VStall:

Path: ACPro/ACPerformance

% Computes the stall velocity.

   Since version 3 (ACT).
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   Form:
   vStall = VStall( d, altitude )
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   ------
   Inputs
   ------
   d              (1,1)  Data structure
                         .cLMax      (1,1) Max lift coefficient
                         .wingArea   (1,1) Wing area
                         .massDesign (1,1) mass
   altitude       (1,1)  Altitude (m)

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

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

Common: Atmosphere/StdAtm
Common: Graphics/Plot2D

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