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
Hello, So I set the airfoil as follows:
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