Hi, I’m trying to draw the mean camber line of an airfoil, and I’ve copied the formulas I’ve found from various places online, so the formulas should be correct, but for some reason the trailing edge doesn’t stay in the same place.
The trailing edge (Furthest right point) should always stay at the same height as the leading edge (furthest left point), creating a horizontal line between them both, but for some reason it raises and lowers depending on the Max Camber(%) and Max Camber Chord Position(%)
The first part (Pos % is before the Max Camber Pos %) works fine, it’s just calculating the part after the max camber that isn’t working properly
Here’s a video of what’s happening MeanCamberLine - YouTube