Airfoil hinge moments needed.
 

Hi,

I'm solving the flow over a 2D airfoil in Fluent V6. One of the outputs I need is the aileron hinge moment. Is there a quick way to generate this automatically. I just need the moment from those parts of the surface from the x-position of the hinge to the trailing edge. I don't have any gaps or anything, it's just a continuous surface.

Any help would be greatly appreciated.