Python interface for XFOIL. The objective of this library is to be able to be able to call XFOIL from Python iteratively for any simulation in a total of 4 lines total.
I was trying to implement the code as shown below.
from aeropy.xfoil_module import find_coefficients
find_coefficients(airfoil='naca0012',alpha=12.)
Whenever I try using any of the modules I get the error [WinError 2] The system cannot find the file specified. Could you explain as to what the problem is?
Hello!
I was trying to implement the code as shown below.
from aeropy.xfoil_module import find_coefficients find_coefficients(airfoil='naca0012',alpha=12.)
Whenever I try using any of the modules I get the error [WinError 2] The system cannot find the file specified. Could you explain as to what the problem is?