Non-linear convergence issue
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Hello,
I am attempting to model a soft poroelastic solid elements (CPT216) which is reinforced by stiff orthotropic linear elastic shell elements. The shell elements themselves have reinforcement fibres running parallel to the wall length, these are what provide the stiffness. Unfortunately, I am unable to get a non-linear solution to converges - the fluid flow will not converge. Is there any way I can upload my project file onto here, so someone can check the model?
Here is the solution information:
Solver Output
Ansys Mechanical Enterprise Academic Research
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2022 R1
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***** ANSYS COMMAND LINE ARGUMENTS *****
BATCH MODE REQUESTED (-b) = NOLIST
INPUT FILE COPY MODE (-c) = COPY
DISTRIBUTED MEMORY PARALLEL REQUESTED
10 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS
TOTAL OF 10 CORES REQUESTED
INPUT FILE NAME = C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7\dummy.dat
OUTPUT FILE NAME = C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7\solve.out
START-UP FILE MODE = NOREAD
STOP FILE MODE = NOREAD
RELEASE= 2022 R1 BUILD= 22.1 UP20211129 VERSION=WINDOWS x64
CURRENT JOBNAME=file0 14:08:47 SEP 05, 2024 CP= 0.047
PARAMETER _DS_PROGRESS = 999.0000000
/INPUT FILE= ds.dat LINE= 0
*** NOTE *** CP = 0.203 TIME= 14:08:48
The /CONFIG,NOELDB command is not valid in a Distributed ANSYS
solution. Command is ignored.
*GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 14.1466667
TITLE=
800um_simplified_TEST--Static Structural (A5)
ACT Extensions:
LSDYNA, 2021.1
5f463412-bd3e-484b-87e7-cbc0a665e474, wbex
SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7\
SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\800um_simplified_TEST_files\dp0\SYS\MECH\
SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_USERFILES_DIR(1) = C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\800um_simplified_TEST_files\user_files\
--- Data in consistent uMKS units. See Solving Units in the help system for mor
uMKS UNITS SPECIFIED FOR INTERNAL
LENGTH = MICROMETERS (um)
MASS = KILOGRAM (kg)
TIME = SECONDS (sec)
TEMPERATURE = CELSIUS (C)
TOFFSET = 273.0
FORCE = MICRONEWTON (uN)
HEAT = PICOJOULES (pJ)
INPUT UNITS ARE ALSO SET TO UMKS
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Research
00000000 VERSION=WINDOWS x64 14:08:48 SEP 05, 2024 CP= 0.203
800um_simplified_TEST--Static Structural (A5)
***** ANSYS ANALYSIS DEFINITION (PREP7) *****
*********** Nodes for the whole assembly ***********
*********** Elements for Body 1 "Solid111" ***********
*********** Elements for Body 2 "Solid111" ***********
*********** Elements for Body 3 "Solid111" ***********
*********** Elements for Body 4 "Solid1111" ***********
*********** Elements for Body 5 "Solid1111" ***********
*********** Elements for Body 6 "Solid1111" ***********
*********** Elements for Body 7 "Solid11111" ***********
*********** Elements for Body 8 "Solid1111" ***********
*********** Elements for Body 9 "Solid11111" ***********
*********** Elements for Body 10 "Solid111111" ***********
*********** Elements for Body 11 "Solid11111" ***********
*********** Elements for Body 12 "Solid1111" ***********
*********** Elements for Body 13 "Solid111111" ***********
*********** Elements for Body 14 "Solid1111111" ***********
*********** Elements for Body 15 "Surface" ***********
*********** Elements for Body 16 "Surface" ***********
*********** Elements for Body 17 "Surface" ***********
*********** Elements for Body 18 "Surface" ***********
*********** Elements for Body 19 "Surface" ***********
*********** Elements for Body 20 "Surface" ***********
*********** Elements for Body 21 "Surface1" ***********
*********** Elements for Body 22 "Surface1" ***********
*********** Elements for Body 23 "Surface1" ***********
*********** Elements for Body 24 "Surface1" ***********
*********** Elements for Body 25 "Surface1" ***********
*********** Elements for Body 26 "Surface11" ***********
*********** Elements for Body 27 "Surface1" ***********
*********** Elements for Body 28 "Surface1" ***********
*********** Elements for Body 29 "Surface1" ***********
*********** Elements for Body 30 "Surface1" ***********
*********** Elements for Body 31 "Surface1" ***********
*********** Elements for Body 32 "Surface1" ***********
*********** Elements for Body 33 "Surface1" ***********
*********** Elements for Body 34 "Surface11" ***********
*********** Elements for Body 35 "Surface11" ***********
*********** Elements for Body 36 "Surface11" ***********
*********** Elements for Body 37 "Surface1" ***********
*********** Elements for Body 38 "Surface1" ***********
*********** Elements for Body 39 "Surface11" ***********
*********** Elements for Body 40 "Surface11" ***********
*********** Send User Defined Coordinate System(s) ***********
*********** Send Element Orientation **********
Sending Element Orientation Object: "Element Orientation"
Sending Element Orientation Object: "Element Orientation 2"
*********** Set Reference Temperature ***********
*********** Send Materials ***********
*********** Send Sheet Properties ***********
*********** Send Named Selection as Element Component ***********
*********** Send Named Selection as Element Component ***********
********* Frictionless Supports X *********
********* Frictionless Supports Z *********
******* Constant Zero Displacement Y *******
*********** Create Displacement Tables and Functions ******
LIST DATA TABLE PLAS FOR MATERIAL 14
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Research
00000000 VERSION=WINDOWS x64 14:08:48 SEP 05, 2024 CP= 0.672
800um_simplified_TEST--Static Structural (A5)
PLASTIC (PLAS) Table For Material 14
ISOTROPIC HARDENING PLASTICITY
1
Temps 2.3000000e+01
PlStrain Stress
0.0000000e+00 5.9620000e+00
2.9670000e-03 1.1480000e+01
8.3930000e-03 1.5190000e+01
1.5420000e-02 1.7980000e+01
2.3740000e-02 2.0030000e+01
3.3180000e-02 2.1570000e+01
4.3610000e-02 2.2760000e+01
5.4960000e-02 2.3600000e+01
6.7140000e-02 2.4230000e+01
8.0120000e-02 2.4640000e+01
***** ROUTINE COMPLETED ***** CP = 0.672
--- Number of total nodes = 10043
--- Number of contact elements = 0
--- Number of spring elements = 0
--- Number of bearing elements = 0
--- Number of solid elements = 10310
--- Number of condensed parts = 0
--- Number of total elements = 10310
*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 14.1466667
****************************************************************************
************************* SOLUTION ********************************
****************************************************************************
***** ANSYS SOLUTION ROUTINE *****
PERFORM A STATIC ANALYSIS
THIS WILL BE A NEW ANALYSIS
LARGE DEFORMATION ANALYSIS
PARAMETER _THICKRATIO = 0.000000000
USE SPARSE MATRIX DIRECT SOLVER
CONTACT INFORMATION PRINTOUT LEVEL 1
DO NOT COMBINE ELEMENT MATRIX FILES (.emat) AFTER DISTRIBUTED PARALLEL SOLUTION
DO NOT COMBINE ELEMENT SAVE DATA FILES (.esav) AFTER DISTRIBUTED PARALLEL SOLUTION
NLDIAG: Nonlinear diagnostics CONT option is set to ON.
Writing frequency : each ITERATION.
DEFINE RESTART CONTROL FOR LOADSTEP LAST
AT FREQUENCY OF LAST AND NUMBER FOR OVERWRITE IS -1
DELETE RESTART FILES OF ENDSTEP
****************************************************
******************* SOLVE FOR LS 1 OF 3 ****************
*** Set Displacements ***
CMBLOCK read of NODE component _CM1384UY_YP completed
SELECT COMPONENT _CM1384UY_YP
SPECIFIED CONSTRAINT UY FOR SELECTED NODES 1 TO 10043 BY 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI1384YP
ALL SELECT FOR ITEM=NODE COMPONENT=
IN RANGE 1 TO 10043 STEP 1
10043 NODES (OF 10043 DEFINED) SELECTED BY NSEL COMMAND.
*** Component For All Non-Zero UY Displacements ***
SELECT COMPONENT _CM1384UY_YP
DEFINITION OF COMPONENT = _DISPNONZEROUY ENTITY=NODE
ALL SELECT FOR ITEM=NODE COMPONENT=
IN RANGE 1 TO 10043 STEP 1
10043 NODES (OF 10043 DEFINED) SELECTED BY NSEL COMMAND.
PRINTOUT RESUMED BY /GOP
USE AUTOMATIC TIME STEPPING THIS LOAD STEP
USE 5 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM
FOR AUTOMATIC TIME STEPPING:
USE 1000 SUBSTEPS AS A MAXIMUM
USE 1 SUBSTEPS AS A MINIMUM
TIME= 0.10000
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
WRITE ALL ITEMS TO THE DATABASE WITH A FREQUENCY OF NONE
FOR ALL APPLICABLE ENTITIES
WRITE NSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EANG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE ETMP ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE VENG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE CONT ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 0.672
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Research
00000000 VERSION=WINDOWS x64 14:08:48 SEP 05, 2024 CP= 0.672
800um_simplified_TEST--Static Structural (A5)
***** ANSYS ANALYSIS DEFINITION (PREP7) *****
ELEMENT TYPE 9991 IS CPT215 3D COUPLED SOLID
KEYOPT( 1- 6)= 0 0 0 0 0 0
KEYOPT( 7-12)= 0 0 0 0 0 0
KEYOPT(13-18)= 0 0 0 0 0 0
CURRENT NODAL DOF SET IS UX UY UZ ROTX ROTY ROTZ
THREE-DIMENSIONAL MODEL
ELEMENT TYPE 9991 IS CPT215 3D COUPLED SOLID
KEYOPT( 1- 6)= 0 0 0 0 0 0
KEYOPT( 7-12)= 0 0 0 0 0 1
KEYOPT(13-18)= 0 0 0 0 0 0
CURRENT NODAL DOF SET IS UX UY UZ ROTX ROTY ROTZ PRES
THREE-DIMENSIONAL MODEL
ELEMENT TYPE 9991 IS CPT215 3D COUPLED SOLID
KEYOPT( 1- 6)= 0 0 0 0 0 1
KEYOPT( 7-12)= 0 0 0 0 0 1
KEYOPT(13-18)= 0 0 0 0 0 0
CURRENT NODAL DOF SET IS UX UY UZ ROTX ROTY ROTZ PRES
THREE-DIMENSIONAL MODEL
SELECT FOR ITEM=TYPE COMPONENT=
IN RANGE 1 TO 14 STEP 1
8550 ELEMENTS (OF 10310 DEFINED) SELECTED BY ESEL COMMAND.
MODIFY ALL SELECTED ELEMENTS TO HAVE TYPE = 9991
SELECT ALL ENTITIES OF TYPE= ALL AND BELOW
MATERIAL 99999 EX = 0.3000000E-02
MATERIAL 99999 PRXY = 0.4900000
PARAMETER FPX = 100000.0000
PARAMETER ALPHA = 1.000000000
FLUID PERMEABILITY OPTION FOR MATERIAL 99999
DATA FOR PM TABLE FOR MATERIAL 99999 AT TEMPERATURE= 23.0000
LOC= 1 1.00000e+05 1.00000e+05 1.00000e+05
FLUID BIOT OPTION FOR MATERIAL 99999
DATA FOR PM TABLE FOR MATERIAL 99999 AT TEMPERATURE= 23.0000
LOC= 1 1.00000e+00
NONE SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 16720 STEP 1
0 ELEMENTS (OF 10310 DEFINED) SELECTED BY ESEL COMMAND.
MATERIAL 88888 EX = 0.1000000E-19
MATERIAL 88888 PRXY = 0.000000
SELECT FOR ITEM=TYPE COMPONENT=
IN RANGE 15 TO 40 STEP 1
1760 ELEMENTS (OF 10310 DEFINED) SELECTED BY ESEL COMMAND.
SET MATERIAL OF SELECTED ELEMENTS TO 88888
MATERIAL 88889 EX = 300.0000
MATERIAL 88889 PRXY = 0.000000
SELECT ALL ENTITIES OF TYPE= ALL AND BELOW
INPUT SECTION ID NUMBER 1
INPUT SECTION TYPE REINF
INPUT REINF SECTION SUBTYPE SMEA
INPUT REINF SECTION NAME 1
SECTION ID NUMBER= 1
SECTION ID NUMBER IS: 1
Reinforcing Behavior: Tension Only
Remove Base Material: YES
Stress State : Uni-axial
REINFORCEMENT # 1
MatID Area Spacing iEsys Ori. Angle
88889 50.0000 8.0000 12 0.0000
PATTern n
LAYN 1
SELECT COMPONENT KCS_12
GENERATE REINF ELEMENTS FROM THE SELECTED ELEMENTS
NUMBER OF ELEMENT TYPES CREATED = 1
MAXIMUM ELEMENT TYPE NUMBER = 9992
Use ETLIST command to list new element types.
NUMBER OF REINF ELEMENT CREATED = 880
MAXIMUM ELEMENT NUMBER = 17600
Use ELIST command to list new elements.
SELECT ALL ENTITIES OF TYPE= ALL AND BELOW
INPUT SECTION ID NUMBER 2
INPUT SECTION TYPE REINF
INPUT REINF SECTION SUBTYPE SMEA
INPUT REINF SECTION NAME 2
SECTION ID NUMBER= 2
SECTION ID NUMBER IS: 2
Reinforcing Behavior: Tension Only
Remove Base Material: YES
Stress State : Uni-axial
REINFORCEMENT # 1
MatID Area Spacing iEsys Ori. Angle
88889 50.0000 8.0000 13 0.0000
PATTern n
LAYN 1
SELECT COMPONENT KCS_13
GENERATE REINF ELEMENTS FROM THE SELECTED ELEMENTS
NUMBER OF REINF ELEMENT CREATED = 880
MAXIMUM ELEMENT NUMBER = 18480
Use ELIST command to list new elements.
SELECT ALL ENTITIES OF TYPE= ALL AND BELOW
SELECT FOR ITEM=TYPE COMPONENT=
IN RANGE 9991 TO 9991 STEP 1
8550 ELEMENTS (OF 12070 DEFINED) SELECTED BY ESEL COMMAND.
SET MATERIAL OF SELECTED ELEMENTS TO 99999
SELECT ALL ENTITIES OF TYPE= ALL AND BELOW
SELECT ALL ENTITIES OF TYPE= ALL AND BELOW
SELECT FOR ITEM=LOC COMPONENT=Y BETWEEN 1000.0 AND 1000.0
KABS= 0. TOLERANCE= 5.00000
913 NODES (OF 10043 DEFINED) SELECTED BY NSEL COMMAND.
ALSO SELECT FOR ITEM=LOC COMPONENT=Y BETWEEN 0.0000 AND 0.0000
KABS= 0. TOLERANCE= 0.100000E-05
1826 NODES (OF 10043 DEFINED) SELECTED BY NSEL COMMAND.
GENERATE SURFACE LOAD FFLX ON SURFACE DEFINED BY ALL SELECTED NODES
VALUE = 0.00000000
NUMBER OF FFLX ELEMENT FACE LOADS STORED = 1710
SELECT ALL ENTITIES OF TYPE= ALL AND BELOW
ACTIVE COORDINATE SYSTEM SET TO 5 (CYLINDRICAL) Y- CYL. AXIS
SELECT FOR ITEM=LOC COMPONENT=X BETWEEN 3250.0 AND 3250.0
KABS= 0. TOLERANCE= 16.2500
583 NODES (OF 10043 DEFINED) SELECTED BY NSEL COMMAND.
SPECIFIED CONSTRAINT PRES FOR SELECTED NODES 1 TO 10043 BY 1
REAL= 0.00000000 IMAG= 0.00000000
SELECT ALL ENTITIES OF TYPE= ALL AND BELOW
ACTIVE COORDINATE SYSTEM SET TO 0 (CARTESIAN)
SELECT ALL ENTITIES OF TYPE= ALL AND BELOW
***** ROUTINE COMPLETED ***** CP = 0.984
***** ANSYS SOLUTION ROUTINE *****
*GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000
*IF ANSINTER_ ( = 0.00000 ) NE
0 ( = 0.00000 ) THEN
*ENDIF
*** NOTE *** CP = 1.125 TIME= 14:08:48
The automatic domain decomposition logic has selected the MESH domain
decomposition method with 10 processes per solution.
***** ANSYS SOLVE COMMAND *****
*** WARNING *** CP = 1.281 TIME= 14:08:48
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** WARNING *** CP = 1.281 TIME= 14:08:48
CPT215 wedges are recommended only in regions of relatively low stress
gradients.
*** NOTE *** CP = 1.281 TIME= 14:08:48
The model data was checked and warning messages were found.
Please review output or errors file ( C:\Users\mbgm4fs3\OneDrive -
The University of Manchester\PhD\Experimental\Data\2.
Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7\file0.err ) for
these warning messages.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 15 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 16 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 17 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 18 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 19 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 20 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 21 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 22 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 23 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 24 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 25 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 26 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 27 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 28 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 29 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 30 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 31 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 32 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 33 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 34 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 35 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 36 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 37 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 38 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 39 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
ELEMENT TYPE 40 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC
MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR
HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED.
KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET
IT MANUALLY IF NECESSARY.
KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Research
00000000 VERSION=WINDOWS x64 14:08:48 SEP 05, 2024 CP= 1.438
800um_simplified_TEST--Static Structural (A5)
S O L U T I O N O P T I O N S
PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
DEGREES OF FREEDOM. . . . . . UX UY UZ ROTX ROTY ROTZ PRES
ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
NONLINEAR GEOMETRIC EFFECTS . . . . . . . . . .ON
EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE
PLASTIC MATERIAL PROPERTIES INCLUDED. . . . . .YES
NEWTON-RAPHSON OPTION . . . . . . . . . . . . .PROGRAM CHOSEN
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .UNSYMMETRIC
*** NOTE *** CP = 1.750 TIME= 14:08:48
The RESCONTROL command does not support fluid analyses. The RESCONTROL
command settings have been de-activated.
*** NOTE *** CP = 1.750 TIME= 14:08:48
This nonlinear analysis defaults to using the full Newton-Raphson
solution procedure. This can be modified using the NROPT command.
*** NOTE *** CP = 1.750 TIME= 14:08:48
Internal nodes from 10044 to 18593 are created.
8550 internal nodes are used for non-contact elements with mixed
formulation.
D I S T R I B U T E D D O M A I N D E C O M P O S E R
...Number of elements: 12070
...Number of nodes: 18593
...Decompose to 10 CPU domains
...Element load balance ratio = 1.708
L O A D S T E P O P T I O N S
LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1
TIME AT END OF THE LOAD STEP. . . . . . . . . . 0.10000
AUTOMATIC TIME STEPPING . . . . . . . . . . . . ON
INITIAL NUMBER OF SUBSTEPS . . . . . . . . . 5
MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . . 1000
MINIMUM NUMBER OF SUBSTEPS . . . . . . . . . 1
MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS. . . . 15
STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO
STRESS-STIFFENING . . . . . . . . . . . . . . . ON
TERMINATE ANALYSIS IF NOT CONVERGED . . . . . .YES (EXIT)
NODAL DOF SOLUTION LIMIT. . . . . . . . . . . . 0.10000E+10
CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS
COPY INTEGRATION POINT VALUES TO NODE . . . . .YES, FOR ELEMENTS WITH
ACTIVE MAT. NONLINEARITIES
PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
DATABASE OUTPUT CONTROLS
ITEM FREQUENCY COMPONENT
ALL NONE
NSOL ALL
RSOL ALL
EANG ALL
ETMP ALL
VENG ALL
STRS ALL
EPEL ALL
EPPL ALL
CONT ALL
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr
*** NOTE *** CP = 3.000 TIME= 14:08:48
Predictor is ON by default for structural elements with rotational
degrees of freedom. Use the PRED,OFF command to turn the predictor
OFF if it adversely affects the convergence.
Range of element maximum matrix coefficients in global coordinates
Maximum = 468.75 at element 18080.
Minimum = 3.511720105E-17 at element 15871.
*** WARNING *** CP = 3.266 TIME= 14:08:48
Coefficient ratio exceeds 1.0e8 - Check results.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
15 80 SHELL181 0.000 0.000000
16 40 SHELL181 0.000 0.000000
17 80 SHELL181 0.000 0.000000
18 80 SHELL181 0.016 0.000195
19 80 SHELL181 0.000 0.000000
20 80 SHELL181 0.000 0.000000
21 80 SHELL181 0.016 0.000195
22 80 SHELL181 0.016 0.000195
23 80 SHELL181 0.000 0.000000
24 40 SHELL181 0.000 0.000000
25 80 SHELL181 0.031 0.000391
26 80 SHELL181 0.016 0.000195
27 40 SHELL181 0.000 0.000000
28 80 SHELL181 0.016 0.000195
29 40 SHELL181 0.000 0.000000
30 40 SHELL181 0.016 0.000391
31 40 SHELL181 0.016 0.000391
32 40 SHELL181 0.000 0.000000
33 40 SHELL181 0.000 0.000000
34 80 SHELL181 0.016 0.000195
35 80 SHELL181 0.000 0.000000
36 80 SHELL181 0.000 0.000000
37 80 SHELL181 0.016 0.000195
38 80 SHELL181 0.000 0.000000
39 80 SHELL181 0.000 0.000000
40 80 SHELL181 0.016 0.000195
9991 8550 CPT215 1.359 0.000159
9992 1760 REINF265 0.047 0.000027
Time at end of element matrix formulation CP = 3.265625.
FORCE CONVERGENCE VALUE = 0.7561 CRITERION= 0.3857E-02
MOMENT CONVERGENCE VALUE = 0.1102E-35 CRITERION= 0.2722E-01
FL FLOW CONVERGENCE VALUE= 0.3939E+05 CRITERION= 201.0
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 51208, Maximum wavefront = 245
Process memory allocated for solver = 144.271 MB
Process memory required for in-core solution = 101.080 MB
Process memory required for out-of-core solution = 49.924 MB
Total memory allocated for solver = 1215.992 MB
Total memory required for in-core solution = 837.109 MB
Total memory required for out-of-core solution = 404.072 MB
*** NOTE *** CP = 3.531 TIME= 14:08:48
The Distributed Sparse Matrix Solver is currently running in the
in-core memory mode. This memory mode uses the most amount of memory
in order to avoid using the hard drive as much as possible, which most
often results in the fastest solution time. This mode is recommended
if enough physical memory is present to accommodate all of the solver
data.
*** WARNING *** CP = 3.531 TIME= 14:08:48
Pivoting has been activated for the Distributed Sparse Matrix Solver .
The memory required may greatly exceed the predicted amount. In that
event, use the DSPOPTION command to change the memory mode and/or
memory size used by the Distributed Sparse Matrix Solver.
*** NOTE *** CP = 3.531 TIME= 14:08:48
The system matrix is unsymmetric.
curEqn= 6154 totEqn= 6154 Job CP sec= 4.281
Factor Done= 97% Factor Wall sec= 0.640 rate= 9.3 GFlops
Distributed sparse solver maximum pivot= 5.229458564E+11 at node 9241
UX.
Distributed sparse solver minimum pivot= -2243515.26 at node 3008 PRES.
Distributed sparse solver minimum pivot in absolute value= 20773.7634
at node 9869 ROTX.
DISP CONVERGENCE VALUE = 0.4267 CRITERION= 0.2177E-01
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4267
FORCE CONVERGENCE VALUE = 3.738 CRITERION= 0.2288E-01
MOMENT CONVERGENCE VALUE = 0.1611E-22 CRITERION= 0.1614 <<< CONVERGED
*** WARNING *** CP = 4.578 TIME= 14:08:50
A reference moment value times the tolerance is used by the
Newton-Raphson method for checking convergence. The calculated
reference MOMENT CONVERGENCE VALUE = 0 is less than a threshold. This
threshold is internally calculated. You can overwrite it by
specifying MINREF on the CNVTOL command. Check results carefully.
FL FLOW CONVERGENCE VALUE= 34.91 CRITERION= 0.1406
DISP CONVERGENCE VALUE = 0.9295E-03 CRITERION= 0.2226E-01 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.9295E-03
FORCE CONVERGENCE VALUE = 0.7697E-04 CRITERION= 0.2341E-01 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.1082E-23 CRITERION= 0.1652 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.8047E-01 CRITERION= 0.1433 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
15 80 SHELL181 0.016 0.000195
16 40 SHELL181 0.000 0.000000
17 80 SHELL181 0.000 0.000000
18 80 SHELL181 0.000 0.000000
19 80 SHELL181 0.000 0.000000
20 80 SHELL181 0.000 0.000000
21 80 SHELL181 0.000 0.000000
22 80 SHELL181 0.000 0.000000
23 80 SHELL181 0.000 0.000000
24 40 SHELL181 0.000 0.000000
25 80 SHELL181 0.016 0.000195
26 80 SHELL181 0.016 0.000195
27 40 SHELL181 0.000 0.000000
28 80 SHELL181 0.000 0.000000
29 40 SHELL181 0.000 0.000000
30 40 SHELL181 0.016 0.000391
31 40 SHELL181 0.016 0.000391
32 40 SHELL181 0.000 0.000000
33 40 SHELL181 0.000 0.000000
34 80 SHELL181 0.000 0.000000
35 80 SHELL181 0.000 0.000000
36 80 SHELL181 0.000 0.000000
37 80 SHELL181 0.016 0.000195
38 80 SHELL181 0.000 0.000000
39 80 SHELL181 0.000 0.000000
40 80 SHELL181 0.000 0.000000
9991 8550 CPT215 0.953 0.000111
9992 1760 REINF265 0.062 0.000036
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
15 80 SHELL181 0.000 0.000000
16 40 SHELL181 0.000 0.000000
17 80 SHELL181 0.000 0.000000
18 80 SHELL181 0.000 0.000000
19 80 SHELL181 0.000 0.000000
20 80 SHELL181 0.000 0.000000
21 80 SHELL181 0.000 0.000000
22 80 SHELL181 0.000 0.000000
23 80 SHELL181 0.000 0.000000
24 40 SHELL181 0.000 0.000000
25 80 SHELL181 0.000 0.000000
26 80 SHELL181 0.000 0.000000
27 40 SHELL181 0.000 0.000000
28 80 SHELL181 0.000 0.000000
29 40 SHELL181 0.000 0.000000
30 40 SHELL181 0.000 0.000000
31 40 SHELL181 0.000 0.000000
32 40 SHELL181 0.000 0.000000
33 40 SHELL181 0.000 0.000000
34 80 SHELL181 0.000 0.000000
35 80 SHELL181 0.000 0.000000
36 80 SHELL181 0.000 0.000000
37 80 SHELL181 0.000 0.000000
38 80 SHELL181 0.000 0.000000
39 80 SHELL181 0.000 0.000000
40 80 SHELL181 0.000 0.000000
9991 8550 CPT215 0.047 0.000005
9992 1760 REINF265 0.000 0.000000
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 2
*** TIME = 0.200000E-01 TIME INC = 0.200000E-01
*** MAX PORE PRESSURE STEP = 0.1063E-04
*** AUTO STEP TIME: NEXT TIME INC = 0.20000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 7.518 CRITERION= 0.4505E-01
MOMENT CONVERGENCE VALUE = 0.3464E-22 CRITERION= 0.3179
FL FLOW CONVERGENCE VALUE= 48.48 CRITERION= 0.1475
DISP CONVERGENCE VALUE = 0.1806E-02 CRITERION= 0.2187E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1806E-02
FORCE CONVERGENCE VALUE = 0.2186E-03 CRITERION= 0.4609E-01 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.2216E-23 CRITERION= 0.3252 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.1420 CRITERION= 0.2256 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.2321E-04 CRITERION= 0.2232E-01 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2321E-04
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 2 COMPLETED. CUM ITER = 4
*** TIME = 0.400000E-01 TIME INC = 0.200000E-01
*** MAX PORE PRESSURE STEP = 0.9987E-05
*** AUTO TIME STEP: NEXT TIME INC = 0.30000E-01 INCREASED (FACTOR = 1.5000)
FORCE CONVERGENCE VALUE = 14.23 CRITERION= 0.7935E-01
MOMENT CONVERGENCE VALUE = 0.7454E-22 CRITERION= 0.5598
FL FLOW CONVERGENCE VALUE= 85.10 CRITERION= 0.3473
DISP CONVERGENCE VALUE = 0.3344E-02 CRITERION= 0.3296E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.3344E-02
FORCE CONVERGENCE VALUE = 0.8090E-03 CRITERION= 0.8120E-01 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6337E-23 CRITERION= 0.5729 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.4175 CRITERION= 0.3764
DISP CONVERGENCE VALUE = 0.7817E-04 CRITERION= 0.3363E-01 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7817E-04
FORCE CONVERGENCE VALUE = 0.3357E-06 CRITERION= 0.8286E-01 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.2434E-27 CRITERION= 0.5846 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.5830E-02 CRITERION= 0.3841 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 3 COMPLETED. CUM ITER = 6
*** TIME = 0.700000E-01 TIME INC = 0.300000E-01
*** MAX PORE PRESSURE STEP = 0.1471E-04
*** AUTO STEP TIME: NEXT TIME INC = 0.30000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 17.30 CRITERION= 0.1142
MOMENT CONVERGENCE VALUE = 0.9108E-22 CRITERION= 0.8056
FL FLOW CONVERGENCE VALUE= 82.59 CRITERION= 0.3852
DISP CONVERGENCE VALUE = 0.4075E-02 CRITERION= 0.3313E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.4075E-02
FORCE CONVERGENCE VALUE = 0.1112E-02 CRITERION= 0.1168 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.7785E-23 CRITERION= 0.8240 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.4981 CRITERION= 0.4322
DISP CONVERGENCE VALUE = 0.1047E-03 CRITERION= 0.3381E-01 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1047E-03
FORCE CONVERGENCE VALUE = 0.6169E-06 CRITERION= 0.1192 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3398E-27 CRITERION= 0.8408 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.8170E-02 CRITERION= 0.4410 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 4 COMPLETED. CUM ITER = 8
*** TIME = 0.100000 TIME INC = 0.300000E-01
*** MAX PORE PRESSURE STEP = 0.1469E-04
*** ANSYS BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
18.938 MB WRITTEN ON ELEMENT MATRIX FILE: file0.emat
9.250 MB WRITTEN ON ELEMENT SAVED DATA FILE: file0.esav
8.500 MB WRITTEN ON ASSEMBLED MATRIX FILE: file0.full
3.875 MB WRITTEN ON RESULTS FILE: file0.rst
*************** Write FE CONNECTORS *********
WRITE OUT CONSTRAINT EQUATIONS TO FILE= file.ce
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
****************************************************
******************* SOLVE FOR LS 2 OF 3 ****************
*** Set Displacements ***
PRINTOUT RESUMED BY /GOP
USE AUTOMATIC TIME STEPPING THIS LOAD STEP
USE 1 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM
FOR AUTOMATIC TIME STEPPING:
USE 200 SUBSTEPS AS A MAXIMUM
USE 1 SUBSTEPS AS A MINIMUM
USE THE FINAL TIME STEP SIZE OF THE PREVIOUS LOAD STEP
AS THE STARTING TIME STEP SIZE.
TIME= 20.000
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
WRITE ALL ITEMS TO THE DATABASE WITH A FREQUENCY OF NONE
FOR ALL APPLICABLE ENTITIES
WRITE NSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EANG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE ETMP ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE VENG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE CONT ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
***** ANSYS SOLVE COMMAND *****
*** NOTE *** CP = 14.094 TIME= 14:08:59
The RESCONTROL command does not support fluid analyses. The RESCONTROL
command settings have been de-activated.
*** NOTE *** CP = 14.094 TIME= 14:08:59
This nonlinear analysis defaults to using the full Newton-Raphson
solution procedure. This can be modified using the NROPT command.
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Research
00000000 VERSION=WINDOWS x64 14:08:59 SEP 05, 2024 CP= 14.125
800um_simplified_TEST--Static Structural (A5)
L O A D S T E P O P T I O N S
LOAD STEP NUMBER. . . . . . . . . . . . . . . . 2
TIME AT END OF THE LOAD STEP. . . . . . . . . . 20.000
AUTOMATIC TIME STEPPING . . . . . . . . . . . . ON
INITIAL NUMBER OF SUBSTEPS . . . . . . . . . 1
MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . . 200
MINIMUM NUMBER OF SUBSTEPS . . . . . . . . . 1
START WITH TIME STEP FROM PREVIOUS SUBSTEP . YES
MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS. . . . 15
STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO
STRESS-STIFFENING . . . . . . . . . . . . . . . ON
TERMINATE ANALYSIS IF NOT CONVERGED . . . . . .YES (EXIT)
NODAL DOF SOLUTION LIMIT. . . . . . . . . . . . 0.10000E+10
CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS
COPY INTEGRATION POINT VALUES TO NODE . . . . .YES, FOR ELEMENTS WITH
ACTIVE MAT. NONLINEARITIES
PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
DATABASE OUTPUT CONTROLS
ITEM FREQUENCY COMPONENT
ALL NONE
NSOL ALL
RSOL ALL
EANG ALL
ETMP ALL
VENG ALL
STRS ALL
EPEL ALL
EPPL ALL
CONT ALL
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr
*** NOTE *** CP = 14.156 TIME= 14:08:59
Predictor is ON by default for structural elements with rotational
degrees of freedom. Use the PRED,OFF command to turn the predictor
OFF if it adversely affects the convergence.
FORCE CONVERGENCE VALUE = 3.825 CRITERION= 0.1161
MOMENT CONVERGENCE VALUE = 0.1426E-24 CRITERION= 0.8192
FL FLOW CONVERGENCE VALUE= 0.1962E+06 CRITERION= 1001.
DISP CONVERGENCE VALUE = 2.159 CRITERION= 0.1102
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 2.159
FORCE CONVERGENCE VALUE = 97.00 CRITERION= 0.2366
MOMENT CONVERGENCE VALUE = 0.8223E-21 CRITERION= 1.670 <<< CONVERGED
*** WARNING *** CP = 15.594 TIME= 14:09:01
A reference moment value times the tolerance is used by the
Newton-Raphson method for checking convergence. The calculated
reference MOMENT CONVERGENCE VALUE = 0 is less than a threshold. This
threshold is internally calculated. You can overwrite it by
specifying MINREF on the CNVTOL command. Check results carefully.
FL FLOW CONVERGENCE VALUE= 890.6 CRITERION= 1.657
DISP CONVERGENCE VALUE = 0.2326E-01 CRITERION= 0.1135 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2326E-01
FORCE CONVERGENCE VALUE = 0.4225E-01 CRITERION= 0.2434 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.1500E-21 CRITERION= 1.717 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 11.07 CRITERION= 1.675
DISP CONVERGENCE VALUE = 0.2779E-02 CRITERION= 0.1159 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2779E-02
FORCE CONVERGENCE VALUE = 0.5512E-03 CRITERION= 0.2483 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4675E-25 CRITERION= 1.752 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.8641 CRITERION= 1.709 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 2 SUBSTEP 1 COMPLETED. CUM ITER = 11
*** TIME = 0.199500 TIME INC = 0.995000E-01
*** MAX PORE PRESSURE STEP = 0.4906E-04
*** AUTO STEP TIME: NEXT TIME INC = 0.99500E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 199.5 CRITERION= 0.3550
MOMENT CONVERGENCE VALUE = 0.2309E-20 CRITERION= 2.505
FL FLOW CONVERGENCE VALUE= 855.3 CRITERION= 1.769
DISP CONVERGENCE VALUE = 0.4801E-01 CRITERION= 0.1133 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.4801E-01
FORCE CONVERGENCE VALUE = 0.1140 CRITERION= 0.3660 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3248E-21 CRITERION= 2.583 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 21.09 CRITERION= 1.898
DISP CONVERGENCE VALUE = 0.7567E-02 CRITERION= 0.1156 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7567E-02
FORCE CONVERGENCE VALUE = 0.4512E-02 CRITERION= 0.3733 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.1455E-24 CRITERION= 2.634 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 2.672 CRITERION= 1.934
DISP CONVERGENCE VALUE = 0.3288E-04 CRITERION= 0.1180 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.3288E-04
FORCE CONVERGENCE VALUE = 0.1117E-05 CRITERION= 0.3809 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6184E-26 CRITERION= 2.687 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.7808E-02 CRITERION= 1.974 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 2 SUBSTEP 2 COMPLETED. CUM ITER = 14
*** TIME = 0.299000 TIME INC = 0.995000E-01
*** MAX PORE PRESSURE STEP = 0.5058E-04
*** AUTO TIME STEP: NEXT TIME INC = 0.14925 INCREASED (FACTOR = 1.5000)
FORCE CONVERGENCE VALUE = 392.1 CRITERION= 0.5498
MOMENT CONVERGENCE VALUE = 0.5622E-20 CRITERION= 3.879
FL FLOW CONVERGENCE VALUE= 2036. CRITERION= 3.107
DISP CONVERGENCE VALUE = 0.9542E-01 CRITERION= 0.1739 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.9542E-01
FORCE CONVERGENCE VALUE = 0.3978 CRITERION= 0.5694 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.9866E-21 CRITERION= 4.018 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 67.98 CRITERION= 3.161
DISP CONVERGENCE VALUE = 0.2438E-01 CRITERION= 0.1774 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2438E-01
FORCE CONVERGENCE VALUE = 0.4422E-01 CRITERION= 0.5802 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.8360E-24 CRITERION= 4.094 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 13.39 CRITERION= 3.217
DISP CONVERGENCE VALUE = 0.1460E-03 CRITERION= 0.1810 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.1460E-03
FORCE CONVERGENCE VALUE = 0.7871E-05 CRITERION= 0.5920 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.9100E-25 CRITERION= 4.177 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.5809E-01 CRITERION= 3.284 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 2 SUBSTEP 3 COMPLETED. CUM ITER = 17
*** TIME = 0.448250 TIME INC = 0.149250
*** MAX PORE PRESSURE STEP = 0.8013E-04
*** AUTO TIME STEP: NEXT TIME INC = 0.22387 INCREASED (FACTOR = 1.5000)
FORCE CONVERGENCE VALUE = 937.8 CRITERION= 0.8648
MOMENT CONVERGENCE VALUE = 0.1953E-19 CRITERION= 6.101
FL FLOW CONVERGENCE VALUE= 4655. CRITERION= 5.524
DISP CONVERGENCE VALUE = 0.2307 CRITERION= 0.2702 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2307
FORCE CONVERGENCE VALUE = 1.735 CRITERION= 0.9064
MOMENT CONVERGENCE VALUE = 0.3717E-20 CRITERION= 6.395 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 271.9 CRITERION= 5.389
DISP CONVERGENCE VALUE = 0.9184E-01 CRITERION= 0.2757 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.9184E-01
FORCE CONVERGENCE VALUE = 0.5686 CRITERION= 0.9209 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6311E-23 CRITERION= 6.497 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 81.36 CRITERION= 5.465
DISP CONVERGENCE VALUE = 0.6871E-03 CRITERION= 0.2813 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.6871E-03
FORCE CONVERGENCE VALUE = 0.9802E-04 CRITERION= 0.9397 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.1729E-23 CRITERION= 6.630 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.5157 CRITERION= 5.583 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 2 SUBSTEP 4 COMPLETED. CUM ITER = 20
*** TIME = 0.672125 TIME INC = 0.223875
*** MAX PORE PRESSURE STEP = 0.1328E-03
*** AUTO TIME STEP: NEXT TIME INC = 0.33581 INCREASED (FACTOR = 1.5000)
FORCE CONVERGENCE VALUE = 2309. CRITERION= 1.398
MOMENT CONVERGENCE VALUE = 0.7181E-19 CRITERION= 9.860
FL FLOW CONVERGENCE VALUE= 0.1100E+05 CRITERION= 10.66
DISP CONVERGENCE VALUE = 0.5877 CRITERION= 0.4277
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.5877
FORCE CONVERGENCE VALUE = 8.988 CRITERION= 1.504
MOMENT CONVERGENCE VALUE = 0.1456E-19 CRITERION= 10.61 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 1181. CRITERION= 9.454
DISP CONVERGENCE VALUE = 0.2859 CRITERION= 0.4365 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2859
FORCE CONVERGENCE VALUE = 6.048 CRITERION= 1.514
MOMENT CONVERGENCE VALUE = 0.5984E-22 CRITERION= 10.68 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 466.7 CRITERION= 9.511
DISP CONVERGENCE VALUE = 0.6182E-02 CRITERION= 0.4454 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.6182E-02
FORCE CONVERGENCE VALUE = 0.6423E-02 CRITERION= 1.545 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.2895E-22 CRITERION= 10.90 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 6.575 CRITERION= 9.733 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 2 SUBSTEP 5 COMPLETED. CUM ITER = 23
*** TIME = 1.00794 TIME INC = 0.335812
*** MAX PORE PRESSURE STEP = 0.2336E-03
*** AUTO TIME STEP: NEXT TIME INC = 0.50372 INCREASED (FACTOR = 1.5000)
FORCE CONVERGENCE VALUE = 5919. CRITERION= 2.363
MOMENT CONVERGENCE VALUE = 0.2848E-18 CRITERION= 16.67
FL FLOW CONVERGENCE VALUE= 0.2711E+05 CRITERION= 23.47
DISP CONVERGENCE VALUE = 1.657 CRITERION= 0.6969
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -1.657
FORCE CONVERGENCE VALUE = 56.33 CRITERION= 2.719
MOMENT CONVERGENCE VALUE = 0.5987E-19 CRITERION= 19.18 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 5722. CRITERION= 18.37
DISP CONVERGENCE VALUE = 0.7270 CRITERION= 0.7112
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7270
FORCE CONVERGENCE VALUE = 54.06 CRITERION= 2.659
MOMENT CONVERGENCE VALUE = 0.7938E-21 CRITERION= 18.76 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 2519. CRITERION= 18.24
DISP CONVERGENCE VALUE = 0.7907E-01 CRITERION= 0.7257 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7907E-01
FORCE CONVERGENCE VALUE = 0.6206 CRITERION= 2.712 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4665E-21 CRITERION= 19.14 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 131.4 CRITERION= 18.67
DISP CONVERGENCE VALUE = 0.9801E-02 CRITERION= 0.7405 <<< CONVERGED
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.9801E-02
FORCE CONVERGENCE VALUE = 0.6155E-02 CRITERION= 2.768 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6029E-23 CRITERION= 19.53 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 13.81 CRITERION= 19.06 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 4
*** LOAD STEP 2 SUBSTEP 6 COMPLETED. CUM ITER = 27
*** TIME = 1.51166 TIME INC = 0.503719
*** MAX PORE PRESSURE STEP = 0.4560E-03
*** AUTO TIME STEP: NEXT TIME INC = 0.75558 INCREASED (FACTOR = 1.5000)
FORCE CONVERGENCE VALUE = 0.1582E+05 CRITERION= 4.343
MOMENT CONVERGENCE VALUE = 0.1287E-17 CRITERION= 30.64
FL FLOW CONVERGENCE VALUE= 0.7247E+05 CRITERION= 63.93
DISP CONVERGENCE VALUE = 4.684 CRITERION= 1.186
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -4.684
FORCE CONVERGENCE VALUE = 431.1 CRITERION= 6.029
MOMENT CONVERGENCE VALUE = 0.2530E-18 CRITERION= 42.54 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.3170E+05 CRITERION= 46.77
DISP CONVERGENCE VALUE = 2.180 CRITERION= 1.222
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 2.180
FORCE CONVERGENCE VALUE = 302.6 CRITERION= 5.411
MOMENT CONVERGENCE VALUE = 0.1157E-19 CRITERION= 38.18 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.1143E+05 CRITERION= 48.47
DISP CONVERGENCE VALUE = 0.5966 CRITERION= 1.247 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.5966
FORCE CONVERGENCE VALUE = 52.40 CRITERION= 5.522
MOMENT CONVERGENCE VALUE = 0.5196E-20 CRITERION= 38.96 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 3061. CRITERION= 49.28
DISP CONVERGENCE VALUE = 0.2303 CRITERION= 1.273 <<< CONVERGED
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2303
FORCE CONVERGENCE VALUE = 3.313 CRITERION= 5.629 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.7963E-21 CRITERION= 39.72 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 692.3 CRITERION= 50.31
DISP CONVERGENCE VALUE = 0.9720E-02 CRITERION= 1.299 <<< CONVERGED
EQUIL ITER 5 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.9720E-02
FORCE CONVERGENCE VALUE = 0.2244E-01 CRITERION= 5.744 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5824E-22 CRITERION= 40.53 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 38.77 CRITERION= 51.33 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 5
*** LOAD STEP 2 SUBSTEP 7 COMPLETED. CUM ITER = 32
*** TIME = 2.26723 TIME INC = 0.755578
*** MAX PORE PRESSURE STEP = 0.1118E-02
*** AUTO TIME STEP: NEXT TIME INC = 1.1334 INCREASED (FACTOR = 1.5000)
VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR 100 U-P ELEMENTS
FORCE CONVERGENCE VALUE = 0.4045E+05 CRITERION= 9.588
MOMENT CONVERGENCE VALUE = 0.7521E-17 CRITERION= 67.65
FL FLOW CONVERGENCE VALUE= 0.2288E+06 CRITERION= 239.4
DISP CONVERGENCE VALUE = 13.24 CRITERION= 2.091
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -13.24
FORCE CONVERGENCE VALUE = 6138. CRITERION= 19.17
MOMENT CONVERGENCE VALUE = 0.1108E-17 CRITERION= 135.2 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.1728E+06 CRITERION= 161.6
DISP CONVERGENCE VALUE = 4.640 CRITERION= 2.227
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -4.640
FORCE CONVERGENCE VALUE = 2161. CRITERION= 17.12
MOMENT CONVERGENCE VALUE = 0.2520E-18 CRITERION= 120.8 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.7262E+05 CRITERION= 212.2
DISP CONVERGENCE VALUE = 3.069 CRITERION= 2.278
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 3.069
FORCE CONVERGENCE VALUE = 1940. CRITERION= 17.57
MOMENT CONVERGENCE VALUE = 0.3257E-19 CRITERION= 124.0 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.3077E+05 CRITERION= 221.1
DISP CONVERGENCE VALUE = 0.9579 CRITERION= 2.329 <<< CONVERGED
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.9579
FORCE CONVERGENCE VALUE = 129.3 CRITERION= 17.83
MOMENT CONVERGENCE VALUE = 0.4058E-19 CRITERION= 125.8 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.1062E+05 CRITERION= 233.4
DISP CONVERGENCE VALUE = 0.3916 CRITERION= 2.377 <<< CONVERGED
EQUIL ITER 5 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.3916
FORCE CONVERGENCE VALUE = 18.15 CRITERION= 18.20 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.2693E-20 CRITERION= 128.4 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 2981. CRITERION= 239.9
DISP CONVERGENCE VALUE = 0.2909E-01 CRITERION= 2.426 <<< CONVERGED
EQUIL ITER 6 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2909E-01
FORCE CONVERGENCE VALUE = 0.1215 CRITERION= 18.57 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4904E-21 CRITERION= 131.0 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 265.3 CRITERION= 245.1
DISP CONVERGENCE VALUE = 0.2002E-02 CRITERION= 2.475 <<< CONVERGED
EQUIL ITER 7 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2002E-02
FORCE CONVERGENCE VALUE = 0.2682E-02 CRITERION= 18.94 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.1349E-20 CRITERION= 133.7 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 14.92 CRITERION= 250.1 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 7
*** LOAD STEP 2 SUBSTEP 8 COMPLETED. CUM ITER = 39
*** TIME = 3.40060 TIME INC = 1.13337
*** MAX PORE PRESSURE STEP = 0.4758E-02
*** AUTO STEP TIME: NEXT TIME INC = 1.1334 UNCHANGED
VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR 390 U-P ELEMENTS
FORCE CONVERGENCE VALUE = 0.4581E+05 CRITERION= 28.54
MOMENT CONVERGENCE VALUE = 0.2427E-16 CRITERION= 201.4
FL FLOW CONVERGENCE VALUE= 0.4307E+06 CRITERION= 660.3
DISP CONVERGENCE VALUE = 17.82 CRITERION= 2.425
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 17.82
FORCE CONVERGENCE VALUE = 5937. CRITERION= 46.44
MOMENT CONVERGENCE VALUE = 0.2157E-17 CRITERION= 327.7 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.2027E+06 CRITERION= 320.4
DISP CONVERGENCE VALUE = 34.97 CRITERION= 2.475
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 34.97
VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR 50 U-P ELEMENTS
FORCE CONVERGENCE VALUE = 7166. CRITERION= 48.01
MOMENT CONVERGENCE VALUE = 0.1096E-17 CRITERION= 338.7 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.2362E+06 CRITERION= 271.3
DISP CONVERGENCE VALUE = 14.97 CRITERION= 2.525
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -14.97
VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR 10 U-P ELEMENTS
FORCE CONVERGENCE VALUE = 1031. CRITERION= 49.50
MOMENT CONVERGENCE VALUE = 0.2221E-18 CRITERION= 349.2 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.7745E+05 CRITERION= 256.4
DISP CONVERGENCE VALUE = 12.01 CRITERION= 2.577
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -12.01
FORCE CONVERGENCE VALUE = 432.7 CRITERION= 50.40
MOMENT CONVERGENCE VALUE = 0.5230E-18 CRITERION= 355.6 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.3753E+05 CRITERION= 268.5
DISP CONVERGENCE VALUE = 2.878 CRITERION= 2.630
EQUIL ITER 5 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -2.878
FORCE CONVERGENCE VALUE = 5.817 CRITERION= 51.48 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.2304E-17 CRITERION= 363.2 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 9376. CRITERION= 275.9
DISP CONVERGENCE VALUE = 0.7062 CRITERION= 2.683 <<< CONVERGED
EQUIL ITER 6 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7062
FORCE CONVERGENCE VALUE = 0.7384 CRITERION= 52.53 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.1639E-16 CRITERION= 370.6 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 2734. CRITERION= 281.7
DISP CONVERGENCE VALUE = 0.2700 CRITERION= 2.738 <<< CONVERGED
EQUIL ITER 7 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 1.130
FORCE CONVERGENCE VALUE = 0.2003 CRITERION= 53.60 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5060E-16 CRITERION= 378.2 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 1057. CRITERION= 287.4
DISP CONVERGENCE VALUE = 0.1129 CRITERION= 2.794 <<< CONVERGED
EQUIL ITER 8 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7755
FORCE CONVERGENCE VALUE = 0.7950E-01 CRITERION= 54.70 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5057E-16 CRITERION= 1304. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 443.5 CRITERION= 293.3
DISP CONVERGENCE VALUE = 0.4754E-01 CRITERION= 2.851 <<< CONVERGED
EQUIL ITER 9 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7791
FORCE CONVERGENCE VALUE = 0.3336E-01 CRITERION= 55.81 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6252E-16 CRITERION= 1444. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 186.3 CRITERION= 299.3 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 9
*** LOAD STEP 2 SUBSTEP 9 COMPLETED. CUM ITER = 48
*** TIME = 4.53397 TIME INC = 1.13337
*** MAX PORE PRESSURE STEP = 0.1223E-01
*** AUTO STEP TIME: NEXT TIME INC = 1.1334 UNCHANGED
VOLUMETRIC COMPATIBILITY IS NOT SATISFIED FOR 190 U-P ELEMENTS
FORCE CONVERGENCE VALUE = 0.2435E+05 CRITERION= 76.72
MOMENT CONVERGENCE VALUE = 0.2261E-15 CRITERION= 541.3
FL FLOW CONVERGENCE VALUE= 0.6893E+06 CRITERION= 382.2
DISP CONVERGENCE VALUE = 8.530 CRITERION= 2.425
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -8.530
FORCE CONVERGENCE VALUE = 1181. CRITERION= 81.14
MOMENT CONVERGENCE VALUE = 0.2108E-15 CRITERION= 572.5 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.9262E+05 CRITERION= 187.3
DISP CONVERGENCE VALUE = 267.2 CRITERION= 13.73
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 267.2
*** ERROR *** CP = 72.000 TIME= 14:09:58
Element 1927 (CPT215) is turning inside out.
*** ERROR *** CP = 72.000 TIME= 14:09:58
Element 1927 (CPT215) is turning inside out.
*** ERROR *** CP = 72.000 TIME= 14:09:58
Element 1927 (CPT215) is turning inside out.
*** ERROR *** CP = 72.000 TIME= 14:09:58
Element 1927 (CPT215) is turning inside out.
*** LOAD STEP 2 SUBSTEP 10 NOT COMPLETED. CUM ITER = 51
*** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 0.39668
FORCE CONVERGENCE VALUE = 5879. CRITERION= 57.09
MOMENT CONVERGENCE VALUE = 0.1579E-15 CRITERION= 402.8
FL FLOW CONVERGENCE VALUE= 0.1463E+06 CRITERION= 97.41
DISP CONVERGENCE VALUE = 3.466 CRITERION= 2.425
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -3.466
FORCE CONVERGENCE VALUE = 185.6 CRITERION= 59.07
MOMENT CONVERGENCE VALUE = 0.3736E-15 CRITERION= 416.7 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 0.1222E+05 CRITERION= 62.15
DISP CONVERGENCE VALUE = 2.332 CRITERION= 2.475 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 2.332
FORCE CONVERGENCE VALUE = 208.7 CRITERION= 60.64
MOMENT CONVERGENCE VALUE = 0.1069E-15 CRITERION= 427.8 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 6387. CRITERION= 62.62
DISP CONVERGENCE VALUE = 0.9841E-01 CRITERION= 2.525 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.7170
FORCE CONVERGENCE VALUE = 0.5591 CRITERION= 61.89 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6755E-16 CRITERION= 436.6 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 155.3 CRITERION= 64.08
DISP CONVERGENCE VALUE = 0.1904E-01 CRITERION= 2.577 <<< CONVERGED
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.5226
FORCE CONVERGENCE VALUE = 0.4401E-01 CRITERION= 63.15 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.8709E-16 CRITERION= 445.6 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 35.96 CRITERION= 65.40 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 4
*** LOAD STEP 2 SUBSTEP 10 COMPLETED. CUM ITER = 54
*** TIME = 4.93065 TIME INC = 0.396679
*** MAX PORE PRESSURE STEP = 0.4618E-02
*** AUTO STEP TIME: NEXT TIME INC = 0.39668 UNCHANGED
FORCE CONVERGENCE VALUE = 666.6 CRITERION= 69.95
MOMENT CONVERGENCE VALUE = 0.1975E-15 CRITERION= 493.5
FL FLOW CONVERGENCE VALUE= 0.7014E+05 CRITERION= 48.63
DISP CONVERGENCE VALUE = 1.067 CRITERION= 2.425 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 1.939
FORCE CONVERGENCE VALUE = 31.23 CRITERION= 71.24 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.2013E-15 CRITERION= 502.6 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 3367. CRITERION= 48.02
DISP CONVERGENCE VALUE = 0.1581 CRITERION= 2.475 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 1.363
FORCE CONVERGENCE VALUE = 1.372 CRITERION= 72.71 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3373E-15 CRITERION= 513.0 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 280.6 CRITERION= 49.06
DISP CONVERGENCE VALUE = 0.2799E-01 CRITERION= 2.525 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -4.089
FORCE CONVERGENCE VALUE = 0.2609 CRITERION= 74.20 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.1580E-15 CRITERION= 523.5 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 43.70 CRITERION= 50.08 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 2 SUBSTEP 11 COMPLETED. CUM ITER = 57
*** TIME = 5.32733 TIME INC = 0.396679
*** MAX PORE PRESSURE STEP = 0.4522E-02
*** AUTO TIME STEP: NEXT TIME INC = 0.59502 INCREASED (FACTOR = 1.5000)
FORCE CONVERGENCE VALUE = 587.3 CRITERION= 87.18
MOMENT CONVERGENCE VALUE = 0.3086E-15 CRITERION= 615.1
FL FLOW CONVERGENCE VALUE= 0.8860E+05 CRITERION= 66.17
DISP CONVERGENCE VALUE = 1.496 CRITERION= 2.425 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 8.691
FORCE CONVERGENCE VALUE = 38.51 CRITERION= 88.40 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3608E-15 CRITERION= 623.7 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 5290. CRITERION= 59.75
DISP CONVERGENCE VALUE = 0.1473 CRITERION= 2.475 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -3.891
FORCE CONVERGENCE VALUE = 1.505 CRITERION= 90.20 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3548E-15 CRITERION= 636.4 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 426.3 CRITERION= 60.97
DISP CONVERGENCE VALUE = 0.3329E-01 CRITERION= 2.525 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 6.286
FORCE CONVERGENCE VALUE = 0.3339 CRITERION= 92.05 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4107E-15 CRITERION= 649.4 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 96.47 CRITERION= 62.20
DISP CONVERGENCE VALUE = 0.3904E-01 CRITERION= 2.577 <<< CONVERGED
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 4.981
FORCE CONVERGENCE VALUE = 0.1015 CRITERION= 93.92 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3452E-15 CRITERION= 662.7 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 102.7 CRITERION= 63.48
DISP CONVERGENCE VALUE = 0.5016E-01 CRITERION= 2.630 <<< CONVERGED
EQUIL ITER 5 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 3.366
FORCE CONVERGENCE VALUE = 0.5361E-01 CRITERION= 95.84 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6781E-15 CRITERION= 676.2 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 126.7 CRITERION= 64.77
DISP CONVERGENCE VALUE = 0.6416E-01 CRITERION= 2.683 <<< CONVERGED
EQUIL ITER 6 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -3.811
FORCE CONVERGENCE VALUE = 0.5683E-01 CRITERION= 97.80 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.7182E-15 CRITERION= 690.0 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 158.6 CRITERION= 66.09
DISP CONVERGENCE VALUE = 0.8207E-01 CRITERION= 2.738 <<< CONVERGED
EQUIL ITER 7 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 2.992
FORCE CONVERGENCE VALUE = 0.7051E-01 CRITERION= 99.79 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4953E-15 CRITERION= 704.1 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 199.4 CRITERION= 67.44
DISP CONVERGENCE VALUE = 0.1050 CRITERION= 2.794 <<< CONVERGED
EQUIL ITER 8 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -2.960
FORCE CONVERGENCE VALUE = 0.8889E-01 CRITERION= 101.8 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.2620E-15 CRITERION= 2546. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 251.6 CRITERION= 68.82
DISP CONVERGENCE VALUE = 0.1342 CRITERION= 2.851 <<< CONVERGED
EQUIL ITER 9 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 2.774
FORCE CONVERGENCE VALUE = 0.1124 CRITERION= 103.9 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.2076E-15 CRITERION= 2547. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 318.3 CRITERION= 70.22
>>> PREDICTED NUMBER OF ITERATIONS FOR CONVERGENCE= 30 EXCEEDS MAX OF 15
*** LOAD STEP 2 SUBSTEP 12 NOT COMPLETED. CUM ITER = 67
*** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 0.29751
FORCE CONVERGENCE VALUE = 205.8 CRITERION= 78.51
MOMENT CONVERGENCE VALUE = 0.2853E-15 CRITERION= 554.0
FL FLOW CONVERGENCE VALUE= 0.3095E+05 CRITERION= 30.83
DISP CONVERGENCE VALUE = 0.6181 CRITERION= 2.425 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -6.432
FORCE CONVERGENCE VALUE = 7.216 CRITERION= 79.88 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.2714E-15 CRITERION= 563.6 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 1083. CRITERION= 29.37
DISP CONVERGENCE VALUE = 0.3623E-01 CRITERION= 2.475 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -4.935
FORCE CONVERGENCE VALUE = 0.3910 CRITERION= 81.51 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3278E-15 CRITERION= 575.1 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 64.57 CRITERION= 30.02
DISP CONVERGENCE VALUE = 0.8467E-02 CRITERION= 2.525 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 5.181
FORCE CONVERGENCE VALUE = 0.9098E-01 CRITERION= 83.17 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4019E-15 CRITERION= 586.8 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 13.85 CRITERION= 30.63 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 2 SUBSTEP 12 COMPLETED. CUM ITER = 69
*** TIME = 5.62483 TIME INC = 0.297509
*** MAX PORE PRESSURE STEP = 0.3283E-02
*** AUTO STEP TIME: NEXT TIME INC = 0.29751 UNCHANGED
FORCE CONVERGENCE VALUE = 97.46 CRITERION= 86.72
MOMENT CONVERGENCE VALUE = 0.6952E-15 CRITERION= 611.8
FL FLOW CONVERGENCE VALUE= 0.2336E+05 CRITERION= 33.00
DISP CONVERGENCE VALUE = 0.3858 CRITERION= 2.425 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 6.305
FORCE CONVERGENCE VALUE = 4.304 CRITERION= 88.32 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6284E-15 CRITERION= 623.2 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 627.0 CRITERION= 30.59
DISP CONVERGENCE VALUE = 0.6861E-01 CRITERION= 2.475 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 3.761
FORCE CONVERGENCE VALUE = 0.5457 CRITERION= 90.13 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5502E-15 CRITERION= 635.9 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 102.3 CRITERION= 31.22
DISP CONVERGENCE VALUE = 0.6230E-01 CRITERION= 2.525 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 6.646
FORCE CONVERGENCE VALUE = 0.1439 CRITERION= 91.97 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5651E-15 CRITERION= 648.9 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 107.4 CRITERION= 31.85
DISP CONVERGENCE VALUE = 0.7607E-01 CRITERION= 2.577 <<< CONVERGED
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 4.688
FORCE CONVERGENCE VALUE = 0.9129E-01 CRITERION= 93.84 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5234E-15 CRITERION= 662.1 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 128.1 CRITERION= 32.50
DISP CONVERGENCE VALUE = 0.9759E-01 CRITERION= 2.630 <<< CONVERGED
EQUIL ITER 5 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 3.905
FORCE CONVERGENCE VALUE = 0.1036 CRITERION= 95.76 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5851E-15 CRITERION= 675.6 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 155.4 CRITERION= 33.17
DISP CONVERGENCE VALUE = 0.1251 CRITERION= 2.683 <<< CONVERGED
EQUIL ITER 6 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 5.946
FORCE CONVERGENCE VALUE = 0.1262 CRITERION= 97.71 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3994E-15 CRITERION= 689.4 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 190.1 CRITERION= 33.84
DISP CONVERGENCE VALUE = 0.1603 CRITERION= 2.738 <<< CONVERGED
EQUIL ITER 7 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 3.675
FORCE CONVERGENCE VALUE = 0.1554 CRITERION= 99.71 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5509E-15 CRITERION= 703.5 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 234.3 CRITERION= 34.53
DISP CONVERGENCE VALUE = 0.2055 CRITERION= 2.794 <<< CONVERGED
EQUIL ITER 8 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 6.289
FORCE CONVERGENCE VALUE = 0.1925 CRITERION= 101.7 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3442E-15 CRITERION= 2363. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 290.2 CRITERION= 35.24
>>> PREDICTED NUMBER OF ITERATIONS FOR CONVERGENCE= 30 EXCEEDS MAX OF 15
*** LOAD STEP 2 SUBSTEP 13 NOT COMPLETED. CUM ITER = 78
*** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 0.99500E-01
FORCE CONVERGENCE VALUE = 21.77 CRITERION= 81.10
MOMENT CONVERGENCE VALUE = 0.5083E-15 CRITERION= 572.2
FL FLOW CONVERGENCE VALUE= 5148. CRITERION= 10.17
DISP CONVERGENCE VALUE = 0.1001 CRITERION= 2.425 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 5.594
FORCE CONVERGENCE VALUE = 0.9471 CRITERION= 82.71 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4473E-15 CRITERION= 583.6 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 52.90 CRITERION= 9.302
DISP CONVERGENCE VALUE = 0.1839E-01 CRITERION= 2.475 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 4.107
FORCE CONVERGENCE VALUE = 0.1159 CRITERION= 84.40 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3971E-15 CRITERION= 595.5 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 9.614 CRITERION= 9.494
DISP CONVERGENCE VALUE = 0.1509E-01 CRITERION= 2.525 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 4.687
FORCE CONVERGENCE VALUE = 0.2872E-01 CRITERION= 86.13 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4126E-15 CRITERION= 607.7 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 8.598 CRITERION= 9.687 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 2 SUBSTEP 13 COMPLETED. CUM ITER = 80
*** TIME = 5.72433 TIME INC = 0.995000E-01
*** MAX PORE PRESSURE STEP = 0.1076E-02
*** AUTO STEP TIME: NEXT TIME INC = 0.99500E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 7.751 CRITERION= 83.84
MOMENT CONVERGENCE VALUE = 0.6206E-15 CRITERION= 591.5
FL FLOW CONVERGENCE VALUE= 2834. CRITERION= 9.998
DISP CONVERGENCE VALUE = 0.7224E-01 CRITERION= 2.425 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -7.322
FORCE CONVERGENCE VALUE = 0.3590 CRITERION= 85.53 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5841E-15 CRITERION= 603.5 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 35.06 CRITERION= 10.53
DISP CONVERGENCE VALUE = 0.4769E-01 CRITERION= 2.475 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -8.339
FORCE CONVERGENCE VALUE = 0.5837E-01 CRITERION= 87.27 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4523E-15 CRITERION= 615.8 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 25.09 CRITERION= 10.75
DISP CONVERGENCE VALUE = 0.5387E-01 CRITERION= 2.525 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 6.505
FORCE CONVERGENCE VALUE = 0.5371E-01 CRITERION= 89.06 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.4416E-15 CRITERION= 628.3 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 27.54 CRITERION= 10.97
DISP CONVERGENCE VALUE = 0.6188E-01 CRITERION= 2.577 <<< CONVERGED
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 8.599
FORCE CONVERGENCE VALUE = 0.5913E-01 CRITERION= 90.87 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5724E-15 CRITERION= 641.2 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 30.53 CRITERION= 11.19
DISP CONVERGENCE VALUE = 0.7110E-01 CRITERION= 2.630 <<< CONVERGED
EQUIL ITER 5 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 6.093
FORCE CONVERGENCE VALUE = 0.6585E-01 CRITERION= 92.73 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.5550E-15 CRITERION= 654.3 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 34.01 CRITERION= 11.42
DISP CONVERGENCE VALUE = 0.8170E-01 CRITERION= 2.683 <<< CONVERGED
EQUIL ITER 6 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 8.481
FORCE CONVERGENCE VALUE = 0.7367E-01 CRITERION= 94.62 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.3846E-15 CRITERION= 667.6 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 38.05 CRITERION= 11.66
DISP CONVERGENCE VALUE = 0.9388E-01 CRITERION= 2.738 <<< CONVERGED
EQUIL ITER 7 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 6.800
FORCE CONVERGENCE VALUE = 0.8275E-01 CRITERION= 96.55 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6934E-15 CRITERION= 681.2 <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 42.75 CRITERION= 11.89
DISP CONVERGENCE VALUE = 0.1079 CRITERION= 2.794 <<< CONVERGED
EQUIL ITER 8 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 6.546
FORCE CONVERGENCE VALUE = 0.9326E-01 CRITERION= 98.52 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6029E-15 CRITERION= 2445. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 48.18 CRITERION= 12.14
DISP CONVERGENCE VALUE = 0.1240 CRITERION= 2.851 <<< CONVERGED
EQUIL ITER 9 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -7.890
FORCE CONVERGENCE VALUE = 0.1054 CRITERION= 100.5 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.7328E-15 CRITERION= 2472. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 54.52 CRITERION= 12.38
DISP CONVERGENCE VALUE = 0.1424 CRITERION= 2.909 <<< CONVERGED
EQUIL ITER 10 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 9.012
FORCE CONVERGENCE VALUE = 0.1195 CRITERION= 102.6 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6199E-15 CRITERION= 2497. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 61.77 CRITERION= 12.64
DISP CONVERGENCE VALUE = 0.1637 CRITERION= 2.968 <<< CONVERGED
EQUIL ITER 11 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 5.415
FORCE CONVERGENCE VALUE = 0.1358 CRITERION= 104.7 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.7637E-15 CRITERION= 2522. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 70.28 CRITERION= 12.89
DISP CONVERGENCE VALUE = 0.1880 CRITERION= 3.029 <<< CONVERGED
EQUIL ITER 12 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 6.784
FORCE CONVERGENCE VALUE = 0.1545 CRITERION= 106.8 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6105E-15 CRITERION= 2547. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 79.94 CRITERION= 13.16
DISP CONVERGENCE VALUE = 0.2161 CRITERION= 3.091 <<< CONVERGED
EQUIL ITER 13 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -6.282
FORCE CONVERGENCE VALUE = 0.1762 CRITERION= 109.0 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.7224E-15 CRITERION= 2571. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 91.38 CRITERION= 13.43
DISP CONVERGENCE VALUE = 0.2483 CRITERION= 3.154 <<< CONVERGED
EQUIL ITER 14 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -4.604
FORCE CONVERGENCE VALUE = 0.2012 CRITERION= 111.2 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6804E-15 CRITERION= 2595. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 104.2 CRITERION= 13.70
DISP CONVERGENCE VALUE = 0.2853 CRITERION= 3.218 <<< CONVERGED
EQUIL ITER 15 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 7.095
FORCE CONVERGENCE VALUE = 0.2300 CRITERION= 113.5 <<< CONVERGED
MOMENT CONVERGENCE VALUE = 0.6416E-15 CRITERION= 2618. <<< CONVERGED
FL FLOW CONVERGENCE VALUE= 119.6 CRITERION= 13.98
*** ERROR *** CP = 131.781 TIME= 14:10:58
Solution not converged at time 5.82383467 (load step 2 substep 14).
Run terminated.
*** WARNING *** CP = 131.781 TIME= 14:10:58
The unconverged solution (identified as time 20 substep 999999) is
output for analysis debug purposes. Results should not be used for
any other purpose.
R E S T A R T I N F O R M A T I O N
REASON FOR TERMINATION. . . . . . . . . .UNCONVERGED SOLUTION
FILES NEEDED FOR RESTARTING . . . . . . . file0.osav
file0.emat
file.db
TIME OF LAST SOLUTION . . . . . . . . . . 5.7243
TIME AT START OF THE LOAD STEP . . . . 0.10000
TIME AT END OF THE LOAD STEP . . . . . 20.000
NOTE: FOR CONVERGING SOLUTIONS, ADDITIONAL EQUILIBRIUM ITERATIONS MAY BE
ADDED IN THE RESTART (NEQIT COMMAND) USING THE RESTART FILE file0.esav
ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.db
FOR POSSIBLE RESUME FROM THIS POINT
NUMBER OF WARNING MESSAGES ENCOUNTERED= 7
NUMBER OF ERROR MESSAGES ENCOUNTERED= 5
***** PROBLEM TERMINATED BY INDICATED ERROR(S) OR BY END OF INPUT DATA *****
+--------- D I S T R I B U T E D A N S Y S S T A T I S T I C S ------------+
Release: 2022 R1 Build: 22.1 Update: UP20211129 Platform: WINDOWS x64
Date Run: 09/05/2024 Time: 14:10 Process ID: 15340
Operating System: Windows 10 (Build: 19044)
Processor Model: 12th Gen Intel(R) Core(TM) i7-12700
Compiler: Intel(R) Fortran Compiler Version 19.0.5 (Build: 20190815)
Intel(R) C/C++ Compiler Version 19.0.5 (Build: 20190815)
Intel(R) Math Kernel Library Version 2020.0.0 Product Build 20191125
BLAS Library supplied by Intel(R) MKL
Number of machines requested : 1
Total number of cores available : 20
Number of physical cores available : 12
Number of processes requested : 10
Number of threads per process requested : 1
Total number of cores requested : 10 (Distributed Memory Parallel)
MPI Type: INTELMPI
MPI Version: Intel(R) MPI Library 2019 Update 10 for Windows* OS
GPU Acceleration: Not Requested
Job Name: file0
Input File: dummy.dat
Core Machine Name Working Directory
-----------------------------------------------------
0 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
1 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
2 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
3 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
4 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
5 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
6 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
7 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
8 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
9 E-10VXXC3177879 C:\Users\mbgm4fs3\OneDrive - The University of Manchester\PhD\Experimental\Data\2. Modelling\workbench 2022 R1\_ProjectScratch\ScrE7A7
Latency time from master to core 1 = 1.974 microseconds
Latency time from master to core 2 = 1.910 microseconds
Latency time from master to core 3 = 1.881 microseconds
Latency time from master to core 4 = 1.907 microseconds
Latency time from master to core 5 = 1.876 microseconds
Latency time from master to core 6 = 1.896 microseconds
Latency time from master to core 7 = 1.889 microseconds
Latency time from master to core 8 = 2.418 microseconds
Latency time from master to core 9 = 2.417 microseconds
Communication speed from master to core 1 = 12783.43 MB/sec
Communication speed from master to core 2 = 13977.95 MB/sec
Communication speed from master to core 3 = 14281.63 MB/sec
Communication speed from master to core 4 = 14028.20 MB/sec
Communication speed from master to core 5 = 13763.91 MB/sec
Communication speed from master to core 6 = 13771.50 MB/sec
Communication speed from master to core 7 = 14067.67 MB/sec
Communication speed from master to core 8 = 9001.31 MB/sec
Communication speed from master to core 9 = 11021.56 MB/sec
Total CPU time for main thread : 130.1 seconds
Total CPU time summed for all threads : 132.4 seconds
Elapsed time spent obtaining a license : 0.4 seconds
Elapsed time spent pre-processing model (/PREP7) : 0.1 seconds
Elapsed time spent solution - preprocessing : 0.2 seconds
Elapsed time spent computing solution : 130.0 seconds
Elapsed time spent solution - postprocessing : 0.3 seconds
Elapsed time spent post-processing model (/POST1) : 0.0 seconds
Equation solver used : Sparse (symmetric)
Equation solver computational rate : 81.3 Gflops
Equation solver effective I/O rate : 21.1 GB/sec
Sum of memory used on all processes : 1570.0 MB
Sum of memory allocated on all processes : 11328.0 MB
Physical memory available : 32 GB
Total amount of I/O written to disk : 33.1 GB
Total amount of I/O read from disk : 37.3 GB
+------ E N D D I S T R I B U T E D A N S Y S S T A T I S T I C S -------+
*---------------------------------------------------------------------------*
| |
| DISTRIBUTED ANSYS RUN COMPLETED |
| |
|---------------------------------------------------------------------------|
| |
| Ansys 2022 R1 Build 22.1 UP20211129 WINDOWS x64 |
| |
|---------------------------------------------------------------------------|
| |
| Database Requested(-db) 1024 MB Scratch Memory Requested 1024 MB |
| Maximum Database Used 17 MB Maximum Scratch Memory Used 174 MB |
| |
|---------------------------------------------------------------------------|
| |
| CP Time (sec) = 132.422 Time = 14:10:59 |
| Elapsed Time (sec) = 133.000 Date = 09/05/2024 |
| |
*---------------------------------------------------------------------------* -
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