The study of hybrid composite plates under transverse sinusoidal load using ANSYS

Composite materials have been widely used in many applications but understanding their failure behavior is always challenging. For years, numerical investigation has been the effective alternative, even though the underlying theories related to composite materials are complicated. This study aims to...

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Published in:Journal of Physics: Conference Series
Main Author: Azmi N.N.; Nasir M.F.M.; Ayoub G.; Hussain A.K.; Mahmud J.
Format: Conference paper
Language:English
Published: Institute of Physics Publishing 2019
Online Access:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85077790754&doi=10.1088%2f1742-6596%2f1349%2f1%2f012030&partnerID=40&md5=2fe61113482584b4e648922f047d7862
id 2-s2.0-85077790754
spelling 2-s2.0-85077790754
Azmi N.N.; Nasir M.F.M.; Ayoub G.; Hussain A.K.; Mahmud J.
The study of hybrid composite plates under transverse sinusoidal load using ANSYS
2019
Journal of Physics: Conference Series
1349
1
10.1088/1742-6596/1349/1/012030
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85077790754&doi=10.1088%2f1742-6596%2f1349%2f1%2f012030&partnerID=40&md5=2fe61113482584b4e648922f047d7862
Composite materials have been widely used in many applications but understanding their failure behavior is always challenging. For years, numerical investigation has been the effective alternative, even though the underlying theories related to composite materials are complicated. This study aims to investigate the improved strength of hybridization by comparing the failure behavior of glass-epoxy composite laminate and hybrid glass-graphite-epoxy laminate under transverse sinusoidal load. The composite and hybrid composite laminates with various aspect ratios were modelled using ANSYS. The plates were simply supported and transverse sinusoidal load were applied until failure occurs. Initially, numerical validation was performed and the simulated results are found to be close to the 3D elasticity analytical results. In general, most simulated parameters produced error less than 2% and thus proving the reliability of the finite element models and implementation. The first ply failure (FPF) and last ply failure (LPF) curves were plotted to compare the failure trend of glass-epoxy composite laminate and its hybrid laminate. The results showed no significant difference in the FPF trend but hybridization could withstand up to 80% more normalized load in terms of the LPF. In conclusion, the present study has shed new knowledge about the failure behavior of hybrid laminate and thus, this knowledge could be applied in designing hybrid composite laminates. © Published under licence by IOP Publishing Ltd.
Institute of Physics Publishing
17426588
English
Conference paper
All Open Access; Gold Open Access
author Azmi N.N.; Nasir M.F.M.; Ayoub G.; Hussain A.K.; Mahmud J.
spellingShingle Azmi N.N.; Nasir M.F.M.; Ayoub G.; Hussain A.K.; Mahmud J.
The study of hybrid composite plates under transverse sinusoidal load using ANSYS
author_facet Azmi N.N.; Nasir M.F.M.; Ayoub G.; Hussain A.K.; Mahmud J.
author_sort Azmi N.N.; Nasir M.F.M.; Ayoub G.; Hussain A.K.; Mahmud J.
title The study of hybrid composite plates under transverse sinusoidal load using ANSYS
title_short The study of hybrid composite plates under transverse sinusoidal load using ANSYS
title_full The study of hybrid composite plates under transverse sinusoidal load using ANSYS
title_fullStr The study of hybrid composite plates under transverse sinusoidal load using ANSYS
title_full_unstemmed The study of hybrid composite plates under transverse sinusoidal load using ANSYS
title_sort The study of hybrid composite plates under transverse sinusoidal load using ANSYS
publishDate 2019
container_title Journal of Physics: Conference Series
container_volume 1349
container_issue 1
doi_str_mv 10.1088/1742-6596/1349/1/012030
url https://www.scopus.com/inward/record.uri?eid=2-s2.0-85077790754&doi=10.1088%2f1742-6596%2f1349%2f1%2f012030&partnerID=40&md5=2fe61113482584b4e648922f047d7862
description Composite materials have been widely used in many applications but understanding their failure behavior is always challenging. For years, numerical investigation has been the effective alternative, even though the underlying theories related to composite materials are complicated. This study aims to investigate the improved strength of hybridization by comparing the failure behavior of glass-epoxy composite laminate and hybrid glass-graphite-epoxy laminate under transverse sinusoidal load. The composite and hybrid composite laminates with various aspect ratios were modelled using ANSYS. The plates were simply supported and transverse sinusoidal load were applied until failure occurs. Initially, numerical validation was performed and the simulated results are found to be close to the 3D elasticity analytical results. In general, most simulated parameters produced error less than 2% and thus proving the reliability of the finite element models and implementation. The first ply failure (FPF) and last ply failure (LPF) curves were plotted to compare the failure trend of glass-epoxy composite laminate and its hybrid laminate. The results showed no significant difference in the FPF trend but hybridization could withstand up to 80% more normalized load in terms of the LPF. In conclusion, the present study has shed new knowledge about the failure behavior of hybrid laminate and thus, this knowledge could be applied in designing hybrid composite laminates. © Published under licence by IOP Publishing Ltd.
publisher Institute of Physics Publishing
issn 17426588
language English
format Conference paper
accesstype All Open Access; Gold Open Access
record_format scopus
collection Scopus
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