PropellerPower:

Path: ACPro/ACEngine

% Propeller power and induced velocity
--------------------------------------------------------------------------
   Form:
   [p, w] = PropellerPower( rho, a, t, v )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   rho       (1,1) Density (kg/m^3)
   a         (1,1) Propeller disk area (m^2)
   t         (1,:) Thrust (N)
   v         (1,1) Velocity (m/s)

   -------
   Outputs
   -------
   p         (1,:) Power (W)
   w         (1,:) Induced velocity (m/s)

--------------------------------------------------------------------------

Children:

Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle

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