[nammeh]

Hello, I've had issues with a project I'm working on and was wondering if someone could help me out. Below is the code from the solver.

"C:\Program Files\ANSYS Inc\ANSYS Student\v191\CFX\bin\perllib\cfx5solve.pl"
-batch -ccl runInput.ccl -fullname "Fluid Flow CFX_020"

Release 19.1

Point Releases and Patches installed:
Academic Student Release 19.1

Setting up CFX Solver run ...

Deleted /SIMULATION CONTROL/EXECUTION CONTROL/SOLVER STEP
CONTROL/PARALLEL ENVIRONMENT/Number of Processes since we are in
Distributed Parallel mode.


+--------------------------------------------------------------------+
| |
| 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 = B3344, B3778, B4256, B4286
BOUNDARY: Domain Interface 1 Side 1
Boundary Type = INTERFACE
(locations cut for character length)
BOUNDARY CONDITIONS:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: Domain Interface 1 Side 2
Boundary Type = INTERFACE
Location = F4223.4256
BOUNDARY CONDITIONS:
MASS AND MOMENTUM:
Option = Conservative Interface Flux
END
TURBULENCE:
Option = Conservative Interface Flux
END
END
END
BOUNDARY: Inlet
Boundary Type = INLET
Location = Inlet
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
MASS AND MOMENTUM:
Normal Speed = 150 [mile hr^-1]
Option = Normal Speed
END
TURBULENCE:
Option = Low 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:
Normal Speed = 150 [mile hr^-1]
Option = Normal Speed
END
END
END
BOUNDARY: Walls
Boundary Type = WALL
Location = Walls
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 = k epsilon
END
TURBULENT WALL FUNCTIONS:
Option = Scalable
END
END
END
DOMAIN INTERFACE: Domain Interface 1
Boundary List1 = Domain Interface 1 Side 1
Boundary List2 = Domain Interface 1 Side 2
Interface Type = Fluid Fluid
INTERFACE MODELS:
Option = General Connection
FRAME CHANGE:
Option = None
END
MASS AND MOMENTUM:
Option = Conservative Interface Flux
MOMENTUM INTERFACE MODEL:
Option = None
END
END
PITCH CHANGE:
Option = None
END
END
MESH CONNECTION:
Option = GGI
INTERSECTION CONTROL:
Option = Direct
Permit No Intersection = On
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 = 1000
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 = 19.1
Results Version = 19.1
END
SIMULATION CONTROL:
EXECUTION CONTROL:
EXECUTABLE SELECTION:
Double Precision = Yes
Large Problem = Yes
END
INTERPOLATOR STEP CONTROL:
Runtime Priority = High
MEMORY CONTROL:
Catalogue Size Override = 150x
Character Memory Override = 150x
Double Precision Memory Override = 150x
Integer Memory Override = 150x
Logical Memory Override = 150x
Memory Allocation Factor = 10
Real Memory Override = 150x
END
END
PARALLEL HOST LIBRARY:
HOST DEFINITION: desktop3f44f7g
Remote Host Name = DESKTOP-3F44F7G
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 = 2
END
PARTITION SMOOTHING:
Maximum Partition Smoothing Sweeps = 100
Option = Smooth
END
PARTITIONING TYPE:
MeTiS Type = k-way
Option = MeTiS
Partition Size Rule = Automatic
Partition Weight Factors = 0.16667, 0.16667, 0.16667, 0.16667, \
0.16667, 0.16667
END
END
RUN DEFINITION:
Run Mode = Full
Solver Input File = Fluid Flow CFX.def
Solver Results File = C:/Users/dahlm/Downloads/Musco Lighting \
Project/Musco_pending/dp0_CFX_Solution/Fluid Flow CFX_020.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 = Fluid Flow CFX_002.res
END
END
END
SOLVER STEP CONTROL:
Runtime Priority = Standard
MEMORY CONTROL:
Memory Allocation Factor = 2
END
PARALLEL ENVIRONMENT:
Parallel Host List = desktop3f44f7g*6
Start Method = Intel MPI Distributed Parallel
END
END
END
END


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




+--------------------------------------------------------------------+
| |
| ANSYS(R) CFX(R) Interpolator |
| |
| Release 19.1 |
| Build 19.1 2018-04-17T13:27:50.069000 |
| Tue Apr 17 15:35:43 GMTDT 2018 |
| |
| Executable Attributes |
| |
| double-64bit-int64-archfort-optimised-std-lcomp |
| |
| (C) 1996-2018 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: DESKTOP-3F44F7G (PID:2396)

Job started: Tue Mar 26 11:45:13 2019


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

| Real | Integer | Character | Logical | Double
----------+------------+------------+-----------+----------+----------
Mwords | 408.03 | 532.18 | 4500.00 | 225.00 | 23.46
Mbytes | 3113.01 | 4060.20 | 4291.53 | 1716.61 | 179.01
----------+------------+------------+-----------+----------+----------


+--------------------------------------------------------------------+
| Host Memory Information (Mbytes) |
+--------------------------------------------------------------------+
| Host | System | Allocated | % |
+-------------------------+----------------+----------------+--------+
| DESKTOP-3F44F7G | 16328.96 | 13360.37 | 81.82 |
+-------------------------+----------------+----------------+--------+

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

Total Number of Nodes in the Target Domain = 52007
Bounding Box Volume of the Target Mesh = 3.13162E+01


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 | 1.19E+00 | 1.19E+00 |
| Isolated Volumes | 1.00E+00 | 4.00E+00 |
| Static Entropy | 0.00E+00 | 0.00E+00 |
| Pressure.Gradient | 0.00E+00 | 0.00E+00 |
| Velocity u.Gradient | 0.00E+00 | 0.00E+00 |
| Velocity v.Gradient | 0.00E+00 | 0.00E+00 |
| Velocity w.Gradient | 0.00E+00 | 1.56E-11 |
| Pressure | 0.00E+00 | 0.00E+00 |
| Specific Heat Capacity at Constant Pressure| 1.00E+03 | 1.00E+03 |
| Turbulence Eddy Dissipation | 1.66E+05 | 1.66E+05 |
| Temperature | 2.98E+02 | 2.98E+02 |
| Turbulence Kinetic Energy | 1.69E+01 | 1.69E+01 |
| Velocity | 6.71E+01 | 6.71E+01 |
| Dynamic Viscosity | 1.83E-05 | 1.83E-05 |
| Eddy Viscosity | 1.83E-04 | 1.83E-04 |

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

+================================================= ===================+
| ****** 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\ANSYS |
| Student\v191\CFX\bin\winnt-amd64\double-int64\solver-mpi.exe |
| exited with return code 1. |
+--------------------------------------------------------------------+


+--------------------------------------------------------------------+
| The following user files have been saved in the directory |
| C:/Users/dahlm/Downloads/Musco Lighting |
| Project/Musco_pending/dp0_CFX_Solution/Fluid Flow CFX_020: |
| |
| job |
+--------------------------------------------------------------------+


+--------------------------------------------------------------------+
| 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.

I've seen several posts on similar topics and a lot of those were resolved through increasing the interpolator memory allocation factor and the catalog size, and I've tried increasing every aspect of the interpolator memory tab and still had no results. Any help would be massively appreciated. Thank you

[Opaque]

The error says:

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

Trying to allocate memory with a size of 0.

You may need to contact ANSYS CFX for support

Separately, the message also says "Copying data .." which may indicate you are using the same mesh between both simulations. In such case, you may try bypassing the interpolation step

cfx5solve -def <mycase>.def -ini <previous results>.res ....

or modify your solver manager setup such as

Use Mesh From = Initial Values
Continue History From = Workbench Initial Values

instead of Solver Input File