A variational approach for predicting initiation of matrix cracking and induced delamination in symmetric composite laminates under in-plane loading
This paper discusses the formation of matrix cracking and induced delaminations in a [ϕm(2)/ψn(1)]s$[\phi _m^{(2)}/\psi _n^{(1)}]s$ laminate subject to arbitrary in-plane loading using a variational approach. To this end, the effects of delaminations coming from the tips of transverse cracks in the...
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Online Access: | https://doi.org/10.1515/secm-2016-0379 |
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doaj-db5f50452f094594a79a04ec90ecf76b2021-09-05T14:00:32ZengDe GruyterScience and Engineering of Composite Materials0792-12332191-03592018-09-0125585586810.1515/secm-2016-0379A variational approach for predicting initiation of matrix cracking and induced delamination in symmetric composite laminates under in-plane loadingTaghavi Larijani Seyed Siamak0Farrokhabadi Amin1Department of Aerospace Engineering, Semnan University, Semnan, IranDepartment of Mechanical Engineering, Tarbiat Modares University, Tehran 14115-111, Iran, Phone: +982182883938This paper discusses the formation of matrix cracking and induced delaminations in a [ϕm(2)/ψn(1)]s$[\phi _m^{(2)}/\psi _n^{(1)}]s$ laminate subject to arbitrary in-plane loading using a variational approach. To this end, the effects of delaminations coming from the tips of transverse cracks in the middle sublaminates are considered to specify the critical crack density points and finally understand which modes of damage are prospects for various lay-ups in the presence of transverse cracks as well as induced delamination. After deriving a very good approximation of the principle of minimum complementary energy by considering complex equations, the stress fields are provided. In this analysis, a unit cell in the ply level of a composite laminate containing both matrix cracking and delamination is considered. Then, the values of the admissible stresses and compliance of cracked laminate are employed to evaluate the energy release rate of each mentioned damage mode. Eventually, the graphs for different lay-ups in such symmetric laminate are drawn, which indicate important points for designers in practical applications. Afterwards, the effects of thickness on the dislocation of critical crack density points are checked. It can be emphasized that the current approach opens a new insight for perceiving the composites’ structural behavior in vulnerable positions.https://doi.org/10.1515/secm-2016-0379induced delaminationmatrix crackingtransverse cracksvariational approach |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Taghavi Larijani Seyed Siamak Farrokhabadi Amin |
spellingShingle |
Taghavi Larijani Seyed Siamak Farrokhabadi Amin A variational approach for predicting initiation of matrix cracking and induced delamination in symmetric composite laminates under in-plane loading Science and Engineering of Composite Materials induced delamination matrix cracking transverse cracks variational approach |
author_facet |
Taghavi Larijani Seyed Siamak Farrokhabadi Amin |
author_sort |
Taghavi Larijani Seyed Siamak |
title |
A variational approach for predicting initiation of matrix cracking and induced delamination in symmetric composite laminates under in-plane loading |
title_short |
A variational approach for predicting initiation of matrix cracking and induced delamination in symmetric composite laminates under in-plane loading |
title_full |
A variational approach for predicting initiation of matrix cracking and induced delamination in symmetric composite laminates under in-plane loading |
title_fullStr |
A variational approach for predicting initiation of matrix cracking and induced delamination in symmetric composite laminates under in-plane loading |
title_full_unstemmed |
A variational approach for predicting initiation of matrix cracking and induced delamination in symmetric composite laminates under in-plane loading |
title_sort |
variational approach for predicting initiation of matrix cracking and induced delamination in symmetric composite laminates under in-plane loading |
publisher |
De Gruyter |
series |
Science and Engineering of Composite Materials |
issn |
0792-1233 2191-0359 |
publishDate |
2018-09-01 |
description |
This paper discusses the formation of matrix cracking and induced delaminations in a [ϕm(2)/ψn(1)]s$[\phi _m^{(2)}/\psi _n^{(1)}]s$ laminate subject to arbitrary in-plane loading using a variational approach. To this end, the effects of delaminations coming from the tips of transverse cracks in the middle sublaminates are considered to specify the critical crack density points and finally understand which modes of damage are prospects for various lay-ups in the presence of transverse cracks as well as induced delamination. After deriving a very good approximation of the principle of minimum complementary energy by considering complex equations, the stress fields are provided. In this analysis, a unit cell in the ply level of a composite laminate containing both matrix cracking and delamination is considered. Then, the values of the admissible stresses and compliance of cracked laminate are employed to evaluate the energy release rate of each mentioned damage mode. Eventually, the graphs for different lay-ups in such symmetric laminate are drawn, which indicate important points for designers in practical applications. Afterwards, the effects of thickness on the dislocation of critical crack density points are checked. It can be emphasized that the current approach opens a new insight for perceiving the composites’ structural behavior in vulnerable positions. |
topic |
induced delamination matrix cracking transverse cracks variational approach |
url |
https://doi.org/10.1515/secm-2016-0379 |
work_keys_str_mv |
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