fastga_he.models.propulsion.components.source.high_rpm_ice.components.sizing_high_rpm_ice_nacelle_dimensions module

class fastga_he.models.propulsion.components.source.high_rpm_ice.components.sizing_high_rpm_ice_nacelle_dimensions.SizingHighRPMICENacelleDimensions(**kwargs)[source]

Bases: ExplicitComponent

Computation of the dimensions of the ICE nacelle. Based on some very simple geometric ratio which depend on the engine position. When not on the wing, the nacelle dimensions will purely be indicative.

Store some bound methods so we can detect runtime overrides.

initialize()[source]

Perform any one-time initialization run at instantiation.

setup()[source]

Declare inputs and outputs.

Available attributes:

name pathname comm options

compute(inputs, outputs, discrete_inputs=None, discrete_outputs=None)[source]

Compute outputs given inputs. The model is assumed to be in an unscaled state.

An inherited component may choose to either override this function or to define a compute_primal function.

Parameters:

  • inputs (Vector) – Unscaled, dimensional input variables read via inputs[key].

  • outputs (Vector) – Unscaled, dimensional output variables read via outputs[key].

  • discrete_inputs (dict-like or None) – If not None, dict-like object containing discrete input values.

  • discrete_outputs (dict-like or None) – If not None, dict-like object containing discrete output values.