Failure analysis of boron/epoxy composite laminates with square cutouts in various size under uniaxial tension

Composite laminates have received much interest in precise engineering fields such as aerospace and automotive industries. Understanding the failure behaviour of laminated composites is important when designing modern structures, but many studies only focus on laminates without cutouts. In practice,...

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Published in:Journal of Physics: Conference Series
Main Author: Zulkifli M.A.A.; Halim Z.I.A.; Norbani N.A.S.; Mahmud J.
Format: Conference paper
Language:English
Published: IOP Publishing Ltd 2021
Online Access:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85119189358&doi=10.1088%2f1742-6596%2f2051%2f1%2f012062&partnerID=40&md5=3106c0ff76b13e0aa608f1a72c91abaa
id 2-s2.0-85119189358
spelling 2-s2.0-85119189358
Zulkifli M.A.A.; Halim Z.I.A.; Norbani N.A.S.; Mahmud J.
Failure analysis of boron/epoxy composite laminates with square cutouts in various size under uniaxial tension
2021
Journal of Physics: Conference Series
2051
1
10.1088/1742-6596/2051/1/012062
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85119189358&doi=10.1088%2f1742-6596%2f2051%2f1%2f012062&partnerID=40&md5=3106c0ff76b13e0aa608f1a72c91abaa
Composite laminates have received much interest in precise engineering fields such as aerospace and automotive industries. Understanding the failure behaviour of laminated composites is important when designing modern structures, but many studies only focus on laminates without cutouts. In practice, the structures are design with cutouts to accommodate the space for fasteners, such as rivets, screws and bolts. This study analyses the failure behaviour of Boron/Epoxy composite laminates with square cutout of various sizes under uniaxial tension. In this study, failure analysis was performed using a Finite Element Analysis (FEA) software, ANSYS, for laminated composite plates with square cutout. The laminas were arranged in the sequence of [θ4/04/-θ4]s where the fibre angle, θ ranges from 0° to 90°. The failure load was predicted based Maximum stress theory. For better visualisation, failure curves are plotted and analysed. Prior to that, the numerical validation procedure has proved the accuracy of the simulation as the results obtained from analytical approach (Matlab) and simulation (ANSYS) are in close agreement. The failure curves show that the Boron/Epoxy composite laminate has weaken seven times due to the square cutout. Such information is vital when designing a structure. Even though more rigorous research should be conducted, it could not be denied that the current study has contributed significant fundamental knowledge. The novelty of this work is that a new set of failure envelopes for Boron/Epoxy laminates with various cutout sizes was developed. © 2021 Institute of Physics Publishing. All rights reserved.
IOP Publishing Ltd
17426588
English
Conference paper
All Open Access; Gold Open Access
author Zulkifli M.A.A.; Halim Z.I.A.; Norbani N.A.S.; Mahmud J.
spellingShingle Zulkifli M.A.A.; Halim Z.I.A.; Norbani N.A.S.; Mahmud J.
Failure analysis of boron/epoxy composite laminates with square cutouts in various size under uniaxial tension
author_facet Zulkifli M.A.A.; Halim Z.I.A.; Norbani N.A.S.; Mahmud J.
author_sort Zulkifli M.A.A.; Halim Z.I.A.; Norbani N.A.S.; Mahmud J.
title Failure analysis of boron/epoxy composite laminates with square cutouts in various size under uniaxial tension
title_short Failure analysis of boron/epoxy composite laminates with square cutouts in various size under uniaxial tension
title_full Failure analysis of boron/epoxy composite laminates with square cutouts in various size under uniaxial tension
title_fullStr Failure analysis of boron/epoxy composite laminates with square cutouts in various size under uniaxial tension
title_full_unstemmed Failure analysis of boron/epoxy composite laminates with square cutouts in various size under uniaxial tension
title_sort Failure analysis of boron/epoxy composite laminates with square cutouts in various size under uniaxial tension
publishDate 2021
container_title Journal of Physics: Conference Series
container_volume 2051
container_issue 1
doi_str_mv 10.1088/1742-6596/2051/1/012062
url https://www.scopus.com/inward/record.uri?eid=2-s2.0-85119189358&doi=10.1088%2f1742-6596%2f2051%2f1%2f012062&partnerID=40&md5=3106c0ff76b13e0aa608f1a72c91abaa
description Composite laminates have received much interest in precise engineering fields such as aerospace and automotive industries. Understanding the failure behaviour of laminated composites is important when designing modern structures, but many studies only focus on laminates without cutouts. In practice, the structures are design with cutouts to accommodate the space for fasteners, such as rivets, screws and bolts. This study analyses the failure behaviour of Boron/Epoxy composite laminates with square cutout of various sizes under uniaxial tension. In this study, failure analysis was performed using a Finite Element Analysis (FEA) software, ANSYS, for laminated composite plates with square cutout. The laminas were arranged in the sequence of [θ4/04/-θ4]s where the fibre angle, θ ranges from 0° to 90°. The failure load was predicted based Maximum stress theory. For better visualisation, failure curves are plotted and analysed. Prior to that, the numerical validation procedure has proved the accuracy of the simulation as the results obtained from analytical approach (Matlab) and simulation (ANSYS) are in close agreement. The failure curves show that the Boron/Epoxy composite laminate has weaken seven times due to the square cutout. Such information is vital when designing a structure. Even though more rigorous research should be conducted, it could not be denied that the current study has contributed significant fundamental knowledge. The novelty of this work is that a new set of failure envelopes for Boron/Epoxy laminates with various cutout sizes was developed. © 2021 Institute of Physics Publishing. All rights reserved.
publisher IOP Publishing Ltd
issn 17426588
language English
format Conference paper
accesstype All Open Access; Gold Open Access
record_format scopus
collection Scopus
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