Takeoff:

Path: ACPro/ACPerformance

% Computes the required roll distance and liftoff velocity.
   To see a demo, run with no inputs:  [s,v,def] = Takeoff;

--------------------------------------------------------------------------
   Form:
   [sTotal, vLiftoff, def] = Takeoff( d, altitude )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   d              (1,1)  See "ConcordeProperties.m"
   altitude       (1,1)  Altitude (m)

   -------
   Outputs
   -------
   sTotal         (1,1)  Ground roll (m)
   vLiftoff       (1,1)  Liftoff velocity (m/s)
   def            {12,3} Data structure definition

--------------------------------------------------------------------------
   Reference: Mair, W. A. and D. L. Birdsall, "Aircraft Performance,"
              Cambridge, p. 139.
--------------------------------------------------------------------------

Children:

ACPro: ACPerformance/VStall
AerospaceUtils: AeroData/AtmData
Common: Atmosphere/StdAtm
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle

Back to the ACPro Module page