I am doing a Non-Compressible CFD on one of my FSAE projects with rear wing. I am facing problems with unstable Omega and K values. Apart from that, I am also facing problems in convergence of pressure.
I am guessing the problem is at inlet as the values over there are not completely stable. I am further trying with enlarged cartesian box I used for refinement around car because the front face was really close to the nosecone which might have created this error but I am not sure.
I tried with your suggested settings and I got a fair convergence. Just a question, what happens on reducing the absolute tolerance of the said factors? Do they seize to take into account that specified change or something else?
Also, I am again having same issues but with standard mesh this time.
Please check ‘16 4 21 e423 e423 s1223 v2’ with sim run named ‘50 kmph new’
As you can see, the residuals plot is of course not converging. So what would you suggest here? I am already at 8M big mesh so I don’t think finesse should be added to it and the quality of the mesh is pretty good also.