Hi Leute,
ich habe Ansys Workbench 16.0 installiert. Mein Problem ist, dass ich, wenn ich ein Modell lösen will, folgende Fehlermeldung bekomme:
"Während der Mechanical APDL-Lösung ist ein unbekannter Fehler aufgetreten. Prüfen Sie die Solver-Ausgabe für das Lösungsinformationsobjekt auf mögliche Ursachen."
Hat da jemand Erfahrung oder weiß woran es liegen und wie man es behebt?
Der Ausgabetext des Solvers ist wie folgt:
ANSYS Multiphysics
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* ANSYS Release 16.0 LEGAL NOTICES *
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Release 16.0
Point Releases and Patches installed:
ANSYS, Inc. Products Release 16.0
ANSYS Mechanical Products Release 16.0
ANSYS Autodyn Release 16.0
ANSYS LS-DYNA Release 16.0
ANSYS AIM Release 16.0
ANSYS CFX (includes ANSYS CFD-Post) Release 16.0
ANSYS Fluent (includes ANSYS CFD-Post) Release 16.0
ANSYS TurboGrid Release 16.0
ANSYS Polyflow (includes ANSYS CFD-Post) Release 16.0
ANSYS ICEM CFD Release 16.0
ANSYS Aqwa Release 16.0
ANSYS Composite PrepPost Release 16.0
ANSYS Icepak (includes ANSYS CFD-Post) Release 16.0
Catia, Version 6 Release 16.0
***** ANSYS COMMAND LINE ARGUMENTS *****
BATCH MODE REQUESTED (-b) = NOLIST
INPUT FILE COPY MODE (-c) = COPY
SHARED MEMORY PARALLEL REQUESTED
SINGLE PROCESS WITH 4 THREADS REQUESTED
TOTAL OF 4 CORES REQUESTED
START-UP FILE MODE = NOREAD
STOP FILE MODE = NOREAD
RELEASE= Release 16.0 BUILD= 16.0 UP20141203 VERSION=WINDOWS x64
CURRENT JOBNAME=file 15:27:33 FEB 15, 2016 CP= 1.438
PARAMETER _DS_PROGRESS = 999.0000000
/INPUT FILE= ds.dat LINE= 0
DO NOT WRITE ELEMENT RESULTS INTO DATABASE
*GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 15.4591667
TITLE=
unsaved_project--Statisch-mechanisch (A5)
SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\Adrian\AppData\Local\Temp\WB_ADRIAN_Adrian_1980_2\_ProjectScratch\Scr3DCD\
SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\Adrian\AppData\Local\Temp\WB_ADRIAN_Adrian_1980_2\unsaved_project_files\dp0\SYS\MECH\
SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_USERFILES_DIR(1) = C:\Users\Adrian\AppData\Local\Temp\WB_ADRIAN_Adrian_1980_2\unsaved_project_files\user_files\
--- Data in consistent NMM units. See Solving Units in the help system for more
MPA UNITS SPECIFIED FOR INTERNAL
LENGTH = MILLIMETERS (mm)
MASS = TONNE (Mg)
TIME = SECONDS (sec)
TEMPERATURE = CELSIUS (C)
TOFFSET = 273.0
FORCE = NEWTON (N)
HEAT = MILLIJOULES (mJ)
INPUT UNITS ARE ALSO SET TO MPA
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE Release 16.0 16.0 ***
ANSYS Multiphysics
00000000 VERSION=WINDOWS x64 15:27:33 FEB 15, 2016 CP= 1.547
unsaved_project--Statisch-mechanisch (A5)
***** ANSYS ANALYSIS DEFINITION (PREP7) *****
*********** Nodes for the whole assembly ***********
*********** Elements for Body 1 "FEDERKLAMMER" ***********
*********** Send User Defined Coordinate System(s) ***********
*********** Set Reference Temperature ***********
*********** Send Materials ***********
*********** Fixed Supports ***********
*********** Define Force Using Surface Effect Elements ***********
***** ROUTINE COMPLETED ***** CP = 1.609
--- Number of total nodes = 1879
--- Number of contact elements = 5
--- Number of spring elements = 0
--- Number of bearing elements = 0
--- Number of solid elements = 868
--- Number of total elements = 873
*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 15.4591667
****************************************************************************
************************* SOLUTION ********************************
****************************************************************************
***** ANSYS SOLUTION ROUTINE *****
PERFORM A STATIC ANALYSIS
THIS WILL BE A NEW ANALYSIS
USE SPARSE MATRIX DIRECT SOLVER
CONTACT INFORMATION PRINTOUT LEVEL 1
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 ****************
SELECT FOR ITEM=TYPE COMPONENT=
IN RANGE 2 TO 2 STEP 1
5 ELEMENTS (OF 873 DEFINED) SELECTED BY ESEL COMMAND.
SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.
18 NODES (OF 1879 DEFINED) SELECTED FROM
5 SELECTED ELEMENTS BY NSLE COMMAND.
SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 1 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI30X
SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 2 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI30Y
SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 3 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI30Z
ALL SELECT FOR ITEM=NODE COMPONENT=
IN RANGE 1 TO 1879 STEP 1
1879 NODES (OF 1879 DEFINED) SELECTED BY NSEL COMMAND.
ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 873 STEP 1
873 ELEMENTS (OF 873 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 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
NONLINEAR STABILIZATION CONTROL:
KEY=OFF
*GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000
*IF ANSINTER_ ( = 0.00000 ) NE
0 ( = 0.00000 ) THEN
*ENDIF
***** ANSYS SOLVE COMMAND *****
*** WARNING *** CP = 1.609 TIME= 15:27:33
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** NOTE *** CP = 1.609 TIME= 15:27:33
The model data was checked and warning messages were found.
Please review output or errors file (
C:\Users\Adrian\AppData\Local\Temp\WB_ADRIAN_Adrian_1980_2\_ProjectScra
atch\Scr3DCD\file.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.
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE Release 16.0 16.0 ***
ANSYS Multiphysics
00000000 VERSION=WINDOWS x64 15:27:33 FEB 15, 2016 CP= 1.609
unsaved_project--Statisch-mechanisch (A5)
S O L U T I O N O P T I O N S
PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
DEGREES OF FREEDOM. . . . . . UX UY UZ
ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC
*** WARNING *** CP = 1.609 TIME= 15:27:33
Material number 2 (used by element 869 ) 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 = 1.656 TIME= 15:27:33
The step data was checked and warning messages were found.
Please review output or errors file (
C:\Users\Adrian\AppData\Local\Temp\WB_ADRIAN_Adrian_1980_2\_ProjectScra
atch\Scr3DCD\file.err ) for these warning messages.
*** NOTE *** CP = 1.656 TIME= 15:27:33
The conditions for direct assembly have been met. No .emat or .erot
files will be produced.
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
STRS ALL
EPEL ALL
EPPL ALL
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr
*********** PRECISE MASS SUMMARY ***********
TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
Translational mass | Coupled translational/rotational mass
0.12072E-06 0.0000 0.0000 | 0.0000 0.10131E-06 -0.64417E-07
0.0000 0.12072E-06 0.0000 | -0.10131E-06 0.0000 0.88739E-13
0.0000 0.0000 0.12072E-06 | 0.64417E-07 -0.88739E-13 0.0000
------------------------------------------ | ------------------------------------------
| Rotational mass (inertia)
| 0.82317E-06 0.74912E-12 0.73075E-12
| 0.74912E-12 0.59399E-05 -0.10832E-06
| 0.73075E-12 -0.10832E-06 0.52307E-05
TOTAL MASS = 0.12072E-06
The mass principal axes coincide with the global Cartesian axes
CENTER OF MASS (X,Y,Z)= 0.73506E-06 0.53360 0.83922
TOTAL INERTIA ABOUT CENTER OF MASS
0.70377E-06 0.79647E-12 0.80522E-12
0.79647E-12 0.58549E-05 -0.54258E-07
0.80522E-12 -0.54258E-07 0.51964E-05
PRINCIPAL INERTIAS = 0.70377E-06 0.58593E-05 0.51919E-05
ORIENTATION VECTORS OF THE INERTIA PRINCIPAL AXES IN GLOBAL CARTESIAN
( 1.000,-0.000,-0.000) ( 0.000, 0.997,-0.082) ( 0.000, 0.082, 0.997)
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.120723E-06
Range of element maximum matrix coefficients in global coordinates
Maximum = 1253281.58 at element 645.
Minimum = 12805.4317 at element 326.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 868 SOLID187 0.688 0.000792
2 5 SURF154 0.000 0.000000
Time at end of element matrix formulation CP = 2.140625.
SPARSE MATRIX DIRECT SOLVER.
Number of equations = 5169, Maximum wavefront = 276
Memory allocated for solver = 24.336 MB
Memory required for in-core = 6.833 MB
Memory required for out-of-core = 2.126 MB
*** NOTE *** CP = 2.562 TIME= 15:27:33
The 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.
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