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Tensile behaviour of anti-symmetric CFRP composite

This paper addresses the response of a 17-ply anti-symmetric carbon/epoxy composite subjected to uniaxial tensile loading. Hashin ply damage model is adopted to describe the damage behaviour of the plies, whereas damage initiation and progression of the interfaces are characterised by mixed-mode coh...

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Main Authors: Wong, King Jye, Gonga, X. J., Aivazzadeh, S., Tamin, Mohd. Nasir
Format: Conference or Workshop Item
Language:English
Published: 2011
Subjects:
TJ Mechanical engineering and machinery
Online Access:http://eprints.utm.my/id/eprint/29430/1/MohdNasirTamin2011_TensileBehaviourofAntiSymmetric.pdf
http://eprints.utm.my/id/eprint/29430/
http://dx.doi.org/10.1016/j.proeng.2011.04.310
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spelling my.utm.294302022-01-31T08:41:26Z http://eprints.utm.my/id/eprint/29430/ Tensile behaviour of anti-symmetric CFRP composite Wong, King Jye Gonga, X. J. Aivazzadeh, S. Tamin, Mohd. Nasir TJ Mechanical engineering and machinery This paper addresses the response of a 17-ply anti-symmetric carbon/epoxy composite subjected to uniaxial tensile loading. Hashin ply damage model is adopted to describe the damage behaviour of the plies, whereas damage initiation and progression of the interfaces are characterised by mixed-mode cohesive damage model. Force displacement curves obtained numerically and experimentally show good agreement. Results show that all laminae and interfaces experience the damage except laminae with 0 o fibre. In addition, damage is concentrated at the tab and central regions of the tensile specimen. Edge delamination is observed in all interfaces. 2011 Conference or Workshop Item PeerReviewed application/pdf en http://eprints.utm.my/id/eprint/29430/1/MohdNasirTamin2011_TensileBehaviourofAntiSymmetric.pdf Wong, King Jye and Gonga, X. J. and Aivazzadeh, S. and Tamin, Mohd. Nasir (2011) Tensile behaviour of anti-symmetric CFRP composite. In: 11th International Conference on the Mechanical Behavior of Material (ICM11), 1 January 2011, Villa Erba, Como, Italy. http://dx.doi.org/10.1016/j.proeng.2011.04.310
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/
language English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Wong, King Jye
Gonga, X. J.
Aivazzadeh, S.
Tamin, Mohd. Nasir
Tensile behaviour of anti-symmetric CFRP composite
description This paper addresses the response of a 17-ply anti-symmetric carbon/epoxy composite subjected to uniaxial tensile loading. Hashin ply damage model is adopted to describe the damage behaviour of the plies, whereas damage initiation and progression of the interfaces are characterised by mixed-mode cohesive damage model. Force displacement curves obtained numerically and experimentally show good agreement. Results show that all laminae and interfaces experience the damage except laminae with 0 o fibre. In addition, damage is concentrated at the tab and central regions of the tensile specimen. Edge delamination is observed in all interfaces.
format Conference or Workshop Item
author Wong, King Jye
Gonga, X. J.
Aivazzadeh, S.
Tamin, Mohd. Nasir
author_facet Wong, King Jye
Gonga, X. J.
Aivazzadeh, S.
Tamin, Mohd. Nasir
author_sort Wong, King Jye
title Tensile behaviour of anti-symmetric CFRP composite
title_short Tensile behaviour of anti-symmetric CFRP composite
title_full Tensile behaviour of anti-symmetric CFRP composite
title_fullStr Tensile behaviour of anti-symmetric CFRP composite
title_full_unstemmed Tensile behaviour of anti-symmetric CFRP composite
title_sort tensile behaviour of anti-symmetric cfrp composite
publishDate 2011
url http://eprints.utm.my/id/eprint/29430/1/MohdNasirTamin2011_TensileBehaviourofAntiSymmetric.pdf
http://eprints.utm.my/id/eprint/29430/
http://dx.doi.org/10.1016/j.proeng.2011.04.310
_version_ 1724073264608706560
score 13.211869

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