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February 8, 2012, 14:18 |
Error ?
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#1 |
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What does this error mean:
ERROR #001100279 has occurred in subroutine ErrAction. | | Message: | | SYMASS_ZIFCS_EL : The solver ran out of temporary space while bui- | | lding a linked list for a domain interface. Try setting the expe- | | rt parameter "topology estimate factor zif" to a value greater th- | | an 1.0. Values higher than 1.2 should not be necessary. I tried values of 2.0+, but still the same error... Could anyone take a look at my model? Thanks! |
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February 8, 2012, 17:42 |
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#2 |
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Glenn Horrocks
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The error is saying it is having a hard time assembling your interface. I would remesh and try to improve the mesh quality around the interface.
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February 8, 2012, 17:44 |
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#3 |
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Make sure you really did set "topology estimate factor zif" and not a very similar parameter that is in the GUI. I think you have to set "topology estimate factor zif" via CCL.
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February 8, 2012, 19:03 |
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#4 |
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How do I get to CCL?
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February 8, 2012, 19:06 |
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#5 |
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February 8, 2012, 23:24 |
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#6 |
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Ok, I got it to solve without errors. But now my results show no motion even though I have a rotational device inside of a fluid... but nothing moves..
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February 8, 2012, 23:31 |
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#7 |
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Glenn Horrocks
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Is it a steady state or transient run? Have you run it long enough to see motion? Is the rotating bit transient rotor-stator of some other form of motion?
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February 8, 2012, 23:45 |
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#8 |
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I would like it to be transient, although I'm not aware of how to enable that. It is basically a fan inside a tube with open ends and the whole thing is in a domain of fluid (air). I want the fan to distribute the air and test the performance.
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February 9, 2012, 07:22 |
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#9 |
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Glenn Horrocks
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Well of course if the simulation is steady state then nothing is going to move at all. Doesn't that explain the lack of motion?
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February 9, 2012, 07:30 |
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#10 |
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February 9, 2012, 07:35 |
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#11 |
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Glenn Horrocks
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Can you post an image of the results and what you are trying to model?
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February 9, 2012, 12:00 |
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#12 |
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February 9, 2012, 17:09 |
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#13 |
Super Moderator
Glenn Horrocks
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I assume the fan rotates and generates a flow. What is the interface which caused the initial problem? Can you post your CCL?
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February 9, 2012, 19:28 |
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#14 |
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Sorry, how do I get to the CCL?
Is this it? +--------------------------------------------------------------------+ | Mesh Statistics | +--------------------------------------------------------------------+ | Domain Name | Orthog. Angle | Exp. Factor | Aspect Ratio | +----------------------+---------------+--------------+--------------+ | | Minimum [deg] | Maximum | Maximum | +----------------------+---------------+--------------+--------------+ | Domain 1 | 90.0 OK | 1 OK | 1 OK | | Domain 2 | 60.9 OK | 3 OK | 2 OK | | Domain 3 | 38.4 ok | 10 ok | 7 OK | | Global | 38.4 ok | 10 ok | 7 OK | +----------------------+---------------+--------------+--------------+ | | %! %ok %OK | %! %ok %OK | %! %ok %OK | +----------------------+---------------+--------------+--------------+ | Domain 1 | 0 0 100 | 0 0 100 | 0 0 100 | | Domain 2 | 0 0 100 | 0 0 100 | 0 0 100 | | Domain 3 | 0 1 99 | 0 2 98 | 0 0 100 | | Global | 0 <1 100 | 0 <1 100 | 0 0 100 | +----------------------+---------------+--------------+--------------+ Domain Name : Domain 1 Total Number of Nodes = 40560 Total Number of Elements = 36875 Total Number of Hexahedrons = 36875 Total Number of Faces = 7150 Domain Name : Domain 2 Total Number of Nodes = 24990 Total Number of Elements = 20160 Total Number of Prisms = 960 Total Number of Hexahedrons = 19200 Total Number of Faces = 10440 Domain Name : Domain 3 Total Number of Nodes = 6497 Total Number of Elements = 21045 Total Number of Tetrahedrons = 21045 Total Number of Faces = 10864 Global Statistics : Global Number of Nodes = 72047 Global Number of Elements = 78080 Total Number of Tetrahedrons = 21045 Total Number of Prisms = 960 Total Number of Hexahedrons = 56075 Global Number of Faces = 28454 +--------------------------------------------------------------------+ | Reference Pressure Information | +--------------------------------------------------------------------+ Domain Group: Domain 1 Pressure has not been set at any boundary conditions. The pressure will be set to 0.00000E+00 at the following location: Domain : Domain 1 Node : 1 (equation 1) Coordinates : ( 1.16840E-01, 1.16840E-01, 2.83513E-01). +--------------------------------------------------------------------+ | Average Scale Information | +--------------------------------------------------------------------+ Domain Name : Domain 1 Global Length = 3.4007E-01 Minimum Extent = 2.5400E-01 Maximum Extent = 6.0960E-01 Density = 1.1850E+00 Dynamic Viscosity = 1.8310E-05 Velocity = 0.0000E+00 Domain Name : Domain 2 Global Length = 7.9063E-02 Minimum Extent = 1.1172E-01 Maximum Extent = 1.5240E-01 Density = 2.7020E+03 Thermal Conductivity = 2.3700E+02 Specific Heat Capacity at Constant Pressure = 9.0300E+02 Thermal Diffusivity = 9.7135E-05 Average Timescale = 6.4354E+01 Minimum Timescale = 1.2849E+02 Maximum Timescale = 2.3911E+02 Domain Name : Domain 3 Global Length = 2.4039E-02 Minimum Extent = 1.2700E-02 Maximum Extent = 8.9638E-02 Density = 2.7020E+03 Thermal Conductivity = 2.3700E+02 Specific Heat Capacity at Constant Pressure = 9.0300E+02 Thermal Diffusivity = 9.7135E-05 Average Timescale = 5.9494E+00 Minimum Timescale = 1.6605E+00 Maximum Timescale = 8.2720E+01 Subsystem : Momentum and Mass U-Mom-Domain 1 --> U-Mom V-Mom-Domain 1 --> V-Mom W-Mom-Domain 1 --> W-Mom P-Mass-Domain 1 --> P-Mass Subsystem : Heat Transfer - 1 T-Energy-Domain 2 --> T-Energy-Domain 2 Subsystem : Heat Transfer - 2 T-Energy-Domain 3 --> T-Energy-Domain 3 Subsystem : TurbKE and Diss.K K-TurbKE-Domain 1 --> K-TurbKE E-Diss.K-Domain 1 --> E-Diss.K CFD Solver started: Thu Feb 09 17:20:52 2012 | Timescale Information | ---------------------------------------------------------------------- | Equation | Type | Timescale | +----------------------+------------------------+--------------------+ | U-Mom-Domain 1 | Auto Timescale | 2.24540E+03 | | V-Mom-Domain 1 | Auto Timescale | 2.24540E+03 | | W-Mom-Domain 1 | Auto Timescale | 2.24540E+03 | +----------------------+------------------------+--------------------+ | T-Energy-Domain 2 | Auto Timescale | 6.43536E+01 | +----------------------+------------------------+--------------------+ | T-Energy-Domain 3 | Auto Timescale | 5.94942E+00 | +----------------------+------------------------+--------------------+ | K-TurbKE-Domain 1 | Auto Timescale | 2.24540E+03 | | E-Diss.K-Domain 1 | Auto Timescale | 2.24540E+03 | +----------------------+------------------------+--------------------+ ================================================== ==================== OUTER LOOP ITERATION = 1 CPU SECONDS = 1.326E+00 ---------------------------------------------------------------------- | Equation | Rate | RMS Res | Max Res | Linear Solution | +----------------------+------+---------+---------+------------------+ | U-Mom | 0.00 | 0.0E+00 | 0.0E+00 | 0.0E+00 OK| | V-Mom | 0.00 | 0.0E+00 | 0.0E+00 | 0.0E+00 OK| | W-Mom | 0.00 | 0.0E+00 | 0.0E+00 | 0.0E+00 OK| | P-Mass | 0.00 | 0.0E+00 | 0.0E+00 | 8.4 0.0E+00 OK| +----------------------+------+---------+---------+------------------+ | T-Energy-Domain 2 | 0.00 | 1.9E-06 | 9.7E-06 | 5.3 4.9E-03 OK| +----------------------+------+---------+---------+------------------+ | T-Energy-Domain 3 | 0.00 | 1.4E-06 | 6.8E-06 | 6.6 9.7E-03 OK| +----------------------+------+---------+---------+------------------+ | K-TurbKE | 0.00 | 1.8E+00 | 1.9E+00 | 5.1 2.2E-08 OK| | E-Diss.K | 0.00 | 6.3E+00 | 6.5E+00 | 7.5 2.5E-08 OK| +----------------------+------+---------+---------+------------------+ CFD Solver finished: Thu Feb 09 17:20:54 2012 CFD Solver wall clock seconds: 2.0000E+00 +--------------------------------------------------------------------+ | U-Mom-Domain 1 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | V-Mom-Domain 1 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | W-Mom-Domain 1 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | P-Mass-Domain 1 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | T-Energy-Domain 2 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | T-Energy-Domain 3 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Locations of Maximum Residuals | +--------------------------------------------------------------------+ | Equation | Node # | X | Y | Z | +--------------------------------------------------------------------+ | U-Mom-Domain 1 | 0 | 0.000E+00 | 0.000E+00 | 0.000E+00 | | V-Mom-Domain 1 | 0 | 0.000E+00 | 0.000E+00 | 0.000E+00 | | W-Mom-Domain 1 | 0 | 0.000E+00 | 0.000E+00 | 0.000E+00 | | P-Mass-Domain 1 | 0 | 0.000E+00 | 0.000E+00 | 0.000E+00 | | T-Energy-Domain 2 | 15473 |-3.063E-02 | 3.395E-02 |-2.540E-02 | | T-Energy-Domain 3 | 1505 | 6.033E-03 | 2.596E-02 | 8.733E-04 | | K-TurbKE-Domain 1 | 29304 |-9.652E-02 |-1.168E-01 | 2.628E-01 | | E-Diss.K-Domain 1 | 17096 |-5.080E-03 | 4.572E-02 | 1.182E-01 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Peak Values of Residuals | +--------------------------------------------------------------------+ | Equation | Loop # | Peak Residual | Final Residual | +--------------------------------------------------------------------+ | U-Mom-Domain 1 | 0 | 0.00000E+00 | 0.00000E+00 | | V-Mom-Domain 1 | 0 | 0.00000E+00 | 0.00000E+00 | | W-Mom-Domain 1 | 0 | 0.00000E+00 | 0.00000E+00 | | P-Mass-Domain 1 | 0 | 0.00000E+00 | 0.00000E+00 | | T-Energy-Domain 2 | 1 | 1.91960E-06 | 1.91960E-06 | | T-Energy-Domain 3 | 1 | 1.35297E-06 | 1.35297E-06 | | K-TurbKE-Domain 1 | 1 | 1.78790E+00 | 1.78790E+00 | | E-Diss.K-Domain 1 | 1 | 6.34034E+00 | 6.34034E+00 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | False Transient Information | +--------------------------------------------------------------------+ | Equation | Type | Elapsed Pseudo-Time | +--------------------------------------------------------------------+ | U-Mom-Domain 1 | Auto | 2.24540E+03 | | V-Mom-Domain 1 | Auto | 2.24540E+03 | | W-Mom-Domain 1 | Auto | 2.24540E+03 | | T-Energy-Domain 2 | Auto | 6.43536E+01 | | T-Energy-Domain 3 | Auto | 5.94942E+00 | | K-TurbKE-Domain 1 | Auto | 2.24540E+03 | | E-Diss.K-Domain 1 | Auto | 2.24540E+03 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Average Scale Information | +--------------------------------------------------------------------+ Domain Name : Domain 1 Global Length = 3.4007E-01 Minimum Extent = 2.5400E-01 Maximum Extent = 6.0960E-01 Density = 1.1850E+00 Dynamic Viscosity = 1.8310E-05 Velocity = 0.0000E+00 Domain Name : Domain 2 Global Length = 7.9063E-02 Minimum Extent = 1.1172E-01 Maximum Extent = 1.5240E-01 Density = 2.7020E+03 Thermal Conductivity = 2.3700E+02 Specific Heat Capacity at Constant Pressure = 9.0300E+02 Thermal Diffusivity = 9.7135E-05 Average Timescale = 6.4354E+01 Minimum Timescale = 1.2849E+02 Maximum Timescale = 2.3911E+02 Temperature Range = 6.1035E-05 Domain Name : Domain 3 Global Length = 2.4039E-02 Minimum Extent = 1.2700E-02 Maximum Extent = 8.9638E-02 Density = 2.7020E+03 Thermal Conductivity = 2.3700E+02 Specific Heat Capacity at Constant Pressure = 9.0300E+02 Thermal Diffusivity = 9.7135E-05 Average Timescale = 5.9494E+00 Minimum Timescale = 1.6605E+00 Maximum Timescale = 8.2720E+01 Temperature Range = 6.1035E-05 +--------------------------------------------------------------------+ | Variable Range Information | +--------------------------------------------------------------------+ Domain Name : Domain 1 +--------------------------------------------------------------------+ | Variable Name | min | max | +--------------------------------------------------------------------+ | Density | 1.18E+00 | 1.18E+00 | | Specific Heat Capacity at Constant Pressure| 1.00E+03 | 1.00E+03 | | Dynamic Viscosity | 1.83E-05 | 1.83E-05 | | Thermal Conductivity | 2.61E-02 | 2.61E-02 | | Static Entropy | 0.00E+00 | 0.00E+00 | | Velocity u | 0.00E+00 | 0.00E+00 | | Velocity v | 0.00E+00 | 0.00E+00 | | Velocity w | 0.00E+00 | 0.00E+00 | | Pressure | 0.00E+00 | 0.00E+00 | | Turbulence Kinetic Energy | 4.77E-07 | 1.99E-01 | | Turbulence Eddy Dissipation | 6.10E-05 | 1.40E+01 | | Eddy Viscosity | 2.65E-10 | 3.05E-04 | | Temperature | 2.98E+02 | 2.98E+02 | +--------------------------------------------------------------------+ Domain Name : Domain 2 +--------------------------------------------------------------------+ | Variable Name | min | max | +--------------------------------------------------------------------+ | Density | 2.70E+03 | 2.70E+03 | | Specific Heat Capacity at Constant Pressure| 9.03E+02 | 9.03E+02 | | Thermal Conductivity | 2.37E+02 | 2.37E+02 | | Static Entropy | 0.00E+00 | 0.00E+00 | | Temperature | 2.98E+02 | 2.98E+02 | | Static Enthalpy | -3.12E-02 | 3.12E-02 | +--------------------------------------------------------------------+ Domain Name : Domain 3 +--------------------------------------------------------------------+ | Variable Name | min | max | +--------------------------------------------------------------------+ | Density | 2.70E+03 | 2.70E+03 | | Specific Heat Capacity at Constant Pressure| 9.03E+02 | 9.03E+02 | | Thermal Conductivity | 2.37E+02 | 2.37E+02 | | Static Entropy | 0.00E+00 | 0.00E+00 | | Temperature | 2.98E+02 | 2.98E+02 | | Static Enthalpy | -3.12E-02 | 3.12E-02 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | CPU Requirements of Numerical Solution | +--------------------------------------------------------------------+ Subsystem Name Discretization Linear Solution (secs. %total) (secs. %total) ---------------------------------------------------------------------- Momentum and Mass 1.01E+00 23.9 % 3.12E-01 7.4 % Heat Transfer - 1 7.80E-02 1.8 % 3.12E-02 0.7 % Heat Transfer - 2 6.24E-02 1.5 % 1.56E-02 0.4 % TurbKE and Diss.K 2.34E-01 5.5 % 1.09E-01 2.6 % -------- ------- -------- ------ Subsystem Summary 1.39E+00 32.7 % 4.68E-01 11.0 % Variable Updates 2.81E-01 6.6 % File Reading 1.56E-02 0.4 % File Writing 2.34E-01 5.5 % Miscellaneous 1.86E+00 43.8 % -------- Total 4.24E+00 +--------------------------------------------------------------------+ | Job Information | +--------------------------------------------------------------------+ End of solution stage. |
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February 9, 2012, 19:39 |
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#15 |
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February 9, 2012, 20:53 |
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#16 |
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Glenn Horrocks
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No, the CCL is the stuff in the first section of the output file - the bit you chopped off.
But I can see you have three domains and do not appear to have any interfaces to connect them. Also your fluid domain does not have a temperature/heat equation so cannot be linked to your solid domains. Looks like you have made some pretty basic setup errors with this simulation. I recommend you do the tutorials on conjugate heat transfer, that is ones with solid and fluid bodies coupled together. |
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February 10, 2012, 01:07 |
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#17 |
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Thanks!
I actually did the Ch 17 Tutorial: Multiphase Flow in a Mixing Vessel... It was helpful, but actually confused me quite a bit. Do you have to model fluid around the propeller and fluid inside the tank separately? That part confused me... How many components do I need to solve my problem? Just the fan, tube, and fluid... so 3 parts? |
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February 10, 2012, 01:12 |
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#18 |
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Glenn Horrocks
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Do some of the rotating machinery tutorials to see how you model rotating devices.
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February 10, 2012, 01:41 |
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#19 |
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I think I have it now -- BTW Ch 17 is turbomachinery tutorial
Last edited by Orb; February 10, 2012 at 05:50. |
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February 12, 2012, 21:36 |
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#20 |
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How do you create a subregion within your meshes? It looks like that's the problem I'm running into.
Last edited by Orb; February 12, 2012 at 22:55. |
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