RotorAssemblyAerodynamics

RotorAssemblyAerodynamics:

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   Computes the aerodynamic force and torque of each surface in the rotor
   assembly. This function should be replaced by a more detailed model.
   This model assumes that the wing camber is along x and the normal
   to the wing is along z. y is along the wing length.
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   Form:
   [force, torque] = RotorAssemblyAerodynamics( v, k )
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   Inputs
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   v   	      (3,1)  Wind-relative velocity vector in the local frame
   k             (1,1)  Element ID
   fd            (3,1)  Additional data* optional
                       

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   Outputs
   -------
   force   	  (3,1)  Force vector
   torque      (3,1)  Torque vector

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Children:

Math: Linear/Mag
Math: Linear/Unit