fastga.models.geometry.geom_components.fuselage.components.compute_fuselage_max_width module

Python module for fuselage maximum width calculation, part of the fuselage dimension.

class fastga.models.geometry.geom_components.fuselage.components.compute_fuselage_max_width.ComputeFuselageMaxWidth(**kwargs)

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Computes maximum cabin width.

Cabin width considered is for side by side seats, and it is computed based on cylindrical fuselage.

Store some bound methods so we can detect runtime overrides.

setup()

Declare inputs and outputs.

Available attributes:

name pathname comm options

compute(inputs, outputs, discrete_inputs=None, discrete_outputs=None)

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

Parameters

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

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

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

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

compute_partials(inputs, partials, discrete_inputs=None)

Compute sub-jacobian parts. The model is assumed to be in an unscaled state.

Parameters

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

• partials (Jacobian) – Sub-jac components written to partials[output_name, input_name]..

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