Elasto-plastic stress analysis of aluminum metal-matrix composite laminated plates under in-plane loading

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dc.contributor.authorSayman O.
dc.contributor.authorAkbulut H.
dc.contributor.authorMeriç C.
dc.date.accessioned2024-07-22T08:25:36Z
dc.date.available2024-07-22T08:25:36Z
dc.date.issued2000
dc.description.abstractThe study presents an elasto-plastic stress analysis of symmetric and antisymmetric cross-ply, angle-ply laminated metal-matrix composite plates. Long stainless steel fiber reinforced aluminum metal-matrix composite layer is manufactured by using moulds under the action of 30 MPa pressure and heating up to 600 °C. A laminated plate consists of four metal-matrix layers bonded symmetrically or antisymmetrically. The first-order shear deformation theory and nine-node Lagrangian finite element is used. The in-plane load is increased gradually.
dc.identifier.DOI-ID10.1016/S0045-7949(99)00086-3
dc.identifier.issn00457949
dc.identifier.urihttp://akademikarsiv.cbu.edu.tr:4000/handle/123456789/20495
dc.language.isoEnglish
dc.publisherElsevier Science Ltd
dc.subjectAluminum
dc.subjectElastoplasticity
dc.subjectFiber reinforced metals
dc.subjectFinite element method
dc.subjectLaminated composites
dc.subjectPlates (structural components)
dc.subjectPressure effects
dc.subjectShear deformation
dc.subjectStainless steel
dc.subjectStress analysis
dc.subjectStructural analysis
dc.subjectThermal effects
dc.subjectIn plane loading
dc.subjectLaminated plates
dc.subjectMetallic matrix composites
dc.titleElasto-plastic stress analysis of aluminum metal-matrix composite laminated plates under in-plane loading
dc.typeArticle

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