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Simulation fails after adding multi-component gas |
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January 18, 2017, 09:26 |
Simulation fails after adding multi-component gas
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#1 |
New Member
Conor Hardiman
Join Date: Jan 2017
Posts: 2
Rep Power: 0 |
Hi all,
I have an exhaust manifold that I am undertaking flow analysis on. when using a single gas model, the simulation runs without fault. However, when I change to a multicomponent gas model, the following error message appears: Error for Segregated Flow: Bi-Conjugate Gradient Stabilized solver did not converge ! Reversed flow on 378 faces on xxxxxxxxxxxxxxxx Error: AMG solver diverged. Error: AMG solver diverged. Error: AMG solver diverged. Error: AMG solver diverged. Error: AMG solver diverged. Error: AMG solver diverged. A floating point exception has occurred: floating point exception [Divide by zero]. The specific cause cannot be identified. Please refer to the troubleshooting section of the User's Guide. Context: star.segregatedflow.SegregatedFlowSolver Command: RunSimulation error: Server Error I have tried refining the mesh, changing from a polyhedral to a tetrahedral, segregated flow and coupled flow with both meshers. Coupled Flow: Coupled Energy, Coupled Flow, Coupled Species, Exact Wall Distance, Gradients, Ideal Gas, K-Epsilon Turbulence, Multi-Component Gas, Non-reacting, Realizable K-Epsilon Two-Layer, Reynolds-Averaged Navier-Stokes, Steady, Three Dimensional, Turbulent, Two-Layer All y+ Wall Treatment Segregated Flow: Exact Wall Distance, Gradients, Ideal Gas, K-Epsilon Turbulence, Multi-Component Gas, Non-reacting, Realizable K-Epsilon Two-Layer, Reynolds-Averaged Navier-Stokes, Segregated Flow, Segregated Fluid Isothermal, Segregated Species, Steady, Three Dimensional, Turbulent, Two-Layer All y+ Wall Treatment Thanks |
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January 20, 2017, 02:29 |
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#2 |
Senior Member
Join Date: Nov 2010
Location: USA
Posts: 1,232
Rep Power: 25 |
Your case is diverging. Did you have a lot of reversed flow on the single gas model?
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January 20, 2017, 06:48 |
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#3 |
New Member
Conor Hardiman
Join Date: Jan 2017
Posts: 2
Rep Power: 0 |
Early iteration did have a lot of reversed flow but after 200 iterations there was no reversed flow.
Do you propose I change the turbulence model? Thanks for the reply |
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January 20, 2017, 10:50 |
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#4 |
Senior Member
Join Date: Nov 2010
Location: USA
Posts: 1,232
Rep Power: 25 |
No, I would say you should fix your initial conditions to remove so much reversed flow at the start.
Your BCs do different things when reversed flow occurs, which is probably why your mutli-component one explodes. You could converge the single-component one and then just switch to mutli-component. |
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Tags |
exhaust gas, exhaust manifold, star ccm+ |
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