An Overview for Effects on Aerodynamic Performance of Using Winglets and Wingtip Devices on Aircraft
dc.authorid | 0000-0003-2391-5441 | en_US |
dc.authorid | 0000-0001-8385-9846 | en_US |
dc.contributor.author | Öztürk, Şeyda | |
dc.contributor.author | Örs, İlker | |
dc.date.accessioned | 2022-08-25T09:40:44Z | |
dc.date.available | 2022-08-25T09:40:44Z | |
dc.date.issued | 2020 | en_US |
dc.department | Selçuk Üniversitesi, Yüksek Okullar, Sivil Havacılık Yüksekokulu | en_US |
dc.description.abstract | In this study, the effects of different types of winglets and wingtip devices on aerodynamic performance in aircraft were investigated. Mostly, CFD analyzes were performed with different turbulence models in the examined studies, as well as experimental studies were also conducted. It has been observed that especially k-?, k-? and Sparlat Almaras turbulence models are used in calculations. As a result of the investigations, it has been observed that both the use of winglets and the use of a wingtip devices significantly reduce the vortex formation in the wingtips compared to the plain wing. It has been determined that the most effective method in reducing wing tip vortexes is the use of winglet. The reduction of these vortexes resulted in an increase in lift force and a decrease in drag force. Thus, the L/D ratio has increased and as a result; better fuel economy, longer range and higher payload are provided. | en_US |
dc.identifier.citation | Öztürk, Ş., Örs, İ. (2020). An overview for effects on aerodynamic performance of using winglets and wingtip devices on aircraft. International Journal of Aeronautics and Astronautics, 1, (1), 1-11. | en_US |
dc.identifier.endpage | 11 | en_US |
dc.identifier.issn | 2757-6574 | en_US |
dc.identifier.issue | 1 | en_US |
dc.identifier.startpage | 1 | en_US |
dc.identifier.uri | https://hdl.handle.net/20.500.12395/42983 | |
dc.identifier.volume | 1 | en_US |
dc.institutionauthor | Öztürk, Şeyda | |
dc.institutionauthor | Örs, İlker | |
dc.language.iso | en | en_US |
dc.publisher | Selçuk Üniversitesi Sivil Havacılık Yüksekokulu | en_US |
dc.relation.ispartof | International Journal of Aeronautics and Astronautics | en_US |
dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı | en_US |
dc.rights | info:eu-repo/semantics/openAccess | en_US |
dc.selcuk | 20240510_oaig | en_US |
dc.subject | Aircraft | en_US |
dc.subject | Drag force | en_US |
dc.subject | Lift force | en_US |
dc.subject | Winglet | en_US |
dc.subject | Wingtip device | en_US |
dc.subject | Uçak | en_US |
dc.subject | Sürükleme kuvveti | en_US |
dc.subject | Kaldırma kuvveti | en_US |
dc.subject | Kanatçık | en_US |
dc.subject | Kanat ucu cihazı | en_US |
dc.title | An Overview for Effects on Aerodynamic Performance of Using Winglets and Wingtip Devices on Aircraft | en_US |
dc.type | Article | en_US |