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dc.creatorSedmak, Aleksandar
dc.creatorČolić, Katarina
dc.creatorGrbović, Aleksandar
dc.creatorBalać, Igor
dc.creatorBurzić, Meri
dc.date.accessioned2022-09-19T18:48:06Z
dc.date.available2022-09-19T18:48:06Z
dc.date.issued2019
dc.identifier.issn0013-7944
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/3126
dc.description.abstractFatigue crack growth in hip implant has been analysed using the extended finite element method. Toward this aim, the three-dimensional finite element model is created and used in ABAQUS and Morfeo/crack add-in for ABAQUS to simulate fatigue crack growth from initial value up to the critical point. Initial crack dimensions are assumed according to the experience with failures of hip implants, whereas the final, critical value was estimated using data for fracture toughness obtained by experimental testing of hip implant made of Ti-6Al-4V alloy. Results for the equivalent stress intensity factor and number of cycles in each of 40 steps of fatigue crack growth are presented and analysed, indicating the point of unstable crack growth.en
dc.publisherPergamon-Elsevier Science Ltd, Oxford
dc.relationinfo:eu-repo/grantAgreement/MESTD/Technological Development (TD or TR)/35040/RS//
dc.rightsrestrictedAccess
dc.sourceEngineering Fracture Mechanics
dc.subjectX-FEMen
dc.subjectTi-6Al-4Ven
dc.subjectHip implanten
dc.subjectFracture toughnessen
dc.subjectFatigue crack growthen
dc.titleNumerical analysis of fatigue crack growth of hip implanten
dc.typearticle
dc.rights.licenseARR
dc.citation.other216: -
dc.citation.rankM21
dc.citation.volume216
dc.identifier.doi10.1016/j.engfracmech.2019.106492
dc.identifier.scopus2-s2.0-85067015642
dc.identifier.wos000477573000030
dc.type.versionpublishedVersion


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Приказ основних података о документу