Progressive failure analysis of bolted single-lap composite joint based on extended finite element method

Zhenqing Wang; Song Zhou; Jifeng Zhang; Xiaodi Wu; Li Min Zhou

doi:10.1016/j.matdes.2011.08.039

Progressive failure analysis of bolted single-lap composite joint based on extended finite element method

Zhenqing Wang, Song Zhou, Jifeng Zhang, Xiaodi Wu, Li Min Zhou

Research output: Journal article publication › Journal article › Academic research › peer-review

45 Citations (Scopus)

Abstract

In this paper, extend finite element method (XFEM) is used to predict the failure of single-lap bolted joints. To simplify calculation of XFEM model, composite laminates of joint are modeled using linear elastic properties. Three-dimensional equivalent material properties are calculated by the MATLAB code written by author. Progressive failure of bolted single-lap composite joint is investigated, and the failure load of joint simulated by XFEM is compared with experiments in literature. Then the influences of geometric parameters on failure load of one bolt single-lap composite joint are studied. Two geometric parameters include plate width-to-hole diameter ratio (W/. D) and the edge-to-hole diameter ratio (E/. D). At last the failure of single-lap joints with one bolt and two bolts are compared.

Original language	English
Pages (from-to)	582-588
Number of pages	7
Journal	Materials and Design
Volume	37
DOIs	https://doi.org/10.1016/j.matdes.2011.08.039
Publication status	Published - 1 May 2012

Keywords

A. Composites
D. Mechanical fastening
H. Failure analysis

ASJC Scopus subject areas

Materials Science(all)
Mechanics of Materials
Mechanical Engineering

More information

10.1016/j.matdes.2011.08.039

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title = "Progressive failure analysis of bolted single-lap composite joint based on extended finite element method",

abstract = "In this paper, extend finite element method (XFEM) is used to predict the failure of single-lap bolted joints. To simplify calculation of XFEM model, composite laminates of joint are modeled using linear elastic properties. Three-dimensional equivalent material properties are calculated by the MATLAB code written by author. Progressive failure of bolted single-lap composite joint is investigated, and the failure load of joint simulated by XFEM is compared with experiments in literature. Then the influences of geometric parameters on failure load of one bolt single-lap composite joint are studied. Two geometric parameters include plate width-to-hole diameter ratio (W/. D) and the edge-to-hole diameter ratio (E/. D). At last the failure of single-lap joints with one bolt and two bolts are compared.",

keywords = "A. Composites, D. Mechanical fastening, H. Failure analysis",

author = "Zhenqing Wang and Song Zhou and Jifeng Zhang and Xiaodi Wu and Zhou, {Li Min}",

year = "2012",

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journal = "International Journal of Materials in Engineering Applications",

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T1 - Progressive failure analysis of bolted single-lap composite joint based on extended finite element method

AU - Wang, Zhenqing

AU - Zhou, Song

AU - Zhang, Jifeng

AU - Wu, Xiaodi

AU - Zhou, Li Min

PY - 2012/5/1

Y1 - 2012/5/1

N2 - In this paper, extend finite element method (XFEM) is used to predict the failure of single-lap bolted joints. To simplify calculation of XFEM model, composite laminates of joint are modeled using linear elastic properties. Three-dimensional equivalent material properties are calculated by the MATLAB code written by author. Progressive failure of bolted single-lap composite joint is investigated, and the failure load of joint simulated by XFEM is compared with experiments in literature. Then the influences of geometric parameters on failure load of one bolt single-lap composite joint are studied. Two geometric parameters include plate width-to-hole diameter ratio (W/. D) and the edge-to-hole diameter ratio (E/. D). At last the failure of single-lap joints with one bolt and two bolts are compared.

AB - In this paper, extend finite element method (XFEM) is used to predict the failure of single-lap bolted joints. To simplify calculation of XFEM model, composite laminates of joint are modeled using linear elastic properties. Three-dimensional equivalent material properties are calculated by the MATLAB code written by author. Progressive failure of bolted single-lap composite joint is investigated, and the failure load of joint simulated by XFEM is compared with experiments in literature. Then the influences of geometric parameters on failure load of one bolt single-lap composite joint are studied. Two geometric parameters include plate width-to-hole diameter ratio (W/. D) and the edge-to-hole diameter ratio (E/. D). At last the failure of single-lap joints with one bolt and two bolts are compared.

KW - A. Composites

KW - D. Mechanical fastening

KW - H. Failure analysis

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U2 - 10.1016/j.matdes.2011.08.039

DO - 10.1016/j.matdes.2011.08.039

M3 - Journal article

SN - 0264-1275

VL - 37

SP - 582

EP - 588

JO - International Journal of Materials in Engineering Applications

JF - International Journal of Materials in Engineering Applications

ER -

Progressive failure analysis of bolted single-lap composite joint based on extended finite element method

Abstract

Keywords

ASJC Scopus subject areas

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