aerooutput.txt

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  ============  AERO RESULTS ========== 
  
  ==== Input for AERO ====
  
Surface Area of the Wing =    293.300    
Aspect Ratio of the Wing =    9.68618    
Length of Fuselage =    12.3300    
Diameter of Fuselage =    12.3300    
  
  === Output from AERO ===
  
Surface Area of the Fuselage =    155.679    
Wetted Area of the Aircract =    918.259    
Lift/Drag of the Aircract =    16.0000    

=========== GEOMETRIC WING DATA =============

Cross Sectional Areas

2.447
3.998
7.433
11.56
16.98
22.34
45.76
104.6
122.3
130.2


Control Points

1,2,2
1,2,3
1,2,4
1,2,5
2,2,4