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  3. Non-linear convergence issue

Non-linear convergence issue

    • September 5, 2024 at 1:40 pm
      fraser.shields
      Subscriber

      Hello,

       

      I am attempting to model a soft poroelastic solid elements (CPT216) which is reinforced by stiff orthotropic linear elastic shell elements. The shell elements themselves have reinforcement fibres running parallel to the wall length, these are what provide the stiffness. Unfortunately, I am unable to get a non-linear solution to converges - the fluid flow will not converge. Is there any way I can upload my project file onto here, so someone can check the model? 

       

      Here is the solution information:

       

      Solver Output

       


       Ansys Mechanical Enterprise Academic Research    


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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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                *****  ANSYS COMMAND LINE ARGUMENTS  *****
        BATCH MODE REQUESTED (-b)    = NOLIST
        INPUT FILE COPY MODE (-c)    = COPY
        DISTRIBUTED MEMORY PARALLEL REQUESTED
            10 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS
          TOTAL OF    10 CORES REQUESTED
        INPUT FILE NAME              = C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7\dummy.dat
        OUTPUT FILE NAME             = C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7\solve.out
        START-UP FILE MODE           = NOREAD
        STOP FILE MODE               = NOREAD

       RELEASE= 2022 R1              BUILD= 22.1      UP20211129   VERSION=WINDOWS x64
       CURRENT JOBNAME=file0  14:08:47  SEP 05, 2024 CP=      0.047


       PARAMETER _DS_PROGRESS =     999.0000000   

       /INPUT FILE= ds.dat  LINE=       0



       *** NOTE ***                            CP =       0.203   TIME= 14:08:48
       The /CONFIG,NOELDB command is not valid in a Distributed ANSYS         
       solution.  Command is ignored.                                         

       *GET  _WALLSTRT  FROM  ACTI  ITEM=TIME WALL  VALUE=  14.1466667   

       TITLE=
       800um_simplified_TEST--Static Structural (A5)                                

        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\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7\

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

       PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\800um_simplified_TEST_files\dp0\SYS\MECH\

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

       PARAMETER _WB_USERFILES_DIR(1) = C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\800um_simplified_TEST_files\user_files\
       --- Data in consistent uMKS units. See Solving Units in the help system for mor

       uMKS UNITS SPECIFIED FOR INTERNAL   
        LENGTH      = MICROMETERS (um)
        MASS        = KILOGRAM (kg)
        TIME        = SECONDS (sec)
        TEMPERATURE = CELSIUS (C)
        TOFFSET     = 273.0
        FORCE       = MICRONEWTON (uN)
        HEAT        = PICOJOULES (pJ)

       INPUT  UNITS ARE ALSO SET TO UMKS

       *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2022 R1          22.1     ***
       DISTRIBUTED Ansys Mechanical Enterprise Academic Research    

       00000000  VERSION=WINDOWS x64   14:08:48  SEP 05, 2024 CP=      0.203

       800um_simplified_TEST--Static Structural (A5)                                



                ***** ANSYS ANALYSIS DEFINITION (PREP7) *****
       *********** Nodes for the whole assembly ***********
       *********** Elements for Body 1 "Solid111" ***********
       *********** Elements for Body 2 "Solid111" ***********
       *********** Elements for Body 3 "Solid111" ***********
       *********** Elements for Body 4 "Solid1111" ***********
       *********** Elements for Body 5 "Solid1111" ***********
       *********** Elements for Body 6 "Solid1111" ***********
       *********** Elements for Body 7 "Solid11111" ***********
       *********** Elements for Body 8 "Solid1111" ***********
       *********** Elements for Body 9 "Solid11111" ***********
       *********** Elements for Body 10 "Solid111111" ***********
       *********** Elements for Body 11 "Solid11111" ***********
       *********** Elements for Body 12 "Solid1111" ***********
       *********** Elements for Body 13 "Solid111111" ***********
       *********** Elements for Body 14 "Solid1111111" ***********
       *********** Elements for Body 15 "Surface" ***********
       *********** Elements for Body 16 "Surface" ***********
       *********** Elements for Body 17 "Surface" ***********
       *********** Elements for Body 18 "Surface" ***********
       *********** Elements for Body 19 "Surface" ***********
       *********** Elements for Body 20 "Surface" ***********
       *********** Elements for Body 21 "Surface1" ***********
       *********** Elements for Body 22 "Surface1" ***********
       *********** Elements for Body 23 "Surface1" ***********
       *********** Elements for Body 24 "Surface1" ***********
       *********** Elements for Body 25 "Surface1" ***********
       *********** Elements for Body 26 "Surface11" ***********
       *********** Elements for Body 27 "Surface1" ***********
       *********** Elements for Body 28 "Surface1" ***********
       *********** Elements for Body 29 "Surface1" ***********
       *********** Elements for Body 30 "Surface1" ***********
       *********** Elements for Body 31 "Surface1" ***********
       *********** Elements for Body 32 "Surface1" ***********
       *********** Elements for Body 33 "Surface1" ***********
       *********** Elements for Body 34 "Surface11" ***********
       *********** Elements for Body 35 "Surface11" ***********
       *********** Elements for Body 36 "Surface11" ***********
       *********** Elements for Body 37 "Surface1" ***********
       *********** Elements for Body 38 "Surface1" ***********
       *********** Elements for Body 39 "Surface11" ***********
       *********** Elements for Body 40 "Surface11" ***********
       *********** Send User Defined Coordinate System(s) ***********
       *********** Send Element Orientation **********
        Sending Element Orientation Object: "Element Orientation"
        Sending Element Orientation Object: "Element Orientation 2"
       *********** Set Reference Temperature ***********
       *********** Send Materials ***********
       *********** Send Sheet Properties ***********
       *********** Send Named Selection as Element Component ***********
       *********** Send Named Selection as Element Component ***********
       ********* Frictionless Supports X *********
       ********* Frictionless Supports Z *********
       ******* Constant Zero Displacement Y *******
       *********** Create Displacement Tables and Functions ******

       LIST DATA TABLE  PLAS  FOR MATERIAL     14

       *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2022 R1          22.1     ***
       DISTRIBUTED Ansys Mechanical Enterprise Academic Research    

       00000000  VERSION=WINDOWS x64   14:08:48  SEP 05, 2024 CP=      0.672

       800um_simplified_TEST--Static Structural (A5)                                



                     PLASTIC  (PLAS) Table For Material    14
                     ISOTROPIC HARDENING PLASTICITY                                                 

                           1
       Temps     2.3000000e+01
            PlStrain       Stress 
       0.0000000e+00 5.9620000e+00
       2.9670000e-03 1.1480000e+01
       8.3930000e-03 1.5190000e+01
       1.5420000e-02 1.7980000e+01
       2.3740000e-02 2.0030000e+01
       3.3180000e-02 2.1570000e+01
       4.3610000e-02 2.2760000e+01
       5.4960000e-02 2.3600000e+01
       6.7140000e-02 2.4230000e+01
       8.0120000e-02 2.4640000e+01



       ***** ROUTINE COMPLETED *****  CP =         0.672


       --- Number of total nodes = 10043
       --- Number of contact elements = 0
       --- Number of spring elements = 0
       --- Number of bearing elements = 0
       --- Number of solid elements = 10310
       --- Number of condensed parts = 0
       --- Number of total elements = 10310

       *GET  _WALLBSOL  FROM  ACTI  ITEM=TIME WALL  VALUE=  14.1466667   
       ****************************************************************************
       *************************    SOLUTION       ********************************
       ****************************************************************************

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


       PERFORM A STATIC ANALYSIS
        THIS WILL BE A NEW ANALYSIS

       LARGE DEFORMATION ANALYSIS

       PARAMETER _THICKRATIO =     0.000000000   

       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.

       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 3 ****************
       *** Set Displacements ***
       CMBLOCK read of NODE component _CM1384UY_YP  completed

       SELECT      COMPONENT _CM1384UY_YP                   

       SPECIFIED CONSTRAINT UY   FOR SELECTED NODES            1 TO       10043 BY           1
       SET ACCORDING TO TABLE PARAMETER = _LOADVARI1384YP

       ALL SELECT   FOR ITEM=NODE COMPONENT=   
        IN RANGE         1 TO      10043 STEP          1

            10043  NODES (OF      10043  DEFINED) SELECTED BY NSEL  COMMAND.
       *** Component For All Non-Zero UY Displacements ***

       SELECT      COMPONENT _CM1384UY_YP                   

       DEFINITION OF COMPONENT = _DISPNONZEROUY  ENTITY=NODE

       ALL SELECT   FOR ITEM=NODE COMPONENT=   
        IN RANGE         1 TO      10043 STEP          1

            10043  NODES (OF      10043  DEFINED) SELECTED BY NSEL  COMMAND.

       PRINTOUT RESUMED BY /GOP

       USE AUTOMATIC TIME STEPPING THIS LOAD STEP

       USE       5 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL  DEGREES OF FREEDOM
       FOR AUTOMATIC TIME STEPPING:
         USE   1000 SUBSTEPS AS A MAXIMUM
         USE      1 SUBSTEPS AS A MINIMUM

       TIME= 0.10000   

       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 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

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

       FINISH SOLUTION PROCESSING


       ***** ROUTINE COMPLETED *****  CP =         0.672



       *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2022 R1          22.1     ***
       DISTRIBUTED Ansys Mechanical Enterprise Academic Research    

       00000000  VERSION=WINDOWS x64   14:08:48  SEP 05, 2024 CP=      0.672

       800um_simplified_TEST--Static Structural (A5)                                



                ***** ANSYS ANALYSIS DEFINITION (PREP7) *****

       ELEMENT TYPE       9991 IS CPT215       3D COUPLED SOLID           
        KEYOPT( 1- 6)=        0      0      0        0      0      0
        KEYOPT( 7-12)=        0      0      0        0      0      0
        KEYOPT(13-18)=        0      0      0        0      0      0

       CURRENT NODAL DOF SET IS  UX    UY    UZ    ROTX  ROTY  ROTZ
        THREE-DIMENSIONAL MODEL

       ELEMENT TYPE    9991 IS CPT215       3D COUPLED SOLID           
        KEYOPT( 1- 6)=        0      0      0        0      0      0
        KEYOPT( 7-12)=        0      0      0        0      0      1
        KEYOPT(13-18)=        0      0      0        0      0      0

       CURRENT NODAL DOF SET IS  UX    UY    UZ    ROTX  ROTY  ROTZ  PRES
        THREE-DIMENSIONAL MODEL

       ELEMENT TYPE    9991 IS CPT215       3D COUPLED SOLID           
        KEYOPT( 1- 6)=        0      0      0        0      0      1
        KEYOPT( 7-12)=        0      0      0        0      0      1
        KEYOPT(13-18)=        0      0      0        0      0      0

       CURRENT NODAL DOF SET IS  UX    UY    UZ    ROTX  ROTY  ROTZ  PRES
        THREE-DIMENSIONAL MODEL

       SELECT       FOR ITEM=TYPE COMPONENT=   
        IN RANGE         1 TO         14 STEP          1

             8550  ELEMENTS (OF      10310  DEFINED) SELECTED BY  ESEL  COMMAND.

       MODIFY ALL SELECTED ELEMENTS TO HAVE  TYPE =      9991

       SELECT ALL ENTITIES OF TYPE= ALL  AND BELOW

       MATERIAL      99999     EX   =  0.3000000E-02     

       MATERIAL      99999     PRXY =  0.4900000         

       PARAMETER FPX =     100000.0000   

       PARAMETER ALPHA =     1.000000000   

         FLUID PERMEABILITY OPTION FOR MATERIAL 99999
       DATA FOR  PM  TABLE FOR MATERIAL   99999 AT TEMPERATURE=  23.0000   
       LOC=  1 1.00000e+05     1.00000e+05     1.00000e+05   


         FLUID BIOT OPTION FOR MATERIAL 99999
       DATA FOR  PM  TABLE FOR MATERIAL   99999 AT TEMPERATURE=  23.0000   
       LOC=  1 1.00000e+00   


       NONE SELECT  FOR ITEM=ELEM COMPONENT=   
        IN RANGE         1 TO      16720 STEP          1

                0  ELEMENTS (OF      10310  DEFINED) SELECTED BY ESEL  COMMAND.

       MATERIAL      88888     EX   =  0.1000000E-19     

       MATERIAL      88888     PRXY =   0.000000         

       SELECT       FOR ITEM=TYPE COMPONENT=   
        IN RANGE        15 TO         40 STEP          1

             1760  ELEMENTS (OF      10310  DEFINED) SELECTED BY  ESEL  COMMAND.

       SET MATERIAL OF SELECTED ELEMENTS TO 88888

       MATERIAL      88889     EX   =   300.0000         

       MATERIAL      88889     PRXY =   0.000000         

       SELECT ALL ENTITIES OF TYPE= ALL  AND BELOW
                                           
         INPUT SECTION ID NUMBER               1
         INPUT SECTION TYPE                 REINF
         INPUT REINF SECTION SUBTYPE        SMEA
         INPUT REINF SECTION NAME           1      

       SECTION ID NUMBER=        1
                          
         SECTION ID NUMBER IS:            1
          Reinforcing Behavior: Tension Only
          Remove Base Material: YES
          Stress State        : Uni-axial
           REINFORCEMENT  #        1
              MatID         Area        Spacing  iEsys     Ori. Angle
              88889       50.0000        8.0000    12        0.0000
              PATTern        n
                LAYN         1


       SELECT      COMPONENT KCS_12                         
       GENERATE REINF ELEMENTS FROM THE SELECTED ELEMENTS

       NUMBER OF ELEMENT TYPES CREATED =          1
       MAXIMUM ELEMENT TYPE NUMBER     =       9992
       Use ETLIST command to list new element types.

       NUMBER OF REINF ELEMENT CREATED =        880
       MAXIMUM ELEMENT NUMBER          =      17600
       Use ELIST command to list new elements.

       SELECT ALL ENTITIES OF TYPE= ALL  AND BELOW
                                           
         INPUT SECTION ID NUMBER               2
         INPUT SECTION TYPE                 REINF
         INPUT REINF SECTION SUBTYPE        SMEA
         INPUT REINF SECTION NAME           2      

       SECTION ID NUMBER=        2
                          
         SECTION ID NUMBER IS:            2
          Reinforcing Behavior: Tension Only
          Remove Base Material: YES
          Stress State        : Uni-axial
           REINFORCEMENT  #        1
              MatID         Area        Spacing  iEsys     Ori. Angle
              88889       50.0000        8.0000    13        0.0000
              PATTern        n
                LAYN         1


       SELECT      COMPONENT KCS_13                         
       GENERATE REINF ELEMENTS FROM THE SELECTED ELEMENTS

       NUMBER OF REINF ELEMENT CREATED =        880
       MAXIMUM ELEMENT NUMBER          =      18480
       Use ELIST command to list new elements.

       SELECT ALL ENTITIES OF TYPE= ALL  AND BELOW

       SELECT       FOR ITEM=TYPE COMPONENT=   
        IN RANGE      9991 TO       9991 STEP          1

             8550  ELEMENTS (OF      12070  DEFINED) SELECTED BY  ESEL  COMMAND.

       SET MATERIAL OF SELECTED ELEMENTS TO 99999

       SELECT ALL ENTITIES OF TYPE= ALL  AND BELOW

       SELECT ALL ENTITIES OF TYPE= ALL  AND BELOW

       SELECT       FOR ITEM=LOC  COMPONENT=Y     BETWEEN  1000.0     AND   1000.0   
         KABS=  0.  TOLERANCE=  5.00000   

              913  NODES (OF      10043  DEFINED) SELECTED BY  NSEL  COMMAND.

       ALSO SELECT  FOR ITEM=LOC  COMPONENT=Y     BETWEEN  0.0000     AND   0.0000   
         KABS=  0.  TOLERANCE= 0.100000E-05

             1826  NODES (OF      10043  DEFINED) SELECTED BY  NSEL  COMMAND.

       GENERATE SURFACE LOAD FFLX ON SURFACE DEFINED BY ALL SELECTED NODES
       VALUE =   0.00000000   

       NUMBER OF FFLX ELEMENT FACE LOADS STORED =       1710

       SELECT ALL ENTITIES OF TYPE= ALL  AND BELOW

       ACTIVE COORDINATE SYSTEM SET TO          5  (CYLINDRICAL) Y- CYL. AXIS

       SELECT       FOR ITEM=LOC  COMPONENT=X     BETWEEN  3250.0     AND   3250.0   
         KABS=  0.  TOLERANCE=  16.2500   

              583  NODES (OF      10043  DEFINED) SELECTED BY  NSEL  COMMAND.

       SPECIFIED CONSTRAINT PRES FOR SELECTED NODES            1 TO       10043 BY           1
       REAL=  0.00000000       IMAG=  0.00000000   

       SELECT ALL ENTITIES OF TYPE= ALL  AND BELOW

       ACTIVE COORDINATE SYSTEM SET TO          0  (CARTESIAN) 

       SELECT ALL ENTITIES OF TYPE= ALL  AND BELOW


       ***** ROUTINE COMPLETED *****  CP =         0.984



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

       *GET  ANSINTER_  FROM  ACTI  ITEM=INT        VALUE=  0.00000000   

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

       *ENDIF

       *** NOTE ***                            CP =       1.125   TIME= 14:08:48
       The automatic domain decomposition logic has selected the MESH domain  
       decomposition method with 10 processes per solution.                   

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

       *** WARNING ***                         CP =       1.281   TIME= 14:08:48
       Element shape checking is currently inactive.  Issue SHPP,ON or        
       SHPP,WARN to reactivate, if desired.                                   

       *** WARNING ***                         CP =       1.281   TIME= 14:08:48
       CPT215 wedges are recommended only in regions of relatively low stress 
       gradients.                                                             

       *** NOTE ***                            CP =       1.281   TIME= 14:08:48
       The model data was checked and warning messages were found.            
        Please review output or errors file ( C:\Users\mbgm4fs3\OneDrive -    
       The University of Manchester\PhD\Experimental\Data\2.                  
       Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7\file0.err ) for    
       these warning messages.                                                

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

       ELEMENT TYPE        15 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        16 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        17 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        18 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        19 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        20 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        21 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        22 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        23 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        24 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        25 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        26 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        27 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        28 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        29 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        30 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        31 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        32 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        33 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        34 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        35 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        36 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        37 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        38 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        39 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0

       ELEMENT TYPE        40 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
       MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
       HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
       KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
       IT MANUALLY IF NECESSARY.
        KEYOPT(1-12)=    0    0    2    0    0    0    0    2    0    0    0    0



       *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2022 R1          22.1     ***
       DISTRIBUTED Ansys Mechanical Enterprise Academic Research    

       00000000  VERSION=WINDOWS x64   14:08:48  SEP 05, 2024 CP=      1.438

       800um_simplified_TEST--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   ROTX ROTY ROTZ PRES
         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 . . . . . . . . . . . . .PROGRAM CHOSEN  
         GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .UNSYMMETRIC

       *** NOTE ***                            CP =       1.750   TIME= 14:08:48
       The RESCONTROL command does not support fluid analyses.  The RESCONTROL
       command settings have been de-activated.                               

       *** NOTE ***                            CP =       1.750   TIME= 14:08:48
       This nonlinear analysis defaults to using the full Newton-Raphson      
       solution procedure.  This can be modified using the NROPT command.     

       *** NOTE ***                            CP =       1.750   TIME= 14:08:48
       Internal nodes from 10044 to 18593 are created.                        
       8550 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: 12070
        ...Number of nodes:    18593
        ...Decompose to 10 CPU domains
        ...Element load balance ratio =     1.708


                            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. . . . . . . . . . 0.10000   
         AUTOMATIC TIME STEPPING . . . . . . . . . . . .    ON
            INITIAL NUMBER OF SUBSTEPS . . . . . . . . .     5
            MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . .  1000
            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) 
         NODAL DOF SOLUTION LIMIT. . . . . . . . . . . . 0.10000E+10
         CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS
         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              
            STRS        ALL              
            EPEL        ALL              
            EPPL        ALL              
            CONT        ALL              


       SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr                                                                                                                                                                                                                                                          

       *** NOTE ***                            CP =       3.000   TIME= 14:08:48
       Predictor is ON by default for structural elements with rotational     
       degrees of freedom.  Use the PRED,OFF command to turn the predictor    
       OFF if it adversely affects the convergence.                           


       Range of element maximum matrix coefficients in global coordinates
       Maximum = 468.75 at element 18080.                                     
       Minimum = 3.511720105E-17 at element 15871.                            

       *** WARNING ***                         CP =       3.266   TIME= 14:08:48
       Coefficient ratio exceeds 1.0e8 - Check results.                       

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

             15        80  SHELL181      0.000   0.000000
             16        40  SHELL181      0.000   0.000000
             17        80  SHELL181      0.000   0.000000
             18        80  SHELL181      0.016   0.000195
             19        80  SHELL181      0.000   0.000000
             20        80  SHELL181      0.000   0.000000
             21        80  SHELL181      0.016   0.000195
             22        80  SHELL181      0.016   0.000195
             23        80  SHELL181      0.000   0.000000
             24        40  SHELL181      0.000   0.000000
             25        80  SHELL181      0.031   0.000391
             26        80  SHELL181      0.016   0.000195
             27        40  SHELL181      0.000   0.000000
             28        80  SHELL181      0.016   0.000195
             29        40  SHELL181      0.000   0.000000
             30        40  SHELL181      0.016   0.000391
             31        40  SHELL181      0.016   0.000391
             32        40  SHELL181      0.000   0.000000
             33        40  SHELL181      0.000   0.000000
             34        80  SHELL181      0.016   0.000195
             35        80  SHELL181      0.000   0.000000
             36        80  SHELL181      0.000   0.000000
             37        80  SHELL181      0.016   0.000195
             38        80  SHELL181      0.000   0.000000
             39        80  SHELL181      0.000   0.000000
             40        80  SHELL181      0.016   0.000195
           9991      8550  CPT215        1.359   0.000159
           9992      1760  REINF265      0.047   0.000027
       Time at end of element matrix formulation CP = 3.265625.               
           FORCE CONVERGENCE VALUE  =  0.7561      CRITERION=  0.3857E-02
           MOMENT CONVERGENCE VALUE =  0.1102E-35  CRITERION=  0.2722E-01
           FL FLOW CONVERGENCE VALUE=  0.3939E+05  CRITERION=   201.0   

       DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
        Number of equations =       51208,    Maximum wavefront =    245

        Process memory allocated for solver              =   144.271 MB
        Process memory required for in-core solution     =   101.080 MB
        Process memory required for out-of-core solution =    49.924 MB

        Total memory allocated for solver                =  1215.992 MB
        Total memory required for in-core solution       =   837.109 MB
        Total memory required for out-of-core solution   =   404.072 MB

       *** NOTE ***                            CP =       3.531   TIME= 14:08:48
       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 =       3.531   TIME= 14:08:48
       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 =       3.531   TIME= 14:08:48
       The system matrix is unsymmetric.                                      
       curEqn=   6154  totEqn=   6154 Job CP sec=      4.281
            Factor Done=  97% Factor Wall sec=      0.640 rate=       9.3 GFlops
       Distributed sparse solver maximum pivot= 5.229458564E+11 at node 9241  
       UX.                                                                    
       Distributed sparse solver minimum pivot= -2243515.26 at node 3008 PRES.
       Distributed sparse solver minimum pivot in absolute value= 20773.7634  
       at node 9869 ROTX.                                                     
           DISP CONVERGENCE VALUE   =  0.4267      CRITERION=  0.2177E-01
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.4267   
           FORCE CONVERGENCE VALUE  =   3.738      CRITERION=  0.2288E-01
           MOMENT CONVERGENCE VALUE =  0.1611E-22  CRITERION=  0.1614     <<< CONVERGED

       *** WARNING ***                         CP =       4.578   TIME= 14:08:50
       A reference moment value times the tolerance is used by the            
       Newton-Raphson method for checking convergence.  The calculated        
       reference MOMENT CONVERGENCE VALUE = 0 is less than a threshold.  This 
       threshold is internally calculated.  You can overwrite it by           
       specifying MINREF on the CNVTOL command.  Check results carefully.     
           FL FLOW CONVERGENCE VALUE=   34.91      CRITERION=  0.1406   
           DISP CONVERGENCE VALUE   =  0.9295E-03  CRITERION=  0.2226E-01 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.9295E-03
           FORCE CONVERGENCE VALUE  =  0.7697E-04  CRITERION=  0.2341E-01 <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.1082E-23  CRITERION=  0.1652     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.8047E-01  CRITERION=  0.1433     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2

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

             15        80  SHELL181      0.016   0.000195
             16        40  SHELL181      0.000   0.000000
             17        80  SHELL181      0.000   0.000000
             18        80  SHELL181      0.000   0.000000
             19        80  SHELL181      0.000   0.000000
             20        80  SHELL181      0.000   0.000000
             21        80  SHELL181      0.000   0.000000
             22        80  SHELL181      0.000   0.000000
             23        80  SHELL181      0.000   0.000000
             24        40  SHELL181      0.000   0.000000
             25        80  SHELL181      0.016   0.000195
             26        80  SHELL181      0.016   0.000195
             27        40  SHELL181      0.000   0.000000
             28        80  SHELL181      0.000   0.000000
             29        40  SHELL181      0.000   0.000000
             30        40  SHELL181      0.016   0.000391
             31        40  SHELL181      0.016   0.000391
             32        40  SHELL181      0.000   0.000000
             33        40  SHELL181      0.000   0.000000
             34        80  SHELL181      0.000   0.000000
             35        80  SHELL181      0.000   0.000000
             36        80  SHELL181      0.000   0.000000
             37        80  SHELL181      0.016   0.000195
             38        80  SHELL181      0.000   0.000000
             39        80  SHELL181      0.000   0.000000
             40        80  SHELL181      0.000   0.000000
           9991      8550  CPT215        0.953   0.000111
           9992      1760  REINF265      0.062   0.000036

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

             15        80  SHELL181      0.000   0.000000
             16        40  SHELL181      0.000   0.000000
             17        80  SHELL181      0.000   0.000000
             18        80  SHELL181      0.000   0.000000
             19        80  SHELL181      0.000   0.000000
             20        80  SHELL181      0.000   0.000000
             21        80  SHELL181      0.000   0.000000
             22        80  SHELL181      0.000   0.000000
             23        80  SHELL181      0.000   0.000000
             24        40  SHELL181      0.000   0.000000
             25        80  SHELL181      0.000   0.000000
             26        80  SHELL181      0.000   0.000000
             27        40  SHELL181      0.000   0.000000
             28        80  SHELL181      0.000   0.000000
             29        40  SHELL181      0.000   0.000000
             30        40  SHELL181      0.000   0.000000
             31        40  SHELL181      0.000   0.000000
             32        40  SHELL181      0.000   0.000000
             33        40  SHELL181      0.000   0.000000
             34        80  SHELL181      0.000   0.000000
             35        80  SHELL181      0.000   0.000000
             36        80  SHELL181      0.000   0.000000
             37        80  SHELL181      0.000   0.000000
             38        80  SHELL181      0.000   0.000000
             39        80  SHELL181      0.000   0.000000
             40        80  SHELL181      0.000   0.000000
           9991      8550  CPT215        0.047   0.000005
           9992      1760  REINF265      0.000   0.000000
       *** LOAD STEP     1   SUBSTEP     1  COMPLETED.    CUM ITER =      2
       *** TIME =  0.200000E-01     TIME INC =  0.200000E-01
       *** MAX PORE PRESSURE STEP = 0.1063E-04
       *** AUTO STEP TIME:  NEXT TIME INC = 0.20000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =   7.518      CRITERION=  0.4505E-01
           MOMENT CONVERGENCE VALUE =  0.3464E-22  CRITERION=  0.3179   
           FL FLOW CONVERGENCE VALUE=   48.48      CRITERION=  0.1475   
           DISP CONVERGENCE VALUE   =  0.1806E-02  CRITERION=  0.2187E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.1806E-02
           FORCE CONVERGENCE VALUE  =  0.2186E-03  CRITERION=  0.4609E-01 <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.2216E-23  CRITERION=  0.3252     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.1420      CRITERION=  0.2256     <<< CONVERGED
           DISP CONVERGENCE VALUE   =  0.2321E-04  CRITERION=  0.2232E-01 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.2321E-04
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     2  COMPLETED.    CUM ITER =      4
       *** TIME =  0.400000E-01     TIME INC =  0.200000E-01
       *** MAX PORE PRESSURE STEP = 0.9987E-05
       *** AUTO TIME STEP:  NEXT TIME INC = 0.30000E-01  INCREASED (FACTOR = 1.5000)

           FORCE CONVERGENCE VALUE  =   14.23      CRITERION=  0.7935E-01
           MOMENT CONVERGENCE VALUE =  0.7454E-22  CRITERION=  0.5598   
           FL FLOW CONVERGENCE VALUE=   85.10      CRITERION=  0.3473   
           DISP CONVERGENCE VALUE   =  0.3344E-02  CRITERION=  0.3296E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.3344E-02
           FORCE CONVERGENCE VALUE  =  0.8090E-03  CRITERION=  0.8120E-01 <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6337E-23  CRITERION=  0.5729     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.4175      CRITERION=  0.3764   
           DISP CONVERGENCE VALUE   =  0.7817E-04  CRITERION=  0.3363E-01 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.7817E-04
           FORCE CONVERGENCE VALUE  =  0.3357E-06  CRITERION=  0.8286E-01 <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.2434E-27  CRITERION=  0.5846     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.5830E-02  CRITERION=  0.3841     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     3  COMPLETED.    CUM ITER =      6
       *** TIME =  0.700000E-01     TIME INC =  0.300000E-01
       *** MAX PORE PRESSURE STEP = 0.1471E-04
       *** AUTO STEP TIME:  NEXT TIME INC = 0.30000E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =   17.30      CRITERION=  0.1142   
           MOMENT CONVERGENCE VALUE =  0.9108E-22  CRITERION=  0.8056   
           FL FLOW CONVERGENCE VALUE=   82.59      CRITERION=  0.3852   
           DISP CONVERGENCE VALUE   =  0.4075E-02  CRITERION=  0.3313E-01 <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.4075E-02
           FORCE CONVERGENCE VALUE  =  0.1112E-02  CRITERION=  0.1168     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.7785E-23  CRITERION=  0.8240     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.4981      CRITERION=  0.4322   
           DISP CONVERGENCE VALUE   =  0.1047E-03  CRITERION=  0.3381E-01 <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.1047E-03
           FORCE CONVERGENCE VALUE  =  0.6169E-06  CRITERION=  0.1192     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3398E-27  CRITERION=  0.8408     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.8170E-02  CRITERION=  0.4410     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   2
       *** LOAD STEP     1   SUBSTEP     4  COMPLETED.    CUM ITER =      8
       *** TIME =  0.100000         TIME INC =  0.300000E-01
       *** MAX PORE PRESSURE STEP = 0.1469E-04


       *** ANSYS BINARY FILE STATISTICS
        BUFFER SIZE USED= 16384
             18.938 MB WRITTEN ON ELEMENT MATRIX FILE: file0.emat
              9.250 MB WRITTEN ON ELEMENT SAVED DATA FILE: file0.esav
              8.500 MB WRITTEN ON ASSEMBLED MATRIX FILE: file0.full
              3.875 MB WRITTEN ON RESULTS FILE: file0.rst
       *************** Write FE CONNECTORS *********

       WRITE OUT CONSTRAINT EQUATIONS TO FILE= file.ce                                                                                                                                                                                                                                                            
       ****************************************************
       *************** FINISHED SOLVE FOR LS 1 *************
       ****************************************************
       ******************* SOLVE FOR LS 2 OF 3 ****************
       *** Set Displacements ***

       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    200 SUBSTEPS AS A MAXIMUM
         USE      1 SUBSTEPS AS A MINIMUM
         USE THE FINAL TIME STEP SIZE OF THE PREVIOUS LOAD STEP
           AS THE STARTING TIME STEP SIZE.

       TIME=  20.000   

       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 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

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

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

       *** NOTE ***                            CP =      14.094   TIME= 14:08:59
       The RESCONTROL command does not support fluid analyses.  The RESCONTROL
       command settings have been de-activated.                               

       *** NOTE ***                            CP =      14.094   TIME= 14:08:59
       This nonlinear analysis defaults to using the full Newton-Raphson      
       solution procedure.  This can be modified using the NROPT command.     

       *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2022 R1          22.1     ***
       DISTRIBUTED Ansys Mechanical Enterprise Academic Research    

       00000000  VERSION=WINDOWS x64   14:08:59  SEP 05, 2024 CP=     14.125

       800um_simplified_TEST--Static Structural (A5)                                



                            L O A D   S T E P   O P T I O N S

         LOAD STEP NUMBER. . . . . . . . . . . . . . . .     2
         TIME AT END OF THE LOAD STEP. . . . . . . . . .  20.000   
         AUTOMATIC TIME STEPPING . . . . . . . . . . . .    ON
            INITIAL NUMBER OF SUBSTEPS . . . . . . . . .     1
            MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . .   200
            MINIMUM NUMBER OF SUBSTEPS . . . . . . . . .     1
            START WITH TIME STEP FROM PREVIOUS SUBSTEP .   YES
         MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS. . . .    15
         STEP CHANGE BOUNDARY CONDITIONS . . . . . . . .    NO
         STRESS-STIFFENING . . . . . . . . . . . . . . .    ON
         TERMINATE ANALYSIS IF NOT CONVERGED . . . . . .YES (EXIT) 
         NODAL DOF SOLUTION LIMIT. . . . . . . . . . . . 0.10000E+10
         CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS
         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              
            STRS        ALL              
            EPEL        ALL              
            EPPL        ALL              
            CONT        ALL              


       SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr                                                                                                                                                                                                                                                          

       *** NOTE ***                            CP =      14.156   TIME= 14:08:59
       Predictor is ON by default for structural elements with rotational     
       degrees of freedom.  Use the PRED,OFF command to turn the predictor    
       OFF if it adversely affects the convergence.                           

           FORCE CONVERGENCE VALUE  =   3.825      CRITERION=  0.1161   
           MOMENT CONVERGENCE VALUE =  0.1426E-24  CRITERION=  0.8192   
           FL FLOW CONVERGENCE VALUE=  0.1962E+06  CRITERION=   1001.   
           DISP CONVERGENCE VALUE   =   2.159      CRITERION=  0.1102   
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   2.159   
           FORCE CONVERGENCE VALUE  =   97.00      CRITERION=  0.2366   
           MOMENT CONVERGENCE VALUE =  0.8223E-21  CRITERION=   1.670     <<< CONVERGED

       *** WARNING ***                         CP =      15.594   TIME= 14:09:01
       A reference moment value times the tolerance is used by the            
       Newton-Raphson method for checking convergence.  The calculated        
       reference MOMENT CONVERGENCE VALUE = 0 is less than a threshold.  This 
       threshold is internally calculated.  You can overwrite it by           
       specifying MINREF on the CNVTOL command.  Check results carefully.     
           FL FLOW CONVERGENCE VALUE=   890.6      CRITERION=   1.657   
           DISP CONVERGENCE VALUE   =  0.2326E-01  CRITERION=  0.1135     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2326E-01
           FORCE CONVERGENCE VALUE  =  0.4225E-01  CRITERION=  0.2434     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.1500E-21  CRITERION=   1.717     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   11.07      CRITERION=   1.675   
           DISP CONVERGENCE VALUE   =  0.2779E-02  CRITERION=  0.1159     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.2779E-02
           FORCE CONVERGENCE VALUE  =  0.5512E-03  CRITERION=  0.2483     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4675E-25  CRITERION=   1.752     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.8641      CRITERION=   1.709     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   3
       *** LOAD STEP     2   SUBSTEP     1  COMPLETED.    CUM ITER =     11
       *** TIME =  0.199500         TIME INC =  0.995000E-01
       *** MAX PORE PRESSURE STEP = 0.4906E-04
       *** AUTO STEP TIME:  NEXT TIME INC = 0.99500E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =   199.5      CRITERION=  0.3550   
           MOMENT CONVERGENCE VALUE =  0.2309E-20  CRITERION=   2.505   
           FL FLOW CONVERGENCE VALUE=   855.3      CRITERION=   1.769   
           DISP CONVERGENCE VALUE   =  0.4801E-01  CRITERION=  0.1133     <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.4801E-01
           FORCE CONVERGENCE VALUE  =  0.1140      CRITERION=  0.3660     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3248E-21  CRITERION=   2.583     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   21.09      CRITERION=   1.898   
           DISP CONVERGENCE VALUE   =  0.7567E-02  CRITERION=  0.1156     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.7567E-02
           FORCE CONVERGENCE VALUE  =  0.4512E-02  CRITERION=  0.3733     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.1455E-24  CRITERION=   2.634     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   2.672      CRITERION=   1.934   
           DISP CONVERGENCE VALUE   =  0.3288E-04  CRITERION=  0.1180     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.3288E-04
           FORCE CONVERGENCE VALUE  =  0.1117E-05  CRITERION=  0.3809     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6184E-26  CRITERION=   2.687     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.7808E-02  CRITERION=   1.974     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   3
       *** LOAD STEP     2   SUBSTEP     2  COMPLETED.    CUM ITER =     14
       *** TIME =  0.299000         TIME INC =  0.995000E-01
       *** MAX PORE PRESSURE STEP = 0.5058E-04
       *** AUTO TIME STEP:  NEXT TIME INC = 0.14925      INCREASED (FACTOR = 1.5000)

           FORCE CONVERGENCE VALUE  =   392.1      CRITERION=  0.5498   
           MOMENT CONVERGENCE VALUE =  0.5622E-20  CRITERION=   3.879   
           FL FLOW CONVERGENCE VALUE=   2036.      CRITERION=   3.107   
           DISP CONVERGENCE VALUE   =  0.9542E-01  CRITERION=  0.1739     <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.9542E-01
           FORCE CONVERGENCE VALUE  =  0.3978      CRITERION=  0.5694     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.9866E-21  CRITERION=   4.018     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   67.98      CRITERION=   3.161   
           DISP CONVERGENCE VALUE   =  0.2438E-01  CRITERION=  0.1774     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.2438E-01
           FORCE CONVERGENCE VALUE  =  0.4422E-01  CRITERION=  0.5802     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.8360E-24  CRITERION=   4.094     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   13.39      CRITERION=   3.217   
           DISP CONVERGENCE VALUE   =  0.1460E-03  CRITERION=  0.1810     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.1460E-03
           FORCE CONVERGENCE VALUE  =  0.7871E-05  CRITERION=  0.5920     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.9100E-25  CRITERION=   4.177     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.5809E-01  CRITERION=   3.284     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   3
       *** LOAD STEP     2   SUBSTEP     3  COMPLETED.    CUM ITER =     17
       *** TIME =  0.448250         TIME INC =  0.149250   
       *** MAX PORE PRESSURE STEP = 0.8013E-04
       *** AUTO TIME STEP:  NEXT TIME INC = 0.22387      INCREASED (FACTOR = 1.5000)

           FORCE CONVERGENCE VALUE  =   937.8      CRITERION=  0.8648   
           MOMENT CONVERGENCE VALUE =  0.1953E-19  CRITERION=   6.101   
           FL FLOW CONVERGENCE VALUE=   4655.      CRITERION=   5.524   
           DISP CONVERGENCE VALUE   =  0.2307      CRITERION=  0.2702     <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2307   
           FORCE CONVERGENCE VALUE  =   1.735      CRITERION=  0.9064   
           MOMENT CONVERGENCE VALUE =  0.3717E-20  CRITERION=   6.395     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   271.9      CRITERION=   5.389   
           DISP CONVERGENCE VALUE   =  0.9184E-01  CRITERION=  0.2757     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.9184E-01
           FORCE CONVERGENCE VALUE  =  0.5686      CRITERION=  0.9209     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6311E-23  CRITERION=   6.497     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   81.36      CRITERION=   5.465   
           DISP CONVERGENCE VALUE   =  0.6871E-03  CRITERION=  0.2813     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.6871E-03
           FORCE CONVERGENCE VALUE  =  0.9802E-04  CRITERION=  0.9397     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.1729E-23  CRITERION=   6.630     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.5157      CRITERION=   5.583     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   3
       *** LOAD STEP     2   SUBSTEP     4  COMPLETED.    CUM ITER =     20
       *** TIME =  0.672125         TIME INC =  0.223875   
       *** MAX PORE PRESSURE STEP = 0.1328E-03
       *** AUTO TIME STEP:  NEXT TIME INC = 0.33581      INCREASED (FACTOR = 1.5000)

           FORCE CONVERGENCE VALUE  =   2309.      CRITERION=   1.398   
           MOMENT CONVERGENCE VALUE =  0.7181E-19  CRITERION=   9.860   
           FL FLOW CONVERGENCE VALUE=  0.1100E+05  CRITERION=   10.66   
           DISP CONVERGENCE VALUE   =  0.5877      CRITERION=  0.4277   
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.5877   
           FORCE CONVERGENCE VALUE  =   8.988      CRITERION=   1.504   
           MOMENT CONVERGENCE VALUE =  0.1456E-19  CRITERION=   10.61     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   1181.      CRITERION=   9.454   
           DISP CONVERGENCE VALUE   =  0.2859      CRITERION=  0.4365     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.2859   
           FORCE CONVERGENCE VALUE  =   6.048      CRITERION=   1.514   
           MOMENT CONVERGENCE VALUE =  0.5984E-22  CRITERION=   10.68     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   466.7      CRITERION=   9.511   
           DISP CONVERGENCE VALUE   =  0.6182E-02  CRITERION=  0.4454     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.6182E-02
           FORCE CONVERGENCE VALUE  =  0.6423E-02  CRITERION=   1.545     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.2895E-22  CRITERION=   10.90     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   6.575      CRITERION=   9.733     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   3
       *** LOAD STEP     2   SUBSTEP     5  COMPLETED.    CUM ITER =     23
       *** TIME =   1.00794         TIME INC =  0.335812   
       *** MAX PORE PRESSURE STEP = 0.2336E-03
       *** AUTO TIME STEP:  NEXT TIME INC = 0.50372      INCREASED (FACTOR = 1.5000)

           FORCE CONVERGENCE VALUE  =   5919.      CRITERION=   2.363   
           MOMENT CONVERGENCE VALUE =  0.2848E-18  CRITERION=   16.67   
           FL FLOW CONVERGENCE VALUE=  0.2711E+05  CRITERION=   23.47   
           DISP CONVERGENCE VALUE   =   1.657      CRITERION=  0.6969   
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -1.657   
           FORCE CONVERGENCE VALUE  =   56.33      CRITERION=   2.719   
           MOMENT CONVERGENCE VALUE =  0.5987E-19  CRITERION=   19.18     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   5722.      CRITERION=   18.37   
           DISP CONVERGENCE VALUE   =  0.7270      CRITERION=  0.7112   
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.7270   
           FORCE CONVERGENCE VALUE  =   54.06      CRITERION=   2.659   
           MOMENT CONVERGENCE VALUE =  0.7938E-21  CRITERION=   18.76     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   2519.      CRITERION=   18.24   
           DISP CONVERGENCE VALUE   =  0.7907E-01  CRITERION=  0.7257     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.7907E-01
           FORCE CONVERGENCE VALUE  =  0.6206      CRITERION=   2.712     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4665E-21  CRITERION=   19.14     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   131.4      CRITERION=   18.67   
           DISP CONVERGENCE VALUE   =  0.9801E-02  CRITERION=  0.7405     <<< CONVERGED
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.9801E-02
           FORCE CONVERGENCE VALUE  =  0.6155E-02  CRITERION=   2.768     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6029E-23  CRITERION=   19.53     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   13.81      CRITERION=   19.06     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   4
       *** LOAD STEP     2   SUBSTEP     6  COMPLETED.    CUM ITER =     27
       *** TIME =   1.51166         TIME INC =  0.503719   
       *** MAX PORE PRESSURE STEP = 0.4560E-03
       *** AUTO TIME STEP:  NEXT TIME INC = 0.75558      INCREASED (FACTOR = 1.5000)

           FORCE CONVERGENCE VALUE  =  0.1582E+05  CRITERION=   4.343   
           MOMENT CONVERGENCE VALUE =  0.1287E-17  CRITERION=   30.64   
           FL FLOW CONVERGENCE VALUE=  0.7247E+05  CRITERION=   63.93   
           DISP CONVERGENCE VALUE   =   4.684      CRITERION=   1.186   
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -4.684   
           FORCE CONVERGENCE VALUE  =   431.1      CRITERION=   6.029   
           MOMENT CONVERGENCE VALUE =  0.2530E-18  CRITERION=   42.54     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.3170E+05  CRITERION=   46.77   
           DISP CONVERGENCE VALUE   =   2.180      CRITERION=   1.222   
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   2.180   
           FORCE CONVERGENCE VALUE  =   302.6      CRITERION=   5.411   
           MOMENT CONVERGENCE VALUE =  0.1157E-19  CRITERION=   38.18     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.1143E+05  CRITERION=   48.47   
           DISP CONVERGENCE VALUE   =  0.5966      CRITERION=   1.247     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.5966   
           FORCE CONVERGENCE VALUE  =   52.40      CRITERION=   5.522   
           MOMENT CONVERGENCE VALUE =  0.5196E-20  CRITERION=   38.96     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   3061.      CRITERION=   49.28   
           DISP CONVERGENCE VALUE   =  0.2303      CRITERION=   1.273     <<< CONVERGED
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.2303   
           FORCE CONVERGENCE VALUE  =   3.313      CRITERION=   5.629     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.7963E-21  CRITERION=   39.72     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   692.3      CRITERION=   50.31   
           DISP CONVERGENCE VALUE   =  0.9720E-02  CRITERION=   1.299     <<< CONVERGED
          EQUIL ITER   5 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.9720E-02
           FORCE CONVERGENCE VALUE  =  0.2244E-01  CRITERION=   5.744     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5824E-22  CRITERION=   40.53     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   38.77      CRITERION=   51.33     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   5
       *** LOAD STEP     2   SUBSTEP     7  COMPLETED.    CUM ITER =     32
       *** TIME =   2.26723         TIME INC =  0.755578   
       *** MAX PORE PRESSURE STEP = 0.1118E-02
       *** AUTO TIME STEP:  NEXT TIME INC =  1.1334      INCREASED (FACTOR = 1.5000)

           VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR    100 U-P ELEMENTS
           FORCE CONVERGENCE VALUE  =  0.4045E+05  CRITERION=   9.588   
           MOMENT CONVERGENCE VALUE =  0.7521E-17  CRITERION=   67.65   
           FL FLOW CONVERGENCE VALUE=  0.2288E+06  CRITERION=   239.4   
           DISP CONVERGENCE VALUE   =   13.24      CRITERION=   2.091   
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -13.24   
           FORCE CONVERGENCE VALUE  =   6138.      CRITERION=   19.17   
           MOMENT CONVERGENCE VALUE =  0.1108E-17  CRITERION=   135.2     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.1728E+06  CRITERION=   161.6   
           DISP CONVERGENCE VALUE   =   4.640      CRITERION=   2.227   
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -4.640   
           FORCE CONVERGENCE VALUE  =   2161.      CRITERION=   17.12   
           MOMENT CONVERGENCE VALUE =  0.2520E-18  CRITERION=   120.8     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.7262E+05  CRITERION=   212.2   
           DISP CONVERGENCE VALUE   =   3.069      CRITERION=   2.278   
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   3.069   
           FORCE CONVERGENCE VALUE  =   1940.      CRITERION=   17.57   
           MOMENT CONVERGENCE VALUE =  0.3257E-19  CRITERION=   124.0     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.3077E+05  CRITERION=   221.1   
           DISP CONVERGENCE VALUE   =  0.9579      CRITERION=   2.329     <<< CONVERGED
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.9579   
           FORCE CONVERGENCE VALUE  =   129.3      CRITERION=   17.83   
           MOMENT CONVERGENCE VALUE =  0.4058E-19  CRITERION=   125.8     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.1062E+05  CRITERION=   233.4   
           DISP CONVERGENCE VALUE   =  0.3916      CRITERION=   2.377     <<< CONVERGED
          EQUIL ITER   5 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.3916   
           FORCE CONVERGENCE VALUE  =   18.15      CRITERION=   18.20     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.2693E-20  CRITERION=   128.4     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   2981.      CRITERION=   239.9   
           DISP CONVERGENCE VALUE   =  0.2909E-01  CRITERION=   2.426     <<< CONVERGED
          EQUIL ITER   6 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.2909E-01
           FORCE CONVERGENCE VALUE  =  0.1215      CRITERION=   18.57     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4904E-21  CRITERION=   131.0     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   265.3      CRITERION=   245.1   
           DISP CONVERGENCE VALUE   =  0.2002E-02  CRITERION=   2.475     <<< CONVERGED
          EQUIL ITER   7 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.2002E-02
           FORCE CONVERGENCE VALUE  =  0.2682E-02  CRITERION=   18.94     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.1349E-20  CRITERION=   133.7     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   14.92      CRITERION=   250.1     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   7
       *** LOAD STEP     2   SUBSTEP     8  COMPLETED.    CUM ITER =     39
       *** TIME =   3.40060         TIME INC =   1.13337   
       *** MAX PORE PRESSURE STEP = 0.4758E-02
       *** AUTO STEP TIME:  NEXT TIME INC =  1.1334      UNCHANGED

           VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR    390 U-P ELEMENTS
           FORCE CONVERGENCE VALUE  =  0.4581E+05  CRITERION=   28.54   
           MOMENT CONVERGENCE VALUE =  0.2427E-16  CRITERION=   201.4   
           FL FLOW CONVERGENCE VALUE=  0.4307E+06  CRITERION=   660.3   
           DISP CONVERGENCE VALUE   =   17.82      CRITERION=   2.425   
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   17.82   
           FORCE CONVERGENCE VALUE  =   5937.      CRITERION=   46.44   
           MOMENT CONVERGENCE VALUE =  0.2157E-17  CRITERION=   327.7     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.2027E+06  CRITERION=   320.4   
           DISP CONVERGENCE VALUE   =   34.97      CRITERION=   2.475   
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   34.97   
           VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR     50 U-P ELEMENTS
           FORCE CONVERGENCE VALUE  =   7166.      CRITERION=   48.01   
           MOMENT CONVERGENCE VALUE =  0.1096E-17  CRITERION=   338.7     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.2362E+06  CRITERION=   271.3   
           DISP CONVERGENCE VALUE   =   14.97      CRITERION=   2.525   
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -14.97   
           VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR     10 U-P ELEMENTS
           FORCE CONVERGENCE VALUE  =   1031.      CRITERION=   49.50   
           MOMENT CONVERGENCE VALUE =  0.2221E-18  CRITERION=   349.2     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.7745E+05  CRITERION=   256.4   
           DISP CONVERGENCE VALUE   =   12.01      CRITERION=   2.577   
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -12.01   
           FORCE CONVERGENCE VALUE  =   432.7      CRITERION=   50.40   
           MOMENT CONVERGENCE VALUE =  0.5230E-18  CRITERION=   355.6     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.3753E+05  CRITERION=   268.5   
           DISP CONVERGENCE VALUE   =   2.878      CRITERION=   2.630   
          EQUIL ITER   5 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -2.878   
           FORCE CONVERGENCE VALUE  =   5.817      CRITERION=   51.48     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.2304E-17  CRITERION=   363.2     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   9376.      CRITERION=   275.9   
           DISP CONVERGENCE VALUE   =  0.7062      CRITERION=   2.683     <<< CONVERGED
          EQUIL ITER   6 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.7062   
           FORCE CONVERGENCE VALUE  =  0.7384      CRITERION=   52.53     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.1639E-16  CRITERION=   370.6     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   2734.      CRITERION=   281.7   
           DISP CONVERGENCE VALUE   =  0.2700      CRITERION=   2.738     <<< CONVERGED
          EQUIL ITER   7 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   1.130   
           FORCE CONVERGENCE VALUE  =  0.2003      CRITERION=   53.60     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5060E-16  CRITERION=   378.2     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   1057.      CRITERION=   287.4   
           DISP CONVERGENCE VALUE   =  0.1129      CRITERION=   2.794     <<< CONVERGED
          EQUIL ITER   8 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.7755   
           FORCE CONVERGENCE VALUE  =  0.7950E-01  CRITERION=   54.70     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5057E-16  CRITERION=   1304.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   443.5      CRITERION=   293.3   
           DISP CONVERGENCE VALUE   =  0.4754E-01  CRITERION=   2.851     <<< CONVERGED
          EQUIL ITER   9 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  0.7791   
           FORCE CONVERGENCE VALUE  =  0.3336E-01  CRITERION=   55.81     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6252E-16  CRITERION=   1444.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   186.3      CRITERION=   299.3     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   9
       *** LOAD STEP     2   SUBSTEP     9  COMPLETED.    CUM ITER =     48
       *** TIME =   4.53397         TIME INC =   1.13337   
       *** MAX PORE PRESSURE STEP = 0.1223E-01
       *** AUTO STEP TIME:  NEXT TIME INC =  1.1334      UNCHANGED

           VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR    190 U-P ELEMENTS
           FORCE CONVERGENCE VALUE  =  0.2435E+05  CRITERION=   76.72   
           MOMENT CONVERGENCE VALUE =  0.2261E-15  CRITERION=   541.3   
           FL FLOW CONVERGENCE VALUE=  0.6893E+06  CRITERION=   382.2   
           DISP CONVERGENCE VALUE   =   8.530      CRITERION=   2.425   
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -8.530   
           FORCE CONVERGENCE VALUE  =   1181.      CRITERION=   81.14   
           MOMENT CONVERGENCE VALUE =  0.2108E-15  CRITERION=   572.5     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.9262E+05  CRITERION=   187.3   
           DISP CONVERGENCE VALUE   =   267.2      CRITERION=   13.73   
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   267.2   

       *** ERROR ***                           CP =      72.000   TIME= 14:09:58
       Element 1927 (CPT215) is turning inside out.                           

       *** ERROR ***                           CP =      72.000   TIME= 14:09:58
       Element 1927 (CPT215) is turning inside out.                           

       *** ERROR ***                           CP =      72.000   TIME= 14:09:58
       Element 1927 (CPT215) is turning inside out.                           

       *** ERROR ***                           CP =      72.000   TIME= 14:09:58
       Element 1927 (CPT215) is turning inside out.                           
       *** LOAD STEP     2   SUBSTEP    10  NOT COMPLETED.  CUM ITER =     51
       *** BEGIN BISECTION NUMBER   1    NEW TIME INCREMENT=  0.39668   

           FORCE CONVERGENCE VALUE  =   5879.      CRITERION=   57.09   
           MOMENT CONVERGENCE VALUE =  0.1579E-15  CRITERION=   402.8   
           FL FLOW CONVERGENCE VALUE=  0.1463E+06  CRITERION=   97.41   
           DISP CONVERGENCE VALUE   =   3.466      CRITERION=   2.425   
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -3.466   
           FORCE CONVERGENCE VALUE  =   185.6      CRITERION=   59.07   
           MOMENT CONVERGENCE VALUE =  0.3736E-15  CRITERION=   416.7     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=  0.1222E+05  CRITERION=   62.15   
           DISP CONVERGENCE VALUE   =   2.332      CRITERION=   2.475     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   2.332   
           FORCE CONVERGENCE VALUE  =   208.7      CRITERION=   60.64   
           MOMENT CONVERGENCE VALUE =  0.1069E-15  CRITERION=   427.8     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   6387.      CRITERION=   62.62   
           DISP CONVERGENCE VALUE   =  0.9841E-01  CRITERION=   2.525     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.7170   
           FORCE CONVERGENCE VALUE  =  0.5591      CRITERION=   61.89     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6755E-16  CRITERION=   436.6     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   155.3      CRITERION=   64.08   
           DISP CONVERGENCE VALUE   =  0.1904E-01  CRITERION=   2.577     <<< CONVERGED
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC= -0.5226   
           FORCE CONVERGENCE VALUE  =  0.4401E-01  CRITERION=   63.15     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.8709E-16  CRITERION=   445.6     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   35.96      CRITERION=   65.40     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   4
       *** LOAD STEP     2   SUBSTEP    10  COMPLETED.    CUM ITER =     54
       *** TIME =   4.93065         TIME INC =  0.396679   
       *** MAX PORE PRESSURE STEP = 0.4618E-02
       *** AUTO STEP TIME:  NEXT TIME INC = 0.39668      UNCHANGED

           FORCE CONVERGENCE VALUE  =   666.6      CRITERION=   69.95   
           MOMENT CONVERGENCE VALUE =  0.1975E-15  CRITERION=   493.5   
           FL FLOW CONVERGENCE VALUE=  0.7014E+05  CRITERION=   48.63   
           DISP CONVERGENCE VALUE   =   1.067      CRITERION=   2.425     <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   1.939   
           FORCE CONVERGENCE VALUE  =   31.23      CRITERION=   71.24     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.2013E-15  CRITERION=   502.6     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   3367.      CRITERION=   48.02   
           DISP CONVERGENCE VALUE   =  0.1581      CRITERION=   2.475     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   1.363   
           FORCE CONVERGENCE VALUE  =   1.372      CRITERION=   72.71     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3373E-15  CRITERION=   513.0     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   280.6      CRITERION=   49.06   
           DISP CONVERGENCE VALUE   =  0.2799E-01  CRITERION=   2.525     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -4.089   
           FORCE CONVERGENCE VALUE  =  0.2609      CRITERION=   74.20     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.1580E-15  CRITERION=   523.5     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   43.70      CRITERION=   50.08     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   3
       *** LOAD STEP     2   SUBSTEP    11  COMPLETED.    CUM ITER =     57
       *** TIME =   5.32733         TIME INC =  0.396679   
       *** MAX PORE PRESSURE STEP = 0.4522E-02
       *** AUTO TIME STEP:  NEXT TIME INC = 0.59502      INCREASED (FACTOR = 1.5000)

           FORCE CONVERGENCE VALUE  =   587.3      CRITERION=   87.18   
           MOMENT CONVERGENCE VALUE =  0.3086E-15  CRITERION=   615.1   
           FL FLOW CONVERGENCE VALUE=  0.8860E+05  CRITERION=   66.17   
           DISP CONVERGENCE VALUE   =   1.496      CRITERION=   2.425     <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   8.691   
           FORCE CONVERGENCE VALUE  =   38.51      CRITERION=   88.40     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3608E-15  CRITERION=   623.7     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   5290.      CRITERION=   59.75   
           DISP CONVERGENCE VALUE   =  0.1473      CRITERION=   2.475     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -3.891   
           FORCE CONVERGENCE VALUE  =   1.505      CRITERION=   90.20     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3548E-15  CRITERION=   636.4     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   426.3      CRITERION=   60.97   
           DISP CONVERGENCE VALUE   =  0.3329E-01  CRITERION=   2.525     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   6.286   
           FORCE CONVERGENCE VALUE  =  0.3339      CRITERION=   92.05     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4107E-15  CRITERION=   649.4     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   96.47      CRITERION=   62.20   
           DISP CONVERGENCE VALUE   =  0.3904E-01  CRITERION=   2.577     <<< CONVERGED
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   4.981   
           FORCE CONVERGENCE VALUE  =  0.1015      CRITERION=   93.92     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3452E-15  CRITERION=   662.7     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   102.7      CRITERION=   63.48   
           DISP CONVERGENCE VALUE   =  0.5016E-01  CRITERION=   2.630     <<< CONVERGED
          EQUIL ITER   5 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   3.366   
           FORCE CONVERGENCE VALUE  =  0.5361E-01  CRITERION=   95.84     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6781E-15  CRITERION=   676.2     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   126.7      CRITERION=   64.77   
           DISP CONVERGENCE VALUE   =  0.6416E-01  CRITERION=   2.683     <<< CONVERGED
          EQUIL ITER   6 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -3.811   
           FORCE CONVERGENCE VALUE  =  0.5683E-01  CRITERION=   97.80     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.7182E-15  CRITERION=   690.0     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   158.6      CRITERION=   66.09   
           DISP CONVERGENCE VALUE   =  0.8207E-01  CRITERION=   2.738     <<< CONVERGED
          EQUIL ITER   7 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   2.992   
           FORCE CONVERGENCE VALUE  =  0.7051E-01  CRITERION=   99.79     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4953E-15  CRITERION=   704.1     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   199.4      CRITERION=   67.44   
           DISP CONVERGENCE VALUE   =  0.1050      CRITERION=   2.794     <<< CONVERGED
          EQUIL ITER   8 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -2.960   
           FORCE CONVERGENCE VALUE  =  0.8889E-01  CRITERION=   101.8     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.2620E-15  CRITERION=   2546.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   251.6      CRITERION=   68.82   
           DISP CONVERGENCE VALUE   =  0.1342      CRITERION=   2.851     <<< CONVERGED
          EQUIL ITER   9 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   2.774   
           FORCE CONVERGENCE VALUE  =  0.1124      CRITERION=   103.9     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.2076E-15  CRITERION=   2547.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   318.3      CRITERION=   70.22   
          >>> PREDICTED NUMBER OF ITERATIONS FOR CONVERGENCE=  30 EXCEEDS MAX OF  15
       *** LOAD STEP     2   SUBSTEP    12  NOT COMPLETED.  CUM ITER =     67
       *** BEGIN BISECTION NUMBER   1    NEW TIME INCREMENT=  0.29751   

           FORCE CONVERGENCE VALUE  =   205.8      CRITERION=   78.51   
           MOMENT CONVERGENCE VALUE =  0.2853E-15  CRITERION=   554.0   
           FL FLOW CONVERGENCE VALUE=  0.3095E+05  CRITERION=   30.83   
           DISP CONVERGENCE VALUE   =  0.6181      CRITERION=   2.425     <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -6.432   
           FORCE CONVERGENCE VALUE  =   7.216      CRITERION=   79.88     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.2714E-15  CRITERION=   563.6     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   1083.      CRITERION=   29.37   
           DISP CONVERGENCE VALUE   =  0.3623E-01  CRITERION=   2.475     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -4.935   
           FORCE CONVERGENCE VALUE  =  0.3910      CRITERION=   81.51     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3278E-15  CRITERION=   575.1     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   64.57      CRITERION=   30.02   
           DISP CONVERGENCE VALUE   =  0.8467E-02  CRITERION=   2.525     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   5.181   
           FORCE CONVERGENCE VALUE  =  0.9098E-01  CRITERION=   83.17     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4019E-15  CRITERION=   586.8     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   13.85      CRITERION=   30.63     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   3
       *** LOAD STEP     2   SUBSTEP    12  COMPLETED.    CUM ITER =     69
       *** TIME =   5.62483         TIME INC =  0.297509   
       *** MAX PORE PRESSURE STEP = 0.3283E-02
       *** AUTO STEP TIME:  NEXT TIME INC = 0.29751      UNCHANGED

           FORCE CONVERGENCE VALUE  =   97.46      CRITERION=   86.72   
           MOMENT CONVERGENCE VALUE =  0.6952E-15  CRITERION=   611.8   
           FL FLOW CONVERGENCE VALUE=  0.2336E+05  CRITERION=   33.00   
           DISP CONVERGENCE VALUE   =  0.3858      CRITERION=   2.425     <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   6.305   
           FORCE CONVERGENCE VALUE  =   4.304      CRITERION=   88.32     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6284E-15  CRITERION=   623.2     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   627.0      CRITERION=   30.59   
           DISP CONVERGENCE VALUE   =  0.6861E-01  CRITERION=   2.475     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   3.761   
           FORCE CONVERGENCE VALUE  =  0.5457      CRITERION=   90.13     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5502E-15  CRITERION=   635.9     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   102.3      CRITERION=   31.22   
           DISP CONVERGENCE VALUE   =  0.6230E-01  CRITERION=   2.525     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   6.646   
           FORCE CONVERGENCE VALUE  =  0.1439      CRITERION=   91.97     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5651E-15  CRITERION=   648.9     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   107.4      CRITERION=   31.85   
           DISP CONVERGENCE VALUE   =  0.7607E-01  CRITERION=   2.577     <<< CONVERGED
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   4.688   
           FORCE CONVERGENCE VALUE  =  0.9129E-01  CRITERION=   93.84     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5234E-15  CRITERION=   662.1     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   128.1      CRITERION=   32.50   
           DISP CONVERGENCE VALUE   =  0.9759E-01  CRITERION=   2.630     <<< CONVERGED
          EQUIL ITER   5 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   3.905   
           FORCE CONVERGENCE VALUE  =  0.1036      CRITERION=   95.76     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5851E-15  CRITERION=   675.6     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   155.4      CRITERION=   33.17   
           DISP CONVERGENCE VALUE   =  0.1251      CRITERION=   2.683     <<< CONVERGED
          EQUIL ITER   6 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   5.946   
           FORCE CONVERGENCE VALUE  =  0.1262      CRITERION=   97.71     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3994E-15  CRITERION=   689.4     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   190.1      CRITERION=   33.84   
           DISP CONVERGENCE VALUE   =  0.1603      CRITERION=   2.738     <<< CONVERGED
          EQUIL ITER   7 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   3.675   
           FORCE CONVERGENCE VALUE  =  0.1554      CRITERION=   99.71     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5509E-15  CRITERION=   703.5     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   234.3      CRITERION=   34.53   
           DISP CONVERGENCE VALUE   =  0.2055      CRITERION=   2.794     <<< CONVERGED
          EQUIL ITER   8 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   6.289   
           FORCE CONVERGENCE VALUE  =  0.1925      CRITERION=   101.7     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3442E-15  CRITERION=   2363.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   290.2      CRITERION=   35.24   
          >>> PREDICTED NUMBER OF ITERATIONS FOR CONVERGENCE=  30 EXCEEDS MAX OF  15
       *** LOAD STEP     2   SUBSTEP    13  NOT COMPLETED.  CUM ITER =     78
       *** BEGIN BISECTION NUMBER   1    NEW TIME INCREMENT=  0.99500E-01

           FORCE CONVERGENCE VALUE  =   21.77      CRITERION=   81.10   
           MOMENT CONVERGENCE VALUE =  0.5083E-15  CRITERION=   572.2   
           FL FLOW CONVERGENCE VALUE=   5148.      CRITERION=   10.17   
           DISP CONVERGENCE VALUE   =  0.1001      CRITERION=   2.425     <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   5.594   
           FORCE CONVERGENCE VALUE  =  0.9471      CRITERION=   82.71     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4473E-15  CRITERION=   583.6     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   52.90      CRITERION=   9.302   
           DISP CONVERGENCE VALUE   =  0.1839E-01  CRITERION=   2.475     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   4.107   
           FORCE CONVERGENCE VALUE  =  0.1159      CRITERION=   84.40     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3971E-15  CRITERION=   595.5     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   9.614      CRITERION=   9.494   
           DISP CONVERGENCE VALUE   =  0.1509E-01  CRITERION=   2.525     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   4.687   
           FORCE CONVERGENCE VALUE  =  0.2872E-01  CRITERION=   86.13     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4126E-15  CRITERION=   607.7     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   8.598      CRITERION=   9.687     <<< CONVERGED
          >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION   3
       *** LOAD STEP     2   SUBSTEP    13  COMPLETED.    CUM ITER =     80
       *** TIME =   5.72433         TIME INC =  0.995000E-01
       *** MAX PORE PRESSURE STEP = 0.1076E-02
       *** AUTO STEP TIME:  NEXT TIME INC = 0.99500E-01  UNCHANGED

           FORCE CONVERGENCE VALUE  =   7.751      CRITERION=   83.84   
           MOMENT CONVERGENCE VALUE =  0.6206E-15  CRITERION=   591.5   
           FL FLOW CONVERGENCE VALUE=   2834.      CRITERION=   9.998   
           DISP CONVERGENCE VALUE   =  0.7224E-01  CRITERION=   2.425     <<< CONVERGED
          EQUIL ITER   1 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -7.322   
           FORCE CONVERGENCE VALUE  =  0.3590      CRITERION=   85.53     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5841E-15  CRITERION=   603.5     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   35.06      CRITERION=   10.53   
           DISP CONVERGENCE VALUE   =  0.4769E-01  CRITERION=   2.475     <<< CONVERGED
          EQUIL ITER   2 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -8.339   
           FORCE CONVERGENCE VALUE  =  0.5837E-01  CRITERION=   87.27     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4523E-15  CRITERION=   615.8     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   25.09      CRITERION=   10.75   
           DISP CONVERGENCE VALUE   =  0.5387E-01  CRITERION=   2.525     <<< CONVERGED
          EQUIL ITER   3 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   6.505   
           FORCE CONVERGENCE VALUE  =  0.5371E-01  CRITERION=   89.06     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.4416E-15  CRITERION=   628.3     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   27.54      CRITERION=   10.97   
           DISP CONVERGENCE VALUE   =  0.6188E-01  CRITERION=   2.577     <<< CONVERGED
          EQUIL ITER   4 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   8.599   
           FORCE CONVERGENCE VALUE  =  0.5913E-01  CRITERION=   90.87     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5724E-15  CRITERION=   641.2     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   30.53      CRITERION=   11.19   
           DISP CONVERGENCE VALUE   =  0.7110E-01  CRITERION=   2.630     <<< CONVERGED
          EQUIL ITER   5 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   6.093   
           FORCE CONVERGENCE VALUE  =  0.6585E-01  CRITERION=   92.73     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.5550E-15  CRITERION=   654.3     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   34.01      CRITERION=   11.42   
           DISP CONVERGENCE VALUE   =  0.8170E-01  CRITERION=   2.683     <<< CONVERGED
          EQUIL ITER   6 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   8.481   
           FORCE CONVERGENCE VALUE  =  0.7367E-01  CRITERION=   94.62     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.3846E-15  CRITERION=   667.6     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   38.05      CRITERION=   11.66   
           DISP CONVERGENCE VALUE   =  0.9388E-01  CRITERION=   2.738     <<< CONVERGED
          EQUIL ITER   7 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   6.800   
           FORCE CONVERGENCE VALUE  =  0.8275E-01  CRITERION=   96.55     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6934E-15  CRITERION=   681.2     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   42.75      CRITERION=   11.89   
           DISP CONVERGENCE VALUE   =  0.1079      CRITERION=   2.794     <<< CONVERGED
          EQUIL ITER   8 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   6.546   
           FORCE CONVERGENCE VALUE  =  0.9326E-01  CRITERION=   98.52     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6029E-15  CRITERION=   2445.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   48.18      CRITERION=   12.14   
           DISP CONVERGENCE VALUE   =  0.1240      CRITERION=   2.851     <<< CONVERGED
          EQUIL ITER   9 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -7.890   
           FORCE CONVERGENCE VALUE  =  0.1054      CRITERION=   100.5     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.7328E-15  CRITERION=   2472.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   54.52      CRITERION=   12.38   
           DISP CONVERGENCE VALUE   =  0.1424      CRITERION=   2.909     <<< CONVERGED
          EQUIL ITER  10 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   9.012   
           FORCE CONVERGENCE VALUE  =  0.1195      CRITERION=   102.6     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6199E-15  CRITERION=   2497.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   61.77      CRITERION=   12.64   
           DISP CONVERGENCE VALUE   =  0.1637      CRITERION=   2.968     <<< CONVERGED
          EQUIL ITER  11 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   5.415   
           FORCE CONVERGENCE VALUE  =  0.1358      CRITERION=   104.7     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.7637E-15  CRITERION=   2522.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   70.28      CRITERION=   12.89   
           DISP CONVERGENCE VALUE   =  0.1880      CRITERION=   3.029     <<< CONVERGED
          EQUIL ITER  12 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   6.784   
           FORCE CONVERGENCE VALUE  =  0.1545      CRITERION=   106.8     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6105E-15  CRITERION=   2547.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   79.94      CRITERION=   13.16   
           DISP CONVERGENCE VALUE   =  0.2161      CRITERION=   3.091     <<< CONVERGED
          EQUIL ITER  13 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -6.282   
           FORCE CONVERGENCE VALUE  =  0.1762      CRITERION=   109.0     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.7224E-15  CRITERION=   2571.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   91.38      CRITERION=   13.43   
           DISP CONVERGENCE VALUE   =  0.2483      CRITERION=   3.154     <<< CONVERGED
          EQUIL ITER  14 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=  -4.604   
           FORCE CONVERGENCE VALUE  =  0.2012      CRITERION=   111.2     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6804E-15  CRITERION=   2595.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   104.2      CRITERION=   13.70   
           DISP CONVERGENCE VALUE   =  0.2853      CRITERION=   3.218     <<< CONVERGED
          EQUIL ITER  15 COMPLETED.  NEW TRIANG MATRIX.  MAX DOF INC=   7.095   
           FORCE CONVERGENCE VALUE  =  0.2300      CRITERION=   113.5     <<< CONVERGED
           MOMENT CONVERGENCE VALUE =  0.6416E-15  CRITERION=   2618.     <<< CONVERGED
           FL FLOW CONVERGENCE VALUE=   119.6      CRITERION=   13.98   

       *** ERROR ***                           CP =     131.781   TIME= 14:10:58
       Solution not converged at time 5.82383467 (load step 2 substep 14).    
        Run terminated.                                                       

       *** WARNING ***                         CP =     131.781   TIME= 14:10:58
       The unconverged solution (identified as time 20 substep 999999) is     
       output for analysis debug purposes.  Results should not be used for    
       any other purpose.                                                     




               R E S T A R T   I N F O R M A T I O N

       REASON FOR TERMINATION. . . . . . . . . .UNCONVERGED SOLUTION                   
       FILES NEEDED FOR RESTARTING . . . . . . .  file0.osav
                                                  file0.emat
                                                  file.db
       TIME OF LAST SOLUTION . . . . . . . . . .  5.7243   
          TIME AT START OF THE LOAD STEP . . . . 0.10000   
          TIME AT END OF THE LOAD STEP . . . . .  20.000   
       NOTE: FOR CONVERGING SOLUTIONS, ADDITIONAL EQUILIBRIUM ITERATIONS MAY BE
             ADDED IN THE RESTART (NEQIT COMMAND) USING THE RESTART FILE file0.esav                                                                                                                                                                                                                                                         

       ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.db
        FOR POSSIBLE RESUME FROM THIS POINT





       NUMBER OF WARNING MESSAGES ENCOUNTERED=          7
       NUMBER OF ERROR   MESSAGES ENCOUNTERED=          5



       ***** PROBLEM TERMINATED BY INDICATED ERROR(S) OR BY END OF INPUT DATA *****

      +--------- D I S T R I B U T E D   A N S Y S   S T A T I S T I C S ------------+

      Release: 2022 R1            Build: 22.1       Update: UP20211129   Platform: WINDOWS x64
      Date Run: 09/05/2024   Time: 14:10     Process ID: 15340
      Operating System: Windows 10  (Build: 19044)

      Processor Model: 12th Gen Intel(R) Core(TM) i7-12700

      Compiler: Intel(R) Fortran Compiler Version 19.0.5  (Build: 20190815)
                Intel(R) C/C++ Compiler Version 19.0.5  (Build: 20190815)
                Intel(R) Math Kernel Library Version 2020.0.0 Product Build 20191125
                BLAS Library supplied by Intel(R) MKL

      Number of machines requested            :    1
      Total number of cores available         :   20
      Number of physical cores available      :   12
      Number of processes requested           :   10
      Number of threads per process requested :    1
      Total number of cores requested         :   10 (Distributed Memory Parallel)              
      MPI Type: INTELMPI
      MPI Version: Intel(R) MPI Library 2019 Update 10 for Windows* OS


      GPU Acceleration: Not Requested

      Job Name: file0
      Input File: dummy.dat

        Core                Machine Name   Working Directory
       -----------------------------------------------------
           0             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
           1             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
           2             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
           3             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
           4             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
           5             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
           6             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
           7             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
           8             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
           9             E-10VXXC3177879   C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
       
      Latency time from master to core     1 =    1.974 microseconds
      Latency time from master to core     2 =    1.910 microseconds
      Latency time from master to core     3 =    1.881 microseconds
      Latency time from master to core     4 =    1.907 microseconds
      Latency time from master to core     5 =    1.876 microseconds
      Latency time from master to core     6 =    1.896 microseconds
      Latency time from master to core     7 =    1.889 microseconds
      Latency time from master to core     8 =    2.418 microseconds
      Latency time from master to core     9 =    2.417 microseconds
       
      Communication speed from master to core     1 = 12783.43 MB/sec
      Communication speed from master to core     2 = 13977.95 MB/sec
      Communication speed from master to core     3 = 14281.63 MB/sec
      Communication speed from master to core     4 = 14028.20 MB/sec
      Communication speed from master to core     5 = 13763.91 MB/sec
      Communication speed from master to core     6 = 13771.50 MB/sec
      Communication speed from master to core     7 = 14067.67 MB/sec
      Communication speed from master to core     8 =  9001.31 MB/sec
      Communication speed from master to core     9 = 11021.56 MB/sec

      Total CPU time for main thread                    :      130.1 seconds
      Total CPU time summed for all threads             :      132.4 seconds

      Elapsed time spent obtaining a license            :        0.4 seconds
      Elapsed time spent pre-processing model (/PREP7)  :        0.1 seconds
      Elapsed time spent solution - preprocessing       :        0.2 seconds
      Elapsed time spent computing solution             :      130.0 seconds
      Elapsed time spent solution - postprocessing      :        0.3 seconds
      Elapsed time spent post-processing model (/POST1) :        0.0 seconds
       
      Equation solver used                              :            Sparse (symmetric)
      Equation solver computational rate                :       81.3 Gflops
      Equation solver effective I/O rate                :       21.1 GB/sec

      Sum of memory used on all processes               :     1570.0 MB
      Sum of memory allocated on all processes          :    11328.0 MB
      Physical memory available                         :         32 GB

      Total amount of I/O written to disk               :       33.1 GB
      Total amount of I/O read from disk                :       37.3 GB

      +------ E N D   D I S T R I B U T E D   A N S Y S   S T A T I S T I C S -------+


       *---------------------------------------------------------------------------*
       |                                                                           |
       |                       DISTRIBUTED ANSYS RUN COMPLETED                     |
       |                                                                           |
       |---------------------------------------------------------------------------|
       |                                                                           |
       | Ansys 2022 R1               Build 22.1         UP20211129     WINDOWS x64 |
       |                                                                           |
       |---------------------------------------------------------------------------|
       |                                                                           |
       | Database Requested(-db)  1024 MB    Scratch Memory Requested      1024 MB |
       | Maximum Database Used      17 MB    Maximum Scratch Memory Used    174 MB |
       |                                                                           |
       |---------------------------------------------------------------------------|
       |                                                                           |
       |        CP Time      (sec) =        132.422       Time  =  14:10:59        |
       |        Elapsed Time (sec) =        133.000       Date  =  09/05/2024      |
       |                                                                           |
       *---------------------------------------------------------------------------*

    • September 11, 2024 at 2:21 pm
      SaiD
      Ansys Employee

      Hello, 

      You can upload your model to OneDrive or Google drive or any such similar location and share the url on the post (third icon from left). Due to sompany policies, Ansys employees are not allowed to download anything, but other forum members might be able to help you.

      In the Solver Output file, I see that there are 4 elements that got turned inside out. I am not an expert in poroelasticity and coupled simulations, but hyperelastic materials also face excessive element distortion error sometimes and this error seems similar to that. Here's a video that may have some helpful tips that you could apply to your problem as well (the tips start at 10:05): How to Handle Element Distortion Errors in Hyperelastic Materials — Lesson 3 - ANSYS Innovation Courses

      Hope this helps.

       

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