Creep/recovery and stress-relaxation tests applied in a standardized carbon fiber/epoxy composite: Design of experiment approach

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MetadadosDescriçãoIdioma
Autor(es): dc.contributorUniversidade Estadual Paulista (Unesp)-
Autor(es): dc.contributorFederal University of Rio Grande do Sul-
Autor(es): dc.creatorMonticeli, Francisco Maciel [UNESP]-
Autor(es): dc.creatorOrnaghi, Heitor Luiz [UNESP]-
Autor(es): dc.creatorNeves, Roberta Motta-
Autor(es): dc.creatorOdila Hilário Cioffi, Maria [UNESP]-
Data de aceite: dc.date.accessioned2022-02-22T00:24:16Z-
Data de disponibilização: dc.date.available2022-02-22T00:24:16Z-
Data de envio: dc.date.issued2020-12-11-
Data de envio: dc.date.issued2020-12-11-
Data de envio: dc.date.issued2020-05-01-
Fonte completa do material: dc.identifierhttp://dx.doi.org/10.1177/0309324719892710-
Fonte completa do material: dc.identifierhttp://hdl.handle.net/11449/198335-
Fonte: dc.identifier.urihttp://educapes.capes.gov.br/handle/11449/198335-
Descrição: dc.descriptionCarbon fiber–reinforced plastic is a trend in the composite field since it has outstanding mechanical properties, which can be applied in several areas. For this work, carbon fiber–reinforced plastic composite using epoxy as matrix was molded by vacuum-assisted resin transfer molding to measure the individual influence of temperature and strain/stress on initial strain, permanent deformation, and modulus decay behavior of carbon fiber–reinforced plastic quantitatively. To achieve this purpose, void content, creep/recovery, and stress-relaxation properties were statistically evaluated by design of experiment approach–Taguchi method and analysis of variance. Results showed that both permanent deformation and modulus decay had influence on temperature and design of experiment confirmed that temperature is the main contributor to each response, considering all three viscoelastic regions (glassy, glass transition, and rubbery) and stress/strain.-
Descrição: dc.descriptionCoordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)-
Descrição: dc.descriptionConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)-
Descrição: dc.descriptionFatigue and Aeronautical Materials Research Group Department of Materials and Technology School of Engineering São Paulo State University (UNESP)-
Descrição: dc.descriptionPostgraduate Program in Mining Metallurgical and Materials Engineering (PPGE3M) Federal University of Rio Grande do Sul-
Descrição: dc.descriptionFatigue and Aeronautical Materials Research Group Department of Materials and Technology School of Engineering São Paulo State University (UNESP)-
Descrição: dc.descriptionCNPq: 15335/2018-1-
Formato: dc.format109-117-
Idioma: dc.languageen-
Relação: dc.relationJournal of Strain Analysis for Engineering Design-
???dc.source???: dc.sourceScopus-
Palavras-chave: dc.subjectCarbon fiber–reinforced plastic-
Palavras-chave: dc.subjectcreep-
Palavras-chave: dc.subjectdesign of experiments-
Palavras-chave: dc.subjectstress relaxation-
Palavras-chave: dc.subjectTaguchi method-
Título: dc.titleCreep/recovery and stress-relaxation tests applied in a standardized carbon fiber/epoxy composite: Design of experiment approach-
Tipo de arquivo: dc.typelivro digital-
Aparece nas coleções:Repositório Institucional - Unesp

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