I am currently working to design a wing. I basically want the Python code which would take the coordinates of the airfoil (.dat file), freestream velocity, Span (b), planform of the wing as input, and give all the characteristics of the wing-like Variation of lift and lift coefficient, drag, etc along the span and variation with angle of attack.
I don't think this is the kind of question I can ask here. But, if it isn't, then pls tell me where to post this query. If you feel like you can help, pls do.
I have googled but the sources were too messy and didn't have a good presentation of the code.