SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Components.Energy.Converters.Propeller.Propeller Class Reference
Inheritance diagram for SUAVE.Components.Energy.Converters.Propeller.Propeller:
SUAVE.Components.Energy.Converters.Rotor.Rotor SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component

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
 

Detailed Description

This is a propeller component, and is a sub-class of rotor.

Assumptions:
None

Source:
None

Member Function Documentation

◆ __defaults__()

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.


The documentation for this class was generated from the following file: