Closed J-Massey closed 5 years ago
Hello Jonahah. Can you try copying the xfoil.exe to your working directory and see if it works? Please let me know if it does as I will add that to the project description.
YES!! That works thank you very much that was silly!
Glad it worked! Hope you find this library quite useful
All i get when i try the example :
find_coefficients(airfoil='naca0012'alpha=12.)
is an output error statingCould you please help me? Here is a picture:![image](https://user-images.githubusercontent.com/44616393/47743155-4a8ff480-dc76-11e8-9e6a-d2b7dbe3773d.png)