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Extended FEM analysis of fatigue crack growth in Ti-6Al-4V orthopaedic plates

dc.creatorVučetić, Filip
dc.creatorČolić, Katarina
dc.creatorGrbović, Aleksandar
dc.creatorRadaković, Zoran
dc.creatorSedmak, Simon
dc.date.accessioned2022-09-19T19:03:02Z
dc.date.available2022-09-19T19:03:02Z
dc.date.issued2020
dc.identifier.issn2452-3216
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/3345
dc.description.abstractThe extended finite element method (xFEM) was used to analyse fatigue crack growth in orthopaedic locking compression plates (LCP), made of Titanium alloy, Ti-6Al-4V, loaded in four-point bending. The optimal geometry was defined previously in respect to the remaining life of LCP used for patients with different body weights (BW - 60, 90 and 120 Kg). The plate with optimal geometry is analysed in more details here to assess the effect of BW and get better insight into fatigue crack growth path.en
dc.publisherElsevier, Amsterdam
dc.relationinfo:eu-repo/grantAgreement/MESTD/Technological Development (TD or TR)/35040/RS//
dc.rightsopenAccess
dc.rights.urihttps://creativecommons.org/licenses/by-nc-nd/4.0/
dc.sourceProcedia Structural Integrity - 1st Virtual European Conference on Fracture - Vecf1
dc.subjectTi-6Al-4Ven
dc.subjectLocking Compression Platesen
dc.subjectFatigue Crack Growthen
dc.subjectExtended Finite Element Methoden
dc.titleExtended FEM analysis of fatigue crack growth in Ti-6Al-4V orthopaedic platesen
dc.typeconferenceObject
dc.rights.licenseBY-NC-ND
dc.citation.epage560
dc.citation.other28: 555-560
dc.citation.spage555
dc.citation.volume28
dc.identifier.doi10.1016/j.prostr.2020.10.065
dc.identifier.fulltexthttp://machinery.mas.bg.ac.rs/bitstream/id/1958/3342.pdf
dc.identifier.scopus2-s2.0-85099844882
dc.identifier.wos000632387500065
dc.type.versionpublishedVersion


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