  
  
  ============  AERO RESULTS ========== 
  
  ==== Input for AERO ====
  
Surface Area of the Wing =    177.300     ft^2
Wing Span =    22.7200     ft
Length of Fuselage =    32.6000     ft
Diameter of Fuselage =    4.85000     ft
  
  === Output from AERO ===
  
Surface Area of the Fuselage =    396.807     ft^2
Wetted Area of the Aircract =    845.680     ft^2
Lift/Drag of the Aircract =    8.44158    
