Experimental and numerical investigation of different wing profiles

Yıl 2023, Cilt: 8 Sayı: 2, 151 - 166, 23.06.2023

Murat Şahin Mehmet Arif Saltan Burak Berk Başkaya

https://doi.org/10.58559/ijes.1220776

Öz

Computational Fluid Dynamics (CFD) techniques are widely used in product development processes due to efficient algorithms to solve Navier Stokes equations. In this study, the coordinates of the NACA 1412 and NACA 2415 sections selected from the standard wing sections of the National Aviation Advisory Committee (NACA) have been implemented with specific procedures to create new geometries and a new wing profile design using the coordinate method. The wing profile geometry is created from the coordinates available in the literature. Fixed two-dimensional viscous flows around the generated wing profiles are simulated using commercially available ANSYS-Fluent software. The mesh structure used was created using the C type and rectangular structure. CFD and wind tunnel analysis of attack angles ranging from certain degrees. The aerodynamic coefficients of the related statuses, i.e. the lift and drag coefficients obtained from the analysis, have been compared with the wind tunnel test results. Aerodynamic research in recent years focuses on active flow control concepts, laminar flow control, fuel economy and higher transport/drag force ratio. This is designed to understand and analyze flow behavior around airfoils using the CFD method.

Anahtar Kelimeler

Aerodynamics, Airfoil, Computational fluid dynamics (CFD)

Kaynakça

• [1] Marqués P, Ronch AD. Advanced uav aerodynamics, flight stability and control: novel concepts, theory and applications. Wiley, West Sussex, UK, 2017.
• [2] Ma P, Yu J, Chen F, Xue Z. Airfoil optimization design based on a combined optimization strategy. 5th International Conference on Frontiers of Manufacturing Science and Measuring Technology (FMSMT 2017), Taiyuan, China, 2017.
• [3] Zargar OA, Lin T, Zebua AG, Lai TJ, Shih YG, Hu SC, Leggett G. The effects of surface modification on aerodynamic characteristics of airfoil du 06 w 200 at low reynolds numbers. International Journal of Thermofluids 2022; 16(3):100208.
• [4] Peng L, Qijin Z, Qiuxian Z. CFD calculations on the unsteady aerodynamic characteristics of a tilt-rotor in a conversion mode. Chinese Journal of Aeronautics 2015; 28(6): 1593–1605.
• [5] Bakirci M, Yilmaz S. Numerical investigations on optimal tip speed ratio of wind turbines using bem and cfd. 1st International Conference on Energy Systems Engineering, Karabuk, Turkey, 2017.
• [6] Tatlıer MS, Baran T. Structural and CFD analysis ofan airfoil subjected to bird strike. European Journal of Mechanics / B Fluids 2020; 84 (2020) 478–486.
• [7] Raymer DP. Aircraft design: a conceptual approac. American Institute of Aeronautics & Ast, Virginia, USA, 2018.
• [8] Yavçin E. Biomechanical investigation of flying and an robotic bird design study. Master of Science Thesis, Sakarya University, 2014.
• [9] Chakraborty S, Ghosh S. A CFD study on the structural parameters of naca 2412 airfoil based air-wing using different composite materials. Materials Today: Proceedings journal 2022; 60 (2022) 894–901.
• [10] Istanbul Technical University Turkey. Fundamentals of Flight – Wings, Tail Surfaces, <https://web.itu.edu.tr/yukselen/UCK111/B%F6l%FCm%205%20U%E7u%FEun%20Esaslar%FD.pdf >; 2021 [accessed 18.07.21].
• [11] Aminjan KK, Ghodrat M, Heidari M, Rahmanivahid P, Khanachah SN, Chitt M, Escobedo-Diaz JP. Numerical and experimental investigation to design a novel morphing airfoil for performance optimization. Propulsion and Power Research 2023; 12(1):83e103.
• [12] Ozel C, Ozbek E, Ekici S. A review on applications and effects of morphing wing technology on uavs. International Journal of Aviation Science and Technology 2020; 30-40.
• [13] Dincer İ. Comprehensive energy systems. Elsevier Science & Technology, Amsterdam, Netherlands, 2018.