AeroPython

2014-04-22T11:53:47Z (GMT) by Lorena A. Barba Olivier Mesnard
<p>Set of lessons in classical Aerodynamics on IPython Notebooks. Lessons start with the fundamental solutions of potential flow and advance to the classical panel methods with source sheets for non-lifting bodies and source-vortex sheets for lifting bodies. These lessons were tested in the classroom at The George Washington University in Spring 2014. </p> <p>The content is shared under CC-BY 4.0 and the code under MIT license.</p>