Lift and drag

Hi,

I have made a wing in caedium and I suceeded to plot the pressure coefficients over the wing.
Now i want to plot the amount of lift and drag and the lift and drag coefficients in a graph, to determine the performance of my model. How can i do this in caedium?
I studied on different tutorials and i think i have to create and add a new kind of result, but i dont have a clue of which scalars or vectors the new result must be composed from. Can someone help me with this?

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Derived from force

Lift and drag coefficients are derived from Vector Variables->F (force) on the Results Tool Palette. For more details see the comment "Lift and Drag Coefficients."

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