check computation of total forces and moments about CG/reference point.

[Bill-B]

We know CFX is negative

[bramesfeld]

• Not sure if we already compute Mx and Mz

• Are the moments computed from the lifting line?

• Mx and Mz should ideally be based on an integrated value of the forces across the DVE span (simple integration of a parabola)

[Bill-B]

In progress.

• Need to fix problem with non-symmetric normal force when m>1.

• Where to position drag? With drag at the TE, it causes a pitch moment

• Need to compare pitch moment to xfoil.

• Need to confirm logic, especially parabolic offset

[Bill-B]

Small differences in moments compared to AVL.
Comparison of 2D case to xfoil Cm is good. Careful, only use n=1 for infinite wing case.