Public Member Functions | |
def | __defaults__ (self) |
Public Member Functions inherited from SUAVE.Components.Energy.Converters.Rotor.Rotor | |
def | spin (self, conditions) |
def | vec_to_vel (self) |
def | body_to_prop_vel (self) |
def | prop_vel_to_body (self) |
def | vec_to_prop_body (self) |
Public Attributes | |
tag | |
orientation_euler_angles | |
use_2d_analysis | |
variable_pitch | |
Public Attributes inherited from SUAVE.Components.Energy.Converters.Rotor.Rotor | |
tag | |
number_of_blades | |
tip_radius | |
hub_radius | |
twist_distribution | |
sweep_distribution | |
chord_distribution | |
thickness_to_chord | |
blade_solidity | |
design_power | |
design_thrust | |
airfoil_geometry | |
airfoil_polars | |
airfoil_polar_stations | |
radius_distribution | |
rotation | |
orientation_euler_angles | |
ducted | |
number_azimuthal_stations | |
vtk_airfoil_points | |
induced_power_factor | |
profile_drag_coefficient | |
use_2d_analysis | |
nonuniform_freestream | |
axial_velocities_2d | |
tangential_velocities_2d | |
radial_velocities_2d | |
start_angle | |
variable_pitch | |
Wake | |
azimuthal_distribution | |
outputs | |
Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component | |
inputs | |
outputs | |
Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component | |
tag | |
mass_properties | |
origin | |
symmetric | |
Public Attributes inherited from SUAVE.Components.Component.Component | |
tag | |
origin | |
generative_design_max_per_vehicle | |
generative_design_characteristics | |
generative_design_special_parent | |
This is a propeller component, and is a sub-class of rotor. Assumptions: None Source: None
def SUAVE.Components.Energy.Converters.Propeller.Propeller.__defaults__ | ( | self | ) |
This sets the default values for the component to function. Assumptions: None Source: N/A Inputs: None Outputs: None Properties Used: None
Reimplemented from SUAVE.Components.Energy.Converters.Rotor.Rotor.