刘新

个人信息Personal Information

副教授

博士生导师

硕士生导师

性别:女

毕业院校:哈尔滨工业大学

学位:博士

所在单位:材料科学与工程学院

学科:航空宇航制造工程. 航空航天力学与工程. 应用与实验力学. 材料学

办公地点:大连理工大学三束实验室4号楼308

联系方式:0411-84706791

电子邮箱:liuxindlut@dlut.edu.cn

扫描关注

论文成果

当前位置: >> 科学研究 >> 论文成果

Microscopic damage mechanisms of fibre reinforced composite laminates subjected to low velocity impact

点击次数:

论文类型:期刊论文

发表时间:2016-01-01

发表刊物:COMPUTATIONAL MATERIALS SCIENCE

收录刊物:SCIE、EI

卷号:111

页面范围:148-156

ISSN号:0927-0256

关键字:Fibre reinforced composite; Low velocity impact; Damage mechanisms; Multiscale modelling; Finite element method (FEM)

摘要:This paper presents an integrated multiscale model for the simulation of fibre reinforced polymeric composite laminate subjected to low velocity impact. The multiscale model is based on the embedded cell method, with detailed microstructure embedded into the macro laminate beneath the impact point, and a transition zone is introduced to link these two scales. Damage model is considered for the fibres and plastic behaviour for the matrix, and cohesive elements are used for the simulation of interface delamination. Both unidirectional and layup embedded cells are considered in the simulation so as to reveal the impact damage mechanisms from monolayer to layup levels. The simulation results indicate matrix cracking is the first damage form which occurs at the bottom of the laminate, and then delamination is induced when the matrix crack propagates to the interface, followed by fibre pull-out and fibre breakage. The simulation results are compared with available experimental results from literatures, with good agreements achieved between them on the damage morphologies. Thus the ability of the presented multiscale model to reveal the damage mechanisms of composite laminate under low velocity impact is validated. (C) 2015 Elsevier B.V. All rights reserved.