Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE Simulation

Glass fibre-reinforced plastic (GFRP) composite laminates are used in many industries due to their excellent mechanical and thermal properties. However, these materials are prone to the initiation and propagation of delamination crack growth between different plies forming the laminate. The crack pr...

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Main Authors: Hassan Ijaz, Waqas Saleem, Muhammad Zain-ul-abdein, Aqeel Ahmad Taimoor, Abdullah Salmeen Bin Mahfouz
Format: Article
Language:English
Published: Wiley 2018-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2018/2081785
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author Hassan Ijaz
Waqas Saleem
Muhammad Zain-ul-abdein
Aqeel Ahmad Taimoor
Abdullah Salmeen Bin Mahfouz
author_facet Hassan Ijaz
Waqas Saleem
Muhammad Zain-ul-abdein
Aqeel Ahmad Taimoor
Abdullah Salmeen Bin Mahfouz
author_sort Hassan Ijaz
collection DOAJ
description Glass fibre-reinforced plastic (GFRP) composite laminates are used in many industries due to their excellent mechanical and thermal properties. However, these materials are prone to the initiation and propagation of delamination crack growth between different plies forming the laminate. The crack propagation may ultimately result in the failure of GFRP laminates as structural parts. In this research, a comprehensive mathematical model is presented to study the delamination crack growth in GFRP composite laminates under fatigue loading. A classical static damage model proposed by Allix and Ladevèze is modified as a fatigue damage model. Subsequently, the model is implemented in commercial finite element software via UMAT subroutine. The results obtained by the finite element simulations verify the experimental findings of Kenane and Benzeggagh for the fatigue crack growth in GFRP composite laminates.
format Article
id doaj-art-a8e5ebc7753c4c0a82a35ce15b89c80e
institution Kabale University
issn 1687-5966
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language English
publishDate 2018-01-01
publisher Wiley
record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-a8e5ebc7753c4c0a82a35ce15b89c80e2025-02-03T01:30:34ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742018-01-01201810.1155/2018/20817852081785Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE SimulationHassan Ijaz0Waqas Saleem1Muhammad Zain-ul-abdein2Aqeel Ahmad Taimoor3Abdullah Salmeen Bin Mahfouz4Department of Mechanical Engineering, University of Jeddah, Jeddah, Saudi ArabiaDepartment of Mechanical Engineering, University of Jeddah, Jeddah, Saudi ArabiaDepartment of Mechanical Engineering, University of Jeddah, Jeddah, Saudi ArabiaDepartment of Chemical and Materials Engineering, King Abdulaziz University, Jeddah, Saudi ArabiaDepartment of Chemical and Materials Engineering, University of Jeddah, Jeddah, Saudi ArabiaGlass fibre-reinforced plastic (GFRP) composite laminates are used in many industries due to their excellent mechanical and thermal properties. However, these materials are prone to the initiation and propagation of delamination crack growth between different plies forming the laminate. The crack propagation may ultimately result in the failure of GFRP laminates as structural parts. In this research, a comprehensive mathematical model is presented to study the delamination crack growth in GFRP composite laminates under fatigue loading. A classical static damage model proposed by Allix and Ladevèze is modified as a fatigue damage model. Subsequently, the model is implemented in commercial finite element software via UMAT subroutine. The results obtained by the finite element simulations verify the experimental findings of Kenane and Benzeggagh for the fatigue crack growth in GFRP composite laminates.http://dx.doi.org/10.1155/2018/2081785
spellingShingle Hassan Ijaz
Waqas Saleem
Muhammad Zain-ul-abdein
Aqeel Ahmad Taimoor
Abdullah Salmeen Bin Mahfouz
Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE Simulation
International Journal of Aerospace Engineering
title Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE Simulation
title_full Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE Simulation
title_fullStr Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE Simulation
title_full_unstemmed Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE Simulation
title_short Fatigue Delamination Crack Growth in GFRP Composite Laminates: Mathematical Modelling and FE Simulation
title_sort fatigue delamination crack growth in gfrp composite laminates mathematical modelling and fe simulation
url http://dx.doi.org/10.1155/2018/2081785
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