fastga_he.models.propulsion.components.connectors.dc_bus.components.sizing_dc_bus_drag module

class fastga_he.models.propulsion.components.connectors.dc_bus.components.sizing_dc_bus_drag.SizingDCBusDrag(**kwargs)

Bases: ExplicitComponent

Class that computes the drag coefficient of the DC bus based on its position. Will be 0.0 all the time as we wil make the assumption that the DC bus is “inside” the fuselage or in the fairing of the motor if inside the wing (and thus is already accounted for in the wing drag calculation).

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