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January 18, 2023 at 6:45 pm
sagar.gupta.satrasala
SubscriberHi,
I am performing a nonlinear buckling analysis on a bamboo model. During the simulation, I am getting this error - "The solver engine was unable to converge on a solution for the nonlinear problem." I already tried increasing the number of substeps but it didnot work. Could someone please help me resolve this error.
I am also attaching the solution information for further reference,
Thank you in advance
Solver Output
Ansys Mechanical Enterprise Academic Research
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***** ANSYS COMMAND LINE ARGUMENTS *****
BATCH MODE REQUESTED (-b) = NOLIST
INPUT FILE COPY MODE (-c) = COPY
DISTRIBUTED MEMORY PARALLEL REQUESTED
4 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS
TOTAL OF 4 CORES REQUESTED
INPUT FILE NAME = \\hybrid-srv\userdata\user4\Satrasala\Imperfection models\_ProjectScratch\ScrD1BD\dummy.dat
OUTPUT FILE NAME = Y:\user4\Satrasala\Imperfection models\_ProjectScratch\ScrD1BD\solve.out
START-UP FILE MODE = NOREAD
STOP FILE MODE = NOREADRELEASE= 2021 R2 BUILD= 21.2 UP20210601 VERSION=WINDOWS x64
CURRENT JOBNAME=file0 16:28:46 JAN 18, 2023 CP= 0.500
PARAMETER _DS_PROGRESS = 999.0000000/INPUT FILE= ds.dat LINE= 0
*** NOTE *** CP = 0.781 TIME= 16:28:47
The /CONFIG,NOELDB command is not valid in a Distributed ANSYS
solution. Command is ignored.*GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 16.4797222
TITLE=
Bow--Static Structural (D5)ACT Extensions:
LSDYNA, 2021.1
5f463412-bd3e-484b-87e7-cbc0a665e474, wbex
SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR
TYPE=STRI DIMENSIONS= 248 1 1PARAMETER _WB_PROJECTSCRATCH_DIR(1) = Y:\user4\Satrasala\Imperfection models\_ProjectScratch\ScrD1BD\
SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1PARAMETER _WB_SOLVERFILES_DIR(1) = Y:\user4\Satrasala\Imperfection models\Bow_files\dp0\SYS-2\MECH\
SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1PARAMETER _WB_USERFILES_DIR(1) = Y:\user4\Satrasala\Imperfection models\Bow_files\user_files\
--- Data in consistent NMM units. See Solving Units in the help system for moreMPA UNITS SPECIFIED FOR INTERNAL
LENGTH = MILLIMETERS (mm)
MASS = TONNE (Mg)
TIME = SECONDS (sec)
TEMPERATURE = CELSIUS (C)
TOFFSET = 273.0
FORCE = NEWTON (N)
HEAT = MILLIJOULES (mJ)INPUT UNITS ARE ALSO SET TO MPA
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2021 R2 21.2 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Research00000000 VERSION=WINDOWS x64 16:28:47 JAN 18, 2023 CP= 0.797
Bow--Static Structural (D5)
***** ANSYS ANALYSIS DEFINITION (PREP7) *****
*********** Nodes for the whole assembly ***********
*********** Elements for Body 1 "L1" ***********
*********** Elements for Body 2 "L2" ***********
*********** Elements for Body 3 "L3" ***********
*********** Elements for Body 4 "Diaphragm.1" ***********
*********** Elements for Body 5 "Diaphragm.2" ***********
*********** Elements for Body 6 "Diaphragm.3" ***********
*********** Elements for Body 7 "Diaphragm.4" ***********
*********** Elements for Body 8 "Diaphragm.5" ***********
*********** Elements for Body 9 "Diaphragm.6" ***********
*********** Elements for Body 10 "Diaphragm.7" ***********
*********** Elements for Body 11 "Diaphragm.8" ***********
*********** Elements for Body 12 "Diaphragm.9" ***********
*********** Elements for Body 13 "Diaphragm.10" ***********
*********** Elements for Body 14 "Diaphragm.11" ***********
*********** Elements for Body 15 "L1" ***********
*********** Elements for Body 16 "L2" ***********
*********** Elements for Body 17 "L3" ***********
*********** Elements for Body 18 "Ext Ridge" ***********
*********** Elements for Body 19 "L1" ***********
*********** Elements for Body 20 "L2" ***********
*********** Elements for Body 21 "L3" ***********
*********** Elements for Body 22 "Ext Ridge" ***********
*********** Elements for Body 23 "L1" ***********
*********** Elements for Body 24 "L2" ***********
*********** Elements for Body 25 "L3" ***********
*********** Elements for Body 26 "Ext Ridge" ***********
*********** Elements for Body 27 "L1" ***********
*********** Elements for Body 28 "L2" ***********
*********** Elements for Body 29 "L3" ***********
*********** Elements for Body 30 "Ext Ridge" ***********
*********** Elements for Body 31 "L1" ***********
*********** Elements for Body 32 "L2" ***********
*********** Elements for Body 33 "L3" ***********
*********** Elements for Body 34 "Ext Ridge" ***********
*********** Elements for Body 35 "L1" ***********
*********** Elements for Body 36 "L2" ***********
*********** Elements for Body 37 "L3" ***********
*********** Elements for Body 38 "Ext Ridge" ***********
*********** Elements for Body 39 "L1" ***********
*********** Elements for Body 40 "L2" ***********
*********** Elements for Body 41 "L3" ***********
*********** Elements for Body 42 "Ext Ridge" ***********
*********** Elements for Body 43 "L1" ***********
*********** Elements for Body 44 "L2" ***********
*********** Elements for Body 45 "L3" ***********
*********** Elements for Body 46 "Ext Ridge" ***********
*********** Elements for Body 47 "L1" ***********
*********** Elements for Body 48 "L2" ***********
*********** Elements for Body 49 "L3" ***********
*********** Elements for Body 50 "Ext Ridge" ***********
*********** Elements for Body 51 "L1" ***********
*********** Elements for Body 52 "L2" ***********
*********** Elements for Body 53 "L3" ***********
*********** Elements for Body 54 "Ext Ridge" ***********
*********** Elements for Body 55 "L1" ***********
*********** Elements for Body 56 "L2" ***********
*********** Elements for Body 57 "L3" ***********
*********** Elements for Body 58 "Ext Ridge" ***********
*********** Elements for Body 59 "L1" ***********
*********** Elements for Body 60 "L2" ***********
*********** Elements for Body 61 "L3" ***********
*********** Elements for Body 62 "Diaphragm.1" ***********
*********** Elements for Body 63 "Diaphragm.2" ***********
*********** Elements for Body 64 "Diaphragm.3" ***********
*********** Elements for Body 65 "Diaphragm.4" ***********
*********** Elements for Body 66 "Diaphragm.5" ***********
*********** Elements for Body 67 "Diaphragm.6" ***********
*********** Elements for Body 68 "Diaphragm.7" ***********
*********** Elements for Body 69 "Diaphragm.8" ***********
*********** Elements for Body 70 "Diaphragm.9" ***********
*********** Elements for Body 71 "Diaphragm.10" ***********
*********** Elements for Body 72 "Diaphragm.11" ***********
*********** Elements for Body 73 "L1" ***********
*********** Elements for Body 74 "L2" ***********
*********** Elements for Body 75 "L3" ***********
*********** Elements for Body 76 "Ext Ridge" ***********
*********** Elements for Body 77 "L1" ***********
*********** Elements for Body 78 "L2" ***********
*********** Elements for Body 79 "L3" ***********
*********** Elements for Body 80 "Ext Ridge" ***********
*********** Elements for Body 81 "L1" ***********
*********** Elements for Body 82 "L2" ***********
*********** Elements for Body 83 "L3" ***********
*********** Elements for Body 84 "Ext Ridge" ***********
*********** Elements for Body 85 "L1" ***********
*********** Elements for Body 86 "L2" ***********
*********** Elements for Body 87 "L3" ***********
*********** Elements for Body 88 "Ext Ridge" ***********
*********** Elements for Body 89 "L1" ***********
*********** Elements for Body 90 "L2" ***********
*********** Elements for Body 91 "L3" ***********
*********** Elements for Body 92 "Ext Ridge" ***********
*********** Elements for Body 93 "L1" ***********
*********** Elements for Body 94 "L2" ***********
*********** Elements for Body 95 "L3" ***********
*********** Elements for Body 96 "Ext Ridge" ***********
*********** Elements for Body 97 "L1" ***********
*********** Elements for Body 98 "L2" ***********
*********** Elements for Body 99 "L3" ***********
*********** Elements for Body 100 "Ext Ridge" ***********
*********** Elements for Body 101 "L1" ***********
*********** Elements for Body 102 "L2" ***********
*********** Elements for Body 103 "L3" ***********
*********** Elements for Body 104 "Ext Ridge" ***********
*********** Elements for Body 105 "L1" ***********
*********** Elements for Body 106 "L2" ***********
*********** Elements for Body 107 "L3" ***********
*********** Elements for Body 108 "Ext Ridge" ***********
*********** Elements for Body 109 "L1" ***********
*********** Elements for Body 110 "L2" ***********
*********** Elements for Body 111 "L3" ***********
*********** Elements for Body 112 "Ext Ridge" ***********
*********** Elements for Body 113 "L1" ***********
*********** Elements for Body 114 "L2" ***********
*********** Elements for Body 115 "L3" ***********
*********** Elements for Body 116 "Ext Ridge" ***********
*********** Send User Defined Coordinate System(s) ***********
*********** Set Reference Temperature ***********
*********** Send Materials ***********
*********** Create Displacement Components For Use In Future MSUP or Multistage
*********** Fixed Supports ***********
******* Constant Zero Displacement X *******
******* Constant Zero Displacement Z *******
*********** Define Force Using Surface Effect Elements ***********
***** ROUTINE COMPLETED ***** CP = 8.078
--- Number of total nodes = 548309
--- Number of contact elements = 126
--- Number of spring elements = 0
--- Number of bearing elements = 0
--- Number of solid elements = 111153
--- Number of condensed parts = 0
--- Number of total elements = 111279*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 16.4808333
****************************************************************************
************************* SOLUTION ********************************
********************************************************************************* ANSYS SOLUTION ROUTINE *****
PERFORM A STATIC ANALYSIS
THIS WILL BE A NEW ANALYSISLARGE DEFORMATION ANALYSIS
PARAMETER _THICKRATIO = 1.000000000
USE PRECONDITIONED CONJUGATE GRADIENT SOLVER
CONVERGENCE TOLERANCE = 1.00000E-08
MAXIMUM ITERATION = NumNode*DofPerNode* 1.0000CONTACT INFORMATION PRINTOUT LEVEL 1
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
****************************************************
******************* SOLVE FOR LS 1 OF 1 ****************SELECT FOR ITEM=TYPE COMPONENT=
IN RANGE 117 TO 117 STEP 1126 ELEMENTS (OF 111279 DEFINED) SELECTED BY ESEL COMMAND.
SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.
462 NODES (OF 548309 DEFINED) SELECTED FROM
126 SELECTED ELEMENTS BY NSLE COMMAND.SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 1 KVAL = 1
VALUES = 0.0000 0.0000 0.0000 0.0000SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 2 KVAL = 1
VALUES = -49.801 -49.801 -49.801 -49.801SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 3 KVAL = 1
VALUES = 0.0000 0.0000 0.0000 0.0000ALL SELECT FOR ITEM=NODE COMPONENT=
IN RANGE 1 TO 548309 STEP 1548309 NODES (OF 548309 DEFINED) SELECTED BY NSEL COMMAND.
ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 328535 STEP 1111279 ELEMENTS (OF 111279 DEFINED) SELECTED BY ESEL COMMAND.
PRINTOUT RESUMED BY /GOP
USE AUTOMATIC TIME STEPPING THIS LOAD STEP
USE 25 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM
FOR AUTOMATIC TIME STEPPING:
USE 30 SUBSTEPS AS A MAXIMUM
USE 25 SUBSTEPS AS A MINIMUMTIME= 1.0000
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
WRITE ALL ITEMS TO THE DATABASE WITH A FREQUENCY OF NONE
FOR ALL APPLICABLE ENTITIESWRITE NSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIESWRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIESWRITE EANG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIESWRITE ETMP ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIESWRITE VENG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIESWRITE STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIESWRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIESWRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIESWRITE CONT ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIESWRITE NLDA ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES*GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000
*IF ANSINTER_ ( = 0.00000 ) NE
0 ( = 0.00000 ) THEN*ENDIF
*** NOTE *** CP = 9.094 TIME= 16:28:51
The automatic domain decomposition logic has selected the MESH domain
decomposition method with 4 processes per solution.***** ANSYS SOLVE COMMAND *****
*** WARNING *** CP = 9.547 TIME= 16:28:51
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.*** NOTE *** CP = 10.594 TIME= 16:28:52
The model data was checked and warning messages were found.
Please review output or errors file ( Y:\user4\Satrasala\Imperfection
models\_ProjectScratch\ScrD1BD\file0.err ) for these warning messages.*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---ELEMENT TYPE 1 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 2 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 3 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 4 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 5 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 6 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 7 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 8 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 9 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 10 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 11 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 12 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 13 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 14 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 15 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 16 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 17 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 18 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 19 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 20 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 21 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 22 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 23 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 24 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 25 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 26 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 27 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 28 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 29 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 30 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 31 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 32 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 33 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 34 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 35 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 36 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 37 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 38 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 39 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 40 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 41 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 42 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 43 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 44 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 45 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 46 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 47 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 48 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 49 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 50 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 51 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 52 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 53 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 54 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 55 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 56 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 57 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 58 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 59 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 60 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 61 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 62 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 63 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 64 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 65 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 66 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 67 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 68 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 69 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 70 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 71 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 72 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 73 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 74 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 75 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 76 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 77 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 78 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 79 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 80 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 81 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 82 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 83 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 84 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 85 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 86 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 87 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 88 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 89 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 90 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 91 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 92 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 93 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 94 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 95 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 96 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 97 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 98 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 99 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 100 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 101 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 102 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 103 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 104 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 105 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 106 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 107 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 108 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 109 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 110 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 111 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 112 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 113 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 114 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 115 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0ELEMENT TYPE 116 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2021 R2 21.2 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Research00000000 VERSION=WINDOWS x64 16:28:53 JAN 18, 2023 CP= 10.656
Bow--Static Structural (D5)
S O L U T I O N O P T I O N S
PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
DEGREES OF FREEDOM. . . . . . UX UY UZ
ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
NONLINEAR GEOMETRIC EFFECTS . . . . . . . . . .ON
EQUATION SOLVER OPTION. . . . . . . . . . . . .PCG
TOLERANCE. . . . . . . . . . . . . . . . . . 1.00000E-08
NEWTON-RAPHSON OPTION . . . . . . . . . . . . .PROGRAM CHOSEN
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC*** NOTE *** CP = 10.703 TIME= 16:28:53
Poisson's ratio PR input has been converted to NU input.*** WARNING *** CP = 10.750 TIME= 16:28:53
Material number 117 (used by element 328410) should normally have at
least one MP or one TB type command associated with it. Output of
energy by material may not be available.*** NOTE *** CP = 10.797 TIME= 16:28:53
The step data was checked and warning messages were found.
Please review output or errors file ( Y:\user4\Satrasala\Imperfection
models\_ProjectScratch\ScrD1BD\file0.err ) for these warning messages.*** NOTE *** CP = 10.797 TIME= 16:28:53
This nonlinear analysis defaults to using the full Newton-Raphson
solution procedure. This can be modified using the NROPT command.*** NOTE *** CP = 10.797 TIME= 16:28:53
The conditions for direct assembly have been met. No .emat or .erot
files will be produced.
D I S T R I B U T E D D O M A I N D E C O M P O S E R
...Number of elements: 111279
...Number of nodes: 548309
...Decompose to 4 CPU domains
...Element load balance ratio = 1.003
L O A D S T E P O P T I O N SLOAD STEP NUMBER. . . . . . . . . . . . . . . . 1
TIME AT END OF THE LOAD STEP. . . . . . . . . . 1.0000
AUTOMATIC TIME STEPPING . . . . . . . . . . . . ON
INITIAL NUMBER OF SUBSTEPS . . . . . . . . . 25
MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . . 30
MINIMUM NUMBER OF SUBSTEPS . . . . . . . . . 25
MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS. . . . 15
STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO
STRESS-STIFFENING . . . . . . . . . . . . . . . ON
TERMINATE ANALYSIS IF NOT CONVERGED . . . . . .YES (EXIT)
CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS
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
NLDA ALL
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr
MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED
TO BE, NEQIT = 22, BY SOLUTION CONTROL LOGIC.
*** NOTE *** CP = 15.203 TIME= 16:29:17
The PCG solver has automatically set the level of difficulty for this
model to 1.Range of element maximum matrix coefficients in global coordinates
Maximum = 125628.73 at element 100773.
Minimum = 5401.92991 at element 7118.*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP1 748 SOLID186 0.188 0.000251
2 748 SOLID186 0.203 0.000272
3 748 SOLID186 0.172 0.000230
4 440 SOLID186 0.188 0.000426
5 440 SOLID186 0.078 0.000178
6 440 SOLID186 0.172 0.000391
7 440 SOLID186 0.203 0.000462
8 440 SOLID186 0.172 0.000391
9 440 SOLID186 0.109 0.000249
10 445 SOLID186 0.219 0.000492
11 440 SOLID186 0.109 0.000249
12 470 SOLID186 0.125 0.000266
13 440 SOLID186 0.094 0.000213
14 445 SOLID186 0.094 0.000211
15 1672 SOLID186 0.297 0.000178
16 1672 SOLID186 0.438 0.000262
17 1672 SOLID186 0.469 0.000280
18 330 SOLID186 0.062 0.000189
19 1672 SOLID186 0.562 0.000336
20 1672 SOLID186 0.438 0.000262
21 1672 SOLID186 0.500 0.000299
22 330 SOLID186 0.109 0.000331
23 1672 SOLID186 0.531 0.000318
24 1672 SOLID186 0.453 0.000271
25 1672 SOLID186 0.438 0.000262
26 330 SOLID186 0.141 0.000426
27 1474 SOLID186 0.391 0.000265
28 1474 SOLID186 0.328 0.000223
29 1474 SOLID186 0.422 0.000286
30 330 SOLID186 0.078 0.000237
31 1408 SOLID186 0.359 0.000255
32 1408 SOLID186 0.328 0.000233
33 1408 SOLID186 0.391 0.000277
34 330 SOLID186 0.094 0.000284
35 1628 SOLID186 0.609 0.000374
36 1628 SOLID186 0.484 0.000298
37 1628 SOLID186 0.766 0.000470
38 330 SOLID186 0.172 0.000521
39 1496 SOLID186 0.500 0.000334
40 1496 SOLID186 0.375 0.000251
41 1496 SOLID186 0.406 0.000272
42 330 SOLID186 0.062 0.000189
43 1408 SOLID186 0.500 0.000355
44 1408 SOLID186 0.453 0.000322
45 1408 SOLID186 0.328 0.000233
46 330 SOLID186 0.094 0.000284
47 1408 SOLID186 0.438 0.000311
48 1408 SOLID186 0.359 0.000255
49 1408 SOLID186 0.328 0.000233
50 330 SOLID186 0.141 0.000426
51 1496 SOLID186 0.484 0.000324
52 1496 SOLID186 0.547 0.000366
53 1496 SOLID186 0.328 0.000219
54 330 SOLID186 0.047 0.000142
55 484 SOLID186 0.109 0.000226
56 484 SOLID186 0.047 0.000097
57 484 SOLID186 0.125 0.000258
58 330 SOLID186 0.094 0.000284
59 680 SOLID186 0.094 0.000138
60 680 SOLID186 0.250 0.000368
61 680 SOLID186 0.188 0.000276
62 400 SOLID186 0.047 0.000117
63 400 SOLID186 0.109 0.000273
64 400 SOLID186 0.078 0.000195
65 400 SOLID186 0.109 0.000273
66 400 SOLID186 0.172 0.000430
67 410 SOLID186 0.094 0.000229
68 400 SOLID186 0.062 0.000156
69 410 SOLID186 0.172 0.000419
70 445 SOLID186 0.141 0.000316
71 400 SOLID186 0.109 0.000273
72 400 SOLID186 0.109 0.000273
73 1520 SOLID186 0.469 0.000308
74 1520 SOLID186 0.375 0.000247
75 1520 SOLID186 0.578 0.000380
76 300 SOLID186 0.109 0.000365
77 1520 SOLID186 0.406 0.000267
78 1520 SOLID186 0.484 0.000319
79 1520 SOLID186 0.453 0.000298
80 300 SOLID186 0.062 0.000208
81 1520 SOLID186 0.531 0.000350
82 1520 SOLID186 0.438 0.000288
83 1520 SOLID186 0.422 0.000278
84 300 SOLID186 0.078 0.000260
85 1340 SOLID186 0.375 0.000280
86 1340 SOLID186 0.391 0.000292
87 1340 SOLID186 0.422 0.000315
88 300 SOLID186 0.125 0.000417
89 1280 SOLID186 0.422 0.000330
90 1280 SOLID186 0.375 0.000293
91 1280 SOLID186 0.297 0.000232
92 300 SOLID186 0.156 0.000521
93 1480 SOLID186 0.406 0.000274
94 1480 SOLID186 0.609 0.000412
95 1480 SOLID186 0.516 0.000348
96 300 SOLID186 0.141 0.000469
97 1360 SOLID186 0.500 0.000368
98 1360 SOLID186 0.484 0.000356
99 1360 SOLID186 0.375 0.000276
100 300 SOLID186 0.125 0.000417
101 1280 SOLID186 0.297 0.000232
102 1280 SOLID186 0.438 0.000342
103 1280 SOLID186 0.438 0.000342
104 300 SOLID186 0.125 0.000417
105 1280 SOLID186 0.516 0.000403
106 1280 SOLID186 0.375 0.000293
107 1280 SOLID186 0.375 0.000293
108 300 SOLID186 0.094 0.000313
109 1360 SOLID186 0.375 0.000276
110 1360 SOLID186 0.328 0.000241
111 1360 SOLID186 0.484 0.000356
112 300 SOLID186 0.078 0.000260
113 440 SOLID186 0.062 0.000142
114 440 SOLID186 0.109 0.000249
115 440 SOLID186 0.234 0.000533
116 300 SOLID186 0.094 0.000313
117 126 SURF154 0.000 0.000000
Time at end of element matrix formulation CP = 37.78125.ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.rdb
FOR POSSIBLE RESUME FROM THIS POINT
FORCE CONVERGENCE VALUE = 187.9 CRITERION= 0.9585*** NOTE *** CP = 42.625 TIME= 16:30:11
The initial memory allocation (-m) has been exceeded.
Supplemental memory allocations are being used.
Iteration= 75 Ratio= 0.308243 Limit= 1.000000E-08 Wall= 6.9
Iteration= 370 Ratio= 9.144846E-04 Limit= 1.000000E-08 Wall= 40.1
Iteration= 710 Ratio= 3.151432E-06 Limit= 1.000000E-08 Wall= 75.9DISTRIBUTED PCG SOLVER SOLUTION CONVERGED
DISTRIBUTED PCG SOLVER SOLUTION STATISTICS
NUMBER OF ITERATIONS= 1030
NUMBER OF EQUATIONS = 1644927
LEVEL OF CONVERGENCE= 1
CALCULATED NORM = 0.98534E-08
SPECIFIED TOLERANCE = 0.10000E-07
TOTAL CPU TIME (sec)= 100.53
TOTAL WALL TIME(sec)= 115.70
TOTAL MEMORY (GB) = 1.18DISP CONVERGENCE VALUE = 1.357 CRITERION= 0.6922E-01
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 1.357
FORCE CONVERGENCE VALUE = 80.73 CRITERION= 2.243
DISP CONVERGENCE VALUE = 0.4551E-01 CRITERION= 0.7300E-01 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4551E-01
FORCE CONVERGENCE VALUE = 0.8080E-01 CRITERION= 2.319 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP1 748 SOLID186 0.078 0.000104
2 748 SOLID186 0.156 0.000209
3 748 SOLID186 0.047 0.000063
4 440 SOLID186 0.109 0.000249
5 440 SOLID186 0.078 0.000178
6 440 SOLID186 0.062 0.000142
7 440 SOLID186 0.062 0.000142
8 440 SOLID186 0.031 0.000071
9 440 SOLID186 0.094 0.000213
10 445 SOLID186 0.047 0.000105
11 440 SOLID186 0.016 0.000036
12 470 SOLID186 0.062 0.000133
13 440 SOLID186 0.094 0.000213
14 445 SOLID186 0.062 0.000140
15 1672 SOLID186 0.312 0.000187
16 1672 SOLID186 0.234 0.000140
17 1672 SOLID186 0.266 0.000159
18 330 SOLID186 0.062 0.000189
19 1672 SOLID186 0.281 0.000168
20 1672 SOLID186 0.250 0.000150
21 1672 SOLID186 0.266 0.000159
22 330 SOLID186 0.047 0.000142
23 1672 SOLID186 0.250 0.000150
24 1672 SOLID186 0.172 0.000103
25 1672 SOLID186 0.234 0.000140
26 330 SOLID186 0.062 0.000189
27 1474 SOLID186 0.156 0.000106
28 1474 SOLID186 0.141 0.000095
29 1474 SOLID186 0.250 0.000170
30 330 SOLID186 0.062 0.000189
31 1408 SOLID186 0.172 0.000122
32 1408 SOLID186 0.281 0.000200
33 1408 SOLID186 0.312 0.000222
34 330 SOLID186 0.062 0.000189
35 1628 SOLID186 0.453 0.000278
36 1628 SOLID186 0.422 0.000259
37 1628 SOLID186 0.375 0.000230
38 330 SOLID186 0.078 0.000237
39 1496 SOLID186 0.250 0.000167
40 1496 SOLID186 0.188 0.000125
41 1496 SOLID186 0.219 0.000146
42 330 SOLID186 0.062 0.000189
43 1408 SOLID186 0.234 0.000166
44 1408 SOLID186 0.359 0.000255
45 1408 SOLID186 0.219 0.000155
46 330 SOLID186 0.016 0.000047
47 1408 SOLID186 0.219 0.000155
48 1408 SOLID186 0.203 0.000144
49 1408 SOLID186 0.172 0.000122
50 330 SOLID186 0.016 0.000047
51 1496 SOLID186 0.172 0.000115
52 1496 SOLID186 0.203 0.000136
53 1496 SOLID186 0.125 0.000084
54 330 SOLID186 0.031 0.000095
55 484 SOLID186 0.109 0.000226
56 484 SOLID186 0.078 0.000161
57 484 SOLID186 0.094 0.000194
58 330 SOLID186 0.031 0.000095
59 680 SOLID186 0.094 0.000138
60 680 SOLID186 0.156 0.000230
61 680 SOLID186 0.094 0.000138
62 400 SOLID186 0.000 0.000000
63 400 SOLID186 0.047 0.000117
64 400 SOLID186 0.062 0.000156
65 400 SOLID186 0.078 0.000195
66 400 SOLID186 0.062 0.000156
67 410 SOLID186 0.016 0.000038
68 400 SOLID186 0.109 0.000273
69 410 SOLID186 0.094 0.000229
70 445 SOLID186 0.109 0.000246
71 400 SOLID186 0.047 0.000117
72 400 SOLID186 0.047 0.000117
73 1520 SOLID186 0.188 0.000123
74 1520 SOLID186 0.234 0.000154
75 1520 SOLID186 0.172 0.000113
76 300 SOLID186 0.062 0.000208
77 1520 SOLID186 0.188 0.000123
78 1520 SOLID186 0.297 0.000195
79 1520 SOLID186 0.188 0.000123
80 300 SOLID186 0.016 0.000052
81 1520 SOLID186 0.203 0.000134
82 1520 SOLID186 0.188 0.000123
83 1520 SOLID186 0.125 0.000082
84 300 SOLID186 0.016 0.000052
85 1340 SOLID186 0.281 0.000210
86 1340 SOLID186 0.203 0.000152
87 1340 SOLID186 0.188 0.000140
88 300 SOLID186 0.031 0.000104
89 1280 SOLID186 0.203 0.000159
90 1280 SOLID186 0.156 0.000122
91 1280 SOLID186 0.219 0.000171
92 300 SOLID186 0.016 0.000052
93 1480 SOLID186 0.328 0.000222
94 1480 SOLID186 0.250 0.000169
95 1480 SOLID186 0.203 0.000137
96 300 SOLID186 0.031 0.000104
97 1360 SOLID186 0.359 0.000264
98 1360 SOLID186 0.219 0.000161
99 1360 SOLID186 0.188 0.000138
100 300 SOLID186 0.094 0.000313
101 1280 SOLID186 0.203 0.000159
102 1280 SOLID186 0.328 0.000256
103 1280 SOLID186 0.172 0.000134
104 300 SOLID186 0.062 0.000208
105 1280 SOLID186 0.156 0.000122
106 1280 SOLID186 0.141 0.000110
107 1280 SOLID186 0.250 0.000195
108 300 SOLID186 0.062 0.000208
109 1360 SOLID186 0.250 0.000184
110 1360 SOLID186 0.141 0.000103
111 1360 SOLID186 0.219 0.000161
112 300 SOLID186 0.062 0.000208
113 440 SOLID186 0.109 0.000249
114 440 SOLID186 0.031 0.000071
115 440 SOLID186 0.078 0.000178
116 300 SOLID186 0.109 0.000365
117 126 SURF154 0.000 0.000000*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP1 748 SOLID186 0.016 0.000021
2 748 SOLID186 0.031 0.000042
3 748 SOLID186 0.016 0.000021
4 440 SOLID186 0.000 0.000000
5 440 SOLID186 0.016 0.000036
6 440 SOLID186 0.016 0.000036
7 440 SOLID186 0.000 0.000000
8 440 SOLID186 0.000 0.000000
9 440 SOLID186 0.000 0.000000
10 445 SOLID186 0.016 0.000035
11 440 SOLID186 0.000 0.000000
12 470 SOLID186 0.000 0.000000
13 440 SOLID186 0.000 0.000000
14 445 SOLID186 0.000 0.000000
15 1672 SOLID186 0.016 0.000009
16 1672 SOLID186 0.016 0.000009
17 1672 SOLID186 0.016 0.000009
18 330 SOLID186 0.000 0.000000
19 1672 SOLID186 0.031 0.000019
20 1672 SOLID186 0.000 0.000000
21 1672 SOLID186 0.016 0.000009
22 330 SOLID186 0.000 0.000000
23 1672 SOLID186 0.016 0.000009
24 1672 SOLID186 0.016 0.000009
25 1672 SOLID186 0.000 0.000000
26 330 SOLID186 0.000 0.000000
27 1474 SOLID186 0.016 0.000011
28 1474 SOLID186 0.000 0.000000
29 1474 SOLID186 0.016 0.000011
30 330 SOLID186 0.000 0.000000
31 1408 SOLID186 0.031 0.000022
32 1408 SOLID186 0.000 0.000000
33 1408 SOLID186 0.031 0.000022
34 330 SOLID186 0.016 0.000047
35 1628 SOLID186 0.062 0.000038
36 1628 SOLID186 0.016 0.000010
37 1628 SOLID186 0.062 0.000038
38 330 SOLID186 0.000 0.000000
39 1496 SOLID186 0.062 0.000042
40 1496 SOLID186 0.047 0.000031
41 1496 SOLID186 0.016 0.000010
42 330 SOLID186 0.000 0.000000
43 1408 SOLID186 0.016 0.000011
44 1408 SOLID186 0.031 0.000022
45 1408 SOLID186 0.031 0.000022
46 330 SOLID186 0.031 0.000095
47 1408 SOLID186 0.047 0.000033
48 1408 SOLID186 0.000 0.000000
49 1408 SOLID186 0.016 0.000011
50 330 SOLID186 0.016 0.000047
51 1496 SOLID186 0.000 0.000000
52 1496 SOLID186 0.031 0.000021
53 1496 SOLID186 0.016 0.000010
54 330 SOLID186 0.000 0.000000
55 484 SOLID186 0.000 0.000000
56 484 SOLID186 0.000 0.000000
57 484 SOLID186 0.016 0.000032
58 330 SOLID186 0.000 0.000000
59 680 SOLID186 0.000 0.000000
60 680 SOLID186 0.016 0.000023
61 680 SOLID186 0.000 0.000000
62 400 SOLID186 0.000 0.000000
63 400 SOLID186 0.000 0.000000
64 400 SOLID186 0.000 0.000000
65 400 SOLID186 0.000 0.000000
66 400 SOLID186 0.031 0.000078
67 410 SOLID186 0.016 0.000038
68 400 SOLID186 0.031 0.000078
69 410 SOLID186 0.016 0.000038
70 445 SOLID186 0.016 0.000035
71 400 SOLID186 0.000 0.000000
72 400 SOLID186 0.016 0.000039
73 1520 SOLID186 0.000 0.000000
74 1520 SOLID186 0.031 0.000021
75 1520 SOLID186 0.047 0.000031
76 300 SOLID186 0.000 0.000000
77 1520 SOLID186 0.031 0.000021
78 1520 SOLID186 0.047 0.000031
79 1520 SOLID186 0.016 0.000010
80 300 SOLID186 0.000 0.000000
81 1520 SOLID186 0.062 0.000041
82 1520 SOLID186 0.031 0.000021
83 1520 SOLID186 0.016 0.000010
84 300 SOLID186 0.000 0.000000
85 1340 SOLID186 0.031 0.000023
86 1340 SOLID186 0.016 0.000012
87 1340 SOLID186 0.000 0.000000
88 300 SOLID186 0.000 0.000000
89 1280 SOLID186 0.062 0.000049
90 1280 SOLID186 0.031 0.000024
91 1280 SOLID186 0.000 0.000000
92 300 SOLID186 0.000 0.000000
93 1480 SOLID186 0.031 0.000021
94 1480 SOLID186 0.047 0.000032
95 1480 SOLID186 0.000 0.000000
96 300 SOLID186 0.000 0.000000
97 1360 SOLID186 0.016 0.000011
98 1360 SOLID186 0.031 0.000023
99 1360 SOLID186 0.016 0.000011
100 300 SOLID186 0.000 0.000000
101 1280 SOLID186 0.031 0.000024
102 1280 SOLID186 0.062 0.000049
103 1280 SOLID186 0.016 0.000012
104 300 SOLID186 0.000 0.000000
105 1280 SOLID186 0.000 0.000000
106 1280 SOLID186 0.000 0.000000
107 1280 SOLID186 0.031 0.000024
108 300 SOLID186 0.000 0.000000
109 1360 SOLID186 0.016 0.000011
110 1360 SOLID186 0.031 0.000023
111 1360 SOLID186 0.031 0.000023
112 300 SOLID186 0.016 0.000052
113 440 SOLID186 0.000 0.000000
114 440 SOLID186 0.000 0.000000
115 440 SOLID186 0.016 0.000036
116 300 SOLID186 0.000 0.000000
117 126 SURF154 0.000 0.000000
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 2
*** TIME = 0.400000E-01 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 172.0 CRITERION= 4.455
DISP CONVERGENCE VALUE = 0.9736E-01 CRITERION= 0.7649E-01
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.9736E-01
FORCE CONVERGENCE VALUE = 0.3701 CRITERION= 4.609 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.3291E-03 CRITERION= 0.7807E-01 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.3291E-03
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 2 COMPLETED. CUM ITER = 4
*** TIME = 0.800000E-01 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 195.0 CRITERION= 6.809
DISP CONVERGENCE VALUE = 0.1077 CRITERION= 0.8199E-01
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1077
FORCE CONVERGENCE VALUE = 0.4527 CRITERION= 7.018 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.4349E-03 CRITERION= 0.8368E-01 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.4349E-03
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 3 COMPLETED. CUM ITER = 6
*** TIME = 0.120000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 222.6 CRITERION= 9.241
DISP CONVERGENCE VALUE = 0.1198 CRITERION= 0.8811E-01
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1198
FORCE CONVERGENCE VALUE = 0.5609 CRITERION= 9.509 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.5815E-03 CRITERION= 0.8994E-01 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.5815E-03
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 4 COMPLETED. CUM ITER = 8
*** TIME = 0.160000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 255.5 CRITERION= 11.76
DISP CONVERGENCE VALUE = 0.1337 CRITERION= 0.9494E-01
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1337
FORCE CONVERGENCE VALUE = 0.6992 CRITERION= 12.09 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.7834E-03 CRITERION= 0.9692E-01 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.7834E-03
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 5 COMPLETED. CUM ITER = 10
*** TIME = 0.200000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 294.8 CRITERION= 14.38
DISP CONVERGENCE VALUE = 0.1499 CRITERION= 0.1026
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1499
FORCE CONVERGENCE VALUE = 0.8787 CRITERION= 14.78 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.1065E-02 CRITERION= 0.1048 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.1065E-02
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 6 COMPLETED. CUM ITER = 12
*** TIME = 0.240000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 342.4 CRITERION= 17.12
DISP CONVERGENCE VALUE = 0.1688 CRITERION= 0.1113
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1688
FORCE CONVERGENCE VALUE = 1.114 CRITERION= 17.58 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.1464E-02 CRITERION= 0.1136 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.1464E-02
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 7 COMPLETED. CUM ITER = 14
*** TIME = 0.280000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 400.2 CRITERION= 19.98
DISP CONVERGENCE VALUE = 0.1909 CRITERION= 0.1211
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1909
FORCE CONVERGENCE VALUE = 1.425 CRITERION= 20.51 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.2035E-02 CRITERION= 0.1237 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.2035E-02
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 8 COMPLETED. CUM ITER = 16
*** TIME = 0.320000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 471.3 CRITERION= 22.99
DISP CONVERGENCE VALUE = 0.2170 CRITERION= 0.1323
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2170
FORCE CONVERGENCE VALUE = 1.841 CRITERION= 23.61 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.2865E-02 CRITERION= 0.1351 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.2865E-02
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 9 COMPLETED. CUM ITER = 18
*** TIME = 0.360000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 559.4 CRITERION= 26.17
DISP CONVERGENCE VALUE = 0.2480 CRITERION= 0.1450
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2480
FORCE CONVERGENCE VALUE = 2.403 CRITERION= 26.87 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.4091E-02 CRITERION= 0.1482 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.4091E-02
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 10 COMPLETED. CUM ITER = 20
*** TIME = 0.400000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 669.8 CRITERION= 29.55
DISP CONVERGENCE VALUE = 0.2850 CRITERION= 0.1598
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2850
FORCE CONVERGENCE VALUE = 3.172 CRITERION= 30.35 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.5935E-02 CRITERION= 0.1634 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.5935E-02
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 11 COMPLETED. CUM ITER = 22
*** TIME = 0.440000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 809.5 CRITERION= 33.17
DISP CONVERGENCE VALUE = 0.3296 CRITERION= 0.1769
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.3296
FORCE CONVERGENCE VALUE = 4.236 CRITERION= 34.07 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.8758E-02 CRITERION= 0.1810 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.8758E-02
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 12 COMPLETED. CUM ITER = 24
*** TIME = 0.480000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 988.5 CRITERION= 37.05
DISP CONVERGENCE VALUE = 0.3835 CRITERION= 0.1969
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.3835
FORCE CONVERGENCE VALUE = 5.729 CRITERION= 38.07 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.1317E-01 CRITERION= 0.2016 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.1317E-01
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 13 COMPLETED. CUM ITER = 26
*** TIME = 0.520000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 1221. CRITERION= 41.26
DISP CONVERGENCE VALUE = 0.4492 CRITERION= 0.2205
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4492
FORCE CONVERGENCE VALUE = 7.845 CRITERION= 42.42 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.2022E-01 CRITERION= 0.2261 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.2022E-01
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 14 COMPLETED. CUM ITER = 28
*** TIME = 0.560000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 1528. CRITERION= 45.86
DISP CONVERGENCE VALUE = 0.5297 CRITERION= 0.2486
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.5297
FORCE CONVERGENCE VALUE = 10.88 CRITERION= 47.17 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.3176E-01 CRITERION= 0.2553 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.3176E-01
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 15 COMPLETED. CUM ITER = 30
*** TIME = 0.600000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 1941. CRITERION= 50.94
DISP CONVERGENCE VALUE = 0.6285 CRITERION= 0.2823
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.6285
FORCE CONVERGENCE VALUE = 15.27 CRITERION= 52.42 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.5113E-01 CRITERION= 0.2907 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.5113E-01
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 16 COMPLETED. CUM ITER = 32
*** TIME = 0.640000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 2506. CRITERION= 56.59
DISP CONVERGENCE VALUE = 0.7499 CRITERION= 0.3231
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7499
FORCE CONVERGENCE VALUE = 21.66 CRITERION= 58.27 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.8455E-01 CRITERION= 0.3341 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.8455E-01
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 17 COMPLETED. CUM ITER = 34
*** TIME = 0.680000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 3297. CRITERION= 62.98
DISP CONVERGENCE VALUE = 0.8984 CRITERION= 0.3733
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.8984
FORCE CONVERGENCE VALUE = 30.91 CRITERION= 64.89 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.1439 CRITERION= 0.3884 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.1439
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 18 COMPLETED. CUM ITER = 36
*** TIME = 0.720000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 4438. CRITERION= 70.28
DISP CONVERGENCE VALUE = 1.078 CRITERION= 0.4356
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 1.078
FORCE CONVERGENCE VALUE = 44.12 CRITERION= 72.46 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.2526 CRITERION= 0.4576 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.2526
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 19 COMPLETED. CUM ITER = 38
*** TIME = 0.760000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 6138. CRITERION= 78.77
DISP CONVERGENCE VALUE = 1.288 CRITERION= 0.5142
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 1.288
FORCE CONVERGENCE VALUE = 62.32 CRITERION= 81.27 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.4585 CRITERION= 0.5485 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.4585
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 20 COMPLETED. CUM ITER = 40
*** TIME = 0.800000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 8787. CRITERION= 88.86
DISP CONVERGENCE VALUE = 1.524 CRITERION= 0.6153
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 1.524
FORCE CONVERGENCE VALUE = 86.04 CRITERION= 91.71 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.8647 CRITERION= 0.6729
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.8647
FORCE CONVERGENCE VALUE = 30.73 CRITERION= 94.21 <<< CONVERGED
DISP CONVERGENCE VALUE = 0.6798E-02 CRITERION= 0.6870 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = 0.6798E-02
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 1 SUBSTEP 21 COMPLETED. CUM ITER = 43
*** TIME = 0.840000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 0.1313E+05 CRITERION= 101.2
DISP CONVERGENCE VALUE = 1.778 CRITERION= 0.7505
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 1.778
FORCE CONVERGENCE VALUE = 116.1 CRITERION= 104.4
DISP CONVERGENCE VALUE = 1.717 CRITERION= 0.8551
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 1.717
FORCE CONVERGENCE VALUE = 118.9 CRITERION= 107.8
DISP CONVERGENCE VALUE = 0.2184E-01 CRITERION= 0.8737 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2184E-01
FORCE CONVERGENCE VALUE = 0.7753E-01 CRITERION= 110.0 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 1 SUBSTEP 22 COMPLETED. CUM ITER = 46
*** TIME = 0.880000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 0.2108E+05 CRITERION= 116.8
DISP CONVERGENCE VALUE = 2.106 CRITERION= 0.9466
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 2.106
FORCE CONVERGENCE VALUE = 194.2 CRITERION= 120.3
DISP CONVERGENCE VALUE = 3.934 CRITERION= 1.171
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 3.934
FORCE CONVERGENCE VALUE = 602.8 CRITERION= 125.6
DISP CONVERGENCE VALUE = 0.1266 CRITERION= 1.201 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1266
FORCE CONVERGENCE VALUE = 1.180 CRITERION= 128.2 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 3
*** LOAD STEP 1 SUBSTEP 23 COMPLETED. CUM ITER = 49
*** TIME = 0.920000 TIME INC = 0.400000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.40000E-01 UNCHANGEDFORCE CONVERGENCE VALUE = 0.3912E+05 CRITERION= 138.2
DISP CONVERGENCE VALUE = 3.433 CRITERION= 1.329
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 3.433
FORCE CONVERGENCE VALUE = 2476. CRITERION= 142.0
DISP CONVERGENCE VALUE = 36.10 CRITERION= 3.235
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 36.10
FORCE CONVERGENCE VALUE = 0.1171E+06 CRITERION= 164.9
DISP CONVERGENCE VALUE = 7.700 CRITERION= 3.707
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 7.700
FORCE CONVERGENCE VALUE = 0.1142E+05 CRITERION= 169.9*** NOTE *** CP = 6486.781 TIME= 18:36:32
The preconditioned conjugate gradient solver failed to converge, and
therefore no solution was obtained. The equation solver is now being
automatically switched to the sparse solver (EQSLV,SPARSE) to allow
this analysis to continue.
DISP CONVERGENCE VALUE = 40.27 CRITERION= 3.783
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -40.27
FORCE CONVERGENCE VALUE = 0.2318E+06 CRITERION= 155.9
>>> SOLUTION PATTERNS SHOW DIVERGENCE AT ITERATION = 5
*** LOAD STEP 1 SUBSTEP 24 NOT COMPLETED. CUM ITER = 54
*** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 0.33333E-01FORCE CONVERGENCE VALUE = 156.6 CRITERION= 120.8
DISP CONVERGENCE VALUE = 23.26 CRITERION= 1.187
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 23.26
FORCE CONVERGENCE VALUE = 0.2037E+05 CRITERION= 140.8
DISP CONVERGENCE VALUE = 3.283 CRITERION= 1.382
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 3.283
FORCE CONVERGENCE VALUE = 2495. CRITERION= 144.7
DISP CONVERGENCE VALUE = 35.97 CRITERION= 3.321
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 35.97
FORCE CONVERGENCE VALUE = 0.1723E+06 CRITERION= 166.4
DISP CONVERGENCE VALUE = 9.410 CRITERION= 3.879
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 9.410
FORCE CONVERGENCE VALUE = 0.1818E+05 CRITERION= 172.5
DISP CONVERGENCE VALUE = 9.915 CRITERION= 3.959
EQUIL ITER 5 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -9.915
FORCE CONVERGENCE VALUE = 0.1258E+06 CRITERION= 173.5
DISP CONVERGENCE VALUE = 82.26 CRITERION= 7.848
EQUIL ITER 6 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 82.26
FORCE CONVERGENCE VALUE = 0.4036E+06 CRITERION= 225.5
DISP CONVERGENCE VALUE = 82.12 CRITERION= 12.40
EQUIL ITER 7 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 82.12*** ERROR *** CP = 7036.000 TIME= 18:47:02
Element 24130 (type = 27, SOLID186) (and maybe other elements) has
become highly distorted. Excessive distortion of elements is usually
a symptom indicating the need for corrective action elsewhere. Try
incrementing the load more slowly (increase the number of substeps or
decrease the time step size). You may need to improve your mesh to
obtain elements with better aspect ratios. Also consider the behavior
of materials, contact pairs, and/or constraint equations. Please rule
out other root causes of this failure before attempting rezoning or
nonlinear adaptive solutions. If this message appears in the first
iteration of first substep, be sure to perform element shape checking.*** WARNING *** CP = 7036.047 TIME= 18:47:02
The unconverged solution (identified as time 1 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 NREASON FOR TERMINATION. . . . . . . . . .ERROR IN ELEMENT FORMULATION
FILES NEEDED FOR RESTARTING . . . . . . . file0.Rnnn
file.ldhi
file.rdb
TIME OF LAST SOLUTION . . . . . . . . . . 0.92000
TIME AT START OF THE LOAD STEP . . . . 0.0000
TIME AT END OF THE LOAD STEP . . . . . 1.0000ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.db
FOR POSSIBLE RESUME FROM THIS POINTNUMBER OF WARNING MESSAGES ENCOUNTERED= 3
NUMBER OF ERROR MESSAGES ENCOUNTERED= 1***** PROBLEM TERMINATED BY INDICATED ERROR(S) OR BY END OF INPUT DATA *****
*** NOTE *** CP = 7060.422 TIME= 18:47:51
The solution for the current simulation was performed using 4 cores.
The parallel performance of this simulation on this hardware indicates
that this simulation would benefit from using additional CPU cores.
Consider using more CPU cores, which may require additional HPC
licenses, when running this simulation again on the same hardware.+--------- 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: 2021 R2 Build: 21.2 Update: UP20210601 Platform: WINDOWS x64
Date Run: 01/18/2023 Time: 18:47 Process ID: 32752
Operating System: Windows 10 (Build: 19044)Processor Model: Intel Xeon Processor (Skylake, IBRS)
Compiler: Intel(R) FORTRAN Compiler Version 19.0.0 (Build: 20190206)
Intel(R) C/C++ Compiler Version 19.0.0 (Build: 20190206)
Intel(R) Math Kernel Library Version 2020.0.0 Product Build 20191125
BLAS Library supplied by Intel(R) MKLNumber of machines requested : 1
Total number of cores available : 8
Number of physical cores available : 4
Number of processes requested : 4
Number of threads per process requested : 1
Total number of cores requested : 4 (Distributed Memory Parallel)
MPI Type: INTELMPI
MPI Version: Intel(R) MPI Library 2019 Update 9 for Windows* OS
GPU Acceleration: Not RequestedJob Name: file0
Input File: \\hybrid-srv\userdata\user4\Satrasala\Imperfection models\_ProjectScratch\ScrD1BD\dummy.datCore Machine Name Working Directory
-----------------------------------------------------
0 Hybrid-VM2 Y:\user4\Satrasala\Imperfection models\_ProjectScratch\ScrD1BD
1 Hybrid-VM2 Y:\user4\Satrasala\Imperfection models\_ProjectScratch\ScrD1BD
2 Hybrid-VM2 Y:\user4\Satrasala\Imperfection models\_ProjectScratch\ScrD1BD
3 Hybrid-VM2 Y:\user4\Satrasala\Imperfection models\_ProjectScratch\ScrD1BD
Latency time from master to core 1 = 6.485 microseconds
Latency time from master to core 2 = 7.718 microseconds
Latency time from master to core 3 = 9.069 microseconds
Communication speed from master to core 1 = 1430.70 MB/sec
Communication speed from master to core 2 = 2197.02 MB/sec
Communication speed from master to core 3 = 2638.93 MB/secTotal CPU time for main thread : 7052.5 seconds
Total CPU time summed for all threads : 7060.4 secondsElapsed time spent obtaining a license : 0.5 seconds
Elapsed time spent pre-processing model (/PREP7) : 3.5 seconds
Elapsed time spent solution - preprocessing : 3.6 seconds
Elapsed time spent computing solution : 8287.6 seconds
Elapsed time spent solution - postprocessing : 40.1 seconds
Elapsed time spent post-processing model (/POST1) : 0.0 seconds
Equation solver used : Sparse (symmetric)
Equation solver computational rate : 79.3 Gflops
Equation solver effective I/O rate : 9.9 GB/secMaximum total memory used : 19778.0 MB
Maximum total memory allocated : 26679.0 MB
Total physical memory available : 64 GBTotal amount of I/O written to disk : 76.2 GB
Total amount of I/O read from disk : 86.0 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 2021 R2 Build 21.2 UP20210601 WINDOWS x64 |
| |
|---------------------------------------------------------------------------|
| |
| Database Requested(-db) 1024 MB Scratch Memory Requested 1024 MB |
| Maximum Database Used 249 MB Maximum Scratch Memory Used 4646 MB |
| |
|---------------------------------------------------------------------------|
| |
| CP Time (sec) = 7060.422 Time = 18:47:51 |
| Elapsed Time (sec) = 8348.000 Date = 01/18/2023 |
| |
*---------------------------------------------------------------------------*All
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January 19, 2023 at 1:22 pm
Manish Dubey
Ansys EmployeeHi,
I suppose you are trying to perform postbuckling analysis (nonlinear). Does the solution converges if you try linear buckling? Is the material linear or nonlinear? How the contacts are defined? Identify the region by asking for newton raphson residual (say, 3) under solution information details and check where the residuals are high. This may give some insight. Also check whether linear buckling analysis converges or not.
Thanks
Manish
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January 19, 2023 at 4:09 pm
Sai Deogekar
Ansys EmployeeHello,
Looks like you are getting an excessive element distortion error. You might find the following video helpful: How to Handle Element Distortion Errors in Hyperelastic Materials — Lesson 3 - ANSYS Innovation Courses
The video is more focused on hyperelastic materials rather than a buckling problem. But you might find some helpful diagnosis tools and tips in the video.
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January 20, 2023 at 6:46 pmSubscriber
Hey Sai,
Thank you for your video suggestion. That worked!!
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- The topic ‘The solver engine was unable to converge on a solution for the nonlinear problem’ is closed to new replies.
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