standardize airfoil #69
Description
There should probably be a function similar to the position coordinates function that takes an arbitrary airfoil and standardizes it. Such a function would need to:
- move the trailing edge to the point (1,0)
- determine the furthest point from the trailing edge, ideally in a smooth manner not limited to the provided coordinates
- determine the angle between those points
- rotate the airfoil to put the leading edge on the axis
- scale the airfoil such that the leading edge is at the point (0,0)
It's a bit more involved in some aspects than the position coordinates function, but the bare bones is just a reverse of it.