Unknown Error in structural mechanics
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Solver Output
ANSYS Mechanical Enterprise
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* ANSYS 2019 R3 LEGAL NOTICES *
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2019 R3
Point Releases and Patches installed:
ANSYS, Inc. Products 2019 R3
SpaceClaim 2019 R3
AIM 2019 R3
Live (includes SpaceClaim) 2019 R3
Autodyn 2019 R3
LS-DYNA 2019 R3
CFD-Post only 2019 R3
CFX (includes CFD-Post) 2019 R3
Chemkin 2019 R3
EnSight 2019 R3
FENSAP-ICE 2019 R3
Fluent (includes CFD-Post) 2019 R3
Forte 2019 R3
Polyflow (includes CFD-Post) 2019 R3
TurboGrid 2019 R3
ICEM CFD 2019 R3
Aqwa 2019 R3
Customization Files for User Programmable Features 2019 R3
Mechanical Products 2019 R3
Additive 2019 R3
Icepak (includes CFD-Post) 2019 R3
Remote Solve Manager Standalone Services 2019 R3
Viewer 2019 R3
ACIS Geometry Interface 2019 R3
AutoCAD Geometry Interface 2019 R3
Catia, Version 4 Geometry Interface 2019 R3
Catia, Version 5 Geometry Interface 2019 R3
Catia, Version 6 Geometry Interface 2019 R3
Creo Elements/Direct Modeling Geometry Interface 2019 R3
Creo Parametric Geometry Interface 2019 R3
Inventor Geometry Interface 2019 R3
JTOpen Geometry Interface 2019 R3
NX Geometry Interface 2019 R3
Parasolid Geometry Interface 2019 R3
Solid Edge Geometry Interface 2019 R3
SOLIDWORKS Geometry Interface 2019 R3
ANSYS, Inc. License Manager 2019 R3
***** 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:UsersBattery broAppDataLocalTempWB_DESKTOP-8KMV5FI_Battery bro_10724_2_ProjectScratchScrDF84dummy.dat
OUTPUT FILE NAME = C:UsersBattery broAppDataLocalTempWB_DESKTOP-8KMV5FI_Battery bro_10724_2_ProjectScratchScrDF84solve.out
START-UP FILE MODE = NOREAD
STOP FILE MODE = NOREAD
RELEASE= 2019 R3 BUILD= 19.5 UP20190805 VERSION=WINDOWS x64
CURRENT JOBNAME=file0 02
37 MAY 02, 2020 CP= 0.391
PARAMETER _DS_PROGRESS = 999.0000000
/INPUT FILE= ds.dat LINE= 0
*** NOTE *** CP = 0.578 TIME= 0237
The /CONFIG,NOELDB command is not valid in a Distributed ANSYS
solution. Command is ignored.
*GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 2.56027778
TITLE=
unsaved_project--Static Structural (A5)
SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:UsersBattery broAppDataLocalTempWB_DESKTOP-8KMV5FI_Battery bro_10724_2_ProjectScratchScrDF84
SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_SOLVERFILES_DIR(1) = C:UsersBattery broAppDataLocalTempWB_DESKTOP-8KMV5FI_Battery bro_10724_2unsaved_project_filesdp0SYSMECH
SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_USERFILES_DIR(1) = C:UsersBattery broAppDataLocalTempWB_DESKTOP-8KMV5FI_Battery bro_10724_2unsaved_project_filesuser_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 2019 R3 19.5 ***
DISTRIBUTED ANSYS Mechanical Enterprise
00000000 VERSION=WINDOWS x64 0237 MAY 02, 2020 CP= 0.578
unsaved_project--Static Structural (A5)
***** ANSYS ANALYSIS DEFINITION (PREP7) *****
*********** Nodes for the whole assembly ***********
*********** Elements for Body 1 "rebar" ***********
*********** Elements for Body 2 "concrete" ***********
*********** Send User Defined Coordinate System(s) ***********
*********** Set Reference Temperature ***********
*********** Send Materials ***********
*********** Create Contact "Contact Region" ***********
Real Constant Set For Above Contact Is 4 & 3
*********** Fixed Supports ***********
*********** Define Force Using Surface Effect Elements ***********
***** ROUTINE COMPLETED ***** CP = 6.250
--- Number of total nodes = 423123
--- Number of contact elements = 188326
--- Number of spring elements = 0
--- Number of bearing elements = 0
--- Number of solid elements = 241860
--- Number of condensed parts = 0
--- Number of total elements = 430186
*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 2.56138889
****************************************************************************
************************* SOLUTION ********************************
****************************************************************************
***** ANSYS SOLUTION ROUTINE *****
PERFORM A STATIC ANALYSIS
THIS WILL BE A NEW ANALYSIS
PARAMETER _THICKRATIO = 0.5000000000
USE SPARSE MATRIX DIRECT SOLVER
CONTACT INFORMATION PRINTOUT LEVEL 1
DO NOT COMBINE ELEMENT MATRIX FILES (.emat) AFTER DISTRIBUTED PARALLEL SOLUTION
DO NOT COMBINE ELEMENT SAVE DATA FILES (.esav) AFTER DISTRIBUTED PARALLEL SOLUTION
NLDIAG: Nonlinear diagnostics CONT option is set to ON.
Writing frequency : each ITERATION.
DO NOT SAVE ANY RESTART FILES AT ALL
****************************************************
******************* SOLVE FOR LS 1 OF 1 ****************
SELECT FOR ITEM=TYPE COMPONENT=
IN RANGE 5 TO 5 STEP 1
1250 ELEMENTS (OF 430186 DEFINED) SELECTED BY ESEL COMMAND.
SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.
2589 NODES (OF 423123 DEFINED) SELECTED FROM
1250 SELECTED ELEMENTS BY NSLE COMMAND.
SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 1 KVAL = 1
VALUES = 0.0000 0.0000 0.0000 0.0000
SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 2 KVAL = 1
VALUES = -9.7510 -9.7510 -9.7510 -9.7510
SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 3 KVAL = 1
VALUES = 0.0000 0.0000 0.0000 0.0000
ALL SELECT FOR ITEM=NODE COMPONENT=
IN RANGE 1 TO 423123 STEP 1
423123 NODES (OF 423123 DEFINED) SELECTED BY NSEL COMMAND.
ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 526706 STEP 1
430186 ELEMENTS (OF 430186 DEFINED) SELECTED BY ESEL COMMAND.
PRINTOUT RESUMED BY /GOP
USE 1 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM
FOR AUTOMATIC TIME STEPPING:
USE 1 SUBSTEPS AS A MAXIMUM
USE 1 SUBSTEPS AS A MINIMUM
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 STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
WRITE CONT ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
*GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000
*IF ANSINTER_ ( = 0.00000 ) NE
0 ( = 0.00000 ) THEN
*ENDIF
*** NOTE *** CP = 6.469 TIME= 023:41
The automatic domain decomposition logic has selected the MESH domain
decomposition method with 2 processes per solution.
***** ANSYS SOLVE COMMAND *****
*** WARNING *** CP = 6.844 TIME= 023:42
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** NOTE *** CP = 7.750 TIME= 023:42
The model data was checked and warning messages were found.
Please review output or errors file ( C:UsersBattery
broAppDataLocalTempWB_DESKTOP-8KMV5FI_Battery
bro_10724_2_ProjectScratchScrDF84file0.err ) for these warning
messages.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS SOLID187. IT IS NOT ASSOCIATED WITH FULLY INCOMPRESSIBLE
HYPERELASTIC MATERIALS. NO SUGGESTION IS AVAILABLE AND NO RESETTING IS NEEDED.
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 2019 R3 19.5 ***
DISTRIBUTED ANSYS Mechanical Enterprise
00000000 VERSION=WINDOWS x64 023:43 MAY 02, 2020 CP= 7.875
unsaved_project--Static Structural (A5)
S O L U T I O N O P T I O N S
PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
DEGREES OF FREEDOM. . . . . . UX UY UZ
ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC
*** WARNING *** CP = 8.906 TIME= 023:44
Material number 5 (used by element 525457) 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 = 9.109 TIME= 023:44
The step data was checked and warning messages were found.
Please review output or errors file ( C:UsersBattery
broAppDataLocalTempWB_DESKTOP-8KMV5FI_Battery
bro_10724_2_ProjectScratchScrDF84file0.err ) for these warning
messages.
*** NOTE *** CP = 9.109 TIME= 023:44
The conditions for direct assembly have been met. No .emat or .erot
files will be produced.
*** NOTE *** CP = 21.781 TIME= 023:57
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.
Linear contact is defined
Contact algorithm: Augmented Lagrange method
Contact detection at: Gauss integration point
Contact stiffness factor FKN 10.000
The resulting initial contact stiffness 0.59488E+06
Default penetration tolerance factor FTOLN 0.10000
The resulting penetration tolerance 0.87542
Default opening contact stiffness OPSF will be used.
Default tangent stiffness factor FKT 1.0000
Use constant contact stiffness
Default Max. friction stress TAUMAX 0.10000E+21
Average contact surface length 12.923
Average contact pair depth 8.7542
Default pinball region factor PINB 0.25000
*WARNING*: The default pinball radius may be too small to capture
contacting zone under small sliding assumption. Redefine the pinball
radius if necessary.
The resulting pinball region 2.1886
Initial penetration/gap is excluded.
Bonded contact (always) is defined.
*** NOTE *** CP = 21.781 TIME= 023:57
Max. Initial penetration 2.18669336 was detected between contact
element 396626 and target element 493914.
You may move entire target surface by : x= 0.709550217, y=
2.600381509E-03, z= -2.06837123,to reduce initial penetration.
*WARNING*: The geometric gap/penetration may be too large. Increase
pinball radius if it is a true geometric gap/penetration. Decrease
pinball if it is a false one.
****************************************
*** NOTE *** CP = 21.781 TIME= 023:57
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.
Linear contact is defined
Contact algorithm: Augmented Lagrange method
Contact detection at: Gauss integration point
Contact stiffness factor FKN 10.000
The resulting initial contact stiffness 0.59488E+06
Default penetration tolerance factor FTOLN 0.10000
The resulting penetration tolerance 1.0086
Default opening contact stiffness OPSF will be used.
Default tangent stiffness factor FKT 1.0000
Use constant contact stiffness
Default Max. friction stress TAUMAX 0.10000E+21
Average contact surface length 15.287
Average contact pair depth 10.086
Default pinball region factor PINB 0.25000
*WARNING*: The default pinball radius may be too small to capture
contacting zone under small sliding assumption. Redefine the pinball
radius if necessary.
The resulting pinball region 2.5215
Initial penetration/gap is excluded.
Bonded contact (always) is defined.
*** NOTE *** CP = 21.781 TIME= 023:57
Max. Initial penetration 2.50842227 was detected between contact
element 452967 and target element 361651.
You may move entire target surface by : x= 2.18388105, y= -1.00742273,
z= -0.712702806,to reduce initial penetration.
*WARNING*: The geometric gap/penetration may be too large. Increase
pinball radius if it is a true geometric gap/penetration. Decrease
pinball if it is a false one.
****************************************
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: 430186
...Number of nodes: 423123
...Decompose to 2 CPU domains
...Element load balance ratio = 1.405
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
NUMBER OF SUBSTEPS. . . . . . . . . . . . . . . 1
STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO
PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
DATABASE OUTPUT CONTROLS
ITEM FREQUENCY COMPONENT
ALL NONE
NSOL ALL
RSOL ALL
EANG ALL
ETMP ALL
VENG ALL
STRS ALL
EPEL ALL
EPPL ALL
CONT ALL
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr
*** NOTE *** CP = 46.266 TIME= 024:22
The initial memory allocation (-m) has been exceeded.
Supplemental memory allocations are being used.
*********** PRECISE MASS SUMMARY ***********
TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
Translational mass | Coupled translational/rotational mass
1.2156 0.0000 0.0000 | 0.0000 -12.889 -13.088
0.0000 1.2156 0.0000 | 12.889 0.0000 7.0414
0.0000 0.0000 1.2156 | 13.088 -7.0414 0.0000
|
| Rotational mass (inertia)
| 0.30566E+06 -75.100 75.262
| -75.100 62109. 140.79
| 75.262 140.79 0.30557E+06
TOTAL MASS = 1.2156
The mass principal axes coincide with the global Cartesian axes
CENTER OF MASS (X,Y,Z)= 5.7925 10.767 -10.603
TOTAL INERTIA ABOUT CENTER OF MASS
0.30538E+06 0.71438 0.59964
0.71438 61931. 2.0104
0.59964 2.0104 0.30539E+06
The inertia principal axes coincide with the global Cartesian axes
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.962458E-01
2 1.11935
Range of element maximum matrix coefficients in global coordinates
Maximum = 75136083.1 at element 458935.
Minimum = 46015.8812 at element 237023.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 75535 SOLID187 8.141 0.000108
2 166325 SOLID187 19.109 0.000115
3 93538 CONTA174 9.641 0.000103
4 93538 TARGE170 1.219 0.000013
5 1250 SURF154 0.078 0.000063
Time at end of element matrix formulation CP = 75.140625.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 1261794, Maximum wavefront = 900
Local memory allocated for solver = 1920.324 MB
Local memory required for in-core solution = 6742.971 MB
Local memory required for out-of-core solution = 1871.101 MB
Total memory allocated for solver = 2723.035 MB
Total memory required for in-core solution = 12598.594 MB
Total memory required for out-of-core solution = 2645.318 MB
*** WARNING *** CP = 94.312 TIME= 025:13
The Distributed Sparse Matrix Solver is currently running in the
out-of-core memory mode. This memory mode may provide significantly
worse performance compared to the in-core memory mode, depending on
the amount of available system memory and I/O speed. Please monitor
the solver performance to ensure that the large amount of I/O to the
solver files does not create a bottleneck for performance.
*** ERROR *** CP = 111.109 TIME= 0253
An error has occurred in the Distributed Sparse Matrix Solver while
processing the matrix values. Error code = 36. Please send the data
leading to this operation to your technical support provider, as this
will allow ANSYS, Inc to improve the program.
NUMBER OF WARNING MESSAGES ENCOUNTERED= 3
NUMBER OF ERROR MESSAGES ENCOUNTERED= 1
***** PROBLEM TERMINATED BY INDICATED ERROR(S) OR BY END OF INPUT DATA *****
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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
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Release: 2019 R3 Build: 19.5 Update: UP20190805 Platform: WINDOWS x64
Date Run: 05/02/2020 Time: 025 Process ID: 12092
Operating System: Windows 10 (Build: 18363)
Processor Model: Intel(R) Core(TM) i5-5300U CPU @ 2.30GHz
Compiler: Intel(R) FORTRAN Compiler Version 17.0.6 (Build: 20171215)
Intel(R) C/C++ Compiler Version 17.0.6 (Build: 20171215)
Intel(R) Math Kernel Library Version 2017.0.3 Product Build 20170413
Number of machines requested : 1
Total number of cores available : 4
Number of physical cores available : 2
Number of processes requested : 2
Number of threads per process requested : 1
Total number of cores requested : 2 (Distributed Memory Parallel)
MPI Type: INTELMPI
MPI Version: Intel(R) MPI Library 2018 Update 3 for Windows* OS
GPU Acceleration: Not Requested
Job Name: file0
Input File: dummy.dat
Core Machine Name Working Directory
0 DESKTOP-8KMV5FI C:UsersBattery broAppDataLocalTempWB_DESKTOP-8KMV5FI_Battery bro_10724_2_ProjectScratchScrDF84
1 DESKTOP-8KMV5FI C:UsersBattery broAppDataLocalTempWB_DESKTOP-8KMV5FI_Battery bro_10724_2_ProjectScratchScrDF84
Latency time from master to core 1 = 3.023 microseconds
Communication speed from master to core 1 = 1794.90 MB/sec
Total CPU time for main thread : 111.3 seconds
Total CPU time summed for all threads : 113.3 seconds
Elapsed time spent pre-processing model (/PREP7) : 4.2 seconds
Elapsed time spent solution - preprocessing : 22.9 seconds
Elapsed time spent computing solution : 88.7 seconds
Elapsed time spent solution - postprocessing : 0.0 seconds
Elapsed time spent post-processing model (/POST1) : 0.0 seconds
Equation solver used : Sparse (symmetric)
Maximum total memory used : 4437.0 MB
Maximum total memory allocated : 6815.0 MB
Total physical memory available : 8 GB
Total amount of I/O written to disk : 1.9 GB
Total amount of I/O read from disk : 0.9 GB
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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
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| Ansys 2019 R3 Build 19.5 UP20190805 WINDOWS x64 |
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