Приказ основних података о документу

dc.creatorGrbović, Aleksandar
dc.creatorKastratović, Gordana
dc.creatorSedmak, Aleksandar
dc.creatorEldwaib, Khalid
dc.creatorKirin, Snežana
dc.date.accessioned2022-09-19T18:46:47Z
dc.date.available2022-09-19T18:46:47Z
dc.date.issued2019
dc.identifier.issn0142-1123
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/3107
dc.description.abstractShape optimisation is a nowadays-standard requirement in the design of lightweight structural components. In this paper, optimisation of I-beam cross-section of integral aluminium 2024-T3 wing spar is presented, taking the maximum fatigue life as the criterion. Toward this aim, the extended finite element method (XFEM) was used to simulate crack growth in complex I-beam geometry. The computations were carried out using Morfeo/Crack add-on based on XFEM implementation in Abaqus software. Fatigue lives of wing spars with different sizes of cross section but constant area were compared. Conducted analysis has shown that XFEM seems to be efficient tool for complex three-dimensional configurations optimisation.en
dc.publisherElsevier Sci Ltd, Oxford
dc.relationinfo:eu-repo/grantAgreement/MESTD/Basic Research (BR or ON)/174004/RS//
dc.rightsrestrictedAccess
dc.sourceInternational Journal of Fatigue
dc.subjectIntegral structuresen
dc.subjectFatigue lifeen
dc.subjectExtended finite element methoden
dc.subjectCrack growth rateen
dc.titleDetermination of optimum wing spar cross section for maximum fatigue lifeen
dc.typearticle
dc.rights.licenseARR
dc.citation.epage311
dc.citation.other127: 305-311
dc.citation.rankM21
dc.citation.spage305
dc.citation.volume127
dc.identifier.doi10.1016/j.ijfatigue.2019.06.019
dc.identifier.scopus2-s2.0-85067564649
dc.identifier.wos000482492600028
dc.type.versionpublishedVersion


Документи

Thumbnail

Овај документ се појављује у следећим колекцијама

Приказ основних података о документу