Learning Forum

[fraser.shields]

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    


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




 ***************************************************************
 *            ANSYS 2022 R1          LEGAL NOTICES             *
 ***************************************************************
 *                                                             *
 * Copyright 1971-2022 ANSYS, Inc.  All rights reserved.       *
 * Unauthorized use, distribution or duplication is            *
 * prohibited.                                                 *
 *                                                             *
 * Ansys is a registered trademark of ANSYS, Inc. or its       *
 * subsidiaries in the United States or other countries.       *
 * See the ANSYS, Inc. online documentation or the ANSYS, Inc. *
 * documentation CD or online help for the complete Legal      *
 * Notice.                                                     *
 *                                                             *
 ***************************************************************
 *                                                             *
 * THIS ANSYS SOFTWARE PRODUCT AND PROGRAM DOCUMENTATION       *
 * INCLUDE TRADE SECRETS AND CONFIDENTIAL AND PROPRIETARY      *
 * PRODUCTS OF ANSYS, INC., ITS SUBSIDIARIES, OR LICENSORS.    *
 * The software products and documentation are furnished by    *
 * ANSYS, Inc. or its subsidiaries under a software license    *
 * agreement that contains provisions concerning               *
 * non-disclosure, copying, length and nature of use,          *
 * compliance with exporting laws, warranties, disclaimers,    *
 * limitations of liability, and remedies, and other           *
 * provisions.  The software products and documentation may be *
 * used, disclosed, transferred, or copied only in accordance  *
 * with the terms and conditions of that software license      *
 * agreement.                                                  *
 *                                                             *
 * ANSYS, Inc. is a UL registered                              *
 * ISO 9001:2015 company.                                      *
 *                                                             *
 ***************************************************************
 *                                                             *
 * This product is subject to U.S. laws governing export and   *
 * re-export.                                                  *
 *                                                             *
 * For U.S. Government users, except as specifically granted   *
 * by the ANSYS, Inc. software license agreement, the use,     *
 * duplication, or disclosure by the United States Government  *
 * is subject to restrictions stated in the ANSYS, Inc.        *
 * software license agreement and FAR 12.212 (for non-DOD      *
 * licenses).                                                  *
 *                                                             *
 ***************************************************************

 2022 R1
    
 Point Releases and Patches installed:  
    
 ANSYS, Inc. License Manager 2022 R1
 Ansys Sherlock 2022 R1 
 SpaceClaim 2022 R1 
 Autodyn 2022 R1
 LS-DYNA 2022 R1
 CFD-Post only 2022 R1  
 CFX (includes CFD-Post) 2022 R1
 Chemkin 2022 R1
 EnSight 2022 R1
 FENSAP-ICE 2022 R1 
 Fluent (includes CFD-Post) 2022 R1 
 Polyflow (includes CFD-Post) 2022 R1
 Forte (includes EnSight) 2022 R1
 TurboGrid 2022 R1  
 Aqwa 2022 R1
 Additive 2022 R1
 Customization Files for User Programmable Features 2022 R1 
 Mechanical Products 2022 R1
 Icepak (includes CFD-Post) 2022 R1 
 Remote Solve Manager Standalone Services 2022 R1
 Ansys Sound - SAS 2022 R1  
 Viewer 2022 R1 
 ACIS Geometry Interface 2022 R1
 AutoCAD Geometry Interface 2022 R1 
 Catia, Version 4 Geometry Interface 2022 R1
 Catia, Version 5 Geometry Interface 2022 R1
 Catia, Version 6 Geometry Interface 2022 R1
 Creo Elements/Direct Modeling Geometry Interface 2022 R1
 Creo Parametric Geometry Interface 2022 R1 
 Inventor Geometry Interface 2022 R1
 JTOpen Geometry Interface 2022 R1  
 NX Geometry Interface 2022 R1  
 Parasolid Geometry Interface  2022 R1  
 Solid Edge Geometry Interface 2022 R1  
 SOLIDWORKS Geometry Interface 2022 R1  


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

All

[Sai Deogekar]

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.