The next result illustrates a wing similar to the B-2 airplane. The data shown is sufficient to define the wing.
In order to make the input file to getmac, the length of the chords at each breakpoint must be known. The LinInterp tool makes it easy to get these points
The chords are 1300, 500, 500, and 0 in length. The leading edges are at 0, 400, 750, and 1000 with y=0, 480, 900, and 1200.