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SUPPORT SITE |
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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) --------------------------------------------------------------------------
Common: Graphics/Plot2D
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