问题 I have a little issue with calculating coordinates. Given are airfoil profiles in two lists with the following exemplary coordinates: Example: x_Coordinates = [1, 0.9, 0.7, 0.5, 0.3, 0.1, 0.0, ...] y_Coordinates = [0, -0.02, -0.06, -0.08, -0.10, -0.05, 0.0, ...] diagram 1: The only known things about the profile are the lists above and the following facts: the first coordinate is always the trailing edge, in the example above at (x=1, y=0) the coordinates always run on the bottom/underside to