THE INFLUENCE OF CARBON FIBER ORIENTATION ANGLE ON BUCKLING PROPERTIES OF FOUR–LAYER SYMMETRIC LAMINATE UNDER BIAXIAL COMPRESSION

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dc.citation.epage108
dc.citation.spage103
dc.citation.volume20
dc.contributor.authorJeremić, Dejan
dc.contributor.authorRadić, Nebojša
dc.contributor.authorVučetić, Nikola
dc.contributor.editorKiss, Imre
dc.date.accessioned2024-02-22T11:27:43Z
dc.date.available2024-02-22T11:27:43Z
dc.date.issued2022
dc.description.abstractThe present work focused on the buckling of four–layer symmetric laminate subjected to biaxial compression. Governing equations are derived based on Classical Laminated Plate Theory (CLPT). The composite plates are bonded by an internal elastic medium and surrounded by external elastic foundation. The influences of carbon fiber orientation angle and aspect ratio on critical buckling load are demonstrated for symmetric laminate. We analyzed four lamination scheme which fiber angle orientation is equal to 0°, 30°, 45° and 90°.
dc.identifier.issn2601 – 2332
dc.identifier.urihttps://vaseljena.ues.rs.ba/handle/123456789/985
dc.language.isoen
dc.publisherUniversity POLITEHNICA Timisoara
dc.sourceAnnals of Faculty Engineering Hunedoara – International Journal of Engineering
dc.subjectanalytical modelling, buckling, composite plates, carbon fiber angle
dc.titleTHE INFLUENCE OF CARBON FIBER ORIENTATION ANGLE ON BUCKLING PROPERTIES OF FOUR–LAYER SYMMETRIC LAMINATE UNDER BIAXIAL COMPRESSION
dc.typeArticle
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Машински факултет [Научни радови] / Faculty of Mechanical Engineering [Scientific papers]