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.
Not sure if still relevant, but you are probably reading an output file in the wrong directory. If you send me your code, I can probably find the problem.
I am trying to use the function find_coefficients to find lift and drag coefficients at various attack angles.
Despite entering different foil profiles and angles as input the same output is returned (the only chnage being the input values)
I can get the desired output from xfoil directly but I would much prefer to use your library as it is much faster and more convenient to use.
Any advice on how to get this running would be much appreciated.
Thanks!