fastga_he.models.propulsion.components.connectors.dc_sspc.components.sizing_dc_sspc_drag module

class fastga_he.models.propulsion.components.connectors.dc_sspc.components.sizing_dc_sspc_drag.SizingDCSSPCDrag(**kwargs)

Bases: ExplicitComponent

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