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

Public Member Functions

def __defaults__ (self)
 
def spin (self, conditions)
 

Public Attributes

 tip_radius
 
 propulsive_efficiency
 
- 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 low-fidelity propeller component.

Assumptions:
None

Source:
None

Member Function Documentation

◆ __defaults__()

def SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid.__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.Energy_Component.Energy_Component.

◆ spin()

def SUAVE.Components.Energy.Converters.Propeller_Lo_Fid.Propeller_Lo_Fid.spin (   self,
  conditions 
)
Analyzes a propeller given geometry and operating conditions.

Assumptions:
per source

Source:
Qprop theory document

Inputs:
self.inputs.omega            [radian/s]
self.inputs.torque           [Nm]
conditions.freestream.
  density                    [kg/m^3]
  dynamic_viscosity          [kg/(m-s)]
  velocity                   [m/s]
  speed_of_sound             [m/s]
  temperature                [K]

Outputs:
conditions.propulsion.etap   [-]  (propulsive efficiency)
thrust                       [N]
Qm                           [Nm] (torque)
power                        [W]
Cp                           [-]  (coefficient of power)

Properties Used:
self.tip_radius              [m]
self.propulsive_efficiency   [-]

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