Application of scaled boundary finite element method for delamination analysis of composite laminates using cohesive zone modelling

被引:15
作者
Garg, Nikhil [1 ]
Prusty, B. Gangadhara [1 ]
Ooi, Ean Tat [2 ]
Song, Chongmin [3 ]
Pearce, Garth [1 ]
Phillips, Andrew W. [4 ]
机构
[1] UNSW Sydney, Sch Mech & Mfg Engn, ARC Training Ctr Automated Manufacture Adv Compos, Sydney, NSW, Australia
[2] Federat Univ, Sch Sci Engn & Informat Technol, Ballarat, Vic 3350, Australia
[3] UNSW Sydney, Sch Civil & Environm Engn, Sydney, NSW, Australia
[4] Def Sci & Technol Grp DST Grp, Maritime Div, Melbourne, Vic, Australia
基金
澳大利亚研究理事会;
关键词
Delamination; Laminated composites; Cohesive zone model; Mixed mode; Scaled boundary finite element method; CRACK-PROPAGATION; CELL METHOD; PROGRESSIVE DELAMINATION; NUMERICAL SIMULATIONS; ACCURATE SIMULATION; GROWTH; LAW; SEPARATION; SINGULARITIES; FORMULATIONS;
D O I
10.1016/j.compstruct.2020.112773
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this paper, the scaled boundary finite element method (SBFEM) is evaluated for two-dimensional delamination analysis of composite laminates. The delamination phenomenon was studied using cohesive zone modelling (CZM). A bi-linear (triangular) traction-separation law was used to describe the interface behaviour, which was modelled using zero-thickness interface elements. Local arc-length solution technique was used to solve the non-linearity due to the interface behaviour. In this research, pure Mode I and Mode II as well as mixed mode delamination studies have been conducted using the SBFEM formulation. A variety of numerical experiments were performed. Good agreement was observed between the SBFEM simulation and the available numerical and experimental results in the open literature. A comparison between the SBFEM and other traditional methods shows that the presented formulation can solve the same physical problem with a reduction in the computational cost by more than half. The study highlights the advantages of SBFEM over other methods for modelling delamination in composite laminates using CZM.
引用
收藏
页数:10
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