airfoil 2D simulation: position of lift force on the airfoil
 

Hello,

I've done 2D simulation of an airfoil in Fluent 13.0. I can calculate the Cl en Cd as shown in several tutorials on the internet.

But I need the coordinates (position) were the lift force acts on the airfoil.
Can this be calculated in Fluent? Or how can I obtain the position?

many thanks!

Koen

Fluent can display moment (torque), then divide it by force and you will know the force arm relatively you reference point

thanks for your reply!!