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Smile Fluent- increasing in the back pressure leading to divergence |
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March 11, 2020, 05:39
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Smile Fluent- increasing in the back pressure leading to divergence
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New Member
RaviTeja Gonnabathula
Join Date: Oct 2019
Posts: 10
Rep Power: 8  |
Dear CFD buddies,
I'm simulating a supersonic inlet by increasing the back pressure ratio. Till the the back pressure ratio of 4 at the interval of 1 I was able to generate results. When I'm simulating for back pressure ratio of 5 I couldn't solve and AMG solver is being detected. Tried refining the mesh- didn't worked Settings: altitude:30km (corresponding P, T values) Mach :2.18 Desnity based solver Spalart–Allmaras turbulence model Explicit solver courant number -0.5 Hope I could find the solution. All suggestions are accepted |
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| divergence amg solver, fluent |
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