Now showing items 1-15 of 15

    • Aerodynamic analysis of the lift reducer device by flow transfer 

      Font Prats, Pau (Universitat Politècnica de Catalunya, 2013-03-08)
      Bachelor thesis
      Open Access
      From the beginnings of aviation and aeronautical world in general, it has searched the goal of creating a machine capable of taking off in a controlled way trying to achieve the highest operational aircraft. Always looking ...
    • Aerodynamic assessment of humpback whale ventral fin shapes 

      Rita Espasa, Damià (Universitat Politècnica de Catalunya, 2011-09)
      Master thesis (pre-Bologna period)
      Open Access
    • Design and construction of a remote-controlled flying wing 

      Franch Ruiz, Sergi (Universitat Politècnica de Catalunya, 2017-06-10)
      Bachelor thesis
      Restricted access - author's decision
      Diseñar completamente, y eventualmente construir, un aparato controlado mediante radio control
    • Design of an all-composite wing for a small UAV Platform. Imside the development process of FEA and Optimization software for composite structures 

      Jiménez Fernández, Marc (Universitat Politècnica de Catalunya / Politecnico di Milano, 2010)
      Master thesis (pre-Bologna period)
      Restricted access - author's decision
      This work is the first movement of the design of an all composite UAV wing, helping a group of aeronautics engineering students, to increase the technologic level of its. To do that, the means and technology from CIMNE ...
    • [E-Project] Study of the most suitable wing configuration for STOL operations 

      González Fernández, Raúl (Universitat Politècnica de Catalunya, 2017-06)
      Bachelor thesis
      Restricted access - author's decision
      he aim of this project is to study, analyse and develop a wing configuration intended to perform STOL operations. The developed wing should be suitable for its use in the electriclightweight aircraft currently being ...
    • Estudi de viabilitat de l’ús d’ales volants com a transport comercial 

      Freixa Barat, Alba (Universitat Politècnica de Catalunya, 2015-06-11)
      Bachelor thesis
      Open Access
      Recopilació de la informació sobre l’estat del mercat i l’estat de l’art. Identificació dels principals avantatges i inconvenients. Proposta de disseny preliminar. Comparació de costos operacionals amb un avió amb capacitats ...
    • Estudio de viabilidad de una línea de producción de larguerillos de alas de avión de CFRP 

      Ruiz Coll, Oriol Enric (Universitat Politècnica de Catalunya, 2015-06)
      Master thesis (pre-Bologna period)
      Restricted access - confidentiality agreement
    • Long endurance solar powered flying wing 

      Moreno Vera, Juan Antonio; Portillo Santiago, Edgar (Universitat Politècnica de Catalunya, 2017-01-27)
      Bachelor thesis
      Restricted access - author's decision
      Covenantee:   Vilniaus Gedimino technikos universitetas
      This project has been carried out by Edgar Portillo and Juan Antonio Moreno during stay of five months in Lithuania. The aim of the project was to realize an UAV (Unmanned Aerial Vehicle) capable to flight with solar energy ...
    • Optimizacion aerodinàmica de los perfiles de ala de un "flying wing" 

      Gomariz Sancha, Angel (Universitat Politècnica de Catalunya, 2006-07-13)
      Master thesis (pre-Bologna period)
      Open Access
      Este trabajo consiste en un estudio de optimización aerodinámica de los perfiles de ala de un “flying wing”, ala volante sin fuselaje, y de la distribución de sustentación a lo largo de éste, así como de la estabilidad ...
    • Optimización aerodinámica de la geometría 3D de un "flying wing" 

      Fraile Perez, Sergio (Universitat Politècnica de Catalunya, 2006-07-13)
      Master thesis (pre-Bologna period)
      Open Access
      El objetivo principal del trabajo consiste en la optimización de la geometría general de un tipo específico de aeronaves, los Flying Wings. Estas aeronaves difieren del concepto de avión actual, por la inexistencia de ...
    • Study of a high-lift wing for a STOL light aircraft 

      Montón Gimeno, Daniel (Universitat Politècnica de Catalunya, 2019-06)
      Bachelor thesis
      Restricted access - author's decision
      In this e-project is performed a study to find a proper wing design for a STOL capable electric light aircraft. This is the continuation of the e-project 1 realized in 2017 and the main objective is to find a final wing ...
    • Study of mixed attack angle wing profiles 

      Lleixà Mármol, Isaac; Ahmed Akhtar, Sajeel Mohammad (Universitat Politècnica de Catalunya, 2010-07-29)
      Bachelor thesis
      Open Access
    • Study of the model-order reduction of the aerolastic behavior of a wing 

      Rodeja Ferrer, Pep (Universitat Politècnica de Catalunya, 2016-06)
      Bachelor thesis
      Open Access
      The main objective of this paper is to apply the model-order reduction technique to an airplane’s wing in order to speed up development of aircrafts or to get real-time results of a plane structural state. However, this ...
    • Study of winglets and other non-planar wing configurations for improved low-speed aerodynamic efficiency 

      Camúñez i Guirao, Aleix (Universitat Politècnica de Catalunya, 2019-01-10)
      Bachelor thesis
      Restricted access - author's decision
      The induced drag is one of the most important sources of aerodynamic drag in an aircraft, and reducing it could mean saving thousands of dollars in fuel per plane and year. For this reason, since the 1970s oil crisis, ...
    • Valoración de la cartera de slots 

      Atué Belmonte, José Antonio (Universitat Politècnica de Catalunya, 2018-02-07)
      Bachelor thesis
      Restricted access - confidentiality agreement