Path: ACPro/ACDesign
% Compute the propeller thrust coefficient This is the minimum power to drive a propeller. This is based on actuator disk theory. Type CTPropeller for a demo. -------------------------------------------------------------------------- Form: cT = CTPropeller( angle, j ) -------------------------------------------------------------------------- ------ Inputs ------ angle (1,:) deg j (1,:) Advance ratio ------- Outputs ------- cT (1,:) Thrust coefficient -------------------------------------------------------------------------- Reference: McCormick 1979, Figure 7.8. --------------------------------------------------------------------------
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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