CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS

Ansys SIG$ILL error

Register Blogs Members List Search Today's Posts Mark Forums Read

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   November 21, 2015, 15:58
Default Ansys SIG$ILL error
  #1
New Member
 
Join Date: Nov 2015
Posts: 2
Rep Power: 0
loth is on a distinguished road
Hi
today i've installed Ansys on my personal machine and I accured strange error that i've never seen before

*** ERROR *** CP = 1.797 TIME= 21:35:31
An unexpected error ( SIG$ILL ) has occurred... ANSYS internal data
has been corrupted. ANSYS is unable to recover and will terminate.
Previously saved files are unaffected. Please send the data leading
to this operation to your technical support provider, as this will
allow ANSYS, Inc to improve the program.



anyone got idea what is it about ?


here is all solver output worksheet


ANSYS Multiphysics


*------------------------------------------------------------------*
| |
| 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 Release 16.0 LEGAL NOTICES *
************************************************** *************
* *
* Copyright 2014 SAS IP, 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 9001:2008 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). *
* *
************************************************** *************

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 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, Inc. License Manager 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 2 THREADS REQUESTED
TOTAL OF 2 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 21:35:30 NOV 21, 2015 CP= 1.359


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= 21.5916667

TITLE=
wchuj--Static Structural (A5)


SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR
TYPE=STRI DIMENSIONS= 248 1 1

PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\loth\Desktop\idzpanwchuj\_ProjectScratch\ ScrA490\

SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1

PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\loth\Desktop\idzpanwchuj\wchuj_files\dp0\ SYS\MECH\

SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1

PARAMETER _WB_USERFILES_DIR(1) = C:\Users\loth\Desktop\idzpanwchuj\wchuj_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 Release 16.0 16.0 ***
ANSYS Multiphysics
00000000 VERSION=WINDOWS x64 21:35:30 NOV 21, 2015 CP= 1.438

wchuj--Static Structural (A5)



***** ANSYS ANALYSIS DEFINITION (PREP7) *****
*********** Nodes for the whole assembly ***********
*********** Elements for Body 1 "Line Body" ***********
*********** Elements for Body 2 "Line Body" ***********
*********** Elements for Body 3 "Line Body" ***********
*********** Send User Defined Coordinate System(s) ***********
*********** Set Reference Temperature ***********
*********** Send Materials ***********
*********** Send Beam Properties ***********
******* Constant Zero Displacement X *******
******* Constant Zero Displacement Y *******
******* Constant Zero Displacement Z *******
*********** Define Line Pressure Vector Using Surface Effect Elements *********
*********** Define Vertex Force Using Follower Elements ***********
*********** Define Vertex Moment Using Follower Elements ***********
*********** Create Remote Point "Internal Remote Point" ***********
*********** Create Remote Point "Internal Remote Point 2" ***********
*********** Create Remote Point "Internal Remote Point 3" ***********
*********** Create Remote Point "Internal Remote Point 4" ***********
*********** Create Joint "Revolute - Line Body To Line Body" ***********
Real Constant Set For Above Joint Is 15
*********** Create Joint "Revolute - Line Body To Line Body" ***********
Real Constant Set For Above Joint Is 16


***** ROUTINE COMPLETED ***** CP = 1.469


--- Number of total nodes = 602
--- Number of contact elements = 40
--- Number of spring elements = 0
--- Number of bearing elements = 0
--- Number of solid elements = 297
--- Number of total elements = 353

*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 21.5916667
************************************************** **************************
************************* 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 4 TO 4 STEP 1

40 ELEMENTS (OF 353 DEFINED) SELECTED BY ESEL COMMAND.

SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.

41 NODES (OF 602 DEFINED) SELECTED FROM
40 SELECTED ELEMENTS BY NSLE COMMAND.

SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 1 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI63X

SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 2 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI63Y

SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 3 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI63Z

ALL SELECT FOR ITEM=NODE COMPONENT=
IN RANGE 1 TO 602 STEP 1

602 NODES (OF 602 DEFINED) SELECTED BY NSEL COMMAND.

ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 358 STEP 1

353 ELEMENTS (OF 353 DEFINED) SELECTED BY ESEL COMMAND.

SELECT FOR ITEM=REAL COMPONENT=
IN RANGE 5 TO 5 STEP 1

1 ELEMENTS (OF 353 DEFINED) SELECTED BY ESEL COMMAND.

SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 1 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI61X

SELECT FOR ITEM=REAL COMPONENT=
IN RANGE 6 TO 6 STEP 1

1 ELEMENTS (OF 353 DEFINED) SELECTED BY ESEL COMMAND.

SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 1 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI61Y

SELECT FOR ITEM=REAL COMPONENT=
IN RANGE 7 TO 7 STEP 1

1 ELEMENTS (OF 353 DEFINED) SELECTED BY ESEL COMMAND.

SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 1 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI61Z

ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 358 STEP 1

353 ELEMENTS (OF 353 DEFINED) SELECTED BY ESEL COMMAND.

SELECT FOR ITEM=REAL COMPONENT=
IN RANGE 8 TO 8 STEP 1

1 ELEMENTS (OF 353 DEFINED) SELECTED BY ESEL COMMAND.

SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 2 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI65X

SELECT FOR ITEM=REAL COMPONENT=
IN RANGE 9 TO 9 STEP 1

1 ELEMENTS (OF 353 DEFINED) SELECTED BY ESEL COMMAND.

SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 2 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI65Y

SELECT FOR ITEM=REAL COMPONENT=
IN RANGE 10 TO 10 STEP 1

1 ELEMENTS (OF 353 DEFINED) SELECTED BY ESEL COMMAND.

SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 2 KVAL = 1
SET ACCORDING TO TABLE PARAMETER = _LOADVARI65Z

ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 358 STEP 1

353 ELEMENTS (OF 353 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

PRINTOUT RESUMED BY /GOP

WRITE MISC ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR THE ENTITIES DEFINED BY COMPONENT _ELMISC

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 = 1.469 TIME= 21:35:30
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.

*** WARNING *** CP = 1.484 TIME= 21:35:30
MPC184 elements are being used in the current analysis and the
NLGEOM,ON command has not been used. Thus, only linearized behavior
will be considered. If finite rotation and large deflection effects
are to be considered, please use the NLGEOM,ON command.

*** NOTE *** CP = 1.484 TIME= 21:35:30
The model data was checked and warning messages were found.
Please review output or errors file (
C:\Users\loth\Desktop\idzpanwchuj\_ProjectScratch\ ScrA490\file.err )
for these warning messages.

*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---

ELEMENT TYPE 1 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

ELEMENT TYPE 1 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
RESETTING IS NEEDED.

ELEMENT TYPE 2 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

ELEMENT TYPE 2 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
RESETTING IS NEEDED.

ELEMENT TYPE 3 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

ELEMENT TYPE 3 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
RESETTING IS NEEDED.



*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE Release 16.0 16.0 ***
ANSYS Multiphysics
00000000 VERSION=WINDOWS x64 21:35:30 NOV 21, 2015 CP= 1.484

wchuj--Static Structural (A5)



S O L U T I O N O P T I O N S

PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
DEGREES OF FREEDOM. . . . . . UX UY UZ ROTX ROTY ROTZ
ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC

*** WARNING *** CP = 1.484 TIME= 21:35:30
Material number 15 (used by element 298 ) 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 = 1.484 TIME= 21:35:30
The step data was checked and warning messages were found.
Please review output or errors file (
C:\Users\loth\Desktop\idzpanwchuj\_ProjectScratch\ ScrA490\file.err )
for these warning messages.

*** NOTE *** CP = 1.484 TIME= 21:35:30
Internal nodes from 603 to 909 are created.
4 internal nodes are used for handling degrees of freedom on pilot
nodes of rigid target surfaces.
6 internal nodes are used for non-contact elements with mixed
formulation.
297 internal nodes are used for quadratic and/or cubic options of
BEAM188, PIPE288, and/or SHELL208.

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
MISC ALL _ELMISC
loth is offline   Reply With Quote

Old   November 21, 2015, 15:59
Default rest of the worksheet
  #2
New Member
 
Join Date: Nov 2015
Posts: 2
Rep Power: 0
loth is on a distinguished road
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr

*** NOTE *** CP = 1.516 TIME= 21:35:30
It is highly recommended to use the auto contact setting option by
issuing CNCHECK,AUTO command for this problem in order to achieve
better convergence.

*** NOTE *** CP = 1.516 TIME= 21:35:30
Rigid target surface identified by real constant set 11. The degrees
of freedom of the rigid surface are driven by the pilot node 598.
Internal MPC will be built.
Boundary conditions can be applied on any target node.
The rigid surface does not overlap other elements.
The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ
****************************************


*** NOTE *** CP = 1.516 TIME= 21:35:30
Rigid target surface identified by real constant set 12. The degrees
of freedom of the rigid surface are driven by the pilot node 599.
Internal MPC will be built.
Boundary conditions can be applied on any target node.
The rigid surface does not overlap other elements.
The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ
****************************************


*** NOTE *** CP = 1.516 TIME= 21:35:30
Rigid target surface identified by real constant set 13. The degrees
of freedom of the rigid surface are driven by the pilot node 600.
Internal MPC will be built.
Boundary conditions can be applied on any target node.
The rigid surface does not overlap other elements.
The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ
****************************************


*** NOTE *** CP = 1.516 TIME= 21:35:30
Rigid target surface identified by real constant set 14. The degrees
of freedom of the rigid surface are driven by the pilot node 601.
Internal MPC will be built.
Boundary conditions can be applied on any target node.
The rigid surface does not overlap other elements.
The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ
****************************************




*** NOTE *** CP = 1.516 TIME= 21:35:30
Predictor is ON by default for structural elements with rotational
degrees of freedom. Use the PRED,OFF command to turn the predictor
OFF if it adversely affects the convergence.


The FEA model contains 0 external CE equations and 24 internal CE
equations.


*********** PRECISE MASS SUMMARY ***********

TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
Translational mass | Coupled translational/rotational mass
486.56 0.0000 0.0000 | 0.0000 0.0000 1302.0
0.0000 486.56 0.0000 | 0.0000 0.0000 1495.7
0.0000 0.0000 486.56 | -1302.0 -1495.7 0.0000
------------------------------------------ | ------------------------------------------
| Rotational mass (inertia)
| 4119.9 4310.2 -0.11553E-15
| 4310.2 6466.9 0.10389E-17
| -0.11553E-15 0.10389E-17 10583.

TOTAL MASS = 486.56
The mass principal axes coincide with the global Cartesian axes

CENTER OF MASS (X,Y,Z)= 3.0739 -2.6760 0.0000

TOTAL INERTIA ABOUT CENTER OF MASS
635.67 307.84 -0.11553E-15
307.84 1869.4 0.10389E-17
-0.11553E-15 0.10389E-17 2501.6

PRINCIPAL INERTIAS = 563.12 1941.9 2501.6
ORIENTATION VECTORS OF THE INERTIA PRINCIPAL AXES IN GLOBAL CARTESIAN
( 0.973,-0.229, 0.000) ( 0.229, 0.973, 0.000) (-0.000, 0.000, 1.000)


*** MASS SUMMARY BY ELEMENT TYPE ***

TYPE MASS
1 89.4900
2 221.231
3 175.840

Range of element maximum matrix coefficients in global coordinates
Maximum = 1.194666667E+11 at element 223.
Minimum = 4.542673074E+10 at element 119.

*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP

1 60 BEAM188 0.047 0.000781
2 157 BEAM188 0.219 0.001393
3 80 BEAM188 0.078 0.000977
4 40 SURF156 0.000 0.000000
5 3 CLOAD201 0.000 0.000000
8 3 CLOAD201 0.000 0.000000
11 2 TARGE170 0.000 0.000000
12 2 TARGE170 0.000 0.000000
13 2 TARGE170 0.000 0.000000
14 2 TARGE170 0.000 0.000000
15 1 MPC184 0.000 0.000000
16 1 MPC184 0.000 0.000000
Time at end of element matrix formulation CP = 1.71875.

SPARSE MATRIX DIRECT SOLVER.
Number of equations = 3588, Maximum wavefront = 36
Memory allocated for solver = 15.259 MB
Memory required for in-core = 1.830 MB
Memory required for out-of-core = 0.776 MB


*** NOTE *** CP = 1.766 TIME= 21:35:31
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.

*** WARNING *** CP = 1.766 TIME= 21:35:31
Pivoting has been activated for the Sparse Matrix solver. The memory
required may greatly exceed the predicted amount. In that event, use
the BCSOPTION command to change the memory mode and/or memory size
used by the Sparse Matrix solver.

*** ERROR *** CP = 1.797 TIME= 21:35:31
An unexpected error ( SIG$ILL ) has occurred... ANSYS internal data
has been corrupted. ANSYS is unable to recover and will terminate.
Previously saved files are unaffected. Please send the data leading
to this operation to your technical support provider, as this will
allow ANSYS, Inc to improve the program.

Current ANSYS Traceback:
xdslf2
xdslfa
bcssl4
SolveFULL
svkan
solvcl
ANSYS

+--------------------- A N S Y S S T A T I S T I C S ------------------------+

Release: Release 16.0 Build: 16.0 Update: UP20141203 Platform: WINDOWS x64
Date Run: 11/21/2015 Time: 21:35
Windows Process ID: 1060

Processor Model: AMD A8-6410 APU with AMD Radeon R5 Graphics

Compiler: Intel(R) FORTRAN Compiler Version 14.0.0 (Build: 20140422)
Intel(R) C/C++ Compiler Version 14.0.0 (Build: 20140422)
Intel(R) Math Kernel Library Version 11.1.3 Product Build 20140917

Total number of cores available : 4
Number of physical cores available : 4
Number of processes requested : 1
Number of threads per process requested : 2
Total number of cores requested : 2 (Shared Memory Parallel)

GPU Acceleration: Not Requested

Job Name: file
Working Directory: C:\Users\loth\Desktop\idzpanwchuj\_ProjectScratch\ ScrA490

Total CPU time for main thread : 1.9 seconds
Total CPU time summed for all threads : 2.0 seconds

Elapsed time spent pre-processing model (/PREP7) : 0.0 seconds
Elapsed time spent solution - preprocessing : 0.0 seconds
Elapsed time spent computing solution : 0.0 seconds
Elapsed time spent solution - postprocessing : 0.0 seconds
Elapsed time spent post-processing model (/POST1) : 0.0 seconds

Maximum total memory used : 29.0 MB
Maximum total memory allocated : 2112.0 MB
Maximum total memory available : 3 GB

+------------------ E N D A N S Y S S T A T I S T I C S -------------------+


*---------------------------------------------------------------------------*
| |
| ANSYS RUN COMPLETED |
| |
|---------------------------------------------------------------------------|
| |
| Ansys Release 16.0 Build 16.0 UP20141203 WINDOWS x64 |
| |
|---------------------------------------------------------------------------|
| |
| Database Requested(-db) 1024 MB Scratch Memory Requested 1024 MB |
| Maximum Database Used 1 MB Maximum Scratch Memory Used 28 MB |
| |
|---------------------------------------------------------------------------|
| |
| CP Time (sec) = 2.047 Time = 21:35:32 |
| Elapsed Time (sec) = 5.000 Date = 11/21/2015 |





pls help
loth is offline   Reply With Quote

Old   December 23, 2015, 17:14
Default Ansys 15.0.7 same sig$ill error
  #3
Ryu
New Member
 
Join Date: Dec 2015
Posts: 2
Rep Power: 0
Ryu is on a distinguished road
Hi

I also had the same problem on ansys mechanical (static structural) on windows 8.1.
I can import geometry, making the update of the mesh and can not set the solution: But when ansys solves shows the error and I can not see the results.
I was advised to downgrade to Windows 7 in the event that there were incompatibilities with win8.1. I installed windows 7 professional, but the error occurs again.
Later it was suggested to install a later version of ansys: so I installed ansys 16.1 instead of ansys 15.0.7 but the error persists.


The worksheet is similar to that shown by loth therefore give only one side and the rest will attach:


*** ERROR *** CP = 3.104 TIME= 23:00:05
An unexpected error ( SIG$ILL ) has occurred... ANSYS internal data
has been corrupted. ANSYS is unable to recover and will terminate.
Previously saved files are unaffected. Please send the data leading
to this operation to your technical support provider, as this will
allow ANSYS, Inc to improve the program.

Current ANSYS Traceback:
FactorBlocked
FactorIVxTV
cPcgPrecond
casiIterate
fastSolve
svkan
solvcl
ANSYS

+--------------------- A N S Y S S T A T I S T I C S ------------------------+

Release: 15.0.7 Build: UP20140420 Platform: WINDOWS x64
Date Run: 12/23/2015 Time: 23:00
Windows Process ID: 1312

Processor Model: AMD A8-6410 APU with AMD Radeon R5 Graphics

Compiler: Intel(R) FORTRAN Compiler Version 12.1.0 (Build: 20120928)
Microsoft(R) Visual C/C++ Compiler Version 16.0 (Build: 40219)
Intel(R) Math Kernel Library Version 11.0.5 Product Build 20130612

Total number of cores available : 4
Number of physical cores available : 4
Number of cores requested : 2 (Shared Memory Parallel)

GPU Acceleration: Not Requested

Job Name: file
Working Directory: C:\Users\Giorgio\AppData\Local\Temp\WB_GIORGIO-PC_Giorgio_1824_2\_ProjectScratch\ScrEADC

Total CPU time for main thread : 2.5 seconds
Total CPU time summed for all threads : 3.4 seconds

Elapsed time spent pre-processing model (/PREP7) : 0.1 seconds
Elapsed time spent solution - preprocessing : 0.1 seconds
Elapsed time spent computing solution : 0.0 seconds
Elapsed time spent solution - postprocessing : 0.0 seconds
Elapsed time spent post-processing model (/POST1) : 0.0 seconds

Maximum total memory used : 31.0 MB
Maximum total memory allocated : 1088.0 MB
Maximum total memory available : 3 GB

+------------------ E N D A N S Y S S T A T I S T I C S -------------------+


*---------------------------------------------------------------------------*
| |
| ANSYS RUN COMPLETED |
| |
|---------------------------------------------------------------------------|
| |
| Release 15.0.7 UP20140420 WINDOWS x64 |
| |
|---------------------------------------------------------------------------|
| |
| Database Requested(-db) 512 MB Scratch Memory Requested 512 MB |
| Maximum Database Used 3 MB Maximum Scratch Memory Used 28 MB |
| |
|---------------------------------------------------------------------------|
| |
| CP Time (sec) = 3.385 Time = 23:00:07 |
| Elapsed Time (sec) = 6.000 Date = 12/23/2015 |
| |
*---------------------------------------------------------------------------*


P.S Sorry for my english =)

Please help me
Attached Files
File Type: txt Ansys-Solution Information.txt (19.6 KB, 1 views)
Ryu is offline   Reply With Quote

Old   December 24, 2015, 05:31
Default Miracle of Christmas Eve
  #4
Ryu
New Member
 
Join Date: Dec 2015
Posts: 2
Rep Power: 0
Ryu is on a distinguished road
I solved the problem by installing on the same notebook ansys v14.5 on windows7 professional N. Then an older version of ansys and not later.

I hope to help someone else
Ryu is offline   Reply With Quote

Reply

Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
[OpenFOAM.org] compile error in dynamicMesh and thermophysicalModels libraries NickG OpenFOAM Installation 3 December 30, 2019 00:21
Compile calcMassFlowC aurore OpenFOAM Programming & Development 13 March 23, 2018 07:43
[OpenFOAM] an error in Calculator's equation immortality ParaView 11 September 3, 2013 16:18
POSDAT problem piotka STAR-CD 4 June 12, 2009 08:43
How to get the max value of the whole field waynezw0618 OpenFOAM Running, Solving & CFD 4 June 17, 2008 05:07


All times are GMT -4. The time now is 17:27.