Hi @LWhitson2, I cant comment much on the accuracy of the other projects, unhelpfully, the force coefficients were not added so it makes it more time consuming to check
however, I think I might be able to help a bit with your own project and I agree, if we could have a more comprehensive validation project that would be amazing.
Firstly, when I looked at your project, the only simulation setup for me to look at was the first one. When we look at drag, the boundary layer plays a large part, so ensuring that boundary layer modelling is correct is very important. Therefore, I looked at your mesh to see your layer setting and couldnât see a layer inflation refinement present, so that would be a good start.
Another point is supported by a validation project I did on the NACA 0012 aerofoil, where I original had high drag, and therefore, the steps I took to get good results I ensured I documented it well, the write up is here:
Particularly about the divergence scheme for velocity and the y+.
Best,
Darren