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dc.contributor.authorAchache, Habib-
dc.date.accessioned2020-01-22T11:42:53Z-
dc.date.available2020-01-22T11:42:53Z-
dc.date.issued2017-
dc.identifier.issn2367-8992-
dc.identifier.urihttps://ds.univ-oran2.dz:8443/jspui/handle/123456789/2875-
dc.description.abstractOur work aims to analyze using the finite element method the evolution of the stress intensity factor (SIF) parameter K of three laminated folded plates stacks [+ α, -α], made of the same epoxy matrix and different reinforcement fibe rs (boron, graphite and glass). Our results show that the angle of orientation of the boron / epoxy composite has no great influence on the variation of the parameter K KI. Compared to composite graphite / epoxy and glass / epoxy, the laminated composite bor on / epoxy reduces more the SIF K KI in the middle of the plate for angles 0 ° ≤α≤30 °.en_US
dc.language.isoenen_US
dc.publisherInternational Journal of Theoretical and Applied Mechanicsen_US
dc.subjectCracks , delamination, stress intensity factor, fibers orientations, finite element method and laminateslaminates.en_US
dc.titleDelamination of a Composite Laminated under Monotonic Loadingen_US
dc.typeArticleen_US
dc.number.totalPage10en_US
Collection(s) :6.Institut de Maintenance et de Sécurité Industrielle

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