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set_wing_angle(self,
value,
unit=' deg ' )
Set the wing angle for the rotor and recalculate the corresponding
reference frame. |
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prepend_references(self,
refs)
Add the tower and nacelle reference frames for every blade |
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get_prandtl_factor(self,
blade,
section)
Return the Prandtl correction factor |
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_average_induced_velocity(self)
The same induced velocity is calculated for the the whole wake |
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_find_skew_section_id(self)
Find the section used to compute the skew angle |
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init_aero_unsteady(self)
Init the unsteady BEM code by finding the deepest point into the
wake |
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_apply_yaw_model(self)
Apply the yaw model, a restoring couple when the rotor is not
facing the wind |
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get_velocity_correction(self)
Supposed to return a velocity correction in the tower shadow model
but not yet used |
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