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December 14, 2022 at 9:19 pm
luandersoncosta
SubscriberHi guys, Im trying to simulate a sphere impact in a Nitinol plate, but Im facing some errors. anyone here can Help me?
Ansys Mechanical Enterprise Academic Student
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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
2 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS
TOTAL OF 2 CORES REQUESTED
INPUT FILE NAME = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScratch\Scr86C5\dummy.dat
OUTPUT FILE NAME = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScratch\Scr86C5\solve.out
START-UP FILE MODE = NOREAD
STOP FILE MODE = NOREAD
RELEASE= 2022 R1 BUILD= 22.1 UP20211129 VERSION=WINDOWS x64
CURRENT JOBNAME=file0 18:01:27 DEC 14, 2022 CP= 0.062
PARAMETER _DS_PROGRESS = 999.0000000
/INPUT FILE= ds.dat LINE= 0
*** NOTE *** CP = 0.141 TIME= 18:01:27
The /CONFIG,NOELDB command is not valid in a Distributed ANSYS
solution. Command is ignored.
*GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 18.0241667
TITLE=
wbnew--Static Structural (B5)
ACT Extensions:
LSDYNA, 2021.1
5f463412-bd3e-484b-87e7-cbc0a665e474, wbex
SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScratch\Scr86C5\
SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\wbnew_files\dp0\SYS\MECH\
SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_USERFILES_DIR(1) = C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\wbnew_files\user_files\
--- Data in consistent NMM units. See Solving Units in the help system for more
MPA UNITS SPECIFIED FOR INTERNAL
LENGTH = MILLIMETERS (mm)
MASS = TONNE (Mg)
TIME = SECONDS (sec)
TEMPERATURE = CELSIUS (C)
TOFFSET = 273.0
FORCE = NEWTON (N)
HEAT = MILLIJOULES (mJ)
INPUT UNITS ARE ALSO SET TO MPA
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Student
00000000 VERSION=WINDOWS x64 18:01:27 DEC 14, 2022 CP= 0.141
wbnew--Static Structural (B5)
***** ANSYS ANALYSIS DEFINITION (PREP7) *****
*********** Nodes for the whole assembly ***********
*********** Nodes for all Remote Points ***********
*********** Elements for Body 1 "Geom\Capo" ***********
*********** Elements for Body 2 "Geom\Solid" ***********
*********** Send User Defined Coordinate System(s) ***********
*********** Set Reference Temperature ***********
*********** Send Materials ***********
*********** Create Contact "Rough - Geom\Capo To Geom\Solid" ***********
Real Constant Set For Above Contact Is 4 & 3
*********** Fixed Supports ***********
*********** Create Remote Point "Internal Remote Point 2" ***********
*********** Create Joint "Translational - Ground To Geom\Solid" ***********
Real Constant Set For Above Joint Is 7
*********** Define Body Force Temperature ***********
*********** Create Joint Drivers **********
***** ROUTINE COMPLETED ***** CP = 0.328
--- Number of total nodes = 28386
--- Number of contact elements = 8064
--- Number of spring elements = 0
--- Number of bearing elements = 0
--- Number of solid elements = 4155
--- Number of condensed parts = 0
--- Number of total elements = 12221
*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 18.0241667
****************************************************************************
************************* SOLUTION ********************************
****************************************************************************
***** ANSYS SOLUTION ROUTINE *****
PERFORM A STATIC ANALYSIS
THIS WILL BE A NEW ANALYSIS
LARGE DEFORMATION ANALYSIS
PARAMETER _THICKRATIO = 0.5000000000
USE SPARSE MATRIX DIRECT SOLVER
USE THE FULL NEWTON-RAPHSON OPTION FOR ALL DEGREES OF FREEDOM
WITH UNSYMMETRIC SOLVER
AND USE THE DEFAULT ADAPTIVE DESCENT OPTION
CONTACT INFORMATION PRINTOUT LEVEL 1
DO NOT COMBINE ELEMENT MATRIX FILES (.emat) AFTER DISTRIBUTED PARALLEL SOLUTION
DO NOT COMBINE ELEMENT SAVE DATA FILES (.esav) AFTER DISTRIBUTED PARALLEL SOLUTION
CORIOLIS IN STATIONARY REFERENCE FRAME: GYROSCOPIC DAMPING MATRIX WILL BE CALCULATED
NLDIAG: Nonlinear diagnostics CONT option is set to ON.
Writing frequency : each ITERATION.
DEFINE RESTART CONTROL FOR LOADSTEP LAST
AT FREQUENCY OF LAST AND NUMBER FOR OVERWRITE IS -1
DELETE RESTART FILES OF ENDSTEP
****************************************************
******************* SOLVE FOR LS 1 OF 4 ****************
PRINTOUT RESUMED BY /GOP
SELECT FOR ITEM=TYPE COMPONENT=
IN RANGE 7 TO 7 STEP 1
1 ELEMENTS (OF 12221 DEFINED) SELECTED BY ESEL COMMAND.
APPLIED BOUNDARY CONDITIONS OR FORCES FOR JOINT ELEMENTS
SPECIFIED VALUE FOR ALL SELECTED ELEMENTS
FORCE, MOMENT, DISPLACEMENT OR ROTATION LABEL = UX
SET ACCORDING TO TABLE PARAMETER = _LOADVARI57
ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 20365 STEP 1
12221 ELEMENTS (OF 12221 DEFINED) SELECTED BY ESEL COMMAND.
USE AUTOMATIC TIME STEPPING THIS LOAD STEP
USE INITIAL TIME STEP SIZE OF 0.1000000E-01 FOR ALL DEGREES OF FREEDOM
FOR AUTOMATIC TIME STEPPING:
USE 0.1000000E-01 AS THE MINIMUM TIME STEP SIZE
USE 0.1000000E-01 AS THE MAXIMUM TIME STEP SIZE
TIME= 1.0000
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
WRITE ALL ITEMS TO THE DATABASE WITH A FREQUENCY OF NONE
FOR ALL APPLICABLE ENTITIES
WRITE NSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EANG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE ETMP ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE VENG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE NLOA ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE SRFS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE BKST ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EPTH ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE MISC ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR THE ENTITIES DEFINED BY COMPONENT _ALLCONTACTS
WRITE CONT ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE NLDA ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
PRINTOUT RESUMED BY /GOP
WRITE MISC ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR THE ENTITIES DEFINED BY COMPONENT _ELMISC
NONLINEAR STABILIZATION CONTROL:
KEY=OFF
*GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000
*IF ANSINTER_ ( = 0.00000 ) NE
0 ( = 0.00000 ) THEN
*ENDIF
*** NOTE *** CP = 0.656 TIME= 18:01:27
The automatic domain decomposition logic has selected the MESH domain
decomposition method with 2 processes per solution.
***** ANSYS SOLVE COMMAND *****
*** WARNING *** CP = 0.656 TIME= 18:01:27
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** NOTE *** CP = 0.703 TIME= 18:01:28
The model data was checked and warning messages were found.
Please review output or errors file (
C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScr
ratch\Scr86C5\file0.err ) for these warning messages.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0
ELEMENT TYPE 2 IS SOLID187. IT IS NOT ASSOCIATED WITH FULLY INCOMPRESSIBLE
HYPERELASTIC MATERIALS. NO SUGGESTION IS AVAILABLE AND NO RESETTING IS NEEDED.
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Student
00000000 VERSION=WINDOWS x64 18:01:28 DEC 14, 2022 CP= 0.703
wbnew--Static Structural (B5)
S O L U T I O N O P T I O N S
PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
DEGREES OF FREEDOM. . . . . . UX UY UZ ROTX ROTY ROTZ
ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
NONLINEAR GEOMETRIC EFFECTS . . . . . . . . . .ON
EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE
PLASTIC MATERIAL PROPERTIES INCLUDED. . . . . .YES
NEWTON-RAPHSON OPTION . . . . . . . . . . . . .FULL UNSYMMETRIC
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .UNSYMMETRIC
*** WARNING *** CP = 0.734 TIME= 18:01:28
Material number 7 (used by element 12300) should normally have at least
one MP or one TB type command associated with it. Output of energy by
material may not be available.
*** NOTE *** CP = 0.766 TIME= 18:01:28
The step data was checked and warning messages were found.
Please review output or errors file (
C:\Users\Luanderson\AppData\Local\Temp\WB_Luanderson_8904_2\_ProjectScr
ratch\Scr86C5\file0.err ) for these warning messages.
*** NOTE *** CP = 0.797 TIME= 18:01:28
Internal nodes from 28387 to 28390 are created.
1 internal nodes are used for handling degrees of freedom on pilot
nodes of rigid target surfaces.
3 internal nodes are used for non-contact elements with mixed
formulation.
*** NOTE *** CP = 0.859 TIME= 18:01:28
Internal nodes from 28387 to 28390 are created.
1 internal nodes are used for handling degrees of freedom on pilot
nodes of rigid target surfaces.
3 internal nodes are used for non-contact elements with mixed
formulation.
*** NOTE *** CP = 1.266 TIME= 18:01:28
Symmetric Deformable- deformable contact pair identified by real
constant set 3 and contact element type 3 has been set up. The
companion pair has real constant set ID 4. Both pairs should have the
same behavior.
ANSYS will deactivate the current pair and keep its companion pair,
resulting in asymmetric contact.
Contact algorithm: Augmented Lagrange method
Contact detection at: Gauss integration point
Contact stiffness factor FKN 1.0000
The resulting initial contact stiffness 1783.2
Default penetration tolerance factor FTOLN 0.10000
The resulting penetration tolerance 0.60566
Default tangent stiffness factor FKT 1.0000
Default elastic slip factor SLTOL 0.50000E-02
The resulting elastic slip tolerance 0.10094
Update contact stiffness at each iteration
Default Max. friction stress TAUMAX 0.10000E+21
Average contact surface length 20.189
Average contact pair depth 6.0566
Average target surface length 11.073
Default pinball region factor PINB 2.0000
The resulting pinball region 12.113
*WARNING*: Initial penetration is included.
Rough contact is defined.
*** NOTE *** CP = 1.266 TIME= 18:01:28
Min. Initial gap 5.03209051 was detected between contact element 18190
and target element 20200.
You may move entire target surface by: x= -1.182266212E-02, y=
-5.03207497, z= -4.082909165E-03, to bring it in contact.
****************************************
*** NOTE *** CP = 1.266 TIME= 18:01:28
Symmetric Deformable- deformable contact pair identified by real
constant set 4 and contact element type 3 has been set up. The
companion pair has real constant set ID 3. Both pairs should have the
same behavior.
ANSYS will keep the current pair and deactivate its companion pair,
resulting in asymmetric contact.
Contact algorithm: Augmented Lagrange method
Contact detection at: Gauss integration point
Contact stiffness factor FKN 1.0000
The resulting initial contact stiffness 1783.2
Default penetration tolerance factor FTOLN 0.10000
The resulting penetration tolerance 0.87119
Default tangent stiffness factor FKT 1.0000
Default elastic slip factor SLTOL 0.50000E-02
The resulting elastic slip tolerance 0.55549E-01
Update contact stiffness at each iteration
Default Max. friction stress TAUMAX 0.10000E+21
Average contact surface length 11.110
Average contact pair depth 8.7119
Average target surface length 20.040
Default pinball region factor PINB 2.0000
The resulting pinball region 17.424
*WARNING*: Initial penetration is included.
Rough contact is defined.
*** NOTE *** CP = 1.266 TIME= 18:01:28
Min. Initial gap 4.80633588 was detected between contact element 20112
and target element 14290.
You may move entire target surface by: x= -0.656985361, y= 4.74818476,
z= -0.352102748, to bring it in contact.
****************************************
*** NOTE *** CP = 1.266 TIME= 18:01:28
Rigid-constraint surface identified by real constant set 5 and contact
element type 5 has been set up. The degrees of freedom of the rigid
surface are driven by the pilot node 28386 which connects to other
element 12300. Internal MPC will be built.
The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ
****************************************
*** NOTE *** CP = 1.297 TIME= 18:01:28
Internal nodes from 28387 to 28390 are created.
1 internal nodes are used for handling degrees of freedom on pilot
nodes of rigid target surfaces.
3 internal nodes are used for non-contact elements with mixed
formulation.
D I S T R I B U T E D D O M A I N D E C O M P O S E R
...Number of elements: 12221
...Number of nodes: 28390
...Decompose to 2 CPU domains
...Element load balance ratio = 1.017
L O A D S T E P O P T I O N S
LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1
TIME AT END OF THE LOAD STEP. . . . . . . . . . 1.0000
AUTOMATIC TIME STEPPING . . . . . . . . . . . . ON
STARTING TIME STEP SIZE. . . . . . . . . . . 0.10000E-01
MINIMUM TIME STEP SIZE . . . . . . . . . . . 0.10000E-01
MAXIMUM TIME STEP SIZE . . . . . . . . . . . 0.10000E-01
MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS. . . . 15
STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO
STRESS-STIFFENING . . . . . . . . . . . . . . . ON
TERMINATE ANALYSIS IF NOT CONVERGED . . . . . .YES (EXIT)
CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS
CORIOLIS EFFECT IN STATIONARY REF. FRAME . . . ON
COPY INTEGRATION POINT VALUES TO NODE . . . . .YES, FOR ELEMENTS WITH
ACTIVE MAT. NONLINEARITIES
PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
DATABASE OUTPUT CONTROLS
ITEM FREQUENCY COMPONENT
ALL NONE
NSOL ALL
RSOL ALL
EANG ALL
ETMP ALL
VENG ALL
NLOA ALL
STRS ALL
SRFS ALL
BKST ALL
EPEL ALL
EPPL ALL
EPTH ALL
MISC ALL _ALLCONTACTS
CONT ALL
NLDA ALL
MISC ALL _ELMISC
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr
*** NOTE *** CP = 1.797 TIME= 18:01:28
Rigid-constraint surface identified by real constant set 5 and contact
element type 5 has been set up. The degrees of freedom of the rigid
surface are driven by the pilot node 28386 which connects to other
element 12300. Internal MPC will be built.
The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ
****************************************
MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED
TO BE, NEQIT = 25, BY SOLUTION CONTROL LOGIC.
The FEA model contains 0 external CE equations and 1068 internal CE
equations.
*********** PRECISE MASS SUMMARY ***********
TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
Translational mass | Coupled translational/rotational mass
0.24526E-02 0.0000 0.0000 | 0.0000 0.23759E-02 -2.1169
0.0000 0.24526E-02 0.0000 | -0.23759E-02 0.0000 5.9711
0.0000 0.0000 0.24526E-02 | 2.1169 -5.9711 0.0000
------------------------------------------ | ------------------------------------------
| Rotational mass (inertia)
| 2019.1 -5151.8 -4.9403
| -5151.8 15155. -2.0171
| -4.9403 -2.0171 16792.
TOTAL MASS = 0.24526E-02
The mass principal axes coincide with the global Cartesian axes
CENTER OF MASS (X,Y,Z)= 2434.6 863.13 0.96874
TOTAL INERTIA ABOUT CENTER OF MASS
191.97 2.0486 0.84408
2.0486 617.88 0.33625E-01
0.84408 0.33625E-01 427.25
PRINCIPAL INERTIAS = 191.96 617.89 427.25
ORIENTATION VECTORS OF THE INERTIA PRINCIPAL AXES IN GLOBAL CARTESIAN
( 1.000,-0.005,-0.004) ( 0.005, 1.000, 0.000) ( 0.004,-0.000, 1.000)
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.219013E-02
2 0.262450E-03
Range of element maximum matrix coefficients in global coordinates
Maximum = 63925971.4 at element 1374.
Minimum = 786780.377 at element 9.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 3900 SOLID186 0.766 0.000196
2 255 SOLID187 0.016 0.000061
3 3988 CONTA174 0.062 0.000016
4 3988 TARGE170 0.000 0.000000
5 88 CONTA174 0.000 0.000000
6 1 TARGE170 0.000 0.000000
7 1 MPC184 0.016 0.015625
Time at end of element matrix formulation CP = 3.40625.
ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.rdb
FOR POSSIBLE RESUME FROM THIS POINT
FORCE CONVERGENCE VALUE = 0.000 CRITERION= 0.5102E-04
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 80820, Maximum wavefront = 1404
*** NOTE *** CP = 4.391 TIME= 18:01:31
The initial memory allocation (-m) has been exceeded.
Supplemental memory allocations are being used.
Process memory allocated for solver = 553.277 MB
Process memory required for in-core solution = 467.341 MB
Process memory required for out-of-core solution = 262.843 MB
Total memory allocated for solver = 959.635 MB
Total memory required for in-core solution = 790.123 MB
Total memory required for out-of-core solution = 367.606 MB
*** NOTE *** CP = 4.391 TIME= 18:01:31
The Distributed Sparse Matrix Solver is currently running in the
in-core memory mode. This memory mode uses the most amount of memory
in order to avoid using the hard drive as much as possible, which most
often results in the fastest solution time. This mode is recommended
if enough physical memory is present to accommodate all of the solver
data.
*** WARNING *** CP = 4.391 TIME= 18:01:31
Pivoting has been activated for the Distributed Sparse Matrix Solver .
The memory required may greatly exceed the predicted amount. In that
event, use the DSPOPTION command to change the memory mode and/or
memory size used by the Distributed Sparse Matrix Solver.
*** NOTE *** CP = 4.391 TIME= 18:01:31
The system matrix is unsymmetric.
curEqn= 40566 totEqn= 40566 Job CP sec= 5.562
Factor Done= 100% Factor Wall sec= 0.563 rate= 27.5 GFlops
Distributed sparse solver maximum pivot= 68371621.1 at node 840 UY.
Distributed sparse solver minimum pivot= 0.99879707 at node 14176 UY.
Distributed sparse solver minimum pivot in absolute value= 0.99879707
at node 14176 UY.
DISP CONVERGENCE VALUE = 0.5000 CRITERION= 0.2551E-01
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.5000
DISP CONVERGENCE VALUE = 0.2500 CRITERION= 0.2603E-01
LINE SEARCH PARAMETER = 0.5000 SCALED MAX DOF INC = -0.2500
FORCE CONVERGENCE VALUE = 0.1101E-05 CRITERION= 0.5206E-04 <<< CONVERGED
*** WARNING *** CP = 8.547 TIME= 18:01:35
A reference force value times the tolerance is used by the
Newton-Raphson method for checking convergence. The calculated
reference FORCE CONVERGENCE VALUE = 6.17053349E-09 is less than a
threshold. This threshold is internally calculated. You can
overwrite it by specifying MINREF on the CNVTOL command. Check
results carefully.
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2500
DISP CONVERGENCE VALUE = 0.1609 CRITERION= 0.2656E-01
LINE SEARCH PARAMETER = 0.6436 SCALED MAX DOF INC = -0.1609
FORCE CONVERGENCE VALUE = 0.1816E-05 CRITERION= 0.5312E-04 <<< CONVERGED
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.8910E-01
DISP CONVERGENCE VALUE = 0.6588E-01 CRITERION= 0.2710E-01
LINE SEARCH PARAMETER = 0.7394 SCALED MAX DOF INC = -0.6588E-01
FORCE CONVERGENCE VALUE = 0.1693E-05 CRITERION= 0.5421E-04 <<< CONVERGED
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2322E-01
DISP CONVERGENCE VALUE = 0.2322E-01 CRITERION= 0.2766E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.2322E-01
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 4
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 3900 SOLID186 0.438 0.000112
2 255 SOLID187 0.016 0.000061
3 3964 CONTA174 0.062 0.000016
5 88 CONTA174 0.000 0.000000
7 1 MPC184 0.000 0.000000
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 3900 SOLID186 0.000 0.000000
2 255 SOLID187 0.000 0.000000
3 3964 CONTA174 0.000 0.000000
5 88 CONTA174 0.000 0.000000
7 1 MPC184 0.000 0.000000
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 4
*** TIME = 0.100000E-01 TIME INC = 0.100000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.10000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 0.1070E-07 CRITERION= 0.5102E-04
DISP CONVERGENCE VALUE = 0.2408E-15 CRITERION= 0.2551E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2408E-15
DISP CONVERGENCE VALUE = 0.2408E-15 CRITERION= 0.2603E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.2408E-15
FORCE CONVERGENCE VALUE = 0.5534E-08 CRITERION= 0.5206E-04 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1390E-15
DISP CONVERGENCE VALUE = 0.1390E-15 CRITERION= 0.2656E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = 0.1390E-15
FORCE CONVERGENCE VALUE = 0.5038E-08 CRITERION= 0.5312E-04 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 2 COMPLETED. CUM ITER = 6
*** TIME = 0.200000E-01 TIME INC = 0.100000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.10000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 0.7496E-08 CRITERION= 0.5102E-04
DISP CONVERGENCE VALUE = 0.2600E-15 CRITERION= 0.2551E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2600E-15
DISP CONVERGENCE VALUE = 0.2600E-15 CRITERION= 0.2603E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = 0.2600E-15
FORCE CONVERGENCE VALUE = 0.5375E-08 CRITERION= 0.5206E-04 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.9855E-16
DISP CONVERGENCE VALUE = 0.9855E-16 CRITERION= 0.2656E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.9855E-16
FORCE CONVERGENCE VALUE = 0.5344E-08 CRITERION= 0.5312E-04 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 3 COMPLETED. CUM ITER = 8
*** TIME = 0.300000E-01 TIME INC = 0.100000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.10000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 0.8173E-08 CRITERION= 0.5102E-04
DISP CONVERGENCE VALUE = 0.2121E-15 CRITERION= 0.2551E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2121E-15
DISP CONVERGENCE VALUE = 0.2121E-15 CRITERION= 0.2603E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = 0.2121E-15
FORCE CONVERGENCE VALUE = 0.5306E-08 CRITERION= 0.5206E-04 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.1000E-15
DISP CONVERGENCE VALUE = 0.1000E-15 CRITERION= 0.2656E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.1000E-15
FORCE CONVERGENCE VALUE = 0.5584E-08 CRITERION= 0.5312E-04 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 4 COMPLETED. CUM ITER = 10
*** TIME = 0.400000E-01 TIME INC = 0.100000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.10000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 0.7482E-08 CRITERION= 0.5102E-04
DISP CONVERGENCE VALUE = 0.2192E-15 CRITERION= 0.2551E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2192E-15
DISP CONVERGENCE VALUE = 0.2192E-15 CRITERION= 0.2603E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.2192E-15
FORCE CONVERGENCE VALUE = 0.5359E-08 CRITERION= 0.5206E-04 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.9096E-16
DISP CONVERGENCE VALUE = 0.9096E-16 CRITERION= 0.2656E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = 0.9096E-16
FORCE CONVERGENCE VALUE = 0.5652E-08 CRITERION= 0.5312E-04 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 5 COMPLETED. CUM ITER = 12
*** TIME = 0.500000E-01 TIME INC = 0.100000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.10000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 0.7310E-08 CRITERION= 0.5102E-04
DISP CONVERGENCE VALUE = 0.6637E-15 CRITERION= 0.2551E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.6637E-15
DISP CONVERGENCE VALUE = 0.6637E-15 CRITERION= 0.2603E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.6637E-15
FORCE CONVERGENCE VALUE = 0.6789E-07 CRITERION= 0.5206E-04 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.4441E-15
DISP CONVERGENCE VALUE = 0.4441E-15 CRITERION= 0.2656E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.4441E-15
FORCE CONVERGENCE VALUE = 0.6817E-07 CRITERION= 0.5312E-04 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 6 COMPLETED. CUM ITER = 14
*** TIME = 0.600000E-01 TIME INC = 0.100000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.10000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 0.1363E-06 CRITERION= 0.5102E-04
DISP CONVERGENCE VALUE = 0.6523E-15 CRITERION= 0.2551E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.6523E-15
DISP CONVERGENCE VALUE = 0.6523E-15 CRITERION= 0.2603E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = 0.6523E-15
FORCE CONVERGENCE VALUE = 0.6835E-07 CRITERION= 0.5206E-04 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.4441E-15
DISP CONVERGENCE VALUE = 0.4441E-15 CRITERION= 0.2656E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.4441E-15
FORCE CONVERGENCE VALUE = 0.6782E-07 CRITERION= 0.5312E-04 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 7 COMPLETED. CUM ITER = 16
*** TIME = 0.700000E-01 TIME INC = 0.100000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.10000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 0.1453E-06 CRITERION= 0.5102E-04
DISP CONVERGENCE VALUE = 0.1146E-12 CRITERION= 0.2551E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1146E-12
DISP CONVERGENCE VALUE = 0.1146E-12 CRITERION= 0.2603E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = 0.1146E-12
FORCE CONVERGENCE VALUE = 0.5967E-08 CRITERION= 0.5206E-04 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1359E-15
DISP CONVERGENCE VALUE = 0.1359E-15 CRITERION= 0.2656E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = 0.1359E-15
FORCE CONVERGENCE VALUE = 0.5084E-08 CRITERION= 0.5312E-04 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 8 COMPLETED. CUM ITER = 18
*** TIME = 0.800000E-01 TIME INC = 0.100000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.10000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 0.1459E-06 CRITERION= 0.5102E-04
DISP CONVERGENCE VALUE = 0.1146E-12 CRITERION= 0.2551E-01 <<< CONVERGED
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.1146E-12
DISP CONVERGENCE VALUE = 0.1146E-12 CRITERION= 0.2603E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.1146E-12
FORCE CONVERGENCE VALUE = 0.5631E-08 CRITERION= 0.5206E-04 <<< CONVERGED
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.1499E-15
DISP CONVERGENCE VALUE = 0.1499E-15 CRITERION= 0.2656E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.1499E-15
FORCE CONVERGENCE VALUE = 0.5314E-08 CRITERION= 0.5312E-04 <<< CONVERGED
>>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2
*** LOAD STEP 1 SUBSTEP 9 COMPLETED. CUM ITER = 20
*** TIME = 0.900000E-01 TIME INC = 0.100000E-01
*** AUTO STEP TIME: NEXT TIME INC = 0.10000E-01 UNCHANGED
FORCE CONVERGENCE VALUE = 2289. CRITERION= 0.5254E-01
DISP CONVERGENCE VALUE = 0.3749 CRITERION= 0.2551E-02
EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.3749
DISP CONVERGENCE VALUE = 0.3558 CRITERION= 0.2603E-02
LINE SEARCH PARAMETER = 0.9493 SCALED MAX DOF INC = 0.3558
FORCE CONVERGENCE VALUE = 0.2480E+05 CRITERION= 0.4034
EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2093
DISP CONVERGENCE VALUE = 0.2093 CRITERION= 0.2656E-01
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.2093
FORCE CONVERGENCE VALUE = 1454. CRITERION= 0.5428E-01
EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1752
DISP CONVERGENCE VALUE = 0.1336 CRITERION= 0.2710E-01
LINE SEARCH PARAMETER = 0.7625 SCALED MAX DOF INC = 0.1336
FORCE CONVERGENCE VALUE = 3580. CRITERION= 0.1221E-01
EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.9788E-01
DISP CONVERGENCE VALUE = 0.9788E-01 CRITERION= 0.2766E-01
LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.9788E-01
FORCE CONVERGENCE VALUE = 777.8 CRITERION= 0.1609
EQUIL ITER 5 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.3449
DISP CONVERGENCE VALUE = 0.1725E-01 CRITERION= 0.2822E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.1725E-01
FORCE CONVERGENCE VALUE = 750.0 CRITERION= 0.1561
EQUIL ITER 6 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.1110
DISP CONVERGENCE VALUE = 0.1109 CRITERION= 0.2880E-01
LINE SEARCH PARAMETER = 0.9993 SCALED MAX DOF INC = -0.1109
FORCE CONVERGENCE VALUE = 1026. CRITERION= 0.1722
EQUIL ITER 7 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2887
DISP CONVERGENCE VALUE = 0.1443E-01 CRITERION= 0.2939E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.1443E-01
FORCE CONVERGENCE VALUE = 982.3 CRITERION= 0.1669
EQUIL ITER 8 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.4275E-01
DISP CONVERGENCE VALUE = 0.4235E-01 CRITERION= 0.2999E-01
LINE SEARCH PARAMETER = 0.9905 SCALED MAX DOF INC = -0.4235E-01
FORCE CONVERGENCE VALUE = 112.6 CRITERION= 0.1805
EQUIL ITER 9 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4186
DISP CONVERGENCE VALUE = 0.2093E-01 CRITERION= 0.3060E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.2093E-01
FORCE CONVERGENCE VALUE = 127.5 CRITERION= 0.3503
EQUIL ITER 10 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.3834E-01
DISP CONVERGENCE VALUE = 0.3676E-01 CRITERION= 0.3122E-01
LINE SEARCH PARAMETER = 0.9586 SCALED MAX DOF INC = -0.3676E-01
FORCE CONVERGENCE VALUE = 90.51 CRITERION= 0.2760
EQUIL ITER 11 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4418
DISP CONVERGENCE VALUE = 0.2209E-01 CRITERION= 0.3186E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.2209E-01
FORCE CONVERGENCE VALUE = 108.5 CRITERION= 0.5358
EQUIL ITER 12 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2592E-01
DISP CONVERGENCE VALUE = 0.2551E-01 CRITERION= 0.3251E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.9841 SCALED MAX DOF INC = -0.2551E-01
FORCE CONVERGENCE VALUE = 39.97 CRITERION= 0.6009
EQUIL ITER 13 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4698
DISP CONVERGENCE VALUE = 0.2349E-01 CRITERION= 0.3317E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.2349E-01
FORCE CONVERGENCE VALUE = 63.79 CRITERION= 0.5834
EQUIL ITER 14 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2571E-01
DISP CONVERGENCE VALUE = 0.2534E-01 CRITERION= 0.3385E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.9858 SCALED MAX DOF INC = -0.2534E-01
FORCE CONVERGENCE VALUE = 40.11 CRITERION= 0.6455
EQUIL ITER 15 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4764
DISP CONVERGENCE VALUE = 0.2382E-01 CRITERION= 0.3454E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.2382E-01
FORCE CONVERGENCE VALUE = 63.81 CRITERION= 0.6268
EQUIL ITER 16 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2444E-01
DISP CONVERGENCE VALUE = 0.2416E-01 CRITERION= 0.3524E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.9886 SCALED MAX DOF INC = -0.2416E-01
FORCE CONVERGENCE VALUE = 38.15 CRITERION= 0.6749
EQUIL ITER 17 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4792
DISP CONVERGENCE VALUE = 0.2396E-01 CRITERION= 0.3596E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.2396E-01
FORCE CONVERGENCE VALUE = 61.78 CRITERION= 0.6553
EQUIL ITER 18 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2438E-01
DISP CONVERGENCE VALUE = 0.2411E-01 CRITERION= 0.3670E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.9888 SCALED MAX DOF INC = -0.2411E-01
FORCE CONVERGENCE VALUE = 38.13 CRITERION= 0.7045
EQUIL ITER 19 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4798
DISP CONVERGENCE VALUE = 0.2399E-01 CRITERION= 0.3745E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.2399E-01
FORCE CONVERGENCE VALUE = 61.73 CRITERION= 0.6840
EQUIL ITER 20 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2429E-01
DISP CONVERGENCE VALUE = 0.2402E-01 CRITERION= 0.3821E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.9890 SCALED MAX DOF INC = -0.2402E-01
FORCE CONVERGENCE VALUE = 38.01 CRITERION= 0.7338
EQUIL ITER 21 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4801
DISP CONVERGENCE VALUE = 0.2400E-01 CRITERION= 0.3899E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.2400E-01
FORCE CONVERGENCE VALUE = 61.60 CRITERION= 0.7125
EQUIL ITER 22 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2428E-01
DISP CONVERGENCE VALUE = 0.2402E-01 CRITERION= 0.3979E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.9891 SCALED MAX DOF INC = -0.2402E-01
FORCE CONVERGENCE VALUE = 38.00 CRITERION= 0.7642
EQUIL ITER 23 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.4801
DISP CONVERGENCE VALUE = 0.2401E-01 CRITERION= 0.4060E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.5000E-01 SCALED MAX DOF INC = 0.2401E-01
FORCE CONVERGENCE VALUE = 61.59 CRITERION= 0.7421
EQUIL ITER 24 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.2427E-01
DISP CONVERGENCE VALUE = 0.2401E-01 CRITERION= 0.4143E-01 <<< CONVERGED
LINE SEARCH PARAMETER = 0.9891 SCALED MAX DOF INC = -0.2401E-01 -
December 15, 2022 at 8:06 am
Erik Kostson
Ansys EmployeeHi
For impact (velocity on a sphere) one would use explicit dynamics - there are many tutorials on that search and you will find.
All the best
Erik
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