Virtual Aircraft Lab

Technological Institute of Aeronautics

Aircraft Design - Design diagram
Landing field length | Takeoff field length | Second segment climb | Missed approach | Cruise speed
Maximum operating Mach number
MMO :   [ -] 		Maximum takeoff weight
MTOW:  [ kg ] 		Cruise altitude [ft] Wing aspect ratio
AR:  [ -]
Number of engines
2
3
4		 Engine by-pass ratio
 Engine diameter
[m]		 MLW/MTOW
0.90
0.81
0.75
Another  
CLmax,landing
[-]		 Landing field length
(MLW, ISA, sea level)
[m]		 Takeoff field length
 (MTOW, ISA, sea level)
[m]		 CLmax,TO
 [-]
   
Sound speed @ cruise
  [m/s]		 LFL Wing loading
  [kg/m2]		 Wetted area
  [m2]

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