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Question about heat transfer simulation convergence |
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May 22, 2013, 06:55 |
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#21 |
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Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
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May 22, 2013, 07:07 |
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#22 |
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Ben B. Huang
Join Date: Oct 2012
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Thanks for your reply
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November 13, 2017, 05:33 |
Transient heat transfer simulation - convergence
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#23 | |
Member
VB
Join Date: Jul 2016
Posts: 35
Rep Power: 10 |
Quote:
The global imblances are with in 1% . I checked the yplus value near the fluid and solid interface and it is 30+ for 70% of the area and 80+ for 30% of the area. I use SST model. What can be the reason for this residual graph shoot up after 350 iterations? |
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November 13, 2017, 08:15 |
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#24 |
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Mr CFD
Join Date: Jun 2012
Location: Britain
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Without knowing what you're simulating it's hard to give a proper answer.
It could be due to a poor mesh, poor choice of model, both, or something else completely. To me it might look like the simulation is resolving some evolving flow physics (maybe vorticies which grow as a function of time?). Start a new thread and give a detailed description of what you're doing. Also I'm sure Ghorrocks will be around to tell you to read the FAQ - so do that too. |
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November 13, 2017, 18:12 |
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#25 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,870
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Sadly, I don't think an FAQ covers this one
I agree with Mr CFD's comments: First check for numerical problems (mesh, models), and if they look OK check for transient flow starting up, such as vortex shedding or gross flow instabilities. |
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November 14, 2017, 05:35 |
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#26 | |
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VB
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Quote:
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November 14, 2017, 05:37 |
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#27 |
Member
VB
Join Date: Jul 2016
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okay,Ghorrocks. I ll try to create new thread with more details on this regard.
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January 13, 2021, 15:43 |
Convergence Issues-CHT for Turbomachinery
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#28 |
New Member
Join Date: May 2020
Posts: 21
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Hello! Thank you all for this useful thread, it helps a lot in CHT related topics.
I am trying to simulate a multistage axial turbine throw CFX to account later for the temperature field on turbine blades by thermal analysis. To succeed more acqurate results i implemented in my model Conjugate Heat Transfer with a loose couple (different mesh between fluid region (TurboGrid) and solid region (Ansys Meshing) through CFX. When i applied CFX to only the second rotor stage (to check if it works fine with my settings (interfaces etc.)) it results with good convergence both from residuals side and global imbalance as well. However, when i tried to add mesh for another stage then RMS-T Energy for the previous stage is diverging like in the attached image. Timescale for fluid domain is set as 1/omega through an expression (as suggested by CFX-manual) I used different Timescales for the solid domains like 1000, 100, 10 and 1s but it tends to give similar results in all cases. I would be grateful if you could make me aware of what is the possible cause of that. Again, Thank you! Residuals' Plots: https://ibb.co/Btk2PMn https://ibb.co/zh2sPQy https://ibb.co/PjrqPpY |
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