Failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / Muhammad Amir Azhan Zulkifli

Hybrid composite laminates have recently increasing attention in precision engineering field such as aerospace and automotive industries. Studies for failure behaviour of hybrid laminated composites under uniform biaxial loads have been obtained without considering cutouts. Nevertheless, in practice...

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主要作者:	Zulkifli, Muhammad Amir Azhan
格式:	Thesis
语言:	English
出版:	2022
主题:	Finite element method Composite materials.
在线阅读:	https://ir.uitm.edu.my/id/eprint/75714/1/75714.pdf
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id	my-uitm-ir.75714
record_format	uketd_dc
spelling	my-uitm-ir.757142023-03-30T13:28:29Z Failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / Muhammad Amir Azhan Zulkifli 2022 Zulkifli, Muhammad Amir Azhan Finite element method Composite materials. Hybrid composite laminates have recently increasing attention in precision engineering field such as aerospace and automotive industries. Studies for failure behaviour of hybrid laminated composites under uniform biaxial loads have been obtained without considering cutouts. Nevertheless, in practice, the structures are provided with cutouts of various sizes subjected to biaxial tension. This study intends to analyse the failure behaviour of Boron/Glass hybrid composite laminates material with various cutout shapes and sizes under biaxial tension. Initially, failure analysis was performed for laminated composite plate without cutout with lamination sequence of (Ɵ4/04/-Ɵ4)s where the angle, 9 ranges from 0° to 90° using a Finite Element Analysis (FEA) software, ANSYS. The accuracy of the analysis were compared using analytical method using Matlab based on First Order Shear Deformation Theory (FSDT). Then, next stage involved the failure analysis of hybrid laminated composite plate with various cutouts (circle, diamond and square) and sizes. The ply angles of (0/±45/90)s, (0/±45)s and (0/90)s are modelled. These analyses were performed to determine the failure load by employing Maximum stress criterion and Tsai-Wu criterion. The failure curves were plotted and analysed. Results of Matlab code and FEA based ANSYS software, are in close agreement. 2022 Thesis https://ir.uitm.edu.my/id/eprint/75714/ https://ir.uitm.edu.my/id/eprint/75714/1/75714.pdf text en public masters Universiti Teknologi MARA (UiTM) College of Engineering Mahmud, Jamaluddin
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Mahmud, Jamaluddin
topic	Finite element method Composite materials.
spellingShingle	Finite element method Composite materials. Zulkifli, Muhammad Amir Azhan Failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / Muhammad Amir Azhan Zulkifli
description	Hybrid composite laminates have recently increasing attention in precision engineering field such as aerospace and automotive industries. Studies for failure behaviour of hybrid laminated composites under uniform biaxial loads have been obtained without considering cutouts. Nevertheless, in practice, the structures are provided with cutouts of various sizes subjected to biaxial tension. This study intends to analyse the failure behaviour of Boron/Glass hybrid composite laminates material with various cutout shapes and sizes under biaxial tension. Initially, failure analysis was performed for laminated composite plate without cutout with lamination sequence of (Ɵ4/04/-Ɵ4)s where the angle, 9 ranges from 0° to 90° using a Finite Element Analysis (FEA) software, ANSYS. The accuracy of the analysis were compared using analytical method using Matlab based on First Order Shear Deformation Theory (FSDT). Then, next stage involved the failure analysis of hybrid laminated composite plate with various cutouts (circle, diamond and square) and sizes. The ply angles of (0/±45/90)s, (0/±45)s and (0/90)s are modelled. These analyses were performed to determine the failure load by employing Maximum stress criterion and Tsai-Wu criterion. The failure curves were plotted and analysed. Results of Matlab code and FEA based ANSYS software, are in close agreement.
format	Thesis
qualification_level	Master's degree
author	Zulkifli, Muhammad Amir Azhan
author_facet	Zulkifli, Muhammad Amir Azhan
author_sort	Zulkifli, Muhammad Amir Azhan
title	Failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / Muhammad Amir Azhan Zulkifli
title_short	Failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / Muhammad Amir Azhan Zulkifli
title_full	Failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / Muhammad Amir Azhan Zulkifli
title_fullStr	Failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / Muhammad Amir Azhan Zulkifli
title_full_unstemmed	Failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / Muhammad Amir Azhan Zulkifli
title_sort	failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / muhammad amir azhan zulkifli
granting_institution	Universiti Teknologi MARA (UiTM)
granting_department	College of Engineering
publishDate	2022
url	https://ir.uitm.edu.my/id/eprint/75714/1/75714.pdf
_version_	1783736074508435456

Failure analysis of boron/glass hybrid composite laminates with various cutouts shapes and sizes under biaxial tension / Muhammad Amir Azhan Zulkifli

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