Aerodynamic Optimization of a Morphing Winglet Design

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dc.contributor.authorABES, Bachir
dc.contributor.authorIMINE, Bachir
dc.date.accessioned2019-05-26T09:22:56Z
dc.date.available2019-05-26T09:22:56Z
dc.date.issued2018-12-10
dc.descriptionInternational Symposium on Mechatronics and Renewable Energies El-Oued 10- 11 December 2018en_US
dc.description.abstractIn the present study, a CFD is used to investigate the flow around an isolated wing equipped by a morphing winglet. In order to obtain initial estimates of lift and drag coefficients with flow velocity of 20 meters per second a various angles of attack, several cases of winglets were tested according to different dihedral angles. The model of k-ω SST turbulence is used for the investigation of the complex flow around the morphing winglet. The present results shown a good agreement with the literature data.en_US
dc.identifier.urihttps://dspace.univ-eloued.dz/handle/123456789/1559
dc.language.isoenen_US
dc.publisherUniversity of Eloued جامعة الواديen_US
dc.subjectMorphing Winglet, Tip Vortex, Angle of Attack, Dihedral Angle, Numerical Analysis.en_US
dc.titleAerodynamic Optimization of a Morphing Winglet Designen_US
dc.typeOtheren_US

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