RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Wing

Wing

class Wing(*args, **kwarg)

Bases: Data

This class that defines parameters of the AVL aircraft wing

Assumptions:

None

Source:

None

Inputs:

None

Outputs:

None

Properties Used:

N/A

append_section(section)

Adds a segment to the wing

class Section(*args, **kwarg)

Bases: Data

This class defines the sections of the aircraft wing in AVL. Each section can be thought of as a trapezoid

Assumptions:

None

Source:

None

Inputs:

None

Outputs:

None

Properties Used:

N/A

append_control_surface(control)

Adds a control_surface to the wing section in AVL

Assumptions:

None

Source:

None

Inputs:

None

Outputs:

None

Properties Used:

N/A

class Control_Surface(*args, **kwarg)

Bases: Data

This class defines the control surface geometry and deflection on the aircraft wing in AVL

Assumptions:

None

Source:

None

Inputs:

None

Outputs:

None

Properties Used:

N/A

class Control_Surface_Data(*args, **kwarg)

Bases: Data

This class stores results from the control surfaces

append_control_surface_result(control_res)

Adds a control_surface to the wing section in AVL

class Control_Surface_Results(*args, **kwarg)

Bases: Data

This class defines the control surface geometry and deflection