fastoad.models.aerodynamics.components.compute_polar module

FAST - Copyright (c) 2016 ONERA ISAE

class fastoad.models.aerodynamics.components.compute_polar.PolarType(value=<no_arg>, names=None, module=None, type=None, start=1, boundary=None)[source]

Bases: aenum.Enum

An enumeration.

HIGH_SPEED = 'high_speed'
LOW_SPEED = 'low_speed'
TAKEOFF = 'takeoff'
LANDING = 'landing'
class fastoad.models.aerodynamics.components.compute_polar.ComputePolar(**kwargs)[source]

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Store some bound methods so we can detect runtime overrides.

Parameters

**kwargs (dict of keyword arguments) – Keyword arguments that will be mapped into the Component options.

initialize()[source]

Perform any one-time initialization run at instantiation.

setup()[source]

Declare inputs and outputs.

Available attributes:

name pathname comm options

setup_partials()[source]

Declare partials.

This is meant to be overridden by component classes. All partials should be declared here since this is called after all size/shape information is known for all variables.

compute(inputs, outputs)[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.

fastoad.models.aerodynamics.components.compute_polar.get_optimum_ClCd(ClCd)[source]