fastga_he.models.propulsion.components.loads.dc_load.components.sizing_aux_load_drag module

class fastga_he.models.propulsion.components.loads.dc_load.components.sizing_aux_load_drag.SizingDCAuxLoadDrag(**kwargs)

Bases: ExplicitComponent

Class that computes the drag coefficient of the auxiliary load based on its position. Will be 0.0 all the time as we wil make the assumption that it is “inside” any part of the aircraft it is located in.

Store some bound methods so we can detect runtime overrides.

initialize()

Perform any one-time initialization run at instantiation.

setup()

Declare inputs and outputs.

Available attributes:

name pathname comm options