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June 5, 2002, 05:06 |
Outlet Boundary Condition
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#1 |
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Hi,
I simulate an air jet with CFX 5.5. Assumptions: - axisymmetric - compressible - 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. |
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June 5, 2002, 16:31 |
Re: Outlet Boundary Condition
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#2 |
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Tighten up your convergence, 1e-3 MAX is very loose. Try 1e-4 or 1e-5.
Robin |
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