Euler solution, NACA0012, Mach = 0.4, AoA = 8

Here's a video from a test of a solver I'm working on. Currently it is inviscid (euler), explicit, and steady. I thought the developing flowfield looked pretty cool. This video represents 100,000 steps. Next step will be to make it implicit so much bigger time steps can be used. The CFL number here was 0.3. After that, I will add viscous fluxes, turbulence models, etc.