Solver-Ausgabe ANSYS Mechanical Enterprise *------------------------------------------------------------------* | | | W E L C O M E T O T H E A N S Y S (R) P R O G R A M | | | *------------------------------------------------------------------* *************************************************************** * ANSYS 2020 R1 LEGAL NOTICES * *************************************************************** * * * Copyright 1971-2020 ANSYS, Inc. All rights reserved. * * Unauthorized use, distribution or duplication is * * prohibited. * * * * Ansys is a registered trademark of ANSYS, Inc. or its * * subsidiaries in the United States or other countries. * * See the ANSYS, Inc. online documentation or the ANSYS, Inc. * * documentation CD or online help for the complete Legal * * Notice. * * * *************************************************************** * * * THIS ANSYS SOFTWARE PRODUCT AND PROGRAM DOCUMENTATION * * INCLUDE TRADE SECRETS AND CONFIDENTIAL AND PROPRIETARY * * PRODUCTS OF ANSYS, INC., ITS SUBSIDIARIES, OR LICENSORS. * * The software products and documentation are furnished by * * ANSYS, Inc. or its subsidiaries under a software license * * agreement that contains provisions concerning * * non-disclosure, copying, length and nature of use, * * compliance with exporting laws, warranties, disclaimers, * * limitations of liability, and remedies, and other * * provisions. The software products and documentation may be * * used, disclosed, transferred, or copied only in accordance * * with the terms and conditions of that software license * * agreement. * * * * ANSYS, Inc. is a UL registered * * ISO 9001:2015 company. * * * *************************************************************** * * * This product is subject to U.S. laws governing export and * * re-export. * * * * For U.S. Government users, except as specifically granted * * by the ANSYS, Inc. software license agreement, the use, * * duplication, or disclosure by the United States Government * * is subject to restrictions stated in the ANSYS, Inc. * * software license agreement and FAR 12.212 (for non-DOD * * licenses). * * * *************************************************************** 2020 R1 Point Releases and Patches installed: ANSYS, Inc. Products 2020 R1 SpaceClaim 2020 R1 AIM 2020 R1 Live (includes SpaceClaim) 2020 R1 Remote Solve Manager Standalone Services 2020 R1 Viewer 2020 R1 ACIS Geometry Interface 2020 R1 AutoCAD Geometry Interface 2020 R1 Catia, Version 4 Geometry Interface 2020 R1 Catia, Version 5 Geometry Interface 2020 R1 Catia, Version 6 Geometry Interface 2020 R1 Creo Elements/Direct Modeling Geometry Interface 2020 R1 Creo Parametric Geometry Interface 2020 R1 Inventor Geometry Interface 2020 R1 JTOpen Geometry Interface 2020 R1 NX Geometry Interface 2020 R1 Parasolid Geometry Interface 2020 R1 Solid Edge Geometry Interface 2020 R1 SOLIDWORKS Geometry Interface 2020 R1 ANSYS, Inc. License Manager 2020 R1 CFD-Post only 2020 R1 CFX (includes CFD-Post) 2020 R1 Chemkin 2020 R1 EnSight 2020 R1 FENSAP-ICE 2020 R1 Fluent (includes CFD-Post) 2020 R1 Forte 2020 R1 Polyflow (includes CFD-Post) 2020 R1 TurboGrid 2020 R1 Aqwa 2020 R1 Customization Files for User Programmable Features 2020 R1 Mechanical Products 2020 R1 Additive 2020 R1 ANSYS Sherlock 2020 R1 Icepak (includes CFD-Post) 2020 R1 ANSYS Remote Solve Manager Standalone Services 2020 R1 ***** ANSYS COMMAND LINE ARGUMENTS ***** BATCH MODE REQUESTED (-b) = NOLIST INPUT FILE COPY MODE (-c) = COPY DISTRIBUTED MEMORY PARALLEL REQUESTED 2 PARALLEL PROCESSES REQUESTED WITH SINGLE THREAD PER PROCESS TOTAL OF 2 CORES REQUESTED INPUT FILE NAME = C:\Users\koeh_mn\Documents\MK ANSYS\Vorpilot ZiRa\_ProjectScratch\Scr9005\dummy.dat OUTPUT FILE NAME = C:\Users\koeh_mn\Documents\MK ANSYS\Vorpilot ZiRa\_ProjectScratch\Scr9005\solve.out START-UP FILE MODE = NOREAD STOP FILE MODE = NOREAD RELEASE= 2020 R1 BUILD= 20.1 UP20191203 VERSION=WINDOWS x64 CURRENT JOBNAME=file0 11:49:58 JUN 08, 2021 CP= 0.359 PARAMETER _DS_PROGRESS = 999.0000000 /INPUT FILE= ds.dat LINE= 0 *** NOTE *** CP = 0.484 TIME= 11:49:58 The /CONFIG,NOELDB command is not valid in a Distributed ANSYS solution. Command is ignored. *GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 11.8327778 TITLE= 21-04-23_Vorpilot_ZiRa_Laufradvariante_DP11_rev01--Statisch-mechanisch (E5) SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\koeh_mn\Documents\MK ANSYS\Vorpilot ZiRa\_ProjectScratch\Scr9005\ SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\koeh_mn\Documents\MK ANSYS\Vorpilot ZiRa\21-04-23_Vorpilot_ZiRa_Laufradvariante_DP11_rev01_files\dp0\SYS-5\MECH\ SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_USERFILES_DIR(1) = C:\Users\koeh_mn\Documents\MK ANSYS\Vorpilot ZiRa\21-04-23_Vorpilot_ZiRa_Laufradvariante_DP11_rev01_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 2020 R1 20.1 *** DISTRIBUTED ANSYS Mechanical Enterprise 00341487 VERSION=WINDOWS x64 11:49:58 JUN 08, 2021 CP= 0.484 21-04-23_Vorpilot_ZiRa_Laufradvariante_DP11_rev01--Statisch-mechanisch (E5) ***** ANSYS ANALYSIS DEFINITION (PREP7) ***** *********** Nodes for the whole assembly *********** *********** Nodes for all Remote Points *********** *********** Elements for Body 1 "Impeller" *********** *********** Elements for Body 2 "Welle" *********** *********** Elements for Body 3 "Scheibe" *********** *********** Send User Defined Coordinate System(s) *********** *********** Set Reference Temperature *********** *********** Send Materials *********** *********** Create Contact "Reibungsbehaftet - Impeller bis Scheibe" ********** Real Constant Set For Above Contact Is 5 & 4 *********** Create Contact "Reibungsbehaftet - Impeller bis Welle" *********** Real Constant Set For Above Contact Is 7 & 6 *********** Create Contact "Reibungsbehaftet - Welle bis Impeller" *********** Real Constant Set For Above Contact Is 9 & 8 *********** Create Contact "Verbund - Welle bis Scheibe" *********** Real Constant Set For Above Contact Is 11 & 10 *********** Create Remote Point "Externer Punkt (intern)" *********** *********** Create Remote Point "Externer Punkt (intern) 2" *********** *********** Construct Remote Displacement *********** *********** Construct Remote Displacement *********** *** Create a component for all remote displacements *** ***** ROUTINE COMPLETED ***** CP = 12.359 --- Number of total nodes = 2965046 --- Number of contact elements = 8733 --- Number of spring elements = 0 --- Number of bearing elements = 0 --- Number of solid elements = 1929091 --- Number of condensed parts = 0 --- Number of total elements = 1937826 *GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 11.8350000 **************************************************************************** ************************* SOLUTION ******************************** **************************************************************************** ***** ANSYS SOLUTION ROUTINE ***** PERFORM A STATIC ANALYSIS THIS WILL BE A NEW ANALYSIS PARAMETER _THICKRATIO = 1.000000000 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 1 **************** SPECIFIED CONSTRAINT UX FOR SELECTED NODES 5504832 TO 5504832 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT UY FOR SELECTED NODES 5504832 TO 5504832 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT UZ FOR SELECTED NODES 5504832 TO 5504832 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES 5504832 TO 5504832 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT ROTY FOR SELECTED NODES 5504832 TO 5504832 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT ROTZ FOR SELECTED NODES 5504832 TO 5504832 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT UX FOR SELECTED NODES 5504833 TO 5504833 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT UY FOR SELECTED NODES 5504833 TO 5504833 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT UZ FOR SELECTED NODES 5504833 TO 5504833 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES 5504833 TO 5504833 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT ROTY FOR SELECTED NODES 5504833 TO 5504833 BY 1 REAL= 0.00000000 IMAG= 0.00000000 SPECIFIED CONSTRAINT ROTZ FOR SELECTED NODES 5504833 TO 5504833 BY 1 REAL= 0.00000000 IMAG= 0.00000000 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 5 SUBSTEPS AS A MAXIMUM USE 5 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 *** NOTE *** CP = 12.750 TIME= 11:50:06 Use of the BCSOPTION has been deprecated. Please use the DSPOPTION command instead to control the sparse solver behavior. BCSOPTION: USE IN-CORE MEMORY ALLOCATION LOGIC FOR SPARSE DIRECT SOLVER *GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000 *IF ANSINTER_ ( = 0.00000 ) NE 0 ( = 0.00000 ) THEN *ENDIF *** NOTE *** CP = 12.875 TIME= 11:50:07 The automatic domain decomposition logic has selected the MESH domain decomposition method with 2 processes per solution. ***** ANSYS SOLVE COMMAND ***** *** WARNING *** CP = 13.688 TIME= 11:50:07 Element shape checking is currently inactive. Issue SHPP,ON or SHPP,WARN to reactivate, if desired. *** NOTE *** CP = 17.047 TIME= 11:50:10 The model data was checked and warning messages were found. Please review output or errors file ( C:\Users\koeh_mn\Documents\MK ANSYS\Vorpilot ZiRa\_ProjectScratch\Scr9005\file0.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. 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 *** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2020 R1 20.1 *** DISTRIBUTED ANSYS Mechanical Enterprise 00341487 VERSION=WINDOWS x64 11:50:10 JUN 08, 2021 CP= 17.656 21-04-23_Vorpilot_ZiRa_Laufradvariante_DP11_rev01--Statisch-mechanisch (E5) 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 *** NOTE *** CP = 18.672 TIME= 11:50:11 This nonlinear analysis defaults to using the full Newton-Raphson solution procedure. This can be modified using the NROPT command. *** NOTE *** CP = 18.672 TIME= 11:50:11 The conditions for direct assembly have been met. No .emat or .erot files will be produced. *** NOTE *** CP = 20.078 TIME= 11:50:12 Internal nodes from 5504834 to 5504835 are created. 2 internal nodes are used for handling degrees of freedom on pilot nodes of rigid target surfaces. *** NOTE *** CP = 21.906 TIME= 11:50:14 Internal nodes from 5504834 to 5504835 are created. 2 internal nodes are used for handling degrees of freedom on pilot nodes of rigid target surfaces. *** NOTE *** CP = 23.125 TIME= 11:50:14 Smoothing on certain contact nodes (e.g.2540385) for pair ID 14 may have accuracy issue. Please verify element normal of connected contact elements (e.g.3923059 & 3923194). *** NOTE *** CP = 23.250 TIME= 11:50:14 Symmetric Deformable- deformable contact pair identified by real constant set 4 and contact element type 4 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 0.50062E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.63645E-04 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.84202E-05 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.84202E-03 Average contact pair depth 0.63645E-03 Default pinball region factor PINB 1.0000 The resulting pinball region 0.63645E-03 *WARNING*: Initial penetration is included. *** NOTE *** CP = 23.250 TIME= 11:50:14 Max. Initial penetration 1.734723476E-18 was detected between contact element 3915315 and target element 3916093. **************************************** *** NOTE *** CP = 23.250 TIME= 11:50:14 Symmetric Deformable- deformable contact pair identified by real constant set 5 and contact element type 4 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 0.50062E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.79901E-04 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.73104E-05 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.73104E-03 Average contact pair depth 0.79901E-03 Default pinball region factor PINB 1.0000 The resulting pinball region 0.79901E-03 *WARNING*: Initial penetration is included. *** NOTE *** CP = 23.250 TIME= 11:50:14 Max. Initial penetration 3.469446952E-18 was detected between contact element 3915563 and target element 3915120. **************************************** *** NOTE *** CP = 23.250 TIME= 11:50:14 Symmetric Deformable- deformable contact pair identified by real constant set 6 and contact element type 6 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 0.50000 The resulting initial contact stiffness 0.12308E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.14451E-03 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Use constant contact stiffness Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.20094E-02 Average contact pair depth 0.14451E-02 Default pinball region factor PINB 1.0000 The resulting pinball region 0.14451E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 23.250 TIME= 11:50:14 Max. Initial penetration 1.060666416E-05 was detected between contact element 3917132 and target element 3918121. You may move entire target surface by : x= -9.742445115E-06, y= 4.193574084E-06, z= 4.909677367E-09,to reduce initial penetration. **************************************** *** NOTE *** CP = 23.250 TIME= 11:50:14 Symmetric Deformable- deformable contact pair identified by real constant set 7 and contact element type 6 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 0.50000 The resulting initial contact stiffness 0.12308E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.16250E-03 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Use constant contact stiffness Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.20916E-02 Average contact pair depth 0.16250E-02 Default pinball region factor PINB 1.0000 The resulting pinball region 0.16250E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 23.250 TIME= 11:50:14 Max. Initial penetration 1.065154794E-05 was detected between contact element 3917433 and target element 3916896. You may move entire target surface by : x= -1.063950756E-05, y= 5.063125671E-07, z= 2.71576548E-21,to reduce initial penetration. **************************************** *** NOTE *** CP = 23.250 TIME= 11:50:14 Symmetric Deformable- deformable contact pair identified by real constant set 8 and contact element type 8 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 0.50000 The resulting initial contact stiffness 0.12453E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.16060E-03 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.19222E-04 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.19222E-02 Average contact pair depth 0.16060E-02 Default pinball region factor PINB 1.0000 The resulting pinball region 0.16060E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 23.250 TIME= 11:50:14 Max. Initial penetration 6.938893904E-18 was detected between contact element 3918323 and target element 3918409. **************************************** *** NOTE *** CP = 23.250 TIME= 11:50:14 Symmetric Deformable- deformable contact pair identified by real constant set 9 and contact element type 8 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 0.50000 The resulting initial contact stiffness 0.12453E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.13292E-03 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.19708E-04 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.19708E-02 Average contact pair depth 0.13292E-02 Default pinball region factor PINB 1.0000 The resulting pinball region 0.13292E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 23.250 TIME= 11:50:14 Max. Initial penetration 1.387778781E-17 was detected between contact element 3918349 and target element 3918290. **************************************** *** NOTE *** CP = 23.250 TIME= 11:50:14 Symmetric Deformable- deformable contact pair identified by real constant set 10 and contact element type 10 has been set up. The companion pair has real constant set ID 11. 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 0.19848E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.20153E-03 Default opening contact stiffness OPSF will be used. Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.50000E-02 The resulting elastic slip tolerance 0.11841E-04 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.23682E-02 Average contact pair depth 0.20153E-02 Default pinball region factor PINB 0.25000 The resulting pinball region 0.50382E-03 Initial penetration/gap is excluded. Bonded contact (always) is defined. *** NOTE *** CP = 23.250 TIME= 11:50:14 Min. Initial gap 4.182433463E-08 was detected between contact element 3918782 and target element 3919293. The gap is closed due to initial settings. Max. Geometric gap 1.430273339E-06 has been detected between contact element 3918808 and target element 3919313. **************************************** *** NOTE *** CP = 23.250 TIME= 11:50:14 Symmetric Deformable- deformable contact pair identified by real constant set 11 and contact element type 10 has been set up. The companion pair has real constant set ID 10. 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 0.19848E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.62448E-04 Default opening contact stiffness OPSF will be used. Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.50000E-02 The resulting elastic slip tolerance 0.39826E-05 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.79652E-03 Average contact pair depth 0.62448E-03 Default pinball region factor PINB 0.25000 The resulting pinball region 0.15612E-03 Initial penetration/gap is excluded. Bonded contact (always) is defined. *** NOTE *** CP = 23.250 TIME= 11:50:14 Max. Initial penetration 9.735751219E-09 was detected between contact element 3919036 and target element 3918523. You may move entire target surface by : x= 9.559653943E-09, y= 1.843330745E-09, z= 2.285716686E-13,to reduce initial penetration. Max. Geometric gap 1.730252568E-06 has been detected between contact element 3919128 and target element 3918510. **************************************** *** NOTE *** CP = 23.250 TIME= 11:50:14 Force-distributed-surface identified by real constant set 12 and contact element type 12 has been set up. The pilot node 5504832 is used to apply the force. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ Please verify constraints (including rotational degrees of freedom) on the pilot node by yourself. **************************************** *** NOTE *** CP = 23.250 TIME= 11:50:14 Force-distributed-surface identified by real constant set 14 and contact element type 14 has been set up. The pilot node 5504833 is used to apply the force. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ Please verify constraints (including rotational degrees of freedom) on the pilot node by yourself. **************************************** *** NOTE *** CP = 24.703 TIME= 11:50:15 Internal nodes from 5504834 to 5504835 are created. 2 internal nodes are used for handling degrees of freedom on pilot nodes of rigid target surfaces. 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: 1937826 ...Number of nodes: 2965048 ...Decompose to 2 CPU domains ...Element load balance ratio = 1.000 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 . . . . . . . . . 5 MINIMUM NUMBER OF SUBSTEPS . . . . . . . . . 5 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 SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr *** NOTE *** CP = 45.938 TIME= 11:50:30 Smoothing on certain contact nodes (e.g.2540385) for pair ID 14 may have accuracy issue. Please verify element normal of connected contact elements (e.g.3923059 & 3923194). *** NOTE *** CP = 46.000 TIME= 11:50:30 Symmetric Deformable- deformable contact pair identified by real constant set 4 and contact element type 4 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 0.50062E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.63645E-04 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.84202E-05 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.84202E-03 Average contact pair depth 0.63645E-03 Default pinball region factor PINB 1.0000 The resulting pinball region 0.63645E-03 *WARNING*: Initial penetration is included. *** NOTE *** CP = 46.000 TIME= 11:50:30 Max. Initial penetration 1.734723476E-18 was detected between contact element 3915315 and target element 3916093. **************************************** *** NOTE *** CP = 46.000 TIME= 11:50:30 Symmetric Deformable- deformable contact pair identified by real constant set 5 and contact element type 4 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 0.50062E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.79901E-04 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.73104E-05 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.73104E-03 Average contact pair depth 0.79901E-03 Default pinball region factor PINB 1.0000 The resulting pinball region 0.79901E-03 *WARNING*: Initial penetration is included. *** NOTE *** CP = 46.000 TIME= 11:50:30 Max. Initial penetration 3.469446952E-18 was detected between contact element 3915563 and target element 3915120. **************************************** *** NOTE *** CP = 46.000 TIME= 11:50:30 Symmetric Deformable- deformable contact pair identified by real constant set 8 and contact element type 8 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 0.50000 The resulting initial contact stiffness 0.12453E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.16060E-03 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.19222E-04 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.19222E-02 Average contact pair depth 0.16060E-02 Default pinball region factor PINB 1.0000 The resulting pinball region 0.16060E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 46.000 TIME= 11:50:30 Max. Initial penetration 6.938893904E-18 was detected between contact element 3918323 and target element 3918409. **************************************** *** NOTE *** CP = 46.000 TIME= 11:50:30 Symmetric Deformable- deformable contact pair identified by real constant set 9 and contact element type 8 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 0.50000 The resulting initial contact stiffness 0.12453E+16 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.13292E-03 Max. initial friction coefficient MU 0.10000 Default tangent stiffness factor FKT 1.0000 Default elastic slip factor SLTOL 0.10000E-01 The resulting elastic slip tolerance 0.19708E-04 Update contact stiffness at each iteration Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.19708E-02 Average contact pair depth 0.13292E-02 Default pinball region factor PINB 1.0000 The resulting pinball region 0.13292E-02 *WARNING*: Initial penetration is included. *** NOTE *** CP = 46.000 TIME= 11:50:30 Max. Initial penetration 1.387778781E-17 was detected between contact element 3918349 and target element 3918290. **************************************** *** NOTE *** CP = 46.000 TIME= 11:50:30 Force-distributed-surface identified by real constant set 12 and contact element type 12 has been set up. The pilot node 5504832 is used to apply the force. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ Please verify constraints (including rotational degrees of freedom) on the pilot node by yourself. **************************************** *** NOTE *** CP = 46.000 TIME= 11:50:30 Force-distributed-surface identified by real constant set 14 and contact element type 14 has been set up. The pilot node 5504833 is used to apply the force. Internal MPC will be built. The used degrees of freedom set is UX UY UZ ROTX ROTY ROTZ Please verify constraints (including rotational degrees of freedom) on the pilot node by yourself. **************************************** MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS HAS BEEN MODIFIED TO BE, NEQIT = 25, BY SOLUTION CONTROL LOGIC. *** WARNING *** CP = 46.062 TIME= 11:50:30 Too many nodes 8555 are included in the force-distributed-surface constraint identified by real constant set 12. This may greatly affect solver performance due to large wave fronts and memory consumption. Also check results carefully and consider solving with a different unit system. The FEA model contains 0 external CE equations and 12 internal CE equations. ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 4 Max. Penetration of -1.734723476E-18 has been detected between contact element 3915385 and target element 3916136. For total 234 contact elements, there are 228 elements are in contact. There are 228 elements are in sticking. Contacting area 4.086697262E-05. Max. Pinball distance 6.364523193E-04. One of the contact searching regions contains at least 30 target elements. Max. Pressure/force 3.750352326E-03. Max. Normal stiffness 2.161930923E+15. Min. Normal stiffness 2.161930923E+15. Max. Tangential stiffness 1.225596498E+13. Min. Tangential stiffness 1.225596498E+13. ************************************************* ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 5 *** NOTE *** CP = 111.219 TIME= 11:51:38 Contact pair is inactive. ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 8 Max. Penetration of -6.938893904E-18 has been detected between contact element 3918328 and target element 3918432. For total 42 contact elements, there are 39 elements are in contact. There are 39 elements are in sticking. Contacting area 2.686112969E-05. Max. Pinball distance 1.606012751E-03. One of the contact searching regions contains at least 12 target elements. Max. Pressure/force 5.040040598E-03. Max. Normal stiffness 7.263463987E+14. Min. Normal stiffness 7.263463987E+14. Max. Tangential stiffness 4.55154993E+12. Min. Tangential stiffness 4.55154993E+12. ************************************************* ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 9 *** NOTE *** CP = 111.219 TIME= 11:51:38 Contact pair is inactive. *********** PRECISE MASS SUMMARY *********** TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN Translational mass | Coupled translational/rotational mass 0.68950 0.0000 0.0000 | 0.0000 0.25758E-01 0.55690E-08 0.0000 0.68950 0.0000 | -0.25758E-01 0.0000 -0.24998E-08 0.0000 0.0000 0.68950 | -0.55690E-08 0.24998E-08 0.0000 ------------------------------------------ | ------------------------------------------ | Rotational mass (inertia) | 0.15210E-02 0.33681E-10 0.53157E-10 | 0.33681E-10 0.15210E-02 0.78510E-10 | 0.53157E-10 0.78510E-10 0.80398E-03 TOTAL MASS = 0.68950 The mass principal axes coincide with the global Cartesian axes CENTER OF MASS (X,Y,Z)= -0.36255E-08 -0.80768E-08 0.37358E-01 TOTAL INERTIA ABOUT CENTER OF MASS 0.55875E-03 0.33681E-10 -0.40229E-10 0.33681E-10 0.55875E-03 -0.12953E-09 -0.40229E-10 -0.12953E-09 0.80398E-03 The inertia principal axes coincide with the global Cartesian axes *** MASS SUMMARY BY ELEMENT TYPE *** TYPE MASS 1 0.569051 2 0.113053 3 0.739845E-02 Range of element maximum matrix coefficients in global coordinates Maximum = 2.063006833E+09 at element 1664082. Minimum = 11130657.3 at element 2314801. *** ELEMENT MATRIX FORMULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 1913085 SOLID187 97.203 0.000051 2 13731 SOLID187 0.906 0.000066 3 2275 SOLID186 0.266 0.000117 4 673 CONTA174 0.125 0.000186 5 673 TARGE170 0.000 0.000000 6 918 CONTA174 0.016 0.000017 7 918 TARGE170 0.000 0.000000 8 86 CONTA174 0.031 0.000363 9 86 TARGE170 0.000 0.000000 10 498 CONTA174 0.031 0.000063 11 498 TARGE170 0.000 0.000000 12 3627 CONTA174 0.125 0.000034 13 1 TARGE170 0.000 0.000000 14 756 CONTA174 0.031 0.000041 15 1 TARGE170 0.000 0.000000 Time at end of element matrix formulation CP = 111.328125. ALL CURRENT ANSYS DATA WRITTEN TO FILE NAME= file.rdb FOR POSSIBLE RESUME FROM THIS POINT FORCE CONVERGENCE VALUE = 0.5369E+06 CRITERION= 9.446 DISTRIBUTED SPARSE MATRIX DIRECT SOLVER. Number of equations = 8895120, Maximum wavefront = 40158 *** WARNING *** CP = 252.656 TIME= 11:54:01 The in-core memory mode has been requested for the Distributed Sparse Matrix Solver, however there is not enough memory to proceed in the in-core memory mode on one or more processes. The Distributed Sparse Matrix Solver will automatically switch to the out-of-core memory mode and continue computing the solution. Local memory allocated for solver = 21.338 GB Local memory required for in-core solution = 69.664 GB Local memory required for out-of-core solution = 20.208 GB Total memory allocated for solver = 35.295 GB Total memory required for in-core solution = 124.922 GB Total memory required for out-of-core solution = 33.455 GB *** WARNING *** CP = 252.828 TIME= 11:54:01 The Distributed 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. *** ERROR *** CP = 306.141 TIME= 11:54:55 An input/output error has occurred while trying to open a file with length = 48 GB. Error code = 112, which translates to: Es steht nicht genug Speicherplatz auf dem Datenträger zur Verfügung. *** ERROR *** CP = 306.219 TIME= 11:55:15 The program is unable to open file file0.DSPtri. If the suggestions in the associated error messages immediately preceding and/or following this error message do not help resolve the file issue, please send the data leading to this operation to your technical support provider, along with the I/O error code of -1 and the system error code of 0, for help in determining the possible reasons as to why this file could not be opened. ********** CURRENT DISK AND DIRECTORY USAGE ********** Datentr„ger in Laufwerk C: ist Windows Volumeseriennummer: 7EA9-AD06 Verzeichnis von C:\Users\koeh_mn\Documents\MK ANSYS\Vorpilot ZiRa\_ProjectScratch\Scr9005 08.06.2021 11:52