General Mechanical

General Mechanical

Sphere Impact simulation Error

    • luandersoncosta
      Subscriber

      Hi guys, Im trying to simulate a sphere impact in a Nitinol plate, but Im facing some errors. anyone here can Help me?

       

      Ansys Mechanical Enterprise Academic Student     


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                *****  ANSYS COMMAND LINE ARGUMENTS  *****
        BATCH MODE REQUESTED (-b)    = NOLIST
        INPUT FILE COPY MODE (-c)    = COPY
        DISTRIBUTED MEMORY PARALLEL REQUESTED
             2 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS
          TOTAL OF     2 CORES REQUESTED
        INPUT FILE NAME              = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScratch\Scr86C5\dummy.dat
        OUTPUT FILE NAME             = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScratch\Scr86C5\solve.out
        START-UP FILE MODE           = NOREAD
        STOP FILE MODE               = NOREAD

       RELEASE= 2022 R1              BUILD= 22.1      UP20211129   VERSION=WINDOWS x64
       CURRENT JOBNAME=file0  18:01:27  DEC 14, 2022 CP=      0.062


       PARAMETER _DS_PROGRESS =     999.0000000   

       /INPUT FILE= ds.dat  LINE=       0



       *** NOTE ***                            CP =       0.141   TIME= 18:01:27
       The /CONFIG,NOELDB command is not valid in a Distributed ANSYS         
       solution.  Command is ignored.                                         

       *GET  _WALLSTRT  FROM  ACTI  ITEM=TIME WALL  VALUE=  18.0241667   

       TITLE=
       wbnew--Static Structural (B5)                                                

        ACT Extensions:
            LSDYNA, 2021.1
            5f463412-bd3e-484b-87e7-cbc0a665e474, wbex
       

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

       PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScratch\Scr86C5\

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

       PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\wbnew_files\dp0\SYS\MECH\

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

       PARAMETER _WB_USERFILES_DIR(1) = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\wbnew_files\user_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 2022 R1          22.1     ***
       DISTRIBUTED Ansys Mechanical Enterprise Academic Student     

       00000000  VERSION=WINDOWS x64   18:01:27  DEC 14, 2022 CP=      0.141

       wbnew--Static Structural (B5)                                                



                ***** ANSYS ANALYSIS DEFINITION (PREP7) *****
       *********** Nodes for the whole assembly ***********
       *********** Nodes for all Remote Points ***********
       *********** Elements for Body 1 "Geom\Capo" ***********
       *********** Elements for Body 2 "Geom\Solid" ***********
       *********** Send User Defined Coordinate System(s) ***********
       *********** Set Reference Temperature ***********
       *********** Send Materials ***********
       *********** Create Contact "Rough - Geom\Capo To Geom\Solid" ***********
                   Real Constant Set For Above Contact Is 4 & 3
       *********** Fixed Supports ***********
       *********** Create Remote Point "Internal Remote Point 2" ***********
       *********** Create Joint "Translational - Ground To Geom\Solid" ***********
                   Real Constant Set For Above Joint Is 7
       *********** Define Body Force Temperature ***********
       *********** Create Joint Drivers **********


       ***** ROUTINE COMPLETED *****  CP =         0.328


       --- Number of total nodes = 28386
       --- Number of contact elements = 8064
       --- Number of spring elements = 0
       --- Number of bearing elements = 0
       --- Number of solid elements = 4155
       --- Number of condensed parts = 0
       --- Number of total elements = 12221

       *GET  _WALLBSOL  FROM  ACTI  ITEM=TIME WALL  VALUE=  18.0241667   
       ****************************************************************************
       *************************    SOLUTION       ********************************
       ****************************************************************************

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


       PERFORM A STATIC ANALYSIS
        THIS WILL BE A NEW ANALYSIS

       LARGE DEFORMATION ANALYSIS

       PARAMETER _THICKRATIO =    0.5000000000   

       USE SPARSE MATRIX DIRECT SOLVER

       USE THE FULL NEWTON-RAPHSON OPTION FOR  ALL DEGREES OF FREEDOM
         WITH UNSYMMETRIC SOLVER
         AND USE THE DEFAULT ADAPTIVE DESCENT OPTION

       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


       CORIOLIS IN STATIONARY REFERENCE FRAME: GYROSCOPIC DAMPING MATRIX WILL BE CALCULATED

       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   -1

       DELETE RESTART FILES OF ENDSTEP
       ****************************************************
       ******************* SOLVE FOR LS 1 OF 4 ****************

       PRINTOUT RESUMED BY /GOP

       SELECT       FOR ITEM=TYPE COMPONENT=   
        IN RANGE         7 TO          7 STEP          1

                1  ELEMENTS (OF      12221  DEFINED) SELECTED BY  ESEL  COMMAND.

       APPLIED BOUNDARY CONDITIONS OR FORCES FOR JOINT ELEMENTS

      SPECIFIED VALUE FOR ALL SELECTED ELEMENTS
      FORCE, MOMENT, DISPLACEMENT OR ROTATION LABEL = UX 
      SET ACCORDING TO TABLE PARAMETER              = _LOADVARI57                    

       ALL SELECT   FOR ITEM=ELEM COMPONENT=   
        IN RANGE         1 TO      20365 STEP          1

            12221  ELEMENTS (OF      12221  DEFINED) SELECTED BY  ESEL  COMMAND.

       USE AUTOMATIC TIME STEPPING THIS LOAD STEP

       USE INITIAL TIME STEP SIZE OF 0.1000000E-01 FOR ALL  DEGREES OF FREEDOM
       FOR AUTOMATIC TIME STEPPING:
         USE 0.1000000E-01 AS THE MINIMUM TIME STEP SIZE
         USE 0.1000000E-01 AS THE MAXIMUM TIME STEP SIZE

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

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

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

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

       WRITE BKST 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

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

       WRITE MISC ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
         FOR THE ENTITIES DEFINED BY COMPONENT _ALLCONTACTS

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

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

       PRINTOUT RESUMED BY /GOP

       WRITE MISC ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
         FOR THE ENTITIES DEFINED BY COMPONENT _ELMISC

       NONLINEAR STABILIZATION CONTROL:
       KEY=OFF


       *GET  ANSINTER_  FROM  ACTI  ITEM=INT        VALUE=  0.00000000   

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

       *ENDIF

       *** NOTE ***                            CP =       0.656   TIME= 18:01:27
       The automatic domain decomposition logic has selected the MESH domain  
       decomposition method with 2 processes per solution.                    

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

       *** WARNING ***                         CP =       0.656   TIME= 18:01:27
       Element shape checking is currently inactive.  Issue SHPP,ON or        
       SHPP,WARN to reactivate, if desired.                                   

       *** NOTE ***                            CP =       0.703   TIME= 18:01:28
       The model data was checked and warning messages were found.            
        Please review output or errors file (                                 
       C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScr
       ratch\Scr86C5\file0.err ) for these warning messages.                  

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

       ELEMENT TYPE         1 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
        KEYOPT(1-12)=    0    0    0    0    0    0    0    0    0    0    0    0

       ELEMENT TYPE         2 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 2022 R1          22.1     ***
       DISTRIBUTED Ansys Mechanical Enterprise Academic Student     

       00000000  VERSION=WINDOWS x64   18:01:28  DEC 14, 2022 CP=      0.703

       wbnew--Static Structural (B5)                                                



                             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   ROTX ROTY ROTZ
         ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
         OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . .  273.15   
         NONLINEAR GEOMETRIC EFFECTS . . . . . . . . . .ON
         EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE            
         PLASTIC MATERIAL PROPERTIES INCLUDED. . . . . .YES
         NEWTON-RAPHSON OPTION . . . . . . . . . . . . .FULL UNSYMMETRIC
         GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .UNSYMMETRIC

       *** WARNING ***                         CP =       0.734   TIME= 18:01:28
       Material number 7 (used by element 12300) 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 =       0.766   TIME= 18:01:28
       The step data was checked and warning messages were found.             
        Please review output or errors file (                                 
       C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScr
       ratch\Scr86C5\file0.err ) for these warning messages.                  

       *** NOTE ***                            CP =       0.797   TIME= 18:01:28
       Internal nodes from 28387 to 28390 are created.                        
       1 internal nodes are used for handling degrees of freedom on pilot     
       nodes of rigid target surfaces.                                        
       3 internal nodes are used for non-contact elements with mixed          
       formulation.                                                           

       *** NOTE ***                            CP =       0.859   TIME= 18:01:28
       Internal nodes from 28387 to 28390 are created.                        
       1 internal nodes are used for handling degrees of freedom on pilot     
       nodes of rigid target surfaces.                                        
       3 internal nodes are used for non-contact elements with mixed          
       formulation.                                                           

       *** NOTE ***                            CP =       1.266   TIME= 18:01:28
       Symmetric Deformable- deformable contact pair identified by real       
       constant set 3 and contact element type 3 has been set up.  The        
       companion pair has real constant set ID 4.  Both pairs should have the 
       same behavior.                                                         
       ANSYS will deactivate the current pair and keep its companion pair,    
       resulting in asymmetric contact.                                       
       Contact algorithm: Augmented Lagrange method
       Contact detection at: Gauss integration point
       Contact stiffness factor FKN                  1.0000   
       The resulting initial contact stiffness       1783.2   
       Default penetration tolerance factor FTOLN   0.10000   
       The resulting penetration tolerance          0.60566   
       Default tangent stiffness factor FKT          1.0000   
       Default elastic slip factor SLTOL            0.50000E-02
       The resulting elastic slip tolerance         0.10094   
       Update contact stiffness at each iteration
       Default Max. friction stress TAUMAX          0.10000E+21
       Average contact surface length                20.189   
       Average contact pair depth                    6.0566   
       Average target surface length                 11.073   
       Default pinball region factor PINB            2.0000   
       The resulting pinball region                  12.113   
       *WARNING*: Initial penetration is included.
       Rough contact is defined.

       *** NOTE ***                            CP =       1.266   TIME= 18:01:28
       Min.  Initial gap 5.03209051 was detected between contact element 18190
       and target element 20200.                                              
       You may move entire target surface by: x= -1.182266212E-02, y=         
       -5.03207497, z= -4.082909165E-03, to bring it in contact.              
       ****************************************
       

       *** NOTE ***                            CP =       1.266   TIME= 18:01:28
       Symmetric Deformable- deformable contact pair identified by real       
       constant set 4 and contact element type 3 has been set up.  The        
       companion pair has real constant set ID 3.  Both pairs should have the 
       same behavior.                                                         
       ANSYS will keep the current pair and deactivate its companion pair,    
       resulting in asymmetric contact.                                       
       Contact algorithm: Augmented Lagrange method
       Contact detection at: Gauss integration point
       Contact stiffness factor FKN                  1.0000   
       The resulting initial contact stiffness       1783.2   
       Default penetration tolerance factor FTOLN   0.10000   
       The resulting penetration tolerance          0.87119   
       Default tangent stiffness factor FKT          1.0000   
       Default elastic slip factor SLTOL            0.50000E-02
       The resulting elastic slip tolerance         0.55549E-01
       Update contact stiffness at each iteration
       Default Max. friction stress TAUMAX          0.10000E+21
       Average contact surface length                11.110   
       Average contact pair depth                    8.7119   
       Average target surface length                 20.040   
       Default pinball region factor PINB            2.0000   
       The resulting pinball region                  17.424   
       *WARNING*: Initial penetration is included.
       Rough contact is defined.

       *** NOTE ***                            CP =       1.266   TIME= 18:01:28
       Min.  Initial gap 4.80633588 was detected between contact element 20112
       and target element 14290.                                              
       You may move entire target surface by: x= -0.656985361, y= 4.74818476, 
       z= -0.352102748, to bring it in contact.                               
       ****************************************
       

       *** NOTE ***                            CP =       1.266   TIME= 18:01:28
       Rigid-constraint surface identified by real constant set 5 and contact 
       element type 5 has been set up.  The degrees of freedom of the rigid   
       surface are driven by the pilot node 28386 which connects to other     
       element 12300.  Internal MPC will be built.                            
       The used degrees of freedom set is  UX   UY   UZ   ROTX ROTY ROTZ
       ****************************************
       
       
       

       *** NOTE ***                            CP =       1.297   TIME= 18:01:28
       Internal nodes from 28387 to 28390 are created.                        
       1 internal nodes are used for handling degrees of freedom on pilot     
       nodes of rigid target surfaces.                                        
       3 internal nodes are used for non-contact elements with mixed          
       formulation.                                                           

       
       
           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: 12221
        ...Number of nodes:    28390
        ...Decompose to 2 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
            STARTING TIME STEP SIZE. . . . . . . . . . . 0.10000E-01
            MINIMUM TIME STEP SIZE . . . . . . . . . . . 0.10000E-01
            MAXIMUM TIME STEP SIZE . . . . . . . . . . . 0.10000E-01
         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
         CORIOLIS EFFECT IN STATIONARY REF. FRAME  . . .    ON
         COPY INTEGRATION POINT VALUES TO NODE . . . . .YES, FOR ELEMENTS WITH
                                                        ACTIVE MAT. NONLINEARITIES
         PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
         DATABASE OUTPUT CONTROLS
            ITEM     FREQUENCY   COMPONENT
             ALL       NONE              
            NSOL        ALL              
            RSOL        ALL              
            EANG        ALL              
            ETMP        ALL              
            VENG        ALL              
            NLOA        ALL              
            STRS        ALL              
            SRFS        ALL              
            BKST        ALL              
            EPEL        ALL              
            EPPL        ALL              
            EPTH        ALL              
            MISC        ALL       _ALLCONTACTS
            CONT        ALL              
            NLDA        ALL              
            MISC        ALL       _ELMISC


       SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr                                                                                                                                                                                                                                                          

       *** NOTE ***                            CP =       1.797   TIME= 18:01:28
       Rigid-constraint surface identified by real constant set 5 and contact 
       element type 5 has been set up.  The degrees of freedom of the rigid   
       surface are driven by the pilot node 28386 which connects to other     
       element 12300.  Internal MPC will be built.                            
       The used degrees of freedom set is  UX   UY   UZ   ROTX ROTY ROTZ
       ****************************************
       
       MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED             
        TO BE, NEQIT = 25, BY SOLUTION CONTROL LOGIC.                         

       
       The FEA model contains 0 external CE equations and 1068 internal CE    
       equations.                                                             


                               ***********  PRECISE MASS SUMMARY  ***********

         TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
                     Translational mass               |   Coupled translational/rotational mass
              0.24526E-02    0.0000        0.0000     |     0.0000       0.23759E-02   -2.1169   
               0.0000       0.24526E-02    0.0000     |   -0.23759E-02    0.0000        5.9711   
               0.0000        0.0000       0.24526E-02 |     2.1169       -5.9711        0.0000   
           ------------------------------------------ | ------------------------------------------
                                                      |         Rotational mass (inertia)
                                                      |     2019.1       -5151.8       -4.9403   
                                                      |    -5151.8        15155.       -2.0171   
                                                      |    -4.9403       -2.0171        16792.   

         TOTAL MASS = 0.24526E-02
           The mass principal axes coincide with the global Cartesian axes

         CENTER OF MASS (X,Y,Z)=    2434.6        863.13       0.96874   

         TOTAL INERTIA ABOUT CENTER OF MASS
               191.97        2.0486       0.84408   
               2.0486        617.88       0.33625E-01
              0.84408       0.33625E-01    427.25   

         PRINCIPAL INERTIAS =    191.96        617.89        427.25   
         ORIENTATION VECTORS OF THE INERTIA PRINCIPAL AXES IN GLOBAL CARTESIAN
           ( 1.000,-0.005,-0.004) ( 0.005, 1.000, 0.000) ( 0.004,-0.000, 1.000)


        *** MASS SUMMARY BY ELEMENT TYPE ***

        TYPE      MASS
           1  0.219013E-02
           2  0.262450E-03

       Range of element maximum matrix coefficients in global coordinates
       Maximum = 63925971.4 at element 1374.                                  
       Minimum = 786780.377 at element 9.                                     

         *** ELEMENT MATRIX FORMULATION TIMES
           TYPE    NUMBER   ENAME      TOTAL CP  AVE CP

              1      3900  SOLID186      0.766   0.000196
              2       255  SOLID187      0.016   0.000061
              3      3988  CONTA174      0.062   0.000016
              4      3988  TARGE170      0.000   0.000000
              5        88  CONTA174      0.000   0.000000
              6         1  TARGE170      0.000   0.000000
              7         1  MPC184        0.016   0.015625
       Time at end of element matrix formulation CP = 3.40625.                

       ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.rdb
        FOR POSSIBLE RESUME FROM THIS POINT
           FORCE CONVERGENCE VALUE  =   0.000      CRITERION=  0.5102E-04

       DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
        Number of equations =       80820,    Maximum wavefront =   1404

       *** NOTE ***                            CP =       4.391   TIME= 18:01:31
       The initial memory allocation (-m) has been exceeded.                  
        Supplemental memory allocations are being used.                       

        Process memory allocated for solver              =   553.277 MB
        Process memory required for in-core solution     =   467.341 MB
        Process memory required for out-of-core solution =   262.843 MB

        Total memory allocated for solver                =   959.635 MB
        Total memory required for in-core solution       =   790.123 MB
        Total memory required for out-of-core solution   =   367.606 MB

       *** NOTE ***                            CP =       4.391   TIME= 18:01:31
       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.                                                                  

       *** WARNING ***                         CP =       4.391   TIME= 18:01:31
       Pivoting has been activated for the Distributed Sparse Matrix Solver . 
       The memory required may greatly exceed the predicted amount.  In that  
       event, use the DSPOPTION command to change the memory mode and/or      
       memory size used by the Distributed Sparse Matrix Solver.              

       *** NOTE ***                            CP =       4.391   TIME= 18:01:31
       The system matrix is unsymmetric.                                      
       curEqn=  40566  totEqn=  40566 Job CP sec=      5.562
            Factor Done= 100% Factor Wall sec=      0.563 rate=      27.5 GFlops
       Distributed sparse solver maximum pivot= 68371621.1 at node 840 UY.    
       Distributed sparse solver minimum pivot= 0.99879707 at node 14176 UY.  
       Distributed sparse solver minimum pivot in absolute value= 0.99879707  
       at node 14176 UY.                                                      
           DISP CONVERGENCE VALUE   =  0.5000      CRITERION=  0.2551E-01
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.5000   
           DISP CONVERGENCE VALUE   =  0.2500      CRITERION=  0.2603E-01
           LINE SEARCH PARAMETER =  0.5000     SCALED MAX DOF INC = -0.2500   
           FORCE CONVERGENCE VALUE  =  0.1101E-05  CRITERION=  0.5206E-04 <<< CONVERGED

       *** WARNING ***                         CP =       8.547   TIME= 18:01:35
       A reference force value times the tolerance is used by the             
       Newton-Raphson method for checking convergence.  The calculated        
       reference FORCE CONVERGENCE VALUE = 6.17053349E-09 is less than a      
       threshold.  This threshold is internally calculated.  You can          
       overwrite it by specifying MINREF on the CNVTOL command.  Check        
       results carefully.                                                     
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2500   
           DISP CONVERGENCE VALUE   =  0.1609      CRITERION=  0.2656E-01
           LINE SEARCH PARAMETER =  0.6436     SCALED MAX DOF INC = -0.1609   
           FORCE CONVERGENCE VALUE  =  0.1816E-05  CRITERION=  0.5312E-04 <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.8910E-01
           DISP CONVERGENCE VALUE   =  0.6588E-01  CRITERION=  0.2710E-01
           LINE SEARCH PARAMETER =  0.7394     SCALED MAX DOF INC = -0.6588E-01
           FORCE CONVERGENCE VALUE  =  0.1693E-05  CRITERION=  0.5421E-04 <<< CONVERGED
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2322E-01
           DISP CONVERGENCE VALUE   =  0.2322E-01  CRITERION=  0.2766E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.2322E-01
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   4

         *** ELEMENT RESULT CALCULATION TIMES
           TYPE    NUMBER   ENAME      TOTAL CP  AVE CP

              1      3900  SOLID186      0.438   0.000112
              2       255  SOLID187      0.016   0.000061
              3      3964  CONTA174      0.062   0.000016
              5        88  CONTA174      0.000   0.000000
              7         1  MPC184        0.000   0.000000

         *** NODAL LOAD CALCULATION TIMES
           TYPE    NUMBER   ENAME      TOTAL CP  AVE CP

              1      3900  SOLID186      0.000   0.000000
              2       255  SOLID187      0.000   0.000000
              3      3964  CONTA174      0.000   0.000000
              5        88  CONTA174      0.000   0.000000
              7         1  MPC184        0.000   0.000000
       *** LOAD STEP     1   SUBSTEP     1  COMPLETED.    CUM ITER =      4
       *** TIME =  0.100000E-01     TIME INC =  0.100000E-01
       *** AUTO STEP TIME:  NEXT TIME INC = 0.10000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =  0.1070E-07  CRITERION=  0.5102E-04
           DISP CONVERGENCE VALUE   =  0.2408E-15  CRITERION=  0.2551E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2408E-15
           DISP CONVERGENCE VALUE   =  0.2408E-15  CRITERION=  0.2603E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.2408E-15
           FORCE CONVERGENCE VALUE  =  0.5534E-08  CRITERION=  0.5206E-04 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.1390E-15
           DISP CONVERGENCE VALUE   =  0.1390E-15  CRITERION=  0.2656E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC =  0.1390E-15
           FORCE CONVERGENCE VALUE  =  0.5038E-08  CRITERION=  0.5312E-04 <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     2  COMPLETED.    CUM ITER =      6
       *** TIME =  0.200000E-01     TIME INC =  0.100000E-01
       *** AUTO STEP TIME:  NEXT TIME INC = 0.10000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =  0.7496E-08  CRITERION=  0.5102E-04
           DISP CONVERGENCE VALUE   =  0.2600E-15  CRITERION=  0.2551E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.2600E-15
           DISP CONVERGENCE VALUE   =  0.2600E-15  CRITERION=  0.2603E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC =  0.2600E-15
           FORCE CONVERGENCE VALUE  =  0.5375E-08  CRITERION=  0.5206E-04 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.9855E-16
           DISP CONVERGENCE VALUE   =  0.9855E-16  CRITERION=  0.2656E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.9855E-16
           FORCE CONVERGENCE VALUE  =  0.5344E-08  CRITERION=  0.5312E-04 <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     3  COMPLETED.    CUM ITER =      8
       *** TIME =  0.300000E-01     TIME INC =  0.100000E-01
       *** AUTO STEP TIME:  NEXT TIME INC = 0.10000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =  0.8173E-08  CRITERION=  0.5102E-04
           DISP CONVERGENCE VALUE   =  0.2121E-15  CRITERION=  0.2551E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.2121E-15
           DISP CONVERGENCE VALUE   =  0.2121E-15  CRITERION=  0.2603E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC =  0.2121E-15
           FORCE CONVERGENCE VALUE  =  0.5306E-08  CRITERION=  0.5206E-04 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.1000E-15
           DISP CONVERGENCE VALUE   =  0.1000E-15  CRITERION=  0.2656E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.1000E-15
           FORCE CONVERGENCE VALUE  =  0.5584E-08  CRITERION=  0.5312E-04 <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     4  COMPLETED.    CUM ITER =     10
       *** TIME =  0.400000E-01     TIME INC =  0.100000E-01
       *** AUTO STEP TIME:  NEXT TIME INC = 0.10000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =  0.7482E-08  CRITERION=  0.5102E-04
           DISP CONVERGENCE VALUE   =  0.2192E-15  CRITERION=  0.2551E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2192E-15
           DISP CONVERGENCE VALUE   =  0.2192E-15  CRITERION=  0.2603E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.2192E-15
           FORCE CONVERGENCE VALUE  =  0.5359E-08  CRITERION=  0.5206E-04 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.9096E-16
           DISP CONVERGENCE VALUE   =  0.9096E-16  CRITERION=  0.2656E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC =  0.9096E-16
           FORCE CONVERGENCE VALUE  =  0.5652E-08  CRITERION=  0.5312E-04 <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     5  COMPLETED.    CUM ITER =     12
       *** TIME =  0.500000E-01     TIME INC =  0.100000E-01
       *** AUTO STEP TIME:  NEXT TIME INC = 0.10000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =  0.7310E-08  CRITERION=  0.5102E-04
           DISP CONVERGENCE VALUE   =  0.6637E-15  CRITERION=  0.2551E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.6637E-15
           DISP CONVERGENCE VALUE   =  0.6637E-15  CRITERION=  0.2603E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.6637E-15
           FORCE CONVERGENCE VALUE  =  0.6789E-07  CRITERION=  0.5206E-04 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.4441E-15
           DISP CONVERGENCE VALUE   =  0.4441E-15  CRITERION=  0.2656E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.4441E-15
           FORCE CONVERGENCE VALUE  =  0.6817E-07  CRITERION=  0.5312E-04 <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     6  COMPLETED.    CUM ITER =     14
       *** TIME =  0.600000E-01     TIME INC =  0.100000E-01
       *** AUTO STEP TIME:  NEXT TIME INC = 0.10000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =  0.1363E-06  CRITERION=  0.5102E-04
           DISP CONVERGENCE VALUE   =  0.6523E-15  CRITERION=  0.2551E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.6523E-15
           DISP CONVERGENCE VALUE   =  0.6523E-15  CRITERION=  0.2603E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC =  0.6523E-15
           FORCE CONVERGENCE VALUE  =  0.6835E-07  CRITERION=  0.5206E-04 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.4441E-15
           DISP CONVERGENCE VALUE   =  0.4441E-15  CRITERION=  0.2656E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.4441E-15
           FORCE CONVERGENCE VALUE  =  0.6782E-07  CRITERION=  0.5312E-04 <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     7  COMPLETED.    CUM ITER =     16
       *** TIME =  0.700000E-01     TIME INC =  0.100000E-01
       *** AUTO STEP TIME:  NEXT TIME INC = 0.10000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =  0.1453E-06  CRITERION=  0.5102E-04
           DISP CONVERGENCE VALUE   =  0.1146E-12  CRITERION=  0.2551E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.1146E-12
           DISP CONVERGENCE VALUE   =  0.1146E-12  CRITERION=  0.2603E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC =  0.1146E-12
           FORCE CONVERGENCE VALUE  =  0.5967E-08  CRITERION=  0.5206E-04 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.1359E-15
           DISP CONVERGENCE VALUE   =  0.1359E-15  CRITERION=  0.2656E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC =  0.1359E-15
           FORCE CONVERGENCE VALUE  =  0.5084E-08  CRITERION=  0.5312E-04 <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     8  COMPLETED.    CUM ITER =     18
       *** TIME =  0.800000E-01     TIME INC =  0.100000E-01
       *** AUTO STEP TIME:  NEXT TIME INC = 0.10000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =  0.1459E-06  CRITERION=  0.5102E-04
           DISP CONVERGENCE VALUE   =  0.1146E-12  CRITERION=  0.2551E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.1146E-12
           DISP CONVERGENCE VALUE   =  0.1146E-12  CRITERION=  0.2603E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.1146E-12
           FORCE CONVERGENCE VALUE  =  0.5631E-08  CRITERION=  0.5206E-04 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.1499E-15
           DISP CONVERGENCE VALUE   =  0.1499E-15  CRITERION=  0.2656E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.1499E-15
           FORCE CONVERGENCE VALUE  =  0.5314E-08  CRITERION=  0.5312E-04 <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     9  COMPLETED.    CUM ITER =     20
       *** TIME =  0.900000E-01     TIME INC =  0.100000E-01
       *** AUTO STEP TIME:  NEXT TIME INC = 0.10000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =   2289.      CRITERION=  0.5254E-01
           DISP CONVERGENCE VALUE   =  0.3749      CRITERION=  0.2551E-02
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.3749   
           DISP CONVERGENCE VALUE   =  0.3558      CRITERION=  0.2603E-02
           LINE SEARCH PARAMETER =  0.9493     SCALED MAX DOF INC =  0.3558   
           FORCE CONVERGENCE VALUE  =  0.2480E+05  CRITERION=  0.4034   
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2093   
           DISP CONVERGENCE VALUE   =  0.2093      CRITERION=  0.2656E-01
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.2093   
           FORCE CONVERGENCE VALUE  =   1454.      CRITERION=  0.5428E-01
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.1752   
           DISP CONVERGENCE VALUE   =  0.1336      CRITERION=  0.2710E-01
           LINE SEARCH PARAMETER =  0.7625     SCALED MAX DOF INC =  0.1336   
           FORCE CONVERGENCE VALUE  =   3580.      CRITERION=  0.1221E-01
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.9788E-01
           DISP CONVERGENCE VALUE   =  0.9788E-01  CRITERION=  0.2766E-01
           LINE SEARCH PARAMETER =   1.000     SCALED MAX DOF INC = -0.9788E-01
           FORCE CONVERGENCE VALUE  =   777.8      CRITERION=  0.1609   
          EQUIL ITER   5 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.3449   
           DISP CONVERGENCE VALUE   =  0.1725E-01  CRITERION=  0.2822E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.1725E-01
           FORCE CONVERGENCE VALUE  =   750.0      CRITERION=  0.1561   
          EQUIL ITER   6 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.1110   
           DISP CONVERGENCE VALUE   =  0.1109      CRITERION=  0.2880E-01
           LINE SEARCH PARAMETER =  0.9993     SCALED MAX DOF INC = -0.1109   
           FORCE CONVERGENCE VALUE  =   1026.      CRITERION=  0.1722   
          EQUIL ITER   7 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.2887   
           DISP CONVERGENCE VALUE   =  0.1443E-01  CRITERION=  0.2939E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.1443E-01
           FORCE CONVERGENCE VALUE  =   982.3      CRITERION=  0.1669   
          EQUIL ITER   8 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.4275E-01
           DISP CONVERGENCE VALUE   =  0.4235E-01  CRITERION=  0.2999E-01
           LINE SEARCH PARAMETER =  0.9905     SCALED MAX DOF INC = -0.4235E-01
           FORCE CONVERGENCE VALUE  =   112.6      CRITERION=  0.1805   
          EQUIL ITER   9 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.4186   
           DISP CONVERGENCE VALUE   =  0.2093E-01  CRITERION=  0.3060E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.2093E-01
           FORCE CONVERGENCE VALUE  =   127.5      CRITERION=  0.3503   
          EQUIL ITER  10 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.3834E-01
           DISP CONVERGENCE VALUE   =  0.3676E-01  CRITERION=  0.3122E-01
           LINE SEARCH PARAMETER =  0.9586     SCALED MAX DOF INC = -0.3676E-01
           FORCE CONVERGENCE VALUE  =   90.51      CRITERION=  0.2760   
          EQUIL ITER  11 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.4418   
           DISP CONVERGENCE VALUE   =  0.2209E-01  CRITERION=  0.3186E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.2209E-01
           FORCE CONVERGENCE VALUE  =   108.5      CRITERION=  0.5358   
          EQUIL ITER  12 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2592E-01
           DISP CONVERGENCE VALUE   =  0.2551E-01  CRITERION=  0.3251E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.9841     SCALED MAX DOF INC = -0.2551E-01
           FORCE CONVERGENCE VALUE  =   39.97      CRITERION=  0.6009   
          EQUIL ITER  13 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.4698   
           DISP CONVERGENCE VALUE   =  0.2349E-01  CRITERION=  0.3317E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.2349E-01
           FORCE CONVERGENCE VALUE  =   63.79      CRITERION=  0.5834   
          EQUIL ITER  14 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2571E-01
           DISP CONVERGENCE VALUE   =  0.2534E-01  CRITERION=  0.3385E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.9858     SCALED MAX DOF INC = -0.2534E-01
           FORCE CONVERGENCE VALUE  =   40.11      CRITERION=  0.6455   
          EQUIL ITER  15 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.4764   
           DISP CONVERGENCE VALUE   =  0.2382E-01  CRITERION=  0.3454E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.2382E-01
           FORCE CONVERGENCE VALUE  =   63.81      CRITERION=  0.6268   
          EQUIL ITER  16 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2444E-01
           DISP CONVERGENCE VALUE   =  0.2416E-01  CRITERION=  0.3524E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.9886     SCALED MAX DOF INC = -0.2416E-01
           FORCE CONVERGENCE VALUE  =   38.15      CRITERION=  0.6749   
          EQUIL ITER  17 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.4792   
           DISP CONVERGENCE VALUE   =  0.2396E-01  CRITERION=  0.3596E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.2396E-01
           FORCE CONVERGENCE VALUE  =   61.78      CRITERION=  0.6553   
          EQUIL ITER  18 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2438E-01
           DISP CONVERGENCE VALUE   =  0.2411E-01  CRITERION=  0.3670E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.9888     SCALED MAX DOF INC = -0.2411E-01
           FORCE CONVERGENCE VALUE  =   38.13      CRITERION=  0.7045   
          EQUIL ITER  19 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.4798   
           DISP CONVERGENCE VALUE   =  0.2399E-01  CRITERION=  0.3745E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.2399E-01
           FORCE CONVERGENCE VALUE  =   61.73      CRITERION=  0.6840   
          EQUIL ITER  20 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2429E-01
           DISP CONVERGENCE VALUE   =  0.2402E-01  CRITERION=  0.3821E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.9890     SCALED MAX DOF INC = -0.2402E-01
           FORCE CONVERGENCE VALUE  =   38.01      CRITERION=  0.7338   
          EQUIL ITER  21 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.4801   
           DISP CONVERGENCE VALUE   =  0.2400E-01  CRITERION=  0.3899E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.2400E-01
           FORCE CONVERGENCE VALUE  =   61.60      CRITERION=  0.7125   
          EQUIL ITER  22 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2428E-01
           DISP CONVERGENCE VALUE   =  0.2402E-01  CRITERION=  0.3979E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.9891     SCALED MAX DOF INC = -0.2402E-01
           FORCE CONVERGENCE VALUE  =   38.00      CRITERION=  0.7642   
          EQUIL ITER  23 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.4801   
           DISP CONVERGENCE VALUE   =  0.2401E-01  CRITERION=  0.4060E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.5000E-01 SCALED MAX DOF INC =  0.2401E-01
           FORCE CONVERGENCE VALUE  =   61.59      CRITERION=  0.7421   
          EQUIL ITER  24 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2427E-01
           DISP CONVERGENCE VALUE   =  0.2401E-01  CRITERION=  0.4143E-01 <<< CONVERGED
           LINE SEARCH PARAMETER =  0.9891     SCALED MAX DOF INC = -0.2401E-01

      All

       

       

    • Erik Kostson
      Ansys Employee

      Hi

       

      For impact (velocity on a sphere) one would use explicit dynamics - there are many tutorials on that search and you will find.

      All the best

       

      Erik

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