Thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid

This paper aims to propose a temperature-dependent cohesive model to predict the delamination of dissimilar metal–composite material hybrid under Mode-I and Mode-II delamination. Commercial nonlinear finite element (FE) code LS-DYNA was used to simulate the material and cohesive model of hybrid alum...

Full description

Saved in:
Bibliographic Details
Main Authors: Chow, Zhen Pei, Ahmad, Zaini, Wong, King Jye, Koloor, Seyed Saeid Rahimian
Format: Article
Published: MDPI AG 2021
Subjects:
Online Access:http://eprints.utm.my/id/eprint/94960/
http://dx.doi.org/10.3390/polym13040492
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Universiti Teknologi Malaysia
id my.utm.94960
record_format eprints
spelling my.utm.949602022-04-29T22:22:51Z http://eprints.utm.my/id/eprint/94960/ Thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid Chow, Zhen Pei Ahmad, Zaini Wong, King Jye Koloor, Seyed Saeid Rahimian TJ Mechanical engineering and machinery This paper aims to propose a temperature-dependent cohesive model to predict the delamination of dissimilar metal–composite material hybrid under Mode-I and Mode-II delamination. Commercial nonlinear finite element (FE) code LS-DYNA was used to simulate the material and cohesive model of hybrid aluminium–glass fibre-reinforced polymer (GFRP) laminate. For an accurate representation of the Mode-I and Mode-II delamination between aluminium and GFRP laminates, cohesive zone modelling with bilinear traction separation law was implemented. Cohesive zone properties at different temperatures were obtained by applying trends of experimental results from double cantilever beam and end notched flexural tests. Results from experimental tests were compared with simulation results at 30, 70 and 110 °C to verify the validity of the model. Mode-I and Mode-II FE models compared to experimental tests show a good correlation of 5.73% and 7.26% discrepancy, respectively. Crack front stress distribution at 30 °C is characterised by a smooth gradual decrease in Mode-I stress from the centre to the edge of the specimen. At 70 °C, the entire crack front reaches the maximum Mode-I stress with the exception of much lower stress build-up at the specimen’s edge. On the other hand, the Mode-II stress increases progressively from the centre to the edge at 30 °C. At 70 °C, uniform low stress is built up along the crack front with the exception of significantly higher stress concentrated only at the free edge. At 110 °C, the stress distribution for both modes transforms back to the similar profile, as observed in the 30 °C case. MDPI AG 2021 Article PeerReviewed Chow, Zhen Pei and Ahmad, Zaini and Wong, King Jye and Koloor, Seyed Saeid Rahimian (2021) Thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid. Polymers, 13 (4). pp. 1-19. ISSN 2073-4360 http://dx.doi.org/10.3390/polym13040492
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Chow, Zhen Pei
Ahmad, Zaini
Wong, King Jye
Koloor, Seyed Saeid Rahimian
Thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid
description This paper aims to propose a temperature-dependent cohesive model to predict the delamination of dissimilar metal–composite material hybrid under Mode-I and Mode-II delamination. Commercial nonlinear finite element (FE) code LS-DYNA was used to simulate the material and cohesive model of hybrid aluminium–glass fibre-reinforced polymer (GFRP) laminate. For an accurate representation of the Mode-I and Mode-II delamination between aluminium and GFRP laminates, cohesive zone modelling with bilinear traction separation law was implemented. Cohesive zone properties at different temperatures were obtained by applying trends of experimental results from double cantilever beam and end notched flexural tests. Results from experimental tests were compared with simulation results at 30, 70 and 110 °C to verify the validity of the model. Mode-I and Mode-II FE models compared to experimental tests show a good correlation of 5.73% and 7.26% discrepancy, respectively. Crack front stress distribution at 30 °C is characterised by a smooth gradual decrease in Mode-I stress from the centre to the edge of the specimen. At 70 °C, the entire crack front reaches the maximum Mode-I stress with the exception of much lower stress build-up at the specimen’s edge. On the other hand, the Mode-II stress increases progressively from the centre to the edge at 30 °C. At 70 °C, uniform low stress is built up along the crack front with the exception of significantly higher stress concentrated only at the free edge. At 110 °C, the stress distribution for both modes transforms back to the similar profile, as observed in the 30 °C case.
format Article
author Chow, Zhen Pei
Ahmad, Zaini
Wong, King Jye
Koloor, Seyed Saeid Rahimian
author_facet Chow, Zhen Pei
Ahmad, Zaini
Wong, King Jye
Koloor, Seyed Saeid Rahimian
author_sort Chow, Zhen Pei
title Thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid
title_short Thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid
title_full Thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid
title_fullStr Thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid
title_full_unstemmed Thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid
title_sort thermal delamination modelling and evaluation of aluminium–glass fibre-reinforced polymer hybrid
publisher MDPI AG
publishDate 2021
url http://eprints.utm.my/id/eprint/94960/
http://dx.doi.org/10.3390/polym13040492
_version_ 1732945415108558848