Please use this identifier to cite or link to this item: 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
Issue Date: 2016
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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