Fatigue crack growth in aluminum alloyt welded joint

dc.creator	Sedmak, Simon
dc.creator	Kraedegh, Abubakr
dc.creator	Grbović, Aleksandar
dc.creator	Sedmak, Aleksandar
dc.date.accessioned	2022-09-19T18:16:58Z
dc.date.available	2022-09-19T18:16:58Z
dc.date.issued	2017
dc.identifier.uri	https://machinery.mas.bg.ac.rs/handle/123456789/2667
dc.description.abstract	The aim of the present investigation is to study the fatigue crack growth of welded T joints made of AA2024-T351 aluminum alloy. Three dimensional finite element models, with cracks as initial defects, will be constructed for this purpose. Fatigue crack growth analyses are performed by using the finite element program ABAQUS to obtain Stress intensity factors around the crack tip for each step of crack propagation. SIF (K) is used as crack tip parameter in Paris equation for the calculation of the fatigue life. In order to predict the fatigue behavior of the welded structure, amplitude tensile loading is applied.	en
dc.publisher	International Conference on Fracture
dc.rights	restrictedAccess
dc.source	ICF 2017 - 14th International Conference on Fracture
dc.title	Fatigue crack growth in aluminum alloyt welded joint	en
dc.type	conferenceObject
dc.rights.license	ARR
dc.citation.epage	815
dc.citation.other	2: 814-815
dc.citation.spage	814
dc.citation.volume	2
dc.identifier.rcub	https://hdl.handle.net/21.15107/rcub_machinery_2667
dc.identifier.scopus	2-s2.0-85066020180
dc.type.version	publishedVersion

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