Well said Joe. When I retired 6 years ago I was running CFD using Fluent. Tim talks about importing the 3D CAD file, but does not mention how the CFD code sets up the grid. The grid can be set up with hexagons, bricks, etc. and is fine towards the boundary to capture the BL and gets coarse further away. When we ran Fluent, we set up the grid ourselves using Fluent or some other code. Just setting up the grid can be an art in itself. In general for setting up a problem if the vehicle is moving parallel to the flow, one may be able to find planes of symmetry to reduce the size of the 3-D problem. If the problem is truly axi-symmetric, then the problem can be run 2-D axi-symmetric. It is interesting to note that Tim said that he could take his model and put in an angle of attack. This immediately makes the problem into 3-D, which means that the code is definitely handling a 3-D problem, which is impressive both for gridding and CFD computation.
In all likelihood our model rocket flow problems are turbulent, although, technically there will be a short transition from laminar to turbulent flow at the front of the problem. Tim does not mention which turbulent model is used nor if the user in the trial version has a choice. There are at least a half-dozen popular turbulent models out there and probably many dozen altogether (heck, I even have a turbulent model that I have worked on for 40 years). The trial CFD version may not be telling what it is doing for turbulence modelling as well what it is doing for the gridding. (One could argue should we include the rocket exhaust in the model, but we are getting carried away.)
I am a TARC mentor, but I don't feel I have time to look into this, but it would be fun.