Fatigue crack growth of Al 7475 T761 under constant and variable amplitude loading

dc.contributorUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-20T15:29:25Z
dc.date.accessioned2022-10-05T16:53:54Z
dc.date.available2014-05-20T15:29:25Z
dc.date.available2022-10-05T16:53:54Z
dc.date.created2014-05-20T15:29:25Z
dc.date.issued1997-01-01
dc.identifierAdvances In Fracture Research, Vols 1-6. Oxford: Pergamon Press Ltd, p. 1483-1490, 1997.
dc.identifierhttp://hdl.handle.net/11449/39010
dc.identifierWOS:A1997BJ89P00168
dc.identifier3511534795805776
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/3910213
dc.description.abstractExperimental programs in constant and variable amplitude loading were performed to obtain a x N curves and to study retardation in fatigue crack growth due to overloads. The main aim of this research program was to analyse the effect of overload ratio and number of overload peaks. The effect of underloads, before and after the overload blocks was also studied. The generalised equation of Paris-Erdogan type was used for modelling of obtained data on crack propagation under constant amplitude load.
dc.languageeng
dc.publisherPergamon Press Ltd
dc.relationAdvances In Fracture Research, Vols 1-6
dc.rightsAcesso aberto
dc.sourceWeb of Science
dc.subjectfatigue crack growth
dc.subjectaluminium
dc.subjectretardation
dc.subjectvariable amplitude loading
dc.subjecta x N curves
dc.titleFatigue crack growth of Al 7475 T761 under constant and variable amplitude loading
dc.typeTrabalho apresentado em evento


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