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dc.contributorMartín Sierra, Aitor
dc.contributor.authorGonzález Fernández, Raúl
dc.date.accessioned2020-01-21T14:06:16Z
dc.date.issued2017-06
dc.identifier.urihttp://hdl.handle.net/2117/175375
dc.descriptionThe target of this study is find the most adequate wing configuration for short take-off and landing operations with a light aircraft.
dc.description.abstracthe 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 developed in the E-Project. Furthermore, along with the development of the wing, this project is intended to provide a complete study of thewing configuration parameters effect on the aerodynamic behaviour of the wing for future improvements.
dc.language.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus
dc.subject.lcshShort take-off and landing aircraft--Design and construction
dc.subject.lcshAirplanes--Wings--Design and construction
dc.subject.lcshElectric airplanes
dc.title[E-Project] Study of the most suitable wing configuration for STOL operations
dc.title.alternativeStudy of the most suitable wing configuration for STOL operations
dc.typeBachelor thesis
dc.subject.lemacAvions -- Disseny i construcció
dc.subject.lemacAvions -- Ales -- Disseny
dc.subject.lemacAvions elèctrics
dc.identifier.slug205-1196
dc.rights.accessRestricted access - author's decision
dc.date.lift10000-01-01
dc.date.updated2019-10-24T11:15:31Z
dc.audience.educationlevelGrau
dc.audience.mediatorEscola Superior d'Enginyeries Industrial, Aeroespacial i Audiovisual de Terrassa
dc.audience.degreeGRAU EN ENGINYERIA EN TECNOLOGIES AEROESPACIALS (Pla 2010)


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