Hello everyone,
I have a confusing question about residual convergence. When I use the first-order NS equation to calculate, the residual can reach 0.01. However, when I increase the order to 2nd and 3rd, the residual can only converge to around 30. It is worth noting that I am calculating the laminar boundary layer, so the residual should be very small.
Is it possible that the high order residual is caused by insufficient mesh refinement? Is there anything special about laminar flow calculation?
Also, I once saw on a forum that compared to turbulent walls, there seems to be a need for particularly fine grids near laminar walls. Why is this?
By the way, is the residual an absolute error or a relative error compared to the previous step?
Thank you for your help!
Best regards.