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A brief discussion on (pure mode I) fatigue crack growth rate data in 5HS weave fabric composites: Evaluation of empirical relations

dc.contributor.authorShiino, Marcos Yutaka [UNESP]
dc.contributor.authorAlderliesten, Reyndert Christiaan
dc.contributor.authorDonadon, Mauricio Vicente
dc.contributor.authorCioffi, Maria Odila Hilário [UNESP]
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.contributor.institutionAerospace Structures and Materials
dc.contributor.institutionVila das Acácias
dc.date.accessioned2018-12-11T16:59:31Z
dc.date.available2018-12-11T16:59:31Z
dc.date.issued2016-03-01
dc.description.abstractA major concern in laminated composites for structural applications has been crack nucleation between plies and its propagation through the interface. A better comprehension of stable crack propagation may lead to more reliable predictions of the rate with which cracks grow in weave fabric laminated composites. To this aim, a number of empirical relationships proposed in the literature were studied for their applicability to satin weave fabric (5HS) composite with spread tows. In order to understand the fatigue delamination process, Double Cantilever Beam specimens were submitted to cyclic loading, and their respective da/dN vs strain energy release rate (SERR) data collected and correlated to these empirical relationships. Despite that the empirical or semi-empirical relations fit equally well to the data, the well-known Hartman-Schijve equation was adopted. This equation was properly modified according to the fracture surface investigation which had its fracture patterns qualitatively correlated with SERR parameters.en
dc.description.affiliationInstituto de Ciência e Tecnologia UNESP - Univ Estadual Paulista Campus de São José Dos Campos Departamento de Engenharia Ambiental, Rodovia Presidente Dutra km 137.8
dc.description.affiliationFaculty of Aerospace Engineering Delft University of Technology - TUDelft Aerospace Structures and Materials, Kluyverweg 1
dc.description.affiliationInstituto Tecnológico da Aeronáutica - ITA Vila das Acácias, Praça Marechal do Ar Eduardo Gomes
dc.description.affiliationFaculdade de Engenharia de Guaratinguetá UNESP - Univ Estadual Paulista Departamento de Materiais e Tecnologia Fatigue and Aeronautic Materials Research Group, Av. Dr. Ariberto Pereira da Cunha 333
dc.description.affiliationUnespInstituto de Ciência e Tecnologia UNESP - Univ Estadual Paulista Campus de São José Dos Campos Departamento de Engenharia Ambiental, Rodovia Presidente Dutra km 137.8
dc.description.affiliationUnespFaculdade de Engenharia de Guaratinguetá UNESP - Univ Estadual Paulista Departamento de Materiais e Tecnologia Fatigue and Aeronautic Materials Research Group, Av. Dr. Ariberto Pereira da Cunha 333
dc.format.extent97-103
dc.identifierhttp://dx.doi.org/10.1016/j.ijfatigue.2015.11.019
dc.identifier.citationInternational Journal of Fatigue, v. 84, p. 97-103.
dc.identifier.doi10.1016/j.ijfatigue.2015.11.019
dc.identifier.file2-s2.0-84949516950.pdf
dc.identifier.issn0142-1123
dc.identifier.lattes2160957529151025
dc.identifier.lattes6119671014416126
dc.identifier.scopus2-s2.0-84949516950
dc.identifier.urihttp://hdl.handle.net/11449/172282
dc.language.isoeng
dc.relation.ispartofInternational Journal of Fatigue
dc.relation.ispartofsjr1,402
dc.rights.accessRightsAcesso aberto
dc.sourceScopus
dc.subjectComposites
dc.subjectConstant load
dc.subjectCrack growth rate
dc.subjectFractography
dc.subjectStrain energy method
dc.titleA brief discussion on (pure mode I) fatigue crack growth rate data in 5HS weave fabric composites: Evaluation of empirical relationsen
dc.typeArtigo
dspace.entity.typePublication
unesp.author.lattes2160957529151025
unesp.author.lattes6119671014416126
unesp.author.orcid0000-0002-4155-4769[4]
unesp.departmentMateriais e Tecnologia - FEGpt

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