July 26, 2023 at 4:35 pm
Farouk Sanni
Subscriber

ANSYS Multiphysics                                


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

 


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 Release 16.0
     
 Point Releases and Patches installed:   
     
 ANSYS, Inc. Products Release 16.0   
 ANSYS Mechanical Products Release 16.0  
 ANSYS Autodyn Release 16.0  
 ANSYS LS-DYNA Release 16.0  
 ANSYS AIM Release 16.0  
 ANSYS CFX (includes ANSYS CFD-Post) Release 16.0
 ANSYS Fluent (includes ANSYS CFD-Post) Release 16.0 
 ANSYS TurboGrid Release 16.0
 ANSYS Polyflow (includes ANSYS CFD-Post) Release 16.0   
 ANSYS ICEM CFD Release 16.0 
 ANSYS Aqwa Release 16.0 
 ANSYS Composite PrepPost Release 16.0   
 ANSYS Icepak (includes ANSYS CFD-Post) Release 16.0 
 Catia, Version 6 Release 16.0   
 ANSYS, Inc. License Manager Release 16.0


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