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dc.creatorElmiladi, Abdulrazag Abdallah
dc.creatorPetrović, Veljko M.
dc.creatorGrbović, Aleksandar
dc.creatorSedmak, Aleksandar
dc.creatorBalać, Igor
dc.date.accessioned2022-09-19T19:15:14Z
dc.date.available2022-09-19T19:15:14Z
dc.date.issued2021
dc.identifier.issn0354-9836
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/3524
dc.description.abstractThis paper presents numerical calculation of thermal stresses generated in a carbon fiber-epoxy laminated composite structure which is operating at low temperatures. The thermal stress evaluation is based on the finite element method. A sample problem involving generated thermal stresses in a real laminated composite structure, exposed to low temperatures (four different temperature levels), is analyzed and discussed. Obtained results suggest that these thermal stresses remarkably decrease the strength of the laminated composite structure.en
dc.publisherUniverzitet u Beogradu - Institut za nuklearne nauke Vinča, Beograd
dc.relationinfo:eu-repo/grantAgreement/MESTD/Integrated and Interdisciplinary Research (IIR or III)/45019/RS//
dc.relationinfo:eu-repo/grantAgreement/MESTD/Technological Development (TD or TR)/35044/RS//
dc.rightsopenAccess
dc.rights.urihttps://creativecommons.org/licenses/by-nc-nd/4.0/
dc.sourceThermal Science
dc.subjectthermal stressesen
dc.subjectreserve of strengthen
dc.subjectfinite element methoden
dc.subjectcarbon fiber-epoxy compositeen
dc.titleNumerical evaluation of thermal stresses generated in laminated composite structure exposed to low temperaturesen
dc.typearticle
dc.rights.licenseBY-NC-ND
dc.citation.epage3856
dc.citation.issue5
dc.citation.other25(5): 3847-3856
dc.citation.rankM23
dc.citation.spage3847
dc.citation.volume25
dc.identifier.doi10.2298/TSCI200729338E
dc.identifier.fulltexthttp://machinery.mas.bg.ac.rs/bitstream/id/2111/3521.pdf
dc.identifier.scopus2-s2.0-85115766601
dc.identifier.wos000698663000019
dc.type.versionpublishedVersion


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