Working out the Lift/Drag Force

Hi, I am a student and new to Ansys CFX. Been using it to analyse an aerofoil for my dissertation project. Managed to mesh and produce a final solution with the aerofoil at AoA 8 degrees at 30m/s. However I am struggling with obtaining the lift/drag data from the aerofoil. How would I do it? Any help would be appreciated, thanks

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