Structural design of the wing for URCUNINA (UAV)
El diseño del ala de URCUNINA (VANT) fue llevado a cabo. El diseño preliminar fue realizado usando restricciones aerodinámicas para proceder al diseño detallado con un análisis estructural. Para este proposito simulaciones en CFD fueron realizadas para obtener las las cargas sobre el ala, se requiri...
- Autores:
-
Pinto Delgado, Juan Sebastian
- Tipo de recurso:
- Trabajo de grado de pregrado
- Fecha de publicación:
- 2019
- Institución:
- Universidad Santo Tomás
- Repositorio:
- Repositorio Institucional USTA
- Idioma:
- spa
- OAI Identifier:
- oai:repository.usta.edu.co:11634/16725
- Acceso en línea:
- http://hdl.handle.net/11634/16725
- Palabra clave:
- Structural-Design
Wing
Composite
Abaqus
Layup
FEA
Tsai-Wu
Laminado
Elementos Finitos
Diseño
Diseño
Diseño Estructural
Materiales compuestos
Abaqus
Laminado
Elementos Finitos
Tsai-Wu
Ala
- Rights
- openAccess
- License
- Atribución-NoComercial-SinDerivadas 2.5 Colombia
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SANTTOMAS2 |
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Repositorio Institucional USTA |
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|
dc.title.spa.fl_str_mv |
Structural design of the wing for URCUNINA (UAV) |
title |
Structural design of the wing for URCUNINA (UAV) |
spellingShingle |
Structural design of the wing for URCUNINA (UAV) Structural-Design Wing Composite Abaqus Layup FEA Tsai-Wu Laminado Elementos Finitos Diseño Diseño Diseño Estructural Materiales compuestos Abaqus Laminado Elementos Finitos Tsai-Wu Ala |
title_short |
Structural design of the wing for URCUNINA (UAV) |
title_full |
Structural design of the wing for URCUNINA (UAV) |
title_fullStr |
Structural design of the wing for URCUNINA (UAV) |
title_full_unstemmed |
Structural design of the wing for URCUNINA (UAV) |
title_sort |
Structural design of the wing for URCUNINA (UAV) |
dc.creator.fl_str_mv |
Pinto Delgado, Juan Sebastian |
dc.contributor.advisor.spa.fl_str_mv |
Carvajal Bonilla, Elver Jofre |
dc.contributor.author.spa.fl_str_mv |
Pinto Delgado, Juan Sebastian |
dc.contributor.cvlac.spa.fl_str_mv |
https://scienti.colciencias.gov.co/cvlac/visualizador/generarCurriculoCv.do?cod_rh=0001403011 |
dc.subject.keyword.spa.fl_str_mv |
Structural-Design Wing Composite Abaqus Layup FEA Tsai-Wu |
topic |
Structural-Design Wing Composite Abaqus Layup FEA Tsai-Wu Laminado Elementos Finitos Diseño Diseño Diseño Estructural Materiales compuestos Abaqus Laminado Elementos Finitos Tsai-Wu Ala |
dc.subject.lemb.spa.fl_str_mv |
Laminado Elementos Finitos Diseño |
dc.subject.proposal.spa.fl_str_mv |
Diseño Diseño Estructural Materiales compuestos Abaqus Laminado Elementos Finitos Tsai-Wu Ala |
description |
El diseño del ala de URCUNINA (VANT) fue llevado a cabo. El diseño preliminar fue realizado usando restricciones aerodinámicas para proceder al diseño detallado con un análisis estructural. Para este proposito simulaciones en CFD fueron realizadas para obtener las las cargas sobre el ala, se requirió un proceso para transformar los datos de salida obtenidos por CFD a información que pueda ser suministrada al modelo de Elementos Finitos.Este proceso incluye recolección de datos, Matlab, extrapolaciones, ajustes polinomiales y construcción del diagrama V-n para tener datos que sirvan para alimentar el modelo de elementos finitos. El análisis fue hecho en el software comercial ABAQUS CAE. La comparación de 3 configuraciones en laminado dieron las herramientas para decidir la configuración estructural de la propuesta después de ser evaluada usando desplazamientos y teorias de falla. |
publishDate |
2019 |
dc.date.accessioned.spa.fl_str_mv |
2019-05-16T01:39:04Z |
dc.date.available.spa.fl_str_mv |
2019-05-16T01:39:04Z |
dc.date.issued.spa.fl_str_mv |
2019-01-22 |
dc.type.none.fl_str_mv |
bachelor thesis |
dc.type.local.spa.fl_str_mv |
Tesis de pregrado |
dc.type.version.none.fl_str_mv |
info:eu-repo/semantics/acceptedVersion |
dc.type.category.spa.fl_str_mv |
Formación de Recurso Humano para la Ctel: Trabajo de grado de Pregrado |
dc.type.coar.none.fl_str_mv |
http://purl.org/coar/resource_type/c_7a1f |
dc.type.drive.none.fl_str_mv |
info:eu-repo/semantics/bachelorThesis |
format |
http://purl.org/coar/resource_type/c_7a1f |
status_str |
acceptedVersion |
dc.identifier.citation.spa.fl_str_mv |
Pinto, J (2019). Structural design of the wing for URCUNINA (UAV). Universidad Santo Tomas, Bogotá, Colombia |
dc.identifier.uri.none.fl_str_mv |
http://hdl.handle.net/11634/16725 |
dc.identifier.reponame.spa.fl_str_mv |
reponame:Repositorio Institucional Universidad Santo Tomás |
dc.identifier.instname.spa.fl_str_mv |
instname:Universidad Santo Tomás |
dc.identifier.repourl.spa.fl_str_mv |
repourl:https://repository.usta.edu.co |
identifier_str_mv |
Pinto, J (2019). Structural design of the wing for URCUNINA (UAV). Universidad Santo Tomas, Bogotá, Colombia reponame:Repositorio Institucional Universidad Santo Tomás instname:Universidad Santo Tomás repourl:https://repository.usta.edu.co |
url |
http://hdl.handle.net/11634/16725 |
dc.language.iso.spa.fl_str_mv |
spa |
language |
spa |
dc.relation.references.spa.fl_str_mv |
@incollection{mcnutt1996seismic, title={Seismic monitoring and eruption forecasting of volcanoes: a review of the state-of-the-art and case histories}, author={McNutt, Stephen R}, booktitle={Monitoring and mitigation of volcano hazards}, pages={99--146}, year={1996}, publisher={Springer} } @article{Darmawan2018, author = {Darmawan, Herlan and Walter, Thomas R. and Brotopuspito, Kirbani Sri and Subandriyo and {I Gusti Made Agung Nandaka}}, doi = {10.1016/j.jvolgeores.2017.11.006}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Estrutura UAV/morphological and structural changes at the merapi lava dome.pdf:pdf}, issn = {03770273}, journal = {Journal of Volcanology and Geothermal Research}, keywords = {Digital elevation model,Lava dome,Merapi volcano,Photogrammetry,Structure from motion,Topography,Volcano monitoring}, mendeley-groups = {Referencias TCC}, pages = {256--267}, publisher = {Elsevier B.V.}, title = {{Morphological and structural changes at the Merapi lava dome monitored in 2012–15 using unmanned aerial vehicles (UAVs)}}, url = {https://doi.org/10.1016/j.jvolgeores.2017.11.006}, volume = {349}, year = {2018} } @techreport{Rosa2014, address = {Sao Carlos}, author = {Rosa, Maiara and Meunier, Nicolas and Augusto, Vitor and Sarmento, De Jesus and Santos, Yuri}, institution = {EESC}, mendeley-groups = {Docmentos por leer,Documentos referencias de TCC,Referencias TCC}, title = {{PROJETO GUIR{\'{A}} Projetos de Aeronaves II}}, year = {2014} } @article{Bravo-Mosquera2017, author = {Bravo-Mosquera, Pedro David and Botero-Bolivar, Laura and Acevedo-Giraldo, Daniel and Cer{\'{o}}n-Mu{\~{n}}oz, Hern{\'{a}}n Dar{\'{i}}o}, doi = {10.1016/j.ast.2017.09.005}, issn = {12709638}, journal = {Aerospace Science and Technology}, keywords = {Aerodynamic design,CFD,Conceptual design,UAV,Volcanic environments,Wind tunnel testing}, mendeley-groups = {Docmentos por leer,Referencias TCC}, pages = {600--614}, publisher = {Elsevier Masson SAS}, title = {{Aerodynamic design analysis of a UAV for superficial research of volcanic environments}}, url = {http://dx.doi.org/10.1016/j.ast.2017.09.005}, volume = {70}, year = {2017} } @article{Garre2017, author = {Garre, Parthasarathy and Arjun, Goli Venkata}, mendeley-groups = {Referencias TCC}, number = {Ii}, pages = {295--315}, title = {{Modeling and Analysis of a RIBS and Spars of An Airplane Wing for Bending and Shear Loads}}, volume = {5}, year = {2017} } @phdthesis{LimadeSousa2011, author = {{Lima de Sousa}, Eduardo Benedito}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Estrutura UAV/Estrutura fuselagem Material composito.pdf:pdf}, mendeley-groups = {Docmentos por leer,Referencias TCC}, pages = {97}, school = {Instituto Tecnologico de Aeron{\'{a}}utica ITA}, title = {{Projeto estrutural de fuselagem de vant em fibra de carbono}}, type = {DP}, volume = {1}, year = {2011} } @phdthesis{Narayan2009, author = {Narayan, Anirudh}, booktitle = {Mechanical Engineering}, mendeley-groups = {Docmentos por leer,Documentos referencias de TCC,Referencias TCC}, pages = {1--76}, school = {Brunel University, West London}, title = {{Conceptual Design of a Carbon-fibre Composite Aircraft And Finite Element Analysis of the Wing}}, volume = {1}, year = {2009} } @phdthesis{AsaLimadeSousa2011, author = {{Lima de Sousa}, Eduardo Benedito}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Estrutura UAV/Estrutura Asa Material composito.pdf:pdf}, mendeley-groups = {Docmentos por leer,Referencias TCC}, pages = {94}, school = {Instituto Tecnologico de Aeron{\'{a}}utica ITA}, title = {{Projeto estrutural da asa de vant em material composito}}, volume = {1}, year = {2011} } @phdthesis{Estructural2013, author = {{Nicol{\'{a}}s Castro}, Jos{\'{e}} and Coronado, William David and Eduardo, Luis}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Estrutura UAV/79561.pdf:pdf}, keywords = {aerodin{\'{a}}mico,criterio de falla,descripci{\'{o}}n del trabajo,diagrama vn,dise{\~{n}}ar la configuraci{\'{o}}n,elementos finitos,esfuerzo cortante,esfuerzo normal,factor de carga,fuerza de arrastre,fuerza de sustentaci{\'{o}}n,materiales compuestos,momento,pandeo lineal,s,se desea proponer y}, mendeley-groups = {Referencias TCC}, pages = {167}, school = {Universidad San Buenaventura}, title = {{Dise{\~{n}}o estructural del fuselaje, ala central y union ala-fuselaje para la aeronave no tripulada (UAV) experimental SKYCRUISER X-1}}, year = {2013} } @article{Mazhar2010, author = {Mazhar, Farrukh and Khan, Abdul Munem}, doi = {AIAA 2010-3099}, isbn = {9781600867422}, issn = {02734508}, journal = {Science And Technology}, mendeley-groups = {Docmentos por leer,Referencias TCC}, number = {April}, pages = {1--12}, title = {{Structural Design of a Uav Wing Using Finite}}, year = {2010} } @phdthesis{Estructural2013, author = {{Nicol{\'{a}}s Castro}, Jos{\'{e}} and Coronado, William David and Eduardo, Luis}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Estrutura UAV/79561.pdf:pdf}, keywords = {aerodin{\'{a}}mico,criterio de falla,descripci{\'{o}}n del trabajo,diagrama vn,dise{\~{n}}ar la configuraci{\'{o}}n,elementos finitos,esfuerzo cortante,esfuerzo normal,factor de carga,fuerza de arrastre,fuerza de sustentaci{\'{o}}n,materiales compuestos,momento,pandeo lineal,s,se desea proponer y}, mendeley-groups = {Referencias TCC}, pages = {167}, school = {Universidad San Buenaventura}, title = {{Dise{\~{n}}o estructural del fuselaje, ala central y union ala-fuselaje para la aeronave no tripulada (UAV) experimental SKYCRUISER X-1}}, year = {2013} } @phdthesis{Alcaraz2015, author = {Alcaraz, Daniel}, pages = {1--228}, school = {Universidad de Sevilla}, title = {{Dise{\~{n}}o estructural y construcci{\'{o}}n de un avi{\'{o}}n no tripulado : El Proyecto C{\'{e}}firo}}, year = {2015} } @phdthesis{Sebastian2016, author = {Sebasti{\'{a}}n, Esmeralda Castillo}, mendeley-groups = {Referencias TCC}, pages = {140}, school = {Universidad Politecnica de Valencia}, title = {{An{\'{a}}lisis de criterios de fallo para materiales compuestos}}, year = {2016} } @book{Daniel1970, author = {Daniel, I.M. and Ishai, Ori.}, booktitle = {Mechanics of Composite Materials}, doi = {10.1016/B978-0-08-006421-5.50049-6}, isbn = {9780080064215}, issn = {0037976X}, mendeley-groups = {Referencias TCC}, pages = {881--886}, pmid = {23153266}, title = {{Mechanics of Composite Materials}}, url = {http://linkinghub.elsevier.com/retrieve/pii/B9780080064215500496}, year = {1970} } @unpublished{Svensson1998, author = {Svensson, N and Shishoo, R and Gilchrist, M}, doi = {10.1177/089270579801100102}, institution = {Kansas University}, isbn = {9780387743646}, issn = {00379875}, mendeley-groups = {Referencias TCC}, series = {1}, title = {{Composite Materials}}, year = {1998} } @misc{abaqus2018web, author = {Web}, keywords = {abaqus}, mendeley-groups = {Referencias TCC}, mendeley-tags = {abaqus}, title = {{3D Cad Portal}}, url = {http://www.3dcadportal.com/abaqus-simulia.html}, year = {2018} } @misc{fem-web, author = {Https://br.comsol.com/multiphysics/finite-element-method}, booktitle = {15 march}, mendeley-groups = {Referencias TCC}, title = {{Explanation of the Finite Element Method}}, url = {https://br.comsol.com/multiphysics/finite-element-method}, year = {2016} } @article{Rodrigues2009, author = {Rodrigues, Luiz Eduardo Miranda Jos{\'{e}} and Queiroz, Fernana Figueir{\'{o}}}, journal = {AeroDesign Magazine}, keywords = {AeroDesign.,Desempenho de Avi{\~{o}}es,Diagrama v-n,Manobras,Rajadas}, mendeley-groups = {Referencias TCC}, pages = {1--5}, title = {{Aspectos te{\'{o}}ricos para o c{\'{a}}lculo e tra{\c{c}}ado do diagrama v-n de manobra e de rajada para uma aeronave destinada a participar da competi{\c{c}}{\~{a}}o SAE-Aerodesign .}}, volume = {1}, year = {2009} } @article{Soutis2005, author = {Soutis, C.}, doi = {10.1016/j.msea.2005.08.064}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Material/Carbon fiber reinforced plastics in aircraft.pdf:pdf}, isbn = {0921-5093}, issn = {09215093}, journal = {Materials Science and Engineering A}, keywords = {Aircraft construction,Carbon fiber reinforcement}, mendeley-groups = {Referencias TCC}, number = {1-2}, pages = {171--176}, title = {{Carbon fiber reinforced plastics in aircraft construction}}, volume = {412}, year = {2005} } @article{McGonigle2008, author = {McGonigle, A. J S and Aiuppa, A. and Giudice, G. and Tamburello, G. and Hodson, A. J. and Gurrieri, S.}, doi = {10.1029/2007GL032508}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Estrutura UAV/McGonigle{\_}et{\_}al-2008-Geophysical{\_}Research{\_}Letters.pdf:pdf}, isbn = {1944-8007}, issn = {00948276}, journal = {Geophysical Research Letters}, keywords = {http://dx.doi.org/10.1029/2007GL032508, doi:10.1029/2007GL032508, volcano monitoring, unmanned aerial vehicles, volcanic gas monitoring}, mendeley-groups = {Referencias TCC}, number = {6}, pages = {3--6}, title = {{Unmanned aerial vehicle measurements of volcanic carbon dioxide fluxes}}, volume = {35}, year = {2008} } |
dc.rights.*.fl_str_mv |
Atribución-NoComercial-SinDerivadas 2.5 Colombia |
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http://creativecommons.org/licenses/by-nc-nd/2.5/co/ |
dc.rights.local.spa.fl_str_mv |
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http://purl.org/coar/access_right/c_abf2 |
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openAccess |
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application/pdf |
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CRAI-USTA Bogotá |
dc.publisher.spa.fl_str_mv |
Universidad Santo Tomás |
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Pregrado Ingeniería Mecánica |
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Facultad de Ingeniería Mecánica |
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Universidad Santo Tomás |
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Carvajal Bonilla, Elver JofrePinto Delgado, Juan Sebastianhttps://scienti.colciencias.gov.co/cvlac/visualizador/generarCurriculoCv.do?cod_rh=00014030112019-05-16T01:39:04Z2019-05-16T01:39:04Z2019-01-22Pinto, J (2019). Structural design of the wing for URCUNINA (UAV). Universidad Santo Tomas, Bogotá, Colombiahttp://hdl.handle.net/11634/16725reponame:Repositorio Institucional Universidad Santo Tomásinstname:Universidad Santo Tomásrepourl:https://repository.usta.edu.coEl diseño del ala de URCUNINA (VANT) fue llevado a cabo. El diseño preliminar fue realizado usando restricciones aerodinámicas para proceder al diseño detallado con un análisis estructural. Para este proposito simulaciones en CFD fueron realizadas para obtener las las cargas sobre el ala, se requirió un proceso para transformar los datos de salida obtenidos por CFD a información que pueda ser suministrada al modelo de Elementos Finitos.Este proceso incluye recolección de datos, Matlab, extrapolaciones, ajustes polinomiales y construcción del diagrama V-n para tener datos que sirvan para alimentar el modelo de elementos finitos. El análisis fue hecho en el software comercial ABAQUS CAE. La comparación de 3 configuraciones en laminado dieron las herramientas para decidir la configuración estructural de la propuesta después de ser evaluada usando desplazamientos y teorias de falla.The structural design of the wing for URCUNINA (UAV) was carried out. The preliminary design was conducted using aerodynamic restrictions to pass into a detailed design by a structural analysis. For this porpoise CFD simulations were accomplish to obtain the loads over the wing, the usage of a process to transform the CFD output into information that could feed the FEA model was accomplished. This process include data collection, Matlab extrapolations, polynomial fits and construction of the V-n diagram to obtain proper data that work as input for the FEA. The analysis was done in the software ABAQUS CAE. The comparison of 3 different configurations of layup give the tools to decide the configuration used as a proposal after being evaluated using displacements and failure theories.Ingeniero Mecánicohttp://unidadinvestigacion.usta.edu.coPregradoapplication/pdfspaUniversidad Santo TomásPregrado Ingeniería MecánicaFacultad de Ingeniería MecánicaAtribución-NoComercial-SinDerivadas 2.5 Colombiahttp://creativecommons.org/licenses/by-nc-nd/2.5/co/Abierto (Texto Completo)info:eu-repo/semantics/openAccesshttp://purl.org/coar/access_right/c_abf2Structural design of the wing for URCUNINA (UAV)bachelor thesisTesis de pregradoinfo:eu-repo/semantics/acceptedVersionFormación de Recurso Humano para la Ctel: Trabajo de grado de Pregradohttp://purl.org/coar/resource_type/c_7a1finfo:eu-repo/semantics/bachelorThesisStructural-DesignWingCompositeAbaqusLayupFEATsai-WuLaminadoElementos FinitosDiseñoDiseñoDiseño EstructuralMateriales compuestosAbaqusLaminadoElementos FinitosTsai-WuAlaCRAI-USTA Bogotá@incollection{mcnutt1996seismic, title={Seismic monitoring and eruption forecasting of volcanoes: a review of the state-of-the-art and case histories}, author={McNutt, Stephen R}, booktitle={Monitoring and mitigation of volcano hazards}, pages={99--146}, year={1996}, publisher={Springer} }@article{Darmawan2018, author = {Darmawan, Herlan and Walter, Thomas R. and Brotopuspito, Kirbani Sri and Subandriyo and {I Gusti Made Agung Nandaka}}, doi = {10.1016/j.jvolgeores.2017.11.006}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Estrutura UAV/morphological and structural changes at the merapi lava dome.pdf:pdf}, issn = {03770273}, journal = {Journal of Volcanology and Geothermal Research}, keywords = {Digital elevation model,Lava dome,Merapi volcano,Photogrammetry,Structure from motion,Topography,Volcano monitoring}, mendeley-groups = {Referencias TCC}, pages = {256--267}, publisher = {Elsevier B.V.}, title = {{Morphological and structural changes at the Merapi lava dome monitored in 2012–15 using unmanned aerial vehicles (UAVs)}}, url = {https://doi.org/10.1016/j.jvolgeores.2017.11.006}, volume = {349}, year = {2018} }@techreport{Rosa2014, address = {Sao Carlos}, author = {Rosa, Maiara and Meunier, Nicolas and Augusto, Vitor and Sarmento, De Jesus and Santos, Yuri}, institution = {EESC}, mendeley-groups = {Docmentos por leer,Documentos referencias de TCC,Referencias TCC}, title = {{PROJETO GUIR{\'{A}} Projetos de Aeronaves II}}, year = {2014} }@article{Bravo-Mosquera2017, author = {Bravo-Mosquera, Pedro David and Botero-Bolivar, Laura and Acevedo-Giraldo, Daniel and Cer{\'{o}}n-Mu{\~{n}}oz, Hern{\'{a}}n Dar{\'{i}}o}, doi = {10.1016/j.ast.2017.09.005}, issn = {12709638}, journal = {Aerospace Science and Technology}, keywords = {Aerodynamic design,CFD,Conceptual design,UAV,Volcanic environments,Wind tunnel testing}, mendeley-groups = {Docmentos por leer,Referencias TCC}, pages = {600--614}, publisher = {Elsevier Masson SAS}, title = {{Aerodynamic design analysis of a UAV for superficial research of volcanic environments}}, url = {http://dx.doi.org/10.1016/j.ast.2017.09.005}, volume = {70}, year = {2017} }@article{Garre2017, author = {Garre, Parthasarathy and Arjun, Goli Venkata}, mendeley-groups = {Referencias TCC}, number = {Ii}, pages = {295--315}, title = {{Modeling and Analysis of a RIBS and Spars of An Airplane Wing for Bending and Shear Loads}}, volume = {5}, year = {2017} }@phdthesis{LimadeSousa2011, author = {{Lima de Sousa}, Eduardo Benedito}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Estrutura UAV/Estrutura fuselagem Material composito.pdf:pdf}, mendeley-groups = {Docmentos por leer,Referencias TCC}, pages = {97}, school = {Instituto Tecnologico de Aeron{\'{a}}utica ITA}, title = {{Projeto estrutural de fuselagem de vant em fibra de carbono}}, type = {DP}, volume = {1}, year = {2011} }@phdthesis{Narayan2009, author = {Narayan, Anirudh}, booktitle = {Mechanical Engineering}, mendeley-groups = {Docmentos por 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configuraci{\'{o}}n,elementos finitos,esfuerzo cortante,esfuerzo normal,factor de carga,fuerza de arrastre,fuerza de sustentaci{\'{o}}n,materiales compuestos,momento,pandeo lineal,s,se desea proponer y}, mendeley-groups = {Referencias TCC}, pages = {167}, school = {Universidad San Buenaventura}, title = {{Dise{\~{n}}o estructural del fuselaje, ala central y union ala-fuselaje para la aeronave no tripulada (UAV) experimental SKYCRUISER X-1}}, year = {2013} }@article{Mazhar2010, author = {Mazhar, Farrukh and Khan, Abdul Munem}, doi = {AIAA 2010-3099}, isbn = {9781600867422}, issn = {02734508}, journal = {Science And Technology}, mendeley-groups = {Docmentos por leer,Referencias TCC}, number = {April}, pages = {1--12}, title = {{Structural Design of a Uav Wing Using Finite}}, year = {2010} }@phdthesis{Estructural2013, author = {{Nicol{\'{a}}s Castro}, Jos{\'{e}} and Coronado, William David and Eduardo, Luis}, file = {:D$\backslash$:/Drive/USTA/TESIS/Articulos/Estrutura UAV/79561.pdf:pdf}, keywords = {aerodin{\'{a}}mico,criterio de falla,descripci{\'{o}}n del trabajo,diagrama vn,dise{\~{n}}ar la configuraci{\'{o}}n,elementos finitos,esfuerzo cortante,esfuerzo normal,factor de carga,fuerza de arrastre,fuerza de sustentaci{\'{o}}n,materiales compuestos,momento,pandeo lineal,s,se desea proponer y}, mendeley-groups = {Referencias TCC}, pages = {167}, school = {Universidad San Buenaventura}, title = {{Dise{\~{n}}o estructural del fuselaje, ala central y union ala-fuselaje para la aeronave no tripulada (UAV) experimental SKYCRUISER X-1}}, year = {2013} }@phdthesis{Alcaraz2015, author = {Alcaraz, Daniel}, pages = {1--228}, school = {Universidad de Sevilla}, title = {{Dise{\~{n}}o estructural y construcci{\'{o}}n de un avi{\'{o}}n no tripulado : El Proyecto C{\'{e}}firo}}, year = {2015} }@phdthesis{Sebastian2016, author = {Sebasti{\'{a}}n, Esmeralda Castillo}, mendeley-groups = {Referencias TCC}, pages = {140}, school = {Universidad Politecnica de Valencia}, title = 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{0921-5093}, issn = {09215093}, journal = {Materials Science and Engineering A}, keywords = {Aircraft construction,Carbon fiber reinforcement}, mendeley-groups = {Referencias TCC}, number = {1-2}, pages = {171--176}, title = {{Carbon fiber reinforced plastics in aircraft construction}}, volume = {412}, year = {2005} }@article{McGonigle2008, author = {McGonigle, A. J S and Aiuppa, A. and Giudice, G. and Tamburello, G. and Hodson, A. 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