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authorAbel Tim <abel@localhost.localdomain>2025-02-24 08:57:09 +0100
committerAbel Tim <abel@localhost.localdomain>2025-02-24 08:57:09 +0100
commit062b8977e06d1fb4c4e0847c3f5cd5066c8ca861 (patch)
tree04e6f5f85ac0264a7e824faff58a0457a5d0ff29 /simulations_V9/structural steel_files/dp0/SYS/MECH/solve.out
parent9fec0cac92427f49b57cb18ecddefddfcdb415b3 (diff)
downloadpws-062b8977e06d1fb4c4e0847c3f5cd5066c8ca861.tar.gz
pws-062b8977e06d1fb4c4e0847c3f5cd5066c8ca861.zip
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+
+ Ansys Mechanical Enterprise Academic Student
+
+
+ *------------------------------------------------------------------*
+ | |
+ | 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 |
+ | |
+ *------------------------------------------------------------------*
+
+
+
+
+ ***************************************************************
+ * ANSYS MAPDL 2024 R2 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. *
+ * *
+ ***************************************************************
+ * *
+ * THIS ANSYS SOFTWARE PRODUCT AND PROGRAM DOCUMENTATION *
+ * INCLUDE TRADE SECRETS AND CONFIDENTIAL AND PROPRIETARY *
+ * PRODUCTS OF ANSYS, INC., ITS SUBSIDIARIES, OR LICENSORS. *
+ * The software products and documentation are furnished by *
+ * Ansys, Inc. or its subsidiaries under a software license *
+ * agreement that contains provisions concerning *
+ * non-disclosure, copying, length and nature of use, *
+ * compliance with exporting laws, warranties, disclaimers, *
+ * limitations of liability, and remedies, and other *
+ * provisions. The software products and documentation may be *
+ * used, disclosed, transferred, or copied only in accordance *
+ * with the terms and conditions of that software license *
+ * agreement. *
+ * *
+ * Ansys, Inc. is a UL registered *
+ * ISO 9001:2015 company. *
+ * *
+ ***************************************************************
+ * *
+ * This product is subject to U.S. laws governing export and *
+ * re-export. *
+ * *
+ * For U.S. Government users, except as specifically granted *
+ * by the Ansys, Inc. software license agreement, the use, *
+ * duplication, or disclosure by the United States Government *
+ * is subject to restrictions stated in the Ansys, Inc. *
+ * software license agreement and FAR 12.212 (for non-DOD *
+ * licenses). *
+ * *
+ ***************************************************************
+
+ 2024 R2
+
+ Point Releases and Patches installed:
+
+ Ansys Service Pack 2024 R2.23068672
+ Discovery 2024 R2.23068672
+ Core WB Files 2024 R2.23068672
+ Ansys Dynamic Reporting 2024 R2.23068672
+ SpaceClaim 2024 R2.23068672
+ CFX (includes CFD-Post) 2024 R2.23068672
+ Chemkin 2024 R2.23068672
+ EnSight 2024 R2.23068672
+ FENSAP-ICE 2024 R2.23068672
+ Fluent (includes CFD-Post) 2024 R2.23068672
+ Polyflow (includes CFD-Post) 2024 R2.23068672
+ Forte (includes EnSight) 2024 R2.23068672
+ TurboGrid 2024 R2.23068672
+ ACIS Geometry Interface 2024 R2.23068672
+ AutoCAD Geometry Interface 2024 R2.23068672
+ Catia, Version 4 Geometry Interface 2024 R2.23068672
+ Catia, Version 5 Geometry Interface 2024 R2.23068672
+ Catia, Version 6 Geometry Interface 2024 R2.23068672
+ Creo Elements/Direct Modeling Geometry Interface 2024 R2.23068672
+ Creo Parametric Geometry Interface 2024 R2.23068672
+ Inventor Geometry Interface 2024 R2.23068672
+ JTOpen Geometry Interface 2024 R2.23068672
+ NX Geometry Interface 2024 R2.23068672
+ Parasolid Geometry Interface 2024 R2.23068672
+ Solid Edge Geometry Interface 2024 R2.23068672
+ SOLIDWORKS Geometry Interface 2024 R2.23068672
+ Speos 2024 R2.23068672
+ Aqwa 2024 R2.23068672
+ Autodyn 2024 R2.23068672
+ Material Calibration App 2024 R2.23068672
+ Customization Files for User Programmable Features 2024 R2.23068672
+ Mechanical Products 2024 R2.23068672
+ Motion 2024 R2.23068672
+ Academic Student 2024 R2.23068672
+
+
+ ***** MAPDL COMMAND LINE ARGUMENTS *****
+ BATCH MODE REQUESTED (-b) = NOLIST
+ INPUT FILE COPY MODE (-c) = COPY
+ DISTRIBUTED MEMORY PARALLEL REQUESTED
+ 2 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS
+ TOTAL OF 2 CORES REQUESTED
+ INPUT FILE NAME = C:\Users\Abel Tim\Documents\pws\simulations_V9\_ProjectScratch\ScrAA48\dummy.dat
+ OUTPUT FILE NAME = C:\Users\Abel Tim\Documents\pws\simulations_V9\_ProjectScratch\ScrAA48\solve.out
+ START-UP FILE MODE = NOREAD
+ STOP FILE MODE = NOREAD
+
+ RELEASE= 2024 R2 BUILD= 24.2 UP20240513 VERSION=WINDOWS x64
+ CURRENT JOBNAME=file0 19:24:14 FEB 02, 2025 CP= 0.125
+
+
+ PARAMETER _DS_PROGRESS = 999.0000000
+
+ /INPUT FILE= ds.dat LINE= 0
+
+
+
+ *** NOTE *** CP = 0.281 TIME= 19:24:15
+ The /CONFIG,NOELDB command is not valid in a distributed memory
+ parallel solution. Command is ignored.
+
+ *GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 19.4041667
+
+ TITLE=
+ structural steel--Static Structural (B5)
+
+ ACT Extensions:
+ LSDYNA, 2024.2
+ 5f463412-bd3e-484b-87e7-cbc0a665e474, wbex
+ /COM, ANSYSMotion, 2024.2
+ 20180725-3f81-49eb-9f31-41364844c769, wbex
+
+
+ SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR
+ TYPE=STRI DIMENSIONS= 248 1 1
+
+ PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\Abel Tim\Documents\pws\simulations_V9\_ProjectScratch\ScrAA48\
+
+ SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR
+ TYPE=STRI DIMENSIONS= 248 1 1
+
+ PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\Abel Tim\Documents\pws\simulations_V9\structural steel_files\dp0\SYS\MECH\
+
+ SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR
+ TYPE=STRI DIMENSIONS= 248 1 1
+
+ PARAMETER _WB_USERFILES_DIR(1) = C:\Users\Abel Tim\Documents\pws\simulations_V9\structural steel_files\user_files\
+ --- Data in consistent MKS units. See Solving Units in the help system for more
+
+ MKS UNITS SPECIFIED FOR INTERNAL
+ LENGTH (l) = METER (M)
+ MASS (M) = KILOGRAM (KG)
+ TIME (t) = SECOND (SEC)
+ TEMPERATURE (T) = CELSIUS (C)
+ TOFFSET = 273.0
+ CHARGE (Q) = COULOMB
+ FORCE (f) = NEWTON (N) (KG-M/SEC2)
+ HEAT = JOULE (N-M)
+
+ PRESSURE = PASCAL (NEWTON/M**2)
+ ENERGY (W) = JOULE (N-M)
+ POWER (P) = WATT (N-M/SEC)
+ CURRENT (i) = AMPERE (COULOMBS/SEC)
+ CAPACITANCE (C) = FARAD
+ INDUCTANCE (L) = HENRY
+ MAGNETIC FLUX = WEBER
+ RESISTANCE (R) = OHM
+ ELECTRIC POTENTIAL = VOLT
+
+ INPUT UNITS ARE ALSO SET TO MKS
+
+ *** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R2 24.2 ***
+ Ansys Mechanical Enterprise Academic Student
+ 01055371 VERSION=WINDOWS x64 19:24:15 FEB 02, 2025 CP= 0.312
+
+ structural steel--Static Structural (B5)
+
+
+
+ ***** MAPDL ANALYSIS DEFINITION (PREP7) *****
+ *********** Nodes for the whole assembly ***********
+ *********** Elements for Body 1 'cam\Solid' ***********
+ *********** Send User Defined Coordinate System(s) ***********
+ *********** Set Reference Temperature ***********
+ *********** Send Materials ***********
+ *********** Fixed Supports ***********
+ *********** Define Force Using Surface Effect Elements ***********
+
+
+ ***** ROUTINE COMPLETED ***** CP = 0.344
+
+
+ --- Number of total nodes = 2829
+ --- Number of contact elements = 10
+ --- Number of spring elements = 0
+ --- Number of bearing elements = 0
+ --- Number of solid elements = 1540
+ --- Number of condensed parts = 0
+ --- Number of total elements = 1550
+
+ *GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 19.4041667
+ ****************************************************************************
+ ************************* SOLUTION ********************************
+ ****************************************************************************
+
+ ***** MAPDL SOLUTION ROUTINE *****
+
+
+ PERFORM A STATIC ANALYSIS
+ THIS WILL BE A NEW ANALYSIS
+
+ PARAMETER _THICKRATIO = 1.000000000
+
+ USE PRECONDITIONED CONJUGATE GRADIENT SOLVER
+ CONVERGENCE TOLERANCE = 1.00000E-08
+ MAXIMUM ITERATION = NumNode*DofPerNode* 1.0000
+
+ CONTACT INFORMATION PRINTOUT LEVEL 1
+
+ CHECK INITIAL OPEN/CLOSED STATUS OF SELECTED CONTACT ELEMENTS
+ AND LIST DETAILED CONTACT PAIR INFORMATION
+
+ SPLIT CONTACT SURFACES AT SOLVE PHASE
+
+ NUMBER OF SPLITTING TBD BY PROGRAM
+
+ DO NOT COMBINE ELEMENT MATRIX FILES (.emat) AFTER DISTRIBUTED PARALLEL SOLUTION
+
+ DO NOT COMBINE ELEMENT SAVE DATA FILES (.esav) AFTER DISTRIBUTED PARALLEL SOLUTION
+
+ NLDIAG: Nonlinear diagnostics CONT option is set to ON.
+ Writing frequency : each ITERATION.
+
+ DO NOT SAVE ANY RESTART FILES AT ALL
+ ****************************************************
+ ******************* SOLVE FOR LS 1 OF 1 ****************
+
+ SELECT FOR ITEM=TYPE COMPONENT=
+ IN RANGE 2 TO 2 STEP 1
+
+ 10 ELEMENTS (OF 1550 DEFINED) SELECTED BY ESEL COMMAND.
+
+ SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.
+
+ 33 NODES (OF 2829 DEFINED) SELECTED FROM
+ 10 SELECTED ELEMENTS BY NSLE COMMAND.
+
+ SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 1 KVAL = 1
+ VALUES = 28.173 28.173 28.173 28.173
+
+ SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 2 KVAL = 1
+ VALUES = 0.52809E+09 0.52809E+09 0.52809E+09 0.52809E+09
+
+ SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 3 KVAL = 1
+ VALUES = 0.0000 0.0000 0.0000 0.0000
+
+ ALL SELECT FOR ITEM=NODE COMPONENT=
+ IN RANGE 1 TO 2829 STEP 1
+
+ 2829 NODES (OF 2829 DEFINED) SELECTED BY NSEL COMMAND.
+
+ ALL SELECT FOR ITEM=ELEM COMPONENT=
+ IN RANGE 1 TO 2276 STEP 1
+
+ 1550 ELEMENTS (OF 1550 DEFINED) SELECTED BY ESEL COMMAND.
+
+ PRINTOUT RESUMED BY /GOP
+
+ USE 1 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM
+ FOR AUTOMATIC TIME STEPPING:
+ USE 1 SUBSTEPS AS A MAXIMUM
+ USE 1 SUBSTEPS AS A MINIMUM
+
+ TIME= 1.0000
+
+ ERASE THE CURRENT DATABASE OUTPUT CONTROL TABLE.
+
+
+ WRITE ALL ITEMS TO THE DATABASE WITH A FREQUENCY OF NONE
+ FOR ALL APPLICABLE ENTITIES
+
+ WRITE NSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
+ FOR ALL APPLICABLE ENTITIES
+
+ WRITE RSOL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
+ FOR ALL APPLICABLE ENTITIES
+
+ WRITE EANG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
+ FOR ALL APPLICABLE ENTITIES
+
+ WRITE ETMP ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
+ FOR ALL APPLICABLE ENTITIES
+
+ WRITE VENG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
+ FOR ALL APPLICABLE ENTITIES
+
+ WRITE STRS ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
+ FOR ALL APPLICABLE ENTITIES
+
+ WRITE EPEL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
+ FOR ALL APPLICABLE ENTITIES
+
+ WRITE EPPL ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
+ FOR ALL APPLICABLE ENTITIES
+
+ WRITE CONT ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
+ FOR ALL APPLICABLE ENTITIES
+
+ *GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000
+
+ *IF ANSINTER_ ( = 0.00000 ) NE
+ 0 ( = 0.00000 ) THEN
+
+ *ENDIF
+
+ *** NOTE *** CP = 0.500 TIME= 19:24:15
+ The automatic domain decomposition logic has selected the MESH domain
+ decomposition method with 2 processes per solution.
+
+ ***** MAPDL SOLVE COMMAND *****
+
+ *** WARNING *** CP = 0.516 TIME= 19:24:15
+ Element shape checking is currently inactive. Issue SHPP,ON or
+ SHPP,WARN to reactivate, if desired.
+
+ *** NOTE *** CP = 0.516 TIME= 19:24:15
+ The model data was checked and warning messages were found.
+ Please review output or errors file ( C:\Users\Abel
+ Tim\Documents\pws\simulations_V9\_ProjectScratch\ScrAA48\file0.err )
+ for these warning messages.
+
+ *** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
+ --- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
+
+ ELEMENT TYPE 1 IS SOLID187. IT IS NOT ASSOCIATED WITH FULLY INCOMPRESSIBLE
+ HYPERELASTIC MATERIALS. NO SUGGESTION IS AVAILABLE AND NO RESETTING IS NEEDED.
+
+
+
+ *** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R2 24.2 ***
+ Ansys Mechanical Enterprise Academic Student
+ 01055371 VERSION=WINDOWS x64 19:24:15 FEB 02, 2025 CP= 0.516
+
+ structural steel--Static Structural (B5)
+
+
+
+ S O L U T I O N O P T I O N S
+
+ PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
+ DEGREES OF FREEDOM. . . . . . UX UY UZ
+ ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
+ OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
+ EQUATION SOLVER OPTION. . . . . . . . . . . . .PCG
+ TOLERANCE. . . . . . . . . . . . . . . . . . 1.00000E-08
+ GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC
+
+ *** WARNING *** CP = 0.516 TIME= 19:24:15
+ Material number 2 (used by element 2267) should normally have at least
+ one MP or one TB type command associated with it. Output of energy by
+ material may not be available.
+
+ *** NOTE *** CP = 0.516 TIME= 19:24:15
+ The step data was checked and warning messages were found.
+ Please review output or errors file ( C:\Users\Abel
+ Tim\Documents\pws\simulations_V9\_ProjectScratch\ScrAA48\file0.err )
+ for these warning messages.
+
+ *** NOTE *** CP = 0.516 TIME= 19:24:15
+ 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: 1550
+ ...Number of nodes: 2829
+ ...Decompose to 2 CPU domains
+ ...Element load balance ratio = 1.006
+
+
+ L O A D S T E P O P T I O N S
+
+ LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1
+ TIME AT END OF THE LOAD STEP. . . . . . . . . . 1.0000
+ NUMBER OF SUBSTEPS. . . . . . . . . . . . . . . 1
+ STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO
+ PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
+ DATABASE OUTPUT CONTROLS
+ ITEM FREQUENCY COMPONENT
+ ALL NONE
+ NSOL ALL
+ RSOL ALL
+ EANG ALL
+ ETMP ALL
+ VENG ALL
+ STRS ALL
+ EPEL ALL
+ EPPL ALL
+ CONT ALL
+
+
+ SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr
+
+
+ *** NOTE *** CP = 0.609 TIME= 19:24:15
+ The PCG solver has automatically set the level of difficulty for this
+ model to 2.
+
+
+ *********** PRECISE MASS SUMMARY ***********
+
+ TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
+ Translational mass | Coupled translational/rotational mass
+ 0.51768E-01 0.0000 0.0000 | 0.0000 -0.39204E-06 -0.10536E-02
+ 0.0000 0.51768E-01 0.0000 | 0.39204E-06 0.0000 -0.32665E-03
+ 0.0000 0.0000 0.51768E-01 | 0.10536E-02 0.32665E-03 0.0000
+ ------------------------------------------ | ------------------------------------------
+ | Rotational mass (inertia)
+ | 0.30371E-04 0.66513E-05 -0.24633E-08
+ | 0.66513E-05 0.47850E-05 0.72554E-08
+ | -0.24633E-08 0.72554E-08 0.34093E-04
+
+ TOTAL MASS = 0.51768E-01
+ The mass principal axes coincide with the global Cartesian axes
+
+ CENTER OF MASS (X,Y,Z)= -0.63100E-02 0.20353E-01 -0.75730E-05
+
+ TOTAL INERTIA ABOUT CENTER OF MASS
+ 0.89267E-05 0.29173E-08 0.10402E-10
+ 0.29173E-08 0.27238E-05 -0.72374E-09
+ 0.10402E-10 -0.72374E-09 0.10587E-04
+ The inertia principal axes coincide with the global Cartesian axes
+
+
+ *** MASS SUMMARY BY ELEMENT TYPE ***
+
+ TYPE MASS
+ 1 0.517676E-01
+
+ Range of element maximum matrix coefficients in global coordinates
+ Maximum = 1.913788161E+09 at element 329.
+ Minimum = 82120380.5 at element 1026.
+
+ *** ELEMENT MATRIX FORMULATION TIMES
+ TYPE NUMBER ENAME TOTAL CP AVE CP
+
+ 1 1540 SOLID187 0.172 0.000112
+ 2 10 SURF154 0.000 0.000000
+ Time at end of element matrix formulation CP = 0.75.
+ Iteration= 10 Ratio= 7.027552E-02 Limit= 1.000000E-08 Wall= 0.0
+ Iteration= 30 Ratio= 7.083987E-04 Limit= 1.000000E-08 Wall= 0.0
+ Iteration= 55 Ratio= 2.090646E-06 Limit= 1.000000E-08 Wall= 0.1
+
+ DISTRIBUTED PCG SOLVER SOLUTION CONVERGED
+
+ DISTRIBUTED PCG SOLVER SOLUTION STATISTICS
+
+ NUMBER OF ITERATIONS= 77
+ NUMBER OF EQUATIONS = 8487
+ LEVEL OF CONVERGENCE= 1
+ CALCULATED NORM = 0.72721E-08
+ SPECIFIED TOLERANCE = 0.10000E-07
+ TOTAL CPU TIME (sec)= 0.08
+ TOTAL WALL TIME(sec)= 0.15
+ TOTAL MEMORY (GB) = 0.00
+
+
+ *** ELEMENT RESULT CALCULATION TIMES
+ TYPE NUMBER ENAME TOTAL CP AVE CP
+
+ 1 1540 SOLID187 0.094 0.000061
+ 2 10 SURF154 0.000 0.000000
+
+ *** NODAL LOAD CALCULATION TIMES
+ TYPE NUMBER ENAME TOTAL CP AVE CP
+
+ 1 1540 SOLID187 0.000 0.000000
+ 2 10 SURF154 0.000 0.000000
+ *** 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
+ 0.812 MB WRITTEN ON RESULTS FILE: file0.rst
+ *************** Write FE CONNECTORS *********
+
+ WRITE OUT CONSTRAINT EQUATIONS TO FILE= file.ce
+ ****************************************************
+ *************** FINISHED SOLVE FOR LS 1 *************
+
+ *GET _WALLASOL FROM ACTI ITEM=TIME WALL VALUE= 19.4041667
+
+ PRINTOUT RESUMED BY /GOP
+
+ *GET _PCGITER FROM ACTI ITEM=SOLU CGIT VALUE= 77.0000000
+
+ FINISH SOLUTION PROCESSING
+
+
+ ***** ROUTINE COMPLETED ***** CP = 1.000
+
+
+
+ *** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2024 R2 24.2 ***
+ Ansys Mechanical Enterprise Academic Student
+ 01055371 VERSION=WINDOWS x64 19:24:15 FEB 02, 2025 CP= 1.000
+
+ structural steel--Static Structural (B5)
+
+
+
+ ***** MAPDL RESULTS INTERPRETATION (POST1) *****
+
+ *** NOTE *** CP = 1.000 TIME= 19:24:15
+ Reading results into the database (SET command) will update the current
+ displacement and force boundary conditions in the database with the
+ values from the results file for that load set. Note that any
+ subsequent solutions will use these values unless action is taken to
+ either SAVE the current values or not overwrite them (/EXIT,NOSAVE).
+
+ Set Encoding of XML File to:ISO-8859-1
+
+ Set Output of XML File to:
+ PARM, , , , , , , , , , , ,
+ , , , , , , ,
+
+ DATABASE WRITTEN ON FILE parm.xml
+
+ EXIT THE MAPDL POST1 DATABASE PROCESSOR
+
+
+ ***** ROUTINE COMPLETED ***** CP = 1.000
+
+
+
+ PRINTOUT RESUMED BY /GOP
+
+ *GET _WALLDONE FROM ACTI ITEM=TIME WALL VALUE= 19.4041667
+
+ PARAMETER _PREPTIME = 0.000000000
+
+ PARAMETER _SOLVTIME = 0.000000000
+
+ PARAMETER _POSTTIME = 0.000000000
+
+ PARAMETER _TOTALTIM = 0.000000000
+
+ *GET _DLBRATIO FROM ACTI ITEM=SOLU DLBR VALUE= 1.00645161
+
+ *GET _COMBTIME FROM ACTI ITEM=SOLU COMB VALUE= 0.167003000E-01
+
+ *GET _SSMODE FROM ACTI ITEM=SOLU SSMM VALUE= 0.00000000
+
+ *GET _NDOFS FROM ACTI ITEM=SOLU NDOF VALUE= 7911.00000
+
+ *GET _SOL_END_TIME FROM ACTI ITEM=SET TIME VALUE= 1.00000000
+
+ *IF _sol_end_time ( = 1.00000 ) EQ
+ 1.000000 ( = 1.00000 ) THEN
+
+ /FCLEAN COMMAND REMOVING ALL LOCAL FILES
+
+ *ENDIF
+ --- Total number of nodes = 2829
+ --- Total number of elements = 1550
+ --- Element load balance ratio = 1.00645161
+ --- Time to combine distributed files = 1.67003E-02
+ --- Sparse memory mode = 0
+ --- Number of DOF = 7911
+
+ EXIT MAPDL WITHOUT SAVING DATABASE
+
+
+ NUMBER OF WARNING MESSAGES ENCOUNTERED= 2
+ NUMBER OF ERROR MESSAGES ENCOUNTERED= 0
+
++--------------------- M A P D L S T A T I S T I C S ------------------------+
+
+Release: 2024 R2 Build: 24.2 Update: UP20240513 Platform: WINDOWS x64
+Date Run: 02/02/2025 Time: 19:24 Process ID: 18388
+Operating System: Windows 10 (Build: 19045)
+
+Processor Model: AMD Ryzen 3 3100 4-Core Processor
+
+Compiler: Intel(R) Fortran Compiler Classic Version 2021.9 (Build: 20230302)
+ Intel(R) C/C++ Compiler Classic Version 2021.9 (Build: 20230302)
+ AOCL-BLAS 4.2.1 Build 20240304
+
+Number of machines requested : 1
+Total number of cores available : 8
+Number of physical cores available : 4
+Number of processes requested : 2
+Number of threads per process requested : 1
+Total number of cores requested : 2 (Distributed Memory Parallel)
+MPI Type: INTELMPI
+MPI Version: Intel(R) MPI Library 2021.11 for Windows* OS
+
+
+GPU Acceleration: Not Requested
+
+Job Name: file0
+Input File: dummy.dat
+
+ Core Machine Name Working Directory
+ -----------------------------------------------------
+ 0 DESKTOP-FJVEEFD C:\Users\Abel Tim\Documents\pws\simulations_V9\_ProjectScratch\ScrAA48
+ 1 DESKTOP-FJVEEFD C:\Users\Abel Tim\Documents\pws\simulations_V9\_ProjectScratch\ScrAA48
+
+Latency time from master to core 1 = 2.883 microseconds
+
+Communication speed from master to core 1 = 3261.94 MB/sec
+
+Total CPU time for main thread : 1.1 seconds
+Total CPU time summed for all threads : 1.3 seconds
+
+Elapsed time spent obtaining a license : 0.5 seconds
+Elapsed time spent pre-processing model (/PREP7) : 0.0 seconds
+Elapsed time spent solution - preprocessing : 0.1 seconds
+Elapsed time spent computing solution : 0.3 seconds
+Elapsed time spent solution - postprocessing : 0.0 seconds
+Elapsed time spent post-processing model (/POST1) : 0.0 seconds
+
+Equation solver used : PCG (symmetric)
+Equation solver computational rate : 4.0 Gflops
+
+Sum of disk space used on all processes : 5.1 MB
+
+Sum of memory used on all processes : 97.0 MB
+Sum of memory allocated on all processes : 2496.0 MB
+Physical memory available : 32 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 R2 Build 24.2 UP20240513 WINDOWS x64 |
+ | |
+ |-----------------------------------------------------------------------------|
+ | |
+ | Database Requested(-db) 1024 MB Scratch Memory Requested 1024 MB |
+ | Max Database Used(Master) 3 MB Max Scratch Used(Master) 47 MB |
+ | Max Database Used(Workers) 1 MB Max Scratch Used(Workers) 46 MB |
+ | Sum Database Used(All) 4 MB Sum Scratch Used(All) 93 MB |
+ | |
+ |-----------------------------------------------------------------------------|
+ | |
+ | CP Time (sec) = 1.297 Time = 19:24:17 |
+ | Elapsed Time (sec) = 4.000 Date = 02/02/2025 |
+ | |
+ *-----------------------------------------------------------------------------*