Iterations
 

Hi I am using a structured c-mesh to analyze the GA (W)-1 airfoil to get a Y+ under 4.0 with Fluent at Spalart-Allmaras model taking into account the realistic conditions of Re, cord, Pt, Tt, density, Viscosity, and turbulent viscosity for an altitude of 966216 Pa, but the iterations are giving non-realistic results and don't converge. Could somebody teach me how I must define all conditions before initialize? Thanks for your help.