Hi, I am doing a CFD simulation of a F1 rear wing design I’ve quickly knocked up in NX. With this kind of simulation I’ve read it is very important to make sure your mesh accurately captures the boundary layer, especially when dealing with large pressure gradients and wanting to check for/where flow seperation occurs. Since I’m using SST turbulence model, I know I want to be aiming for y+ value of around 1. And from other reading, ideally I would want at least 25-30 prism layers, however, max S
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