I'm trying to reproduce the shape of an airfoil's camber line using the leading edge angle, the trailing edge angle, the chord and the max camber value.
I cannot use a spline because it overshoots the "max camber".
I cannot use 'pchip', a piecewise cubic Hermitian interpolation because I can't clamp ends.
I cannot use 'csape' as well because it is a cubic spline interpolation (and therefore overshoots)
I'm playing around to generate a fifth order function, but I fear it is a futile endeavor.