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Products Release 16.2 ANSYS Mechanical Products Release 16.2 ANSYS Customization Files for User Programmable Features Release 16.2 ANSYS Autodyn Release 16.2 ANSYS Aqwa Release 16.2 ANSYS Composite PrepPost Release 16.2 ANSYS, Inc. License Manager Release 16.2 ANSYS, Inc. Products 16.2.3 *** NOTE *** CP = 3.058 TIME= 08:09:13 The /CONFIG,NOELDB command is not valid in a Distributed ANSYS solution. Command is ignored. *GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 8.15361111 TITLE= Kriechmodel_V10--Static Structural (F5) ACT Extensions: SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR TYPE=STRI DIMENSIONS= 248 1 1 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 16.2 16.2 *** DISTRIBUTED ANSYS Mechanical 00201982 VERSION=WINDOWS x64 08:09:13 DEC 01, 2016 CP= 3.136 Kriechmodel_V10--Static Structural (F5) ***** ANSYS ANALYSIS DEFINITION (PREP7) ***** *********** Nodes for the whole assembly *********** *********** Elements for Body 1 "Solid" *********** *********** Send User Defined Coordinate System(s) *********** *********** Set Reference Temperature *********** *********** Send Materials *********** IMPLICIT CREEP OPTION is used, CREEP MODEL is 7 ********* Frictionless Supports X ********* ********* Frictionless Supports Z ********* *********** Node Rotations *********** *********** Define Pressure Using Surface Effect Elements *********** *********** Construct Weak Springs, Prototype 1 *********** *********** Define Rotational Velocity *********** ***** ROUTINE COMPLETED ***** CP = 3.822 --- Number of total nodes = 8502 --- Number of contact elements = 120 --- Number of spring elements = 24 --- Number of bearing elements = 0 --- Number of solid elements = 1717 --- Number of total elements = 1861 *GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 8.15444444 **************************************************************************** ************************* SOLUTION ******************************** **************************************************************************** ***** ANSYS SOLUTION ROUTINE ***** PERFORM A STATIC ANALYSIS THIS WILL BE A NEW ANALYSIS USE PRECONDITIONED CONJUGATE GRADIENT SOLVER CONVERGENCE TOLERANCE = 1.00000E-08 MAXIMUM ITERATION = NumNode*DofPerNode* 1.0000 CONTACT INFORMATION PRINTOUT LEVEL 1 DO NOT COMBINE ELEMENT MATRIX FILES (.emat) AFTER DISTRIBUTED PARALLEL SOLUTION DO NOT COMBINE ELEMENT SAVE DATA FILES (.esav) AFTER DISTRIBUTED PARALLEL SOLUTION NLDIAG: Nonlinear diagnostics CONT option is set to ON. Writing frequency : each ITERATION. DEFINE RESTART CONTROL FOR LOADSTEP LAST AT FREQUENCY OF LAST AND NUMBER FOR OVERWRITE IS 0 DELETE RESTART FILES OF ENDSTEP **************************************************** ******************* SOLVE FOR LS 1 **************** SELECT FOR ITEM=TYPE COMPONENT= IN RANGE 2 TO 2 STEP 1 120 ELEMENTS (OF 1861 DEFINED) SELECTED BY ESEL COMMAND. SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET. 407 NODES (OF 8502 DEFINED) SELECTED FROM 120 SELECTED ELEMENTS BY NSLE COMMAND. GENERATE SURFACE LOAD PRES ON SURFACE DEFINED BY ALL SELECTED NODES SET ACCORDING TO TABLE PARAMETER = _LOADVARI26 NUMBER OF PRES ELEMENT FACE LOADS STORED = 120 ALL SELECT FOR ITEM=NODE COMPONENT= IN RANGE 1 TO 8502 STEP 1 8502 NODES (OF 8502 DEFINED) SELECTED BY NSEL COMMAND. ALL SELECT FOR ITEM=ELEM COMPONENT= IN RANGE 1 TO 1861 STEP 1 1861 ELEMENTS (OF 1861 DEFINED) SELECTED BY ESEL COMMAND. CMOMEGA on component= cm_rotvelcity173 OMEGX IS SET ACCORDING TO TABLE PARAMETER = _LOADVARI173X OMEGY IS SET ACCORDING TO TABLE PARAMETER = _LOADVARI173Y OMEGZ IS SET ACCORDING TO TABLE PARAMETER = _LOADVARI173Z X1, Y1, Z1= 0.87380 -0.23702E-01 0.40000E-01 ALL SELECT FOR ITEM=ELEM COMPONENT= IN RANGE 1 TO 1861 STEP 1 1861 ELEMENTS (OF 1861 DEFINED) SELECTED BY ESEL COMMAND. PRINTOUT RESUMED BY /GOP USE AUTOMATIC TIME STEPPING THIS LOAD STEP USE 5 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM 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 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 WRITE EPCR ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIES NONLINEAR STABILIZATION CONTROL: KEY=OFF DO NOT INCLUDE STRAIN RATE EFFECT ON ANALYSIS FROM THIS LOAD STEP ONWARDS (VISCOPLASTICITY/CREEP ANALYSIS). *GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000 *IF ANSINTER_ ( = 0.00000 ) NE 0 ( = 0.00000 ) THEN *ENDIF ***** ANSYS SOLVE COMMAND ***** *** WARNING *** CP = 4.649 TIME= 08:09:17 Element shape checking is currently inactive. Issue SHPP,ON or SHPP,WARN to reactivate, if desired. *** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS *** --- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS --- ELEMENT TYPE 1 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET. KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0 *** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE Release 16.2 16.2 *** DISTRIBUTED ANSYS Mechanical 00201982 VERSION=WINDOWS x64 08:09:17 DEC 01, 2016 CP= 4.930 Kriechmodel_V10--Static Structural (F5) 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. . . . . . . . . . . . .PCG TOLERANCE. . . . . . . . . . . . . . . . . . 1.00000E-08 CREEP MATERIAL PROPERTIES INCLUDED. . . . . . .YES NEWTON-RAPHSON OPTION . . . . . . . . . . . . .PROGRAM CHOSEN GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC *** WARNING *** CP = 5.101 TIME= 08:09:17 Material number 2 (used by element 1718 ) 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 = 5.132 TIME= 08:09:18 This nonlinear analysis defaults to using the full Newton-Raphson solution procedure. This can be modified using the NROPT command. D I S T R I B U T E D D O M A I N D E C O M P O S E R ...Number of elements: 1861 ...Number of nodes: 8502 ...Decompose to 2 CPU domains ...Element load balance ratio = 1.018 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) CREEP CRITERION . . . . . . . . . . . . . . . . none CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS 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 STRS ALL EPEL ALL EPPL ALL EPCR ALL SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 22, BY SOLUTION CONTROL LOGIC. *** NOTE *** CP = 9.953 TIME= 08:10:10 The PCG solver has automatically set the level of difficulty for this model to 2. *********** PRECISE MASS SUMMARY *********** TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN Translational mass | Coupled translational/rotational mass 0.72485 0.0000 0.0000 | 0.0000 0.28994E-01 -0.36339 0.0000 0.72485 0.0000 | -0.28994E-01 0.0000 0.63337 0.0000 0.0000 0.72485 | 0.36339 -0.63337 0.0000 ------------------------------------------ | ------------------------------------------ | Rotational mass (inertia) | 0.18377 -0.31753 -0.25335E-01 | -0.31753 0.55510 -0.14536E-01 | -0.25335E-01 -0.14536E-01 0.73578 TOTAL MASS = 0.72485 The mass principal axes coincide with the global Cartesian axes CENTER OF MASS (X,Y,Z)= 0.87380 0.50134 0.40000E-01 TOTAL INERTIA ABOUT CENTER OF MASS 0.42933E-03 0.17980E-11 -0.22347E-13 0.17980E-11 0.49447E-03 0.33492E-11 -0.22347E-13 0.33492E-11 0.15162E-03 The inertia principal axes coincide with the global Cartesian axes *** MASS SUMMARY BY ELEMENT TYPE *** TYPE MASS 1 0.724852 Range of element maximum matrix coefficients in global coordinates Maximum = 4.111840238E+09 at element 527. Minimum = 0.754917906 at element 1855. *** WARNING *** CP = 10.312 TIME= 08:10:11 Coefficient ratio exceeds 1.0e8 - Check results. *** ELEMENT MATRIX FORMULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 1717 SOLID186 0.530 0.000309 2 120 SURF154 0.000 0.000000 3 24 COMBIN14 0.000 0.000000 Time at end of element matrix formulation CP = 10.3116665. ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.rdb FOR POSSIBLE RESUME FROM THIS POINT FORCE CONVERGENCE VALUE = 3206. CRITERION= 16.36 Iteration= 15 Ratio= 0.312702 Limit= 1.000000E-08 Wall= 0.0 Iteration= 85 Ratio= 7.377912E-04 Limit= 1.000000E-08 Wall= 1.3 Iteration= 175 Ratio= 2.715723E-06 Limit= 1.000000E-08 Wall= 2.1 DISTRIBUTED PCG SOLVER SOLUTION CONVERGED DISTRIBUTED PCG SOLVER SOLUTION STATISTICS NUMBER OF DOMAINS = 51 NUMBER OF ITERATIONS= 255 NUMBER OF EQUATIONS = 25506 LEVEL OF CONVERGENCE= 1 CALCULATED NORM = 0.97138E-08 SPECIFIED TOLERANCE = 0.10000E-07 TOTAL CPU TIME (sec)= 2.72 TOTAL WALL TIME(sec)= 2.72 TOTAL MEMORY (GB) = 0.02 DISP CONVERGENCE VALUE = 0.2906E-05 CRITERION= 0.1483E-06 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2906E-05 FORCE CONVERGENCE VALUE = 0.3115E-04 CRITERION= 28.47 <<< CONVERGED DISP CONVERGENCE VALUE = 0.4023E-13 CRITERION= 0.1513E-06 <<< CONVERGED EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = -0.4023E-13 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2 *** ELEMENT RESULT CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 1717 SOLID186 0.265 0.000154 2 120 SURF154 0.016 0.000130 3 24 COMBIN14 0.000 0.000000 *** NODAL LOAD CALCULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 1717 SOLID186 0.000 0.000000 2 120 SURF154 0.000 0.000000 3 24 COMBIN14 0.000 0.000000 *** LOAD STEP 1 SUBSTEP 1 COMPLETED. CUM ITER = 2 *** TIME = 0.200000 TIME INC = 0.200000 *** AUTO STEP TIME: NEXT TIME INC = 0.20000 UNCHANGED FORCE CONVERGENCE VALUE = 172.5 CRITERION= 55.89 DISP CONVERGENCE VALUE = 0.3185E-06 CRITERION= 0.1608E-06 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.3185E-06 FORCE CONVERGENCE VALUE = 0.1656E-05 CRITERION= 59.09 <<< CONVERGED DISP CONVERGENCE VALUE = 0.1910E-14 CRITERION= 0.1641E-06 <<< CONVERGED EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = -0.1910E-14 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2 *** LOAD STEP 1 SUBSTEP 2 COMPLETED. CUM ITER = 4 *** TIME = 0.400000 TIME INC = 0.200000 *** AUTO TIME STEP: NEXT TIME INC = 0.30000 INCREASED (FACTOR = 1.5000) FORCE CONVERGENCE VALUE = 323.5 CRITERION= 103.2 DISP CONVERGENCE VALUE = 0.5971E-06 CRITERION= 0.2646E-06 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.5971E-06 FORCE CONVERGENCE VALUE = 0.3105E-05 CRITERION= 109.2 <<< CONVERGED DISP CONVERGENCE VALUE = 0.3581E-14 CRITERION= 0.2700E-06 <<< CONVERGED EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = -0.3581E-14 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2 *** LOAD STEP 1 SUBSTEP 3 COMPLETED. CUM ITER = 6 *** TIME = 0.700000 TIME INC = 0.300000 *** AUTO STEP TIME: NEXT TIME INC = 0.30000 UNCHANGED FORCE CONVERGENCE VALUE = 388.2 CRITERION= 156.5 DISP CONVERGENCE VALUE = 0.7166E-06 CRITERION= 0.2928E-06 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7166E-06 FORCE CONVERGENCE VALUE = 0.3725E-05 CRITERION= 164.5 <<< CONVERGED DISP CONVERGENCE VALUE = 0.4298E-14 CRITERION= 0.2987E-06 <<< CONVERGED EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC = -0.4298E-14 >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 2 *** LOAD STEP 1 SUBSTEP 4 COMPLETED. CUM ITER = 8 *** TIME = 1.00000 TIME INC = 0.300000 *** ANSYS BINARY FILE STATISTICS BUFFER SIZE USED= 16384 0.125 MB WRITTEN ON ELEMENT MATRIX FILE: file0.emat 5.812 MB WRITTEN ON ELEMENT SAVED DATA FILE: file0.esav 4.875 MB WRITTEN ON RESULTS FILE: file0.rst *************** Write FE CONNECTORS ********* WRITE OUT CONSTRAINT EQUATIONS TO FILE= file.ce **************************************************** *************** FINISHED SOLVE FOR LS 1 ************* **************************************************** ******************* SOLVE FOR LS 2 **************** ALL SELECT FOR ITEM=ELEM COMPONENT= IN RANGE 1 TO 1861 STEP 1 1861 ELEMENTS (OF 1861 DEFINED) SELECTED BY ESEL COMMAND. PRINTOUT RESUMED BY /GOP USE AUTOMATIC TIME STEPPING THIS LOAD STEP USE 5 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM FOR AUTOMATIC TIME STEPPING: USE 1000 SUBSTEPS AS A MAXIMUM USE 1 SUBSTEPS AS A MINIMUM TIME= 50000. 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 WRITE EPCR ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIES NONLINEAR STABILIZATION CONTROL: KEY=OFF INCLUDE STRAIN RATE EFFECT ON ANALYSIS FROM THIS LOAD STEP ONWARDS (VISCOPLASTICITY/CREEP ANALYSIS). IMPLICIT CREEP RATIO CONTROL = 1.000 ***** ANSYS SOLVE COMMAND ***** *** WARNING *** CP = 32.682 TIME= 08:14:07 Material number 2 (used by element 1718 ) 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 = 32.932 TIME= 08:14:08 This nonlinear analysis defaults to using the full Newton-Raphson solution procedure. This can be modified using the NROPT command. *** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE Release 16.2 16.2 *** DISTRIBUTED ANSYS Mechanical 00201982 VERSION=WINDOWS x64 08:14:10 DEC 01, 2016 CP= 33.213 Kriechmodel_V10--Static Structural (F5) L O A D S T E P O P T I O N S LOAD STEP NUMBER. . . . . . . . . . . . . . . . 2 TIME AT END OF THE LOAD STEP. . . . . . . . . . 50000. 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) CREEP CRITERION . . . . . . . . . . . . . . . . 1.0000 CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS 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 STRS ALL EPEL ALL EPPL ALL EPCR ALL SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 22, BY SOLUTION CONTROL LOGIC. *** WARNING *** CP = 33.774 TIME= 08:14:58 The creep integration algorithm does not converge for element 543, material 1, creep model 7. *** WARNING *** CP = 33.774 TIME= 08:14:58 The creep integration algorithm does not converge for element 1063, material 1, creep model 7. *** WARNING *** CP = 33.774 TIME= 08:14:58 The creep integration algorithm does not converge for element 1063, material 1, creep model 7. *** WARNING *** CP = 33.774 TIME= 08:14:58 The creep integration algorithm does not converge for element 1063, material 1, creep model 7. *** WARNING *** CP = 33.774 TIME= 08:14:58 The creep integration algorithm does not converge for element 1063, material 1, creep model 7. *** LOAD STEP 2 SUBSTEP 1 NOT COMPLETED. CUM ITER = 9 *** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 3499.9 FORCE CONVERGENCE VALUE = 0.1220E+05 CRITERION= 140.5 DISP CONVERGENCE VALUE = 0.7182E-05 CRITERION= 0.1191E-05 EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7182E-05 FORCE CONVERGENCE VALUE = 4615. CRITERION= 165.1 DISP CONVERGENCE VALUE = 0.2639E-05 CRITERION= 0.1340E-05 EQUIL ITER 2 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2639E-05 FORCE CONVERGENCE VALUE = 3334. CRITERION= 171.2 DISP CONVERGENCE VALUE = 0.5434E-06 CRITERION= 0.1368E-05 <<< CONVERGED EQUIL ITER 3 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.5434E-06 FORCE CONVERGENCE VALUE = 420.6 CRITERION= 174.5 DISP CONVERGENCE VALUE = 0.1415E-06 CRITERION= 0.1395E-05 <<< CONVERGED EQUIL ITER 4 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1415E-06 FORCE CONVERGENCE VALUE = 56.05 CRITERION= 178.1 <<< CONVERGED *** NOTE *** CP = 42.682 TIME= 08:16:02 The creep ratio computed in this iteration is larger than the criterion of 1 leading to bisection of loads. You may try incrementing the load more slowly by increasing the number of substeps or use the CUTCONTROL command to re-specify this criterion. *** LOAD STEP 2 SUBSTEP 1 NOT COMPLETED. CUM ITER = 13 *** BEGIN BISECTION NUMBER 2 NEW TIME INCREMENT= 49.999 FORCE CONVERGENCE VALUE = 231.4 CRITERION= 160.8 DISP CONVERGENCE VALUE = 0.1313E-06 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1313E-06 FORCE CONVERGENCE VALUE = 1.864 CRITERION= 164.5 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 1 COMPLETED. CUM ITER = 13 *** TIME = 50.9990 TIME INC = 49.9990 *** CREEP RATIO = 0.2251 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO STEP TIME: NEXT TIME INC = 49.999 UNCHANGED FORCE CONVERGENCE VALUE = 4.794 CRITERION= 161.3 DISP CONVERGENCE VALUE = 0.1173E-08 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1173E-08 FORCE CONVERGENCE VALUE = 0.1846E-03 CRITERION= 164.6 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 2 COMPLETED. CUM ITER = 14 *** TIME = 100.998 TIME INC = 49.9990 *** CREEP RATIO = 0.2408 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO TIME STEP: NEXT TIME INC = 74.999 INCREASED (FACTOR = 1.5000) FORCE CONVERGENCE VALUE = 1.836 CRITERION= 161.4 DISP CONVERGENCE VALUE = 0.3532E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= -0.3532E-09 FORCE CONVERGENCE VALUE = 0.7529E-04 CRITERION= 164.7 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 3 COMPLETED. CUM ITER = 15 *** TIME = 175.997 TIME INC = 74.9985 *** CREEP RATIO = 0.4033 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO TIME STEP: NEXT TIME INC = 112.50 INCREASED (FACTOR = 1.5000) FORCE CONVERGENCE VALUE = 6.223 CRITERION= 161.5 DISP CONVERGENCE VALUE = 0.7754E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7754E-09 FORCE CONVERGENCE VALUE = 0.5940E-03 CRITERION= 164.8 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 4 COMPLETED. CUM ITER = 16 *** TIME = 288.494 TIME INC = 112.498 *** CREEP RATIO = 0.7223 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO TIME STEP: NEXT TIME INC = 155.75 INCREASED (FACTOR = 1.3844) FORCE CONVERGENCE VALUE = 12.00 CRITERION= 161.7 DISP CONVERGENCE VALUE = 0.1386E-08 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1386E-08 FORCE CONVERGENCE VALUE = 0.3751E-02 CRITERION= 165.0 <<< CONVERGED *** NOTE *** CP = 52.931 TIME= 08:33:03 The creep ratio computed in this iteration is larger than the criterion of 1 leading to bisection of loads. You may try incrementing the load more slowly by increasing the number of substeps or use the CUTCONTROL command to re-specify this criterion. *** LOAD STEP 2 SUBSTEP 5 NOT COMPLETED. CUM ITER = 18 *** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 117.98 FORCE CONVERGENCE VALUE = 7.010 CRITERION= 161.6 DISP CONVERGENCE VALUE = 0.8048E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.8048E-09 FORCE CONVERGENCE VALUE = 0.1070E-02 CRITERION= 164.9 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 5 COMPLETED. CUM ITER = 18 *** TIME = 406.474 TIME INC = 117.979 *** CREEP RATIO = 0.9336 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO STEP TIME: NEXT TIME INC = 117.98 UNCHANGED FORCE CONVERGENCE VALUE = 7.250 CRITERION= 161.8 DISP CONVERGENCE VALUE = 0.7858E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.7858E-09 FORCE CONVERGENCE VALUE = 0.1704E-02 CRITERION= 165.1 <<< CONVERGED *** NOTE *** CP = 72.899 TIME= 08:43:21 The creep ratio computed in this iteration is larger than the criterion of 1 leading to bisection of loads. You may try incrementing the load more slowly by increasing the number of substeps or use the CUTCONTROL command to re-specify this criterion. *** LOAD STEP 2 SUBSTEP 6 NOT COMPLETED. CUM ITER = 20 *** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 99.260 FORCE CONVERGENCE VALUE = 5.181 CRITERION= 161.7 DISP CONVERGENCE VALUE = 0.5590E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.5590E-09 FORCE CONVERGENCE VALUE = 0.7963E-03 CRITERION= 165.0 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 6 COMPLETED. CUM ITER = 20 *** TIME = 505.734 TIME INC = 99.2602 *** CREEP RATIO = 0.9617 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO STEP TIME: NEXT TIME INC = 99.260 UNCHANGED FORCE CONVERGENCE VALUE = 5.348 CRITERION= 161.9 DISP CONVERGENCE VALUE = 0.5539E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.5539E-09 FORCE CONVERGENCE VALUE = 0.1274E-02 CRITERION= 165.2 <<< CONVERGED *** NOTE *** CP = 76.643 TIME= 08:50:09 The creep ratio computed in this iteration is larger than the criterion of 1 leading to bisection of loads. You may try incrementing the load more slowly by increasing the number of substeps or use the CUTCONTROL command to re-specify this criterion. *** LOAD STEP 2 SUBSTEP 7 NOT COMPLETED. CUM ITER = 22 *** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 81.808 FORCE CONVERGENCE VALUE = 3.668 CRITERION= 161.8 DISP CONVERGENCE VALUE = 0.3781E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.3781E-09 FORCE CONVERGENCE VALUE = 0.5540E-03 CRITERION= 165.1 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 7 COMPLETED. CUM ITER = 22 *** TIME = 587.542 TIME INC = 81.8081 *** CREEP RATIO = 0.9594 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO STEP TIME: NEXT TIME INC = 81.808 UNCHANGED FORCE CONVERGENCE VALUE = 3.774 CRITERION= 161.9 DISP CONVERGENCE VALUE = 0.3761E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.3761E-09 FORCE CONVERGENCE VALUE = 0.8617E-03 CRITERION= 165.2 <<< CONVERGED *** NOTE *** CP = 80.387 TIME= 08:50:42 The creep ratio computed in this iteration is larger than the criterion of 1 leading to bisection of loads. You may try incrementing the load more slowly by increasing the number of substeps or use the CUTCONTROL command to re-specify this criterion. *** LOAD STEP 2 SUBSTEP 8 NOT COMPLETED. CUM ITER = 24 *** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 49.999 FORCE CONVERGENCE VALUE = 1.436 CRITERION= 161.9 DISP CONVERGENCE VALUE = 0.1419E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1419E-09 FORCE CONVERGENCE VALUE = 0.1041E-03 CRITERION= 165.2 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 8 COMPLETED. CUM ITER = 24 *** TIME = 637.541 TIME INC = 49.9990 *** CREEP RATIO = 0.6688 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO STEP TIME: NEXT TIME INC = 49.999 UNCHANGED FORCE CONVERGENCE VALUE = 1.464 CRITERION= 161.9 DISP CONVERGENCE VALUE = 0.1415E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1415E-09 FORCE CONVERGENCE VALUE = 0.1420E-03 CRITERION= 165.3 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 9 COMPLETED. CUM ITER = 25 *** TIME = 687.540 TIME INC = 49.9990 *** CREEP RATIO = 0.7711 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO TIME STEP: NEXT TIME INC = 64.841 INCREASED (FACTOR = 1.2968) FORCE CONVERGENCE VALUE = 2.488 CRITERION= 162.0 DISP CONVERGENCE VALUE = 0.2355E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.2355E-09 FORCE CONVERGENCE VALUE = 0.5821E-03 CRITERION= 165.3 <<< CONVERGED *** NOTE *** CP = 86.128 TIME= 08:53:34 The creep ratio computed in this iteration is larger than the criterion of 1 leading to bisection of loads. You may try incrementing the load more slowly by increasing the number of substeps or use the CUTCONTROL command to re-specify this criterion. *** LOAD STEP 2 SUBSTEP 10 NOT COMPLETED. CUM ITER = 27 *** BEGIN BISECTION NUMBER 1 NEW TIME INCREMENT= 49.999 FORCE CONVERGENCE VALUE = 1.493 CRITERION= 162.0 DISP CONVERGENCE VALUE = 0.1409E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1409E-09 FORCE CONVERGENCE VALUE = 0.1985E-03 CRITERION= 165.3 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 10 COMPLETED. CUM ITER = 27 *** TIME = 737.539 TIME INC = 49.9990 *** CREEP RATIO = 0.8992 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO STEP TIME: NEXT TIME INC = 49.999 UNCHANGED FORCE CONVERGENCE VALUE = 1.524 CRITERION= 162.1 DISP CONVERGENCE VALUE = 0.1399E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1399E-09 FORCE CONVERGENCE VALUE = 0.2715E-03 CRITERION= 165.4 <<< CONVERGED >>> SOLUTION CONVERGED AFTER EQUILIBRIUM ITERATION 1 *** LOAD STEP 2 SUBSTEP 11 COMPLETED. CUM ITER = 28 *** TIME = 787.538 TIME INC = 49.9990 *** CREEP RATIO = 1.060 CRITERION FOR CREEP RATIO CONTROL = 1.000 *** AUTO STEP TIME: NEXT TIME INC = 49.999 UNCHANGED FORCE CONVERGENCE VALUE = 1.557 CRITERION= 162.1 DISP CONVERGENCE VALUE = 0.1385E-09 CRITERION= 0.1313E-05 <<< CONVERGED EQUIL ITER 1 COMPLETED. NEW TRIANG MATRIX. MAX DOF INC= 0.1385E-09 FORCE CONVERGENCE VALUE = 0.3590E-03 CRITERION= 165.4 <<< CONVERGED *** ERROR *** CP = 92.368 TIME= 08:53:41 Equivalent creep strain ratio has exceeded the specified limit value. Since the time increment has reached the minimum value, the analysis is stopped. *** NOTE *** CP = 92.415 TIME= 08:53:41 During this loadstep the PCG iterative solver took more than 1000 iterations to solve the system of equations. In the future it may be more efficient to choose a direct solver, such as the SPARSE solver, for this analysis. NUMBER OF WARNING MESSAGES ENCOUNTERED= 9 NUMBER OF ERROR MESSAGES ENCOUNTERED= 1 ***** PROBLEM TERMINATED BY INDICATED ERROR(S) OR BY END OF INPUT DATA ***** *** WARNING *** CP = 130.386 TIME= 08:54:28 During this session the elapsed time exceeds the CPU time by 2038%. Often this indicates either a lack of physical memory (RAM) required to efficiently handle this simulation or it indicates a particularly slow hard drive configuration. This simulation can be expected to run faster on identical hardware if additional RAM or a faster hard drive configuration is made available. For more details, please see the ANSYS Performance Guide which is part of the ANSYS Help system. +--------- D I S T R I B U T E D A N S Y S S T A T I S T I C S ------------+ Release: Release 16.2 Build: 16.2 Update: UP20150629 Platform: WINDOWS x64 Date Run: 12/01/2016 Time: 08:54 Windows Process ID: 4380 Processor Model: Intel(R) Core(TM) i5-2520M CPU @ 2.50GHz 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 : 2 Number of processes requested : 2 Number of threads per process requested : 1 Total number of cores requested : 2 (Distributed Memory Parallel) MPI Type: NATIVE GPU Acceleration: Not Requested Job Name: file0 Input File: dummy.dat Latency time from master to core 1 = 0.290 microseconds Communication speed from master to core 1 = 3508.06 MB/sec Total CPU time for main thread : 127.4 seconds Total CPU time summed for all threads : 130.4 seconds Elapsed time spent pre-processing model (/PREP7) : 2.1 seconds Elapsed time spent solution - preprocessing : 0.8 seconds Elapsed time spent computing solution : 2648.2 seconds Elapsed time spent solution - postprocessing : 0.5 seconds Elapsed time spent post-processing model (/POST1) : 0.0 seconds Equation solver computational rate : 3784.1 Mflops Maximum total memory used : 80.0 MB Maximum total memory allocated : 3136.0 MB Maximum total memory available : 8 GB +------ E N D D I S T R I B U T E D A N S Y S S T A T I S T I C S -------+ *---------------------------------------------------------------------------* | | | DISTRIBUTED ANSYS RUN COMPLETED | | | |---------------------------------------------------------------------------| | | | Ansys Release 16.2 Build 16.2 UP20150629 WINDOWS x64 | | | |---------------------------------------------------------------------------| | | | Database Requested(-db) 1024 MB Scratch Memory Requested 1024 MB | | Maximum Database Used 5 MB Maximum Scratch Memory Used 41 MB | | | |---------------------------------------------------------------------------| | | | CP Time (sec) = 130.386 Time = 08:54:28 | | Elapsed Time (sec) = 2723.000 Date = 12/01/2016 | | | *---------------------------------------------------------------------------*