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License Manager 2020 R2 ***** ANSYS COMMAND LINE ARGUMENTS ***** BATCH MODE REQUESTED (-b) = NOLIST INPUT FILE COPY MODE (-c) = COPY DISTRIBUTED MEMORY PARALLEL REQUESTED 4 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS TOTAL OF 4 CORES REQUESTED DESIGNXPLORER REQUESTED INPUT FILE NAME = \\NGR-FILE\01-Office$\Projekte\Entwicklungsprojekte\E-20914_ReaktorkopfModifikation\02_KonstruktionMechanisch\FEM Analyse Durchbiegung Lochplatte\CAD\_ProjectScratch\Scr0C57\dummy.dat OUTPUT FILE NAME = \\ngr.local\01-NGR-AUT\Office\Projekte\Entwicklungsprojekte\E-20914_ReaktorkopfModifikation\02_KonstruktionMechanisch\FEM Analyse Durchbiegung Lochplatte\CAD\_ProjectScratch\Scr0C57\solve.out START-UP FILE MODE = NOREAD STOP FILE MODE = NOREAD RELEASE= 2020 R2 BUILD= 20.2 UP20200601 VERSION=WINDOWS x64 CURRENT JOBNAME=file0 19:01:10 DEC 16, 2020 CP= 0.250 PARAMETER _DS_PROGRESS = 999.0000000 /INPUT FILE= ds.dat LINE= 0 *** NOTE *** CP = 0.328 TIME= 19:01:10 The /CONFIG,NOELDB command is not valid in a Distributed ANSYS solution. Command is ignored. *GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 19.0194444 TITLE= Durchbiegung Lochplatte--Static Structural (I5) SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_PROJECTSCRATCH_DIR(1) = \\ngr.local\01-NGR-AUT\Office\Projekte\Entwicklungsprojekte\E-20914_ReaktorkopfModifikation\02_KonstruktionMechanisch\FEM Analyse Durchbiegung Lochplatte\CAD\_ProjectScratch\Scr0C57\ SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_SOLVERFILES_DIR(1) = \\ngr.local\01-NGR-AUT\Office\Projekte\Entwicklungsprojekte\E-20914_ReaktorkopfModifikation\02_KonstruktionMechanisch\FEM Analyse Durchbiegung Lochplatte\CAD\Durchbiegung Lochplatte_files\dp0\SYS-8\MECH\ SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_USERFILES_DIR(1) = \\ngr.local\01-NGR-AUT\Office\Projekte\Entwicklungsprojekte\E-20914_ReaktorkopfModifikation\02_KonstruktionMechanisch\FEM Analyse Durchbiegung Lochplatte\CAD\Durchbiegung Lochplatte_files\user_files\ --- Data in consistent NMM units. See Solving Units in the help system for more MPA UNITS SPECIFIED FOR INTERNAL LENGTH = MILLIMETERS (mm) MASS = TONNE (Mg) TIME = SECONDS (sec) TEMPERATURE = CELSIUS (C) TOFFSET = 273.0 FORCE = NEWTON (N) HEAT = MILLIJOULES (mJ) INPUT UNITS ARE ALSO SET TO MPA *** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2020 R2 20.2 *** DISTRIBUTED ANSYS Academic Research Mechanical 01132000 VERSION=WINDOWS x64 19:01:10 DEC 16, 2020 CP= 0.328 Durchbiegung Lochplatte--Static Structural (I5) ***** ANSYS ANALYSIS DEFINITION (PREP7) ***** *********** Nodes for the whole assembly *********** *********** Nodes for all Remote Points *********** *********** Elements for Body 1 "SYS-8\12tel FEM dopp DF_Lochplatte_A-09105-010 *********** Elements for Body 2 "SYS-8\12tel FEM dopp DF_Druckverteilplatte_A-0 *********** Elements for Body 3 "SYS-8\12tel FEM dopp DF_Grafitdichtung.par:1" *********** Elements for Body 4 "SYS-8\Solid" *********** *********** Send User Defined Coordinate System(s) *********** *********** Set Reference Temperature *********** *********** Send Materials *********** *********** Create Contact "Frictional - SYS-8\12tel FEM dopp DF_Lochplatte_A-0 Real Constant Set For Above Contact Is 6 & 5 *********** Create Contact "Frictional - SYS-8\12tel FEM dopp DF_Lochplatte_A-0 Real Constant Set For Above Contact Is 8 & 7 *********** Create Contact "Frictional - SYS-8\Solid To SYS-8\12tel FEM dopp DF Real Constant Set For Above Contact Is 10 & 9 *********** Send Named Selection as Node Component *********** *********** Fixed Supports *********** *********** Node Rotations *********** *********** Define Pressure Using Surface Effect Elements *********** *********** Create Remote Point "Internal Remote Point 7" *********** *********** Create Remote Point "Internal Remote Point 8" *********** *********** 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 Beam Connection "Circular - SYS-8\12tel FEM dopp DF_Druckver Real Constant Set For Above Beam Connection Is 28 *********** Create Beam Connection "Circular - SYS-8\12tel FEM dopp DF_Lochplat Real Constant Set For Above Beam Connection Is 29 *********** Create Beam Connection "Circular - SYS-8\12tel FEM dopp DF_Lochplat Real Constant Set For Above Beam Connection Is 30 *********** Create Beam Connection "Circular - SYS-8\12tel FEM dopp DF_Druckver Real Constant Set For Above Beam Connection Is 31 *********** Create Bolt Pretension "Bolt Pretension" *********** *********** Create Bolt Pretension "Bolt Pretension 2" *********** *********** Create Bolt Pretension "Bolt Pretension 3" *********** *********** Create Bolt Pretension "Bolt Pretension 4" *********** *********** Create Periodic/Cyclic Symmetry *********** *********** Create Periodic/Cyclic Symmetry *********** *********** Create Periodic/Cyclic Symmetry *********** *********** Create Periodic/Cyclic Symmetry *********** LIST CYCLIC SYMMETRY SOLUTION OPTION STATUS LIST OF CYCLIC SYMMETRY HARMONIC INDICES TO BE SOLVED 0 THROUGH 0 ALL CYCLIC SYMMETRY EDGE COMPONENT PAIRS TO USE ALL ACTIVE DEGREES OF FREEDOM CYCLIC SYMMETRY SPECIFIED DISTANCE TOLERANCE (RELATIVE) = 0.10000E-03 LOADINGS FOR STATIC CYCLIC SYMMETRY ARE TO BE APPLIED TO ALL SECTORS. USER WILL APPLY NODAL ROTATIONS TO ALL EDGE COMPONENT NODES (ALL AUTOMATIC ROTATIONS SUPPRESSED) ***** ROUTINE COMPLETED ***** CP = 25.062 --- Number of total nodes = 2130921 --- Number of contact elements = 57858 --- Number of spring elements = 0 --- Number of bearing elements = 0 --- Number of solid elements = 1452708 --- Number of condensed parts = 0 --- Number of total elements = 1510586 *GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 19.0236111 **************************************************************************** ************************* SOLUTION ******************************** **************************************************************************** ***** ANSYS SOLUTION ROUTINE ***** PERFORM A STATIC ANALYSIS THIS WILL BE A NEW ANALYSIS PARAMETER _THICKRATIO = 0.7500000000 USE SPARSE MATRIX DIRECT SOLVER 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 -1 DELETE RESTART FILES OF ENDSTEP **************************************************** ******************* SOLVE FOR LS 1 OF 2 **************** SELECT FOR ITEM=TYPE COMPONENT= IN RANGE 11 TO 11 STEP 1 11377 ELEMENTS (OF 1510586 DEFINED) SELECTED BY ESEL COMMAND. SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET. 24326 NODES (OF 2130921 DEFINED) SELECTED FROM 11377 SELECTED ELEMENTS BY NSLE COMMAND. GENERATE SURFACE LOAD PRES ON SURFACE DEFINED BY ALL SELECTED NODES SET ACCORDING TO TABLE PARAMETER = _LOADVARI119 NUMBER OF PRES ELEMENT FACE LOADS STORED = 11377 ALL SELECT FOR ITEM=NODE COMPONENT= IN RANGE 1 TO 2130921 STEP 1 2130921 NODES (OF 2130921 DEFINED) SELECTED BY NSEL COMMAND. ALL SELECT FOR ITEM=ELEM COMPONENT= IN RANGE 1 TO 1671056 STEP 1 1510586 ELEMENTS (OF 1510586 DEFINED) SELECTED BY ESEL COMMAND. ALL SELECT FOR ITEM=ELEM COMPONENT= IN RANGE 1 TO 1671056 STEP 1 1510586 ELEMENTS (OF 1510586 DEFINED) SELECTED BY ESEL COMMAND. PRINTOUT RESUMED BY /GOP SPECIFIED NODAL LOAD FX FOR SELECTED NODES 2130910 TO 2130910 BY 1 REAL= 39900.0000 IMAG= 0.00000000 SPECIFIED NODAL LOAD FX FOR SELECTED NODES 2130911 TO 2130911 BY 1 REAL= 39900.0000 IMAG= 0.00000000 SPECIFIED NODAL LOAD FX FOR SELECTED NODES 2130912 TO 2130912 BY 1 REAL= 39900.0000 IMAG= 0.00000000 SPECIFIED NODAL LOAD FX FOR SELECTED NODES 2130913 TO 2130913 BY 1 REAL= 39900.0000 IMAG= 0.00000000 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 EANG ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIES WRITE ETMP ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL FOR ALL APPLICABLE ENTITIES WRITE VENG 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 CONT 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 *GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000 *IF ANSINTER_ ( = 0.00000 ) NE 0 ( = 0.00000 ) THEN *ENDIF *** NOTE *** CP = 28.453 TIME= 19:01:26 The automatic domain decomposition logic has selected the MESH domain decomposition method with 4 processes per solution. *** WARNING *** CP = 28.453 TIME= 19:01:26 The cyclic sector model contains line and volume element types. Please verify the auto detected LOW and HIGH nodal edge component pairs (CYCLIC command) for cyclic symmetry solution. *** 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. ELEMENT TYPE 3 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 ELEMENT TYPE 4 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 ELEMENT TYPE 28 IS BEAM188 . KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 28 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 29 IS BEAM188 . KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 29 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 30 IS BEAM188 . KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 30 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 31 IS BEAM188 . KEYOPT(3)=2 IS ALWAYS SUGGESTED. KEYOPT(3) HAS BEEN RESET KEYOPT(1-12)= 0 0 2 0 0 0 0 0 0 0 0 0 ELEMENT TYPE 31 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. *** NOTE *** CP = 30.906 TIME= 19:01:27 Internal nodes from 2130922 to 2130937 are created. 8 internal nodes are used for handling degrees of freedom on pilot nodes of rigid target surfaces. 8 internal nodes are used for quadratic and/or cubic options of BEAM188, PIPE288, and/or SHELL208. *** WARNING *** CP = 87.281 TIME= 19:02:22 Element shape checking is currently inactive. Issue SHPP,ON or SHPP,WARN to reactivate, if desired. *** NOTE *** CP = 98.250 TIME= 19:02:27 The model data was checked and warning messages were found. Please review output or errors file ( \\ngr.local\01-NGR-AUT\Office\Projekte\Entwicklungsprojekte\E-20914_Rea ktorkopfModifikation\02_KonstruktionMechanisch\FEM Analyse Durchbiegung Lochplatte\CAD\_ProjectScratch\Scr0C57\file0.err ) for these warning messages. GENERATE CYCLIC SYMMETRY CONSTRAINT EQUATIONS USING USER-SUPPLIED LOW TO HIGH NODE XREF ARRAY = _CYCLICMAP NUMBER OF CONSTRAINT EQUATIONS GENERATED= 58656 (USING USER SUPPLIED EDGE NODE MAPPING) ***** ANSYS SOLVE COMMAND ***** *** 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. ELEMENT TYPE 3 IS SOLID186. KEYOPT(2) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 4 IS SOLID186. KEYOPT(2) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 28 IS BEAM188 . KEYOPT(3) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 28 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 29 IS BEAM188 . KEYOPT(3) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 29 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 30 IS BEAM188 . KEYOPT(3) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 30 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 31 IS BEAM188 . KEYOPT(3) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 31 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. *** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2020 R2 20.2 *** DISTRIBUTED ANSYS Academic Research Mechanical 01132000 VERSION=WINDOWS x64 19:02:32 DEC 16, 2020 CP= 104.719 Durchbiegung Lochplatte--Static Structural (I5) S O L U T I O N O P T I O N S PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D CYCLIC SYMMETRY SECTOR ANGLE. . . . . . . . . . 30.000 DEGREES 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 = 107.188 TIME= 19:02:35 Material number 32 (used by element 1671050) 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 = 108.797 TIME= 19:02:36 The step data was checked and warning messages were found. Please review output or errors file ( \\ngr.local\01-NGR-AUT\Office\Projekte\Entwicklungsprojekte\E-20914_Rea ktorkopfModifikation\02_KonstruktionMechanisch\FEM Analyse Durchbiegung Lochplatte\CAD\_ProjectScratch\Scr0C57\file0.err ) for these warning messages. *** NOTE *** CP = 108.797 TIME= 19:02:36 This nonlinear analysis defaults to using the full Newton-Raphson solution procedure. This can be modified using the NROPT command. *WARNING*: Node 217570 has been used on different contact pairs (real ID 16 & 20). These two pairs will be merged. Please check the model carefully. *** NOTE *** CP = 116.047 TIME= 19:02:44 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 0.55000E+06 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.76915E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.10720E-01 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 1.0720 Average contact pair depth 0.76915 Default pinball region factor PINB 1.0000 The resulting pinball region 0.76915 *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.047 TIME= 19:02:44 Max. Initial penetration 1.776356839E-15 was detected between contact element 1616199 and target element 1622409. **************************************** *** NOTE *** CP = 116.047 TIME= 19:02:44 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 0.55000E+06 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.40000E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.68580E-02 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.68580 Average contact pair depth 0.40000 Default pinball region factor PINB 1.0000 The resulting pinball region 0.40000 *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.047 TIME= 19:02:44 Max. Initial penetration 1.776356839E-15 was detected between contact element 1619258 and target element 1613757. **************************************** *** NOTE *** CP = 116.047 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 7 and contact element type 7 has been set up. The companion pair has real constant set ID 8. 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 0.52952E+07 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.70252E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.96361E-02 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.96361 Average contact pair depth 0.70252 Default pinball region factor PINB 1.0000 The resulting pinball region 0.70252 *** NOTE *** CP = 116.062 TIME= 19:02:44 One of the contact searching regions contains at least 133 target elements. You may reduce the pinball radius. *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.062 TIME= 19:02:44 Max. Initial penetration 1.284887655E-04 was detected between contact element 1634297 and target element 1642295. You may move entire target surface by : x= 1.743843361E-05, y= 1.272998975E-04, z= -7.26778744E-12,to reduce initial penetration. **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 8 and contact element type 7 has been set up. The companion pair has real constant set ID 7. 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 0.52952E+07 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.64418E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.76614E-02 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.76614 Average contact pair depth 0.64418 Default pinball region factor PINB 1.0000 The resulting pinball region 0.64418 *** NOTE *** CP = 116.062 TIME= 19:02:44 One of the contact searching regions contains at least 57 target elements. You may reduce the pinball radius. *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.062 TIME= 19:02:44 Max. Initial penetration 1.285006848E-04 was detected between contact element 1638659 and target element 1628696. You may move entire target surface by : x= -1.687161022E-05, y= -1.273882834E-04, z= -2.761371815E-11,to reduce initial penetration. **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 9 and contact element type 9 has been set up. The companion pair has real constant set ID 10. 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 0.55000E+06 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.25000 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.14821E-01 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 1.4821 Average contact pair depth 2.5000 Default pinball region factor PINB 1.0000 The resulting pinball region 2.5000 *** NOTE *** CP = 116.062 TIME= 19:02:44 One of the contact searching regions contains at least 171 target elements. You may reduce the pinball radius. *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.062 TIME= 19:02:44 Max. Initial penetration 8.881784197E-16 was detected between contact element 1644717 and target element 1649528. **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 10 and contact element type 9 has been set up. The companion pair has real constant set ID 9. 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 0.55000E+06 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.40000E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.69196E-02 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.69196 Average contact pair depth 0.40000 Default pinball region factor PINB 1.0000 The resulting pinball region 0.40000 *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.062 TIME= 19:02:44 Max. Initial penetration 1.776356839E-15 was detected between contact element 1647724 and target element 1643305. **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 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 2130908 which connects to other element 1613170. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 14 and contact element type 14 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2130909 which connects to other element 1671055. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 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 2130902 which connects to other element 1613167. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 20. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 18 and contact element type 18 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2130903 which connects to other element 1671049. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ *WARNING*: Boundary conditions, coupling, and/or constraint equations have been applied on certain contact nodes (for example 16406). **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 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 2130904 which connects to other element 1613168. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 16. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ *WARNING*: Boundary conditions, coupling, and/or constraint equations have been applied on certain contact nodes (for example 436805). **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 22 and contact element type 22 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2130905 which connects to other element 1671051. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ *WARNING*: Boundary conditions, coupling, and/or constraint equations have been applied on certain contact nodes (for example 16478). **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 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 2130906 which connects to other element 1613169. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 26 and contact element type 26 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 2130907 which connects to other element 1671053. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 40 and contact element type 5 has been set up. The companion pair has real constant set ID 41. 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 0.55000E+06 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.76915E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.10720E-01 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 1.0720 Average contact pair depth 0.76915 Default pinball region factor PINB 1.0000 The resulting pinball region 0.76915 *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.062 TIME= 19:02:44 Max. Initial penetration 1.776356839E-15 was detected between contact element 3287255 and target element 3293465. **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 41 and contact element type 5 has been set up. The companion pair has real constant set ID 40. 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 0.55000E+06 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.40000E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.68580E-02 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.68580 Average contact pair depth 0.40000 Default pinball region factor PINB 1.0000 The resulting pinball region 0.40000 *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.062 TIME= 19:02:44 Max. Initial penetration 1.776356839E-15 was detected between contact element 3290314 and target element 3284813. **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 42 and contact element type 7 has been set up. The companion pair has real constant set ID 43. 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 0.52952E+07 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.70252E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.96361E-02 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.96361 Average contact pair depth 0.70252 Default pinball region factor PINB 1.0000 The resulting pinball region 0.70252 *** NOTE *** CP = 116.062 TIME= 19:02:44 One of the contact searching regions contains at least 133 target elements. You may reduce the pinball radius. *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.062 TIME= 19:02:44 Max. Initial penetration 1.284887655E-04 was detected between contact element 3305353 and target element 3313351. You may move entire target surface by : x= 1.743843361E-05, y= 1.272998975E-04, z= -7.26778744E-12,to reduce initial penetration. **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 43 and contact element type 7 has been set up. The companion pair has real constant set ID 42. 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 0.52952E+07 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.64418E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.76614E-02 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.76614 Average contact pair depth 0.64418 Default pinball region factor PINB 1.0000 The resulting pinball region 0.64418 *** NOTE *** CP = 116.062 TIME= 19:02:44 One of the contact searching regions contains at least 57 target elements. You may reduce the pinball radius. *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.062 TIME= 19:02:44 Max. Initial penetration 1.285006848E-04 was detected between contact element 3309715 and target element 3299752. You may move entire target surface by : x= -1.687161022E-05, y= -1.273882834E-04, z= -2.761371815E-11,to reduce initial penetration. **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 44 and contact element type 9 has been set up. The companion pair has real constant set ID 45. 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 0.55000E+06 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.25000 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.14821E-01 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 1.4821 Average contact pair depth 2.5000 Default pinball region factor PINB 1.0000 The resulting pinball region 2.5000 *** NOTE *** CP = 116.062 TIME= 19:02:44 One of the contact searching regions contains at least 171 target elements. You may reduce the pinball radius. *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.062 TIME= 19:02:44 Max. Initial penetration 8.881784197E-16 was detected between contact element 3315773 and target element 3320584. **************************************** *** NOTE *** CP = 116.062 TIME= 19:02:44 Symmetric Deformable- deformable contact pair identified by real constant set 45 and contact element type 9 has been set up. The companion pair has real constant set ID 44. 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 0.55000E+06 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.40000E-01 Max. initial friction coefficient MU 0.20000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.69196E-02 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.69196 Average contact pair depth 0.40000 Default pinball region factor PINB 1.0000 The resulting pinball region 0.40000 *WARNING*: Initial penetration is included. *** NOTE *** CP = 116.078 TIME= 19:02:44 Max. Initial penetration 1.776356839E-15 was detected between contact element 3318780 and target element 3314361. **************************************** *** NOTE *** CP = 116.078 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 47 and contact element type 12 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261845 which connects to other element 3284226. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 116.078 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 49 and contact element type 14 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261846 which connects to other element 3342111. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 116.078 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 51 and contact element type 16 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261839 which connects to other element 3284223. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 55. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 116.078 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 53 and contact element type 18 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261840 which connects to other element 3342105. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ *WARNING*: Boundary conditions, coupling, and/or constraint equations have been applied on certain contact nodes (for example 2147343). **************************************** *** NOTE *** CP = 116.078 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 55 and contact element type 20 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261841 which connects to other element 3284224. Internal MPC will be built. This pair will be merged with other pair defined by real constant set 51. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ *WARNING*: Boundary conditions, coupling, and/or constraint equations have been applied on certain contact nodes (for example 2567742). **************************************** *** NOTE *** CP = 116.078 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 57 and contact element type 22 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261842 which connects to other element 3342107. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ *WARNING*: Boundary conditions, coupling, and/or constraint equations have been applied on certain contact nodes (for example 2147415). **************************************** *** NOTE *** CP = 116.078 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 59 and contact element type 24 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261843 which connects to other element 3284225. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 116.078 TIME= 19:02:44 Rigid-constraint surface identified by real constant set 61 and contact element type 26 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261844 which connects to other element 3342109. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** WARNING *** CP = 116.078 TIME= 19:02:44 Overconstraint may occur for Lagrange multiplier or MPC based contact algorithm. The reasons for possible overconstraint are: *** WARNING *** CP = 116.078 TIME= 19:02:44 Boundary conditions, coupling, and/or constraint equations have been applied on certain contact nodes (for example 2147415). **************************************** 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: 1510586 ...Number of nodes: 2130937 ...Decompose to 4 CPU domains ...Element load balance ratio = 1.022 L O A D S T E P O P T I O N S LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1 CYCLIC SYMMETRY HARMONIC INDEX. . . . . . . . . 0 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 EANG ALL ETMP ALL VENG ALL STRS ALL EPEL ALL EPPL ALL CONT ALL MISC ALL _ELMISC SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr >>>> PRETENSION ELEMENT STATUS <<<< SECTION NAME PT.NODE --------STATUS-------------------- ----LOAD SOURCE---- 33 2130911 APPLIED PRELOAD FORCE= 39900. F COMMAND 34 2130912 APPLIED PRELOAD FORCE= 39900. F COMMAND 68 4261848 APPLIED PRELOAD FORCE= 39900. F COMMAND 69 4261849 APPLIED PRELOAD FORCE= 39900. F COMMAND 32 2130910 APPLIED PRELOAD FORCE= 39900. F COMMAND 35 2130913 APPLIED PRELOAD FORCE= 39900. F COMMAND 67 4261847 APPLIED PRELOAD FORCE= 39900. F COMMAND 70 4261850 APPLIED PRELOAD FORCE= 39900. F COMMAND *** NOTE *** CP = 147.297 TIME= 19:03:15 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 2130908 which connects to other element 1613170. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 147.297 TIME= 19:03:15 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 2130906 which connects to other element 1613169. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 147.297 TIME= 19:03:15 Rigid-constraint surface identified by real constant set 47 and contact element type 12 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261845 which connects to other element 3284226. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** *** NOTE *** CP = 147.297 TIME= 19:03:15 Rigid-constraint surface identified by real constant set 59 and contact element type 24 has been set up. The degrees of freedom of the rigid surface are driven by the pilot node 4261843 which connects to other element 3284225. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ **************************************** MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 26, BY SOLUTION CONTROL LOGIC. *** NOTE *** CP = 148.734 TIME= 19:03:17 Predictor is ON by default for structural elements with rotational degrees of freedom. Use the PRED,OFF command to turn the predictor OFF if it adversely affects the convergence. *** WARNING *** CP = 149.625 TIME= 19:03:18 Multiple constraints have been applied on degree of freedom 2 of contact node 4513. The program will remove certain internal MPCs. Please check the model carefully. *** WARNING *** CP = 149.625 TIME= 19:03:18 Multiple constraints have been applied on degree of freedom 2 of contact node 164191. The program will remove certain internal MPCs. Please check the model carefully. *** FATAL *** CP = 151.312 TIME= 19:03:21 The internal constraint equation 224199 share degrees of freedom with the constraint equations along the edge of the cyclic symmetry sector. This is not allowed. Please modify your contact pair to avoid this. ERROR: Slave process(es) with rank(s) 1, 2, 3 have encountered a FATAL error. The information below was gathered from the file*.out output file(s). Please review the slave process output file(s) listed below for more details on this error. Slave Process Output File .\file1.out: *** FATAL *** CP = 32.062 TIME= 19:03:21 The internal constraint equation 224199 share degrees of freedom with the constraint equations along the edge of the cyclic symmetry sector. This is not allowed. Please modify your contact pair to avoid this. Slave Process Output File .\file2.out: *** FATAL *** CP = 31.531 TIME= 19:03:21 The internal constraint equation 224199 created by contact pair share degrees of freedom with the constraint equations along the edge of the cyclic symmetry sector. This is not allowed. Please modify your contact pair to avoid this. Slave Process Output File .\file3.out: *** FATAL *** CP = 32.266 TIME= 19:03:21 The internal constraint equation 224199 share degrees of freedom with the constraint equations along the edge of the cyclic symmetry sector. This is not allowed. Please modify your contact pair to avoid this.