Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells

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El texto completo de este trabajo no está disponible en el Repositorio Académico UPC por restricciones de la casa editorial donde ha sido publicado.
Detalles Bibliográficos
Autores: Monge, J. C., Mantari, J. L., Arciniega, R. A.
Formato: artículo
Fecha de Publicación:2020
Institución:Universidad Peruana de Ciencias Aplicadas
Repositorio:UPC-Institucional
Lenguaje:inglés
OAI Identifier:oai:repositorioacademico.upc.edu.pe:10757/656405
Enlace del recurso:http://hdl.handle.net/10757/656405
Nivel de acceso:acceso embargado
Materia:Equilibrium Equations
Laminated composite
Sandwich Structures
Shell
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dc.title.en_US.fl_str_mv Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells
title Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells
spellingShingle Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells
Monge, J. C.
Equilibrium Equations
Laminated composite
Sandwich Structures
Shell
title_short Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells
title_full Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells
title_fullStr Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells
title_full_unstemmed Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells
title_sort Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells
author Monge, J. C.
author_facet Monge, J. C.
Mantari, J. L.
Arciniega, R. A.
author_role author
author2 Mantari, J. L.
Arciniega, R. A.
author2_role author
author
dc.contributor.author.fl_str_mv Monge, J. C.
Mantari, J. L.
Arciniega, R. A.
dc.subject.en_US.fl_str_mv Equilibrium Equations
Laminated composite
Sandwich Structures
Shell
topic Equilibrium Equations
Laminated composite
Sandwich Structures
Shell
description El texto completo de este trabajo no está disponible en el Repositorio Académico UPC por restricciones de la casa editorial donde ha sido publicado.
publishDate 2020
dc.date.accessioned.none.fl_str_mv 2021-06-08T13:00:42Z
dc.date.available.none.fl_str_mv 2021-06-08T13:00:42Z
dc.date.issued.fl_str_mv 2020-10-15
dc.type.en_US.fl_str_mv info:eu-repo/semantics/article
format article
dc.identifier.issn.none.fl_str_mv 01410296
dc.identifier.doi.none.fl_str_mv 10.1016/j.engstruct.2020.110938
dc.identifier.uri.none.fl_str_mv http://hdl.handle.net/10757/656405
dc.identifier.eissn.none.fl_str_mv 18737323
dc.identifier.journal.en_US.fl_str_mv Engineering Structures
dc.identifier.eid.none.fl_str_mv 2-s2.0-85087983584
dc.identifier.scopusid.none.fl_str_mv SCOPUS_ID:85087983584
dc.identifier.pii.none.fl_str_mv S0141029619354616
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identifier_str_mv 01410296
10.1016/j.engstruct.2020.110938
18737323
Engineering Structures
2-s2.0-85087983584
SCOPUS_ID:85087983584
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url http://hdl.handle.net/10757/656405
dc.language.iso.en_US.fl_str_mv eng
language eng
dc.relation.url.en_US.fl_str_mv https://www.sciencedirect.com/science/article/abs/pii/S0141029619354616
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dc.publisher.en_US.fl_str_mv Elsevier Ltd
dc.source.none.fl_str_mv reponame:UPC-Institucional
instname:Universidad Peruana de Ciencias Aplicadas
instacron:UPC
instname_str Universidad Peruana de Ciencias Aplicadas
instacron_str UPC
institution UPC
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collection UPC-Institucional
dc.source.journaltitle.none.fl_str_mv Engineering Structures
dc.source.volume.none.fl_str_mv 221
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https://repositorioacademico.upc.edu.pe/bitstream/10757/656405/1/license.txt
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spelling 1ab4da19501604b4a66fb77f554d6d8f300ce793fbc9dfb602a7033119b1c5382543be5aa610b96c77740439e04827deb9eMonge, J. C.Mantari, J. L.Arciniega, R. A.2021-06-08T13:00:42Z2021-06-08T13:00:42Z2020-10-150141029610.1016/j.engstruct.2020.110938http://hdl.handle.net/10757/65640518737323Engineering Structures2-s2.0-85087983584SCOPUS_ID:85087983584S01410296193546160000 0001 2196 144XEl texto completo de este trabajo no está disponible en el Repositorio Académico UPC por restricciones de la casa editorial donde ha sido publicado.In this paper, a three-dimensional numerical solution for the bending study of laminated composite doubly-curved shells is presented. The partial differential equations are solved analytically by the Navier summation for the midsurface variables; this method is only valid for shells with constant curvature where boundary conditions are considered simply supported. The partial differential equations present different coefficients, which depend on the thickness coordinates. A semi-analytical solution and the so-called Differential Quadrature Method are used to calculate an approximated derivative of a certain function by a weighted summation of the function evaluated in a certain grin domain. Each layer is discretized by a grid point distribution such as: Chebyshev-Gauss-Lobatto, Legendre, Ding and Uniform. As part of the formulation, the inter-laminar continuity conditions of displacements and transverse shear stresses between the interfaces of two layers are imposed. The proper traction conditions at the top and bottom of the shell due to applied transverse loadings are also considered. The present results are compared with other 3D solutions available in the literature, classical 2D models, Layer-wise models, etc. Comparison of the results show that the present formulation correctly predicts through-the-thickness distributions for stresses and displacements while maintaining a low computational cost.Consejo Nacional de Ciencia, Tecnología e Innovación Tecnológicaapplication/htmlengElsevier Ltdhttps://www.sciencedirect.com/science/article/abs/pii/S0141029619354616info:eu-repo/semantics/embargoedAccessEquilibrium EquationsLaminated compositeSandwich StructuresShellComputational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shellsinfo:eu-repo/semantics/articleEngineering Structures221reponame:UPC-Institucionalinstname:Universidad Peruana de Ciencias Aplicadasinstacron:UPCTHUMBNAILelsevier-thumbnail.pngapplication/octet-stream57707https://repositorioacademico.upc.edu.pe/bitstream/10757/656405/2/elsevier-thumbnail.png063758aa0d02d47887715447696e1d6aMD52falseLICENSElicense.txtlicense.txttext/plain; charset=utf-81748https://repositorioacademico.upc.edu.pe/bitstream/10757/656405/1/license.txt8a4605be74aa9ea9d79846c1fba20a33MD51false10757/656405oai:repositorioacademico.upc.edu.pe:10757/6564052021-06-09 09:15:52.128Repositorio académico upcupc@openrepository.comTk9URTogUExBQ0UgWU9VUiBPV04gTElDRU5TRSBIRVJFClRoaXMgc2FtcGxlIGxpY2Vuc2UgaXMgcHJvdmlkZWQgZm9yIGluZm9ybWF0aW9uYWwgcHVycG9zZXMgb25seS4KCk5PTi1FWENMVVNJVkUgRElTVFJJQlVUSU9OIExJQ0VOU0UKCkJ5IHNpZ25pbmcgYW5kIHN1Ym1pdHRpbmcgdGhpcyBsaWNlbnNlLCB5b3UgKHRoZSBhdXRob3Iocykgb3IgY29weXJpZ2h0Cm93bmVyKSBncmFudHMgdG8gRFNwYWNlIFVuaXZlcnNpdHkgKERTVSkgdGhlIG5vbi1leGNsdXNpdmUgcmlnaHQgdG8gcmVwcm9kdWNlLAp0cmFuc2xhdGUgKGFzIGRlZmluZWQgYmVsb3cpLCBhbmQvb3IgZGlzdHJpYnV0ZSB5b3VyIHN1Ym1pc3Npb24gKGluY2x1ZGluZwp0aGUgYWJzdHJhY3QpIHdvcmxkd2lkZSBpbiBwcmludCBhbmQgZWxlY3Ryb25pYyBmb3JtYXQgYW5kIGluIGFueSBtZWRpdW0sCmluY2x1ZGluZyBidXQgbm90IGxpbWl0ZWQgdG8gYXVkaW8gb3IgdmlkZW8uCgpZb3UgYWdyZWUgdGhhdCBEU1UgbWF5LCB3aXRob3V0IGNoYW5naW5nIHRoZSBjb250ZW50LCB0cmFuc2xhdGUgdGhlCnN1Ym1pc3Npb24gdG8gYW55IG1lZGl1bSBvciBmb3JtYXQgZm9yIHRoZSBwdXJwb3NlIG9mIHByZXNlcnZhdGlvbi4KCllvdSBhbHNvIGFncmVlIHRoYXQgRFNVIG1heSBrZWVwIG1vcmUgdGhhbiBvbmUgY29weSBvZiB0aGlzIHN1Ym1pc3Npb24gZm9yCnB1cnBvc2VzIG9mIHNlY3VyaXR5LCBiYWNrLXVwIGFuZCBwcmVzZXJ2YXRpb24uCgpZb3UgcmVwcmVzZW50IHRoYXQgdGhlIHN1Ym1pc3Npb24gaXMgeW91ciBvcmlnaW5hbCB3b3JrLCBhbmQgdGhhdCB5b3UgaGF2ZQp0aGUgcmlnaHQgdG8gZ3JhbnQgdGhlIHJpZ2h0cyBjb250YWluZWQgaW4gdGhpcyBsaWNlbnNlLiBZb3UgYWxzbyByZXByZXNlbnQKdGhhdCB5b3VyIHN1Ym1pc3Npb24gZG9lcyBub3QsIHRvIHRoZSBiZXN0IG9mIHlvdXIga25vd2xlZGdlLCBpbmZyaW5nZSB1cG9uCmFueW9uZSdzIGNvcHlyaWdodC4KCklmIHRoZSBzdWJtaXNzaW9uIGNvbnRhaW5zIG1hdGVyaWFsIGZvciB3aGljaCB5b3UgZG8gbm90IGhvbGQgY29weXJpZ2h0LAp5b3UgcmVwcmVzZW50IHRoYXQgeW91IGhhdmUgb2J0YWluZWQgdGhlIHVucmVzdHJpY3RlZCBwZXJtaXNzaW9uIG9mIHRoZQpjb3B5cmlnaHQgb3duZXIgdG8gZ3JhbnQgRFNVIHRoZSByaWdodHMgcmVxdWlyZWQgYnkgdGhpcyBsaWNlbnNlLCBhbmQgdGhhdApzdWNoIHRoaXJkLXBhcnR5IG93bmVkIG1hdGVyaWFsIGlzIGNsZWFybHkgaWRlbnRpZmllZCBhbmQgYWNrbm93bGVkZ2VkCndpdGhpbiB0aGUgdGV4dCBvciBjb250ZW50IG9mIHRoZSBzdWJtaXNzaW9uLgoKSUYgVEhFIFNVQk1JU1NJT04gSVMgQkFTRUQgVVBPTiBXT1JLIFRIQVQgSEFTIEJFRU4gU1BPTlNPUkVEIE9SIFNVUFBPUlRFRApCWSBBTiBBR0VOQ1kgT1IgT1JHQU5JWkFUSU9OIE9USEVSIFRIQU4gRFNVLCBZT1UgUkVQUkVTRU5UIFRIQVQgWU9VIEhBVkUKRlVMRklMTEVEIEFOWSBSSUdIVCBPRiBSRVZJRVcgT1IgT1RIRVIgT0JMSUdBVElPTlMgUkVRVUlSRUQgQlkgU1VDSApDT05UUkFDVCBPUiBBR1JFRU1FTlQuCgpEU1Ugd2lsbCBjbGVhcmx5IGlkZW50aWZ5IHlvdXIgbmFtZShzKSBhcyB0aGUgYXV0aG9yKHMpIG9yIG93bmVyKHMpIG9mIHRoZQpzdWJtaXNzaW9uLCBhbmQgd2lsbCBub3QgbWFrZSBhbnkgYWx0ZXJhdGlvbiwgb3RoZXIgdGhhbiBhcyBhbGxvd2VkIGJ5IHRoaXMKbGljZW5zZSwgdG8geW91ciBzdWJtaXNzaW9uLgo=
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Computational semi-analytical method for the 3D elasticity bending solution of laminated composite and sandwich doubly-curved shells
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