Plot uniform wing surface using airfoil points

Produce a 3D surface plot of a uniform wing using the X and Y data of an airfoil.

airfoil2wing(X2D, Y2D, WingSpan, MeshSize) returns a 3D surface plot of

the wing described by X2D and Y2D airfoil.

Inputs:

- X2D: column/row vector containing the X-xoordinates of the

airfoil

- Y2D: column/row vector containing the Y-xoordinates of the

airfoil

- WingSpan: a scalar describing the desired span of the wing.

- MeshSize: an integer number describing the number of mesh

elements along the length of the wing

- varargin (Optional): options for the surf function

Outputs:

- X3D, Y3D, Z3D: 2D matrices containing the x, y, and z coordinates

of the surface of the wing