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  2. University of Kragujevac
  3. Faculty of Engineering, Kragujevac
Please use this identifier to cite or link to this item: https://scidar.kg.ac.rs/handle/123456789/22439
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dc.contributor.authorTošić, Gordana-
dc.contributor.authorMilovanović, Vladimir-
dc.contributor.authorZivkovic, Miroslav-
dc.contributor.authorGrujić, Bojana-
dc.contributor.authorMiljanić, Dragomir-
dc.contributor.editorMirjanić, Dragoljub-
dc.date.accessioned2025-07-21T08:43:05Z-
dc.date.available2025-07-21T08:43:05Z-
dc.date.issued2025-
dc.identifier.issn1986-8669en_US
dc.identifier.urihttps://scidar.kg.ac.rs/handle/123456789/22439-
dc.description.abstractThis paper deals with laminated plates subjected to uniaxial compression. The effects of lamination scheme and material properties on the critical loads are considered, as well as variations of boundary conditions and direction of the acting loads. The buckling analysis was conducted using the finite elements method implemented in the Simcenter Femap software package. The obtained results were compared with the already available ones.en_US
dc.description.urihttps://doisrpska.nub.rs/index.php/conterporarymaterials3-1/abouten_US
dc.language.isoenen_US
dc.relation.ispartofCONTEMPORARY MATERIALSen_US
dc.rightsAttribution 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by/3.0/us/*
dc.subjectBucklingen_US
dc.subjectlaminated platesen_US
dc.titleBUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATESen_US
dc.typearticleen_US
dc.identifier.doihttps://doi.org/10.7251/COMEN2501066Ten_US
Appears in Collections:Faculty of Engineering, Kragujevac

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