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dc.contributorTrias Miquel, Francesc Xavier
dc.contributorPérez Segarra, Carlos David
dc.contributor.authorSefo, Sea
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Màquines i Motors Tèrmics
dc.date.accessioned2021-05-04T07:50:13Z
dc.date.issued2021-02-15
dc.identifier.urihttp://hdl.handle.net/2117/345018
dc.description.abstractThrough the means of temperature variations of the aerofoil surface this report aimed to investigate and enhance the aerodynamic efficiency of micro air vehicles. Through the process of heating the lower edge of the aerofoil nose and cooling the upper leading edge of the nose surface, an increase of Lift/Drag coefficient was observed. The focus of this research lies in the computational investigation of this affect on small scale high cambered aerofoils at a range of zero angle of attack at moderate Reynolds number flow
dc.language.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.subjectÀrees temàtiques de la UPC::Enginyeria mecànica::Mecànica de fluids
dc.subject.lcshDrone aircraft
dc.subject.lcshAerodynamics
dc.subject.lcshComputational fluid dynamics
dc.subject.otherThermal camber
dc.subject.otherCFD
dc.subject.otherMicro air vehicles
dc.titleAdvanced study for the numerical resolution of the Navier-Stokes equations with observation of the thermal camber on high camber aerofoils in moderate reynolds number flow
dc.typeMaster thesis
dc.subject.lemacAvions no tripulats
dc.subject.lemacDinàmica de fluids computacional
dc.subject.lemacAerodinàmica
dc.identifier.slugPRISMA-154073
dc.rights.accessRestricted access - author's decision
dc.date.lift10000-01-01
dc.date.updated2021-03-17T19:33:25Z
dc.audience.educationlevelMàster
dc.audience.mediatorEscola Superior d'Enginyeries Industrial, Aeroespacial i Audiovisual de Terrassa
dc.audience.degreeMÀSTER UNIVERSITARI EN ENGINYERIA ESPACIAL I AERONÀUTICA (Pla 2016)


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