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

dc.contributor.authorSayman O.
dc.contributor.authorAkbulut H.
dc.contributor.authorMeriç C.
dc.date.accessioned2025-04-10T11:18:16Z
dc.date.available2025-04-10T11:18:16Z
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.urihttp://hdl.handle.net/20.500.14701/53315
dc.publisherElsevier Science Ltd
dc.titleElasto-plastic stress analysis of aluminum metal-matrix composite laminated plates under in-plane loading
dc.typeArticle

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