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dc.contributorHernández Ortega, Joaquín Alberto
dc.contributorCante Terán, Juan Carlos
dc.contributor.authorRubio Álvarez, Laura
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Resistència de Materials i Estructures a l'Enginyeria
dc.date.accessioned2020-02-10T17:51:04Z
dc.date.available2020-02-10T17:51:04Z
dc.date.issued2016-06
dc.identifier.urihttp://hdl.handle.net/2117/177367
dc.description.abstractThe present study concerns the design of an optimal structure, made of composite materials, for an Unmanned Aerial Vehicle (UAV), as well as its manufacturing. This document shows the most important steps in the decision of which is the most proper structure for the UAV. This project starts studying the flight envelope of the prototype with XFLR5®, then using Matlab® the first structure is obtained to begin the analysis with the FEM. Finally, through a finite element element mesh with GiD® and Matlab ®, the structure will be optimized.
dc.language.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus
dc.subjectÀrees temàtiques de la UPC::Enginyeria dels materials::Materials compostos
dc.subject.lcshComposite materials
dc.subject.lcshDrone aircraft--Design and construction
dc.titleStudy of the structural behaviour of a UAV'S composite wing using the finite element method
dc.typeBachelor thesis
dc.subject.lemacAvions no tripulats -- Disseny i construcció
dc.subject.lemacMaterials compostos
dc.identifier.slug205-800
dc.rights.accessOpen Access
dc.date.updated2019-10-16T07:34:59Z
dc.audience.educationlevelGrau
dc.audience.mediatorEscola Superior d'Enginyeries Industrial, Aeroespacial i Audiovisual de Terrassa


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