dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorVoorwald, H. J C
dc.creatorTorres, M. A S
dc.creatorPinto Júnior, C. C E
dc.date2014-05-27T11:17:25Z
dc.date2016-10-25T18:12:45Z
dc.date2014-05-27T11:17:25Z
dc.date2016-10-25T18:12:45Z
dc.date1991-09-01
dc.date.accessioned2017-04-06T00:43:19Z
dc.date.available2017-04-06T00:43:19Z
dc.identifierInternational Journal of Fatigue, v. 13, n. 5, p. 423-427, 1991.
dc.identifier0142-1123
dc.identifierhttp://hdl.handle.net/11449/64139
dc.identifierhttp://acervodigital.unesp.br/handle/11449/64139
dc.identifier10.1016/0142-1123(91)90600-4
dc.identifier2-s2.0-0026226244
dc.identifierhttp://dx.doi.org/10.1016/0142-1123(91)90600-4
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/886059
dc.descriptionIn variable-amplitude loading there are interaction effects between the loading history and the crack propagation rate. The most important of these effects is the retardation in the crack propagation, which may raise the life of the cracked structureconsiderably. The main objective of this research is to analyse and quantify the retardation of crack propagation in a thin plate of the high-resistance aluminium alloy 2024-T3, comparing the results obtained from the mathematical models proposed to account for the retardation effect. The specimens were tested under high-low loading sequences, for different crack sizes and overload ratios. A simplified model was developed, based on crack closure theory, that could represent the crack behaviour during retardation very well. © 1991.
dc.languageeng
dc.relationInternational Journal of Fatigue
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectcrack growth
dc.subjectretardation
dc.titleModelling of fatigue crack growth following overloads
dc.typeOtro


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