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Error in Ansys CFX Solver

    • cfdshark
      Subscriber

      Hi, I am new to Ansys and trying out this tutorial from YouTube on the 2023 R1 version (CFX fluid). I run into these errors: (I uninstalled Ansys and re-installed it but the same errors persist, I attempted every solution I could find on the all-knowing Oracle, Google but to no avail)

      The ANSYS CFX solver exited with return code 1.

      Update failed for the Solution component in Fluid Flow (CFX). The solver failed with a non-zero exit code of : 2

      I've put the tilde in the place of my license ID

      This run of the CFX 2023 R1 Solver started at 04:11:12 on 12 Jun 2023

      by user user on ~ (intel_xeon64.sse2_winnt) using the

      command:

      "C:\Program Files\ANSYS Inc\ANSYS Student\v231\CFX\bin\perllib\cfx5solve.pl"

      -batch -ccl runInput.ccl -fullname "Fluid Flow CFX_001"

      2023 R1

      Point Releases and Patches installed:

      Discovery 2023 R1

      Autodyn 2023 R1

      SpaceClaim 2023 R1

      CFX (includes CFD-Post) 2023 R1

      Chemkin 2023 R1

      EnSight 2023 R1

      FENSAP-ICE 2023 R1

      Fluent (includes CFD-Post) 2023 R1

      Polyflow (includes CFD-Post) 2023 R1

      Forte (includes EnSight) 2023 R1

      TurboGrid 2023 R1

      Aqwa 2023 R1

      Speos 2023 R1

      Mechanical Products 2023 R1

      Material Calibration App 2023 R1

      ACIS Geometry Interface 2023 R1

      AutoCAD Geometry Interface 2023 R1

      Catia, Version 4 Geometry Interface 2023 R1

      Catia, Version 5 Geometry Interface 2023 R1

      Catia, Version 6 Geometry Interface 2023 R1

      Creo Elements/Direct Modeling Geometry Interface 2023 R1

      Creo Parametric Geometry Interface 2023 R1

      Inventor Geometry Interface 2023 R1

      JTOpen Geometry Interface 2023 R1

      NX Geometry Interface 2023 R1

      Parasolid Geometry Interface 2023 R1

      Solid Edge Geometry Interface 2023 R1

      SOLIDWORKS Geometry Interface 2023 R1

      Academic Student 2023 R1

      Setting up CFX Solver run ...

      +--------------------------------------------------------------------+

      | |

      | CFX Command Language for Run |

      | |

      +--------------------------------------------------------------------+

      LIBRARY:

      MATERIAL: Air at 25 C

      Material Description = Air at 25 C and 1 atm (dry)

      Material Group = Air Data, Constant Property Gases

      Option = Pure Substance

      Thermodynamic State = Gas

      PROPERTIES:

      Option = General Material

      EQUATION OF STATE:

      Density = 1.185 [kg m^-3]

      Molar Mass = 28.96 [kg kmol^-1]

      Option = Value

      END

      SPECIFIC HEAT CAPACITY:

      Option = Value

      Specific Heat Capacity = 1.0044E+03 [J kg^-1 K^-1]

      Specific Heat Type = Constant Pressure

      END

      REFERENCE STATE:

      Option = Specified Point

      Reference Pressure = 1 [atm]

      Reference Specific Enthalpy = 0. [J/kg]

      Reference Specific Entropy = 0. [J/kg/K]

      Reference Temperature = 25 [C]

      END

      DYNAMIC VISCOSITY:

      Dynamic Viscosity = 1.831E-05 [kg m^-1 s^-1]

      Option = Value

      END

      THERMAL CONDUCTIVITY:

      Option = Value

      Thermal Conductivity = 2.61E-02 [W m^-1 K^-1]

      END

      ABSORPTION COEFFICIENT:

      Absorption Coefficient = 0.01 [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 = 0.003356 [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 = Steady State

      EXTERNAL SOLVER COUPLING:

      Option = None

      END

      END

      DOMAIN: Default Domain

      Coord Frame = Coord 0

      Domain Type = Fluid

      Location = B186, B98

      BOUNDARY: inlet

      Boundary Type = INLET

      Location = F30.98

      BOUNDARY CONDITIONS:

      FLOW REGIME:

      Option = Subsonic

      END

      MASS AND MOMENTUM:

      Normal Speed = 40 [km hr^-1]

      Option = Normal Speed

      END

      TURBULENCE:

      Option = Medium Intensity and Eddy Viscosity Ratio

      END

      END

      END

      BOUNDARY: opening

      Boundary Type = OPENING

      Location = F26.98,F28.98,F29.98

      BOUNDARY CONDITIONS:

      FLOW DIRECTION:

      Option = Normal to Boundary Condition

      END

      FLOW REGIME:

      Option = Subsonic

      END

      MASS AND MOMENTUM:

      Option = Opening Pressure and Direction

      Relative Pressure = 0 [Pa]

      END

      TURBULENCE:

      Option = Medium Intensity and Eddy Viscosity Ratio

      END

      END

      END

      BOUNDARY: outlet

      Boundary Type = OUTLET

      Location = F31.98

      BOUNDARY CONDITIONS:

      FLOW REGIME:

      Option = Subsonic

      END

      MASS AND MOMENTUM:

      Option = Average Static Pressure

      Pressure Profile Blend = 0.05

      Relative Pressure = 0 [Pa]

      END

      PRESSURE AVERAGING:

      Option = Average Over Whole Outlet

      END

      END

      END

      BOUNDARY: wall

      Boundary Type = WALL

      Location = \

      F139.186,F140.186,F141.186,F142.186,F143.186,F144.186,F145.186,F146.1\

      86,F147.186,F163.186,F164.186,F166.186,F168.186,F169.186,F171.186,F17\

      3.186,F181.186,F182.186,F183.186,F187.186,F188.186,F189.186,F27.98,F3\

      2.98,F33.98,F34.98,F35.98,F36.98,F37.98,F38.98,F39.98,F40.98,F41.98,F\

      42.98,F43.98,F44.98,F45.98,F46.98,F47.98,F48.98,F49.98,F50.98,F51.98,\

      F52.98,F53.98

      BOUNDARY CONDITIONS:

      MASS AND MOMENTUM:

      Option = No Slip Wall

      END

      WALL ROUGHNESS:

      Option = Smooth Wall

      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 = Air at 25 C

      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 = SST

      END

      TURBULENT WALL FUNCTIONS:

      Option = Automatic

      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:

      Length Scale Option = Conservative

      Maximum Number of Iterations = 100

      Minimum Number of Iterations = 1

      Timescale Control = Auto Timescale

      Timescale Factor = 1.0

      END

      CONVERGENCE CRITERIA:

      Residual Target = 1.E-4

      Residual Type = RMS

      END

      DYNAMIC MODEL CONTROL:

      Global Dynamic Model Control = On

      END

      INTERRUPT CONTROL:

      Option = Any Interrupt

      CONVERGENCE CONDITIONS:

      Option = Default Conditions

      END

      END

      END

      EXPERT PARAMETERS:

      topology estimate factor = 1.0

      END

      END

      COMMAND FILE:

      Version = 23.1

      Results Version = 23.1

      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

      Option = Model Based

      END

      END

      PARALLEL HOST LIBRARY:

      HOST DEFINITION: ~

      Remote Host Name = ~

      Host Architecture String = winnt-amd64

      Installation Root = C:\Program Files\ANSYS Inc\ANSYS Student\v%v\CFX

      END

      END

      PARTITIONER STEP CONTROL:

      Multidomain Option = Automatic

      Runtime Priority = Standard

      MEMORY CONTROL:

      Memory Allocation Factor = 1.0

      Option = Model Based

      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 = \

      C:/Users/user/AppData/Local/Temp/WB_user_18340_2/wbnew_pending/dp0_\

      CFX_Solution/Fluid Flow CFX_001.res

      END

      SOLVER STEP CONTROL:

      Runtime Priority = Standard

      MEMORY CONTROL:

      Memory Allocation Factor = 1.0

      Option = Model Based

      END

      PARALLEL ENVIRONMENT:

      Number of Processes = 1

      Start Method = Serial

      END

      END

      END

      END

      +--------------------------------------------------------------------+

      | |

      | Solver |

      | |

      +--------------------------------------------------------------------+

       

       

       

      +--------------------------------------------------------------------+

      | |

      | ANSYS(R) CFX(R) Solver |

      | |

      | 2023 R1 |

      | Build 23.1 2022-11-25T14:31:12.124816 |

      | Fri Nov 25 16:32:25 GMTST 2022 |

      | |

      | Executable Attributes |

      | |

      | single-64bit-int32-archfort-optimised-std-lcomp |

      | |

      | (C) 1996-2023 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: Mon Jun 12 04:11:16 2023

       

      +--------------------------------------------------------------------+

      | License Information |

      +--------------------------------------------------------------------+

      License Cap: ANSYS CFD Solver

      License ID: ~

       

      INFO: You are using an academic student license which enables meshes

      up to 512000 vertices.

       

      INFO: Your license enables 4-way parallel execution.

      For faster simulations, please start the application with the

      appropriate parallel options.

       

       

      +--------------------------------------------------------------------+

      | Initial Memory Allocation (Actual usage may vary) |

      +--------------------------------------------------------------------+

       

      | Real | Integer | Character | Logical | Double

      ----------+------------+------------+-----------+----------+----------

      Mwords | 12.70 | 3.83 | 9.30 | 0.12 | 0.47

      Mbytes | 48.46 | 14.63 | 8.87 | 0.46 | 3.60

      ----------+------------+------------+-----------+----------+----------

       

       

      +--------------------------------------------------------------------+

      | Host Memory Information (Mbytes): Solver |

      +--------------------------------------------------------------------+

      | Host | System | Allocated | % |

      +-------------------------+----------------+----------------+--------+

      | ~ | 12167.33 | 76.02 | 0.62 |

      +-------------------------+----------------+----------------+--------+

       

      +--------------------------------------------------------------------+

      | ****** Notice ****** |

      | |

      | One or more expert parameters have been enabled. Note that expert |

      | parameters are intended for use only by customers who are |

      | experienced in the use of CFX, or who have been instructed to use |

      | them by ANSYS Customer Support. Use of the parameters is not fully |

      | supported, and may have unexpected or unintended consequences both |

      | for the quality of results and the performance of the CFX-Solver. |

      +--------------------------------------------------------------------+

       

      +--------------------------------------------------------------------+

      | Topology Simplification |

      +--------------------------------------------------------------------+

       

      +--------------------------------------------------------------------+

      | ****** Warning ****** |

      | |

      | Topology simplification is activated with the following |

      | restrictions: |

      | |

      | - Mesh regions referenced only within User Fortran and NOT |

      | in the command file will cause the solver to stop. |

      | - The solver will stop during any "Edit Run in Progress" step |

      | if new 2D regions are referenced. |

      +--------------------------------------------------------------------+

       

      +--------------------------------------------------------------------+

      | Mesh Statistics |

      +--------------------------------------------------------------------+

      | Domain Name | Orthog. Angle | Exp. Factor | Aspect Ratio |

      +----------------------+---------------+--------------+--------------+

      | | Minimum [deg] | Maximum | Maximum |

      +----------------------+---------------+--------------+--------------+

      | Default Domain | 3.4 ! | 6807 ! | 48 OK |

      +----------------------+---------------+--------------+--------------+

      | | %! %ok %OK | %! %ok %OK | %! %ok %OK |

      +----------------------+---------------+--------------+--------------+

      | Default Domain | <1 1 99 | <1 4 96 | 0 0 100 |

      +----------------------+---------------+--------------+--------------+

       

      Domain Name : Default Domain

       

      Total Number of Nodes = 15276

       

      Total Number of Elements = 77322

      Total Number of Tetrahedrons = 77322

       

      Total Number of Faces = 9126

       

      +--------------------------------------------------------------------+

      | Average Scale Information |

      +--------------------------------------------------------------------+

       

      Domain Name : Default Domain

      Global Length = 8.9411E-02

      Minimum Extent = 5.8849E-02

      Maximum Extent = 1.4100E-01

      Density = 1.1850E+00

      Dynamic Viscosity = 1.8310E-05

      Velocity = 1.1111E+01

      Advection Time = 8.0470E-03

      Reynolds Number = 6.4295E+04

       

      +--------------------------------------------------------------------+

      | Checking for Isolated Fluid Regions |

      +--------------------------------------------------------------------+

      2 isolated fluid regions were found in domain Default Domain

      If the isolated regions do not have the pressure level set either

      by the boundary conditions or using a reference pressure equation,

      you may encounter severe robustness problems.

      This situation may have arisen because a domain interface was not

      properly defined during problem setup. Please carefully check

      the setup.

      The solver will stop now and write a results file. The isolated

      regions can be visualised in CFX Post by making plots of the

      variable "Isolated Volumes".

      If you are sure that the pressure level is set in each isolated

      fluid region then you can force the solver to turn off this check

      by setting the expert parameter "check isolated regions = f".

       

       

      +--------------------------------------------------------------------+

      | Host Memory Information (Mbytes): Solver |

      +--------------------------------------------------------------------+

      | Host | System | Peak | % |

      +-------------------------+----------------+----------------+--------+

      | ~ | 12167.33 | 105.42 | 0.87 |

      +-------------------------+----------------+----------------+--------+

       

      +--------------------------------------------------------------------+

      | CPU Time Requirements of Solver |

      +--------------------------------------------------------------------+

      File Reading 8.41E-01 29.0 %

      Variable Updates 1.90E-02 0.7 %

      File Writing 2.01E-01 6.9 %

      Miscellaneous 1.84E+00 63.4 %

      --------

      Total 2.90E+00

       

      +--------------------------------------------------------------------+

      | Job Information at End of Run |

      +--------------------------------------------------------------------+

       

      Host computer: DESKTOP-T14J19H (PID:3952)

       

      Job finished: Mon Jun 12 04:11:19 2023

       

      Total wall clock time: 2.287E+00 seconds

      or: ( 0: 0: 0: 2.287 )

      ( Days: Hours: Minutes: Seconds )

       

       

      +--------------------------------------------------------------------+

      | An error has occurred in cfx5solve: |

      | |

      | The ANSYS CFX solver exited with return code 1. |

      +--------------------------------------------------------------------+

       

      End of solution stage.

       

      +--------------------------------------------------------------------+

      | The results from this run of the ANSYS CFX Solver have been |

      | written to |

      | C:/Users/user/AppData/Local/Temp/WB_user_18340_2/wbnew_pending/- |

      | dp0_CFX_Solution/Fluid Flow CFX_001.res |

      +--------------------------------------------------------------------+

       

       

      +--------------------------------------------------------------------+

      | The following user files have been saved in the directory |

      | C:/Users/user/AppData/Local/Temp/WB_user_18340_2/wbnew_pending/- |

      | dp0_CFX_Solution/Fluid Flow CFX_001: |

      | |

      | mon |

      +--------------------------------------------------------------------+

       

       

      +--------------------------------------------------------------------+

      | 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.

    • V.P
      Ansys Employee

      Hi cfdshark,

      From the report shared here, I can see that the solver has detected two isolated fluid regions. That is why the solver has stopped. Please follow the instructions that follow as given in the report. You can check isolated regions in CFD post by loading the .res file and then going to Insert > Location > Volume. Set Method = Isovolume, and Variable = Isolated Regions. Set Mode = At Value, and Value = 1 or 2 (or any other number from 1 to the number of isolated fluid regions). The interface between volumes of different values will show where there is a wall. There is likely a wall between isolated fluid regions and making a modification in Geometry to allow for a conformal mesh to be generated

    • cfdshark
      Subscriber

      Hi CFD_Friend, thank you for taking the time to go through the results message I posted. It is greatly appreciated. I finally fixed the problem, I went back to the mesh and deleted the vehicle geometry, leaving only the enclosure geometry. That took care of the problem, now I can go about my cfdsharking business

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