fastga.models.geometry.geom_components.wing_tank.components.compute_wing_tank_width_array module

Python module for tank width computation class(es), part of the advanced MFW computation method.

class fastga.models.geometry.geom_components.wing_tank.components.compute_wing_tank_width_array.ComputeWingTankWidthArray(**kwargs)[source]

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Computes the wing tank width array taking into account aileron and wing chord percentages. Does not consider reduction due to engine and landing.

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.

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)[source]

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.