aircraft.components.fuselage

Module Contents

Classes

Fuselage	The fuslage component class.
FuselageGeometricQuantities
FuselageParameters

class aircraft.components.fuselage.Fuselage(length: Union[int, float, csdl_alpha.Variable], max_width: Union[int, float, csdl_alpha.Variable, None] = None, max_height: Union[int, float, csdl_alpha.Variable, None] = None, geometry: Union[lsdo_function_spaces.FunctionSet, None] = None, **kwargs)

Bases: CADDEE_alpha.core.component.Component

The fuslage component class.

Parameters

- length

- max_width

- max_height

Note that parameters may be design variables for optimizaiton.

If a geometry is provided, the geometry parameterization sovler

will manipulate the geometry through free-form deformation such

that the wing geometry satisfies these parameters.

Attributes

- parametersdata class storing the above parameters

- geometryb-spline set or subset containing the wing geometry

- compsdictionary for children components

- quantitiesdictionary for storing (solver) data (e.g., field data)

_extract_geometric_quantities_from_ffd_block()

Extract the following quantities from the FFD block: - fuselage length - fuselage max width - fuselage max heigtht

_setup_ffd_block(ffd_block, parameterization_solver, plot: bool = False)

Set up the fuselage ffd block.

_setup_ffd_parameterization(fuselage_geometric_qts: FuselageGeometricQuantities, ffd_geometric_variables)

Set up the fuselage parameterization.

_setup_geometry(parameterization_solver, ffd_geometric_variables, plot: bool = False)

Set up the fuselage geometry (mainly for FFD)

class aircraft.components.fuselage.FuselageGeometricQuantities

height: csdl_alpha.Variable

length: csdl_alpha.Variable

width: csdl_alpha.Variable

class aircraft.components.fuselage.FuselageParameters

S_wet: Union[float, int, csdl_alpha.Variable, None]

length: Union[float, int, csdl_alpha.Variable]

max_height: Union[float, int, csdl_alpha.Variable]

max_width: Union[float, int, csdl_alpha.Variable]