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 | |
This is a low-fidelity propeller component. Assumptions: None Source: None
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.
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 [-]