Outlet Boundary Condition
I simulate an air jet with CFX 5.5. Assumptions: - axisymmetric
- subsonic everywhere
- Inlet: total pressure and static Temperature
- Outlet: static pressure (atmospheric pressure)
After convergence (res_max < 1.0e-3), i notice that the oulet boundary condition is not respected. What can I do to impose this static pressure outlet ?
Thanks for your help. Francisca.
Re: Outlet Boundary Condition
Tighten up your convergence, 1e-3 MAX is very loose. Try 1e-4 or 1e-5.
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