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

Estimation of geometry of fuselage part A - Cabin (Commercial).

class fastga.models.geometry.geom_components.fuselage.components.compute_fuselage_dimensions.ComputeFuselageGeometryBasic(**kwargs)

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Geometry of fuselage - Cabin length defined with total fuselage length input (no sizing).

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.

class fastga.models.geometry.geom_components.fuselage.components.compute_fuselage_dimensions.ComputeFuselageGeometryCabinSizingFD(**kwargs)

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Geometry of fuselage - Cabin is sized based on layout (seats, aisle…) and HTP/VTP position (Fixed tail Distance).

Store some bound methods so we can detect runtime overrides.

initialize()

Perform any one-time initialization run at instantiation.

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.

class fastga.models.geometry.geom_components.fuselage.components.compute_fuselage_dimensions.ComputeFuselageGeometryCabinSizingFL(**kwargs)

Bases: openmdao.core.explicitcomponent.ExplicitComponent

Geometry of fuselage - Cabin is sized based on layout (seats, aisle…) and additional rear length (Fixed Length).

Store some bound methods so we can detect runtime overrides.

initialize()

Perform any one-time initialization run at instantiation.

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.