Support for checking if panelling failed for an Airfoil.

[atharvaaalok]

Hello,
So I set the airfoil as follows:

xf = XFoil()
xf.airfoil = my_airfoil_obj

But I get an output on the console saying that the airfoil could be panelled.
How can I obtain this from the function itself?
How can I, in python, determine that xfoil could not panel the airfoil that I set.

Attaching the error I see and my airfoil coordinate file.

air.txt