Lift and Drag Coefficient settings for airfoil with AOA and aileron deflection

hey guys, I'm trying to find the lift and drag coefficient for my airfoil(8 degrees AOA) with an aileron deflection (20 degrees upwards), but confused on how to set the lift coefficient and drag coefficient, monitors, especially the x and y directions for the force vectors. Does anyone have any suggestions? the airfoil picture is below.

 

 

 

 

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