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dc.contributor.authorKaynak, Ünver-
dc.contributor.authorÇoban, A. B.-
dc.identifier.citation9th International Conference on Computational Fluid Dynamics, ICCFD 2016, 11 July 2016 through 15 July 2016, , 159582en_US
dc.description.abstractIn 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.en_US
dc.publisherInternational Conference on Computational Fluid Dynamics 2016en_US
dc.relation.ispartof9th International Conference on Computational Fluid Dynamics, ICCFD 2016 - Proceedingsen_US
dc.subjectComputational Fluid Dynamicsen_US
dc.subjectNumerical Algorithmsen_US
dc.subjectTurbulence Modelingen_US
dc.subjectUnmanned Aerial Vehicleen_US
dc.titleNumerical investigation of winglets used to improve the flying performance of unmanned aerial vehicleen_US
dc.typeConference Objecten_US
dc.departmentFaculties, Faculty of Engineering, Department of Mechanical Engineeringen_US
dc.departmentFakülteler, Mühendislik Fakültesi, Makine Mühendisliği Bölümütr_TR
dc.institutionauthorKaynak, Ünver-
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.relation.conference9th International Conference on Computational Fluid Dynamics, ICCFD 2016en_US
item.fulltextNo Fulltext-
item.openairetypeConference Object- Department of Mechanical Engineering-
Appears in Collections:Makine Mühendisliği Bölümü / Department of Mechanical Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
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