-
-
April 21, 2023 at 12:58 pm
Xabier Tamayo
SubscriberHi everyone, Im trying a really simple modal simulation, but it always gives me an error message. I have tried to find out what the error is using the output solver, but I still don't know what it is. I attach some screenshots and the solver output.
And the output solver says the next:
Ansys Mechanical Enterprise Academic Teaching
*------------------------------------------------------------------*
| |
| 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 2022 R1 LEGAL NOTICES *
***************************************************************
* *
* Copyright 1971-2022 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). *
* *
***************************************************************
2022 R1
Point Releases and Patches installed:
ANSYS, Inc. License Manager 2022 R1
Ansys, Inc. Products 2022 R1
SpaceClaim 2022 R1
CFX (includes CFD-Post) 2022 R1
Chemkin 2022 R1
EnSight 2022 R1
FENSAP-ICE 2022 R1
Fluent (includes CFD-Post) 2022 R1
Polyflow (includes CFD-Post) 2022 R1
Forte (includes EnSight) 2022 R1
TurboGrid 2022 R1
Icepak (includes CFD-Post) 2022 R1
ACIS Geometry Interface 2022 R1
AutoCAD Geometry Interface 2022 R1
Catia, Version 4 Geometry Interface 2022 R1
Catia, Version 5 Geometry Interface 2022 R1
Catia, Version 6 Geometry Interface 2022 R1
Creo Elements/Direct Modeling Geometry Interface 2022 R1
Creo Parametric Geometry Interface 2022 R1
Inventor Geometry Interface 2022 R1
JTOpen Geometry Interface 2022 R1
NX Geometry Interface 2022 R1
Parasolid Geometry Interface 2022 R1
Solid Edge Geometry Interface 2022 R1
SOLIDWORKS Geometry Interface 2022 R1
Ansys Sherlock 2022 R1
Autodyn 2022 R1
LS-DYNA 2022 R1
Aqwa 2022 R1
Additive 2022 R1
Mechanical Products 2022 R1
***** ANSYS COMMAND LINE ARGUMENTS *****
BATCH MODE REQUESTED (-b) = NOLIST
INPUT FILE COPY MODE (-c) = COPY
DISTRIBUTED MEMORY PARALLEL REQUESTED
2 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS
TOTAL OF 2 CORES REQUESTED
INPUT FILE NAME = \\dcloud.local\public\018\018_xabier.tamayo\Desktop\Ansys pruebas\_ProjectScratch\Scr1F42\dummy.dat
OUTPUT FILE NAME = \\dcloud.local\public\018\018_xabier.tamayo\Desktop\Ansys pruebas\_ProjectScratch\Scr1F42\solve.out
START-UP FILE MODE = NOREAD
STOP FILE MODE = NOREAD
RELEASE= 2022 R1 BUILD= 22.1 UP20211129 VERSION=WINDOWS x64
CURRENT JOBNAME=file0 14:53:35 APR 21, 2023 CP= 0.109
PARAMETER _DS_PROGRESS = 999.0000000
/INPUT FILE= ds.dat LINE= 0
*** NOTE *** CP = 0.219 TIME= 14:53:35
The /CONFIG,NOELDB command is not valid in a Distributed ANSYS
solution. Command is ignored.
*GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 14.8930556
TITLE=
Modal_piezasolid--Modal (A5)
ACT Extensions:
LSDYNA, 2021.1
5f463412-bd3e-484b-87e7-cbc0a665e474, wbex
SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_PROJECTSCRATCH_DIR(1) = \\dcloud.local\public\018\018_xabier.tamayo\Desktop\Ansys pruebas\_ProjectScratch\Scr1F42\
SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_SOLVERFILES_DIR(1) = \\dcloud.local\public\018\018_xabier.tamayo\Desktop\Ansys pruebas\Modal_piezasolid_files\dp0\SYS\MECH\
SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_USERFILES_DIR(1) = \\dcloud.local\public\018\018_xabier.tamayo\Desktop\Ansys pruebas\Modal_piezasolid_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
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Teaching
00000000 VERSION=WINDOWS x64 14:53:35 APR 21, 2023 CP= 0.219
Modal_piezasolid--Modal (A5)
***** ANSYS ANALYSIS DEFINITION (PREP7) *****
*********** Nodes for the whole assembly ***********
*********** Elements for Body 1 "Part 1" ***********
*********** Send User Defined Coordinate System(s) ***********
*********** Set Reference Temperature ***********
*********** Send Materials ***********
*********** Fixed Supports ***********
***** ROUTINE COMPLETED ***** CP = 0.234
--- Number of total nodes = 1370
--- Number of contact elements = 0
--- Number of spring elements = 0
--- Number of bearing elements = 0
--- Number of solid elements = 156
--- Number of condensed parts = 0
--- Number of total elements = 156
*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 14.8930556
***** ANSYS SOLUTION ROUTINE *****
PERFORM A MODAL ANALYSIS
THIS WILL BE A NEW ANALYSIS
PARAMETER _THICKRATIO = 0.000000000
USE SYM. BLOCK LANCZOS MODE EXTRACTION METHOD
EXTRACT 7 MODES
NORMALIZE THE MODE SHAPES TO THE MASS MATRIX
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 ETMP ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR ALL APPLICABLE ENTITIES
EXPAND ALL EXTRACTED MODES
DO NOT CALCULATE ELEMENT RESULTS
DO NOT COMBINE ELEMENT SAVE DATA FILES (.esav) AFTER DISTRIBUTED PARALLEL SOLUTION
DO NOT COMBINE ELEMENT MATRIX FILES (.emat) AFTER DISTRIBUTED PARALLEL SOLUTION
DO NOT COMBINE ASSEMBLED MATRIX FILES (.full) AFTER DISTRIBUTED PARALLEL SOLUTION
*GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000
*IF ANSINTER_ ( = 0.00000 ) NE
0 ( = 0.00000 ) THEN
*ENDIF
*** NOTE *** CP = 0.266 TIME= 14:53:35
The automatic domain decomposition logic has selected the MESH domain
decomposition method with 2 processes per solution.
***** ANSYS SOLVE COMMAND *****
*** WARNING *** CP = 0.266 TIME= 14:53:35
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** NOTE *** CP = 0.281 TIME= 14:53:35
The model data was checked and warning messages were found.
Please review output or errors file (
\\dcloud.local\public\018\018_xabier.tamayo\Desktop\Ansys
pruebas\_ProjectScratch\Scr1F42\file0.err ) for these warning
messages.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Teaching
00000000 VERSION=WINDOWS x64 14:53:35 APR 21, 2023 CP= 0.281
Modal_piezasolid--Modal (A5)
S O L U T I O N O P T I O N S
PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
DEGREES OF FREEDOM. . . . . . UX UY UZ
ANALYSIS TYPE . . . . . . . . . . . . . . . . .MODAL
EXTRACTION METHOD. . . . . . . . . . . . . .BLOCK LANCZOS
OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
NUMBER OF MODES TO EXTRACT. . . . . . . . . . . 7
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC
NUMBER OF MODES TO EXPAND . . . . . . . . . . .ALL
ELEMENT RESULTS CALCULATION . . . . . . . . . .OFF
*** NOTE *** CP = 0.281 TIME= 14:53:35
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: 156
...Number of nodes: 1370
...Decompose to 2 CPU domains
...Element load balance ratio = 1.000
L O A D S T E P O P T I O N S
LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1
THERMAL STRAINS INCLUDED IN THE LOAD VECTOR . . YES
PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
DATABASE OUTPUT CONTROLS
ITEM FREQUENCY COMPONENT
ALL NONE
NSOL ALL
ETMP ALL
*********** PRECISE MASS SUMMARY ***********
TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
Translational mass | Coupled translational/rotational mass
0.91539E-02 0.0000 0.0000 | 0.0000 0.27736E-05 -0.45312E-04
0.0000 0.91539E-02 0.0000 | -0.27736E-05 0.0000 0.91539E-03
0.0000 0.0000 0.91539E-02 | 0.45312E-04 -0.91539E-03 0.0000
------------------------------------------ | ------------------------------------------
| Rotational mass (inertia)
| 0.30018E-06 -0.45312E-05 -0.27736E-06
| -0.45312E-05 0.12205E-03 -0.13729E-07
| -0.27736E-06 -0.13729E-07 0.12235E-03
TOTAL MASS = 0.91539E-02
The mass principal axes coincide with the global Cartesian axes
CENTER OF MASS (X,Y,Z)= 0.10000 0.49500E-02 0.30300E-03
TOTAL INERTIA ABOUT CENTER OF MASS
0.75044E-07 0.35662E-20 0.29390E-21
0.35662E-20 0.30513E-04 0.81169E-23
0.29390E-21 0.81169E-23 0.30588E-04
The inertia principal axes coincide with the global Cartesian axes
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.915388E-02
Range of element maximum matrix coefficients in global coordinates
Maximum = 2.90253469E+09 at element 103.
Minimum = 2.90253454E+09 at element 100.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 156 SOLID186 0.000 0.000000
Time at end of element matrix formulation CP = 0.484375.
BLOCK LANCZOS CALCULATION OF UP TO 7 EIGENVECTORS.
NUMBER OF EQUATIONS = 4056
MAXIMUM WAVEFRONT = 153
MAXIMUM MODES STORED = 7
MINIMUM EIGENVALUE = 0.00000E+00
MAXIMUM EIGENVALUE = 0.10000E+31
Process memory allocated for solver = 6.656 MB
Process memory required for in-core solution = 6.346 MB
Process memory required for out-of-core solution = 3.976 MB
Total memory allocated for solver = 13.364 MB
Total memory required for in-core solution = 12.741 MB
Total memory required for out-of-core solution = 7.949 MB
*** NOTE *** CP = 0.703 TIME= 14:53:35
The Distributed Sparse Matrix Solver used by the Block Lanczos
eigensolver 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.
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Teaching
00000000 VERSION=WINDOWS x64 14:53:35 APR 21, 2023 CP= 0.781
Modal_piezasolid--Modal (A5)
*** FREQUENCIES FROM BLOCK LANCZOS ITERATION ***
MODE FREQUENCY (HERTZ)
1 11.71618911070
2 73.41753812852
3 190.2039651007
4 205.5969093043
5 403.0167525196
6 450.9853165402
7 666.5432548624
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Teaching
00000000 VERSION=WINDOWS x64 14:53:36 APR 21, 2023 CP= 0.797
Modal_piezasolid--Modal (A5)
***** PARTICIPATION FACTOR CALCULATION ***** X DIRECTION
CUMULATIVE RATIO EFF.MASS
MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS
1 11.7162 0.85352E-01 0.0000 0.000000 0.00000 0.00000 0.00000
2 73.4175 0.13621E-01 0.0000 0.000000 0.00000 0.00000 0.00000
3 190.204 0.52575E-02 0.0000 0.000000 0.00000 0.00000 0.00000
4 205.597 0.48639E-02 0.0000 0.000000 0.00000 0.00000 0.00000
5 403.017 0.24813E-02 0.0000 0.000000 0.00000 0.00000 0.00000
6 450.985 0.22174E-02 0.0000 0.000000 0.00000 0.00000 0.00000
7 666.543 0.15003E-02 0.0000 0.000000 0.00000 0.00000 0.00000
***** PARTICIPATION FACTOR CALCULATION ***** Y DIRECTION
CUMULATIVE RATIO EFF.MASS
MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS
1 11.7162 0.85352E-01 0.0000 0.000000 0.00000 0.00000 0.00000
2 73.4175 0.13621E-01 0.0000 0.000000 0.00000 0.00000 0.00000
3 190.204 0.52575E-02 0.74898E-01 1.000000 0.560975E-02 1.00000 0.612828
4 205.597 0.48639E-02 0.0000 0.000000 0.00000 1.00000 0.00000
5 403.017 0.24813E-02 0.0000 0.000000 0.00000 1.00000 0.00000
6 450.985 0.22174E-02 0.0000 0.000000 0.00000 1.00000 0.00000
7 666.543 0.15003E-02 0.0000 0.000000 0.00000 1.00000 0.00000
-----------------------------------------------------------------------------------------------------------------
sum 0.560975E-02 0.612828
-----------------------------------------------------------------------------------------------------------------
***** PARTICIPATION FACTOR CALCULATION ***** Z DIRECTION
CUMULATIVE RATIO EFF.MASS
MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS
1 11.7162 0.85352E-01 0.74819E-01 1.000000 0.559793E-02 0.666584 0.611536
2 73.4175 0.13621E-01 -0.41479E-01 0.554393 0.172053E-02 0.871460 0.187956
3 190.204 0.52575E-02 0.0000 0.000000 0.00000 0.871460 0.00000
4 205.597 0.48639E-02 0.24338E-01 0.325287 0.592328E-03 0.941992 0.647078E-01
5 403.017 0.24813E-02 -0.17416E-01 0.232769 0.303305E-03 0.978109 0.331340E-01
6 450.985 0.22174E-02 0.0000 0.000000 0.00000 0.978109 0.00000
7 666.543 0.15003E-02 0.13559E-01 0.181220 0.183840E-03 1.00000 0.200833E-01
-----------------------------------------------------------------------------------------------------------------
sum 0.839793E-02 0.917417
-----------------------------------------------------------------------------------------------------------------
***** PARTICIPATION FACTOR CALCULATION *****ROTX DIRECTION
CUMULATIVE RATIO EFF.MASS
MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS
1 11.7162 0.85352E-01 0.37036E-03 1.000000 0.137163E-06 0.514958 0.456940
2 73.4175 0.13621E-01 -0.20532E-03 0.554393 0.421573E-07 0.673231 0.140441
3 190.204 0.52575E-02 -0.22694E-04 0.061277 0.515026E-09 0.675164 0.171573E-02
4 205.597 0.48639E-02 0.12047E-03 0.325287 0.145135E-07 0.729653 0.483497E-01
5 403.017 0.24813E-02 -0.86207E-04 0.232769 0.743173E-08 0.757554 0.247577E-01
6 450.985 0.22174E-02 0.24510E-03 0.661790 0.600728E-07 0.983088 0.200124
7 666.543 0.15003E-02 0.67116E-04 0.181220 0.450455E-08 1.00000 0.150063E-01
-----------------------------------------------------------------------------------------------------------------
sum 0.266358E-06 0.887334
-----------------------------------------------------------------------------------------------------------------
***** PARTICIPATION FACTOR CALCULATION *****ROTY DIRECTION
CUMULATIVE RATIO EFF.MASS
MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS
1 11.7162 0.85352E-01 -0.40827E-02 0.623871 0.166685E-04 0.177793 0.136568
2 73.4175 0.13621E-01 0.65441E-02 1.000000 0.428259E-04 0.634591 0.350880
3 190.204 0.52575E-02 0.0000 0.000000 0.00000 0.634591 0.00000
4 205.597 0.48639E-02 -0.42373E-02 0.647492 0.179546E-04 0.826102 0.147105
5 403.017 0.24813E-02 0.31592E-02 0.482753 0.998059E-05 0.932559 0.817726E-01
6 450.985 0.22174E-02 0.0000 0.000000 0.00000 0.932559 0.00000
7 666.543 0.15003E-02 -0.25145E-02 0.384239 0.632278E-05 1.00000 0.518036E-01
-----------------------------------------------------------------------------------------------------------------
sum 0.937523E-04 0.768129
-----------------------------------------------------------------------------------------------------------------
***** PARTICIPATION FACTOR CALCULATION *****ROTZ DIRECTION
CUMULATIVE RATIO EFF.MASS
MODE FREQUENCY PERIOD PARTIC.FACTOR RATIO EFFECTIVE MASS MASS FRACTION TO TOTAL MASS
1 11.7162 0.85352E-01 0.0000 0.000000 0.00000 0.00000 0.00000
2 73.4175 0.13621E-01 0.0000 0.000000 0.00000 0.00000 0.00000
3 190.204 0.52575E-02 0.40917E-02 1.000000 0.167416E-04 1.00000 0.136833
4 205.597 0.48639E-02 0.0000 0.000000 0.00000 1.00000 0.00000
5 403.017 0.24813E-02 0.0000 0.000000 0.00000 1.00000 0.00000
6 450.985 0.22174E-02 0.0000 0.000000 0.00000 1.00000 0.00000
7 666.543 0.15003E-02 0.0000 0.000000 0.00000 1.00000 0.00000
-----------------------------------------------------------------------------------------------------------------
sum 0.167416E-04 0.136833
-----------------------------------------------------------------------------------------------------------------
*** NOTE *** CP = 0.797 TIME= 14:53:36
The modes requested are mass normalized (Nrmkey on MODOPT). However,
the modal masses and kinetic energies below are calculated with unit
normalized modes.
***** MODAL MASSES, KINETIC ENERGIES, AND TRANSLATIONAL EFFECTIVE MASSES SUMMARY *****
EFFECTIVE MASS
MODE FREQUENCY MODAL MASS KENE | X-DIR RATIO% Y-DIR RATIO% Z-DIR RATIO%
1 11.72 0.2283E-02 6.185 | 0.000 0.00 0.000 0.00 0.5598E-02 61.15
2 73.42 0.2283E-02 242.9 | 0.000 0.00 0.000 0.00 0.1721E-02 18.80
3 190.2 0.2293E-02 1637. | 0.000 0.00 0.5610E-02 61.28 0.000 0.00
4 205.6 0.2282E-02 1904. | 0.000 0.00 0.000 0.00 0.5923E-03 6.47
5 403.0 0.2281E-02 7314. | 0.000 0.00 0.000 0.00 0.3033E-03 3.31
6 451.0 0.1511E-02 6065. | 0.000 0.00 0.000 0.00 0.000 0.00
7 666.5 0.2279E-02 0.1999E+05 | 0.000 0.00 0.000 0.00 0.1838E-03 2.01
--------------------------------------------------------------------------------------------------------------
sum | 0.000 0.00 0.5610E-02 61.28 0.8398E-02 91.74
--------------------------------------------------------------------------------------------------------------
*** ANSYS BINARY FILE STATISTICS
BUFFER SIZE USED= 16384
1.688 MB WRITTEN ON ASSEMBLED MATRIX FILE: file0.full
0.125 MB WRITTEN ON MODAL MATRIX FILE: file0.mode
0.500 MB WRITTEN ON RESULTS FILE: file0.rst
*************** Write FE CONNECTORS *********
WRITE OUT CONSTRAINT EQUATIONS TO FILE= file.ce
*GET _NMODALSOLPROC FROM ACTI ITEM=NUMC VALUE= 2.00000000
FINISH SOLUTION PROCESSING
***** ROUTINE COMPLETED ***** CP = 0.906
PRINTOUT RESUMED BY /GOP
*GET _WALLASOL FROM ACTI ITEM=TIME WALL VALUE= 14.8933333
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R1 22.1 ***
DISTRIBUTED Ansys Mechanical Enterprise Academic Teaching
00000000 VERSION=WINDOWS x64 14:53:36 APR 21, 2023 CP= 0.906
Modal_piezasolid--Modal (A5)
***** ANSYS RESULTS INTERPRETATION (POST1) *****
*** NOTE *** CP = 0.969 TIME= 14:53:36
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).
PRINTOUT RESUMED BY /GOP
Set Encoding of XML File to:ISO-8859-1
Set Output of XML File to:
PARM, , , , , , , , , , , ,
, , , , , , ,
DATABASE WRITTEN ON FILE parm.xml
EXIT THE ANSYS POST1 DATABASE PROCESSOR
***** ROUTINE COMPLETED ***** CP = 1.141
PRINTOUT RESUMED BY /GOP
*GET _WALLDONE FROM ACTI ITEM=TIME WALL VALUE= 14.8933333
PARAMETER _PREPTIME = 0.000000000
PARAMETER _SOLVTIME = 1.000000000
PARAMETER _POSTTIME = 0.000000000
PARAMETER _TOTALTIM = 1.000000000
*GET _DLBRATIO FROM ACTI ITEM=SOLU DLBR VALUE= 1.00000000
*GET _COMBTIME FROM ACTI ITEM=SOLU COMB VALUE= 0.186647900
*GET _SSMODE FROM ACTI ITEM=SOLU SSMM VALUE= 2.00000000
*GET _NDOFS FROM ACTI ITEM=SOLU NDOF VALUE= 4056.00000
/FCLEAN COMMAND REMOVING ALL LOCAL FILES
--- Total number of nodes = 1370
--- Total number of elements = 156
--- Element load balance ratio = 1
--- Time to combine distributed files = 0.1866479
--- Sparse memory mode = 2
--- Number of DOF = 4056
EXIT ANSYS WITHOUT SAVING DATABASE
NUMBER OF WARNING MESSAGES ENCOUNTERED= 1
NUMBER OF ERROR MESSAGES ENCOUNTERED= 0
+--------- D I S T R I B U T E D A N S Y S S T A T I S T I C S ------------+
Release: 2022 R1 Build: 22.1 Update: UP20211129 Platform: WINDOWS x64
Date Run: 04/21/2023 Time: 14:53 Process ID: 10464
Operating System: Windows 10 (Build: 19042)
Processor Model: Intel(R) Xeon(R) Gold 6240R CPU @ 2.40GHz
Compiler: Intel(R) Fortran Compiler Version 19.0.5 (Build: 20190815)
Intel(R) C/C++ Compiler Version 19.0.5 (Build: 20190815)
Intel(R) Math Kernel Library Version 2020.0.0 Product Build 20191125
BLAS Library supplied by Intel(R) MKL
Number of machines requested : 1
Total number of cores available : 4
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 2019 Update 10 for Windows* OS
GPU Acceleration: Not Requested
Job Name: file0
Input File: dummy.dat
Core Machine Name Working Directory
-----------------------------------------------------
0 AB018IND038 \\dcloud.local\public\018\018_xabier.tamayo\Desktop\Ansys pruebas\_ProjectScratch\Scr1F42
1 AB018IND038 \\dcloud.local\public\018\018_xabier.tamayo\Desktop\Ansys pruebas\_ProjectScratch\Scr1F42
Latency time from master to core 1 = 8.192 microseconds
Communication speed from master to core 1 = 5838.61 MB/sec
Total CPU time for main thread : 1.3 seconds
Total CPU time summed for all threads : 1.5 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 : 0.0 seconds
Elapsed time spent computing solution : 0.4 seconds
Elapsed time spent solution - postprocessing : 0.2 seconds
Elapsed time spent post-processing model (/POST1) : 0.3 seconds
Eigensolver used : Block Lanczos
Equation solver computational rate : 4.8 Gflops
Sum of memory used on all processes : 92.0 MB
Sum of memory allocated on all processes : 3136.0 MB
Physical memory available : 16 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 D I S T R I B U T E D A N S Y S S T A T I S T I C S -------+
*---------------------------------------------------------------------------*
| |
| DISTRIBUTED ANSYS RUN COMPLETED |
| |
|---------------------------------------------------------------------------|
| |
| Ansys 2022 R1 Build 22.1 UP20211129 WINDOWS x64 |
| |
|---------------------------------------------------------------------------|
| |
| Database Requested(-db) 1024 MB Scratch Memory Requested 1024 MB |
| Maximum Database Used 1 MB Maximum Scratch Memory Used 45 MB |
| |
|---------------------------------------------------------------------------|
| |
| CP Time (sec) = 1.516 Time = 14:53:37 |
| Elapsed Time (sec) = 4.000 Date = 04/21/2023 |
| |
*---------------------------------------------------------------------------* -
April 21, 2023 at 1:25 pm
ErKo
Ansys EmployeeHi
So it is solving as you can see (frequencies are there and no errors), so there is something when opening results. Likely the result file does not exist or is not written (.rst file).
Can you clear solution and data and untick the distributed solve box when solving, and solve again.
If that does not work, try not to use any cloud related services/folders, just solve it locally on your lapotop/desktop.
Thank you
Erik
-
April 21, 2023 at 5:59 pm
Xabier Tamayo
SubscriberI opened it again from another remote and this time it worked. Thank you very much.
-
- The topic ‘Error: An unknown error occurred during solution’ is closed to new replies.
-
4607
-
1510
-
1386
-
1209
-
1021
© 2025 Copyright ANSYS, Inc. All rights reserved.
