Implementation of the refined zigzag theory in shell elements with large displacements and rotations
- Autores
- Flores, Fernando Gabriel
- Año de publicación
- 2014
- Idioma
- inglés
- Tipo de recurso
- artículo
- Estado
- versión publicada
- Descripción
- This work shows a possible implementation of the refined zigzag theory in elements based on Simo’s shell theory. Refined zigzag theory can deal with composite laminate economically, adding only two nodal degrees of freedom, with very good accuracy. Two existing elements are considered, a four-node bi-linear quadrilateral and a six-node linear triangle. This geometry is enhanced with a hierarchical field of in-plane displacement expressed in convective coordinates. The objective is to have simple and efficient elements to analyze composite laminates under large displacements and rotations but small elastic strains. General aspects of the implementation are presented, and in particular the assumed natural strain technique used to prevent transverse shear locking. Several examples are considered to compare on the one hand with analytical static solutions and natural frequencies of plates, and on the other hand to observe the buckling loads and non-linear behavior with large displacement in double curved shells. In these latter cases comparisons are against numerical solutions obtained with solid elements. The results obtained are in a very good agreement with the targets used.
Fil: Flores, Fernando Gabriel. Universidad Nacional de Córdoba. Facultad de Ciencias Exactas Físicas y Naturales. Departamento de Estructuras; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina - Materia
-
Finite Elements
Shells
Refined Zigzag
Sandwich Laminate - Nivel de accesibilidad
- acceso abierto
- Condiciones de uso
- https://creativecommons.org/licenses/by-nc-nd/2.5/ar/
- Repositorio
- Institución
- Consejo Nacional de Investigaciones Científicas y Técnicas
- OAI Identificador
- oai:ri.conicet.gov.ar:11336/34416
Ver los metadatos del registro completo
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Implementation of the refined zigzag theory in shell elements with large displacements and rotationsFlores, Fernando GabrielFinite ElementsShellsRefined ZigzagSandwich Laminatehttps://purl.org/becyt/ford/2.3https://purl.org/becyt/ford/2This work shows a possible implementation of the refined zigzag theory in elements based on Simo’s shell theory. Refined zigzag theory can deal with composite laminate economically, adding only two nodal degrees of freedom, with very good accuracy. Two existing elements are considered, a four-node bi-linear quadrilateral and a six-node linear triangle. This geometry is enhanced with a hierarchical field of in-plane displacement expressed in convective coordinates. The objective is to have simple and efficient elements to analyze composite laminates under large displacements and rotations but small elastic strains. General aspects of the implementation are presented, and in particular the assumed natural strain technique used to prevent transverse shear locking. Several examples are considered to compare on the one hand with analytical static solutions and natural frequencies of plates, and on the other hand to observe the buckling loads and non-linear behavior with large displacement in double curved shells. In these latter cases comparisons are against numerical solutions obtained with solid elements. The results obtained are in a very good agreement with the targets used.Fil: Flores, Fernando Gabriel. Universidad Nacional de Córdoba. Facultad de Ciencias Exactas Físicas y Naturales. Departamento de Estructuras; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas; ArgentinaElsevier2014-08info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionhttp://purl.org/coar/resource_type/c_6501info:ar-repo/semantics/articuloapplication/pdfapplication/pdfhttp://hdl.handle.net/11336/34416Flores, Fernando Gabriel; Implementation of the refined zigzag theory in shell elements with large displacements and rotations; Elsevier; Composite Structures; 118; 8-2014; 560-5700263-8223CONICET DigitalCONICETenginfo:eu-repo/semantics/altIdentifier/doi/10.1016/j.compstruct.2014.07.034info:eu-repo/semantics/altIdentifier/url/https://www.sciencedirect.com/science/article/pii/S0263822314003572info:eu-repo/semantics/openAccesshttps://creativecommons.org/licenses/by-nc-nd/2.5/ar/reponame:CONICET Digital (CONICET)instname:Consejo Nacional de Investigaciones Científicas y Técnicas2025-09-29T09:40:13Zoai:ri.conicet.gov.ar:11336/34416instacron:CONICETInstitucionalhttp://ri.conicet.gov.ar/Organismo científico-tecnológicoNo correspondehttp://ri.conicet.gov.ar/oai/requestdasensio@conicet.gov.ar; lcarlino@conicet.gov.arArgentinaNo correspondeNo correspondeNo correspondeopendoar:34982025-09-29 09:40:13.302CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicasfalse |
dc.title.none.fl_str_mv |
Implementation of the refined zigzag theory in shell elements with large displacements and rotations |
title |
Implementation of the refined zigzag theory in shell elements with large displacements and rotations |
spellingShingle |
Implementation of the refined zigzag theory in shell elements with large displacements and rotations Flores, Fernando Gabriel Finite Elements Shells Refined Zigzag Sandwich Laminate |
title_short |
Implementation of the refined zigzag theory in shell elements with large displacements and rotations |
title_full |
Implementation of the refined zigzag theory in shell elements with large displacements and rotations |
title_fullStr |
Implementation of the refined zigzag theory in shell elements with large displacements and rotations |
title_full_unstemmed |
Implementation of the refined zigzag theory in shell elements with large displacements and rotations |
title_sort |
Implementation of the refined zigzag theory in shell elements with large displacements and rotations |
dc.creator.none.fl_str_mv |
Flores, Fernando Gabriel |
author |
Flores, Fernando Gabriel |
author_facet |
Flores, Fernando Gabriel |
author_role |
author |
dc.subject.none.fl_str_mv |
Finite Elements Shells Refined Zigzag Sandwich Laminate |
topic |
Finite Elements Shells Refined Zigzag Sandwich Laminate |
purl_subject.fl_str_mv |
https://purl.org/becyt/ford/2.3 https://purl.org/becyt/ford/2 |
dc.description.none.fl_txt_mv |
This work shows a possible implementation of the refined zigzag theory in elements based on Simo’s shell theory. Refined zigzag theory can deal with composite laminate economically, adding only two nodal degrees of freedom, with very good accuracy. Two existing elements are considered, a four-node bi-linear quadrilateral and a six-node linear triangle. This geometry is enhanced with a hierarchical field of in-plane displacement expressed in convective coordinates. The objective is to have simple and efficient elements to analyze composite laminates under large displacements and rotations but small elastic strains. General aspects of the implementation are presented, and in particular the assumed natural strain technique used to prevent transverse shear locking. Several examples are considered to compare on the one hand with analytical static solutions and natural frequencies of plates, and on the other hand to observe the buckling loads and non-linear behavior with large displacement in double curved shells. In these latter cases comparisons are against numerical solutions obtained with solid elements. The results obtained are in a very good agreement with the targets used. Fil: Flores, Fernando Gabriel. Universidad Nacional de Córdoba. Facultad de Ciencias Exactas Físicas y Naturales. Departamento de Estructuras; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina |
description |
This work shows a possible implementation of the refined zigzag theory in elements based on Simo’s shell theory. Refined zigzag theory can deal with composite laminate economically, adding only two nodal degrees of freedom, with very good accuracy. Two existing elements are considered, a four-node bi-linear quadrilateral and a six-node linear triangle. This geometry is enhanced with a hierarchical field of in-plane displacement expressed in convective coordinates. The objective is to have simple and efficient elements to analyze composite laminates under large displacements and rotations but small elastic strains. General aspects of the implementation are presented, and in particular the assumed natural strain technique used to prevent transverse shear locking. Several examples are considered to compare on the one hand with analytical static solutions and natural frequencies of plates, and on the other hand to observe the buckling loads and non-linear behavior with large displacement in double curved shells. In these latter cases comparisons are against numerical solutions obtained with solid elements. The results obtained are in a very good agreement with the targets used. |
publishDate |
2014 |
dc.date.none.fl_str_mv |
2014-08 |
dc.type.none.fl_str_mv |
info:eu-repo/semantics/article info:eu-repo/semantics/publishedVersion http://purl.org/coar/resource_type/c_6501 info:ar-repo/semantics/articulo |
format |
article |
status_str |
publishedVersion |
dc.identifier.none.fl_str_mv |
http://hdl.handle.net/11336/34416 Flores, Fernando Gabriel; Implementation of the refined zigzag theory in shell elements with large displacements and rotations; Elsevier; Composite Structures; 118; 8-2014; 560-570 0263-8223 CONICET Digital CONICET |
url |
http://hdl.handle.net/11336/34416 |
identifier_str_mv |
Flores, Fernando Gabriel; Implementation of the refined zigzag theory in shell elements with large displacements and rotations; Elsevier; Composite Structures; 118; 8-2014; 560-570 0263-8223 CONICET Digital CONICET |
dc.language.none.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
info:eu-repo/semantics/altIdentifier/doi/10.1016/j.compstruct.2014.07.034 info:eu-repo/semantics/altIdentifier/url/https://www.sciencedirect.com/science/article/pii/S0263822314003572 |
dc.rights.none.fl_str_mv |
info:eu-repo/semantics/openAccess https://creativecommons.org/licenses/by-nc-nd/2.5/ar/ |
eu_rights_str_mv |
openAccess |
rights_invalid_str_mv |
https://creativecommons.org/licenses/by-nc-nd/2.5/ar/ |
dc.format.none.fl_str_mv |
application/pdf application/pdf |
dc.publisher.none.fl_str_mv |
Elsevier |
publisher.none.fl_str_mv |
Elsevier |
dc.source.none.fl_str_mv |
reponame:CONICET Digital (CONICET) instname:Consejo Nacional de Investigaciones Científicas y Técnicas |
reponame_str |
CONICET Digital (CONICET) |
collection |
CONICET Digital (CONICET) |
instname_str |
Consejo Nacional de Investigaciones Científicas y Técnicas |
repository.name.fl_str_mv |
CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicas |
repository.mail.fl_str_mv |
dasensio@conicet.gov.ar; lcarlino@conicet.gov.ar |
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1844613272475533312 |
score |
13.070432 |