Introduction

When working with aerodynamic properties such as drag, it’s common practice to normalize these values against some sort of reference area. For most ground vehicles with a pressure dominated drag contribution this ends up being the cross-sectional area as seen from the front (or projected onto the inlet plane). Most of the time, acquiring these values is pretty easy, especially if you’re dealing with some nice clean CAD files. Annoyingly though, sometimes all you have are the non-parametric, triangulated geometry (STL) files. When you find yourself in this situation, there are only a few options (Blender, ParaView, etc..) and they’re all fairly tedious, time…

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