Hi there,
first of all, it`s really great to have this module.
I tried to set the transition position, but got the following error:
`>>> xf.xtr((1.0, 0.95))
Traceback (most recent call last):
File "", line 1, in
File "/home/moritz/.local/lib/python3.10/site-packages/xfoil/xfoil.py", line 126, in xtr
return float(xtr_top), float(xtr_bot)
ValueError: could not convert string to float: c_float(1.0)
`
I used the included naca0012 airfoil.
Thanks in advance,
Moritz