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.accessioned2024-07-18T11:53:22Z
dc.date.available2024-07-18T11:53:22Z
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 degrees 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. (C) 2000 Elsevier Science Ltd. All rights reserved.
dc.identifier.issn0045-7949
dc.identifier.urihttp://akademikarsiv.cbu.edu.tr:4000/handle/123456789/5555
dc.language.isoEnglish
dc.publisherPERGAMON-ELSEVIER SCIENCE LTD
dc.subjectFINITE-ELEMENT ANALYSIS
dc.subjectSHELLS
dc.subjectHOLES
dc.titleElasto-plastic stress analysis of aluminum metal-matrix composite laminated plates under in-plane loading
dc.typeArticle

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