This is a bunch of bash scripts and Python scripts that is used to automate the testing of a bunch of airfoils by running XFoil.

XFoil is a program written by Professor Mark Drela of MIT. It is a low-order model that can be used to make effective predictions of airfoils at low Reynold’s Numbers.

This project can be used to select airfoils for preliminary aircraft design. Python with its extensive libraries like Numpy and Matplotlib is then used for some data visualization capabilities and data analysis of “choosing” which airfoil we would like.

Documentation would be written for this as well.