MEAN AERODYNAMIC CHORD DEFINED BY b2.nml
# y xle c xte
1 0.00000 0.00000 1300.00000 1300.00000
2 480.00000 400.00000 500.00000 900.00000
3 900.00000 750.00000 500.00000 1250.00000
4 1200.00000 1000.00000 0.00000 1000.00000
area of wing= 717000.0000
length of MAC= 759.2748
y of MAC= 429.8745
xle of MAC= 358.2287
xte of MAC= 1117.5035
x of c/4 of MAC= 548.0474