RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.create_avl_datastructures.append_avl_wing_control_surfaces

append_avl_wing_control_surfaces(rcaide_wing, avl_wing, semispan, root_chord_percent, tip_chord_percent, tip_percent_span, root_percent_span, root_twist, tip_twist, tip_airfoil, seg_tag, dihedral, origin, sweep)

Converts control surfaces on a rcaide wing to sections in avl wing

Assumptions:

None

Source:

None

Inputs:

rcaide_wing [-] avl_wing [-] semispan [meters] root_chord_percent [unitless] tip_chord_percent [unitless] tip_percent_span [unitless] root_percent_span [unitless] root_twist [radians] tip_twist [radians] tip_airfoil [unitless] seg_tag [unitless] dihedral [radians] origin [meters] sweep [radians]

Outputs:

None

Properties Used:

N/A