[DavidB]

Hi!

I simulating a transonic wing with airplane body and air inlet behind the wing . I use pressure far filed, pressure outlet for the limits of the domains and a pressure outlet with target mass flow rate for the inlet. Density based with Rke.

If i achieve the convergence starting from the first order and at the end the second order I obtain ad solution that's different from the ones that i achieve starting the solution from a lower incidence solution with the second order active from the start.

Anyone has the same problem (in terms of discrepancies of the solution)?