Study of mixed attack angle wing profiles

Vista senzilla d'ítem
dc.audience.degreeENGINYERIA TÈCNICA D'AERONÀUTICA, ESPECIALITAT EN AERONAVEGACIÓ (Pla 2003)
dc.audience.educationlevelEstudis de primer/segon cicle
dc.audience.mediatorEscola Politècnica Superior de Castelldefels
dc.contributorCrespo Artiaga, Daniel
dc.contributor.authorLleixà Mármol, Isaac
dc.contributor.authorAhmed Akhtar, Sajeel Mohammad
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Física Aplicada
dc.date.accessioned2010-09-03T11:17:15Z
dc.date.available2010-09-03T11:17:15Z
dc.date.issued2010-07-29
dc.date.updated2010-07-30T05:13:39Z
dc.descriptionThe goal of this study is to analyze how a wing constructed in such a way that has different in-built angles of attack behaves in front of a conventional built wing. The flow around the wing profile of the Airbus A380 was simulated by CFD and the normalized aerodynamical data (lift, drag, aerodynamic center etc. ) was be obtained. Next, the wing profile was modified by changing the in-built angle of attack progressively from root to tip. The aerodynamic behaviouf of the resulting twisted wing profile was simulated by CFD and the aerodynamic data was compared with that of the standard wing. The potential benefits and difficulties of the mixed profiles wing was analysed both from the aerodynamic (flight stability, fuel consumption, etc.) and the structural (induced stress, construction methods, and available materials) points of view.
dc.identifier.urihttps://hdl.handle.net/2099.1/9671
dc.language.isospa
dc.publisherUniversitat Politècnica de Catalunya
dc.rights.accessOpen Access
dc.rights.licensenameAttribution-NonCommercial-ShareAlike 3.0 Spain
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/3.0/es/
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica
dc.subject.lcshAirplanes--Wings
dc.subject.lcshLeading edges (Aerodynamics)
dc.subject.lemacAvions -- Ales -- Disseny
dc.subject.lemacAerodinamica
dc.subject.otherWing profiles
dc.subject.otherFlight stability
dc.titleStudy of mixed attack angle wing profiles
dc.typeBachelor thesis
dspace.entity.typePublication

Fitxers

Paquet original

Mostrant 1 - 1 de 1
Miniatura
Nom:
memoria.pdf
Mida:
3.15 MB
Format:
Adobe Portable Document Format

Col·leccions

E. T. d'Aeronàutica, especialitat en Aeronavegació (Pla 2003)