The effects on critical load of metal-matrix composite plates with a hole under in-plane loadings

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dc.contributor.authorOkumus, F.
dc.contributor.authorTurgut, A.
dc.date.accessioned2026-08-12T16:09:59Z
dc.date.issued2001
dc.departmentFırat Üniversitesi
dc.descriptionASME 2001 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC-CIE 2001 -- 9 September 2001 through 12 September 2001 -- Pittsburgh -- 164952
dc.description.abstractMetal-matrix composite plates consists of several layers of unidirectionally reinforced, fibrous composite laminae which have different in-plane orientations and are bonded together in a certain stacking sequence. Thus, they provide new materials with superior properties of high strength and stiffness. This study deals with analysis of rectangular metal-matrix composite laminates with circular holes under in-plane static loadings. The first-order shear deformation theory is employed in mathematical formulation. The effects on critical load by hole size, ply lamination geometry, plate thickness ratio, loading types and material modulus ratio have been investigated. The finite element method is used for finding critical loads. Numerical solutions are given in graphical forms. Copyright © 2001 by ASME
dc.description.sponsorshipComputers and Information in Engineering Division; Design Engineering Division
dc.identifier.doi10.1115/DETC2001/RSAFP-21746
dc.identifier.endpage57
dc.identifier.scopus2-s2.0-85096777364
dc.identifier.scopusqualityN/A
dc.identifier.startpage47
dc.identifier.urihttps://doi.org/10.1115/DETC2001/RSAFP-21746
dc.identifier.urihttps://hdl.handle.net/11508/41696
dc.identifier.volume5
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherAmerican Society of Mechanical Engineers (ASME)
dc.relation.ispartofProceedings of the ASME Design Engineering Technical Conference
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_Scopus_20260511
dc.subjectDesign; Laminated composites; Plates (structural components); Reliability analysis; Shear deformation; Stress analysis; Fibrous composites; First-order shear deformation theory; In-plane orientation; Inplane loading; Lamination geometry; Mathematical formulation; Numerical solution; Stacking sequence; Metallic matrix composites
dc.titleThe effects on critical load of metal-matrix composite plates with a hole under in-plane loadings
dc.typeConference Object

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