Response of CFRP laminates under high strain rate compression until failure

Detalhes bibliográficos
Autor(a) principal: R. M. Guedes
Data de Publicação: 2005
Outros Autores: M. A Vaz, F. J. Ferreira, J. L. Morais
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
Texto Completo: https://hdl.handle.net/10216/55267
Resumo: This work describes an experimental characterization: the non-linear rate-dependent mechanical behavior of a composite material under compression. Fiber reinforced polymer matrix composites exhibit non-linear mechanical behavior, except in fiber direction, which is rate-dependent. In this work the Texipreg (R) HS160 REM material system was used, comprising high strength carbon fiber and epoxy resin. Unidirectional laminates were tested under uniaxial compression tests on a universal testing machine. The stress/strain curves of several specimens were obtained at three different strain rates of 0.07, 0.001 and 0.0001/s. In all cases tests were continued until failure was reached to measure the strain rate effect on strength. A 3-parameter constitutive viscoplastic model /6,7/ was used to describe the mechanical behavior. This model was developed based on data for strain rate between 0.0001 and 0.07/s. In transverse direction the viscoplastic model was able to predict the high strain rate experiments conducted on a Split Hopkinson Pressure Bar.
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spelling Response of CFRP laminates under high strain rate compression until failureEngenharia dos materiaisMaterials engineeringThis work describes an experimental characterization: the non-linear rate-dependent mechanical behavior of a composite material under compression. Fiber reinforced polymer matrix composites exhibit non-linear mechanical behavior, except in fiber direction, which is rate-dependent. In this work the Texipreg (R) HS160 REM material system was used, comprising high strength carbon fiber and epoxy resin. Unidirectional laminates were tested under uniaxial compression tests on a universal testing machine. The stress/strain curves of several specimens were obtained at three different strain rates of 0.07, 0.001 and 0.0001/s. In all cases tests were continued until failure was reached to measure the strain rate effect on strength. A 3-parameter constitutive viscoplastic model /6,7/ was used to describe the mechanical behavior. This model was developed based on data for strain rate between 0.0001 and 0.07/s. In transverse direction the viscoplastic model was able to predict the high strain rate experiments conducted on a Split Hopkinson Pressure Bar.20052005-01-01T00:00:00Zinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttps://hdl.handle.net/10216/55267eng0334-181XR. M. GuedesM. A VazF. J. FerreiraJ. L. Moraisinfo:eu-repo/semantics/openAccessreponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãoinstacron:RCAAP2023-11-29T15:10:44Zoai:repositorio-aberto.up.pt:10216/55267Portal AgregadorONGhttps://www.rcaap.pt/oai/openaireopendoar:71602024-03-20T00:17:27.088669Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãofalse
dc.title.none.fl_str_mv Response of CFRP laminates under high strain rate compression until failure
title Response of CFRP laminates under high strain rate compression until failure
spellingShingle Response of CFRP laminates under high strain rate compression until failure
R. M. Guedes
Engenharia dos materiais
Materials engineering
title_short Response of CFRP laminates under high strain rate compression until failure
title_full Response of CFRP laminates under high strain rate compression until failure
title_fullStr Response of CFRP laminates under high strain rate compression until failure
title_full_unstemmed Response of CFRP laminates under high strain rate compression until failure
title_sort Response of CFRP laminates under high strain rate compression until failure
author R. M. Guedes
author_facet R. M. Guedes
M. A Vaz
F. J. Ferreira
J. L. Morais
author_role author
author2 M. A Vaz
F. J. Ferreira
J. L. Morais
author2_role author
author
author
dc.contributor.author.fl_str_mv R. M. Guedes
M. A Vaz
F. J. Ferreira
J. L. Morais
dc.subject.por.fl_str_mv Engenharia dos materiais
Materials engineering
topic Engenharia dos materiais
Materials engineering
description This work describes an experimental characterization: the non-linear rate-dependent mechanical behavior of a composite material under compression. Fiber reinforced polymer matrix composites exhibit non-linear mechanical behavior, except in fiber direction, which is rate-dependent. In this work the Texipreg (R) HS160 REM material system was used, comprising high strength carbon fiber and epoxy resin. Unidirectional laminates were tested under uniaxial compression tests on a universal testing machine. The stress/strain curves of several specimens were obtained at three different strain rates of 0.07, 0.001 and 0.0001/s. In all cases tests were continued until failure was reached to measure the strain rate effect on strength. A 3-parameter constitutive viscoplastic model /6,7/ was used to describe the mechanical behavior. This model was developed based on data for strain rate between 0.0001 and 0.07/s. In transverse direction the viscoplastic model was able to predict the high strain rate experiments conducted on a Split Hopkinson Pressure Bar.
publishDate 2005
dc.date.none.fl_str_mv 2005
2005-01-01T00:00:00Z
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dc.identifier.uri.fl_str_mv https://hdl.handle.net/10216/55267
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repository.name.fl_str_mv Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informação
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