Update failed for the Solution component in CFX. The solver failed with a non-zero exit code of : 2
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Is this file - output file?
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If i am right, the problem with mesh?
Below i put all information from outfile. What can be the problem?
Thanks.
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OUTPUT FILE
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LIBRARY:
MATERIAL: Air Ideal Gas
Material Description = Air Ideal Gas (constant Cp)
Material Group = Air Data, Calorically Perfect Ideal Gases
Option = Pure Substance
Thermodynamic State = Gas
PROPERTIES:
Option = General Material
EQUATION OF STATE:
Molar Mass = 28.96 [kg kmol^-1]
Option = Ideal Gas
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-2 [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
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 =
END
ANALYSIS TYPE:
Option = Steady State
EXTERNAL SOLVER COUPLING:
Option = None
END
END
DOMAIN: Default Domain
Coord Frame = Coord 0
Domain Type = Fluid
Location = B218, B573
BOUNDARY: Bott
Boundary Type = OPENING
Location = Bott
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: Default Domain Default
Boundary Type = WALL
Location =
F193.218,F194.218,F195.218,F196.218,F198.218,F199.218,F200.218,F201.2
18,F202.218,F203.218,F204.218,F205.218,F206.218,F207.218,F209.218,F21
0.218,F211.218,F212.218,F213.218,F214.218,F215.218,F216.218,F217.218,
F219.218,F220.218,F221.218,F222.218,F223.218,F224.218,F225.218,F226.2
18,F227.218,F228.218,F229.218,F230.218,F231.218,F232.218,F233.218,F23
4.218,F236.218,F237.218,F238.218,F240.218,F241.218,F242.218,F243.218,
F244.218,F245.218,F246.218,F247.218,F248.218,F249.218,F250.218,F251.2
18,F252.218,F253.218,F254.218,F255.218,F256.218,F257.218,F258.218,F25
9.218,F260.218,F261.218,F262.218,F263.218,F264.218,F265.218,F266.218,
F647.573
BOUNDARY CONDITIONS:
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: Inlet
Boundary Type = INLET
Location = Inlet
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Normal Speed = 20 [km hr^-1]
Option = Normal Speed
END
TURBULENCE:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
BOUNDARY: Outlet
Boundary Type = OUTLET
Location = Outlet
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: Surfaces
Boundary Type = WALL
Location = Surfaces
BOUNDARY CONDITIONS:
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: Sym1
Boundary Type = SYMMETRY
Location = Sym1
END
BOUNDARY: Sym2
Boundary Type = SYMMETRY
Location = Sem2
END
BOUNDARY: Top
Boundary Type = OPENING
Location = Top
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
DOMAIN MODELS:
BUOYANCY MODEL:
Option = Non Buoyant
END
DOMAIN MOTION:
Option = Stationary
END
MESH DEFORMATION:
Option = None
END
REFERENCE PRESSURE:
Reference Pressure = 0.2354 [atm]
END
END
FLUID DEFINITION: Fluid 1
Material = Air Ideal Gas
Option = Material Library
MORPHOLOGY:
Option = Continuous Fluid
END
END
FLUID MODELS:
COMBUSTION MODEL:
Option = None
END
HEAT TRANSFER MODEL:
Fluid Temperature = 216.65 [K]
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 = 150
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
END
END
COMMAND FILE:
Version = 16.2
Results Version = 16.2
END
SIMULATION CONTROL:
EXECUTION CONTROL:
EXECUTABLE SELECTION:
Double Precision = No
END
INTERPOLATOR STEP CONTROL:
Runtime Priority = Standard
MEMORY CONTROL:
Memory Allocation Factor = 1.0
END
END
PARALLEL HOST LIBRARY:
HOST DEFINITION: dimapc
Remote Host Name = DIMA-PC
Host Architecture String = winnt-amd64
Installation Root = C:Program FilesANSYS Incv%vCFX
END
END
PARTITIONER STEP CONTROL:
Multidomain Option = Automatic
Runtime Priority = Standard
EXECUTABLE SELECTION:
Use Large Problem Partitioner = Off
END
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 = CFX.def
Solver Results File =
D
MEGA/Mega/Education/PhD/Model/Aerodinamic/Ansys_wing/Ansys_wing_va
r5/Ansys_wing_var3_pending/dp0_CFX_Solution/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 = CFX_001.res
END
END
END
SOLVER STEP CONTROL:
Runtime Priority = Standard
MEMORY CONTROL:
Memory Allocation Factor = 1.0
END
PARALLEL ENVIRONMENT:
Number of Processes = 1
Start Method = Serial
END
END
END
END
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| Interpolation of Initial Values |
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| ANSYS(R) CFX(R) Interpolator |
| |
| Release 16.2 |
| Build 16.2 2015.06.29-10.01-134376 |
| Mon Jun 29 10
6:10 GMTDT 2015 |
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| Executable Attributes |
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| single-64bit-int32-supfort-optimised-noprof-lcomp |
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| (C) 2015 ANSYS, Inc. |
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| 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
Host computer: DIMA-PC (PID:2784)
Job started: Tue Feb 04 21:28:59 2020
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| Memory Allocated for Run (Actual usage may be less) |
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| Real | Integer | Character | Logical | Double
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Mwords | 59.18 | 70.63 | 0.20 | 0.01 | 0.30
Mbytes | 225.75 | 269.43 | 0.19 | 0.04 | 2.29
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| Host Memory Information (Mbytes) |
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| Host | System | Allocated | % |
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| DIMA-PC | 8078.36 | 497.70 | 6.16 |
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======================================================================
Interpolating Onto Domain "Default Domain"
======================================================================
Total Number of Nodes in the Target Domain = 915134
Bounding Box Volume of the Target Mesh = 3.31665E+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".
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| Variable Range Information |
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| Variable Name | min | max |
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| Isothermal Compressibility | 4.19E-05 | 4.19E-05 |
| Thermal Conductivity | 2.61E-02 | 2.61E-02 |
| Courant Number | 0.00E+00 | 0.00E+00 |
| Density | 3.83E-01 | 3.83E-01 |
| Isolated Volumes | 1.00E+00 | 2.00E+00 |
| Density Derivative wrt Pressure at Constant| 1.61E-05 | 1.61E-05 |
| Static Entropy | 9.46E+01 | 9.46E+01 |
| Density.Gradient | 0.00E+00 | 1.67E-01 |
| Pressure.Gradient | 0.00E+00 | 0.00E+00 |
| Velocity u.Gradient | 0.00E+00 | 1.03E+02 |
| Velocity v.Gradient | 0.00E+00 | 0.00E+00 |
| Velocity w.Gradient | 0.00E+00 | 0.00E+00 |
| Wall Scale.Gradient | 0.00E+00 | 0.00E+00 |
| Pressure | 0.00E+00 | 0.00E+00 |
| Specific Heat Capacity at Constant Pressure| 1.00E+03 | 1.00E+03 |
| Second Blending Function for SST model | 1.00E+00 | 1.00E+00 |
| Turbulence Eddy Frequency | 4.40E+05 | 4.40E+05 |
| Temperature | 2.17E+02 | 2.17E+02 |
| Turbulence Kinetic Energy | 2.10E+02 | 2.10E+02 |
| Velocity | 2.37E+02 | 2.37E+02 |
| Dynamic Viscosity | 1.83E-05 | 1.83E-05 |
| Eddy Viscosity | 1.83E-04 | 1.83E-04 |
| Wall Scale | 0.00E+00 | 0.00E+00 |
Details of error:-
Error detected by routine MAKDAT
Illegal data area length CDANAM = NCOMPT CDTYPE = INTR ISIZE = 0
CRESLT = SIZE
Current Directory : /INTERP/SOLUTION/DST/VX
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| ****** PROBLEM REPORT ****** |
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| Subsystem: Input and Output |
| Subroutine name: ErrAction |
| Severity level: Fatal Error |
| Error message number: 001100279 |
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| Message: |
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| Stopped in routine MEMERR |
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+====================================================================+
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| An error has occurred in cfx5solve: |
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| Error interpolating results onto the new mesh: C:Program |
| FilesANSYS Incv162CFXbinwinnt-amd64solver-pcmpi.exe exited |
| with return code 1. |
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| The following user files have been saved in the directory |
| D
MEGA/Mega/Education/PhD/Model/Aerodinamic/Ansys_wing/Ansys_win- |
| g_var5/Ansys_wing_var3_pending/dp0_CFX_Solution/CFX_003: |
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| job |
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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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| Warning! |
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| After waiting for 60 seconds, 1 solver manager process(es) appear |
| not to have noticed that this run has ended. You may get errors |
| removing some files if they are still open in the solver manager. |
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This run of the ANSYS CFX Solver has finished.
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When i try to open solution i have trouble, window with solution are not responding((
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- The topic ‘Update failed for the Solution component in CFX. The solver failed with a non-zero exit code of : 2’ is closed to new replies.
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