SVET, SKP and EIS study of the corrosion behaviour of high strength Al and Al-Li alloys used in aircraft fabrication

dc.contributorUniversidade de São Paulo (USP)
dc.contributorUniv Minho
dc.contributorIFGoiano
dc.contributorUniversidade Federal do Paraná (UFPR)
dc.contributorUniversidade Estadual Paulista (Unesp)
dc.contributorUniv Lisbon
dc.contributorInst Super Tecn
dc.date.accessioned2014-12-03T13:11:46Z
dc.date.available2014-12-03T13:11:46Z
dc.date.created2014-12-03T13:11:46Z
dc.date.issued2014-07-01
dc.identifierCorrosion Science. Oxford: Pergamon-elsevier Science Ltd, v. 84, p. 30-41, 2014.
dc.identifier0010-938X
dc.identifierhttp://hdl.handle.net/11449/113521
dc.identifier10.1016/j.corsci.2014.03.001
dc.identifierWOS:000336464200004
dc.description.abstractThe 2XXX and 7XXX series aluminium alloys are commonly used in aircraft applications where high strength-to-weight ratios are required. The present study aims to compare the corrosion resistance of two novel alloys developed for aircraft industry (AA2198-T851 and 7081-T73511) to that presented by the alternative base alloys (AA2524-T3 and 7050-T7451, respectively). Results indicate that AA2198-T851 may show a superior corrosion performance compared to AA2524-T3, being a potential candidate for its replacement, due to best mechanical properties. In what concerns the 7081-T73511, its resistance to pitting corrosion may be lower than for the base line alloy 7050-T7451. (C) 2014 Elsevier Ltd. All rights reserved.
dc.languageeng
dc.publisherElsevier B.V.
dc.relationCorrosion Science
dc.relation4.862
dc.rightsAcesso restrito
dc.sourceWeb of Science
dc.subjectAluminium alloys
dc.subjectIntermetallics
dc.subjectEIS
dc.subjectSVET
dc.subjectSKP
dc.titleSVET, SKP and EIS study of the corrosion behaviour of high strength Al and Al-Li alloys used in aircraft fabrication
dc.typeArtículos de revistas


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