Aerodynamic Optimization of a Morphing Winglet Design
| dc.contributor.author | ABES, Bachir | |
| dc.contributor.author | IMINE, Bachir | |
| dc.date.accessioned | 2019-05-26T09:22:56Z | |
| dc.date.available | 2019-05-26T09:22:56Z | |
| dc.date.issued | 2018-12-10 | |
| dc.description | International Symposium on Mechatronics and Renewable Energies El-Oued 10- 11 December 2018 | en_US |
| dc.description.abstract | In 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.uri | http://dspace.univ-eloued.dz/handle/123456789/1559 | |
| dc.language.iso | en | en_US |
| dc.publisher | University of Eloued جامعة الوادي | en_US |
| dc.subject | Morphing Winglet, Tip Vortex, Angle of Attack, Dihedral Angle, Numerical Analysis. | en_US |
| dc.title | Aerodynamic Optimization of a Morphing Winglet Design | en_US |
| dc.type | Other | en_US |
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