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Proceedings of the 3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)
When the γ − Re transition model is used to calculate the aerodynamic performance of the wind turbine airfoils, the SIMPLE algorithm is usually applied to solve the equation of speed and pressure for airfoil surface. Consequently the precision of the results by using SIMPLE algorithm is comparatively low. Therefore, For the newly wind turbine airfoil named CQU-DTU-LN118, COUPLED algorithm is selected to solve the equation of speed and pressure for airfoil fluid surface. The results of SIMPLEdoi:10.2991/mme-16.2017.53 fatcat:kzb3mjlbnzezhcp4wxdzeeueqq