Open jazzguru1 opened 2 years ago
Hey, I know this is over 2 years old now, but just in case you or someone else comes across this issue looking for a solution, the trick is to use the parameter NACA=False
when calling the function. For example:
find_coefficients(airfoil="e423.dat", alpha=5, Reynolds=200000, NACA=False)
Hello, I want to use an airfoil that is not a NACA section.
As far as I understand, I need to pass the call() function with airfoil='name of the file'.
However, when I do so I get the following error:
FileNotFoundError: [Errno 2] No such file or directory: 'Polar_''''the name of my file in here''_17114543.382491257_0.0_25.0_3'
Any insight on this would be much appreciated, thanks