Analyse CFD de l’écoulement transsonique autour d’un profil d’aile NACA 0012

Computational Fluid Dynamics (CFD) incorporates mathematical relations and algorithms to analyze and solve the problems regarding fluid flow. CFD analysis of an airfoil produces results such as lift and drag forces which determines the ability of an airfoil. In this paper a transonic flow will be modelled over a NACA 0012 airfoil for which experimental data has been published, so that a comparison can be made. The flow to be considered is compressible and turbulent and the solver used is the density based implicit solver, which gives good results for high speed compressible
flows. The results show that the predicted lift, drag and pressure coefficients are in good agreement with experimental data.

Computational Fluid Dynamics (CFD) incorporates mathematical relations and algorithms to analyze and solve the problems regarding fluid flow. CFD analysis of an airfoil produces results such as lift and drag forces which determines the ability of an airfoil. In this paper a transonic flow will be modelled over a NACA 0012 airfoil for which experimental data has been published, so that a comparison can be made. The flow to be considered is compressible and turbulent and the solver used is the density based implicit solver, which gives good results for high speed compressible
flows. The results show that the predicted lift, drag and pressure coefficients are in good agreement with experimental data.

CFD aerodynamic NACA 0012 pressure coefficient airfoil

CFD aerodynamic NACA 0012 pressure coefficient airfoil