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An error occurs.'Increase the file catalog size. ' |
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April 8, 2022, 04:39 |
An error occurs.'Increase the file catalog size. '
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#1 |
New Member
Junyeol
Join Date: Mar 2022
Posts: 18
Rep Power: 4 |
dear all, I got the following error message: 'Increase the file catalog size. '
The analysis worked fine in the steady state setting, but after changing the setting to transient, the above error occurs. I've tried the following solutions: 1. Increase Catalog Size in solver tab (1.2x~6.0x) 2. Increase mesh size, increase mesh quality 3. Increase Memory Alloc Factor in Interpolatpr memory tab But I keep getting the same errors. I'm attaching an Outfile to see if it's a Boundary condition problem. There are many rigid walls, which are curved surfaces. This run of the CFX 2022 R1 Solver started at 16:12:20 on 08 Apr 2022 by user PMC on (intel_xeon64.sse2_winnt) using the command: "C:\Program Files\ANSYS Inc\v221\CFX\bin\perllib\cfx5solve.pl" -batch -ccl runInput.ccl -fullname "Fluid Flow CFX_003" 2022 R1 Point Releases and Patches installed: ANSYS, Inc. License Manager 2022 R1 CFD-Post only 2022 R1 SpaceClaim 2022 R1 CFX (includes CFD-Post) 2022 R1 Chemkin 2022 R1 EnSight 2022 R1 FENSAP-ICE 2022 R1 Fluent (includes CFD-Post) 2022 R1 Polyflow (includes CFD-Post) 2022 R1 Forte (includes EnSight) 2022 R1 TurboGrid 2022 R1 Remote Solve Manager Standalone Services 2022 R1 Viewer 2022 R1 ACIS Geometry Interface 2022 R1 AutoCAD Geometry Interface 2022 R1 Catia, Version 4 Geometry Interface 2022 R1 Catia, Version 5 Geometry Interface 2022 R1 Catia, Version 6 Geometry Interface 2022 R1 Creo Elements/Direct Modeling Geometry Interface 2022 R1 Creo Parametric Geometry Interface 2022 R1 Inventor Geometry Interface 2022 R1 JTOpen Geometry Interface 2022 R1 NX Geometry Interface 2022 R1 Parasolid Geometry Interface 2022 R1 Solid Edge Geometry Interface 2022 R1 SOLIDWORKS Geometry Interface 2022 R1 Setting up CFX Solver run ... +--------------------------------------------------------------------+ | | | CFX Command Language for Run | | | +--------------------------------------------------------------------+ LIBRARY: MATERIAL: Water Material Description = Water (liquid) Material Group = Water Data, Constant Property Liquids Option = Pure Substance Thermodynamic State = Liquid PROPERTIES: Option = General Material EQUATION OF STATE: Density = 997.0 [kg m^-3] Molar Mass = 18.02 [kg kmol^-1] Option = Value END SPECIFIC HEAT CAPACITY: Option = Value Specific Heat Capacity = 4181.7 [J kg^-1 K^-1] Specific Heat Type = Constant Pressure END REFERENCE STATE: Option = Specified Point Reference Pressure = 1 [atm] Reference Specific Enthalpy = 0.0 [J/kg] Reference Specific Entropy = 0.0 [J/kg/K] Reference Temperature = 25 [C] END DYNAMIC VISCOSITY: Dynamic Viscosity = 8.899E-4 [kg m^-1 s^-1] Option = Value END THERMAL CONDUCTIVITY: Option = Value Thermal Conductivity = 0.6069 [W m^-1 K^-1] END ABSORPTION COEFFICIENT: Absorption Coefficient = 1.0 [m^-1] Option = Value END SCATTERING COEFFICIENT: Option = Value Scattering Coefficient = 0.0 [m^-1] END REFRACTIVE INDEX: Option = Value Refractive Index = 1.0 [m m^-1] END THERMAL EXPANSIVITY: Option = Value Thermal Expansivity = 2.57E-04 [K^-1] END END END END FLOW: Flow Analysis 1 SOLUTION UNITS: Angle Units = [rad] Length Units = [m] Mass Units = [kg] Solid Angle Units = [sr] Temperature Units = [K] Time Units = [s] END ANALYSIS TYPE: Option = Transient EXTERNAL SOLVER COUPLING: Option = None END INITIAL TIME: Option = Automatic END TIME DURATION: Option = Total Time Total Time = 6 [s] END TIME STEPS: Option = Timesteps Timesteps = 0.0125 [s] END END DOMAIN: Default Domain Coord Frame = Coord 0 Domain Type = Fluid Location = B347968 BOUNDARY: Default Domain Default Boundary Type = WALL Location = \(too many walls) BOUNDARY CONDITIONS: MASS AND MOMENTUM: Option = No Slip Wall END WALL ROUGHNESS: Option = Smooth Wall END END END BOUNDARY: Inlet Boundary Type = INLET Location = F317474.347968,F317338.347968 BOUNDARY CONDITIONS: FLOW DIRECTION: Option = Normal to Boundary Condition END FLOW REGIME: Option = Subsonic END MASS AND MOMENTUM: Option = Total Pressure Relative Pressure = 3 [mm Hg] END TURBULENCE: Option = Medium Intensity and Eddy Viscosity Ratio END END END BOUNDARY: Inner Boundary Type = OUTLET Location = F317473.347968 BOUNDARY CONDITIONS: FLOW REGIME: Option = Subsonic END MASS AND MOMENTUM: Mass Flow Rate = 0.05 [kg s^-1] Mass Flow Rate Area = As Specified Option = Mass Flow Rate END END END BOUNDARY: Outer Boundary Type = INLET Location = F317472.347968 BOUNDARY CONDITIONS: FLOW DIRECTION: Option = Normal to Boundary Condition END FLOW REGIME: Option = Subsonic END MASS AND MOMENTUM: Mass Flow Rate = 0.05 [kg s^-1] Mass Flow Rate Area = As Specified Option = Mass Flow Rate END TURBULENCE: Option = Medium Intensity and Eddy Viscosity Ratio END END END BOUNDARY: Outlet Boundary Type = OUTLET Location = F317255.347968 BOUNDARY CONDITIONS: FLOW REGIME: Option = Subsonic END MASS AND MOMENTUM: Option = Static Pressure Relative Pressure = 0 [mm Hg] END END END DOMAIN MODELS: BUOYANCY MODEL: Option = Non Buoyant END DOMAIN MOTION: Option = Stationary END MESH DEFORMATION: Option = None END REFERENCE PRESSURE: Reference Pressure = 1 [atm] END END FLUID DEFINITION: Fluid 1 Material = Water Option = Material Library MORPHOLOGY: Option = Continuous Fluid END END FLUID MODELS: COMBUSTION MODEL: Option = None END HEAT TRANSFER MODEL: Fluid Temperature = 25 [C] Option = Isothermal END THERMAL RADIATION MODEL: Option = None END TURBULENCE MODEL: Option = k epsilon END TURBULENT WALL FUNCTIONS: Option = Scalable END END END OUTPUT CONTROL: RESULTS: File Compression Level = Default Option = Standard END END SOLVER CONTROL: Turbulence Numerics = First Order ADVECTION SCHEME: Option = High Resolution END CONVERGENCE CONTROL: Maximum Number of Coefficient Loops = 10 Minimum Number of Coefficient Loops = 1 Timescale Control = Coefficient Loops END CONVERGENCE CRITERIA: Residual Target = 1.E-4 Residual Type = RMS END INTERRUPT CONTROL: Option = Any Interrupt CONVERGENCE CONDITIONS: Option = Default Conditions END END TRANSIENT SCHEME: Option = Second Order Backward Euler TIMESTEP INITIALISATION: Option = Automatic END END END END COMMAND FILE: Version = 22.1 Results Version = 22.1 END SIMULATION CONTROL: EXECUTION CONTROL: EXECUTABLE SELECTION: Double Precision = No Large Problem = No END INTERPOLATOR STEP CONTROL: Runtime Priority = Standard MEMORY CONTROL: Memory Allocation Factor = 1.0 END END PARALLEL HOST LIBRARY: HOST DEFINITION: desktopr4lieb7 Remote Host Name = DESKTOP-R4LIEB7 Host Architecture String = winnt-amd64 Installation Root = C:\Program Files\ANSYS Inc\v%v\CFX END END PARTITIONER STEP CONTROL: Multidomain Option = Automatic Runtime Priority = Standard MEMORY CONTROL: Memory Allocation Factor = 1.0 END PARTITION SMOOTHING: Maximum Partition Smoothing Sweeps = 100 Option = Smooth END PARTITIONING TYPE: MeTiS Type = k-way Option = MeTiS Partition Size Rule = Automatic END END RUN DEFINITION: Run Mode = Full Solver Input File = Fluid Flow CFX.def Solver Results File = \ D:/ \ CFX_Solution/Fluid Flow CFX_003.res INITIAL VALUES SPECIFICATION: INITIAL VALUES CONTROL: Use Mesh From = Solver Input File Continue History From = Workbench Initial Values END INITIAL VALUES: Workbench Initial Values Option = Results File File Name = Fluid Flow CFX_001.res END END END SOLVER STEP CONTROL: Runtime Priority = Standard MEMORY CONTROL: Catalogue Size Override = 2.5x Memory Allocation Factor = 1 END PARALLEL ENVIRONMENT: Number of Processes = 1 Start Method = Serial END END END END +--------------------------------------------------------------------+ | | | Interpolation of Initial Values | | | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | | | ANSYS(R) CFX(R) Interpolator | | | | 2022 R1 | | Build 22.1 2021-11-24T09:38:14.749480 | | Wed Nov 24 09:41:16 GMTST 2021 | | | | Executable Attributes | | | | single-64bit-int32-archfort-optimised-std-lcomp | | | | (C) 1996-2022 ANSYS, Inc. | | | | All rights reserved. Unauthorized use, distribution or duplication | | is prohibited. This product is subject to U.S. laws governing | | export and re-export. For full Legal Notice, see documentation. | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Job Information at Start of Run | +--------------------------------------------------------------------+ Run mode: serial run Host computer: Job started: Fri Apr 8 16:12:22 2022 +--------------------------------------------------------------------+ | Initial Memory Allocation (Actual usage may vary) | +--------------------------------------------------------------------+ | Real | Integer | Character | Logical | Double ----------+------------+------------+-----------+----------+---------- Mwords | 4.59 | 13.71 | 7.05 | 0.01 | 0.18 Mbytes | 17.50 | 52.30 | 6.72 | 0.04 | 1.38 ----------+------------+------------+-----------+----------+---------- +--------------------------------------------------------------------+ | Host Memory Information (Mbytes): Interpolator | +--------------------------------------------------------------------+ | Host | System | Allocated | % | +-------------------------+----------------+----------------+--------+ | | 16331.86 | 77.95 | 0.48 | +-------------------------+----------------+----------------+--------+ ================================================== ==================== Interpolating Onto Domain "Default Domain" ================================================== ==================== Total Number of Nodes in the Target Domain = 60304 Bounding Box Volume of the Target Mesh = 1.14680E-03 Checking all source domains from the source file: Target mesh is the same as domain "Default Domain". Start direct copying of variables from domain "Default Domain". +--------------------------------------------------------------------+ | Variable Range Information | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | Variable Name | min | max | +--------------------------------------------------------------------+ | Velocity u.Beta | 5.78E-06 | 1.00E+00 | | Velocity v.Beta | 9.89E-06 | 1.00E+00 | | Velocity w.Beta | 5.30E-06 | 1.00E+00 | | Thermal Conductivity | 6.07E-01 | 6.07E-01 | | Courant Number | 8.67E-02 | 3.93E+01 | | Density | 9.97E+02 | 9.97E+02 | | Static Enthalpy | -6.12E+00 | 4.88E+00 | | Static Entropy | 0.00E+00 | 0.00E+00 | | Volume Porosity | 1.00E+00 | 1.00E+00 | | Pressure.Gradient | 2.52E+01 | 1.56E+06 | | Velocity u.Gradient | 4.58E-02 | 3.12E+02 | | Velocity v.Gradient | 5.04E-02 | 3.26E+02 | | Velocity w.Gradient | 6.97E-02 | 9.65E+02 | | Absolute Pressure | 9.52E+04 | 1.06E+05 | | Pressure | -6.17E+03 | 4.90E+03 | | Total Pressure | -4.72E+03 | 7.64E+03 | | Specific Heat Capacity at Constant Pressure| 4.18E+03 | 4.18E+03 | | Specific Heat Capacity at Constant Volume | 4.18E+03 | 4.18E+03 | | Specific Volume | 1.00E-03 | 1.00E-03 | | Shear Strain Rate | 2.64E-01 | 1.05E+03 | | Turbulence Eddy Dissipation | 5.74E-03 | 3.18E+02 | | Turbulence Eddy Frequency | 7.11E+01 | 2.79E+04 | | Temperature | 2.98E+02 | 2.98E+02 | | Turbulence Kinetic Energy | 4.77E-04 | 1.27E-01 | | Velocity | 2.55E-03 | 2.82E+00 | | Dynamic Viscosity | 8.90E-04 | 8.90E-04 | | Eddy Viscosity | 1.28E-03 | 7.54E-02 | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | *** INSUFFICIENT CATALOGUE SIZE *** | | | | ACTION REQUIRED : Increase the file catalogue size. | | | | If the situation persists please contact the CFX Customer Helpline | | giving the following details:- | | Current catalogue size : 122220 | +--------------------------------------------------------------------+ Details of error:- ---------------- Error detected by routine MAKDAT CDANAM = KELPF CDTYPE = INTR ISIZE = 2 CRESLT = FCAT Current Directory : /INTERP/OLD1/MESH/TSTEP0/CLOOP0/ZN1/FCS6039 WARNING: CFXSTP, Recursion check error. CRESLT=FCAT +--------------------------------------------------------------------+ | An error has occurred in cfx5solve: | | | | Error interpolating results onto the new mesh: C:\Program | | Files\ANSYS Inc\v221\CFX\bin\winnt-amd64\solver-mpi.exe exited | | with return code 1. | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | For CFX runs launched from Workbench, the final locations of | | directories and files generated may differ from those shown. | +--------------------------------------------------------------------+ This run of the ANSYS CFX Solver has finished. |
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April 8, 2022, 07:09 |
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#2 |
Senior Member
Gert-Jan
Join Date: Oct 2012
Location: Europe
Posts: 1,910
Rep Power: 28 |
If you investigate your output file carefully, you will see that the error occurs when CFX is interpolating the initial solution on your new definition file.
So you need to increase the catalogue size for the interpolation process, not for the solving process. |
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April 8, 2022, 09:25 |
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#3 | |
Senior Member
Join Date: Jun 2009
Posts: 1,869
Rep Power: 33 |
As Gert-Jan mentioned
Quote:
__________________
Note: I do not answer CFD questions by PM. CFD questions should be posted on the forum. |
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April 10, 2022, 21:13 |
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#4 |
New Member
Junyeol
Join Date: Mar 2022
Posts: 18
Rep Power: 4 |
I solved the problem.. thank you for everyone.
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