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Please use this identifier to cite or link to this item: http://acervodigital.unesp.br/handle/11449/9372
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dc.contributor.authorShiino, M. Y.-
dc.contributor.authorDe Camargo, L. M.-
dc.contributor.authorCioffi, M. O. H.-
dc.contributor.authorVoorwald, Herman Jacobus Cornelis-
dc.contributor.authorOrtiz, E. C.-
dc.contributor.authorRezende, M. C.-
dc.date.accessioned2014-05-20T13:28:13Z-
dc.date.accessioned2016-10-25T16:47:58Z-
dc.date.available2014-05-20T13:28:13Z-
dc.date.available2016-10-25T16:47:58Z-
dc.date.issued2012-07-01-
dc.identifierhttp://dx.doi.org/10.1016/j.compositesb.2012.01.074-
dc.identifier.citationComposites Part B-engineering. Oxford: Elsevier B.V., v. 43, n. 5, p. 2244-2248, 2012.-
dc.identifier.issn1359-8368-
dc.identifier.urihttp://hdl.handle.net/11449/9372-
dc.identifier.urihttp://acervodigital.unesp.br/handle/11449/9372-
dc.description.abstractQuantitative fractographic studies have become an important field to understand the fracture process. Future trends pointed out quantitative fractographic analysis as an important tool for a better comprehension of the damage and currently it had been focused on studies about geometric attributes of the fracture topographic surface and microstructure features. This research aimed a quantitative analysis of the cusp aspects generated in an axial fatigue test by carrying out fractographic measurements in order to know their influence on the fatigue test parameters, e.g. stress level, number of cycles, frequency, and stress ratio. Fatigue tests in tension-tension mode were undertaken in different stress levels, consequently leading to different number of cycles. Quasi-isotropic laminates were fatigue tested until the fracture, which was observed in SEM, and the hackle patterns were measured in the public domain program called Image J. The response of the laminate obeyed a cusp size pattern according to a number of cycles until the fracture was reached. (C) 2012 Elsevier Ltd. All rights reserved.en
dc.description.sponsorshipFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)-
dc.format.extent2244-2248-
dc.language.isoeng-
dc.publisherElsevier B.V.-
dc.sourceWeb of Science-
dc.subjectLaminateen
dc.subjectFatigueen
dc.subjectFractographyen
dc.titleCorrelation of microcrack fracture size with fatigue cycling on non-crimp fabric/RTM6 composite in the uniaxial fatigue testen
dc.typeoutro-
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.contributor.institutionInstituto Tecnológico de Aeronáutica (ITA)-
dc.contributor.institutionDiv Mat IAE CTA-
dc.description.affiliationUNESP Univ Estadual Paulista, Guaratingueta Fac Engn, Mat & Technol Dept, Fatigue & Aeronaut Mat Res Grp, BR-12516410 Guaratingueta, SP, Brazil-
dc.description.affiliationInst Tecnol Aeronaut, BR-12228900 Sao Jose Dos Campos, SP, Brazil-
dc.description.affiliationDiv Mat IAE CTA, BR-12228904 Sao Jose Dos Campos, SP, Brazil-
dc.description.affiliationUnespUNESP Univ Estadual Paulista, Guaratingueta Fac Engn, Mat & Technol Dept, Fatigue & Aeronaut Mat Res Grp, BR-12516410 Guaratingueta, SP, Brazil-
dc.description.sponsorshipIdFAPESP: 06/02121-6-
dc.description.sponsorshipIdFAPESP: 09/04123-4-
dc.description.sponsorshipIdFAPESP: 11/01937-0-
dc.identifier.doi10.1016/j.compositesb.2012.01.074-
dc.identifier.wosWOS:000305356700019-
dc.rights.accessRightsAcesso restrito-
dc.relation.ispartofComposites Part B: Engineering-
Appears in Collections:Artigos, TCCs, Teses e Dissertações da Unesp

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