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General Mechanical

General Mechanical

Topics related to Mechanical Enterprise, Motion, Additive Print and more.

An unknown error during Solution.

    • AshishChauhan
      Subscriber

      Hello, I'm getting an error and a warning during solution, while all other things are good.


      Error: "An unknown error occurred during solution.  Check the Solver Output on the Solution Information object for possible causes."


      And,


      Warning: "Not all Named Selections were successfully written because one or more names are not valid for the solver."


      Association: Project>Model>Static Structural>Solution


      I'm using Ansys 18.1 and doing an analysis on a layered composite helical spring model generated in Ansys ACP-Pre.


      I have also attached a text file containing the Solution Information.


       


      PLEASE HELP!


       

    • Sandeep Medikonda
      Ansys Employee

      Ashish, Can you copy paste the output using preformatted option in the toolbar above where you type? Not everyone is allowed to download the file? Even the last part after the statistics are written out will do.


      Regards,
      Sandeep

    • AshishChauhan
      Subscriber

      Hello Sir,


      Actually, i saw one post on the forum where the similar error was posted and it mentioned to close some of the other running programs. After closing one of the programs and running the solution again I got rid of the above-mentioned error, but now it shows one more Unknown error.


      Also, the Warning: "Not all Named Selections were successfully written because one or more names are not valid for the solver"  is still there.


       


      I am pasting the solution information for the second error here.


       



      Solver Output



       




       ANSYS Mechanical
      Enterprise                      



       *


      *
       |                                                                 
      |
       |   W E L C O M E   T O   T H E   A N S Y S (R)  P R O G R A M    
      |
       |                                                                 
      |
       *
      *




       ***************************************************************
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       Release
      18.1
          
       Point Releases and Patches installed:  
          
       ANSYS Inc. Products Release 18.1  
       ANSYS Mechanical Products Release 18.1 

       ANSYS Autodyn Release 18.1 
       ANSYS LS-DYNA Release 18.1 
       ANSYS AIM
      Release 18.1 
       ANSYS CFX (includes ANSYS CFD-Post) Release 18.1
       ANSYS
      Fluent (includes ANSYS CFD-Post) Release 18.1
       ANSYS TurboGrid Release
      18.1
       ANSYS FENSAP-ICE Release 18.1  
       ANSYS Polyflow (includes ANSYS
      CFD-Post) Release 18.1  
       ANSYS CFD-Post only Release 18.1
       ANSYS Forte
      Release 18.1
       ANSYS Chemkin Release 18.1 
       ANSYS ICEM CFD Release 18.1

       ANSYS Aqwa Release 18.1
       ANSYS Icepak (includes ANSYS CFD-Post) Release
      18.1
       AutoCAD Release 18.1
       ACIS Release 18.1  
       Catia, Version 4
      Release 18.1  
       Catia, Version 5 Release 18.1  
       Catia, Version 6
      Release 18.1  
       Creo Elements/Direct Modeling Release 18.1 
       Inventor
      Release 18.1  
       JTOpen Release 18.1
       NX Release 18.1
       Parasolid
      Release 18.1 
       Creo Parametric Release 18.1
       Solid Edge Release 18.1

       SolidWorks Release 18.1
       ANSYS, Inc. License Manager Release
      18.1


                *****  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
        MPI
      OPTION                   = INTELMPI
        INPUT FILE NAME              =
      C:UsersMAYANKDesktopNAYA MODEL01 (Ansys
      18.1)_ProjectScratchScr9956dummy.dat
        OUTPUT FILE NAME             =
      C:UsersMAYANKDesktopNAYA MODEL01 (Ansys
      18.1)_ProjectScratchScr9956solve.out
        START-UP FILE MODE           =
      NOREAD
        STOP FILE MODE               = NOREAD

       RELEASE= Release
      18.1         BUILD= 18.1      UP20170403   VERSION=WINDOWS x64
       CURRENT
      JOBNAME=file0  00:161  DEC 08, 2018 CP=      0.344


       PARAMETER
      _DS_PROGRESS =     999.0000000   

       /INPUT FILE= ds.dat  LINE=      
      0



       *** NOTE ***                            CP =       0.562  
      TIME= 00:161
       The /CONFIG,NOELDB command is not valid in a Distributed
      ANSYS         
       solution.  Command is
      ignored.                                         

       *GET  _WALLSTRT 
      FROM  ACTI  ITEM=TIME WALL  VALUE= 0.275277778   

       TITLE=

       NEW--Static Structural
      (K3)                                                  

        ACT
      Extensions:
            MechanicalDropTest, 2.0
           
      f0fd899f-9d88-4f46-8cf1-36bf5c218d65, wbex
       

       SET PARAMETER
      DIMENSIONS ON  _WB_PROJECTSCRATCH_DIR
        TYPE=STRI  DIMENSIONS=     
      248        1        1

       PARAMETER _WB_PROJECTSCRATCH_DIR(1) =
      C:UsersMAYANKDesktopNAYA MODEL01 (Ansys
      18.1)_ProjectScratchScr9956

       SET PARAMETER DIMENSIONS ON 
      _WB_SOLVERFILES_DIR
        TYPE=STRI  DIMENSIONS=      248        1       
      1

       PARAMETER _WB_SOLVERFILES_DIR(1) = C:UsersMAYANKDesktopNAYA
      MODEL01 (Ansys 18.1)NEW_filesdp0SYS-5MECH

       SET PARAMETER DIMENSIONS
      ON  _WB_USERFILES_DIR
        TYPE=STRI  DIMENSIONS=      248        1       
      1

       PARAMETER _WB_USERFILES_DIR(1) = C:UsersMAYANKDesktopNAYA MODEL01
      (Ansys 18.1)NEW_filesuser_files
       --- Data in consistent NMM units. See
      Solving Units in the help system for more

       MPA UNITS SPECIFIED FOR
      INTERNAL   
        LENGTH      = MILLIMETERS (mm)
        MASS        = TONNE
      (Mg)
        TIME        = SECONDS (sec)
        TEMPERATURE = CELSIUS (C)
       
      TOFFSET     = 273.0
        FORCE       = NEWTON (N)
        HEAT        = MILLIJOULES
      (mJ)

       INPUT  UNITS ARE ALSO SET TO MPA

       *** ANSYS - ENGINEERING
      ANALYSIS SYSTEM  RELEASE Release 18.1     18.1     ***
       DISTRIBUTED ANSYS
      Mechanical Enterprise                      

       00000000  VERSION=WINDOWS
      x64   00:161  DEC 08, 2018 CP=      0.562

       NEW--Static Structural
      (K3)                                                  



               
      ***** ANSYS ANALYSIS DEFINITION (PREP7) *****
       *********** Nodes for the
      whole assembly ***********
       *********** Elements for Body 1 "SolidModel.1"
      ***********
       *********** Send User Defined Coordinate System(s)
      ***********
       *********** Set Reference Temperature
      ***********
       *********** Send Materials ***********
       *********** Sending
      Coordinate Systems for External Layered Section***********
       ***********
      Sending Materials for External Layered Section***********
       *********** Send
      External Layered Section Properties ***********
       *********** Send Named
      Selection as Node Component ***********
       *********** Send Named Selection as
      Node Component ***********
       *********** Send Named Selection as Node
      Component ***********
       *********** Send Named Selection as Node Component
      ***********
       *********** Send Named Selection as Node Component
      ***********
       *********** Send Named Selection as Node Component
      ***********
       *********** Send Named Selection as Node Component
      ***********
       *********** Send Named Selection as Node Component
      ***********
       *********** Send Named Selection as Node Component
      ***********
       *********** Send Named Selection as Node Component
      ***********
       *********** Fixed Supports ***********
       *********** Define
      Force Using Surface Effect Elements ***********


       ***** ROUTINE
      COMPLETED *****  CP =        29.469


       --- Number of total nodes =
      1695840
       --- Number of contact elements = 8488
       --- Number of spring
      elements = 0
       --- Number of bearing elements = 0
       --- Number of solid
      elements = 1526112
       --- Number of condensed parts = 0
       --- Number of total
      elements = 1534600

       *GET  _WALLBSOL  FROM  ACTI  ITEM=TIME WALL  VALUE=
      0.282777778   

       ****************************************************************************
       *************************   
      SOLUTION      
      ********************************
       ****************************************************************************

       ***** 
      ANSYS SOLUTION ROUTINE  *****


       PERFORM A STATIC ANALYSIS
        THIS
      WILL BE A NEW ANALYSIS

       LARGE DEFORMATION ANALYSIS

       USE
      PRECONDITIONED CONJUGATE GRADIENT SOLVER
        CONVERGENCE TOLERANCE =
      1.00000E-08
        MAXIMUM ITERATION     = NumNode*DofPerNode*  1.0000   


       MEMORY SAVING OPTION TURNED ON FOR PCG 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.

       DEFINE RESTART CONTROL FOR LOADSTEP LAST
       AT FREQUENCY OF
      LAST AND NUMBER FOR OVERWRITE IS    0

       DELETE RESTART FILES OF
      ENDSTEP
       ****************************************************
       *******************
      SOLVE FOR LS 1 OF 1 ****************

       SELECT       FOR ITEM=TYPE
      COMPONENT=   
        IN RANGE        13 TO         13 STEP         
      1

             8488  ELEMENTS (OF    1534600  DEFINED) SELECTED BY  ESEL 
      COMMAND.

       SELECT      ALL NODES HAVING ANY ELEMENT IN ELEMENT
      SET.

           9558 NODES (OF  1695840  DEFINED) SELECTED FROM
           8488
      SELECTED ELEMENTS BY NSLE COMMAND.

       SPECIFIED SURFACE LOAD PRES FOR ALL
      SELECTED ELEMENTS  LKEY =  1   KVAL = 1
            SET ACCORDING TO TABLE
      PARAMETER = _LOADVARI87X                   

       SPECIFIED SURFACE LOAD PRES
      FOR ALL SELECTED ELEMENTS  LKEY =  2   KVAL = 1
            SET ACCORDING TO TABLE
      PARAMETER = _LOADVARI87Y                   

       SPECIFIED SURFACE LOAD PRES
      FOR ALL SELECTED ELEMENTS  LKEY =  3   KVAL = 1
            SET ACCORDING TO TABLE
      PARAMETER = _LOADVARI87Z                   

       ALL SELECT   FOR ITEM=NODE
      COMPONENT=   
        IN RANGE         1 TO    1865424 STEP          1

         
      1695840  NODES (OF    1695840  DEFINED) SELECTED BY NSEL  COMMAND.

       ALL
      SELECT   FOR ITEM=ELEM COMPONENT=   
        IN RANGE         1 TO    1704168
      STEP          1

          1534600  ELEMENTS (OF    1534600  DEFINED) SELECTED
      BY  ESEL  COMMAND.

       PRINTOUT RESUMED BY /GOP

       USE AUTOMATIC TIME
      STEPPING THIS LOAD STEP

       USE       1 SUBSTEPS INITIALLY THIS LOAD STEP
      FOR ALL  DEGREES OF FREEDOM
       FOR AUTOMATIC TIME STEPPING:
         USE     10
      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 =      30.422   TIME= 00:16:58
       Element shape
      checking is currently inactive.  Issue SHPP,ON or        
       SHPP,WARN to
      reactivate, if desired.                                   

       *** NOTE
      ***                            CP =      71.734   TIME= 00:17:12
       The model
      data was checked and warning messages were found.            
        Please
      review output or errors file ( C:UsersMAYANKDesktopNAYA    
       MODEL01
      (Ansys 18.1)_ProjectScratchScr9956file0.err ) for these     
       warning
      messages.                                                      

       ***
      SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
            --- GIVE
      SUGGESTIONS AND RESET THE KEY OPTIONS ---

       ELEMENT TYPE    1 IS SOLID185.
      IT IS ASSOCIATED WITH LINEAR MATERIALS ONLY
       BUT MATERIALS ARE ANISOTROPIC.
      KEYOPT(2)=2 IS SUGGESTED AND HAS BEEN RESET.
        KEYOPT(1-12)=    0    2   
      1    0    0    0    0    1    0    0    0    0



       *** ANSYS -
      ENGINEERING ANALYSIS SYSTEM  RELEASE Release 18.1     18.1    
      ***
       DISTRIBUTED ANSYS Mechanical Enterprise                      


       00000000  VERSION=WINDOWS x64   00:17:14  DEC 08, 2018 CP=    
      73.094

       NEW--Static Structural
      (K3)                                                  




                             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   
         NONLINEAR GEOMETRIC EFFECTS . . . . . . . . .
      .ON
         EQUATION SOLVER OPTION. . . . . . . . . . . . .PCG               

            MEMORY SAVING OPTION. . . .  . . . . . . . .ON
            TOLERANCE. . .
      . . . . . . . . . . . . . . . 1.00000E-08
         NEWTON-RAPHSON OPTION . . . . .
      . . . . . . . .PROGRAM CHOSEN  
         GLOBALLY ASSEMBLED MATRIX . . . . . . . .
      . . .SYMMETRIC 

       *** NOTE ***                            CP =     
      73.531   TIME= 00:17:14
       Poisson's ratio PR input has been converted to NU
      input.               

       *** WARNING ***                         CP =     
      74.609   TIME= 00:17:15
       Material number 13 (used by element 1695681 ) 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 =      75.484   TIME= 00:17:16
       The step
      data was checked and warning messages were found.             
        Please
      review output or errors file ( C:UsersMAYANKDesktopNAYA    
       MODEL01
      (Ansys 18.1)_ProjectScratchScr9956file0.err ) for these     
       warning
      messages.                                                      

       ***
      NOTE ***                            CP =      75.484   TIME= 00:17:16
       This
      nonlinear analysis defaults to using the full Newton-Raphson      
       solution
      procedure.  This can be modified using the NROPT command.     

       *** NOTE
      ***                            CP =      75.484   TIME= 00:17:16
       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: 1534600
        ...Number of nodes:    1695840
       
      ...Decompose to 4 CPU domains
        ...Element load balance ratio =    
      1.017


                            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   
         AUTOMATIC TIME
      STEPPING . . . . . . . . . . . .    ON
            INITIAL NUMBER OF SUBSTEPS . . .
      . . . . . .     1
            MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . .   
      10
            MINIMUM NUMBER OF SUBSTEPS . . . . . . . . .     1
         MAXIMUM
      NUMBER OF EQUILIBRIUM ITERATIONS. . . .    15
         STEP CHANGE BOUNDARY
      CONDITIONS . . . . . . . .    NO
         STRESS-STIFFENING . . . . . . . . . . . .
      . . .    ON
         TERMINATE ANALYSIS IF NOT CONVERGED . . . . . .YES (EXIT) 

         CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS
         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                                                                                                                                                                                                                                                          

       MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED             

        TO BE, NEQIT = 22, BY SOLUTION CONTROL LOGIC.                         



       *** NOTE ***                            CP =      91.141   TIME=
      00:170
       The PCG solver has automatically set the level of difficulty for
      this  
       model to
      4.                                                            

       ***
      WARNING ***                         CP =     151.609   TIME= 00:19:24
       An
      error has occurred writing to the file = 3 which may imply a full   

       disk.                                                                  

       The system I/O error = 28.  Please refer to your system documentation  

       on I/O errors.                                                         

                                                                              

                                                                              



       


       


       

       

    • Sandeep Medikonda
      Ansys Employee

      Ashish, it looks like you have a full disk. Make some space and also based on some of the warnings, you might want to turn off distributed solve and run. See this post.


      The comment about named selection seems like a warning to me and doesn't seem to be the problem Right click on that message and identify the object that is creating the problem. See what is wrong in the naming of it and correct it.


      Regards,
      Sandeep
      Guidelines on the Student Community

    • AshishChauhan
      Subscriber
      Hello sir
      I checked my disk space while solution was running and it was getting full , as you said.
      And, after increasing my disk space, the solution ran fine.

      Thank you for the help.
    • Goddy
      Subscriber

      I know I'm not supposed to do this but I put up a question a couple of days ago and no one has responded. So maybe doing this can draw your attention this link will take you to the post /forum/forums/topic/unknown-error-the-optimization-run-was-terminated-check-the-optimization-output/


      Thanks


       

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