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November 6, 2022, 03:31 |
Compressible Flow, Temperature Problem
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#1 |
New Member
Tim
Join Date: Feb 2021
Posts: 3
Rep Power: 5 |
Hi everyone,
I am simulating a gas turbine stator passage and I have some Problems with the convergence. I set a Monitor Points behind my Blade near to the Shroud for Pressure and Temperature. While the Monitor Point for Pressure is not changing, the Monitor Points for Temperatur is Oscillating. The RMS Residuals are between 10^-4 and 10^-5. The flow is compressible, so that I am using the Total Energy Modell with Air Ideal Gas. At the Inlet I set a Total Pressure and at the Outlet a Static Pressure. Does anyone habe any suggestions? Tim |
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November 6, 2022, 06:43 |
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#2 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,871
Rep Power: 144 |
My suggestion is read the FAQ on this: https://www.cfd-online.com/Wiki/Ansy...gence_criteria
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Note: I do not answer CFD questions by PM. CFD questions should be posted on the forum. |
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November 9, 2022, 12:55 |
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#3 |
Senior Member
Join Date: Jun 2009
Posts: 1,880
Rep Power: 33 |
Would you mind posting plots for the convergence of MassMomentun and Heat Transfer?
You can also create an additional plot for the Imbalances showing for P-Mass, H-Energy and U/V/W-Mom
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