Hi,

I just wanted to say thank you for the AeroPython Lesson 6 assignment on conformal mapping. I recently created a small project using your procedure to compute lift over an airfoil and referenced your work. I’ve also added a GUI and implemented an inverse optimization procedure to obtain the circle parameters given an airfoil.

Here’s the repo if you’re interested: https://github.com/kaanatak/airfoil-conformal-mapping

Best regards,
Kaan