Publication:
Effect of Laminate Properties on the Failure of Cross Arm Structure under Multi-Axial Load

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dc.citedby12
dc.contributor.authorMohamad D.en_US
dc.contributor.authorSyamsir A.en_US
dc.contributor.authorBeddu S.en_US
dc.contributor.authorKamal N.L.M.en_US
dc.contributor.authorZainoodin M.M.en_US
dc.contributor.authorRazali M.F.en_US
dc.contributor.authorAbas A.en_US
dc.contributor.authorSeman S.A.H.A.en_US
dc.contributor.authorNg F.C.en_US
dc.contributor.authorid57200335404en_US
dc.contributor.authorid57195320482en_US
dc.contributor.authorid55812080500en_US
dc.contributor.authorid56239107300en_US
dc.contributor.authorid57202388764en_US
dc.contributor.authorid55535311300en_US
dc.contributor.authorid56893346700en_US
dc.contributor.authorid57200530460en_US
dc.contributor.authorid57192101900en_US
dc.date.accessioned2023-05-29T07:29:42Z
dc.date.available2023-05-29T07:29:42Z
dc.date.issued2019
dc.descriptionAxial loads; Laminated composites; Manufacture; Safety engineering; Structural properties; Three dimensional computer graphics; ITS applications; Laminate configuration; Laminate damage; Laminate properties; Mechanical deformation; Quasi-static loading; Three dimensional finite element model; Ultimate stress; Failure (mechanical)en_US
dc.description.abstractThis study investigated the influence of laminate properties toward the collapse of composite cross arm structure under multi-axial quasi-static loading. A three-dimensional finite-element model of a cross arm was developed and integrated with Hashin's failure subroutine to predict the inter-laminar damages of the composite upon its application. The mechanical deformation and failure of the composite structure were evaluated over three laminate properties. This investigation revealed that variation in laminates properties yielded different structural deflection and laminate damages. The cross arm with a greater young modulus and ultimate stresses (laminate B) experienced a single failure mode of fiber buckling in compression at deflection of 0.082 m. For the given multi-axial load, the laminate configuration and properties considered in this study failed to prevent the failure of the cross arm. � 2019 IOP Publishing Ltd. All rights reserved.en_US
dc.description.natureFinalen_US
dc.identifier.ArtNo12029
dc.identifier.doi10.1088/1757-899X/530/1/012029
dc.identifier.issue1
dc.identifier.scopus2-s2.0-85070333285
dc.identifier.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-85070333285&doi=10.1088%2f1757-899X%2f530%2f1%2f012029&partnerID=40&md5=298d5da61ddaa748c456f707f9a0fdb0
dc.identifier.urihttps://irepository.uniten.edu.my/handle/123456789/24976
dc.identifier.volume530
dc.publisherInstitute of Physics Publishingen_US
dc.relation.ispartofAll Open Access, Bronze
dc.sourceScopus
dc.sourcetitleIOP Conference Series: Materials Science and Engineering
dc.titleEffect of Laminate Properties on the Failure of Cross Arm Structure under Multi-Axial Loaden_US
dc.typeConference Paperen_US
dspace.entity.typePublication
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