Public Member Functions | |
def | __defaults__ (self) |
def | evaluate_thrust (self, state) |
Public Attributes | |
propulsor | |
battery | |
motor_efficiency | |
tag | |
number_of_engines | |
esc | |
avionics | |
payload | |
voltage | |
generative_design_minimum | |
Public Attributes inherited from SUAVE.Components.Energy.Networks.Network.Network | |
tag | |
generative_design_max_per_vehicle | |
non_dimensional_origin | |
number_of_engines | |
engine_length | |
wing_mounted | |
areas | |
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 | |
Simply connects a battery to a ducted fan, with an assumed motor efficiency Assumptions: None Source: None
def SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan.__defaults__ | ( | self | ) |
This sets the default values for the network to function. This network operates slightly different than most as it attaches a propulsor to the net. Assumptions: Source: N/A Inputs: None Outputs: None Properties Used: N/A
Reimplemented from SUAVE.Components.Energy.Networks.Network.Network.
def SUAVE.Components.Energy.Networks.Battery_Ducted_Fan.Battery_Ducted_Fan.evaluate_thrust | ( | self, | |
state | |||
) |
Calculate thrust given the current state of the vehicle Assumptions: Constant mass batteries ESC input voltage is constant at max battery voltage Source: N/A Inputs: state [state()] Outputs: results.thrust_force_vector [newtons] results.vehicle_mass_rate [kg/s] Properties Used: Defaulted values