A Comparative Study of Turbulence Models on Aerodynamics Characteristics of a NACA0012 Airfoil

• DOI: 10.30880/ijie.2018.10.01.019
• Publication Date: 2018-06-13T02:27:25Z
• Authors: Azmahani Sadikin; Nurul Akma Mohd Y...; ; Saiful Anuar Abd ...; ; Al Emran Ismail; ; Salihatun Salleh; ; Sufizar Ahmad; ; Mohd Nasrull Abdo...; ; Shahruddin Mahzan; ; Sallehuddin Shah ...
• Keywords: 0103 physical sciences; TJ Mechanical engineering and machinery; TJ170-179 Mechanics applied to machinery. Dynamics; 01 natural sciences; TL500-777 Aeronautics. Aeronautical engineering; 620

This paper presented a computational fluid dynamics (CFD) simulation of air flow past a 2D model NACA0012 airfoil at high Reynolds number (Re = 3.0 x 106) at various angles of attack (-10° to 15°). The simulations were undertaken to inform on how the fluid flowed around the airfoil by solving the steady state governing equations of continuity and momentum conservation that are combined with one of three turbulence models Spalart-Allmaras, Realizable k-e and k-ω shear stress transport (SST). It is observed that the Realizable k- e eliminates the small separation bubble on the upper surface of the airfoil and delaying separation flow. Also, for the lift coefficient, CL and drag coefficient, CD investigated in this paper, the predicted data have good agreement with other published data.