This simulation was done using variable order unstructured triangles. Igor Lomtev is currently writing the 3D version of this code for tetrahedra using the Local Discontinuous Galerkin Method. When I have figured this scheme out I will be using it for the polyhedra and for Maxwell's Equations.
This simulation was done using unstructured prisms and hexahedra. It was run by Mike Kirby. It is a simulation of flow past a NACA0012 airfoil with endplates. The flow is at an angle of attack of 10 degrees to the airfoil. Contours of streamwise momentum are shown.