Automatic wing structure generator with NACA profiles in CATIA using Python scripts (PyCATIA)

Python script that permits to generate a simple wing structure using a NACA profile calculator. The user can input the desired wing parameters (i.e. span, winglet dimensions, NACA airfoil shape digits, number of ribs, sweep angle...) and the final output is the final solid wing structure with the winglet and skin surfaces. I leave here the link to my course where you will learn how to do this and much more! https://www.udemy.com/course/pycatia-module/?referralCode=2DD1EED7C21165084D3A