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Overview

This project was elaborated because of the need of optimizing an airfoil according to its aerodynamic and structural performance (conference paper). Therefore I needed a quick and easy way to find the aerodynamic pressure and the drag and lift coefficients. I

I list other developers who create similar tools, but I felt that their code was not straightforward enough:

• https://github.com/convexopt/pyxfoil
• https://github.com/diarmuidw/python-airfoil

Contrary to the other two developers, I did not use classes or create a GUI. This library is intended to be used in Python codes for optimizations or any other process that requires several aerodynamic analysis.