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June 25, 2020, 16:58 |
Convergence problem
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#1 |
New Member
Felipe Silva Maffei
Join Date: Dec 2015
Posts: 12
Rep Power: 10 |
Hello everyone!
It is the second time that I have posted something on this forum, so, if I doing anything wrong, sorry. That said, lets to my question: I am trying to simulate an incompressible jet pump. The boundary conditions was setup as normal velocity equal 1 m/s at secondary and primary inlets. At the outlet, it was used the outlet-pressure with reference pressure equal to zero and the wall with no slip conditions. The turbulence model used was the RNG k-epsilon. The mesh was built in the ICEM CFD using the structured type (finer elements was positioned near the walls). I am using the SIMPLE solver with: Gradient -> Green Gauss node based Pressure -> Linear Momentum, and tubulenty properties -> First order URF -> fluent standard I already try a lot of configuration, but I cannot avoid the behavior that is shown in the figure 1, thus, the residuals do not decrease. Way is it happen? Fig1 -> Velocity field with the error highlighted with red line Fig2 -> Mesh detail 1 at this region Fig3 -> Mesh detail 2 at the region |
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June 26, 2020, 09:32 |
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#2 |
Senior Member
André
Join Date: Mar 2016
Posts: 133
Rep Power: 10 |
what are the residuals showing?
Is that first plot velocity or residuals? looks like velocity to me...
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convergence failure |
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