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Old   August 16, 2013, 11:45
Default ansys cfx solver exit with return code 1!!!!!
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hi, i'm using ansys transient structural and cfx coupling to analyse a two way fsi problem in a free surface flow condition, but when cfx solver starts the run, in the beginnig this error comes up and no result files will be created:
The ANSYS CFX solver exited with return code 1. No results file
has been created.
for the record, i'm analysing a circular column in water, can anybody help me please?
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Old   August 16, 2013, 12:29
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Post the .out file and read the FAQ.
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Old   August 16, 2013, 14:05
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here is the out file
Attached Files
File Type: zip Fluid Flow CFX_001.zip (7.0 KB, 30 views)
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Old   August 16, 2013, 15:42
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Can you just simply copy and paste the text in here?

Besides that .zip file does not work anyway.

Also what simulations are you doing exactly? You're not exactly spoon feeding us the information we need for us to help you!
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Old   August 16, 2013, 22:40
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ok here we go, in the structural part, earthquake acceleration is given to the columns bottom; in cfx part, we have a two phase (air and water) domain to show the depth of water the column is in, and of course it is coupled to the structural, below is the full out file:
This run of the CFX-14.0 Solver started at 22:24:37 on 16 Aug 2013 by
user amir on AMIR-PC (intel_xeon64.sse2_winnt) using the command:

"E:\ANSYS Inc\v140\CFX\bin\perllib\cfx5solve.pl" -batch -ccl runInput.ccl
-fullname "Fluid Flow CFX_001"

Setting up CFX Solver run ...


+--------------------------------------------------------------------+
| |
| Processing ANSYS Input File (Running CCL2MF) |
| |
+--------------------------------------------------------------------+

Created
C:\Users\amir\Desktop\work\01_pending_tasks\dp0_CF X_Solution_1\Fluid
Flow CFX_001.ansys\ANSYS.mf

+--------------------------------------------------------------------+
| |
| Starting ANSYS Solver |
| |
+--------------------------------------------------------------------+


+--------------------------------------------------------------------+
| |
| CFX Command Language for Run |
| |
+--------------------------------------------------------------------+

LIBRARY:
CEL:
EXPRESSIONS:
a = step((y-uph)/1[m])
uph = 9 [m]
wat = 1-a
END
END
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
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:
ANSYS Input File = ds.dat
Option = ANSYS MultiField
COUPLING TIME CONTROL:
COUPLING INITIAL TIME:
Option = Automatic
END
COUPLING TIME DURATION:
Option = Total Time
Total Time = 1 [s]
END
COUPLING TIME STEPS:
Option = Timesteps
Timesteps = 0.01 [s]
END
END
END
INITIAL TIME:
Option = Coupling Initial Time
END
TIME DURATION:
Option = Coupling Time Duration
END
TIME STEPS:
Option = Coupling Timesteps
END
END
DOMAIN: Default Domain
Coord Frame = Coord 0
Domain Type = Fluid
Location = B26
BOUNDARY: Default Domain Default
Boundary Type = WALL
Location = F20.26,F21.26,F22.26,F24.26
BOUNDARY CONDITIONS:
MASS AND MOMENTUM:
Option = No Slip Wall
END
MESH MOTION:
Option = Stationary
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: in
Boundary Type = INLET
Location = F23.26
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Normal Speed = 0 [m s^-1]
Option = Normal Speed
END
MESH MOTION:
Option = Stationary
END
TURBULENCE:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
FLUID: air
BOUNDARY CONDITIONS:
VOLUME FRACTION:
Option = Value
Volume Fraction = a
END
END
END
FLUID: water
BOUNDARY CONDITIONS:
VOLUME FRACTION:
Option = Value
Volume Fraction = wat
END
END
END
END
BOUNDARY: interface
Boundary Type = WALL
Location = F25.26
BOUNDARY CONDITIONS:
MASS AND MOMENTUM:
Option = No Slip Wall
END
MESH MOTION:
ANSYS Interface = FSIN_1
Option = ANSYS MultiField
Receive from ANSYS = Total Mesh Displacement
Send to ANSYS = Total Force
END
WALL ROUGHNESS:
Option = Smooth Wall
END
END
END
BOUNDARY: top
Boundary Type = OPENING
Location = F27.26
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Option = Entrainment
Relative Pressure = 0 [Pa]
END
MESH MOTION:
Option = Stationary
END
TURBULENCE:
Option = Zero Gradient
END
END
FLUID: air
BOUNDARY CONDITIONS:
VOLUME FRACTION:
Option = Value
Volume Fraction = 1
END
END
END
FLUID: water
BOUNDARY CONDITIONS:
VOLUME FRACTION:
Option = Value
Volume Fraction = 0
END
END
END
END
DOMAIN MODELS:
BUOYANCY MODEL:
Buoyancy Reference Density = 1.185 [kg m^-3]
Gravity X Component = 0 [m s^-2]
Gravity Y Component = -g
Gravity Z Component = 0 [m s^-2]
Option = Buoyant
BUOYANCY REFERENCE LOCATION:
Option = Automatic
END
END
DOMAIN MOTION:
Option = Stationary
END
MESH DEFORMATION:
Option = Regions of Motion Specified
MESH MOTION MODEL:
Option = Displacement Diffusion
MESH STIFFNESS:
Option = Increase near Small Volumes
Stiffness Model Exponent = 10
END
END
END
REFERENCE PRESSURE:
Reference Pressure = 1 [atm]
END
END
FLUID DEFINITION: air
Material = Air at 25 C
Option = Material Library
MORPHOLOGY:
Option = Continuous Fluid
END
END
FLUID DEFINITION: water
Material = Water
Option = Material Library
MORPHOLOGY:
Option = Continuous Fluid
END
END
FLUID MODELS:
COMBUSTION MODEL:
Option = None
END
FLUID: air
FLUID BUOYANCY MODEL:
Option = Density Difference
END
END
FLUID: water
FLUID BUOYANCY MODEL:
Option = Density Difference
END
END
HEAT TRANSFER MODEL:
Fluid Temperature = 25 [C]
Homogeneous Model = True
Option = Isothermal
END
THERMAL RADIATION MODEL:
Option = None
END
TURBULENCE MODEL:
Option = k epsilon
BUOYANCY TURBULENCE:
Option = None
END
END
TURBULENT WALL FUNCTIONS:
Option = Scalable
END
END
FLUID PAIR: air | water
INTERPHASE TRANSFER MODEL:
Option = None
END
MASS TRANSFER:
Option = None
END
SURFACE TENSION MODEL:
Option = None
END
END
MULTIPHASE MODELS:
Homogeneous Model = On
FREE SURFACE MODEL:
Option = Standard
END
END
END
INITIALISATION:
Option = Automatic
FLUID: air
INITIAL CONDITIONS:
VOLUME FRACTION:
Option = Automatic with Value
Volume Fraction = a
END
END
END
FLUID: water
INITIAL CONDITIONS:
VOLUME FRACTION:
Option = Automatic with Value
Volume Fraction = wat
END
END
END
INITIAL CONDITIONS:
Velocity Type = Cartesian
CARTESIAN VELOCITY COMPONENTS:
Option = Automatic with Value
U = 0 [m s^-1]
V = 0 [m s^-1]
W = 0 [m s^-1]
END
STATIC PRESSURE:
Option = Automatic with Value
Relative Pressure = 0 [Pa]
END
TURBULENCE INITIAL CONDITIONS:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END
OUTPUT CONTROL:
RESULTS:
File Compression Level = Default
Option = Standard
END
END
SOLVER CONTROL:
Turbulence Numerics = First Order
ADVECTION SCHEME:
Option = Upwind
END
CONVERGENCE CONTROL:
Maximum Number of Coefficient Loops = 3
Minimum Number of Coefficient Loops = 1
Timescale Control = Coefficient Loops
END
CONVERGENCE CRITERIA:
Residual Target = 1.E-4
Residual Type = RMS
END
EXTERNAL SOLVER COUPLING CONTROL:
COUPLING DATA TRANSFER CONTROL:
Convergence Target = 1e-2
Under Relaxation Factor = 0.75
END
COUPLING STEP CONTROL:
Maximum Number of Coupling Iterations = 10
Minimum Number of Coupling Iterations = 1
SOLUTION SEQUENCE CONTROL:
Solve ANSYS Fields = Before CFX Fields
END
END
END
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Old   August 16, 2013, 22:41
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MULTIPHASE CONTROL:
Volume Fraction Coupling = Coupled
END
TRANSIENT SCHEME:
Option = First Order Backward Euler
END
END
END
COMMAND FILE:
Version = 14.0
Results Version = 14.0
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
MFX RUN CONTROL:
MFX RUN DEFINITION:
MFX Run Mode = Start ANSYS and CFX
Process ANSYS Input File = On
Restart ANSYS Run = Off
END
MFX SOLVER CONTROL:
ANSYS Installation Root = E:\ANSYS Inc\v140\ansys
END
END
PARALLEL HOST LIBRARY:
HOST DEFINITION: amirpc
Remote Host Name = AMIR-PC
Host Architecture String = winnt-amd64
Installation Root = E:\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
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
PROCESS COUPLING:
Process Name = CFX
Host Port = 52438
Host Name = AMIR-PC
END
END
END
END


+--------------------------------------------------------------------+
| |
| Solver |
| |
+--------------------------------------------------------------------+




+--------------------------------------------------------------------+
| |
| ANSYS(R) CFX(R) Solver 14.0 |
| |
| Version 2011.10.10-23.01 Tue Oct 11 00:28:38 GMTDT 2011 |
| |
| Executable Attributes |
| |
| single-int32-64bit-novc8-noifort-novc6-optimised-supfort-noprof-nos|
| |
| (C) 2011 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 |
+--------------------------------------------------------------------+

Run mode: serial run

Host computer: AMIR-PC (PID:18568)
Job started: Fri Aug 16 22:24:50 2013

Connecting to the following master process:
Host Name : AMIR-PC
Port Number : 52438
License Cap: ANSYS CFX Solver (Max 128K Nodes)
License ID: AMIR-PC-SYSTEM-1620-011915


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

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

Real 35111.7 8991.47 10972.40 137155.0 35965.88
Integer 1859.1 476.08 580.96 7262.0 1904.31
Character 3791.4 970.91 1184.81 3702.5 970.91
Logical 80.0 20.49 25.00 312.5 81.95
Double 56.4 14.44 17.62 440.6 115.54

+--------------------------------------------------------------------+
| Mesh Statistics |
+--------------------------------------------------------------------+
| Domain Name | Orthog. Angle | Exp. Factor | Aspect Ratio |
+----------------------+---------------+--------------+--------------+
| | Minimum [deg] | Maximum | Maximum |
+----------------------+---------------+--------------+--------------+
| Default Domain | 67.5 OK | 3 OK | 4 OK |
+----------------------+---------------+--------------+--------------+
| | %! %ok %OK | %! %ok %OK | %! %ok %OK |
+----------------------+---------------+--------------+--------------+
| Default Domain | 0 0 100 | 0 0 100 | 0 0 100 |
+----------------------+---------------+--------------+--------------+

Domain Name : Default Domain

Total Number of Nodes = 3905

Total Number of Elements = 3200
Total Number of Prisms = 40
Total Number of Hexahedrons = 3160

Total Number of Faces = 1380

+--------------------------------------------------------------------+
| Buoyancy Reference Information |
+--------------------------------------------------------------------+

Domain Group: Default Domain

Buoyancy has been activated. The absolute pressure will include
hydrostatic pressure contribution, using the following reference
coordinates: ( 2.91154E-01, 1.00000E+01, 3.73309E-02).

+--------------------------------------------------------------------+
| Initial Conditions Supplied by Fields in the Input Files |
+--------------------------------------------------------------------+

Domain Name : Default Domain
Mesh Coordinates

+--------------------------------------------------------------------+
| Average Scale Information |
+--------------------------------------------------------------------+

Domain Name : Default Domain
Global Length = 1.4285E+01
Minimum Extent = 1.0000E+01
Maximum Extent = 1.7970E+01
water.Density = 9.9700E+02
water.Dynamic Viscosity = 8.8990E-04
water.Velocity = 0.0000E+00
water.Mass (Conservative) = 2.6155E+06
water.Mass (Normalised) = 2.6155E+06
water.Volume = 2.6233E+03
water.Volume Fraction = 9.0000E-01
air.Density = 1.1850E+00
air.Dynamic Viscosity = 1.8310E-05
air.Velocity = 0.0000E+00
air.Mass (Conservative) = 3.4541E+02
air.Mass (Normalised) = 3.4541E+02
air.Volume = 2.9148E+02
air.Volume Fraction = 1.0000E-01
Wave Speed = 1.1836E+01
Froude Number = 0.0000E+00

+--------------------------------------------------------------------+
| Boundary Condition Data Supplied by External Solver Coupling |
+--------------------------------------------------------------------+

ANSYS Multi-field Solver : ANSYS
CFX Boundary : interface
CFX Variable : Total Mesh Displacement
ANSYS Interface : 1
ANSYS Variable : DISP

+--------------------------------------------------------------------+
| Checking for Isolated Fluid Regions |
+--------------------------------------------------------------------+

No isolated fluid regions were found.

+--------------------------------------------------------------------+
| The Equations Solved in This Calculation |
+--------------------------------------------------------------------+

Subsystem : Mesh Displacement

X-Disp
Y-Disp
Z-Disp

Subsystem : Momentum and Mass

U-Mom-Bulk
V-Mom-Bulk
W-Mom-Bulk
VF-Constraint
Mass-water
Mass-air

Subsystem : TurbKE and Diss.K

K-TurbKE-Bulk
E-Diss.K-Bulk

CFD Solver started: Fri Aug 16 22:24:53 2013


+--------------------------------------------------------------------+
| Convergence History |
+--------------------------------------------------------------------+


================================================== ====================
| Timestepping Information |
----------------------------------------------------------------------
| Timestep | RMS Courant Number | Max Courant Number |
+----------------------+----------------------+----------------------+
| 1.0000E-02 | 0.00 | 0.00 |
----------------------------------------------------------------------

================================================== ====================
TIME STEP = 1 SIMULATION TIME = 1.0000E-02 CPU SECONDS = 3.627E+00
----------------------------------------------------------------------
| COUPLING/STAGGER ITERATION = 1 |
----------------------------------------------------------------------
| SOLVING : Mesh Displacement |
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| X-Disp | 0.00 | 0.0E+00 | 0.0E+00 | 0.0E+00 OK|
| Y-Disp | 0.00 | 0.0E+00 | 0.0E+00 | 0.0E+00 OK|
| Z-Disp | 0.00 | 0.0E+00 | 0.0E+00 | 10.6 0.0E+00 OK|
+----------------------+------+---------+---------+------------------+
+--------------------------------------------------------------------+
| Mesh Statistics |
+--------------------------------------------------------------------+
| Domain Name | Orthog. Angle | Exp. Factor | Aspect Ratio |
+----------------------+---------------+--------------+--------------+
| | Minimum [deg] | Maximum | Maximum |
+----------------------+---------------+--------------+--------------+
| Default Domain | 67.5 OK | 3 OK | 4 OK |
+----------------------+---------------+--------------+--------------+
| | %! %ok %OK | %! %ok %OK | %! %ok %OK |
+----------------------+---------------+--------------+--------------+
| Default Domain | 0 0 100 | 0 0 100 | 0 0 100 |
+----------------------+---------------+--------------+--------------+
----------------------------------------------------------------------
COEFFICIENT LOOP ITERATION = 1 CPU SECONDS = 3.774E+00
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom-Bulk | 0.00 | 0.0E+00 | 0.0E+00 | 0.0E+00 OK|
| V-Mom-Bulk | 0.00 | 1.9E-02 | 6.2E-02 | 1.2E-02 ok|
| W-Mom-Bulk | 0.00 | 0.0E+00 | 0.0E+00 | 0.0E+00 OK|
| Mass-water | 0.00 | 1.3E-04 | 4.6E-04 | 5.7E-01 ok|
| Mass-air | 0.00 | 1.2E-04 | 3.8E-04 | 8.6 3.3E+00 F |
+----------------------+------+---------+---------+------------------+
| K-TurbKE-Bulk | 0.00 | 3.1E-02 | 9.8E-01 | 11.2 2.3E-08 OK|
| E-Diss.K-Bulk | 0.00 | 2.2E-02 | 1.0E+00 | 9.4 2.8E-08 OK|
+----------------------+------+---------+---------+------------------+
----------------------------------------------------------------------
COEFFICIENT LOOP ITERATION = 2 CPU SECONDS = 4.531E+00
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom-Bulk | 0.00 | 1.2E-03 | 4.3E-02 | 4.5E+01 F |
| V-Mom-Bulk | 0.02 | 3.4E-04 | 1.2E-02 | 8.6E+00 F |
| W-Mom-Bulk | 0.00 | 2.1E-03 | 1.1E-01 | 4.5E+01 F |
| Mass-water | 0.02 | 2.3E-06 | 6.6E-05 | 1.6E+01 F |
| Mass-air | 0.02 | 1.9E-06 | 4.4E-05 | 8.6 2.5E+01 F |
+----------------------+------+---------+---------+------------------+
| K-TurbKE-Bulk | 0.83 | 2.5E-02 | 7.2E-01 | 11.0 4.2E-08 OK|
| E-Diss.K-Bulk | 0.76 | 1.7E-02 | 1.0E+00 | 9.4 5.0E-07 OK|
+----------------------+------+---------+---------+------------------+
----------------------------------------------------------------------
COEFFICIENT LOOP ITERATION = 3 CPU SECONDS = 5.079E+00
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom-Bulk |13.10 | 1.5E-02 | 4.5E-01 | 6.2E-03 OK|
| V-Mom-Bulk |29.20 | 1.0E-02 | 3.9E-01 | 1.3E-03 OK|
| W-Mom-Bulk | 7.86 | 1.6E-02 | 4.6E-01 | 1.3E-03 OK|
| Mass-water |99.99 | 9.5E-04 | 3.5E-02 | 4.3E-01 ok|
| Mass-air |99.99 | 1.2E-03 | 5.2E-02 | 16.3 1.2E+00 F |
+----------------------+------+---------+---------+------------------+
| K-TurbKE-Bulk | 0.27 | 6.8E-03 | 4.0E-01 | 10.2 9.9E-02 OK|
| E-Diss.K-Bulk | 2.52 | 4.3E-02 | 1.0E+00 | 17.3 3.2E-02 OK|
+----------------------+------+---------+---------+------------------+
----------------------------------------------------------------------
| COUPLING/STAGGER ITERATION = 2 |
----------------------------------------------------------------------
| SOLVING : Mesh Displacement |
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| X-Disp | 0.00 | 9.5E-04 | 8.6E-03 | 2.2E-08 OK|
| Y-Disp | 0.00 | 7.1E-04 | 4.9E-03 | 2.1E-08 OK|
| Z-Disp | 0.00 | 2.9E-03 | 2.4E-02 | 10.6 2.2E-08 OK|
+----------------------+------+---------+---------+------------------+
| X-Disp | 0.04 | 4.1E-05 | 5.2E-04 | 4.4E-05 OK|
| Y-Disp | 0.07 | 4.8E-05 | 4.2E-04 | 3.1E-06 OK|
| Z-Disp | 0.05 | 1.3E-04 | 1.7E-03 | 10.6 5.3E-05 OK|
+----------------------+------+---------+---------+------------------+
| X-Disp | 0.23 | 9.5E-06 | 9.8E-05 | 9.3E-05 OK|
| Y-Disp | 0.26 | 1.3E-05 | 1.4E-04 | 1.6E-05 OK|
| Z-Disp | 0.24 | 3.0E-05 | 3.0E-04 | 10.6 3.3E-04 OK|
+----------------------+------+---------+---------+------------------+
+--------------------------------------------------------------------+
| Mesh Statistics |
+--------------------------------------------------------------------+
| Domain Name | Orthog. Angle | Exp. Factor | Aspect Ratio |
+----------------------+---------------+--------------+--------------+
| | Minimum [deg] | Maximum | Maximum |
+----------------------+---------------+--------------+--------------+
| Default Domain | 67.5 OK | 3 OK | 4 OK |
+----------------------+---------------+--------------+--------------+
| | %! %ok %OK | %! %ok %OK | %! %ok %OK |
+----------------------+---------------+--------------+--------------+
| Default Domain | 0 0 100 | 0 0 100 | 0 0 100 |
+----------------------+---------------+--------------+--------------+
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Old   August 16, 2013, 22:41
Default
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----------------------------------------------------------------------
COEFFICIENT LOOP ITERATION = 4 CPU SECONDS = 6.412E+00
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom-Bulk | 2.02 | 3.1E-02 | 9.0E-01 | 7.8E-01 ok|
| V-Mom-Bulk | 1.08 | 1.1E-02 | 4.4E-01 | 1.8E-01 ok|
| W-Mom-Bulk | 2.51 | 4.1E-02 | 1.4E+00 | 4.2E-01 ok|
| Mass-water | 0.15 | 1.4E-04 | 6.0E-03 | 9.6E-01 ok|
| Mass-air | 0.11 | 1.3E-04 | 5.7E-03 | 8.6 6.0E-01 ok|
+----------------------+------+---------+---------+------------------+
| K-TurbKE-Bulk | 9.66 | 6.6E-02 | 8.1E-01 | 10.3 3.1E-08 OK|
| E-Diss.K-Bulk | 1.01 | 4.3E-02 | 7.3E-01 | 17.5 3.0E-08 OK|
+----------------------+------+---------+---------+------------------+
----------------------------------------------------------------------
COEFFICIENT LOOP ITERATION = 5 CPU SECONDS = 6.996E+00
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom-Bulk | 0.03 | 9.1E-04 | 1.8E-02 | 7.6E+00 F |
| V-Mom-Bulk | 0.04 | 4.1E-04 | 1.0E-02 | 4.6E-01 ok|
| W-Mom-Bulk | 0.02 | 1.0E-03 | 2.6E-02 | 1.4E+01 F |
| Mass-water | 0.00 | 4.9E-07 | 1.2E-05 | 4.4E+00 F |
| Mass-air | 0.00 | 2.0E-07 | 8.0E-06 | 8.6 3.6E+01 F |
+----------------------+------+---------+---------+------------------+
| K-TurbKE-Bulk | 0.45 | 2.9E-02 | 7.2E-01 | 10.7 7.1E-06 OK|
| E-Diss.K-Bulk | 0.52 | 2.2E-02 | 1.0E+00 |100.3 7.8E-08 OK|
+----------------------+------+---------+---------+------------------+
----------------------------------------------------------------------
COEFFICIENT LOOP ITERATION = 6 CPU SECONDS = 7.577E+00
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom-Bulk |23.29 | 2.1E-02 | 6.9E-01 | 2.6E-03 OK|
| V-Mom-Bulk |29.12 | 1.2E-02 | 5.8E-01 | 7.0E-04 OK|
| W-Mom-Bulk |23.57 | 2.4E-02 | 6.2E-01 | 2.5E-03 OK|
| Mass-water |99.99 | 1.5E-03 | 5.6E-02 | 4.0E-02 ok|
| Mass-air |99.99 | 9.6E-04 | 3.9E-02 | 12.5 2.2E-01 ok|
+----------------------+------+---------+---------+------------------+
| K-TurbKE-Bulk | 0.38 | 1.1E-02 | 5.4E-01 | 10.7 5.1E-05 OK|
| E-Diss.K-Bulk | 1.63 | 3.6E-02 | 9.9E-01 | 9.3 1.9E-03 OK|
+----------------------+------+---------+---------+------------------+
----------------------------------------------------------------------
| COUPLING/STAGGER ITERATION = 3 |
----------------------------------------------------------------------
| SOLVING : Mesh Displacement |
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| X-Disp |75.06 | 7.1E-02 | 6.7E-01 | 2.1E-08 OK|
| Y-Disp |37.82 | 2.7E-02 | 2.4E-01 | 2.3E-08 OK|
| Z-Disp |13.42 | 3.8E-02 | 3.8E-01 | 10.6 2.6E-08 OK|
+----------------------+------+---------+---------+------------------+
| X-Disp | 0.04 | 2.9E-03 | 3.6E-02 | 3.3E-05 OK|
| Y-Disp | 0.07 | 1.8E-03 | 1.9E-02 | 2.4E-06 OK|
| Z-Disp | 0.04 | 1.6E-03 | 2.4E-02 | 10.6 3.8E-06 OK|
+----------------------+------+---------+---------+------------------+
| X-Disp | 0.23 | 6.7E-04 | 7.1E-03 | 5.3E-05 OK|
| Y-Disp | 0.31 | 5.4E-04 | 6.3E-03 | 1.7E-05 OK|
| Z-Disp | 0.19 | 2.9E-04 | 2.5E-03 | 10.6 1.8E-05 OK|
+----------------------+------+---------+---------+------------------+
| X-Disp | 0.15 | 9.8E-05 | 1.2E-03 | 4.0E-04 OK|
| Y-Disp | 0.14 | 7.8E-05 | 1.1E-03 | 2.9E-05 OK|
| Z-Disp | 0.16 | 4.8E-05 | 5.1E-04 | 10.6 1.4E-04 OK|
+----------------------+------+---------+---------+------------------+
+--------------------------------------------------------------------+
| Mesh Statistics |
+--------------------------------------------------------------------+
| Domain Name | Orthog. Angle | Exp. Factor | Aspect Ratio |
+----------------------+---------------+--------------+--------------+
| | Minimum [deg] | Maximum | Maximum |
+----------------------+---------------+--------------+--------------+
| Default Domain | 67.4 OK | 4 OK | 5 OK |
+----------------------+---------------+--------------+--------------+
| | %! %ok %OK | %! %ok %OK | %! %ok %OK |
+----------------------+---------------+--------------+--------------+
| Default Domain | 0 0 100 | 0 0 100 | 0 0 100 |
+----------------------+---------------+--------------+--------------+
----------------------------------------------------------------------
COEFFICIENT LOOP ITERATION = 7 CPU SECONDS = 9.274E+00
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom-Bulk | 1.72 | 3.6E-02 | 1.1E+00 | 2.2E-04 OK|
| V-Mom-Bulk | 1.61 | 1.9E-02 | 7.8E-01 | 3.6E-04 OK|
| W-Mom-Bulk | 1.86 | 4.4E-02 | 1.7E+00 | 1.6E-04 OK|
| Mass-water | 3.65 | 5.5E-03 | 1.8E-01 | 5.4E-03 OK|
| Mass-air | 5.34 | 5.1E-03 | 1.3E-01 | 16.3 1.1E-03 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE-Bulk | 6.64 | 7.4E-02 | 2.1E+00 | 10.3 8.6E-05 OK|
| E-Diss.K-Bulk | 2.32 | 8.5E-02 | 2.7E+00 | 17.5 4.9E-06 OK|
+----------------------+------+---------+---------+------------------+
----------------------------------------------------------------------
COEFFICIENT LOOP ITERATION = 8 CPU SECONDS = 9.857E+00
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom-Bulk | 1.38 | 5.0E-02 | 1.9E+00 | 8.2E-04 OK|
| V-Mom-Bulk | 2.08 | 4.0E-02 | 1.7E+00 | 7.1E-04 OK|
| W-Mom-Bulk | 1.24 | 5.5E-02 | 2.8E+00 | 8.1E-04 OK|
| Mass-water | 1.61 | 9.0E-03 | 2.5E-01 | 3.4E-03 OK|
| Mass-air | 2.01 | 1.0E-02 | 2.9E-01 | 12.4 1.3E-03 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE-Bulk | 0.51 | 3.8E-02 | 5.0E-01 | 10.1 1.7E-03 OK|
| E-Diss.K-Bulk | 0.45 | 3.8E-02 | 9.7E-01 | 17.5 3.8E-05 OK|
+----------------------+------+---------+---------+------------------+
----------------------------------------------------------------------
COEFFICIENT LOOP ITERATION = 9 CPU SECONDS = 1.042E+01
----------------------------------------------------------------------
| Equation | Rate | RMS Res | Max Res | Linear Solution |
+----------------------+------+---------+---------+------------------+
| U-Mom-Bulk | 0.65 | 3.3E-02 | 6.1E-01 | 7.7E-04 OK|
| V-Mom-Bulk | 0.97 | 3.9E-02 | 6.8E-01 | 8.1E-04 OK|
| W-Mom-Bulk | 1.07 | 5.8E-02 | 2.5E+00 | 6.4E-04 OK|
| Mass-water | 0.37 | 3.3E-03 | 6.7E-02 | 4.4E-03 OK|
| Mass-air | 0.40 | 4.1E-03 | 8.7E-02 | 12.5 4.5E-04 OK|
+----------------------+------+---------+---------+------------------+
| K-TurbKE-Bulk | 0.91 | 3.4E-02 | 6.0E-01 | 10.0 2.0E-04 OK|
| E-Diss.K-Bulk | 1.02 | 3.9E-02 | 1.7E+00 | 17.4 4.1E-06 OK|
+----------------------+------+---------+---------+------------------+

+--------------------------------------------------------------------+
| ERROR #001100279 has occurred in subroutine ErrAction. |
| Message: |
| CFX encountered the error: Read. Fatal error occurred when reque- |
| sting Total Mesh Displacement for interface. |
| |
| |
| |
| |
+--------------------------------------------------------------------+

+--------------------------------------------------------------------+
| ERROR #001100279 has occurred in subroutine ErrAction. |
| Message: |
| cplg_SendCommand failed to send the command: ERROR -- CFX encount- |
| ered the error: Read. Fatal error occurred when requesting Total |
| Mesh Displacement for interface. |
| |
| |
| |
+--------------------------------------------------------------------+

+--------------------------------------------------------------------+
| Writing crash recovery file |
+--------------------------------------------------------------------+

+--------------------------------------------------------------------+
| ERROR #001100279 has occurred in subroutine ErrAction. |
| Message: |
| Stopped in routine cplg_SendCommand |
| |
| |
| |
| |
| |
+--------------------------------------------------------------------+

+--------------------------------------------------------------------+
| An error has occurred in cfx5solve: |
| |
| The ANSYS CFX solver exited with return code 1. No results file |
| has been created. |
+--------------------------------------------------------------------+

End of solution stage.

+--------------------------------------------------------------------+
| An error has occurred in cfx5solve: |
| |
| ANSYS Solver terminated with return code 256 |
+--------------------------------------------------------------------+


+--------------------------------------------------------------------+
| The results from this run of the ANSYS solver have been written to |
| C:\Users\amir\Desktop\work\01_pending_tasks\dp0_CF X_Solution_1\Fl- |
| uid Flow CFX_001.ansys |
+--------------------------------------------------------------------+


+--------------------------------------------------------------------+
| Warning! |
| |
| The ANSYS CFX Solver has written a crash recovery file. This file |
| has been saved as |
| C:/Users/amir/Desktop/work/01_pending_tasks/dp0_CFX_Solution_1/Fl- |
| uid Flow CFX_001.res.err and may be an aid to diagnosing the |
| problem or restarting the run. More details should be available |
| in the solver output section of the output file. |
+--------------------------------------------------------------------+


+--------------------------------------------------------------------+
| The following user files have been saved in the directory |
| C:/Users/amir/Desktop/work/01_pending_tasks/dp0_CFX_Solution_1/Fl- |
| uid Flow CFX_001: |
| |
| mon |
+--------------------------------------------------------------------+


This run of the ANSYS CFX Solver has finished.
mhabibnia is offline   Reply With Quote

Old   August 19, 2013, 03:53
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Quote:
Originally Posted by mhabibnia View Post

+--------------------------------------------------------------------+
| ERROR #001100279 has occurred in subroutine ErrAction. |
| Message: |
| cplg_SendCommand failed to send the command: ERROR -- CFX encount- |
| ered the error: Read. Fatal error occurred when requesting Total |
| Mesh Displacement for interface. |
| |
| |
| |
+--------------------------------------------------------------------+
See the output from the structural solver, it has crashed and CFX cannot get the displacements.
Lance is offline   Reply With Quote

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