Different strategy of convergence, different solution
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)? |
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