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March 29, 2010, 03:05 |
Refiner Error 255
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#1 |
New Member
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Hello All,
I try to model CH4 combustion and I'd like to make mesh adaption in the reaction region. Hence, I set up CH4.Mass Fraction as adaption criteria in CFX12 Pre. Mesh Adaption was started every 10 iterations. While solver was running, Refiner has started and terminated with the message: "An error has occurred in cfx5solve: The ANSYS CFX mesh refiner could not be started, or exited with return code 255:" Before that one I've recived a windows send report message about refiner. What does code 255 means? When it usually appears? Regards, A.m. |
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March 31, 2010, 11:23 |
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#2 |
New Member
zhao xin
Join Date: Feb 2010
Location: Goteborg
Posts: 28
Rep Power: 16 |
what i can tell you is, last time I encountered this error code is because of large aspect ratio which exceeded the limit.
Hope this would help.. |
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April 1, 2010, 03:54 |
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#3 |
New Member
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Thanks zxin,
I've solved this problem by mesh changing. First time I used ANSYS Meshing to generate mesh. I checked its quality in ICEM CFD and received following results: min = 0.013, max = 23.05, mean = 1.87 (aspect ratio). Then I generated ICEM CFD mesh and checked it. I received following: min = 0.25, max = 0.99, mean = 0.75 (aspect ratio). Also I decreased a numer of elements by a factor of 1.8 and removed prism layers (inflantion). With the new mesh remesher works perfectly. P.S. old mesh new mesh |
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April 1, 2010, 04:51 |
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#4 |
New Member
zhao xin
Join Date: Feb 2010
Location: Goteborg
Posts: 28
Rep Power: 16 |
That's great...
but sometimes, my mesh with aspect ratio close to 1000 generated by Ansys Mesh, works fine with CFX, CFX is quite stable solver, i think... |
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April 1, 2010, 07:32 |
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#5 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,870
Rep Power: 144 |
But with no prism layers your boundary layer modelling will be hopeless. You clearly have a mesh quality problem, but you need to generate a high quality mesh with prism layers.
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April 1, 2010, 09:25 |
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#6 |
New Member
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I' m modeling the CH4 combustion process, therefore finer stoichiometric region is more important for me then boundary layer.
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April 2, 2010, 07:07 |
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#7 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,870
Rep Power: 144 |
Isn't the heat transfer important? Won't that set the heat lost to the walls, and be a major contributor to combustion temperature? You will need a good prism layer mesh to resolve that.
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April 2, 2010, 09:04 |
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#8 |
New Member
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Thanks ghorrocks,
Sure it is very important too and I'm working on it By the way, how many prism layers I need to resolve the wall heat transfer? |
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April 3, 2010, 07:31 |
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#9 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,870
Rep Power: 144 |
That's problem dependent. The discussion in the CFX documentation on near-wall modelling is a good starting point, but you then need to do a sensitivity study to find out what your specific case requires.
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April 4, 2010, 04:57 |
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#10 |
New Member
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Thanks a lot!
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August 3, 2010, 21:38 |
Error Code 255
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#11 |
New Member
Maritime Systems Engineering
Join Date: Jul 2010
Posts: 13
Rep Power: 16 |
I do not know what Error code 255 means. Im not an expert at Ansys or CFD. But I do know that it has been solved, every single time, by deleting my mesh and remeshing with new settings. I am not saying you should do this. If you are truly desperate you may give it a try.
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August 8, 2010, 05:22 |
Error 255
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#12 |
Senior Member
Ugly Kid Joe
Join Date: Aug 2010
Posts: 193
Rep Power: 16 |
What kind of meshing is advisable to solve the ERROR code 255 ???
I am using ICEM CFD to mesh my geometry. Am ugetting the following error "The ANSYS CFX solver could not be started, or exited with return | | code 255: . No results file has been created." Now am using the following: Mesh type on surface: All Tri Mesh type in volume: Tetra/Mixed surface Mesh method: Patch Independent volume Mesh method: Robust (octree) Thank you very much |
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