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dc.creatorGrbović, Aleksandar
dc.creatorSedmak, Aleksandar
dc.creatorPetrovski, Blagoj
dc.creatorSghayer, Abulgasem
dc.creatorSedmak, Simon
dc.creatorRazavi, J.
dc.creatorBerto, Filippo
dc.date.accessioned2022-09-19T19:24:20Z
dc.date.available2022-09-19T19:24:20Z
dc.date.issued2021
dc.identifier.issn2452-3216
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/3657
dc.description.abstractFatigue crack growth in a panel with 4 stringers and 3-clips, made of AA6156 T6, was modelled numerically using xFEM. The central crack of the length a=17 mm was propagated in the total of 91 steps (in each step crack length increased by 2 mm) and after 14 steps the first clip began to deform. At the same time, crack continued to grow through the base plate, reaching the right and left stringers after 91 steps and beginning to grow along those stringers. Number of cycles for panel with additional 3-clips was higher than for panel with just 4-stringer, (278476 cycles vs. 2649587) cycles, improving fatigue life for cca 5%.en
dc.publisherElsevier B.V.
dc.relationinfo:eu-repo/grantAgreement/MESTD/inst-2020/200105/RS//
dc.rightsopenAccess
dc.rights.urihttps://creativecommons.org/licenses/by-nc-nd/4.0/
dc.sourceProcedia Structural Integrity
dc.subjectxFEMen
dc.subjectPanel with Stringersen
dc.subjectFatigue Crack Growthen
dc.subjectClipsen
dc.subjectAA6156 T6en
dc.titleNumerical simulation of fatigue crack growth in AA6156 T6 panelsen
dc.typeconferenceObject
dc.rights.licenseBY-NC-ND
dc.citation.epage791
dc.citation.issueC
dc.citation.other39(C): 786-791
dc.citation.spage786
dc.citation.volume39
dc.identifier.doi10.1016/j.prostr.2022.03.155
dc.identifier.fulltexthttp://machinery.mas.bg.ac.rs/bitstream/id/2222/3654.pdf
dc.identifier.scopus2-s2.0-85129430187
dc.type.versionpublishedVersion


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