个人信息Personal Information
副教授
博士生导师
硕士生导师
性别:男
毕业院校:北京航空航天大学
学位:博士
所在单位:力学与航空航天学院
学科:飞行器设计. 航空航天力学与工程. 工程力学
办公地点:综合实验1号楼409B
联系方式:+86 411 84706213
电子邮箱:yangl@dlut.edu.cn
Micromechanical modelling and simulation of unidirectional fibre-reinforced composite under shear loading
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论文类型:期刊论文
发表时间:2015-01-01
发表刊物:JOURNAL OF REINFORCED PLASTICS AND COMPOSITES
收录刊物:SCIE、EI、Scopus
卷号:34
期号:1
页面范围:72-83
ISSN号:0731-6844
关键字:Fibre reinforced polymer; transverse shear; in-plane shear; representative volume element; failure mechanism
摘要:In this paper, micromechanical modelling and simulation were performed for unidirectional fibre reinforced composites subjected to transverse and in-plane shear by finite element method. Representative volume element consisting of fibre, matrix and interface was established for the simulation, considering random fibre distribution. The two dominant damage mechanisms of fibre reinforced composites, matrix plastic deformation and interfacial debonding were taken into account in the simulation. Periodic boundary conditions were applied to the representative volume elements. The simulation results indicate that the failure behaviour of the composites under transverse shear is dominated by matrix plastic damage, while the in-plane shear damage is initiated by interfacial debonding and then ultimate failure is caused by matrix damage. Fibre distribution is found to have a more significant effect on the failure behaviour of the composites under transverse shear than in-plane shear. The predicted in-plane shear strength and failure strain show reasonable agreement with the experimental results.