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

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

class fastga.models.geometry.geom_components.wing_tank.components.compute_wing_tank_thickness_array.ComputeWingTankThicknessArray(**kwargs)[source]

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Computes the thickness for each section of the tank. Based on wing thickness and a correction penalty.

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.