[losiola]

Hello ,
Good Morning

I am trying to make a wind turbine airfoil simulation , the blade is made of 3 different Airfoils ,

So i made the 2D airfoil simulation and got the graphs for both Cl Cd Cm for each airfoil .

now I ve made the 3D geometry and i want to calculate Cl Cd And Cm at different sections of the Blade . Does anyone Know How can i do that ? (Calculate Cl Cd Cm for different sections of the Blade )

Many Thanks