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dc.contributor.authorda Costa, Adriana A.
dc.contributor.authorda Silva, Danielle F. N. R.
dc.contributor.authorTravessa, Dilermando N.
dc.contributor.authorBotelho, Edson Cocchieri [UNESP]
dc.date.accessioned2014-05-20T13:28:14Z
dc.date.available2014-05-20T13:28:14Z
dc.date.issued2012-12-01
dc.identifierhttp://dx.doi.org/10.1016/j.matdes.2012.06.038
dc.identifier.citationMaterials & Design. Oxford: Elsevier B.V., v. 42, p. 434-440, 2012.
dc.identifier.issn0261-3069
dc.identifier.urihttp://hdl.handle.net/11449/9378
dc.description.abstractThe effect of thermal-shock cycles on the mechanical properties of fiber-metal laminates (FMLs) has been evaluated. FML plates were composed by two AA2024 Al sheets (1.6 mm thick) and one composite ply formed by two layers of unidirectional glass fiber epoxy prepreg and two layers of epoxy adhesive tape of glass fiber reinforced epoxy adhesive. The set was manufactured by hand layup and typical vacuum bag technique. The curing cycle was in autoclave at 125 +/- 5 degrees C for 90 min and an autoclave pressure of 400 kPa. FML coupons taken from the manufactured plate were submitted to temperature variations between -50 and +80 degrees C, with a fast transition between these temperatures. Tensile and interlaminar shear strength were evaluated on samples after 1000 and 2000 cycles, and compared to nonexposed samples. 2000 Cycles corresponds to typical C Check interval for commercial aircraft maintenance programs. It was observed that the thermal-shock cycles did not result in significant microstructural changes on the FML, particularly on the composite ply. Similarly, no appreciable effect on the mechanical properties of FML was observed by the thermal-shock cycles. (c) 2012 Elsevier Ltd. All rights reserved.en
dc.format.extent434-440
dc.language.isoeng
dc.publisherElsevier B.V.
dc.relation.ispartofMaterials & Design
dc.sourceWeb of Science
dc.subjectFiber-metal laminatesen
dc.subjectThermal cyclingen
dc.subjectTensile strengthen
dc.subjectInterlaminar shear strengthen
dc.titleThe effect of thermal cycles on the mechanical properties of fiber-metal laminatesen
dc.typeArtigo
dcterms.licensehttp://www.elsevier.com/about/open-access/open-access-policies/article-posting-policy
dcterms.rightsHolderElsevier B.V.
dc.contributor.institutionUniversidade Federal de São Paulo (UNIFESP)
dc.contributor.institutionEmbraer Empresa Brasileira Aeronaut SA
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)
dc.description.affiliationUniv Fed São Paulo, Dept Ciência & Tecnol, BR-12231280 São Paulo, Brazil
dc.description.affiliationEmbraer Empresa Brasileira Aeronaut SA, BR-12227901 São Paulo, Brazil
dc.description.affiliationUniv Estadual Paulista, Fac Engn Guaratingueta, Dept Mat & Tecnol, BR-12516410 São Paulo, Brazil
dc.description.affiliationUnespUniv Estadual Paulista, Fac Engn Guaratingueta, Dept Mat & Tecnol, BR-12516410 São Paulo, Brazil
dc.identifier.doi10.1016/j.matdes.2012.06.038
dc.identifier.wosWOS:000308077400055
dc.rights.accessRightsAcesso restrito
unesp.campusUniversidade Estadual Paulista (UNESP), Faculdade de Engenharia, Guaratinguetápt
dc.identifier.lattes4378078337343660
dc.identifier.orcid0000-0001-8338-4879
unesp.author.lattes4378078337343660[4]
unesp.author.orcid0000-0001-8338-4879[4]
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