Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression

Autores
Xiong, Jian; Zhang, Meng; Stocchi, Ariel Leonardo; Hong, Hu; Ma, Li; Wu, Linzhi; Zhang, Zhong
Año de publicación
2013
Idioma
inglés
Tipo de recurso
artículo
Estado
versión publicada
Descripción
Mechanical properties and failure modes of carbon fiber composite egg and pyramidal honeycombs cores under in plane compression were studied in the present paper. An interlocking method was developed for both kinds of three-dimensional honeycombs. Euler or core shear macro-buckling, face wrinkling, face inter-cell buckling, core member crushing and face sheet crushing were considered and theoretical relationships for predicting the failure load associated with each mode were presented. Failure mechanism maps were constructed to predict the failure of these composite sandwich panels subjected to in-plane compression. The response of the sandwich panels under axial compression was measured up to failure. The measured peak loads obtained in the experiments showed a good agreement with the analytical predictions. The finite element method was used to investigate the Euler buckling of sandwich beams made with two different honeycomb cores and the comparisons between two kinds of honeycomb cores were conducted.
Fil: Xiong, Jian. Harbin Institute of Technology. Center for Composite Materials and Structures; China
Fil: Zhang, Meng. Harbin Institute of Technology. Center for Composite Materials and Structures; China
Fil: Stocchi, Ariel Leonardo. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Mar del Plata. Instituto de Investigación En Ciencia y Tecnología de Materiales (i); Argentina. Universidad Nacional de Mar del Plata. Facultad de Ingeniería; Argentina
Fil: Hong, Hu. The Hong Kong Polytechnic University; China
Fil: Ma, Li. Harbin Institute of Technology. Center for Composite Materials and Structures; China
Fil: Wu, Linzhi. Harbin Institute of Technology. Center for Composite Materials and Structures; China
Fil: Zhang, Zhong. Beijing Institute of Structure and Environment Engineering; China
Materia
Honeycomb
Mechanical Properties
Analytical Modelling
Mechanical Testing
Nivel de accesibilidad
acceso abierto
Condiciones de uso
https://creativecommons.org/licenses/by-nc-nd/2.5/ar/
Repositorio
CONICET Digital (CONICET)
Institución
Consejo Nacional de Investigaciones Científicas y Técnicas
OAI Identificador
oai:ri.conicet.gov.ar:11336/5529
Acceder
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oai_identifier_str oai:ri.conicet.gov.ar:11336/5529
network_acronym_str CONICETDig
repository_id_str 3498
network_name_str CONICET Digital (CONICET)
spelling Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compressionXiong, JianZhang, MengStocchi, Ariel LeonardoHong, HuMa, LiWu, LinzhiZhang, ZhongHoneycombMechanical PropertiesAnalytical ModellingMechanical Testinghttps://purl.org/becyt/ford/2.5https://purl.org/becyt/ford/2Mechanical properties and failure modes of carbon fiber composite egg and pyramidal honeycombs cores under in plane compression were studied in the present paper. An interlocking method was developed for both kinds of three-dimensional honeycombs. Euler or core shear macro-buckling, face wrinkling, face inter-cell buckling, core member crushing and face sheet crushing were considered and theoretical relationships for predicting the failure load associated with each mode were presented. Failure mechanism maps were constructed to predict the failure of these composite sandwich panels subjected to in-plane compression. The response of the sandwich panels under axial compression was measured up to failure. The measured peak loads obtained in the experiments showed a good agreement with the analytical predictions. The finite element method was used to investigate the Euler buckling of sandwich beams made with two different honeycomb cores and the comparisons between two kinds of honeycomb cores were conducted.Fil: Xiong, Jian. Harbin Institute of Technology. Center for Composite Materials and Structures; ChinaFil: Zhang, Meng. Harbin Institute of Technology. Center for Composite Materials and Structures; ChinaFil: Stocchi, Ariel Leonardo. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Mar del Plata. Instituto de Investigación En Ciencia y Tecnología de Materiales (i); Argentina. Universidad Nacional de Mar del Plata. Facultad de Ingeniería; ArgentinaFil: Hong, Hu. The Hong Kong Polytechnic University; ChinaFil: Ma, Li. Harbin Institute of Technology. Center for Composite Materials and Structures; ChinaFil: Wu, Linzhi. Harbin Institute of Technology. Center for Composite Materials and Structures; ChinaFil: Zhang, Zhong. Beijing Institute of Structure and Environment Engineering; ChinaElsevier2013-12-31info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionhttp://purl.org/coar/resource_type/c_6501info:ar-repo/semantics/articuloapplication/pdfapplication/pdfhttp://hdl.handle.net/11336/5529Xiong, Jian; Zhang, Meng; Stocchi, Ariel Leonardo; Hong, Hu; Ma, Li; et al.; Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression; Elsevier; Composites Part B: Engineering; 60; 31-12-2013; 350-3581359-8368enginfo:eu-repo/semantics/altIdentifier/url/http://www.sciencedirect.com/science/article/pii/S1359836813007798info:eu-repo/semantics/altIdentifier/doi/info:eu-repo/semantics/altIdentifier/doi/10.1016/j.compositesb.2013.12.049info:eu-repo/semantics/openAccesshttps://creativecommons.org/licenses/by-nc-nd/2.5/ar/reponame:CONICET Digital (CONICET)instname:Consejo Nacional de Investigaciones Científicas y Técnicas2025-09-29T10:12:02Zoai:ri.conicet.gov.ar:11336/5529instacron: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 10:12:02.334CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicasfalse
dc.title.none.fl_str_mv Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression
title Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression
spellingShingle Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression
Xiong, Jian
Honeycomb
Mechanical Properties
Analytical Modelling
Mechanical Testing
title_short Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression
title_full Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression
title_fullStr Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression
title_full_unstemmed Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression
title_sort Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression
dc.creator.none.fl_str_mv Xiong, Jian
Zhang, Meng
Stocchi, Ariel Leonardo
Hong, Hu
Ma, Li
Wu, Linzhi
Zhang, Zhong
author Xiong, Jian
author_facet Xiong, Jian
Zhang, Meng
Stocchi, Ariel Leonardo
Hong, Hu
Ma, Li
Wu, Linzhi
Zhang, Zhong
author_role author
author2 Zhang, Meng
Stocchi, Ariel Leonardo
Hong, Hu
Ma, Li
Wu, Linzhi
Zhang, Zhong
author2_role author
author
author
author
author
author
dc.subject.none.fl_str_mv Honeycomb
Mechanical Properties
Analytical Modelling
Mechanical Testing
topic Honeycomb
Mechanical Properties
Analytical Modelling
Mechanical Testing
purl_subject.fl_str_mv https://purl.org/becyt/ford/2.5
https://purl.org/becyt/ford/2
dc.description.none.fl_txt_mv Mechanical properties and failure modes of carbon fiber composite egg and pyramidal honeycombs cores under in plane compression were studied in the present paper. An interlocking method was developed for both kinds of three-dimensional honeycombs. Euler or core shear macro-buckling, face wrinkling, face inter-cell buckling, core member crushing and face sheet crushing were considered and theoretical relationships for predicting the failure load associated with each mode were presented. Failure mechanism maps were constructed to predict the failure of these composite sandwich panels subjected to in-plane compression. The response of the sandwich panels under axial compression was measured up to failure. The measured peak loads obtained in the experiments showed a good agreement with the analytical predictions. The finite element method was used to investigate the Euler buckling of sandwich beams made with two different honeycomb cores and the comparisons between two kinds of honeycomb cores were conducted.
Fil: Xiong, Jian. Harbin Institute of Technology. Center for Composite Materials and Structures; China
Fil: Zhang, Meng. Harbin Institute of Technology. Center for Composite Materials and Structures; China
Fil: Stocchi, Ariel Leonardo. Consejo Nacional de Investigaciones Científicas y Técnicas. Centro Científico Tecnológico Mar del Plata. Instituto de Investigación En Ciencia y Tecnología de Materiales (i); Argentina. Universidad Nacional de Mar del Plata. Facultad de Ingeniería; Argentina
Fil: Hong, Hu. The Hong Kong Polytechnic University; China
Fil: Ma, Li. Harbin Institute of Technology. Center for Composite Materials and Structures; China
Fil: Wu, Linzhi. Harbin Institute of Technology. Center for Composite Materials and Structures; China
Fil: Zhang, Zhong. Beijing Institute of Structure and Environment Engineering; China
description Mechanical properties and failure modes of carbon fiber composite egg and pyramidal honeycombs cores under in plane compression were studied in the present paper. An interlocking method was developed for both kinds of three-dimensional honeycombs. Euler or core shear macro-buckling, face wrinkling, face inter-cell buckling, core member crushing and face sheet crushing were considered and theoretical relationships for predicting the failure load associated with each mode were presented. Failure mechanism maps were constructed to predict the failure of these composite sandwich panels subjected to in-plane compression. The response of the sandwich panels under axial compression was measured up to failure. The measured peak loads obtained in the experiments showed a good agreement with the analytical predictions. The finite element method was used to investigate the Euler buckling of sandwich beams made with two different honeycomb cores and the comparisons between two kinds of honeycomb cores were conducted.
publishDate 2013
dc.date.none.fl_str_mv 2013-12-31
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/11336/5529
Xiong, Jian; Zhang, Meng; Stocchi, Ariel Leonardo; Hong, Hu; Ma, Li; et al.; Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression; Elsevier; Composites Part B: Engineering; 60; 31-12-2013; 350-358
1359-8368
url http://hdl.handle.net/11336/5529
identifier_str_mv Xiong, Jian; Zhang, Meng; Stocchi, Ariel Leonardo; Hong, Hu; Ma, Li; et al.; Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression; Elsevier; Composites Part B: Engineering; 60; 31-12-2013; 350-358
1359-8368
dc.language.none.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv info:eu-repo/semantics/altIdentifier/url/http://www.sciencedirect.com/science/article/pii/S1359836813007798
info:eu-repo/semantics/altIdentifier/doi/
info:eu-repo/semantics/altIdentifier/doi/10.1016/j.compositesb.2013.12.049
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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score 13.070432

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