I am doing a flow sim of a 2D airfoil.
For getting Lift and Drag forces I have selected the globle component of forces.Also a moment can be found by a globle component of torque.
For getting the coefficient of moment I need a point at which the flow sim calculates a torque value. Also to get a quarter chord coefficient of
moment I need the point on the chord of airfoil at which lift and Drag forces are acting.
I went through the tutorials but it didn't help much.
Can anyone help me out in this .???