Structural design of the wing for URCUNINA (UAV)

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dc.contributor.advisorCarvajal Bonilla, Elver Jofrespa
dc.contributor.authorPinto Delgado, Juan Sebastianspa
dc.contributor.cvlachttps://scienti.colciencias.gov.co/cvlac/visualizador/generarCurriculoCv.do?cod_rh=0001403011spa
dc.coverage.campusCRAI-USTA Bogotáspa
dc.date.accessioned2019-05-16T01:39:04Zspa
dc.date.available2019-05-16T01:39:04Zspa
dc.date.issued2019-01-22spa
dc.descriptionEl 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.spa
dc.description.abstractThe 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.spa
dc.description.degreelevelPregradospa
dc.description.degreenameIngeniero Mecánicospa
dc.description.domainhttp://unidadinvestigacion.usta.edu.cospa
dc.format.mimetypeapplication/pdfspa
dc.identifier.citationPinto, J (2019). Structural design of the wing for URCUNINA (UAV). Universidad Santo Tomas, Bogotá, Colombiaspa
dc.identifier.instnameinstname:Universidad Santo Tomásspa
dc.identifier.reponamereponame:Repositorio Institucional Universidad Santo Tomásspa
dc.identifier.repourlrepourl:https://repository.usta.edu.cospa
dc.identifier.urihttp://hdl.handle.net/11634/16725
dc.language.isospaspa
dc.publisherUniversidad Santo Tomásspa
dc.publisher.facultyFacultad de Ingeniería Mecánicaspa
dc.publisher.programPregrado Ingeniería Mecánicaspa
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dc.rightsAtribución-NoComercial-SinDerivadas 2.5 Colombia*
dc.rights.accessrightsinfo:eu-repo/semantics/openAccess
dc.rights.coarhttp://purl.org/coar/access_right/c_abf2
dc.rights.localAbierto (Texto Completo)spa
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/2.5/co/*
dc.subject.keywordStructural-Designspa
dc.subject.keywordWingspa
dc.subject.keywordCompositespa
dc.subject.keywordAbaqusspa
dc.subject.keywordLayupspa
dc.subject.keywordFEAspa
dc.subject.keywordTsai-Wuspa
dc.subject.lembLaminadospa
dc.subject.lembElementos Finitosspa
dc.subject.lembDiseñospa
dc.subject.proposalDiseñospa
dc.subject.proposalDiseño Estructuralspa
dc.subject.proposalMateriales compuestosspa
dc.subject.proposalAbaqusspa
dc.subject.proposalLaminadospa
dc.subject.proposalElementos Finitosspa
dc.subject.proposalTsai-Wuspa
dc.subject.proposalAlaspa
dc.titleStructural design of the wing for URCUNINA (UAV)spa
dc.typebachelor thesis
dc.type.categoryFormación de Recurso Humano para la Ctel: Trabajo de grado de Pregradospa
dc.type.coarhttp://purl.org/coar/resource_type/c_7a1f
dc.type.coarversionhttp://purl.org/coar/version/c_ab4af688f83e57aa
dc.type.driveinfo:eu-repo/semantics/bachelorThesis
dc.type.localTesis de pregradospa
dc.type.versioninfo:eu-repo/semantics/acceptedVersion

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