Non-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites
Descripción del Articulo
The mechanical behavior of advanced composites can be modeled mathematically through unknown variables and Shear Strain Thickness Functions (SSTFs). Such SSTFs can be of polynomial or non-polynomial nature and some parameters of non-polynomial SSTFs can be optimized to get optimal results. In this p...
| Autores: | , , |
|---|---|
| Formato: | artículo |
| Fecha de Publicación: | 2019 |
| Institución: | Universidad de Ingeniería y tecnología |
| Repositorio: | UTEC-Institucional |
| Lenguaje: | inglés |
| OAI Identifier: | oai:repositorio.utec.edu.pe:20.500.12815/198 |
| Enlace del recurso: | https://hdl.handle.net/20.500.12815/198 https://doi.org/10.1016/j.cja.2019.02.001 |
| Nivel de acceso: | acceso abierto |
| Materia: | Composite materials Plates (structural components) Plating Shear deformation Shear strain Carrera unified formulations Equivalent single layers Principle of virtual displacements Shear deformation theory Stress and displacements Thickness distributions Trigonometric functions Zig-zag effects Polynomials |
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Mantari, J.LRamos, I.AMonge, J.C.2021-03-16T23:23:01Z2021-03-16T23:23:01Z2019-041000-9361https://hdl.handle.net/20.500.12815/198https://doi.org/10.1016/j.cja.2019.02.001Chinese Journal of AeronauticsThe mechanical behavior of advanced composites can be modeled mathematically through unknown variables and Shear Strain Thickness Functions (SSTFs). Such SSTFs can be of polynomial or non-polynomial nature and some parameters of non-polynomial SSTFs can be optimized to get optimal results. In this paper, these parameters are called “r” and “s” and they are the argument of the trigonometric SSTFs introduced within the Carrera Unified Formulation (CUF). The Equivalent Single Layer (ESL) governing equations are obtained by employing the Principle of Virtual Displacement (PVD) and are solved using Navier method solution. Furthermore, trigonometric expansion with Murakami theory was implemented in order to reproduce the Zig-Zag effects which are important for multilayer structures. Several combinations of optimization parameters are evaluated and selected by different criteria of average error. Results of the present unified trigonometrical theory with CUF bases confirm that it is possible to improve the stress and displacement results through the thickness distribution of models with reduced unknown variables. Since the idea is to find a theory with reduced numbers of unknowns, the present method appears to be an appropriate technique to select a simple model. However these optimization parameters depend on the plate geometry and the order of expansion or unknown variables. So, the topic deserves further research.application/pdfengElsevierinfo:eu-repo/semantics/openAccesshttp://creativecommons.org/licenses/by-nc-nd/4.0/Repositorio Institucional UTECUniversidad de Ingeniería y Tecnología - UTECreponame:UTEC-Institucionalinstname:Universidad de Ingeniería y tecnologíainstacron:UTECComposite materialsPlates (structural components)PlatingShear deformationShear strainCarrera unified formulationsEquivalent single layersPrinciple of virtual displacementsShear deformation theoryStress and displacementsThickness distributionsTrigonometric functionsZig-zag effectsPolynomialsNon-polynomial Zig-Zag and ESL shear deformation theory to study advanced compositesinfo:eu-repo/semantics/articleORIGINAL10.1016j.cja.2019.02.001.pdf10.1016j.cja.2019.02.001.pdf10.1016j.cja.2019.02.001application/pdf4090646http://repositorio.utec.edu.pe/bitstream/20.500.12815/198/1/10.1016j.cja.2019.02.001.pdfb40d97bb3efcdf660b35d663405e00f9MD51open accessTEXT10.1016j.cja.2019.02.001.pdf.txt10.1016j.cja.2019.02.001.pdf.txtExtracted texttext/plain44943http://repositorio.utec.edu.pe/bitstream/20.500.12815/198/6/10.1016j.cja.2019.02.001.pdf.txtdca01c1b9aeab0187c782079fd1758f2MD56open accessTHUMBNAIL10.1016j.cja.2019.02.001.pdf.jpg10.1016j.cja.2019.02.001.pdf.jpgGenerated Thumbnailimage/jpeg13114http://repositorio.utec.edu.pe/bitstream/20.500.12815/198/7/10.1016j.cja.2019.02.001.pdf.jpgf1d02d5e3d8623b3eda563e7b516ad82MD57open access20.500.12815/198oai:repositorio.utec.edu.pe:20.500.12815/1982024-04-10 15:56:58.956open accessRepositorio Institucional UTECrepositorio@utec.edu.pe |
| dc.title.es_PE.fl_str_mv |
Non-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites |
| title |
Non-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites |
| spellingShingle |
Non-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites Mantari, J.L Composite materials Plates (structural components) Plating Shear deformation Shear strain Carrera unified formulations Equivalent single layers Principle of virtual displacements Shear deformation theory Stress and displacements Thickness distributions Trigonometric functions Zig-zag effects Polynomials |
| title_short |
Non-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites |
| title_full |
Non-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites |
| title_fullStr |
Non-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites |
| title_full_unstemmed |
Non-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites |
| title_sort |
Non-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites |
| author |
Mantari, J.L |
| author_facet |
Mantari, J.L Ramos, I.A Monge, J.C. |
| author_role |
author |
| author2 |
Ramos, I.A Monge, J.C. |
| author2_role |
author author |
| dc.contributor.author.fl_str_mv |
Mantari, J.L Ramos, I.A Monge, J.C. |
| dc.subject.es_PE.fl_str_mv |
Composite materials Plates (structural components) Plating Shear deformation Shear strain Carrera unified formulations Equivalent single layers Principle of virtual displacements Shear deformation theory Stress and displacements Thickness distributions Trigonometric functions Zig-zag effects Polynomials |
| topic |
Composite materials Plates (structural components) Plating Shear deformation Shear strain Carrera unified formulations Equivalent single layers Principle of virtual displacements Shear deformation theory Stress and displacements Thickness distributions Trigonometric functions Zig-zag effects Polynomials |
| description |
The mechanical behavior of advanced composites can be modeled mathematically through unknown variables and Shear Strain Thickness Functions (SSTFs). Such SSTFs can be of polynomial or non-polynomial nature and some parameters of non-polynomial SSTFs can be optimized to get optimal results. In this paper, these parameters are called “r” and “s” and they are the argument of the trigonometric SSTFs introduced within the Carrera Unified Formulation (CUF). The Equivalent Single Layer (ESL) governing equations are obtained by employing the Principle of Virtual Displacement (PVD) and are solved using Navier method solution. Furthermore, trigonometric expansion with Murakami theory was implemented in order to reproduce the Zig-Zag effects which are important for multilayer structures. Several combinations of optimization parameters are evaluated and selected by different criteria of average error. Results of the present unified trigonometrical theory with CUF bases confirm that it is possible to improve the stress and displacement results through the thickness distribution of models with reduced unknown variables. Since the idea is to find a theory with reduced numbers of unknowns, the present method appears to be an appropriate technique to select a simple model. However these optimization parameters depend on the plate geometry and the order of expansion or unknown variables. So, the topic deserves further research. |
| publishDate |
2019 |
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2021-03-16T23:23:01Z |
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2021-03-16T23:23:01Z |
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2019-04 |
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info:eu-repo/semantics/article |
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article |
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1000-9361 |
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https://hdl.handle.net/20.500.12815/198 |
| dc.identifier.doi.es_PE.fl_str_mv |
https://doi.org/10.1016/j.cja.2019.02.001 |
| dc.identifier.journal.es_PE.fl_str_mv |
Chinese Journal of Aeronautics |
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1000-9361 Chinese Journal of Aeronautics |
| url |
https://hdl.handle.net/20.500.12815/198 https://doi.org/10.1016/j.cja.2019.02.001 |
| dc.language.iso.es_PE.fl_str_mv |
eng |
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eng |
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http://creativecommons.org/licenses/by-nc-nd/4.0/ |
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Elsevier |
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Repositorio Institucional UTEC Universidad de Ingeniería y Tecnología - UTEC |
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La información contenida en este registro es de entera responsabilidad de la institución que gestiona el repositorio institucional donde esta contenido este documento o set de datos. El CONCYTEC no se hace responsable por los contenidos (publicaciones y/o datos) accesibles a través del Repositorio Nacional Digital de Ciencia, Tecnología e Innovación de Acceso Abierto (ALICIA).