Note
Go to the end to download the full example code.
Topology optimization of a simple cantilever beam#
This example demonstrates the structural topology optimization of a simple cantilever beam. The structural analysis is performed with basic constraints and load, which is then transferred to the topology optimization.
Import necessary libraries#
import os
import ansys.mechanical.core as mech
from ansys.mechanical.core.examples import delete_downloads, download_file
from matplotlib import image as mpimg
from matplotlib import pyplot as plt
Embed Mechanical and set global variables
app = mech.App(version=241)
globals().update(mech.global_variables(app, True))
print(app)
def display_image(image_name):
plt.figure(figsize=(16, 9))
plt.imshow(mpimg.imread(os.path.join(cwd, image_name)))
plt.xticks([])
plt.yticks([])
plt.axis("off")
plt.show()
cwd = os.path.join(os.getcwd(), "out")
Ansys Mechanical [Ansys Mechanical Enterprise]
Product Version:241
Software build date: 11/27/2023 10:24:20
Configure graphics for image export
ExtAPI.Graphics.Camera.SetSpecificViewOrientation(ViewOrientationType.Front)
image_export_format = GraphicsImageExportFormat.PNG
settings_720p = Ansys.Mechanical.Graphics.GraphicsImageExportSettings()
settings_720p.Resolution = GraphicsResolutionType.EnhancedResolution
settings_720p.Background = GraphicsBackgroundType.White
settings_720p.Width = 1280
settings_720p.Height = 720
settings_720p.CurrentGraphicsDisplay = False
Import structural analsys#
Download .mechdat file
structural_mechdat_file = download_file(
"cantilever.mechdat", "pymechanical", "embedding"
)
app.open(structural_mechdat_file)
STRUCT = ExtAPI.DataModel.Project.Model.Analyses[0]
STRUCT_SLN = STRUCT.Solution
STRUCT_SLN.Solve(True)
Display structural analsys results#
Total deformation
STRUCT_SLN.Children[1].Activate()
ExtAPI.Graphics.Camera.SetFit()
ExtAPI.Graphics.ExportImage(
os.path.join(cwd, "total_deformation.png"), image_export_format, settings_720p
)
display_image("total_deformation.png")
Equivalent stress
STRUCT_SLN.Children[2].Activate()
ExtAPI.Graphics.Camera.SetFit()
ExtAPI.Graphics.ExportImage(
os.path.join(cwd, "equivalent_stress.png"), image_export_format, settings_720p
)
display_image("equivalent_stress.png")
Topology optimization#
# Set MKS unit system
ExtAPI.Application.ActiveUnitSystem = MechanicalUnitSystem.StandardMKS
# Store all main tree nodes as variables
GEOM = ExtAPI.DataModel.Project.Model.Geometry
MSH = ExtAPI.DataModel.Project.Model.Mesh
NS_GRP = ExtAPI.DataModel.Project.Model.NamedSelections
CONN_GRP = ExtAPI.DataModel.Project.Model.Connections
MY_TOTAL_VOL = GEOM.Volume.Value
MY_TOTAL_MA = GEOM.Mass.Value
# Get structural analysis and link to topology optimization
TOPO_OPT = ExtAPI.DataModel.Project.Model.AddTopologyOptimizationAnalysis()
TOPO_OPT.TransferDataFrom(STRUCT)
# Set ``None`` for optimization region boundary condition exclusion region
# Optimization region
OPT_REG = TOPO_OPT.Children[1]
# OPT_REG.BoundaryCondition=BoundaryConditionType.None
# Using ``getattr`` because Python.Net does not support the ``None`` enum
OPT_REG.BoundaryCondition = BoundaryConditionType.AllLoadsAndSupports
# Insert volume response constraint object for topology optimization
# Delete mass response constraint
MASS_CONSTRN = TOPO_OPT.Children[3]
MASS_CONSTRN.Delete()
# Add volume response constraint
VOL_CONSTRN = TOPO_OPT.AddVolumeConstraint()
# VOL_CONSTRN.DefineBy=ResponseConstraintDefineBy.Constant
# VOL_CONSTRN.PercentageToRetain=50
# Insert member size manufacturing constraint
MEM_SIZE_MFG_CONSTRN = TOPO_OPT.AddMemberSizeManufacturingConstraint()
MEM_SIZE_MFG_CONSTRN.Minimum = ManuMemberSizeControlledType.Manual
MEM_SIZE_MFG_CONSTRN.MinSize = Quantity("2.4 [m]")
# # Store coordinate system ID for use in symmetry manufacturing constraint
# Coordinate_Systems = DataModel.Project.Model.CoordinateSystems
# coord_sys7 = Coordinate_Systems.Children[7]
# # Insert symmetry manufacturing constraint
# SYMM_MFG_CONSTRN = TOPO_OPT.AddSymmetryManufacturingConstraint()
# SYMM_MFG_CONSTRN.CoordinateSystem = coord_sys7
TOPO_OPT.Activate()
ExtAPI.Graphics.Camera.SetFit()
ExtAPI.Graphics.ExportImage(
os.path.join(cwd, "boundary_conditions.png"), image_export_format, settings_720p
)
display_image("boundary_conditions.png")
Solve#
TOPO_OPT_SLN = TOPO_OPT.Solution
TOPO_OPT_SLN.Solve(True)
Messages#
Messages = ExtAPI.Application.Messages
if Messages:
for message in Messages:
print(f"[{message.Severity}] {message.DisplayString}")
else:
print("No [Info]/[Warning]/[Error] Messages")
[Info] For Mass, Volume, Center of Gravity or Moment of Inertia Response constraints, it is recommended to use Criterion objects in Measures object (inserted from Model Object).
[Warning] The default mesh size calculations have changed in 18.2. Specifically, the default min size values and/or defeature size values scale dynamically in relation to the element (max face) size. These settings could lead to a significantly different mesh, so the model will be resumed using the previous values for min size and defeature size rather than leaving those values as default.
Display results#
TOPO_OPT_SLN.Children[1].Activate()
TOPO_DENS = TOPO_OPT_SLN.Children[1]
Add smoothing to the STL
TOPO_DENS.AddSmoothing()
TOPO_OPT.Solution.EvaluateAllResults()
TOPO_DENS.Children[0].Activate()
ExtAPI.Graphics.Camera.SetFit()
ExtAPI.Graphics.ExportImage(
os.path.join(cwd, "topo_opitimized_smooth.png"), image_export_format, settings_720p
)
display_image("topo_opitimized_smooth.png")
Export animation
animation_export_format = (
Ansys.Mechanical.DataModel.Enums.GraphicsAnimationExportFormat.GIF
)
settings_720p = Ansys.Mechanical.Graphics.AnimationExportSettings()
settings_720p.Width = 1280
settings_720p.Height = 720
TOPO_DENS.ExportAnimation(
os.path.join(cwd, "Topo_opitimized.gif"), animation_export_format, settings_720p
)
Review the results
# Print topology density results
print("Topology Density Results")
print("Minimum Density: ", TOPO_DENS.Minimum)
print("Maximum Density: ", TOPO_DENS.Maximum)
print("Iteration Number: ", TOPO_DENS.IterationNumber)
print("Original Volume: ", TOPO_DENS.OriginalVolume.Value)
print("Final Volume: ", TOPO_DENS.FinalVolume.Value)
print("Percent Volume of Original: ", TOPO_DENS.PercentVolumeOfOriginal)
print("Original Mass: ", TOPO_DENS.OriginalMass.Value)
print("Final Mass: ", TOPO_DENS.FinalMass.Value)
print("Percent Mass of Original: ", TOPO_DENS.PercentMassOfOriginal)
Topology Density Results
Minimum Density: 0.0010000000474974513
Maximum Density: 1.0
Iteration Number: 35
Original Volume: 1000.0000054389238
Final Volume: 522.4924773573875
Percent Volume of Original: 52.24924745155908
Original Mass: 7849999.975463867
Final Mass: 4101565.9057617188
Percent Mass of Original: 52.24924737046705
Display output file from solve#
def write_file_contents_to_console(path):
"""Write file contents to console."""
with open(path, "rt") as file:
for line in file:
print(line, end="")
solve_path = TOPO_OPT.WorkingDir
solve_out_path = os.path.join(solve_path, "solve.out")
if solve_out_path:
write_file_contents_to_console(solve_out_path)
Ansys Mechanical Enterprise
*------------------------------------------------------------------*
| |
| W E L C O M E T O T H E A N S Y S (R) P R O G R A M |
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*------------------------------------------------------------------*
***************************************************************
* ANSYS MAPDL 2024 R1 LEGAL NOTICES *
***************************************************************
* *
* Copyright 1971-2024 Ansys, Inc. All rights reserved. *
* Unauthorized use, distribution or duplication is *
* prohibited. *
* *
* Ansys is a registered trademark of Ansys, Inc. or its *
* subsidiaries in the United States or other countries. *
* See the Ansys, Inc. online documentation or the Ansys, Inc. *
* documentation CD or online help for the complete Legal *
* Notice. *
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* INCLUDE TRADE SECRETS AND CONFIDENTIAL AND PROPRIETARY *
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***************************************************************
2024 R1
Point Releases and Patches installed:
Ansys, Inc. License Manager 2024 R1
Structures 2024 R1
LS-DYNA 2024 R1
Mechanical Products 2024 R1
***** MAPDL COMMAND LINE ARGUMENTS *****
INITIAL JOBNAME = file
BATCH MODE REQUESTED (-b) = LIST
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 = /github/home/.local/share/ansys_mechanical_core/examples/cantilever_Mech_Files/StructuralOptimization/ds.dat
OUTPUT FILE NAME = /github/home/.local/share/ansys_mechanical_core/examples/cantilever_Mech_Files/StructuralOptimization/solve.out
RELEASE= 2024 R1 BUILD= 24.1 UP20231106 VERSION=LINUX x64
CURRENT JOBNAME=file0 07:42:49 MAY 06, 2024 CP= 0.232
1 /batch
2 /config,noeldb,1 ! force off writing results to database
3 ! Ansys input file written by Workbench version 2024 R1
4
5 *GET,numcpu,active,0,NUMCPU
6 *cfopen,numCPU,dat
7 *VWRITE,numcpu
8 (F8.0)
9 *cfclose
10 /SYS,"/install/ansys_inc/v241/aisol/CommonFiles/linx64/Opti.exe" 45077 NEW
11
12 /CLEAR,NOSTART
13 /FILNAME,file_Static20
14 resume,,db
15 esel,u,ename,,153,156
16 esel,r,sfe,pres,-1e100,1e100
17 *get,_numsfeelem,elem,0,count
18 *if,_numsfeelem,ne,0,then
19 allsel
20 /solu
21 bfedele,all, TEMP ! Deletes temperature based body load
22 bfdele,all, TEMP ! Deletes temperature based body load
23 acel,0.0,0.0,0.0 ! Deletes linear acceleration
24 cgom,0.0,0.0,0.0 ! Deletes rotational velocity
25 dcgomg,0.0,0.0,0.0 ! Deletes rotational acceleration
26 rescontrol,,none ! No multiframe restarts file
27 /com,******************* SOLVE FOR LS 1 ****************
28 outres,erase
29 outres,all,none
30 outres,nsol,last
31 outres,eangl,last
32 outres,etmp,last
33 outres,veng,last
34 outres,nload,last ! Output nodal forces at all time points for Topology Optimization future intent
35 ! *********** WB SOLVE COMMAND ***********
36 ! check interactive state
37 *get,ANSINTER_,active,,int
38 *if,ANSINTER_,ne,0,then
39 /eof
40 *endif
41 nsubst,1,1,1
42 ematwrite,yes
43 psolve,elform,topo
44 *GET,numcpu,active,0,NUMCPU
45 *cfopen,numCPU,dat
46 *VWRITE,numcpu
47 (F8.0)
48 *cfclose
49 fini
50 /SYS,"/install/ansys_inc/v241/aisol/CommonFiles/linx64/Opti.exe" 45077 PRES1
51 /solu
52 /com,****************************************************
53 /com,*************** FINISHED SOLVE FOR LS 1 *************
54 *get,_wallasol,active,,time,wall
55
56 *else
57 /SYS,"/install/ansys_inc/v241/aisol/CommonFiles/linx64/Opti.exe" 45077 PRES1
58 *endif
59
60 *DIM,notconverged_array,,1
61 *vread,notconverged_array(1),notconverged,dat
62 (F8.0)
63 *SET,notconverged,notconverged_array(1)
64 *if,notconverged,ne,1,then
65 /eof
66 *endif
67 *dowhile,notconverged
68 /CLEAR,NOSTART
69 /FILNAME,file_Static20
70 resume,,db
71 /config,resuprec,0 ! We read the element nodal forces (ENF) from the rst file
72 ! and need these values in double precision
73 /solu
74 rescontrol,,none ! No multiframe restarts file
75 /com,******************* SOLVE FOR LS 1 ****************
76 outres,erase
77 outres,all,none
78 outres,nsol,last
79 outres,eangl,last
80 outres,etmp,last
81 outres,veng,last
82 outres,nload,last ! Output nodal forces at all time points for Topology Optimization future intent
83 ! *********** WB SOLVE COMMAND ***********
84 ! check interactive state
85 *get,ANSINTER_,active,,int
86 *if,ANSINTER_,ne,0,then
87 /eof
88 *endif
89 outres, rsol,last
90 ncnv,,1e+12
91 DMPOPTION,rst,no
92 TOTYPE,EXTERNAL ! Activates modification of element stiffness matrices
93 solve
94 /com,****************************************************
95 /com,*************** FINISHED SOLVE FOR LS 1 *************
96 *get,_wallasol,active,,time,wall
97
98 *GET,numcpu,active,0,NUMCPU
99 *cfopen,numCPU,dat
100 *VWRITE,numcpu
101 (F8.0)
102 *cfclose
103 finish
104
105 /SYS,"/install/ansys_inc/v241/aisol/CommonFiles/linx64/Opti.exe" 45077 TOPO1
106
107 *DIM,notconverged_array,,1
108 *vread,notconverged_array(1),notconverged,dat
109 (F8.0)
110 *SET,notconverged,notconverged_array(1)
111 *ENDDO
112 /exit,nosave
RUN SETUP PROCEDURE FROM FILE= /install/ansys_inc/v241/ansys/apdl/start.ans
/INPUT FILE= /install/ansys_inc/v241/ansys/apdl/start.ans LINE= 0
*** NOTE *** CP = 0.301 TIME= 07:42:49
The /CONFIG,NOELDB command is not valid in a distributed memory
parallel solution. Command is ignored.
*GET NUMCPU FROM ACTI ITEM=NUMC VALUE= 4.00000000
OPENED FILE= numCPU.dat FOR COMMAND FILE DATA
COMMAND FILE CLOSED
SYSTEM=
"/install/ansys_inc/v241/aisol/CommonFiles/linx64/Opti.exe" 45077 NEW
CLEAR MAPDL DATABASE AND RESTART
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
*** NOTE *** CP = 0.332 TIME= 07:42:49
The defined jobname (file_Static20) contains a numeric value (0->9) for
the last character. Therefore, when creating local solution files,
the distributed memory parallel solver will append an underscore to
the jobname prior to appending the MPI rank.
RESUME ANSYS DATA FROM FILE NAME=file_Static20.db
*** MAPDL GLOBAL STATUS ***
TITLE = --Static Structural (B5)
ANALYSIS TYPE = STATIC (STEADY-STATE)
1 ELEM TYPES DEFINED MAX ELEM TYPE NUMBER = 1
4000 ELEMENTS DEFINED MAX ELEMENT NUMBER = 4000
12261 NODES DEFINED MAX NODE NUMBER = 12261
1 MATERIALS DEFINED MAX MATERIAL NUMBER = 1
1 REAL CONSTS DEFINED MAX REAL CONST NUMBER = 1
0 SECTIONS DEFINED MAX SECTION NUMBER = 0
8 COORD SYS DEFINED MAX COORD SYS NUMBER = 19
ACTIVE COORDINATE SYSTEM = 0 (CARTESIAN)
NUMBER OF DEFINED NODAL CONSTRAINTS = 202
NUMBER OF DEFINED NODAL LOADS = 2
NUMBER OF DEFINED COMPONENTS = 17
NUMBER OF DEFINED ELEM SURFACE LOADS = 0
NUMBER OF DEFINED ELEM BODY LOADS = 0
NUMBER OF DEFINED NODE BODY FORCES = 0
INITIAL JOBNAME = file
CURRENT JOBNAME = file_Static20
UNSELECT FOR ITEM=ENAM COMPONENT=
IN RANGE 153 TO 156 STEP 1
4000 ELEMENTS (OF 4000 DEFINED) SELECTED BY ESEL COMMAND.
RESELECT FOR ITEM=SFE COMPONENT=PRES BETWEEN-0.10000+101 AND 0.10000+101
KABS= 0. TOLERANCE= 0.00000
0 ELEMENTS (OF 4000 DEFINED) SELECTED BY ESEL COMMAND.
*GET _NUMSFEELEM FROM ELEM ITEM=COUN VALUE= 0.00000000
*IF _numsfeelem ( = 0.00000 ) NE
0 ( = 0.00000 ) THEN
*ELSE
SYSTEM=
"/install/ansys_inc/v241/aisol/CommonFiles/linx64/Opti.exe" 45077 PRES1
*ENDIF
SET PARAMETER DIMENSIONS ON NOTCONVERGED_ARRAY
TYPE=ARRA DIMENSIONS= 1 1 1
VECTOR READ OPERATION *VREAD
notconve READ FROM FILE notconverged.dat
VECTOR LENGTH= 1
LOOP DIRECTIONS=IJK COUNTS= 1 1 1
FORMAT=(F8.0)
PARAMETER NOTCONVERGED = 1.000000000
*IF notconverged ( = 1.00000 ) NE
1 ( = 1.00000 ) THEN
*ENDIF
*DOWHILE LOOP ON PARAMETER= NOTCONVERGED
CLEAR MAPDL DATABASE AND RESTART
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
*** NOTE *** CP = 0.629 TIME= 07:42:49
The defined jobname (file_Static20) contains a numeric value (0->9) for
the last character. Therefore, when creating local solution files,
the distributed memory parallel solver will append an underscore to
the jobname prior to appending the MPI rank.
RESUME ANSYS DATA FROM FILE NAME=file_Static20.db
*** MAPDL GLOBAL STATUS ***
TITLE = --Static Structural (B5)
ANALYSIS TYPE = STATIC (STEADY-STATE)
1 ELEM TYPES DEFINED MAX ELEM TYPE NUMBER = 1
4000 ELEMENTS DEFINED MAX ELEMENT NUMBER = 4000
12261 NODES DEFINED MAX NODE NUMBER = 12261
1 MATERIALS DEFINED MAX MATERIAL NUMBER = 1
1 REAL CONSTS DEFINED MAX REAL CONST NUMBER = 1
0 SECTIONS DEFINED MAX SECTION NUMBER = 0
8 COORD SYS DEFINED MAX COORD SYS NUMBER = 19
ACTIVE COORDINATE SYSTEM = 0 (CARTESIAN)
NUMBER OF DEFINED NODAL CONSTRAINTS = 202
NUMBER OF DEFINED NODAL LOADS = 2
NUMBER OF DEFINED COMPONENTS = 17
NUMBER OF DEFINED ELEM SURFACE LOADS = 0
NUMBER OF DEFINED ELEM BODY LOADS = 0
NUMBER OF DEFINED NODE BODY FORCES = 0
INITIAL JOBNAME = file
CURRENT JOBNAME = file_Static20
USE DOUBLE PRECISION RESULTS FILE FORMAT
***** MAPDL SOLUTION ROUTINE *****
DO NOT SAVE ANY RESTART FILES AT ALL
******************* SOLVE FOR LS 1 ****************
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 LAST
FOR ALL APPLICABLE ENTITIES
WRITE EANG ITEMS TO THE DATABASE WITH A FREQUENCY OF LAST
FOR ALL APPLICABLE ENTITIES
WRITE ETMP ITEMS TO THE DATABASE WITH A FREQUENCY OF LAST
FOR ALL APPLICABLE ENTITIES
WRITE VENG ITEMS TO THE DATABASE WITH A FREQUENCY OF LAST
FOR ALL APPLICABLE ENTITIES
WRITE NLOA ITEMS TO THE DATABASE WITH A FREQUENCY OF LAST
FOR ALL APPLICABLE ENTITIES
*GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000
*IF ANSINTER_ ( = 0.00000 ) NE
0 ( = 0.00000 ) THEN
*ENDIF
WRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF LAST
FOR ALL APPLICABLE ENTITIES
KEY TO TERMINATE RUN IF NO CONVERGENCE= 1
DEGREE OF FREEDOM (DISPLACEMENT) LIMIT= 0.10000E+13
CUMULATIVE ITERATION LIMIT= 0
ELAPSED TIME LIMIT (SEC)= 0.0000 ( 0 HOURS 0 MIN)
CPU TIME LIMIT (SEC)= 0.0000 ( 0 HOURS 0 MIN)
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
SET TOPOLOGICAL OPTIMIZATION METHOD TO EXTERNALLY SUPPLIED METHOD
*** NOTE *** CP = 0.731 TIME= 07:42:49
The automatic domain decomposition logic has selected the MESH domain
decomposition method with 4 processes per solution.
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 0.753 TIME= 07:42:49
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** NOTE *** CP = 0.773 TIME= 07:42:49
The model data was checked and warning messages were found.
Please review output or errors file (
/github/home/.local/share/ansys_mechanical_core/examples/cantilever_Mec
ch_Files/StructuralOptimization/file0.err ) for these warning messages.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:49 MAY 06, 2024 CP= 0.775
--Static Structural (B5)
S O L U T I O N O P T I O N S
PROBLEM DIMENSIONALITY. . . . . . . . . . . . .2-D
DEGREES OF FREEDOM. . . . . . UX UY
ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC
*** NOTE *** CP = 0.791 TIME= 07:42:49
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
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 LAST
EANG LAST
ETMP LAST
VENG LAST
NLOA LAST
RSOL LAST
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.321 0.000080
Time at end of element matrix formulation CP = 1.18635297.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 1.231 TIME= 07:42:50
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 1.059
Factor Done= 100% Factor Wall sec= 0.029 rate= 3.0 GFlops
Distributed sparse solver maximum pivot= 8.498134039E+11 at node 4183
UX.
Distributed sparse solver minimum pivot= 4.475744808E+09 at node 975
UY.
Distributed sparse solver minimum pivot in absolute value=
4.475744808E+09 at node 975 UY.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.113 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.016 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
*GET _WALLASOL FROM ACTI ITEM=TIME WALL VALUE= 7.71388889
*GET NUMCPU FROM ACTI ITEM=NUMC VALUE= 4.00000000
OPENED FILE= numCPU.dat FOR COMMAND FILE DATA
COMMAND FILE CLOSED
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 1.340
SYSTEM=
"/install/ansys_inc/v241/aisol/CommonFiles/linx64/Opti.exe" 45077 TOPO1
SET PARAMETER DIMENSIONS ON NOTCONVERGED_ARRAY
TYPE=ARRA DIMENSIONS= 1 1 1
VECTOR READ OPERATION *VREAD
notconve READ FROM FILE notconverged.dat
VECTOR LENGTH= 1
LOOP DIRECTIONS=IJK COUNTS= 1 1 1
FORMAT=(F8.0)
PARAMETER NOTCONVERGED = 1.000000000
*ENDDO INDEX= NOTCONVERGED
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 1.435 TIME= 07:42:50
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:50 MAY 06, 2024 CP= 1.482
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.323 0.000081
Time at end of element matrix formulation CP = 1.9239279.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 1.961 TIME= 07:42:50
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 1.784
Factor Done= 100% Factor Wall sec= 0.012 rate= 6.9 GFlops
Distributed sparse solver maximum pivot= 8.498134039E+11 at node 4183
UX.
Distributed sparse solver minimum pivot= 1.908976253E+09 at node 137
UY.
Distributed sparse solver minimum pivot in absolute value=
1.908976253E+09 at node 137 UY.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 2.061
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 2.159 TIME= 07:42:50
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:50 MAY 06, 2024 CP= 2.206
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.314 0.000079
Time at end of element matrix formulation CP = 2.61809802.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 2.680 TIME= 07:42:51
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 2.502
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.498134039E+11 at node 4183
UX.
Distributed sparse solver minimum pivot= 192206.996 at node 11239 UX.
Distributed sparse solver minimum pivot in absolute value= 192206.996
at node 11239 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 2.779
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 2.836 TIME= 07:42:51
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:51 MAY 06, 2024 CP= 2.857
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.218 0.000054
Time at end of element matrix formulation CP = 3.08154202.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 3.250 TIME= 07:42:51
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 3.086
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 224.500092 at node 3329 UX.
Distributed sparse solver minimum pivot in absolute value= 224.500092
at node 3329 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 3.363
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 3.420 TIME= 07:42:51
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:51 MAY 06, 2024 CP= 3.441
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.195 0.000049
Time at end of element matrix formulation CP = 3.64268804.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 3.730 TIME= 07:42:51
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 3.627
Factor Done= 100% Factor Wall sec= 0.023 rate= 3.8 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 3.928
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 4.001 TIME= 07:42:52
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:52 MAY 06, 2024 CP= 4.033
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.212 0.000053
Time at end of element matrix formulation CP = 4.34767389.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 4.480 TIME= 07:42:52
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 4.302
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 4.580
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 4.637 TIME= 07:42:52
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:52 MAY 06, 2024 CP= 4.657
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.219 0.000055
Time at end of element matrix formulation CP = 4.88470268.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 5.067 TIME= 07:42:52
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 4.890
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.0 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 5.167
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 5.240 TIME= 07:42:53
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:53 MAY 06, 2024 CP= 5.272
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.296 0.000074
Time at end of element matrix formulation CP = 5.67399502.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 5.738 TIME= 07:42:53
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 5.560
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.108 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 5.837
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 5.908 TIME= 07:42:53
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:53 MAY 06, 2024 CP= 5.941
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.213 0.000053
Time at end of element matrix formulation CP = 6.25520897.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 6.390 TIME= 07:42:53
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 6.212
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 6.488
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 6.546 TIME= 07:42:54
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:54 MAY 06, 2024 CP= 6.566
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.193 0.000048
Time at end of element matrix formulation CP = 6.76718187.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 6.878 TIME= 07:42:54
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 6.780
Factor Done= 100% Factor Wall sec= 0.031 rate= 2.8 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 7.057
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 7.138 TIME= 07:42:54
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:54 MAY 06, 2024 CP= 7.170
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.234 0.000059
Time at end of element matrix formulation CP = 7.45944166.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 7.615 TIME= 07:42:54
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 7.437
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 7.714
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 7.773 TIME= 07:42:54
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:54 MAY 06, 2024 CP= 7.793
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.191 0.000048
Time at end of element matrix formulation CP = 7.99436426.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 8.082 TIME= 07:42:55
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 8.002
Factor Done= 100% Factor Wall sec= 0.027 rate= 3.2 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 8.280
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 8.339 TIME= 07:42:55
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:55 MAY 06, 2024 CP= 8.360
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.195 0.000049
Time at end of element matrix formulation CP = 8.55923462.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 8.647 TIME= 07:42:55
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 8.567
Factor Done= 100% Factor Wall sec= 0.027 rate= 3.2 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.108 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 8.846
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 8.903 TIME= 07:42:55
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:55 MAY 06, 2024 CP= 8.923
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.198 0.000050
Time at end of element matrix formulation CP = 9.1287899.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 9.224 TIME= 07:42:55
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 9.136
Factor Done= 100% Factor Wall sec= 0.031 rate= 2.8 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 9.412
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 9.486 TIME= 07:42:56
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:56 MAY 06, 2024 CP= 9.518
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.215 0.000054
Time at end of element matrix formulation CP = 9.82779598.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 9.959 TIME= 07:42:56
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 9.780
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 10.058
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 10.114 TIME= 07:42:56
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:56 MAY 06, 2024 CP= 10.135
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.219 0.000055
Time at end of element matrix formulation CP = 10.3599281.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 10.529 TIME= 07:42:56
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 10.365
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 10.643
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 10.718 TIME= 07:42:56
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:56 MAY 06, 2024 CP= 10.750
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.273 0.000068
Time at end of element matrix formulation CP = 11.1410551.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 11.213 TIME= 07:42:57
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 11.035
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.0 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 11.311
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 11.370 TIME= 07:42:57
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:57 MAY 06, 2024 CP= 11.390
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.234 0.000058
Time at end of element matrix formulation CP = 11.6317034.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 11.801 TIME= 07:42:57
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 11.623
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.501612847E+11 at node 11376
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 11.901
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 11.980 TIME= 07:42:57
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:57 MAY 06, 2024 CP= 12.012
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.273 0.000068
Time at end of element matrix formulation CP = 12.3640461.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 12.467 TIME= 07:42:58
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 12.289
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.0 GFlops
Distributed sparse solver maximum pivot= 8.510798055E+11 at node 4684
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.112 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.016 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 12.567
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 12.626 TIME= 07:42:58
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:58 MAY 06, 2024 CP= 12.647
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.191 0.000048
Time at end of element matrix formulation CP = 12.846858.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 12.999 TIME= 07:42:58
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 12.863
Factor Done= 100% Factor Wall sec= 0.014 rate= 6.0 GFlops
Distributed sparse solver maximum pivot= 8.51944378E+11 at node 4684
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.108 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 13.140
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 13.212 TIME= 07:42:58
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:58 MAY 06, 2024 CP= 13.244
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.233 0.000058
Time at end of element matrix formulation CP = 13.5643301.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 13.688 TIME= 07:42:58
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 13.510
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.0 GFlops
Distributed sparse solver maximum pivot= 8.51944378E+11 at node 4684
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 13.787
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 13.844 TIME= 07:42:59
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:59 MAY 06, 2024 CP= 13.864
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.219 0.000055
Time at end of element matrix formulation CP = 14.090147.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 14.268 TIME= 07:42:59
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 14.094
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.2 GFlops
Distributed sparse solver maximum pivot= 8.519418221E+11 at node 4684
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 14.372
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 14.431 TIME= 07:42:59
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:59 MAY 06, 2024 CP= 14.451
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.193 0.000048
Time at end of element matrix formulation CP = 14.6520224.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 14.740 TIME= 07:42:59
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 14.636
Factor Done= 100% Factor Wall sec= 0.023 rate= 3.7 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 14.936
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 15.015 TIME= 07:42:59
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:42:59 MAY 06, 2024 CP= 15.047
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.234 0.000059
Time at end of element matrix formulation CP = 15.3376074.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 15.489 TIME= 07:43:00
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 15.311
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.0 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.111 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 15.589
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 15.669 TIME= 07:43:00
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:00 MAY 06, 2024 CP= 15.701
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.309 0.000077
Time at end of element matrix formulation CP = 16.111517.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 16.170 TIME= 07:43:00
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 15.992
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.115 0.000029
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.016 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 16.272
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 16.371 TIME= 07:43:00
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:00 MAY 06, 2024 CP= 16.418
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.307 0.000077
Time at end of element matrix formulation CP = 16.8191452.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 16.876 TIME= 07:43:01
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 16.698
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 16.975
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 17.054 TIME= 07:43:01
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:01 MAY 06, 2024 CP= 17.086
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.293 0.000073
Time at end of element matrix formulation CP = 17.4823704.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 17.550 TIME= 07:43:01
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 17.372
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.112 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 17.650
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 17.748 TIME= 07:43:01
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:01 MAY 06, 2024 CP= 17.796
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.259 0.000065
Time at end of element matrix formulation CP = 18.1312428.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 18.245 TIME= 07:43:02
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 18.067
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.111 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 18.345
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 18.419 TIME= 07:43:02
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:02 MAY 06, 2024 CP= 18.452
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.276 0.000069
Time at end of element matrix formulation CP = 18.8443604.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 18.914 TIME= 07:43:02
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 18.736
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.216034 at node 131 UX.
Distributed sparse solver minimum pivot in absolute value= 101.216034
at node 131 UX.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.111 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.016 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 19.013
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 19.070 TIME= 07:43:02
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:02 MAY 06, 2024 CP= 19.091
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.214 0.000054
Time at end of element matrix formulation CP = 19.355772.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 19.510 TIME= 07:43:03
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 19.332
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.0 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.205088 at node 4374 UY.
Distributed sparse solver minimum pivot in absolute value= 101.205088
at node 4374 UY.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 19.610
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 19.667 TIME= 07:43:03
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:03 MAY 06, 2024 CP= 19.687
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.192 0.000048
Time at end of element matrix formulation CP = 19.8873787.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 19.975 TIME= 07:43:03
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 19.872
Factor Done= 100% Factor Wall sec= 0.023 rate= 3.8 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.052074 at node 4374 UY.
Distributed sparse solver minimum pivot in absolute value= 101.052074
at node 4374 UY.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 20.174
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 20.239 TIME= 07:43:03
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:03 MAY 06, 2024 CP= 20.260
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.238 0.000060
Time at end of element matrix formulation CP = 20.5207081.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 20.675 TIME= 07:43:03
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 20.496
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.052061 at node 4374 UY.
Distributed sparse solver minimum pivot in absolute value= 101.052061
at node 4374 UY.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.109 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 20.774
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 20.844 TIME= 07:43:04
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:04 MAY 06, 2024 CP= 20.876
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.274 0.000068
Time at end of element matrix formulation CP = 21.2724285.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 21.340 TIME= 07:43:04
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 21.163
Factor Done= 100% Factor Wall sec= 0.013 rate= 6.4 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.05188 at node 4374 UY.
Distributed sparse solver minimum pivot in absolute value= 101.05188 at
node 4374 UY.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000028
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 21.451
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 21.548 TIME= 07:43:04
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:04 MAY 06, 2024 CP= 21.596
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.276 0.000069
Time at end of element matrix formulation CP = 21.973278.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 22.043 TIME= 07:43:04
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 21.865
Factor Done= 100% Factor Wall sec= 0.012 rate= 7.1 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 101.051786 at node 4374 UY.
Distributed sparse solver minimum pivot in absolute value= 101.051786
at node 4374 UY.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 22.143
CLEAR MAPDL DATABASE AND RESTART
Topology Optimization: released
Ansys Mechanical Enterprise
CURRENT JOBNAME REDEFINED AS file_Static20
***** MAPDL SOLUTION ROUTINE *****
******************* SOLVE FOR LS 1 ****************
ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
DO NOT COMBINE RESULT FILES (.rst, .rth, etc.) AFTER DISTRIBUTED PARALLEL SOLUTION
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 22.199 TIME= 07:43:05
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS PLANE183 WITH PLANE STRESS OPTION. NO SUGGESTION IS
AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R1 24.1 ***
Ansys Mechanical Enterprise
00000000 VERSION=LINUX x64 07:43:05 MAY 06, 2024 CP= 22.219
--Static Structural (B5)
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: 4000
...Number of nodes: 12261
...Decompose to 4 CPU domains
...Element load balance ratio = 1.000
Topology Optimization: Multipliers prepared
Topology Optimization: Multipliers updated
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file_Static20.mntr
**** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA ****
CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID
TOTAL MASS = 0.78500E+07
MOM. OF INERTIA MOM. OF INERTIA
CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS
XC = 20.000 IXX = 0.1635E+10 IXX = 0.4087E+09
YC = 12.500 IYY = 0.4187E+10 IYY = 0.1047E+10
ZC = 0.0000 IZZ = 0.5822E+10 IZZ = 0.1455E+10
IXY = -0.1962E+10 IXY = 0.4123E-02
IYZ = 0.000 IYZ = 0.000
IZX = 0.000 IZX = 0.000
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.785000E+07
Range of element maximum matrix coefficients in global coordinates
Maximum = 4.259917493E+11 at element 31.
Minimum = 4.249084863E+11 at element 1033.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.193 0.000048
Time at end of element matrix formulation CP = 22.4209652.
DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
Number of equations = 24320, Maximum wavefront = 40
Process memory allocated for solver = 11.583 MB
Process memory required for in-core solution = 11.138 MB
Process memory required for out-of-core solution = 6.663 MB
Total memory allocated for solver = 45.835 MB
Total memory required for in-core solution = 44.072 MB
Total memory required for out-of-core solution = 26.283 MB
*** NOTE *** CP = 22.532 TIME= 07:43:05
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.
curEqn= 6132 totEqn= 6132 Job CP sec= 22.432
Factor Done= 100% Factor Wall sec= 0.026 rate= 3.3 GFlops
Distributed sparse solver maximum pivot= 8.519768656E+11 at node 4690
UY.
Distributed sparse solver minimum pivot= 100.978483 at node 4374 UY.
Distributed sparse solver minimum pivot in absolute value= 100.978483
at node 4374 UY.
*** ELEMENT RESULT CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.110 0.000027
*** NODAL LOAD CALCULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 4000 PLANE183 0.015 0.000004
*** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1
*** TIME = 1.00000 TIME INC = 1.00000 NEW TRIANG MATRIX
*** MAPDL BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file_Static20_0.full
1.062 MB WRITTEN ON RESULTS FILE: file_Static20_0.rst
****************************************************
*************** FINISHED SOLVE FOR LS 1 *************
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 22.709
EXIT MAPDL WITHOUT SAVING DATABASE
NUMBER OF WARNING MESSAGES ENCOUNTERED= 35
NUMBER OF ERROR MESSAGES ENCOUNTERED= 0
Topology Optimization: released
+--------------------- M A P D L S T A T I S T I C S ------------------------+
Release: 2024 R1 Build: 24.1 Update: UP20231106 Platform: LINUX x64
Date Run: 05/06/2024 Time: 07:43 Process ID: 12561
Operating System: Ubuntu 20.04.6 LTS
Processor Model: AMD EPYC 7763 64-Core Processor
Compiler: Intel(R) Fortran Compiler Classic Version 2021.9 (Build: 20230302)
Intel(R) C/C++ Compiler Classic Version 2021.9 (Build: 20230302)
Intel(R) Math Kernel Library Version 2020.0.0 Product Build 20191122
BLAS Library supplied by AMD BLIS
Number 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 2021.10 for Linux* OS
GPU Acceleration: Not Requested
Job Name: file_Static20_0
Input File: ds.dat
Core Machine Name Working Directory
-----------------------------------------------------
0 f8cd179a5ae7 /github/home/.local/share/ansys_mechanical_core/examples/cantilever_Mech_Files/StructuralOptimization
1 f8cd179a5ae7 /github/home/.local/share/ansys_mechanical_core/examples/cantilever_Mech_Files/StructuralOptimization
2 f8cd179a5ae7 /github/home/.local/share/ansys_mechanical_core/examples/cantilever_Mech_Files/StructuralOptimization
3 f8cd179a5ae7 /github/home/.local/share/ansys_mechanical_core/examples/cantilever_Mech_Files/StructuralOptimization
Latency time from master to core 1 = 2.237 microseconds
Latency time from master to core 2 = 2.229 microseconds
Latency time from master to core 3 = 1.962 microseconds
Communication speed from master to core 1 = 9208.20 MB/sec
Communication speed from master to core 2 = 13834.61 MB/sec
Communication speed from master to core 3 = 13972.93 MB/sec
Total CPU time for main thread : 10.5 seconds
Total CPU time summed for all threads : 22.7 seconds
Elapsed time spent obtaining a license : 0.3 seconds
Elapsed time spent pre-processing model (/PREP7) : 0.0 seconds
Elapsed time spent solution - preprocessing : 2.3 seconds
Elapsed time spent computing solution : 8.0 seconds
Elapsed time spent solution - postprocessing : 0.1 seconds
Elapsed time spent post-processing model (/POST1) : 0.0 seconds
Equation solver used : Sparse (symmetric)
Equation solver computational rate : 13.1 Gflops
Equation solver effective I/O rate : 731.7 GB/sec
Sum of disk space used on all processes : 15.2 MB
Sum of memory used on all processes : 549.0 MB
Sum of memory allocated on all processes : 2880.0 MB
Physical memory available : 31 GB
Total amount of I/O written to disk : 0.0 GB
Total amount of I/O read from disk : 0.0 GB
+------------------ E N D M A P D L S T A T I S T I C S -------------------+
*-----------------------------------------------------------------------------*
| |
| RUN COMPLETED |
| |
|-----------------------------------------------------------------------------|
| |
| Ansys MAPDL 2024 R1 Build 24.1 UP20231106 LINUX x64 |
| |
|-----------------------------------------------------------------------------|
| |
| Database Requested(-db) 1024 MB Scratch Memory Requested 1024 MB |
| Max Database Used(Master) 7 MB Max Scratch Used(Master) 137 MB |
| Max Database Used(Workers) 1 MB Max Scratch Used(Workers) 134 MB |
| Sum Database Used(All) 10 MB Sum Scratch Used(All) 539 MB |
| |
|-----------------------------------------------------------------------------|
| |
| CP Time (sec) = 22.718 Time = 07:43:06 |
| Elapsed Time (sec) = 18.000 Date = 05/06/2024 |
| |
*-----------------------------------------------------------------------------*
Project tree#
def print_tree(node, indentation=""):
print(f"{indentation}├── {node.Name}")
if (
hasattr(node, "Children")
and node.Children is not None
and node.Children.Count > 0
):
for child in node.Children:
print_tree(child, indentation + "| ")
root_node = DataModel.Project
print_tree(root_node)
├── Project
| ├── Model
| | ├── Geometry Imports
| | | ├── Geometry Import
| | ├── Geometry
| | | ├── Surface Body Bodies
| | | | ├── Surface Body
| | ├── Materials
| | | ├── Structural Steel
| | ├── Coordinate Systems
| | | ├── Global Coordinate System
| | | ├── Coordinate System
| | | ├── Coordinate System 2
| | | ├── Coordinate System 3
| | | ├── Coordinate System 4
| | | ├── Coordinate System 5
| | | ├── Coordinate System 6
| | | ├── Coordinate System 7
| | | ├── Coordinate System 8
| | ├── Remote Points
| | ├── Mesh
| | | ├── Face Sizing
| | ├── Named Selections
| | | ├── Selection
| | | ├── Bottom_Elements
| | | ├── Top_Elements
| | | ├── Middle1_Elements
| | | ├── Middle2_Elements
| | | ├── Left1_Elements
| | | ├── Left2_Elements
| | | ├── Right1_Elements
| | | ├── Right2_Elements
| | | ├── Optimized_Shape
| | | ├── Outside_Optimized_Shape
| | | ├── Selection 2
| | | ├── Selection 3
| | | ├── Selection 4
| | | ├── Selection 5
| | ├── Static Structural
| | | ├── Analysis Settings
| | | ├── Fixed Support
| | | ├── Nodal Force
| | | ├── Solution
| | | | ├── Solution Information
| | | | ├── Total Deformation
| | | | ├── Equivalent Stress
| | ├── Structural Optimization
| | | ├── Analysis Settings
| | | ├── Optimization Region
| | | ├── Objective
| | | ├── Response Constraint
| | | ├── Manufacturing Constraint
| | | ├── Solution
| | | | ├── Solution Information
| | | | | ├── Topology Density Tracker
| | | | ├── Topology Density
| | | | | ├── Smoothing
Cleanup#
Save project
app.save(os.path.join(cwd, "cantilever_beam_topology_optimization.mechdat"))
app.new()
Delete the example files
delete_downloads()
True
Total running time of the script: (0 minutes 35.833 seconds)