Crack interactions; XFEM; Cohesive elements; Progressive damage; Composite laminates

摘要:Progressive damage and failure in composites are generally complex and involve multiple interacting failure modes. Depending on factors such as lay-up sequence, loading and specimen configurations, failure may be dominated by extensive matrix crack-delamination interactions, which are very difficult to model accurately. The present study further develops an integrated extended finite element method (XFEM) and cohesive element (CE) method for three-dimensional (3D) delamination migration in multi-directional composite laminates, and validates the results with experiment performed on a double-cantilever beam (DCB). The plies are modeled by using XFEM brick elements, while the interfaces are modeled using CEs. The interaction between matrix crack and delamination is achieved by enriching the nodes of cohesive element. The mechanisms of matrix fracture and delamination migration are explained and discussed. Matrix crack initiation and propagation can be predicted and delamination migration is also observed in the results. The algorithm provides for the prediction of matrix crack angles through the ply thickness. The proposed method provides a platform for the realistic simulation of progressive failure of composite laminates. (C) 2016 Elsevier Ltd. All rights reserved.