You are an expert in writing code in many different languages. Your goal is to perform code completion for the following code, keeping in mind the rest of the code and the file meta data.
    Metadata details:
    filename: wingAirfoilMapCreateEmpty.m
    path of file: ./repos/LADAC/aerodynamics/vlm_wing/airfoil
    
    the code of the file until where you have to start completion: function airfoil_map = wingAirfoilMapCreateEmpty( )
% wingAirfoilMapCreateEmpty creates an empty airfoil_map struct.
% 
% Outputs:
%   airfoil_map         Struct that contains multiple profile aerodynamics
%                       maps (structs)
% 

% Disclamer:
%   SPDX-License-Identifier: GPL-3.0-only
% 
%   Copyright (C) 2020-2022 Yannic Beyer
%   Copyright (C) 2022 TU Braunschweig, Institute of Flight Guidance
% *************************************************************************

airfoil_map.map_cl.data=0;
airfoil_map.map_cl.dim=[1,1,1,1,1];
airfoil_map.map_cd.data=0;
airfoil_map.map_cd.dim=[1,1,1,1,1];
airfoil_map.map_cm.data=0;

    
function airfoil_map = wingAirfoilMapCreateEmpty( )
% wingAirfoilMapCreateEmpty creates an empty airfoil_map struct.
% 
% Outputs:
%   airfoil_map         Struct that contains multiple profile aerodynamics
%                       maps (structs)
% 

% Disclamer:
%   SPDX-License-Identifier: GPL-3.0-only
% 
%   Copyright (C) 2020-2022 Yannic Beyer
%   Copyright (C) 2022 TU Braunschweig, Institute of Flight Guidance
% *************************************************************************

airfoil_map.map_cl.data=0;
airfoil_map.map_cl.dim=[1,1,1,1,1];
airfoil_map.map_cd.data=0;
airfoil_map.map_cd.dim=[1,1,1,1,1];
airfoil_map.map_cm.data=0;
airfoil_map.map_cm.dim=[1,1,1,1,1];
airfoil_map.alpha.data=0;
airfoil_map.alpha.dim=[1,1];
airfoil_map.Mach.data=0;
airfoil_map.Mach.dim=[1,1];
airfoil_map.Reynolds.data=0;
airfoil_map.Reynolds.dim=[1,1];
airfoil_map.actuator_1.data=0;
airfoil_map.actuator_1.dim=[1,1];
airfoil_map.actuator_2.data=0;
airfoil_map.actuator_2.dim=[1,1];

end