Please use this identifier to cite or link to this item: http://dspace2020.uniten.edu.my:8080/handle/123456789/21459
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dc.contributor.authorMohamad D.en_US
dc.contributor.authorSyamsir A.en_US
dc.contributor.authorSa'Don S.N.en_US
dc.contributor.authorZahari N.M.en_US
dc.contributor.authorSeman S.A.H.A.en_US
dc.contributor.authorRazali M.F.en_US
dc.contributor.authorAbas A.en_US
dc.contributor.authorNg F.C.en_US
dc.date.accessioned2021-11-08T07:18:33Z-
dc.date.available2021-11-08T07:18:33Z-
dc.date.issued2019-
dc.identifier.urihttp://dspace2020.uniten.edu.my:8080/handle/123456789/21459-
dc.description.abstractIn this paper, the effects of the stacking sequence on the mechanical performance and damage formation of composite laminates subjected to multi-axial quasi-static loading is investigated, considering intra-laminar damage onset. The response of the composite laminate configurations characterized by different stacking sequences subjected to multi-axial quasi-static loading have been studied to predict the influence on the static displacement and damage development. A finite element (FE) model has been used to numerically simulate the response of the composite structure. ABAQUS/EXPLICT FE environment has been considered for the analyses and Hashin's failure criteria has been adopted using a VUMAT subroutine to model the intra-laminar damage formation in the analyzed composite structure. © 2019 IOP Publishing Ltd. All rights reserved.en_US
dc.language.isoenen_US
dc.titleStacking sequence effects on performance of composite laminate structure subjected to multi-axial quasi-static loadingen_US
dc.typeconference paperen_US
item.cerifentitytypePublications-
item.languageiso639-1en-
item.fulltextWith Fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_5794-
item.grantfulltextreserved-
item.openairetypeconference paper-
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