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https://hdl.handle.net/20.500.11851/5856| Title: | Numerical investigation of winglets used to improve the flying performance of unmanned aerial vehicle | Authors: | Kaynak, Ünver Çoban, A. B. |
Keywords: | Computational Fluid Dynamics Numerical Algorithms Turbulence Modeling Unmanned Aerial Vehicle Winglet |
Publisher: | International Conference on Computational Fluid Dynamics 2016 | Source: | 9th International Conference on Computational Fluid Dynamics, ICCFD 2016, 11 July 2016 through 15 July 2016, , 159582 | Abstract: | In this study, the aerodynamic forces, velocity and pressure distributions are analyzed on SD7062 wing profile with CFD program FLUENT. Calculations are made for one clean wing and 3 different winglets named End-Plate, Blended and Scimitar which are added on this clean wing. Each model are analyzed for different angle of attack degrees between -5 and 17. After calculations were ended, it is seen that wings’ with winglets aerodynamic performances are increased. Additionally, stall was occurred around 15 aoa degrees. © 2016 9th International Conference on Computational Fluid Dynamics, ICCFD 2016 - Proceedings. All rights reserved. | URI: | https://hdl.handle.net/20.500.11851/5856 |
| Appears in Collections: | Makine Mühendisliği Bölümü / Department of Mechanical Engineering Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection |
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