fastga.models.aerodynamics.components.compute_cl_extreme module

Estimation of the 3D maximum lift coefficients for wing and tail.

class fastga.models.aerodynamics.components.compute_cl_extreme.ComputeAircraftMaxCl(**kwargs)[source]

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Add high-lift contribution (flaps)

Store some bound methods so we can detect runtime overrides.

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.