Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructure

Detalhes bibliográficos
Autor(a) principal: Sharma,Rajneesh
Data de Publicação: 2014
Outros Autores: Bhagat,Atul Ramesh, Mahajan,Puneet
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Latin American journal of solids and structures (Online)
Texto Completo: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1679-78252014000200002
Resumo: Finite element mesh of multi-directional 4D carbon/carbon (C/C) composite was reconstructed from 2D images obtained by X-ray tomography. Thus, imperfections in the composite such as voids, misalignment and cross-section distortion of the fibre bundles were directly incorporated in the finite element mesh. 2D images of the composite were also used for the characterization of the porosity in the composite. The effect of these micro structural imperfections was studies by assuming perfect bonding at the bundle/matrix interface. The initial mechanical properties of the composite were obtained from unit cell analysis using asymptotic homogenization and moduli in x, y and z directions were 39, 25 and 44 GPa. However, matrix and bundle/matrix interfacial cracks were also clearly visible in the X-ray tomographic images. Later, the effects of debonding was incorporated by using frictional cohesive interaction at bundle/matrix interfaces and matrix cracking was modeled by degrading the elastic properties of matrix. Final, the response of the composite was studied under six individual load cases.
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spelling Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructureCarbon/Carbon compositesHomogenizationX-ray tomography reconstructionImage based FEMCohesive surfacesFinite element mesh of multi-directional 4D carbon/carbon (C/C) composite was reconstructed from 2D images obtained by X-ray tomography. Thus, imperfections in the composite such as voids, misalignment and cross-section distortion of the fibre bundles were directly incorporated in the finite element mesh. 2D images of the composite were also used for the characterization of the porosity in the composite. The effect of these micro structural imperfections was studies by assuming perfect bonding at the bundle/matrix interface. The initial mechanical properties of the composite were obtained from unit cell analysis using asymptotic homogenization and moduli in x, y and z directions were 39, 25 and 44 GPa. However, matrix and bundle/matrix interfacial cracks were also clearly visible in the X-ray tomographic images. Later, the effects of debonding was incorporated by using frictional cohesive interaction at bundle/matrix interfaces and matrix cracking was modeled by degrading the elastic properties of matrix. Final, the response of the composite was studied under six individual load cases.Associação Brasileira de Ciências Mecânicas2014-03-01info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersiontext/htmlhttp://old.scielo.br/scielo.php?script=sci_arttext&pid=S1679-78252014000200002Latin American Journal of Solids and Structures v.11 n.2 2014reponame:Latin American journal of solids and structures (Online)instname:Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)instacron:ABCM10.1590/S1679-78252014000200002info:eu-repo/semantics/openAccessSharma,RajneeshBhagat,Atul RameshMahajan,Puneeteng2013-07-30T00:00:00Zoai:scielo:S1679-78252014000200002Revistahttp://www.scielo.br/scielo.php?script=sci_serial&pid=1679-7825&lng=pt&nrm=isohttps://old.scielo.br/oai/scielo-oai.phpabcm@abcm.org.br||maralves@usp.br1679-78251679-7817opendoar:2013-07-30T00:00Latin American journal of solids and structures (Online) - Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)false
dc.title.none.fl_str_mv Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructure
title Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructure
spellingShingle Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructure
Sharma,Rajneesh
Carbon/Carbon composites
Homogenization
X-ray tomography reconstruction
Image based FEM
Cohesive surfaces
title_short Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructure
title_full Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructure
title_fullStr Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructure
title_full_unstemmed Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructure
title_sort Finite element analysis for mechanical characterization of 4D inplane carbon/carbon composite with imperfect microstructure
author Sharma,Rajneesh
author_facet Sharma,Rajneesh
Bhagat,Atul Ramesh
Mahajan,Puneet
author_role author
author2 Bhagat,Atul Ramesh
Mahajan,Puneet
author2_role author
author
dc.contributor.author.fl_str_mv Sharma,Rajneesh
Bhagat,Atul Ramesh
Mahajan,Puneet
dc.subject.por.fl_str_mv Carbon/Carbon composites
Homogenization
X-ray tomography reconstruction
Image based FEM
Cohesive surfaces
topic Carbon/Carbon composites
Homogenization
X-ray tomography reconstruction
Image based FEM
Cohesive surfaces
description Finite element mesh of multi-directional 4D carbon/carbon (C/C) composite was reconstructed from 2D images obtained by X-ray tomography. Thus, imperfections in the composite such as voids, misalignment and cross-section distortion of the fibre bundles were directly incorporated in the finite element mesh. 2D images of the composite were also used for the characterization of the porosity in the composite. The effect of these micro structural imperfections was studies by assuming perfect bonding at the bundle/matrix interface. The initial mechanical properties of the composite were obtained from unit cell analysis using asymptotic homogenization and moduli in x, y and z directions were 39, 25 and 44 GPa. However, matrix and bundle/matrix interfacial cracks were also clearly visible in the X-ray tomographic images. Later, the effects of debonding was incorporated by using frictional cohesive interaction at bundle/matrix interfaces and matrix cracking was modeled by degrading the elastic properties of matrix. Final, the response of the composite was studied under six individual load cases.
publishDate 2014
dc.date.none.fl_str_mv 2014-03-01
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1679-78252014000200002
url http://old.scielo.br/scielo.php?script=sci_arttext&pid=S1679-78252014000200002
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv 10.1590/S1679-78252014000200002
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv text/html
dc.publisher.none.fl_str_mv Associação Brasileira de Ciências Mecânicas
publisher.none.fl_str_mv Associação Brasileira de Ciências Mecânicas
dc.source.none.fl_str_mv Latin American Journal of Solids and Structures v.11 n.2 2014
reponame:Latin American journal of solids and structures (Online)
instname:Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron:ABCM
instname_str Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron_str ABCM
institution ABCM
reponame_str Latin American journal of solids and structures (Online)
collection Latin American journal of solids and structures (Online)
repository.name.fl_str_mv Latin American journal of solids and structures (Online) - Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
repository.mail.fl_str_mv abcm@abcm.org.br||maralves@usp.br
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