Load–displacement behavior of glass fiber/epoxy composite plates with circular cut-outs subjected to compressive load

Hakim S. Sultan Aljibori; W.P. Chong; T.M.I. Mahlia; W.T. Chong; Prasetyo Edi; Haidar Fadhil Abbas Al-Qrimli; Irfan Anjum; R. Zahari

doi:10.1016/j.matdes.2009.07.005

Load–displacement behavior of glass fiber/epoxy composite plates with circular cut-outs subjected to compressive load

Hakim S. Sultan Aljibori, W.P. Chong, T.M.I. Mahlia, W.T. Chong, Prasetyo Edi, Haidar Fadhil Abbas Al-Qrimli, Irfan Anjum, R. Zahari

School of Engineering & Physical Sciences

Research output: Contribution to journal › Article › peer-review

27 Citations (Scopus)

Abstract

An experimental study of the behavior of woven glass fiber/epoxy composite laminated panels under compression is presented. Compression tests were performed on to 16 fiber-glass laminated plates with and without circular cut-outs using the compressed machine. The maximum load of failure for each of the glass-fiber/epoxy laminated plates under compression has been determined experimentally. A parametric study was performed as well to investigate the effects of varying the centrally located circular cut-out sizes and fiber angle-ply orientations on to the ultimate load. The experimental work revealed that as the cut-out size increases, the maximum load of the composite plate decreases. Also, it has been observed that cross-ply laminates possess the greatest ultimate load as compared to other types of ply stacking sequences and orientations.

Original language	English
Pages (from-to)	466–474
Number of pages	9
Journal	Materials & Design
Volume	31
DOIs	https://doi.org/10.1016/j.matdes.2009.07.005 https://doi.org/10.1016/j.matdes.2009.07.005
Publication status	Published - Jan 2010

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Sultan Aljibori, H. S., Chong, W. P., Mahlia, T. M. I., Chong, W. T., Edi, P., Al-Qrimli, H. F. A., Anjum, I., & Zahari, R. (2010). Load–displacement behavior of glass fiber/epoxy composite plates with circular cut-outs subjected to compressive load. Materials & Design, 31, 466–474. https://doi.org/10.1016/j.matdes.2009.07.005, https://doi.org/10.1016/j.matdes.2009.07.005

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title = "Load–displacement behavior of glass fiber/epoxy composite plates with circular cut-outs subjected to compressive load",

abstract = "An experimental study of the behavior of woven glass fiber/epoxy composite laminated panels under compression is presented. Compression tests were performed on to 16 fiber-glass laminated plates with and without circular cut-outs using the compressed machine. The maximum load of failure for each of the glass-fiber/epoxy laminated plates under compression has been determined experimentally. A parametric study was performed as well to investigate the effects of varying the centrally located circular cut-out sizes and fiber angle-ply orientations on to the ultimate load. The experimental work revealed that as the cut-out size increases, the maximum load of the composite plate decreases. Also, it has been observed that cross-ply laminates possess the greatest ultimate load as compared to other types of ply stacking sequences and orientations.",

author = "\{Sultan Aljibori\}, \{Hakim S.\} and W.P. Chong and T.M.I. Mahlia and W.T. Chong and Prasetyo Edi and Al-Qrimli, \{Haidar Fadhil Abbas\} and Irfan Anjum and R. Zahari",

year = "2010",

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doi = "10.1016/j.matdes.2009.07.005",

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T1 - Load–displacement behavior of glass fiber/epoxy composite plates with circular cut-outs subjected to compressive load

AU - Sultan Aljibori, Hakim S.

AU - Chong, W.P.

AU - Mahlia, T.M.I.

AU - Chong, W.T.

AU - Edi, Prasetyo

AU - Al-Qrimli, Haidar Fadhil Abbas

AU - Anjum, Irfan

AU - Zahari, R.

PY - 2010/1

Y1 - 2010/1

N2 - An experimental study of the behavior of woven glass fiber/epoxy composite laminated panels under compression is presented. Compression tests were performed on to 16 fiber-glass laminated plates with and without circular cut-outs using the compressed machine. The maximum load of failure for each of the glass-fiber/epoxy laminated plates under compression has been determined experimentally. A parametric study was performed as well to investigate the effects of varying the centrally located circular cut-out sizes and fiber angle-ply orientations on to the ultimate load. The experimental work revealed that as the cut-out size increases, the maximum load of the composite plate decreases. Also, it has been observed that cross-ply laminates possess the greatest ultimate load as compared to other types of ply stacking sequences and orientations.

AB - An experimental study of the behavior of woven glass fiber/epoxy composite laminated panels under compression is presented. Compression tests were performed on to 16 fiber-glass laminated plates with and without circular cut-outs using the compressed machine. The maximum load of failure for each of the glass-fiber/epoxy laminated plates under compression has been determined experimentally. A parametric study was performed as well to investigate the effects of varying the centrally located circular cut-out sizes and fiber angle-ply orientations on to the ultimate load. The experimental work revealed that as the cut-out size increases, the maximum load of the composite plate decreases. Also, it has been observed that cross-ply laminates possess the greatest ultimate load as compared to other types of ply stacking sequences and orientations.

U2 - 10.1016/j.matdes.2009.07.005

DO - 10.1016/j.matdes.2009.07.005

M3 - Article

SN - 0261-3069

VL - 31

SP - 466

EP - 474

JO - Materials & Design

JF - Materials & Design

ER -

Load–displacement behavior of glass fiber/epoxy composite plates with circular cut-outs subjected to compressive load

Abstract

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