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November 21, 2015, 15:58 |
Ansys SIG$ILL error
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Hi
today i've installed Ansys on my personal machine and I accured strange error that i've never seen before *** ERROR *** CP = 1.797 TIME= 21:35:31 An unexpected error ( SIG$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 |
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November 21, 2015, 15:59 |
rest of the worksheet
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#2 |
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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 |
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December 23, 2015, 17:14 |
Ansys 15.0.7 same sig$ill error
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#3 |
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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 |
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December 24, 2015, 05:31 |
Miracle of Christmas Eve
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#4 |
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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 |
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