Numerical analysis of RC plane structures: a concentrated nonlinear effect approach

Detalhes bibliográficos
Autor(a) principal: Lemes, I. J. M.
Data de Publicação: 2018
Outros Autores: Barros, R. C., Silveira, R. A. M., Silva, A. R. D., Rocha, P. A. S.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Institucional da UFLA
Texto Completo: http://repositorio.ufla.br/jspui/handle/1/33701
Resumo: The present work aims to study the nonlinear behavior of reinforced concrete structures via Refined Plastic Hinge Method (RPHM). Pseudo-springs are used at the finite element ends, where the gradual loss of stiffness is determined by the combination of the normal force and bending moment (NM) in the cross section. The limiting of the uncracked, elastic and plastic regimes is done in the NM diagram. The concrete cracking is explicitly simulated with two approaches to calculate the effective moment of inertia of the cross section. The displacement-based formulation is referenced to the co-rotational system and coupled with continuation strategies to allow to overcome the possible critical points in the equilibrium paths. For validation of the numerical simulations, the results found with the proposed formulation are confronted with experimental and numerical data present in literature.
id UFLA_d2cba07ce0f0413082e88784d90936d7
oai_identifier_str oai:localhost:1/33701
network_acronym_str UFLA
network_name_str Repositório Institucional da UFLA
repository_id_str
spelling Numerical analysis of RC plane structures: a concentrated nonlinear effect approachRC structuresInteraction curvesConcentrated plasticityRefined plastic hinge methodEstruturas RCCurvas de interaçãoPlasticidade concentradaMétodo de dobradura plástica refinadaThe present work aims to study the nonlinear behavior of reinforced concrete structures via Refined Plastic Hinge Method (RPHM). Pseudo-springs are used at the finite element ends, where the gradual loss of stiffness is determined by the combination of the normal force and bending moment (NM) in the cross section. The limiting of the uncracked, elastic and plastic regimes is done in the NM diagram. The concrete cracking is explicitly simulated with two approaches to calculate the effective moment of inertia of the cross section. The displacement-based formulation is referenced to the co-rotational system and coupled with continuation strategies to allow to overcome the possible critical points in the equilibrium paths. For validation of the numerical simulations, the results found with the proposed formulation are confronted with experimental and numerical data present in literature.Associação Brasileira de Ciências Mecânicas2019-04-23T13:25:23Z2019-04-23T13:25:23Z2018info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfLEMES, I. J. M. et al. Numerical analysis of RC plane structures: a concentrated nonlinear effect approach. Latin American Journal of Solids and Structures, Rio de Janeiro, v. 15, n. 2, p. 1-22, 2018. DOI: http://dx.doi.org/10.1590/1679-78254681.http://repositorio.ufla.br/jspui/handle/1/33701Latin American Journal of Solids and Structuresreponame:Repositório Institucional da UFLAinstname:Universidade Federal de Lavras (UFLA)instacron:UFLAhttp://creativecommons.org/licenses/by/4.0/info:eu-repo/semantics/openAccessLemes, I. J. M.Barros, R. C.Silveira, R. A. M.Silva, A. R. D.Rocha, P. A. S.eng2023-05-02T18:42:27Zoai:localhost:1/33701Repositório InstitucionalPUBhttp://repositorio.ufla.br/oai/requestnivaldo@ufla.br || repositorio.biblioteca@ufla.bropendoar:2023-05-02T18:42:27Repositório Institucional da UFLA - Universidade Federal de Lavras (UFLA)false
dc.title.none.fl_str_mv Numerical analysis of RC plane structures: a concentrated nonlinear effect approach
title Numerical analysis of RC plane structures: a concentrated nonlinear effect approach
spellingShingle Numerical analysis of RC plane structures: a concentrated nonlinear effect approach
Lemes, I. J. M.
RC structures
Interaction curves
Concentrated plasticity
Refined plastic hinge method
Estruturas RC
Curvas de interação
Plasticidade concentrada
Método de dobradura plástica refinada
title_short Numerical analysis of RC plane structures: a concentrated nonlinear effect approach
title_full Numerical analysis of RC plane structures: a concentrated nonlinear effect approach
title_fullStr Numerical analysis of RC plane structures: a concentrated nonlinear effect approach
title_full_unstemmed Numerical analysis of RC plane structures: a concentrated nonlinear effect approach
title_sort Numerical analysis of RC plane structures: a concentrated nonlinear effect approach
author Lemes, I. J. M.
author_facet Lemes, I. J. M.
Barros, R. C.
Silveira, R. A. M.
Silva, A. R. D.
Rocha, P. A. S.
author_role author
author2 Barros, R. C.
Silveira, R. A. M.
Silva, A. R. D.
Rocha, P. A. S.
author2_role author
author
author
author
dc.contributor.author.fl_str_mv Lemes, I. J. M.
Barros, R. C.
Silveira, R. A. M.
Silva, A. R. D.
Rocha, P. A. S.
dc.subject.por.fl_str_mv RC structures
Interaction curves
Concentrated plasticity
Refined plastic hinge method
Estruturas RC
Curvas de interação
Plasticidade concentrada
Método de dobradura plástica refinada
topic RC structures
Interaction curves
Concentrated plasticity
Refined plastic hinge method
Estruturas RC
Curvas de interação
Plasticidade concentrada
Método de dobradura plástica refinada
description The present work aims to study the nonlinear behavior of reinforced concrete structures via Refined Plastic Hinge Method (RPHM). Pseudo-springs are used at the finite element ends, where the gradual loss of stiffness is determined by the combination of the normal force and bending moment (NM) in the cross section. The limiting of the uncracked, elastic and plastic regimes is done in the NM diagram. The concrete cracking is explicitly simulated with two approaches to calculate the effective moment of inertia of the cross section. The displacement-based formulation is referenced to the co-rotational system and coupled with continuation strategies to allow to overcome the possible critical points in the equilibrium paths. For validation of the numerical simulations, the results found with the proposed formulation are confronted with experimental and numerical data present in literature.
publishDate 2018
dc.date.none.fl_str_mv 2018
2019-04-23T13:25:23Z
2019-04-23T13:25:23Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv LEMES, I. J. M. et al. Numerical analysis of RC plane structures: a concentrated nonlinear effect approach. Latin American Journal of Solids and Structures, Rio de Janeiro, v. 15, n. 2, p. 1-22, 2018. DOI: http://dx.doi.org/10.1590/1679-78254681.
http://repositorio.ufla.br/jspui/handle/1/33701
identifier_str_mv LEMES, I. J. M. et al. Numerical analysis of RC plane structures: a concentrated nonlinear effect approach. Latin American Journal of Solids and Structures, Rio de Janeiro, v. 15, n. 2, p. 1-22, 2018. DOI: http://dx.doi.org/10.1590/1679-78254681.
url http://repositorio.ufla.br/jspui/handle/1/33701
dc.language.iso.fl_str_mv eng
language eng
dc.rights.driver.fl_str_mv http://creativecommons.org/licenses/by/4.0/
info:eu-repo/semantics/openAccess
rights_invalid_str_mv http://creativecommons.org/licenses/by/4.0/
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
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
reponame:Repositório Institucional da UFLA
instname:Universidade Federal de Lavras (UFLA)
instacron:UFLA
instname_str Universidade Federal de Lavras (UFLA)
instacron_str UFLA
institution UFLA
reponame_str Repositório Institucional da UFLA
collection Repositório Institucional da UFLA
repository.name.fl_str_mv Repositório Institucional da UFLA - Universidade Federal de Lavras (UFLA)
repository.mail.fl_str_mv nivaldo@ufla.br || repositorio.biblioteca@ufla.br
_version_ 1815439197104766976