Hello guys

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 .???