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Please use this identifier to cite or link to this item: http://acervodigital.unesp.br/handle/11449/9323
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dc.contributor.authorCamargo, A.-
dc.contributor.authorVoorwald, H.-
dc.date.accessioned2014-05-20T13:28:07Z-
dc.date.accessioned2016-10-25T16:47:53Z-
dc.date.available2014-05-20T13:28:07Z-
dc.date.available2016-10-25T16:47:53Z-
dc.date.issued2007-11-01-
dc.identifierhttp://dx.doi.org/10.1111/j.1460-2695.2007.01169.x-
dc.identifier.citationFatigue & Fracture of Engineering Materials & Structures. Oxford: Blackwell Publishing, v. 30, n. 11, p. 993-1007, 2007.-
dc.identifier.issn8756-758X-
dc.identifier.urihttp://hdl.handle.net/11449/9323-
dc.identifier.urihttp://acervodigital.unesp.br/handle/11449/9323-
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.en
dc.format.extent993-1007-
dc.language.isoeng-
dc.publisherBlackwell Publishing-
dc.sourceWeb of Science-
dc.subject7050-T7451 aluminium alloypt
dc.subjectanodizationpt
dc.subjectcoatingspt
dc.subjectfatiguept
dc.subjectresidual stresspt
dc.subjectshot peeningpt
dc.titleInfluence of anodization on the fatigue strength of 7050-T7451 aluminium alloyen
dc.typeoutro-
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.description.affiliationUNESP, FEG, DMT, Fatigue & Aeronaut Mat Res Grp, BR-12516410 Guaratingueta, SP, Brazil-
dc.description.affiliationUnespUNESP, FEG, DMT, Fatigue & Aeronaut Mat Res Grp, BR-12516410 Guaratingueta, SP, Brazil-
dc.identifier.doi10.1111/j.1460-2695.2007.01169.x-
dc.identifier.wosWOS:000250145500001-
dc.rights.accessRightsAcesso restrito-
dc.relation.ispartofFatigue & Fracture of Engineering Materials & Structures-
Appears in Collections:Artigos, TCCs, Teses e Dissertações da Unesp

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