Structural design of the wing for URCUNINA (UAV)

dc.contributorCarvajal Bonilla, Elver Jofre
dc.contributorhttps://scienti.colciencias.gov.co/cvlac/visualizador/generarCurriculoCv.do?cod_rh=0001403011
dc.creatorPinto Delgado, Juan Sebastian
dc.date.accessioned2019-05-16T01:39:04Z
dc.date.available2019-05-16T01:39:04Z
dc.date.created2019-05-16T01:39:04Z
dc.date.issued2019-01-22
dc.identifierPinto, J (2019). Structural design of the wing for URCUNINA (UAV). Universidad Santo Tomas, Bogotá, Colombia
dc.identifierhttp://hdl.handle.net/11634/16725
dc.identifierreponame:Repositorio Institucional Universidad Santo Tomás
dc.identifierinstname:Universidad Santo Tomás
dc.identifierrepourl:https://repository.usta.edu.co
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.
dc.languagespa
dc.publisherUniversidad Santo Tomás
dc.publisherPregrado Ingeniería Mecánica
dc.publisherFacultad de Ingeniería Mecánica
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dc.rightshttp://creativecommons.org/licenses/by-nc-nd/2.5/co/
dc.rightsAbierto (Texto Completo)
dc.rightsinfo:eu-repo/semantics/openAccess
dc.rightshttp://purl.org/coar/access_right/c_abf2
dc.rightsAtribución-NoComercial-SinDerivadas 2.5 Colombia
dc.titleStructural design of the wing for URCUNINA (UAV)
dc.typebachelor thesis


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