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License Manager Release 19.0 ***** 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 19.0 BUILD= 19.0 UP20171214 VERSION=WINDOWS x64 CURRENT JOBNAME=file 15:44:01 MAY 13, 2020 CP= 0.188 PARAMETER _DS_PROGRESS = 999.0000000 /INPUT FILE= ds.dat LINE= 0 DO NOT WRITE ELEMENT RESULTS INTO DATABASE *GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 15.7336111 TITLE= Test 1--Static Structural (A5) SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\andre\Documents\Titomic\Test 1 - 12.05.20\_ProjectScratch\Scr5C95\ SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\andre\Documents\Titomic\Test 1 - 12.05.20\Test 1_files\dp0\SYS\MECH\ SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_USERFILES_DIR(1) = C:\Users\andre\Documents\Titomic\Test 1 - 12.05.20\Test 1_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 19.0 19.0 *** ANSYS Mechanical Enterprise 20120530 VERSION=WINDOWS x64 15:44:01 MAY 13, 2020 CP= 0.297 Test 1--Static Structural (A5) ***** ANSYS ANALYSIS DEFINITION (PREP7) ***** *********** Nodes for the whole assembly *********** *********** Nodes for all Remote Points *********** *********** Elements for Body 1 "Solid" *********** *********** Elements for Body 2 "Solid" *********** *********** Send User Defined Coordinate System(s) *********** *********** Set Reference Temperature *********** *********** Send Materials *********** *********** Create Contact "Frictional - FrictionHub To FrictionWheel" ******** Real Constant Set For Above Contact Is 4 & 3 *********** Create Contact "Frictionless - FrictionlessHub To FrictionlessWheel Real Constant Set For Above Contact Is 6 & 5 *********** Send Named Selection as Node Component *********** *********** Send Named Selection as Node Component *********** *********** Send Named Selection as Node Component *********** *********** Send Named Selection as Node Component *********** *********** Send Named Selection as Node Component *********** *********** Send Named Selection as Node Component *********** *********** Send Named Selection as Node Component *********** *********** Send Named Selection as Node Component *********** *********** Fixed Supports *********** *********** Define Pressure Using Surface Effect 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 Remote Point "Internal Remote Point 5" *********** *********** Create Remote Point "Internal Remote Point 6" *********** *********** Create Remote Point "Internal Remote Point 7" *********** *********** Create Remote Point "Internal Remote Point 8" *********** *********** Create Remote Point "Internal Remote Point 9" *********** *********** Create Remote Point "Internal Remote Point 10" *********** *********** Create Remote Point "Internal Remote Point 11" *********** *********** Create Remote Point "Internal Remote Point 12" *********** *********** Create Remote Point "Internal Remote Point 13" *********** *********** Create Remote Point "Internal Remote Point 14" *********** *********** Create Remote Point "Internal Remote Point 15" *********** *********** Create Remote Point "Internal Remote Point 16" *********** *********** Construct Remote Force *********** *********** Construct Remote Force *********** *********** Create Joint "Cylindrical - Solid To Solid" *********** Real Constant Set For Above Joint Is 40 *********** Create Joint "Cylindrical - Solid To Solid" *********** Real Constant Set For Above Joint Is 41 *********** Create Joint "Cylindrical - Solid To Solid" *********** Real Constant Set For Above Joint Is 42 *********** Create Joint "Cylindrical - Solid To Solid" *********** Real Constant Set For Above Joint Is 43 *********** Create Joint "Cylindrical - Solid To Solid" *********** Real Constant Set For Above Joint Is 44 *********** Create Joint "Cylindrical - Solid To Solid" *********** Real Constant Set For Above Joint Is 45 *********** Create Spring Connection "Longitudinal - Solid To Solid" ********** Real Constant Set For Above Spring Connection Is 46 ***** ROUTINE COMPLETED ***** CP = 5.625 --- Number of total nodes = 543548 --- Number of contact elements = 22471 --- Number of spring elements = 0 --- Number of bearing elements = 0 --- Number of solid elements = 341495 --- Number of condensed parts = 0 --- Number of total elements = 363989 *GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 15.7347222 **************************************************************************** ************************* 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 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 OF 1 **************** SELECT FOR ITEM=TYPE COMPONENT= IN RANGE 7 TO 7 STEP 1 6518 ELEMENTS (OF 363989 DEFINED) SELECTED BY ESEL COMMAND. SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET. 13513 NODES (OF 543548 DEFINED) SELECTED FROM 6518 SELECTED ELEMENTS BY NSLE COMMAND. GENERATE SURFACE LOAD PRES ON SURFACE DEFINED BY ALL SELECTED NODES SET ACCORDING TO TABLE PARAMETER = _LOADVARI321 NUMBER OF PRES ELEMENT FACE LOADS STORED = 6518 ALL SELECT FOR ITEM=NODE COMPONENT= IN RANGE 1 TO 2070630 STEP 1 543548 NODES (OF 543548 DEFINED) SELECTED BY NSEL COMMAND. ALL SELECT FOR ITEM=ELEM COMPONENT= IN RANGE 1 TO 1452885 STEP 1 363989 ELEMENTS (OF 363989 DEFINED) SELECTED BY ESEL COMMAND. SELECT FOR ITEM=NODE COMPONENT= IN RANGE 2070629 TO 2070629 STEP 1 1 NODES (OF 543548 DEFINED) SELECTED BY NSEL COMMAND. SPECIFIED NODAL LOAD FX FOR SELECTED NODES 1 TO 2070630 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI342X SPECIFIED NODAL LOAD FY FOR SELECTED NODES 1 TO 2070630 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI342Y SPECIFIED NODAL LOAD FZ FOR SELECTED NODES 1 TO 2070630 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI342Z SELECT FOR ITEM=NODE COMPONENT= IN RANGE 2070630 TO 2070630 STEP 1 1 NODES (OF 543548 DEFINED) SELECTED BY NSEL COMMAND. SPECIFIED NODAL LOAD FX FOR SELECTED NODES 1 TO 2070630 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI345X SPECIFIED NODAL LOAD FY FOR SELECTED NODES 1 TO 2070630 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI345Y SPECIFIED NODAL LOAD FZ FOR SELECTED NODES 1 TO 2070630 BY 1 SET ACCORDING TO TABLE PARAMETER = _LOADVARI345Z ALL SELECT FOR ITEM=NODE COMPONENT= IN RANGE 1 TO 2070630 STEP 1 543548 NODES (OF 543548 DEFINED) SELECTED BY NSEL COMMAND. ALL SELECT FOR ITEM=ELEM COMPONENT= IN RANGE 1 TO 1452885 STEP 1 363989 ELEMENTS (OF 363989 DEFINED) SELECTED BY ESEL COMMAND. PRINTOUT RESUMED BY /GOP USE AUTOMATIC TIME STEPPING THIS LOAD STEP USE 1 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM FOR AUTOMATIC TIME STEPPING: USE 10 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 = 6.578 TIME= 15:44:05 Element shape checking is currently inactive. Issue SHPP,ON or SHPP,WARN to reactivate, if desired. *** WARNING *** CP = 7.141 TIME= 15:44:06 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. *** WARNING *** CP = 7.141 TIME= 15:44:06 The sparse solver must be used if any current technology elements with u-P formulation or MPC184 elements using Lagrangian multiplier are included in the model. The equation solver option has been switched to the sparse solver. *** NOTE *** CP = 7.906 TIME= 15:44:06 The model data was checked and warning messages were found. Please review output or errors file ( C:\Users\andre\Documents\Titomic\Test 1 - 12.05.20\_ProjectScratch\Scr5C95\file.err ) for these warning messages. *** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS *** --- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS --- ELEMENT TYPE 1 IS SOLID187. IT IS NOT ASSOCIATED WITH FULLY INCOMPRESSIBLE HYPERELASTIC MATERIALS. NO SUGGESTION IS AVAILABLE AND NO RESETTING IS NEEDED. ELEMENT TYPE 2 IS SOLID187. IT IS NOT ASSOCIATED WITH FULLY INCOMPRESSIBLE HYPERELASTIC MATERIALS. NO SUGGESTION IS AVAILABLE AND NO RESETTING IS NEEDED. *** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE Release 19.0 19.0 *** ANSYS Mechanical Enterprise 20120530 VERSION=WINDOWS x64 15:44:06 MAY 13, 2020 CP= 8.047 Test 1--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 NEWTON-RAPHSON OPTION . . . . . . . . . . . . .PROGRAM CHOSEN GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC *** WARNING *** CP = 8.453 TIME= 15:44:07 Material number 46 (used by element 1430390 ) 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 = 8.844 TIME= 15:44:07 The step data was checked and warning messages were found. Please review output or errors file ( C:\Users\andre\Documents\Titomic\Test 1 - 12.05.20\_ProjectScratch\Scr5C95\file.err ) for these warning messages. *** NOTE *** CP = 8.844 TIME= 15:44:07 This nonlinear analysis defaults to using the full Newton-Raphson solution procedure. This can be modified using the NROPT command. *** NOTE *** CP = 9.328 TIME= 15:44:08 Internal nodes from 2070631 to 2070664 are created. 16 internal nodes are used for handling degrees of freedom on pilot nodes of rigid target surfaces. 18 internal nodes are used for non-contact elements with mixed formulation. *** NOTE *** CP = 15.531 TIME= 15:44:12 The initial memory allocation (-m) has been exceeded. Supplemental memory allocations are being used. 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 . . . . . . . . . 1 MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . . 10 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 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 SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr *WARNING*: Node 380990 has been used on different contact pairs (real ID 10 & 12). These two pairs will be merged. Please check the model carefully. *WARNING*: Some MPC/Lagrange based elements (e.g.1449884) in real constant set 36 overlap with other MPC/Lagrange based elements (e.g.1451398) in real constant set 38 which can cause overconstraint. *** NOTE *** CP = 16.438 TIME= 15:44:13 Symmetric Deformable- deformable contact pair identified by real constant set 3 and contact element type 3 has been set up. The companion pair has real constant set ID 4. Both pairs should have the same behavior. ANSYS will deactivate the current pair and keep its companion pair, resulting in asymmetric contact. Small sliding logic is assumed Contact algorithm: Augmented Lagrange method Contact detection at: Gauss integration point Contact stiffness factor FKN 1.0000 The resulting initial contact stiffness 0.55107E+15 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.30397E-03 Max. initial friction coefficient MU 0.50000E-01 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.42921E-04 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.42921E-02 Average contact pair depth 0.30397E-02 Default pinball region factor PINB 1.0000 The resulting pinball region 0.30397E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 16.438 TIME= 15:44:13 Max. Initial penetration 9.545229742E-07 was detected between contact element 1431955 and target element 1435839. You may move entire target surface by : x= 6.686653218E-07, y= -6.750456953E-07, z= 9.118171374E-08,to reduce initial penetration. **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Symmetric Deformable- deformable contact pair identified by real constant set 4 and contact element type 3 has been set up. The companion pair has real constant set ID 3. Both pairs should have the same behavior. ANSYS will keep the current pair and deactivate its companion pair, resulting in asymmetric contact. Small sliding logic is assumed Contact algorithm: Augmented Lagrange method Contact detection at: Gauss integration point Contact stiffness factor FKN 1.0000 The resulting initial contact stiffness 0.55107E+15 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.25768E-03 Max. initial friction coefficient MU 0.50000E-01 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.40387E-04 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.40387E-02 Average contact pair depth 0.25768E-02 Default pinball region factor PINB 1.0000 The resulting pinball region 0.25768E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 16.438 TIME= 15:44:13 Max. Initial penetration 9.971493862E-07 was detected between contact element 1434539 and target element 1430451. You may move entire target surface by : x= -6.982532085E-07, y= 7.05181438E-07, z= -9.73061899E-08,to reduce initial penetration. **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Symmetric Deformable- deformable contact pair identified by real constant set 5 and contact element type 5 has been set up. The companion pair has real constant set ID 6. Both pairs should have the same behavior. ANSYS will deactivate the current pair and keep its companion pair, resulting in asymmetric contact. Small sliding logic is assumed Contact algorithm: Augmented Lagrange method Contact detection at: Gauss integration point Contact stiffness factor FKN 1.0000 The resulting initial contact stiffness 0.47386E+15 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.30403E-03 Frictionless contact pair is defined Update contact stiffness at each iteration Average contact surface length 0.41714E-02 Average contact pair depth 0.30403E-02 Default pinball region factor PINB 1.0000 The resulting pinball region 0.30403E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 16.438 TIME= 15:44:13 Max. Initial penetration 1.094222043E-06 was detected between contact element 1437026 and target element 1439336. You may move entire target surface by : x= -1.653588229E-07, y= 5.925929773E-10, z= -1.081655207E-06,to reduce initial penetration. **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Symmetric Deformable- deformable contact pair identified by real constant set 6 and contact element type 5 has been set up. The companion pair has real constant set ID 5. Both pairs should have the same behavior. ANSYS will keep the current pair and deactivate its companion pair, resulting in asymmetric contact. Small sliding logic is assumed Contact algorithm: Augmented Lagrange method Contact detection at: Gauss integration point Contact stiffness factor FKN 1.0000 The resulting initial contact stiffness 0.47386E+15 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.29967E-03 Frictionless contact pair is defined Update contact stiffness at each iteration Average contact surface length 0.38426E-02 Average contact pair depth 0.29967E-02 Default pinball region factor PINB 1.0000 *WARNING*: The default pinball radius may be too small to capture contacting zone under small sliding assumption. Redefine the pinball radius if necessary. The resulting pinball region 0.29967E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 16.438 TIME= 15:44:13 Max. Initial penetration 1.191868173E-06 was detected between contact element 1438339 and target element 1436095. You may move entire target surface by : x= 1.852512095E-07, y= -2.998823519E-11, z= -1.177383425E-06,to reduce initial penetration. **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Rigid-constraint surface identified by real constant set 8 and contact element type 8 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2070615 which connects to other element 1430390. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Rigid-constraint surface identified by real constant set 10 and contact element type 10 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2070616 which connects to other element 1430390. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 32. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Rigid-constraint surface identified by real constant set 12 and contact element type 12 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2070617 which connects to other element 1430391. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 10. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Force-distributed-surface identified by real constant set 14 and contact element type 14 has been set up. The pilot node 2070618 is used to apply the force which connects to other element 1430391. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Rigid-constraint surface identified by real constant set 16 and contact element type 16 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2070619 which connects to other element 1430392. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 10. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Force-distributed-surface identified by real constant set 18 and contact element type 18 has been set up. The pilot node 2070620 is used to apply the force which connects to other element 1430392. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Rigid-constraint surface identified by real constant set 20 and contact element type 20 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2070621 which connects to other element 1430393. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 10. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Force-distributed-surface identified by real constant set 22 and contact element type 22 has been set up. The pilot node 2070622 is used to apply the force which connects to other element 1430393. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Rigid-constraint surface identified by real constant set 24 and contact element type 24 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2070623 which connects to other element 1430394. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 10. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Force-distributed-surface identified by real constant set 26 and contact element type 26 has been set up. The pilot node 2070624 is used to apply the force which connects to other element 1430394. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Rigid-constraint surface identified by real constant set 28 and contact element type 28 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2070625 which connects to other element 1430395. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 10. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Force-distributed-surface identified by real constant set 30 and contact element type 30 has been set up. The pilot node 2070626 is used to apply the force which connects to other element 1430395. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Rigid-constraint surface identified by real constant set 32 and contact element type 32 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2070627 which connects to other element 1430396. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 10. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Force-distributed-surface identified by real constant set 34 and contact element type 34 has been set up. The pilot node 2070628 is used to apply the force which connects to other element 1430396. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Force-distributed-surface identified by real constant set 36 and contact element type 36 has been set up. The pilot node 2070629 is used to apply the force. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ *WARNING*: Certain contact elements (for example 1451065&1452867) overlap each other. Please verify constraints (including rotational degrees of freedom) on the pilot node by yourself. **************************************** *** NOTE *** CP = 16.438 TIME= 15:44:13 Force-distributed-surface identified by real constant set 38 and contact element type 38 has been set up. The pilot node 2070630 is used to apply the force. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ *WARNING*: Certain contact elements (for example 1452867&1450990) overlap each other. Please verify constraints (including rotational degrees of freedom) on the pilot node by yourself. **************************************** *** WARNING *** CP = 16.438 TIME= 15:44:13 Overconstraint may occur for Lagrange multiplier or MPC based contact algorithm. The reasons for possible overconstraint are: *** WARNING *** CP = 16.438 TIME= 15:44:13 Certain contact elements (for example 1452867 & 1450990) overlap with other. **************************************** MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC. The FEA model contains 0 external CE equations and 14922 internal CE equations. ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 3 *** NOTE *** CP = 54.531 TIME= 15:44:38 Contact pair is inactive. ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 4 Max. Penetration of -9.971493862E-07 has been detected between contact element 1434539 and target element 1430451. For total 1300 contact elements, there are 1286 elements are in contact. There are 1286 elements are in sticking. Contacting area 6.178832563E-03. Max. Pinball distance 2.576802064E-03. One of the contact searching regions contains at least 33 target elements. Max. Pressure/force 142721668. Max. Normal stiffness 1.431296753E+14. Min. Normal stiffness 1.431296753E+14. Max. Tangential stiffness 3.424536142E+11. Min. Tangential stiffness 3.424536142E+11. ************************************************* ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 5 *** NOTE *** CP = 54.531 TIME= 15:44:38 Contact pair is inactive. ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 6 Max. Penetration of -1.191868173E-06 has been detected between contact element 1438339 and target element 1436095. For total 719 contact elements, there are 292 elements are in contact. Contacting area 7.839052235E-04. Max. Pinball distance 2.996681314E-03. One of the contact searching regions contains at least 36 target elements. Max. Pressure/force 267862041. Max. Normal stiffness 2.247413318E+14. Min. Normal stiffness 2.247413318E+14. ************************************************* *********** PRECISE MASS SUMMARY *********** TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN Translational mass | Coupled translational/rotational mass 16.890 0.0000 0.0000 | 0.0000 5.8660 0.70566 0.0000 16.890 0.0000 | -5.8660 0.0000 -0.31005E-03 0.0000 0.0000 16.890 | -0.70566 0.31005E-03 0.0000 ------------------------------------------ | ------------------------------------------ | Rotational mass (inertia) | 2.3759 -0.27720E-04 0.14546E-03 | -0.27720E-04 2.4844 0.24508 | 0.14546E-03 0.24508 0.33881 TOTAL MASS = 16.890 The mass principal axes coincide with the global Cartesian axes CENTER OF MASS (X,Y,Z)= -0.18357E-04 -0.41779E-01 0.34730 TOTAL INERTIA ABOUT CENTER OF MASS 0.30921 -0.14767E-04 0.37779E-04 -0.14767E-04 0.44716 0.67616E-05 0.37779E-04 0.67616E-05 0.30933 The inertia principal axes coincide with the global Cartesian axes *** MASS SUMMARY BY ELEMENT TYPE *** TYPE MASS 1 6.51675 2 10.3736 Range of element maximum matrix coefficients in global coordinates Maximum = 3.04989176E+11 at element 223155. Minimum = 13299085.4 at element 147352. *** ELEMENT MATRIX FORMULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 114144 SOLID187 19.609 0.000172 2 227351 SOLID187 39.656 0.000174 3 2804 CONTA174 1.000 0.000357 4 2804 TARGE170 0.156 0.000056 5 1681 CONTA174 0.656 0.000390 6 1681 TARGE170 0.094 0.000056 7 6518 SURF154 0.906 0.000139 8 654 CONTA174 0.125 0.000191 9 1 TARGE170 0.000 0.000000 10 1278 CONTA174 0.219 0.000171 11 1 TARGE170 0.000 0.000000 12 56 CONTA174 0.000 0.000000 13 1 TARGE170 0.000 0.000000 14 280 CONTA174 0.031 0.000112 15 1 TARGE170 0.000 0.000000 16 56 CONTA174 0.000 0.000000 17 1 TARGE170 0.000 0.000000 18 288 CONTA174 0.094 0.000326 19 1 TARGE170 0.000 0.000000 20 56 CONTA174 0.062 0.001116 21 1 TARGE170 0.000 0.000000 22 306 CONTA174 0.062 0.000204 23 1 TARGE170 0.000 0.000000 24 56 CONTA174 0.031 0.000558 25 1 TARGE170 0.000 0.000000 26 266 CONTA174 0.000 0.000000 27 1 TARGE170 0.000 0.000000 28 56 CONTA174 0.062 0.001116 29 1 TARGE170 0.000 0.000000 30 290 CONTA174 0.000 0.000000 31 1 TARGE170 0.000 0.000000 32 52 CONTA174 0.000 0.000000 33 1 TARGE170 0.000 0.000000 34 284 CONTA174 0.062 0.000220 35 1 TARGE170 0.000 0.000000 36 1487 CONTA174 0.156 0.000105 37 1 TARGE170 0.000 0.000000 38 1518 CONTA174 0.219 0.000144 39 1 TARGE170 0.000 0.000000 40 1 MPC184 0.000 0.000000 41 1 MPC184 0.000 0.000000 42 1 MPC184 0.000 0.000000 43 1 MPC184 0.000 0.000000 44 1 MPC184 0.000 0.000000 45 1 MPC184 0.000 0.000000 46 1 COMBIN14 0.016 0.015625 Time at end of element matrix formulation CP = 54.5625. ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.rdb FOR POSSIBLE RESUME FROM THIS POINT FORCE CONVERGENCE VALUE = 0.2052E+06 CRITERION= 14.27 SPARSE MATRIX DIRECT SOLVER. Number of equations = 1607652, Maximum wavefront = 36684 Memory allocated for solver = 2577.865 MB Memory required for in-core solution = 12375.224 MB Memory required for out-of-core solution = 2174.964 MB *** WARNING *** CP = 76.125 TIME= 15:45:18 The Sparse Matrix Solver is currently running in the out-of-core memory mode. This memory mode may provide significantly worse performance compared to the in-core memory mode, depending on the amount of available system memory and I/O speed. Please monitor the solver performance to ensure that the large amount of I/O to the solver files does not create a bottleneck for performance. *** WARNING *** CP = 76.125 TIME= 15:45:18 Pivoting has been activated for the Sparse Matrix Solver . The memory required may greatly exceed the predicted amount. In that event, use the DSPOPTION command to change the memory mode and/or memory size used by the Sparse Matrix Solver. curEqn= 194656 totEqn= 1607652 Job CP sec= 194.500 Factor Done= 26% Factor Wall sec= 78.965 rate= 15092.7 Mflops curEqn= 381463 totEqn= 1607652 Job CP sec= 320.531 Factor Done= 51% Factor Wall sec= 160.848 rate= 14601.0 Mflops curEqn= 599442 totEqn= 1607652 Job CP sec= 437.562 Factor Done= 77% Factor Wall sec= 237.295 rate= 14910.1 Mflops GetOverlappedResult failed. (112) ********** CURRENT DISK AND DIRECTORY USAGE ********** Volume in drive C is OS Volume Serial Number is 40D3-6139 Directory of C:\Users\andre\Documents\Titomic\Test 1 - 12.05.20\_ProjectScratch\Scr5C95 13/05/2020 03:47 PM . 13/05/2020 03:47 PM .. 13/05/2020 11:19 AM 0 ANSYSFatalError.log 13/05/2020 11:19 AM 0 ANSYSTraceBack.log 13/05/2020 03:43 PM 83,320 CAERep.xml 13/05/2020 03:43 PM 107,657,511 ds.dat 13/05/2020 03:49 PM 26 ds_file.stat 13/05/2020 03:44 PM 115 ds_file.xml 13/05/2020 03:43 PM 70 dummy.dat 13/05/2020 03:44 PM 78 file.bat 13/05/2020 03:44 PM 7,345 file.cnd 13/05/2020 03:45 PM 0 file.DSPmatK 13/05/2020 03:45 PM 0 file.DSPstack 13/05/2020 03:45 PM 0 file.DSPsymb 13/05/2020 03:45 PM 10,327,709,184 file.DSPtri 13/05/2020 03:45 PM 0 file.DSPtriU 13/05/2020 03:44 PM 0 file.emat 13/05/2020 03:45 PM 2,729 file.err 13/05/2020 03:44 PM 0 file.esav 13/05/2020 03:45 PM 915,275,776 file.full 13/05/2020 03:44 PM 814,970 file.ldhi 13/05/2020 03:44 PM 0 file.lock 13/05/2020 03:44 PM 10 file.log 13/05/2020 03:44 PM 2 file.mntr 13/05/2020 03:44 PM 0 file.osav 13/05/2020 03:44 PM 0 file.page 13/05/2020 03:44 PM 289,210,368 file.rdb 13/05/2020 03:44 PM 0 file.rst 13/05/2020 03:49 PM 160 file.stat 13/05/2020 03:43 PM 37,130 MatML.xml 13/05/2020 03:43 PM 632 SecInput.txt 13/05/2020 03:49 PM 47,646 solve.out 30 File(s) 11,640,847,072 bytes 2 Dir(s) 0 bytes free *** ERROR *** CP = 500.719 TIME= 15:50:20 An input/output error has occurred on the process with MPI Rank ID = 0. Please check to see if the disk is full. NUMBER OF WARNING MESSAGES ENCOUNTERED= 8 NUMBER OF ERROR MESSAGES ENCOUNTERED= 1 ***** PROBLEM TERMINATED BY INDICATED ERROR(S) OR BY END OF INPUT DATA ***** +--------------------- A N S Y S S T A T I S T I C S ------------------------+ Release: Release 19.0 Build: 19.0 Update: UP20171214 Platform: WINDOWS x64 Date Run: 05/13/2020 Time: 15:50 Process ID: 16080 Operating System: Windows 10 (Build: 18362) Processor Model: Intel(R) Core(TM) i5-7200U CPU @ 2.50GHz Compiler: Intel(R) FORTRAN Compiler Version 15.0.7 (Build: 20160518) Intel(R) C/C++ Compiler Version 15.0.7 (Build: 20160518) Intel(R) Math Kernel Library Version 2017.0.2 Product Build 20170126 Number of machines requested : 1 Total number of cores available : 4 Number of physical cores available : 2 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\andre\Documents\Titomic\Test 1 - 12.05.20\_ProjectScratch\Scr5C95 Total CPU time for main thread : 309.2 seconds Total CPU time summed for all threads : 502.8 seconds Elapsed time spent pre-processing model (/PREP7) : 4.3 seconds Elapsed time spent solution - preprocessing : 5.2 seconds Elapsed time spent computing solution : 367.5 seconds Elapsed time spent solution - postprocessing : 0.0 seconds Elapsed time spent post-processing model (/POST1) : 0.0 seconds Equation solver used : Sparse (symmetric) Maximum total memory used : 3925.0 MB Maximum total memory allocated : 5094.0 MB Total physical memory available : 8 GB +------------------ E N D A N S Y S S T A T I S T I C S -------------------+ *---------------------------------------------------------------------------* | | | ANSYS RUN COMPLETED | | | |---------------------------------------------------------------------------| | | | Ansys Release 19.0 Build 19.0 UP20171214 WINDOWS x64 | | | |---------------------------------------------------------------------------| | | | Database Requested(-db) 1024 MB Scratch Memory Requested 1024 MB | | Maximum Database Used 419 MB Maximum Scratch Memory Used 3506 MB | | | |---------------------------------------------------------------------------| | | | CP Time (sec) = 502.781 Time = 15:50:22 | | Elapsed Time (sec) = 383.000 Date = 05/13/2020 | | | *---------------------------------------------------------------------------*