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July 24, 2023 at 7:58 pmFarouk SanniSubscriber
Hello everyone,
Whenever I try to run a simulation, I get an Error that says "An unknown error occurred during solution,Check the solver output on the solution. Project > Model > Static Structural > Solution"
I have seen previous topics about the particular type of error but the solutions did not work for me. How do I resolve this?
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July 25, 2023 at 4:12 amVJAnsys Employee
What is written in the solve.out file? Please share the output.Â
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July 26, 2023 at 1:15 amFarouk SanniSubscriber
Hello VJ, I do not know how to share the solve out file here so Im attaching a link to it. Kindly Find it here
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July 26, 2023 at 1:36 amVJAnsys Employee
Sorry, we cannot download any files from the forum. Please paste it in the comments.
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July 26, 2023 at 4:35 pmFarouk SanniSubscriber
ANSYS Multiphysics                Â
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     *****  ANSYS COMMAND LINE ARGUMENTS  *****
 BATCH MODE REQUESTED (-b)   = NOLIST
 INPUT FILE COPY MODE (-c)   = COPY
 DISTRIBUTED MEMORY PARALLEL REQUESTED
    4 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS
  TOTAL OF   4 CORES REQUESTED
 INPUT FILE NAME        = C:\Users\Yakuba\AppData\Local\Temp\WB_FARSAN_Yakub_10084_2\_ProjectScratch\Scr8F73\dummy.dat
 OUTPUT FILE NAME       = C:\Users\Yakuba\AppData\Local\Temp\WB_FARSAN_Yakub_10084_2\_ProjectScratch\Scr8F73\solve.out
 START-UP FILE MODE      = NOREAD
 STOP FILE MODE        = NOREAD RELEASE= Release 16.0     BUILD= 16.0    UP20141203  VERSION=WINDOWS x64Â
 CURRENT JOBNAME=file0  16:13:18  JUL 23, 2023 CP=    1.500
 PARAMETER _DS_PROGRESS =   999.0000000  Â /INPUT FILE= ds.dat  LINE=    0
Â
 *** NOTE ***               CP =    2.609  TIME= 16:13:21
 The /CONFIG,NOELDB command is not valid in a Distributed ANSYS     Â
 solution.  Command is ignored.                     Â *GET  _WALLSTRT  FROM  ACTI  ITEM=TIME WALL  VALUE=  16.2225000  Â
 TITLE=Â
 unsaved_project--Static Structural (A5)                    Â
 SET PARAMETER DIMENSIONS ON  _WB_PROJECTSCRATCH_DIR
 TYPE=STRI  DIMENSIONS=    248     1     1 PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\Yakuba\AppData\Local\Temp\WB_FARSAN_Yakub_10084_2\_ProjectScratch\Scr8F73\
 SET PARAMETER DIMENSIONS ON  _WB_SOLVERFILES_DIR
 TYPE=STRI  DIMENSIONS=    248     1     1 PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\Yakuba\AppData\Local\Temp\WB_FARSAN_Yakub_10084_2\unsaved_project_files\dp0\SYS\MECH\
 SET PARAMETER DIMENSIONS ON  _WB_USERFILES_DIR
 TYPE=STRI  DIMENSIONS=    248     1     1 PARAMETER _WB_USERFILES_DIR(1) = C:\Users\Yakuba\AppData\Local\Temp\WB_FARSAN_Yakub_10084_2\unsaved_project_files\user_files\
 --- Data in consistent MKS units. See Solving Units in the help system for more MKS UNITS SPECIFIED FOR INTERNAL  Â
 LENGTH     (l)  = METER (M)
 MASS      (M)  = KILOGRAM (KG)
 TIME      (t)  = SECOND (SEC)
 TEMPERATURE  (T)  = CELSIUS (C)
 TOFFSET       = 273.0
 CHARGE     (Q)  = COULOMB
 FORCE     (f)  = NEWTON (N) (KG-M/SEC2)
 HEAT        = JOULE (N-M) PRESSURE      = PASCAL (NEWTON/M**2)
 ENERGY     (W)  = JOULE (N-M)
 POWER     (P)  = WATT (N-M/SEC)
 CURRENT    (i)  = AMPERE (COULOMBS/SEC)
 CAPACITANCE  (C)  = FARAD
 INDUCTANCE   (L)  = HENRY
 MAGNETIC FLUX    = WEBER
 RESISTANCE   (R)  = OHM
 ELECTRIC POTENTIAL = VOLT INPUT  UNITS ARE ALSO SET TO MKSÂ
 *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE Release 16.0   16.0   ***
 DISTRIBUTED ANSYS Multiphysics                Â 00000000  VERSION=WINDOWS x64  16:13:21  JUL 23, 2023 CP=    2.625
 unsaved_project--Static Structural (A5)                    Â
Â
     ***** ANSYS ANALYSIS DEFINITION (PREP7) *****
 *********** Nodes for the whole assembly ***********
 *********** Elements for Body 1 "Solid" ***********
 *********** Send User Defined Coordinate System(s) ***********
 *********** Set Reference Temperature ***********
 *********** Send Materials ***********
 *********** Fixed Supports ***********
 *********** Define Force Using Surface Effect Elements ***********
 ***** ROUTINE COMPLETED *****  CP =     3.734
 --- Number of total nodes = 1066
 --- Number of contact elements = 4
 --- Number of spring elements = 0
 --- Number of bearing elements = 0
 --- Number of solid elements = 458
 --- Number of total elements = 462 *GET  _WALLBSOL  FROM  ACTI  ITEM=TIME WALL  VALUE=  16.2233333  Â
 ****************************************************************************
 *************************   SOLUTION    ********************************
 **************************************************************************** *****  ANSYS SOLUTION ROUTINE  *****
 PERFORM A STATIC ANALYSIS
 THIS WILL BE A NEW ANALYSIS USE SPARSE MATRIX DIRECT SOLVER
 CONTACT INFORMATION PRINTOUT LEVEL    1
 DO NOT COMBINE ELEMENT MATRIX FILES (.emat) AFTER DISTRIBUTED PARALLEL SOLUTION
 DO NOT COMBINE ELEMENT SAVE DATA FILES (.esav) AFTER DISTRIBUTED PARALLEL SOLUTION
 NLDIAG: Nonlinear diagnostics CONT option is set to ON.Â
     Writing frequency : each ITERATION. DO NOT SAVE ANY RESTART FILES AT ALL
 ****************************************************
 ******************* SOLVE FOR LS 1 **************** SELECT    FOR ITEM=TYPE COMPONENT=  Â
 IN RANGE     2 TO      2 STEP      1     4  ELEMENTS (OF     462  DEFINED) SELECTED BY  ESEL  COMMAND.
 SELECT    ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.
    15 NODES (OF   1066  DEFINED) SELECTED FROM
    4 SELECTED ELEMENTS BY NSLE COMMAND. SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1  KVAL = 1
   SET ACCORDING TO TABLE PARAMETER = _LOADVARI27X          Â SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  2  KVAL = 1
   SET ACCORDING TO TABLE PARAMETER = _LOADVARI27Y          Â SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  3  KVAL = 1
   SET ACCORDING TO TABLE PARAMETER = _LOADVARI27Z          Â ALL SELECT  FOR ITEM=NODE COMPONENT=  Â
 IN RANGE     1 TO    1066 STEP      1    1066  NODES (OF    1066  DEFINED) SELECTED BY NSEL  COMMAND.
 ALL SELECT  FOR ITEM=ELEM COMPONENT=  Â
 IN RANGE     1 TO     462 STEP      1    462  ELEMENTS (OF     462  DEFINED) SELECTED BY  ESEL  COMMAND.
 PRINTOUT RESUMED BY /GOP
 USE    1 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL  DEGREES OF FREEDOM
 FOR AUTOMATIC TIME STEPPING:
  USE    1 SUBSTEPS AS A MAXIMUM
  USE    1 SUBSTEPS AS A MINIMUM TIME=  1.0000  Â
 ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
 WRITE ALL  ITEMS TO THE DATABASE WITH A FREQUENCY OF NONE
  FOR ALL APPLICABLE ENTITIES WRITE NSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALLÂ
  FOR ALL APPLICABLE ENTITIES WRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALLÂ
  FOR ALL APPLICABLE ENTITIES WRITE STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALLÂ
  FOR ALL APPLICABLE ENTITIES WRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALLÂ
  FOR ALL APPLICABLE ENTITIES WRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALLÂ
  FOR ALL APPLICABLE ENTITIES NONLINEAR STABILIZATION CONTROL:
 KEY=OFFÂ
 *GET  ANSINTER_  FROM  ACTI  ITEM=INT     VALUE=  0.00000000  Â *IF  ANSINTER_             ( =  0.00000   )  NE Â
   0                 ( =  0.00000   )  THEN  Â *ENDIF
 *****  ANSYS SOLVE   COMMAND  *****
 *** WARNING ***             CP =    4.641  TIME= 16:13:25
 Element shape checking is currently inactive.  Issue SHPP,ON or     Â
 SHPP,WARN to reactivate, if desired.                  Â *** NOTE ***               CP =    4.656  TIME= 16:13:25
 The model data was checked and warning messages were found.       Â
 Please review output or errors file (                 Â
 C:\Users\Yakuba\AppData\Local\Temp\WB_FARSAN_Yakub_10084_2\_ProjectScraÂ
 atch\Scr8F73\file0.err ) for these warning messages.          Â *** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
   --- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS --- ELEMENT TYPE   1 IS SOLID187. IT IS NOT ASSOCIATED WITH FULLY INCOMPRESSIBLE
 HYPERELASTIC MATERIALS. NO SUGGESTION IS AVAILABLE AND NO RESETTING IS NEEDED.Â
 *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE Release 16.0   16.0   ***
 DISTRIBUTED ANSYS Multiphysics                Â 00000000  VERSION=WINDOWS x64  16:13:25  JUL 23, 2023 CP=    4.672
 unsaved_project--Static Structural (A5)                    Â
Â
            S O L U T I O N  O P T I O N S
  PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D         Â
  DEGREES OF FREEDOM. . . . . . UX  UY  UZ Â
  ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
  OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . .  273.15  Â
  EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE       Â
  GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC  *** WARNING ***             CP =    4.688  TIME= 16:13:25
 Material number 2 (used by element 459 ) should normally have at least Â
 one MP or one TB type command associated with it.  Output of energy by Â
 material may not be available.                     Â *** NOTE ***               CP =    4.688  TIME= 16:13:25
 The step data was checked and warning messages were found.       Â
 Please review output or errors file (                 Â
 C:\Users\Yakuba\AppData\Local\Temp\WB_FARSAN_Yakub_10084_2\_ProjectScraÂ
 atch\Scr8F73\file0.err ) for these warning messages.          Â *** NOTE ***               CP =    4.688  TIME= 16:13:25
 The conditions for direct assembly have been met.  No .emat or .erot  Â
 files will be produced.                         Â Â
 Â
   D I S T R I B U T E D  D O M A I N  D E C O M P O S E R
 Â
 ...Number of elements: 462
 ...Number of nodes:   1066
 ...Decompose to 4 CPU domains
 ...Element load balance ratio =   1.035
           L O A D  S T E P  O P T I O N S  LOAD STEP NUMBER. . . . . . . . . . . . . . . .   1
  TIME AT END OF THE LOAD STEP. . . . . . . . . .  1.0000  Â
  NUMBER OF SUBSTEPS. . . . . . . . . . . . . . .   1
  STEP CHANGE BOUNDARY CONDITIONS . . . . . . . .   NO
  PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
  DATABASE OUTPUT CONTROLS
   ITEM   FREQUENCY  COMPONENT
    ALL    NONE        Â
   NSOL     ALL        Â
   RSOL     ALL        Â
   STRS     ALL        Â
   EPEL     ALL        Â
   EPPL     ALL        Â
 SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr                                                                                                                              ÂÂ
             ***********  PRECISE MASS SUMMARY  ***********
  TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
        Translational mass        |  Coupled translational/rotational mass
     74.543     0.0000     0.0000   |   0.0000    -0.13576E-01  -0.82937E-02
     0.0000     74.543     0.0000   |   0.13576E-01   0.0000    0.35178E-01
     0.0000     0.0000     74.543   |   0.82937E-02  -0.35178E-01   0.0000  Â
   ------------------------------------------ | ------------------------------------------
                        |     Rotational mass (inertia)
                        |   0.66083E-01  -0.63907E-03  0.85759E-03
                        |  -0.63907E-03   20.834    -0.27442E-03
                        |   0.85759E-03  -0.27442E-03   20.835  Â  TOTAL MASS =  74.543  Â
   The mass principal axes coincide with the global Cartesian axes  CENTER OF MASS (X,Y,Z)=  0.47192E-03  0.11126E-03  -0.18212E-03
  TOTAL INERTIA ABOUT CENTER OF MASS
    0.66079E-01  -0.63516E-03  0.85118E-03
    -0.63516E-03   20.834    -0.27593E-03
    0.85118E-03  -0.27593E-03   20.835  Â
   The inertia principal axes coincide with the global Cartesian axes
 *** MASS SUMMARY BY ELEMENT TYPE *** TYPE    MASS
   1  74.5429  Â Range of element maximum matrix coefficients in global coordinates
 Maximum = 6.686368032E+10 at element 63.                Â
 Minimum = 2.912786913E+09 at element 406.                Â  *** ELEMENT MATRIX FORMULATION TIMES
 TYPE   NUMBER  ENAME    TOTAL CP  AVE CP   1    458  SOLID187    0.125  0.000273
   2     4  SURF154    0.016  0.003906
 Time at end of element matrix formulation CP = 4.890625.        Â DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
 Number of equations =     3153,   Maximum wavefront =   156 Local memory allocated for solver        =    2.463 MB
 Local memory required for in-core solution   =    2.369 MB
 Local memory required for out-of-core solution =    1.588 MB Total memory allocated for solver        =    8.548 MB
 Total memory required for in-core solution   =    8.230 MB
 Total memory required for out-of-core solution =    5.897 MB *** NOTE ***               CP =    4.938  TIME= 16:13:27
 The Distributed Sparse Matrix Solver is currently running in the    Â
 in-core memory mode.  This memory mode uses the most amount of memory  Â
 in order to avoid using the hard drive as much as possible, which most Â
 often results in the fastest solution time.  This mode is recommended  Â
 if enough physical memory is present to accommodate all of the solver  Â
 data.                                  Â *** ERROR ***              CP =    4.938  TIME= 16:13:27
 An unexpected error ( SIG$ILL ) has occurred...  ANSYS internal data  Â
 has been corrupted.  ANSYS is unable to recover and will terminate.   Â
 Previously saved files are unaffected.  Please send the data leading  Â
 to this operation to your technical support provider, as this will   Â
 allow ANSYS, Inc to improve the program.                Â Current ANSYS Traceback:
   mf2Factor            Â
   DSPmain             Â
   SolveFULL            Â
   svkan              Â
   solvcl             Â
   ANSYS
 *---------------------------------------------------------------------------*
 |                                      |
 |            DISTRIBUTED ANSYS RUN COMPLETED           |
 |                                      |
 |---------------------------------------------------------------------------|
 |                                      |
 | Ansys Release 16.0      Build 16.0     UP20141203   WINDOWS x64 |
 |                                      |
 |---------------------------------------------------------------------------|
 |                                      |
 | Database Requested(-db)  1024 MB   Scratch Memory Requested    1024 MB |
 | Maximum Database Used    1 MB   Maximum Scratch Memory Used   36 MB |
 |                                      |
 |---------------------------------------------------------------------------|
 |                                      |
 |     CP Time    (sec) =      5.109    Time  =  16:13:28     |
 |     Elapsed Time (sec) =     13.000    Date  =  07/23/2023    |
 |                                      |
 *---------------------------------------------------------------------------* -
July 26, 2023 at 4:46 pmVJAnsys Employee
I see you are using a very old version 16.0 which is not supported officially by us. Is it possible to try a newer version?
Also, it looks like some data is corrupted in the project as per the message. Have you tried running a simple project?
An unexpected error ( SIG$ILL ) has occurred...  ANSYS internal data  Â
 has been corrupted.  ANSYS is unable to recover and will terminate.   Â
 Previously saved files are unaffected.  Please send the data leading  Â
 to this operation to your technical support provider, as this will   Â
 allow ANSYS, Inc to improve the program.        ÂÂ
You can try renaming the %appdata%\Ansys folder to %appdata%\Ansys.old and then retry again.  Â
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July 27, 2023 at 9:12 pmFarouk SanniSubscriber
I use an older version of windows hence my reason for this ANSYS model. I use windows 8 but I will try your solution to see if it works.
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- The topic ‘HELPP ANSYS SIMULATION ERROR’ is closed to new replies.
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