Pressure Coefficient
 

Hi,
firstly, I would like to apologize if there exists this thread, but i couldn´t find it. I created mesh for DLR F11 (from AIAA workshop) and in Fluent I calculated it. Now I would like to see the distribution of pressure coefficient on wing, flap and slot in determined distance from symmetry. I made a plane in distance which I want to analyze but when I make XY Plot for this plane, it makes tens of thousands points and it is impossible to match this points for wing or slot or flap. Is there some easy way how to get only few points of distribuion of pressure coefficient in intersection of wing or slot or flap? Thank you very much :-)