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June 12, 2023 at 2:34 am
cfdshark
SubscriberHi, 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 |
| |
+--------------------------------------------------------------------+
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+--------------------------------------------------------------------+
| |
| 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. |
+--------------------------------------------------------------------+
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+--------------------------------------------------------------------+
| Job Information at Start of Run |
+--------------------------------------------------------------------+
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Run mode: serial run
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Host computer: ~
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Job started: Mon Jun 12 04:11:16 2023
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+--------------------------------------------------------------------+
| License Information |
+--------------------------------------------------------------------+
License Cap: ANSYS CFD Solver
License ID: ~
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INFO: You are using an academic student license which enables meshes
up to 512000 vertices.
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INFO: Your license enables 4-way parallel execution.
For faster simulations, please start the application with the
appropriate parallel options.
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+--------------------------------------------------------------------+
| Initial Memory Allocation (Actual usage may vary) |
+--------------------------------------------------------------------+
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| 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
----------+------------+------------+-----------+----------+----------
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+--------------------------------------------------------------------+
| Host Memory Information (Mbytes): Solver |
+--------------------------------------------------------------------+
| Host | System | Allocated | % |
+-------------------------+----------------+----------------+--------+
| ~ | 12167.33 | 76.02 | 0.62 |
+-------------------------+----------------+----------------+--------+
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+--------------------------------------------------------------------+
| ****** 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. |
+--------------------------------------------------------------------+
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+--------------------------------------------------------------------+
| Topology Simplification |
+--------------------------------------------------------------------+
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+--------------------------------------------------------------------+
| ****** 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. |
+--------------------------------------------------------------------+
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+--------------------------------------------------------------------+
| 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 |
+----------------------+---------------+--------------+--------------+
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Domain Name : Default Domain
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Total Number of Nodes = 15276
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Total Number of Elements = 77322
Total Number of Tetrahedrons = 77322
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Total Number of Faces = 9126
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+--------------------------------------------------------------------+
| Average Scale Information |
+--------------------------------------------------------------------+
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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
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+--------------------------------------------------------------------+
| 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".
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+--------------------------------------------------------------------+
| Host Memory Information (Mbytes): Solver |
+--------------------------------------------------------------------+
| Host | System | Peak | % |
+-------------------------+----------------+----------------+--------+
| ~ | 12167.33 | 105.42 | 0.87 |
+-------------------------+----------------+----------------+--------+
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+--------------------------------------------------------------------+
| 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
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+--------------------------------------------------------------------+
| Job Information at End of Run |
+--------------------------------------------------------------------+
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Host computer: DESKTOP-T14J19H (PID:3952)
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Job finished: Mon Jun 12 04:11:19 2023
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Total wall clock time: 2.287E+00 seconds
or: ( 0: 0: 0: 2.287 )
( Days: Hours: Minutes: Seconds )
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+--------------------------------------------------------------------+
| An error has occurred in cfx5solve: |
| |
| The ANSYS CFX solver exited with return code 1. |
+--------------------------------------------------------------------+
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End of solution stage.
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+--------------------------------------------------------------------+
| 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 |
+--------------------------------------------------------------------+
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+--------------------------------------------------------------------+
| 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 |
+--------------------------------------------------------------------+
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+--------------------------------------------------------------------+
| For CFX runs launched from Workbench, the final locations of |
| directories and files generated may differ from those shown. |
+--------------------------------------------------------------------+
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This run of the ANSYS CFX Solver has finished.
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June 13, 2023 at 10:25 am
V.P
Ansys EmployeeHi 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
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June 14, 2023 at 3:06 am
cfdshark
SubscriberHi 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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