I got code 1 error from ANSYS CFX

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March 11, 2014, 20:22
I got code 1 error from ANSYS CFX
#1
New Member

Chaeyeong Kim
Join Date: Mar 2014
Posts: 1
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you can check my modelling from attachment file.

below this line is the error message which i got from ANSYS CFX

I don't know What is the PROBLEM!!!

would you guys explain this in detail?
-------------------------------------------------------------------------
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 = Automatic
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:
Length Units = [m]
Mass Units = [kg]
Solid Angle Units = [sr]
Temperature Units = [K]
Time Units = [s]
END
ANALYSIS TYPE:
EXTERNAL SOLVER COUPLING:
Option = None
END
END
DOMAIN: Default Domain
Coord Frame = Coord 0
Domain Type = Fluid
Location = B20, B6
BOUNDARY: Default Domain Default
Boundary Type = WALL
Location = F7.6
BOUNDARY CONDITIONS:
MASS AND MOMENTUM:
Option = No Slip Wall
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: inlet
Boundary Type = INLET
Location = F26.20
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Normal Speed = 5 [m s^-1]
Option = Normal Speed
END
TURBULENCE:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
BOUNDARY: outlet
Boundary Type = OUTLET
Location = F22.20
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Option = Static Pressure
Relative Pressure = 0 [Pa]
END
END
END
BOUNDARY: wall
Boundary Type = WALL
Location = F21.20,F23.20,F24.20,F25.20
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:
Option = None
END
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
Option = Upwind
END
CONVERGENCE CONTROL:
Length Scale Option = Conservative
Maximum Number of Iterations = 20
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 = 13.0
Results Version = 13.0
END
SIMULATION CONTROL:
EXECUTION CONTROL:
EXECUTABLE SELECTION:
Double Precision = Off
END
INTERPOLATOR STEP CONTROL:
Runtime Priority = Standard
MEMORY CONTROL:
Memory Allocation Factor = 1.0
END
END
PARALLEL HOST LIBRARY:
HOST DEFINITION: kimliapc
Remote Host Name = KIMLIA-PC
Host Architecture String = winnt-amd64
Installation Root = C:\Program Files\ANSYS Inc\v%v\CFX
END
END
PARTITIONER STEP CONTROL:
Multidomain Option = Independent Partitioning
Runtime Priority = Standard
EXECUTABLE SELECTION:
Use Large Problem Partitioner = Off
END
MEMORY CONTROL:
Memory Allocation Factor = 1.0
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
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:
Memory Allocation Factor = 1.0
END
PARALLEL ENVIRONMENT:
Number of Processes = 1
Start Method = Serial
END
END
END
END

+--------------------------------------------------------------------+
| |
| Interpolation of Initial Values |
| |
+--------------------------------------------------------------------+

+--------------------------------------------------------------------+
| |
| ANSYS CFX Interpolator 13.0 |
| |
| Version 2010.10.01-23.02 Sat Oct 2 02:31:59 GMTDT 2010 |
| |
| Executable Attributes |
| |
| single-int32-64bit-novc8-noifort-novc6-optimised-supfort-noprof-nos|
| |
| Copyright 2010 ANSYS Inc. |
+--------------------------------------------------------------------+

+--------------------------------------------------------------------+
| Job Information |
+--------------------------------------------------------------------+

Run mode: serial run

Host computer: KIMLIA-PC (PID:4004)
Job started: Wed Mar 12 09:16:33 2014

+--------------------------------------------------------------------+
| Memory Allocated for Run (Actual usage may be less) |
+--------------------------------------------------------------------+

Data Type Kwords Words/Node Words/Elem Kbytes Bytes/Node

Real 12672.0 71.05 13.57 49499.9 284.19
Integer 16508.7 92.56 17.68 64487.0 370.24
Character 200.0 1.12 0.21 195.3 1.12
Logical 10.0 0.06 0.01 39.1 0.22
Double 300.0 1.68 0.32 2343.8 13.46

================================================== ====================
Interpolating Onto Domain "Default Domain"
================================================== ====================

Total Number of Nodes in the Target Domain = 178357
Bounding Box Volume of the Target Mesh = 2.88000E+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 |
+--------------------------------------------------------------------+
| Thermal Conductivity | 2.61E-02 | 2.61E-02 |
| Courant Number | 0.00E+00 | 0.00E+00 |
| Density | 1.18E+00 | 1.18E+00 |
| Isolated Volumes | 1.00E+00 | 2.00E+00 |
| Static Entropy | 0.00E+00 | 0.00E+00 |
| Pressure | 8.06E+05 | 8.06E+05 |
| Specific Heat Capacity at Constant Pressure| 1.00E+03 | 1.00E+03 |
| Turbulence Eddy Dissipation | 3.20E+03 | 3.20E+03 |
| Temperature | 2.98E+02 | 2.98E+02 |
| Turbulence Kinetic Energy | 2.34E+00 | 2.34E+00 |
| Velocity | 2.50E+01 | 2.50E+01 |
| Dynamic Viscosity | 1.83E-05 | 1.83E-05 |
| Eddy Viscosity | 1.83E-04 | 1.83E-04 |

Details of error:-
Details of error:-
----------------
----------------
Error detected by routine MAKDAT
Error detected by routine MAKDAT
Illegal data area length CDANAM = NCOMPT CDTYPE = INTR ISIZE = 0
Illegal data area length CDANAM = NCOMPT CDTYPE = INTR ISIZE = 0
CRESLT = SIZE
CRESLT = SIZE

Current Directory : /INTERP/SOLUTION/DST/VX
Current Directory : /INTERP/SOLUTION/DST/VX

+================================================= ===================+
| ****** PROBLEM REPORT ****** |
|--------------------------------------------------------------------|
| Subsystem: Input and Output |
| Subroutine name: ErrAction |
| Severity level: Fatal Error |
| Error message number: 001100279 |
|--------------------------------------------------------------------|
| Message: |
| |
| Stopped in routine MEMERR |
| |
| |
| |
| |
| |
+================================================= ===================+

+--------------------------------------------------------------------+
| An error has occurred in cfx5solve: |
| |
| Error interpolating results onto the new mesh: C:\Program |
| Files\ANSYS Inc\v130\CFX\bin\winnt-amd64\solver-hpmpi.exe exited |
| with return code 1. |
+--------------------------------------------------------------------+
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