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

  • Azmahani Sadikin Universiti Tun Hussein Onn Malaysia http://orcid.org/0000-0003-4501-5081
  • Nurul Akma Mohd Yunus
  • Saiful Anuar Abd Hamid
  • Al Emran Ismail
  • Salihatun Md Salleh
  • Mohd Nasrull Abdol Rahman
  • Shahruddin Mahzan
  • Sallehuddin Shah Ayop
Keywords: NACA0012 airfoil, CFD, Spalart-Allmaras, Realizable k- ε, k-ω SST, lift coefficient, drag coefficient

Abstract

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-ε and k-ω shear stress transport (SST). It is observed that the Realizable k- ε 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.

Published
2018-04-25
How to Cite
Sadikin, A., Mohd Yunus, N. A., Abd Hamid, S. A., Ismail, A. E., Md Salleh, S., Abdol Rahman, M. N., Mahzan, S., & Ayop, S. S. (2018). A Comparative Study of Turbulence Models on Aerodynamics Characteristics of a NACA0012 Airfoil. International Journal of Integrated Engineering, 10(1). Retrieved from https://publisher.uthm.edu.my/ojs/index.php/ijie/article/view/1901
Section
Articles

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