A set of scripts for undergraduate-level aerospace engineering class work.

The compressible flow scripts are inspired by the Compressible Aerodynamics Calculator and my interest in having something similar available on a TI-84 Plus CE-T Python Edition calculator.

The max-q.py script is a modified version of the script from chapter 3 of Python for Aerospace and Mechanical Engineering by Alex Kenan which includes a pitch maneuver and acceleration calculations based on drag and vehicle mass as a function of time.