dc.contributorUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-20T13:28:07Z
dc.date.accessioned2022-10-05T13:24:54Z
dc.date.available2014-05-20T13:28:07Z
dc.date.available2022-10-05T13:24:54Z
dc.date.created2014-05-20T13:28:07Z
dc.date.issued2007-11-01
dc.identifierFatigue & Fracture of Engineering Materials & Structures. Oxford: Blackwell Publishing, v. 30, n. 11, p. 993-1007, 2007.
dc.identifier8756-758X
dc.identifierhttp://hdl.handle.net/11449/9323
dc.identifier10.1111/j.1460-2695.2007.01169.x
dc.identifierWOS:000250145500001
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/3885730
dc.description.abstractIn recent years, with higher demand for improved quality and corrosion resistance, recovered substrates have been extensively used. Consequently residual stresses originated from these coatings reduce the fatigue strength of a component. Due to this negative influence occasioned by corrosion resistance protective coatings, an effective process like shot peening must be considered to improve the fatigue strength. The shot peening treatment pushes the crack sources beneath the surface in most of medium and high cycle cases due to the compressive residual stress field (CRSF) induced. The aim of this study was to evaluate the influence on the fatigue life of anodic films grown on 7050-T7451 aluminium alloy by sulphuric acid anodizing, chromic acid anodizing and hard anodizing. The influence on the rotating and reverse bending fatigue strength of anodic films grown on the aluminium alloy is to degrade the stress life fatigue performance of the base material.A consistent gain in fatigue life in relation to the base material was obtained through the shot peening process in coated specimens, associated to a residual stress field compressive near the surface, useful to avoid fatigue crack nucleation and delay or even stop crack propagation.
dc.languageeng
dc.publisherBlackwell Publishing
dc.relationFatigue & Fracture of Engineering Materials & Structures
dc.relation2.533
dc.rightsAcesso restrito
dc.sourceWeb of Science
dc.subject7050-T7451 aluminium alloy
dc.subjectanodization
dc.subjectcoatings
dc.subjectfatigue
dc.subjectresidual stress
dc.subjectshot peening
dc.titleInfluence of anodization on the fatigue strength of 7050-T7451 aluminium alloy
dc.typeArtigo


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