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Plastic CTOD as fatigue crack growth characterising parameter in 2024-T3 and 7050-T6 aluminium alloys using DIC

dc.contributor.authorVasco, José Manuel
dc.contributor.authorDiaz-Garrido, Francisco Alberto
dc.contributor.authorAntunes, Fernando Ventura
dc.contributor.authorJames, Neil
dc.date.accessioned2025-01-08T12:57:30Z
dc.date.available2025-01-08T12:57:30Z
dc.date.issued2020-03-03
dc.descriptionT1, Q2 (Mechanical Engineering; IF = 3.459)es_ES
dc.description.abstractThe plastic range of crack tip opening displacement (CTOD) has been used for the experimental characterisation of fatigue crack growth for 2024-T3 and 7050-T6 aluminium alloys using digital image correlation (DIC). Analysis of a complete loading cycle allowed resolving the CTOD into elastic and plastic components. Fatigue tests were conducted on compact tension specimens with a thickness of 1 mm and a width of 20 mm at stress ratios of 0.1, 0.3 and 0.5. The range of plastic CTOD could be related linearly to da/dN independent of stress ratio for both alloys. To facilitate accurate measurements of CTOD, a method was developed for correctly locating the crack tip and a sensitivity analysis was performed to explore the effect of measurement position behind the crack tip on the CTOD. The plastic range of CTOD was demonstrated to be a suitable alternate parameter to the stress intensity factor range for characterising fatigue crack propagation. A particularly innovative aspect of the work is that the paper describes a DIC-based technique that the authors believe gives a reliable way to determine the appropriate position to measure CTOD.es_ES
dc.description.sponsorshipThe authors want to acknowledge the financial support from the Spanish Government through the research project “Proyecto de Investigación de Excelencia del Ministerio de Economía y Competitividad MAT2016-76951-1-P,” without which this work could not have been performed.es_ES
dc.identifier.citationJ.M. Vasco-Olmo, F.A. Díaz, F.V. Antunes, M.N. James. Plastic CTOD as fatigue crack growth characterising parameter in 2024-T3 and 7050-T6 aluminium alloys using DIC. Fatigue & Fracture of Engineering Materials & Structures, 43: 1719–1730, 2020. https://onlinelibrary.wiley.com/doi/full/10.1111/ffe.13210.es_ES
dc.identifier.issn8756-758Xes_ES
dc.identifier.other10.1111/ffe.13210es_ES
dc.identifier.urihttps://onlinelibrary.wiley.com/doi/full/10.1111/ffe.13210es_ES
dc.identifier.urihttps://hdl.handle.net/10953/3782
dc.language.isoenges_ES
dc.publisherWiley.es_ES
dc.relation.ispartofFatigue & Fracture of Engineering Materials & Structureses_ES
dc.rightsAtribución-NoComercial-SinDerivadas 3.0 España*
dc.rights.accessRightsinfo:eu-repo/semantics/openAccesses_ES
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/es/*
dc.subject2024-T3 and 7050-T6 aluminium alloyses_ES
dc.subjectCTODes_ES
dc.subjectDICes_ES
dc.subjectFatigue crack growthes_ES
dc.titlePlastic CTOD as fatigue crack growth characterising parameter in 2024-T3 and 7050-T6 aluminium alloys using DICes_ES
dc.typeinfo:eu-repo/semantics/articlees_ES
dc.type.versioninfo:eu-repo/semantics/acceptedVersiones_ES

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