ANSYS Academic Teaching Introductory *-------------------------------------------------------------* | | | W E L C O M E T O T H E A N S Y S P R O G R A M | | | *-------------------------------------------------------------* *************************************************************** * ANSYS 11.0 LEGAL NOTICES * *************************************************************** * * * COPYRIGHT AND TRADEMARK INFORMATION * * * * Copyright 2007 SAS IP, Inc. All rights reserved. * * Unauthorized use, distribution or duplication is prohibited.* * * * See the ANSYS, Inc. online documentation or the ANSYS, Inc. * * documentation CD for the complete Legal Notice. * * * *************************************************************** * * * DISCLAIMER NOTICE * * * * THIS ANSYS SOFTWARE PRODUCT AND PROGRAM DOCUMENTATION * * INCLUDE TRADE SECRETS AND ARE CONFIDENTIAL AND PROPRIETARY * * PRODUCTS OF ANSYS, INC., ITS SUBSIDIARIES, OR LICENSORS. * * The software products and documentation are furnished by * * ANSYS, Inc., its subsidiaries, or affiliates 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. and ANSYS Europe, Ltd. are UL registered * * ISO 9001:2000 Companies. * * * *************************************************************** * * * U.S. GOVERNMENT RIGHTS * * * * 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). * * * *************************************************************** Completing ANSYS Load Process. ***** ANSYS COMMAND LINE ARGUMENTS ***** BATCH MODE REQUESTED = NOLIST 2 PARALLEL CPUS REQUESTED DESIGNXPLORER REQUESTED MEMORY REQUESTED (MB) = 82 START-UP FILE MODE = NOREAD STOP FILE MODE = NOREAD DATABASE SIZE REQUESTED (MB) = 32 *** WARNING *** CP = 0.594 TIME= 22:38:15 Use of the -M switch is no longer recommended for normal ANSYS use. ANSYS now dynamically allocates memory as needed. Only use the -M switch if you are certain that you need to do so. PARAMETER STATUS- ( 1 PARAMETERS DEFINED) (INCLUDING 1 INTERNAL PARAMETERS) 00224004 VERSION=INTEL NT RELEASE= 11.0 UP20070125 CURRENT JOBNAME=file 22:38:15 JUN 16, 2009 CP= 0.594 PARAMETER _DS_PROGRESS = 999.0000000 /INPUT FILE= ds.dat LINE= 0 *GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 22.6375000 --- Data in consistent MKS units. 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 *****TRACK MONITOR LEVEL= -1 TRACK PRINT LEVEL = 0 TRACK SUMMARY LEVEL= 0 1 ***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 11.0 ***** ANSYS Academic Teaching Introductory 00224004 VERSION=INTEL NT 22:38:15 JUN 16, 2009 CP= 0.625 ***** ANSYS ANALYSIS DEFINITION (PREP7) ***** *********** Nodes for the whole assembly *********** *********** Elements for Part 1 *********** *********** Elements for Part 2 *********** *********** Elements for Part 3 *********** *********** Elements for Part 4 *********** *********** Elements for Part 5 *********** *********** Elements for Part 6 *********** *********** Elements for Part 7 *********** *********** Elements for Part 8 *********** *********** Elements for Part 9 *********** *********** Elements for Part 10 *********** *********** Send Materials *********** *********** Send Sheet Properties *********** *********** Send Beam Properties *********** *********** Fixed Supports *********** *********** Construct Remote Displacement Using RBE3/CERIG Contact *********** *********** Construct Remote Displacement Using RBE3/CERIG Contact *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Create Spot Weld *********** *********** Set Reference Temperature *********** *********** Send User Defined Coordinate System(s) *********** LIST DATA TABLE BISO FOR MATERIAL 5 1 ***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 11.0 ***** ANSYS Academic Teaching Introductory 00224004 VERSION=INTEL NT 22:38:40 JUN 16, 2009 CP= 11.453 BiIso Pl (BISO) Table For Material 5 1 Temps 0.0000 Yld Strs 0.25000E+09 Tang Mod 0.0000 ***** ROUTINE COMPLETED ***** CP = 11.453 --- Number of total nodes = 346 --- Number of contact elements = 0 --- Number of spring elements = 0 --- Number of solid elements = 194 --- Number of total elements = 276 *GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 22.6447222 **************************************************************************** ************************* SOLUTION ******************************** **************************************************************************** ***** ANSYS SOLUTION ROUTINE ***** PERFORM A STATIC ANALYSIS THIS WILL BE A NEW ANALYSIS NEW SOLUTION CONTROL OPTION IS ACTIVATED, THE FOLLOWING COMMANDS ARE RESET TO NEW DEFAULTS: AUTOTS, DELTIM, NSUB, CNVTOL, LNSRCH, PRED, NROPT, TINTP, CUTCONTROL, OPNCONTROL, MONITOR, NEQIT, SSTIF, KBC. CONTACT TIME PREDICTIONS ARE BASED ON ELEMENT KEYOPT(7) SPECIFIED Avg ratio= 1, totalParts=10, thickParts=0, thickPcent= 0 USE SPARSE MATRIX DIRECT SOLVER DO NOT SAVE ANY RESTART FILES AT ALL CONTACT INFORMATION PRINTOUT LEVEL 1 NLDIAG: Nonlinear diagnostics CONT option is set to ON. Writing frequence : each ITERATION. **************************************************** ******************* SOLVE FOR LS 1 **************** SPECIFIED CONSTRAINT UX FOR SELECTED NODES 331 TO 331 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI75UX SPECIFIED CONSTRAINT UY FOR SELECTED NODES 331 TO 331 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI75UY SPECIFIED CONSTRAINT UZ FOR SELECTED NODES 331 TO 331 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI75UZ SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES 331 TO 331 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI75ROTX SPECIFIED CONSTRAINT ROTZ FOR SELECTED NODES 331 TO 331 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI75ROTZ SPECIFIED CONSTRAINT UX FOR SELECTED NODES 332 TO 332 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI76UX SPECIFIED CONSTRAINT UY FOR SELECTED NODES 332 TO 332 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI76UY SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES 332 TO 332 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI76ROTX SPECIFIED CONSTRAINT ROTZ FOR SELECTED NODES 332 TO 332 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI76ROTZ *********** Create Acceleration *********** SET PARAMETER DIMENSIONS ON _ACELX TYPE=TABL DIMENSIONS= 2 1 1 TIME PARAMETER _ACELX(1,0) = 0.000000000 PARAMETER _ACELX(2,0) = 1.000000000 PARAMETER _ACELX(1,1) = 0.000000000 PARAMETER _ACELX(2,1) = 0.000000000 SET PARAMETER DIMENSIONS ON _ACELY TYPE=TABL DIMENSIONS= 2 1 1 TIME PARAMETER _ACELY(1,0) = 0.000000000 PARAMETER _ACELY(2,0) = 1.000000000 PARAMETER _ACELY(1,1) = 0.000000000 PARAMETER _ACELY(2,1) = 0.000000000 SET PARAMETER DIMENSIONS ON _ACELZ TYPE=TABL DIMENSIONS= 2 1 1 TIME PARAMETER _ACELZ(1,0) = 0.000000000 PARAMETER _ACELZ(2,0) = 1.000000000 PARAMETER _ACELZ(1,1) = 0.000000000 PARAMETER _ACELZ(2,1) = 9.806650000 ACELX IS SET ACCORDING TO TABLE PARAMETER = _ACELX ACELY IS SET ACCORDING TO TABLE PARAMETER = _ACELY ACELZ IS SET ACCORDING TO TABLE PARAMETER = _ACELZ PRINTOUT RESUMED BY /GOP USE AUTOMATIC TIME STEPPING THIS LOAD STEP USE 5 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DOFS FOR AUTOMATIC TIME STEPPING: USE 1000 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 NLOA 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 SELECT FOR ITEM=MAT COMPONENT= IN RANGE 2 TO 2 STEP 1 13 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM=MAT COMPONENT= IN RANGE 3 TO 3 STEP 1 26 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM=MAT COMPONENT= IN RANGE 4 TO 4 STEP 1 39 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM=MAT COMPONENT= IN RANGE 5 TO 5 STEP 1 52 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM=MAT COMPONENT= IN RANGE 6 TO 6 STEP 1 60 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM=MAT COMPONENT= IN RANGE 7 TO 7 STEP 1 71 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM=MAT COMPONENT= IN RANGE 8 TO 8 STEP 1 82 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM=MAT COMPONENT= IN RANGE 9 TO 9 STEP 1 90 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. ALSO SELECT FOR ITEM=MAT COMPONENT= IN RANGE 10 TO 10 STEP 1 98 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. DEFINITION OF COMPONENT = _ELMISC ENTITY=ELEM ALL SELECT FOR ITEM=ELEM COMPONENT= IN RANGE 1 TO 276 STEP 1 276 ELEMENTS (OF 276 DEFINED) SELECTED BY ESEL COMMAND. WRITE MISC ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR THE ENTITIES DEFINED BY COMPONENT _ELMISC ***** ANSYS SOLVE COMMAND ***** *** NOTE *** CP = 11.469 TIME= 22:38:41 There is no title defined for this analysis. *** WARNING *** CP = 11.469 TIME= 22:38:41 Element shape checking is currently inactive. Issue SHPP,ON or SHPP,WARN to reactivate, if desired. *** NOTE *** CP = 11.469 TIME= 22:38:41 The model data was checked and warning messages were found. Please review output or errors file ( E:\Brücke\Brücke_2 Simulationsdateien\Statisch-mechanisch_Eigengewicht\file.err ) for these warning messages. *** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS *** --- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS --- ELEMENT TYPE 1 IS SHELL181. IT IS ASSOCIATED WITH ELASTOPLASTIC MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND KEYOPT(3)=2 IS SUGGESTED FOR HIGHER ACCURACY OF MEMBRANE STRESSES; OTHERWISE, KEYOPT(3)=0 IS SUGGESTED. KEYOPT(8) HAS BEEN RESET BUT KEYOPT(3) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 2 0 0 0 0 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 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 4 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 5 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 6 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 7 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 8 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 9 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 10 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 15 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 16 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 17 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 18 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 19 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 20 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 21 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 22 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 23 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 24 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 25 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 26 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 27 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 28 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS AND KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET BUT KEYOPT(1) CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 1 ***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 11.0 ***** ANSYS Academic Teaching Introductory 00224004 VERSION=INTEL NT 22:38:41 JUN 16, 2009 CP= 11.469 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) EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE PLASTIC MATERIAL PROPERTIES INCLUDED. . . . . .YES NEWTON-RAPHSON OPTION . . . . . . . . . . . . .PROGRAM CHOSEN GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC *** NOTE *** CP = 11.484 TIME= 22:38:41 Nonlinear analysis, NROPT set to the FULL Newton-Raphson solution procedure for ALL degrees of freedom. *** NOTE *** CP = 11.484 TIME= 22:38:41 The conditions for direct assembly have been met. No .emat or .erot files will be produced. *** NOTE *** CP = 11.484 TIME= 22:38:41 Internal nodes from 347 to 506 are created. 2 internal nodes are used for handling DOF on pilot nodes of rigid target surfaces. 158 internal nodes are used for quadratic option of BEAM188/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 AUTOMATIC TIME STEPPING . . . . . . . . . . . . ON INITIAL NUMBER OF SUBSTEPS . . . . . . . . . 5 MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . . 1000 MINIMUM NUMBER OF SUBSTEPS . . . . . . . . . 1 MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS. . . . 15 STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO TERMINATE ANALYSIS IF NOT CONVERGED . . . . . .YES (EXIT) CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS INERTIA LOADS X Y Z ACEL . . . . . . . . . . . ._ACELX _ACELY _ACELZ COPY INTEGRATION POINT VALUES TO NODE . . . . .YES, FOR ELEMENTS WITH ACTIVE MAT. NONLINEARITIES PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT DATABASE OUTPUT CONTROLS ITEM FREQUENCY COMPONENT ALL NONE NSOL ALL RSOL ALL NLOA ALL STRS ALL EPEL ALL EPPL ALL MISC ALL _ELMISC SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 25, BY SOLUTION CONTROL LOGIC. *** NOTE *** CP = 12.516 TIME= 22:38:44 Smoothing on certain contact nodes (e.g.55) for pair ID 11 may have accuracy issue. Please verify face normal of connected elements. *** NOTE *** CP = 12.516 TIME= 22:38:44 Smoothing on certain contact nodes (e.g.57) for pair ID 11 may have accuracy issue. Please verify face normal of connected elements. *** NOTE *** CP = 12.516 TIME= 22:38:44 Smoothing on certain contact nodes (e.g.88) for pair ID 11 may have accuracy issue. Please verify face normal of connected elements. *** NOTE *** CP = 12.516 TIME= 22:38:44 Smoothing on certain contact nodes (e.g.89) for pair ID 11 may have accuracy issue. Please verify face normal of connected elements. *** NOTE *** CP = 12.516 TIME= 22:38:44 Smoothing on certain contact nodes (e.g.93) for pair ID 11 may have accuracy issue. Please verify face normal of connected elements. *** NOTE *** CP = 12.516 TIME= 22:38:44 Smoothing on certain contact nodes (e.g.102) for pair ID 11 may have accuracy issue. Please verify face normal of connected elements. *** NOTE *** CP = 12.516 TIME= 22:38:44 Smoothing on certain contact nodes (e.g.103) for pair ID 11 may have accuracy issue. Please verify face normal of connected elements. *** NOTE *** CP = 12.516 TIME= 22:38:44 Smoothing on certain contact nodes (e.g.104) for pair ID 11 may have accuracy issue. Please verify face normal of connected elements. *** NOTE *** CP = 12.516 TIME= 22:38:44 Force-distributed-surface identified by real constant set 11 and contact element type 11 has been set up. The pilot node 331 is used to apply the force. Internal MPC will be built. The used DOF set is UX UY UZ ROTX ROTY ROTZ Please verify constraints (including rotational DOF) on the pilot node by yourself. *** NOTE *** CP = 12.516 TIME= 22:38:44 Force-distributed-surface identified by real constant set 13 and contact element type 13 has been set up. The pilot node 332 is used to apply the force. Internal MPC will be built. The used DOF set is UX UY UZ ROTX ROTY ROTZ Please verify constraints (including rotational DOF) on the pilot node by yourself. **** CENTER OF MASS, MASS, AND MASS MOMENTS OF INERTIA **** CALCULATIONS ASSUME ELEMENT MASS AT ELEMENT CENTROID TOTAL MASS = 72527. MOM. OF INERTIA MOM. OF INERTIA CENTER OF MASS ABOUT ORIGIN ABOUT CENTER OF MASS XC = 0.50828 IXX = 0.1653E+07 IXX = 0.1026E+07 YC = 0.38404E-16 IYY = 0.2595E+07 IYY = 0.1949E+07 ZC = 2.9411 IZZ = 0.1445E+07 IZZ = 0.1426E+07 IXY = -0.1819E-11 IXY = -0.4033E-12 IYZ = -0.3638E-11 IYZ = 0.4554E-11 IZX = -0.2728E-11 IZX = 0.1084E+06 *** MASS SUMMARY BY ELEMENT TYPE *** TYPE MASS 1 9216.00 2 7091.72 3 7091.72 4 7091.72 5 7091.72 6 4992.00 7 9984.00 8 9984.00 9 4992.00 10 4992.00 Range of element maximum matrix coefficients in global coordinates Maximum= 4.490516503E+11 at element 219. Minimum= 1.817381948E+09 at element 15. *** ELEMENT MATRIX FORMULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 96 SHELL181 0.188 0.001953 2 13 BEAM188 0.094 0.007212 3 13 BEAM188 0.062 0.004808 4 13 BEAM188 0.094 0.007212 5 13 BEAM188 0.078 0.006010 6 8 BEAM188 0.016 0.001953 7 11 BEAM188 0.000 0.000000 8 11 BEAM188 0.031 0.002841 9 8 BEAM188 0.031 0.003906 10 8 BEAM188 0.719 0.089844 11 10 CONTA175 0.000 0.000000 12 1 TARGE170 0.000 0.000000 13 10 CONTA175 0.000 0.000000 14 1 TARGE170 0.000 0.000000 15 2 BEAM188 0.016 0.007812 16 2 BEAM188 0.000 0.000000 17 2 BEAM188 0.000 0.000000 18 2 BEAM188 0.016 0.007812 19 8 BEAM188 0.078 0.009766 20 8 BEAM188 0.031 0.003906 21 2 BEAM188 0.016 0.007812 22 2 BEAM188 0.016 0.007812 23 2 BEAM188 0.000 0.000000 24 2 BEAM188 0.000 0.000000 25 6 BEAM188 0.031 0.005208 26 6 BEAM188 0.594 0.098958 27 8 BEAM188 0.031 0.003906 28 8 BEAM188 0.078 0.009766 Time at end of element matrix formulation CP= 13.65625. FORCE CONVERGENCE VALUE = 9696. CRITERION= 49.47 MOMENT CONVERGENCE VALUE = 0.000 CRITERION= 13.70 SPARSE MATRIX DIRECT SOLVER. Number of equations = 2403, Maximum wavefront = 126 Memory available for solver = 37.791 MB Memory required for in-core = 1.445 MB Optimal memory required for out-of-core = 0.445 MB Minimum memory required for out-of-core = 0.418 MB Sparse solver maximum pivot= 4.490516503E+11 at node 450 UX. Sparse solver minimum pivot= 411909.265 at node 124 ROTX. Sparse solver minimum pivot in absolute value= 411909.265 at node 124 ROTX. EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.1030 LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.1030 *** NOTE *** CP = 15.625 TIME= 22:38:50 The initial memory allocation (-m) has been exceeded. Supplemental memory allocations are being used. FORCE CONVERGENCE VALUE = 0.8477E-06 CRITERION= 567.4 <<< CONVERGED MOMENT CONVERGENCE VALUE = 0.1451E-05 CRITERION= 20.46 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** ELEMENT RESULT CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 96 SHELL181 0.266 0.002767 2 13 BEAM188 0.500 0.038462 3 13 BEAM188 0.109 0.008413 4 13 BEAM188 0.078 0.006010 5 13 BEAM188 0.484 0.037260 6 8 BEAM188 0.016 0.001953 7 11 BEAM188 0.031 0.002841 8 11 BEAM188 0.031 0.002841 9 8 BEAM188 0.016 0.001953 10 8 BEAM188 0.656 0.082031 11 10 CONTA175 0.000 0.000000 12 1 TARGE170 0.000 0.000000 13 10 CONTA175 0.000 0.000000 14 1 TARGE170 0.000 0.000000 15 2 BEAM188 0.000 0.000000 16 2 BEAM188 0.000 0.000000 17 2 BEAM188 0.000 0.000000 18 2 BEAM188 0.016 0.007812 19 8 BEAM188 0.062 0.007812 20 8 BEAM188 0.016 0.001953 21 2 BEAM188 0.016 0.007812 22 2 BEAM188 0.016 0.007812 23 2 BEAM188 0.000 0.000000 24 2 BEAM188 0.000 0.000000 25 6 BEAM188 0.094 0.015625 26 6 BEAM188 0.156 0.026042 27 8 BEAM188 0.000 0.000000 28 8 BEAM188 0.047 0.005859 *** NODAL LOAD CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 96 SHELL181 0.016 0.000163 2 13 BEAM188 0.000 0.000000 3 13 BEAM188 0.000 0.000000 4 13 BEAM188 0.000 0.000000 5 13 BEAM188 0.000 0.000000 6 8 BEAM188 0.000 0.000000 7 11 BEAM188 0.000 0.000000 8 11 BEAM188 0.000 0.000000 9 8 BEAM188 0.000 0.000000 10 8 BEAM188 0.000 0.000000 11 10 CONTA175 0.000 0.000000 12 1 TARGE170 0.000 0.000000 13 10 CONTA175 0.000 0.000000 14 1 TARGE170 0.000 0.000000 15 2 BEAM188 0.000 0.000000 16 2 BEAM188 0.000 0.000000 17 2 BEAM188 0.000 0.000000 18 2 BEAM188 0.000 0.000000 19 8 BEAM188 0.000 0.000000 20 8 BEAM188 0.000 0.000000 21 2 BEAM188 0.000 0.000000 22 2 BEAM188 0.000 0.000000 23 2 BEAM188 0.000 0.000000 24 2 BEAM188 0.000 0.000000 25 6 BEAM188 0.000 0.000000 26 6 BEAM188 0.000 0.000000 27 8 BEAM188 0.000 0.000000 28 8 BEAM188 0.000 0.000000 *** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 1 *** TIME = 0.200000 TIME INC = 0.200000 *** AUTO STEP TIME: NEXT TIME INC = 0.20000 UNCHANGED FORCE CONVERGENCE VALUE = 9696. CRITERION= 562.6 MOMENT CONVERGENCE VALUE = 0.1451E-05 CRITERION= 20.05 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.1030 LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.1030 FORCE CONVERGENCE VALUE = 0.5614E-06 CRITERION= 1135. <<< CONVERGED MOMENT CONVERGENCE VALUE = 0.1448E-05 CRITERION= 40.93 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 1 SUBSTEP 2 COMPLETED. CUM ITER = 2 *** TIME = 0.400000 TIME INC = 0.200000 *** AUTO TIME STEP: NEXT TIME INC = 0.30000 INCREASED (FACTOR = 1.5000) FORCE CONVERGENCE VALUE = 0.1454E+05 CRITERION= 1121. MOMENT CONVERGENCE VALUE = 0.1448E-05 CRITERION= 40.11 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.1545 LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.1545 FORCE CONVERGENCE VALUE = 0.8620E-06 CRITERION= 1986. <<< CONVERGED MOMENT CONVERGENCE VALUE = 0.2174E-05 CRITERION= 71.62 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 1 SUBSTEP 3 COMPLETED. CUM ITER = 3 *** TIME = 0.700000 TIME INC = 0.300000 *** AUTO STEP TIME: NEXT TIME INC = 0.30000 UNCHANGED FORCE CONVERGENCE VALUE = 0.1454E+05 CRITERION= 1954. MOMENT CONVERGENCE VALUE = 0.2174E-05 CRITERION= 70.19 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.1545 LINE SEARCH PARAMETER = 1.000 SCALED MAX DOF INC = -0.1545 FORCE CONVERGENCE VALUE = 0.7919E-06 CRITERION= 2837. <<< CONVERGED MOMENT CONVERGENCE VALUE = 0.2176E-05 CRITERION= 102.3 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 1 SUBSTEP 4 COMPLETED. CUM ITER = 4 *** TIME = 1.00000 TIME INC = 0.300000 *** ANSYS BINARY FILE STATISTICS BUFFER SIZE USED= 16384 5.250 MB WRITTEN ON ELEMENT SAVED DATA FILE: file.esav 0.375 MB WRITTEN ON ASSEMBLED MATRIX FILE: file.full 5.562 MB WRITTEN ON RESULTS FILE: file.rst **************************************************** *************** FINISHED SOLVE FOR LS 1 ************* PARAMETER _DS_PROGRESS DELETED. *GET _WALLASOL FROM ACTI ITEM=TIME WALL VALUE= 22.6566667 FINISH SOLUTION PROCESSING ***** ROUTINE COMPLETED ***** CP = 31.672 1 ***** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 11.0 ***** ANSYS Academic Teaching Introductory 00224004 VERSION=INTEL NT 22:39:24 JUN 16, 2009 CP= 31.812 ***** ANSYS RESULTS INTERPRETATION (POST1) ***** *** NOTE *** CP = 31.812 TIME= 22:39:24 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 Output of XML File to: PARM, , , , , , , , , , , , , , , , , , , DATABASE WRITTEN ON FILE parm.xml PRINTOUT RESUMED BY /GOP EXIT THE ANSYS POST1 DATABASE PROCESSOR ***** ROUTINE COMPLETED ***** CP = 31.812 PRINTOUT RESUMED BY /GOP *GET _WALLDONE FROM ACTI ITEM=TIME WALL VALUE= 22.6569444 PARAMETER _PREPTIME = 26.00000000 PARAMETER _SOLVTIME = 43.00000000 PARAMETER _POSTTIME = 1.000000000 PARAMETER _TOTALTIM = 70.00000000 EXIT ANSYS WITHOUT SAVING DATABASE NUMBER OF WARNING MESSAGES ENCOUNTERED= 2 NUMBER OF ERROR MESSAGES ENCOUNTERED= 0 ***************************************************** CPU TIME SPENT FOR CONTACT DATABASE 0.000 CONTACT SEARCH 0.000 CONTACT ELEMENTS 0.000 OTHER ELEMENTS 14.156 EQUATION SOLVER 6.203 TOTAL SYSTEM 20.359 ***************************************************** *---------------------------------------------------------------------------* | | | ANSYS RUN COMPLETED | | | |---------------------------------------------------------------------------| | | | Release 11.0 UP20070125 INTEL NT | | | |---------------------------------------------------------------------------| | | | Maximum Scratch Memory Used = 12141908 Words 46.318 MB | | | |---------------------------------------------------------------------------| | | | CP Time (sec) = 31.812 Time = 22:39:25 | | Elapsed Time (sec) = 71.000 Date = 06/16/2009 | | | *---------------------------------------------------------------------------*