Ir al contenido (pulsa Retorno)

Universitat Politècnica de Catalunya

    • Català
    • Castellano
    • English
    • LoginRegisterLog in (no UPC users)
  • mailContact Us
  • world English 
    • Català
    • Castellano
    • English
  • userLogin   
      LoginRegisterLog in (no UPC users)

UPCommons. Global access to UPC knowledge

Banner header
66.439 UPC academic works
You are here:
View Item 
  •   DSpace Home
  • Treballs acadèmics
  • Escola Tècnica Superior d'Enginyeria Industrial de Barcelona
  • Grau en Enginyeria en Tecnologies Industrials (Pla 2010)
  • View Item
  •   DSpace Home
  • Treballs acadèmics
  • Escola Tècnica Superior d'Enginyeria Industrial de Barcelona
  • Grau en Enginyeria en Tecnologies Industrials (Pla 2010)
  • View Item
JavaScript is disabled for your browser. Some features of this site may not work without it.

Aerodynamic design of a RC model airplane for SAE Aero Design

Thumbnail
View/Open
TFG_POL_BERNALDO.pdf (2,381Mb) (Restricted access)
  View Usage Statistics
  LA Referencia / Recolecta stats
Cita com:
hdl:2117/97160

Show full item record
Bernaldo Franco, Pol
Tutor / directorTrillas i Gay, EnricMés informacióMés informació
Document typeBachelor thesis
Date2016-10-03
Rights accessRestricted access - author's decision
Attribution-NonCommercial-NoDerivs 3.0 Spain
Except where otherwise noted, content on this work is licensed under a Creative Commons license : Attribution-NonCommercial-NoDerivs 3.0 Spain
Abstract
This project focuses on the aerodynamic design of a RC model airplane for the SAE Aero Design competition of 2016. It solely includes the aerodynamic design, thus, no structural / mechanical analysis nor manufacturing process are described. The SAE Aero Design is a collegiate competition based on designing, building and flying and airplane with the highest payload possible. The aerodynamic design defines the shape of the airplane and its external components: wing, fuselage and tail. Detailed analysis is conducted to estimate the lift and drag forces, which determine the performance in flight. The main objective is to design an airplane to win the competition, hence, the payload lifted by the airplane is the relevant parameter to maximize. The project aims to develop a design capable of lifting a minimum gross weight of 22 kg. The project outcome shows the design of an airplane capable of lifting more than 22 kg of gross weight. Theoretical and empirical equations and analysis are used along the design project to come up with the promising final results.
SubjectsAerodynamics, Airplanes -- Design, Aerodinàmica, Avions -- Disseny
DegreeGRAU EN ENGINYERIA EN TECNOLOGIES INDUSTRIALS (Pla 2010)
URIhttp://hdl.handle.net/2117/97160
Collections
  • Escola Tècnica Superior d'Enginyeria Industrial de Barcelona - Grau en Enginyeria en Tecnologies Industrials (Pla 2010) [3.025]
  View Usage Statistics

Show full item record

FilesDescriptionSizeFormatView
TFG_POL_BERNALDO.pdfBlocked2,381MbPDFRestricted access

Browse

This CollectionBy Issue DateAuthorsOther contributionsTitlesSubjectsThis repositoryCommunities & CollectionsBy Issue DateAuthorsOther contributionsTitlesSubjects

© UPC Obrir en finestra nova . Servei de Biblioteques, Publicacions i Arxius

info.biblioteques@upc.edu

  • About This Repository
  • Contact Us
  • Send Feedback
  • Privacy Settings
  • Inici de la pàgina