StallVelocity:

Path: ACPro/ACPerformance

% Computes takeoff velocity.

   Type StallVelocityTakeoffVelocity for a demo.
   Since version 5.
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   Form:
   vStall = StallVelocity( m, cLMax, s, rho )
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   Inputs
   ------
   m              (1,1)  Mass (m)
   cLMax          (1,1)  Maximum Lift coefficient
   s              (1,1)  Reference area
   rho            (1,1)  Atmospheric density (kg/m^3)

   -------
   Outputs
   -------
   vStall         (1,:)  Stall velocity

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   Reference: Anderson, J. D., "Introduction to Flight 3rd Edition,",
              McGraw-Hill 1989, pp 318-324.
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