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|Title:||Drag analysis of a supersonic fighter aircraft||Authors:||Akgun O.
Golcuk A. I.
Kurtulus D. F.
|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:||For aircraft design, drag optimization is very important for having better flight performance and less fuel consumption. In this study, drag effects of fuselage, wing and tail section are separately analyzed using a generic F-16 fighter aircraft model in ANSYS Fluent CFD tool with polyhedral mesh. Pressure drag and viscous drag effects are shown on different section of the aircraft as fuselage, wing, vertical tail and horizontal tail. Drag values are presented on subsonic, transonic and supersonic flights. © 2016 9th International Conference on Computational Fluid Dynamics, ICCFD 2016 - Proceedings. All rights reserved.||URI:||https://hdl.handle.net/20.500.11851/5680|
|Appears in Collections:||Makine Mühendisliği Bölümü / Department of Mechanical Engineering|
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
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