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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