Please use this identifier to cite or link to this item: http://dspace2020.uniten.edu.my:8080/handle/123456789/6230
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dc.contributor.authorAljibori, H.S.S.
dc.contributor.authorChong, W.P.
dc.contributor.authorMahlia, T.M.I.
dc.contributor.authorChong, W.T.
dc.contributor.authorEdi, P.
dc.contributor.authorAl-qrimli, H.
dc.contributor.authorAnjum, I.
dc.contributor.authorZahari, R.
dc.date.accessioned2017-12-08T09:12:15Z-
dc.date.available2017-12-08T09:12:15Z-
dc.date.issued2010
dc.identifier.urihttp://dspace.uniten.edu.my/jspui/handle/123456789/6230-
dc.description.abstractAn 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. © 2009 Elsevier Ltd. All rights reserved.
dc.titleLoad-displacement behavior of glass fiber/epoxy composite plates with circular cut-outs subjected to compressive load
item.fulltextNo Fulltext-
item.grantfulltextnone-
Appears in Collections:COE Scholarly Publication
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