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HELPP ANSYS SIMULATION ERROR

    • Farouk Sanni
      Subscriber

      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?

    • VJ
      Ansys Employee

      What is written in the solve.out file? Please share the output. 

    • Farouk Sanni
      Subscriber

      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

    • VJ
      Ansys Employee

      Sorry, we cannot download any files from the forum. Please paste it in the comments.

    • Farouk Sanni
      Subscriber

      ANSYS Multiphysics                                


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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 x64 
       CURRENT JOBNAME=file0  16:13:18  JUL 23, 2023 CP=      1.500


       PARAMETER _DS_PROGRESS =     999.0000000    

       /INPUT FILE= ds.dat  LINE=       0

       

       *** NOTE ***                            CP =       2.609   TIME= 16:13:21
       The /CONFIG,NOELDB command is not valid in a Distributed ANSYS          
       solution.  Command is ignored.                                          

       *GET  _WALLSTRT  FROM  ACTI  ITEM=TIME WALL  VALUE=  16.2225000    

       TITLE= 
       unsaved_project--Static Structural (A5)                                       


       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    
        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 MKS 

       *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE Release 16.0     16.0     ***
       DISTRIBUTED ANSYS Multiphysics                                

       00000000  VERSION=WINDOWS x64   16:13:21  JUL 23, 2023 CP=      2.625

       unsaved_project--Static Structural (A5)                                       

       

                ***** 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    
       ****************************************************************************
       *************************    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. 
               Writing frequency : each ITERATION.

       DO NOT SAVE ANY RESTART FILES AT ALL
       ****************************************************
       ******************* SOLVE FOR LS 1 ****************

       SELECT       FOR ITEM=TYPE COMPONENT=    
        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                    

       SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  2   KVAL = 1
            SET ACCORDING TO TABLE PARAMETER = _LOADVARI27Y                    

       SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  3   KVAL = 1
            SET ACCORDING TO TABLE PARAMETER = _LOADVARI27Z                    

       ALL SELECT   FOR ITEM=NODE COMPONENT=    
        IN RANGE         1 TO       1066 STEP          1

             1066  NODES (OF       1066  DEFINED) SELECTED BY NSEL  COMMAND.

       ALL SELECT   FOR ITEM=ELEM COMPONENT=    
        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    

       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 ALL 
         FOR ALL APPLICABLE ENTITIES

       WRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL 
         FOR ALL APPLICABLE ENTITIES

       WRITE STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL 
         FOR ALL APPLICABLE ENTITIES

       WRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL 
         FOR ALL APPLICABLE ENTITIES

       WRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL 
         FOR ALL APPLICABLE ENTITIES

       NONLINEAR STABILIZATION CONTROL:
       KEY=OFF 


       *GET  ANSINTER_  FROM  ACTI  ITEM=INT        VALUE=  0.00000000    

       *IF  ANSINTER_                         ( =   0.00000     )  NE  
            0                                 ( =   0.00000     )  THEN    

       *ENDIF

       *****  ANSYS SOLVE    COMMAND  *****

       *** WARNING ***                         CP =       4.641   TIME= 16:13:25
       Element shape checking is currently inactive.  Issue SHPP,ON or         
       SHPP,WARN to reactivate, if desired.                                    

       *** NOTE ***                            CP =       4.656   TIME= 16:13:25
       The model data was checked and warning messages were found.             
        Please review output or errors file (                                  
       C:\Users\Yakuba\AppData\Local\Temp\WB_FARSAN_Yakub_10084_2\_ProjectScra 
       atch\Scr8F73\file0.err ) for these warning messages.                    

       *** 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.

       

       *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE Release 16.0     16.0     ***
       DISTRIBUTED ANSYS Multiphysics                                

       00000000  VERSION=WINDOWS x64   16:13:25  JUL 23, 2023 CP=      4.672

       unsaved_project--Static Structural (A5)                                       

       

                             S O L U T I O N   O P T I O N S

         PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D                  
         DEGREES OF FREEDOM. . . . . . UX   UY   UZ  
         ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
         OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . .  273.15    
         EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE             
         GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC  

       *** WARNING ***                         CP =       4.688   TIME= 16:13:25
       Material number 2 (used by element 459 ) should normally have at least  
       one MP or one TB type command associated with it.  Output of energy by  
       material may not be available.                                          

       *** NOTE ***                            CP =       4.688   TIME= 16:13:25
       The step data was checked and warning messages were found.              
        Please review output or errors file (                                  
       C:\Users\Yakuba\AppData\Local\Temp\WB_FARSAN_Yakub_10084_2\_ProjectScra 
       atch\Scr8F73\file0.err ) for these warning messages.                    

       *** NOTE ***                            CP =       4.688   TIME= 16:13:25
       The conditions for direct assembly have been met.  No .emat or .erot    
       files will be produced.                                                 

        
        
           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
        
        ...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    
         NUMBER OF SUBSTEPS. . . . . . . . . . . . . . .     1
         STEP CHANGE BOUNDARY CONDITIONS . . . . . . . .    NO
         PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
         DATABASE OUTPUT CONTROLS
            ITEM     FREQUENCY   COMPONENT
             ALL       NONE               
            NSOL        ALL               
            RSOL        ALL               
            STRS        ALL               
            EPEL        ALL               
            EPPL        ALL               


       SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr                                                                                                                                                                                                                                                           

       

                               ***********  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    
           ------------------------------------------ | ------------------------------------------
                                                      |         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    

         TOTAL MASS =  74.543    
           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    
           The inertia principal axes coincide with the global Cartesian axes


        *** MASS SUMMARY BY ELEMENT TYPE ***

        TYPE      MASS
           1   74.5429    

       Range of element maximum matrix coefficients in global coordinates
       Maximum = 6.686368032E+10 at element 63.                                
       Minimum = 2.912786913E+09 at element 406.                               

         *** 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.                

       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        
       in-core memory mode.  This memory mode uses the most amount of memory   
       in order to avoid using the hard drive as much as possible, which most  
       often results in the fastest solution time.  This mode is recommended   
       if enough physical memory is present to accommodate all of the solver   
       data.                                                                   

       *** ERROR ***                           CP =       4.938   TIME= 16:13:27
       An unexpected error ( SIG$ILL ) has occurred...  ANSYS internal data    
       has been corrupted.  ANSYS is unable to recover and will terminate.     
       Previously saved files are unaffected.  Please send the data leading    
       to this operation to your technical support provider, as this will      
       allow ANSYS, Inc to improve the program.                                

       Current ANSYS Traceback:
           mf2Factor                       
           DSPmain                         
           SolveFULL                       
           svkan                           
           solvcl                          
           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      |
       |                                                                           |
       *---------------------------------------------------------------------------*

    • VJ
      Ansys 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    
       has been corrupted.  ANSYS is unable to recover and will terminate.     
       Previously saved files are unaffected.  Please send the data leading    
       to this operation to your technical support provider, as this will      
       allow ANSYS, Inc to improve the program.                

       

      You can try renaming the %appdata%\Ansys folder to %appdata%\Ansys.old and then retry again.    

    • Farouk Sanni
      Subscriber

      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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