Thanks for the link...

Here are my results: Would you confirm my interpretation?

Mean Aerodynamic Chord (MAC) = 12.34

MAC distance from root chord (d) = 15.3

Wing Aerodynamic Center aft of root LE = 3.59

Ideal Center of Gravity %MAC = NaN%

Actual Center of Gravity %MAC = no value

Ideal CG aft of root LE = NaN

Neutral Point %MAC (NP) = 44.6%

Neutral Point aft of Wing's root LE (NP) = 6

Distance between Ideal CG and NP (E) = NaN


Would I set the CG at 44.6% of 12.34 inches?