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License Manager 2019 R3 ***** 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 INPUT FILE NAME = C:\Users\Admin\Documents\ansys\_ProjectScratch\Scr6808\dummy.dat OUTPUT FILE NAME = C:\Users\Admin\Documents\ansys\_ProjectScratch\Scr6808\solve.out START-UP FILE MODE = NOREAD STOP FILE MODE = NOREAD RELEASE= 2019 R3 BUILD= 19.5 UP20190805 VERSION=WINDOWS x64 CURRENT JOBNAME=file 17:55:13 SEP 20, 2019 CP= 0.250 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= 17.9202778 TITLE= Chakra--Static Structural (A5) SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\Admin\Documents\ansys\_ProjectScratch\Scr6808\ SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\Admin\Documents\ansys\Chakra_files\dp0\SYS\MECH\ SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR TYPE=STRI DIMENSIONS= 248 1 1 PARAMETER _WB_USERFILES_DIR(1) = C:\Users\Admin\Documents\ansys\Chakra_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 2019 R3 19.5 *** ANSYS Mechanical Enterprise 20120530 VERSION=WINDOWS x64 17:55:13 SEP 20, 2019 CP= 0.359 Chakra--Static Structural (A5) ***** ANSYS ANALYSIS DEFINITION (PREP7) ***** *********** Nodes for the whole assembly *********** *********** Elements for Body 1 "top plate" *********** *********** Elements for Body 2 "bottom plat" *********** *********** Elements for Body 3 "spacer 1" *********** *********** Elements for Body 4 "spacer 2" *********** *********** Elements for Body 5 "spacer 3" *********** *********** Elements for Body 6 "spacer 4" *********** *********** Elements for Body 7 "spacer 5" *********** *********** Elements for Body 8 "spacer 6" *********** *********** Elements for Body 9 "spacer 7" *********** *********** Elements for Body 10 "spacer 8" *********** *********** Elements for Body 11 "spacer 9" *********** *********** Elements for Body 12 "spacer 10" *********** *********** Elements for Body 13 "spacer 11" *********** *********** Elements for Body 14 "spacer 12" *********** *********** Elements for Body 15 "spacer 13" *********** *********** Elements for Body 16 "spacer 14" *********** *********** Elements for Body 17 "spacer 15" *********** *********** Elements for Body 18 "spacer 16" *********** *********** Elements for Body 19 "spacer 17" *********** *********** Elements for Body 20 "spacer 18" *********** *********** Elements for Body 21 "spacer 19" *********** *********** Elements for Body 22 "spacer 20" *********** *********** Elements for Body 23 "spacer 21" *********** *********** Elements for Body 24 "spacer 22" *********** *********** Elements for Body 25 "spacer 23" *********** *********** Elements for Body 26 "spacer 24" *********** *********** Elements for Body 27 "spacer 25" *********** *********** Elements for Body 28 "spacer 26" *********** *********** Elements for Body 29 "spacer 27" *********** *********** Elements for Body 30 "spacer 28" *********** *********** Send User Defined Coordinate System(s) *********** *********** Set Reference Temperature *********** *********** Send Materials *********** *********** Send Sheet Properties *********** *********** Send Beam Properties *********** *********** Create Contact "Bonded - Top beam To Top plate holes" *********** Real Constant Set For Above Contact Is 32 & 31 *********** Create Contact "Bonded - Bottom beam To bottom plate holes" ******* Real Constant Set For Above Contact Is 34 & 33 *********** Send Named Selection as Element 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 Force Using Surface Effect Elements *********** ***** ROUTINE COMPLETED ***** CP = 4.234 --- Number of total nodes = 792654 --- Number of contact elements = 184252 --- Number of spring elements = 0 --- Number of bearing elements = 0 --- Number of solid elements = 259540 --- Number of condensed parts = 0 --- Number of total elements = 443848 *GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 17.9211111 **************************************************************************** ************************* SOLUTION ******************************** **************************************************************************** ***** ANSYS SOLUTION ROUTINE ***** PERFORM A STATIC ANALYSIS THIS WILL BE A NEW ANALYSIS PARAMETER _THICKRATIO = 0.000000000 USE SPARSE MATRIX DIRECT SOLVER CONTACT INFORMATION PRINTOUT LEVEL 1 NLDIAG: Nonlinear diagnostics CONT option is set to ON. Writing frequency : each ITERATION. DO NOT SAVE ANY RESTART FILES AT ALL **************************************************** ******************* SOLVE FOR LS 1 OF 1 **************** SELECT FOR ITEM=TYPE COMPONENT= IN RANGE 35 TO 35 STEP 1 182624 ELEMENTS (OF 443848 DEFINED) SELECTED BY ESEL COMMAND. SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET. 555524 NODES (OF 792654 DEFINED) SELECTED FROM 182624 SELECTED ELEMENTS BY NSLE COMMAND. SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 1 KVAL = 1 VALUES = -0.94695E-03 -0.94695E-03 -0.94695E-03 -0.94695E-03 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 2 KVAL = 1 VALUES = 0.0000 0.0000 0.0000 0.0000 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS LKEY = 3 KVAL = 1 VALUES = 0.0000 0.0000 0.0000 0.0000 ALL SELECT FOR ITEM=NODE COMPONENT= IN RANGE 1 TO 792654 STEP 1 792654 NODES (OF 792654 DEFINED) SELECTED BY NSEL COMMAND. ALL SELECT FOR ITEM=ELEM COMPONENT= IN RANGE 1 TO 443848 STEP 1 443848 ELEMENTS (OF 443848 DEFINED) SELECTED BY ESEL COMMAND. PRINTOUT RESUMED BY /GOP USE 1 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM FOR AUTOMATIC TIME STEPPING: USE 1 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 ***** ANSYS SOLVE COMMAND ***** *** WARNING *** CP = 5.578 TIME= 17:55:17 Element shape checking is currently inactive. Issue SHPP,ON or SHPP,WARN to reactivate, if desired. *** NOTE *** CP = 7.281 TIME= 17:55:18 The model data was checked and warning messages were found. Please review output or errors file ( C:\Users\Admin\Documents\ansys\_ProjectScratch\Scr6808\file.err ) for these warning messages. *** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS *** --- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS --- ELEMENT TYPE 1 IS SHELL281. IT IS ASSOCIATED WITH ELASTOPLASTIC MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND HAS BEEN RESET. KEYOPT(1-12)= 0 0 0 0 0 0 0 2 0 0 0 0 ELEMENT TYPE 2 IS SHELL281. IT IS ASSOCIATED WITH ELASTOPLASTIC MATERIALS ONLY. KEYOPT(8)=2 IS SUGGESTED AND HAS BEEN RESET. KEYOPT(1-12)= 0 0 0 0 0 0 0 2 0 0 0 0 ELEMENT TYPE 3 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 3 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 4 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 4 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 5 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 5 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 6 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 6 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 7 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 7 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 8 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 8 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 9 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 9 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 10 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 10 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 11 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 11 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 12 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 12 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 13 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 13 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 14 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 14 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 15 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 15 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 16 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 16 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 17 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 17 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 18 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 18 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 19 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 19 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 20 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 20 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 21 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 21 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 22 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 22 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 23 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 23 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 24 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 24 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 25 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 25 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 26 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 26 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 27 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 27 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 28 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 28 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 29 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 29 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. ELEMENT TYPE 30 IS BEAM189 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS SECTIONS BUT IT CAN NOT BE RESET HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY. ELEMENT TYPE 30 IS BEAM189 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO RESETTING IS NEEDED. *** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE 2019 R3 19.5 *** ANSYS Mechanical Enterprise 20120530 VERSION=WINDOWS x64 17:55:19 SEP 20, 2019 CP= 7.688 Chakra--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 GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC *** WARNING *** CP = 7.938 TIME= 17:55:19 Material number 35 (used by element 261225) 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 = 8.797 TIME= 17:55:20 The step data was checked and warning messages were found. Please review output or errors file ( C:\Users\Admin\Documents\ansys\_ProjectScratch\Scr6808\file.err ) for these warning messages. *** NOTE *** CP = 8.797 TIME= 17:55:20 The conditions for direct assembly have been met. No .emat or .erot files will be produced. *** NOTE *** CP = 16.406 TIME= 17:55:24 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 NUMBER OF SUBSTEPS. . . . . . . . . . . . . . . 1 STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO 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 *** NOTE *** CP = 17.516 TIME= 17:55:26 Deformable-deformable contact pair identified by real constant set 31 and contact element type 31 has been set up. Penalty based shell-shell assembly Node-surface contact pair is defined Contact force based contact model Linear contact is defined Contact algorithm: Augmented Lagrange method Contact detection at: nodal point (normal to target surface) Contact stiffness factor FKN 10.000 The resulting initial contact stiffness 0.20000E+08 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.50000E-01 Default opening contact stiffness OPSF will be used. Default tangent stiffness factor FKT 1.0000 Use constant contact stiffness Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.50000 Average contact pair depth 0.50000 Pinball region factor PINB 1.0000 The resulting pinball region 0.50000 Default target edge extension factor TOLS 10.000 Initial penetration/gap is excluded. Bonded contact (always) is defined. *** NOTE *** CP = 17.516 TIME= 17:55:26 No contact was detected for this contact pair. **************************************** *** NOTE *** CP = 17.516 TIME= 17:55:26 Deformable-deformable contact pair identified by real constant set 33 and contact element type 33 has been set up. Penalty based shell-shell assembly Node-surface contact pair is defined Contact force based contact model Linear contact is defined Contact algorithm: Augmented Lagrange method Contact detection at: nodal point (normal to target surface) Contact stiffness factor FKN 10.000 The resulting initial contact stiffness 0.20000E+08 Default penetration tolerance factor FTOLN 0.10000 The resulting penetration tolerance 0.50000E-01 Default opening contact stiffness OPSF will be used. Default tangent stiffness factor FKT 1.0000 Use constant contact stiffness Default Max. friction stress TAUMAX 0.10000E+21 Average contact surface length 0.50000 Average contact pair depth 0.50000 Pinball region factor PINB 1.0000 The resulting pinball region 0.50000 Default target edge extension factor TOLS 10.000 Initial penetration/gap is excluded. Bonded contact (always) is defined. *** NOTE *** CP = 17.516 TIME= 17:55:26 No contact was detected for this contact pair. **************************************** *** WARNING *** CP = 17.516 TIME= 17:55:26 All selected contact pairs are initially open. Rigid body motion can occur. You may use auto CNOF/ICONT by setting KEYOPT(5) to close small gaps. *** NOTE *** CP = 17.516 TIME= 17:55:26 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. ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 31 *** NOTE *** CP = 77.266 TIME= 17:56:03 No contact was detected. Max. Pinball distance 0.5. One of the contact searching regions contains at least 20 target elements. ************************************************* ************************************************* SUMMARY FOR CONTACT PAIR IDENTIFIED BY REAL CONSTANT SET 33 *** NOTE *** CP = 77.297 TIME= 17:56:03 No contact was detected. Max. Pinball distance 0.5. One of the contact searching regions contains at least 16 target elements. ************************************************* *********** PRECISE MASS SUMMARY *********** TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN Translational mass | Coupled translational/rotational mass 0.17124E-02 0.0000 0.0000 | 0.0000 -0.45278E-01 -0.40101E-03 0.0000 0.17124E-02 0.0000 | 0.45278E-01 0.0000 0.35139E-01 0.0000 0.0000 0.17124E-02 | 0.40101E-03 -0.35139E-01 0.0000 ------------------------------------------ | ------------------------------------------ | Rotational mass (inertia) | 33.735 0.45901E-03 1.4671 | 0.45901E-03 25.556 -0.28989E-01 | 1.4671 -0.28989E-01 10.773 TOTAL MASS = 0.17124E-02 The mass principal axes coincide with the global Cartesian axes CENTER OF MASS (X,Y,Z)= 20.520 0.23418 -26.441 TOTAL INERTIA ABOUT CENTER OF MASS 32.538 0.86880E-02 0.53798 0.86880E-02 23.637 -0.39592E-01 0.53798 -0.39592E-01 10.052 PRINCIPAL INERTIAS = 32.550 23.637 10.039 ORIENTATION VECTORS OF THE INERTIA PRINCIPAL AXES IN GLOBAL CARTESIAN ( 1.000, 0.001, 0.024) (-0.001, 1.000,-0.003) (-0.024, 0.003, 1.000) *** MASS SUMMARY BY ELEMENT TYPE *** TYPE MASS 1 0.795821E-03 2 0.748920E-03 3 0.598808E-05 4 0.598808E-05 5 0.598808E-05 6 0.598808E-05 7 0.598808E-05 8 0.598808E-05 9 0.598808E-05 10 0.598808E-05 11 0.598808E-05 12 0.598808E-05 13 0.598808E-05 14 0.598808E-05 15 0.598808E-05 16 0.598808E-05 17 0.598808E-05 18 0.598808E-05 19 0.598808E-05 20 0.598808E-05 21 0.598808E-05 22 0.598808E-05 23 0.598808E-05 24 0.598808E-05 25 0.598808E-05 26 0.598808E-05 27 0.598808E-05 28 0.598808E-05 29 0.598808E-05 30 0.598808E-05 Range of element maximum matrix coefficients in global coordinates Maximum = 63912778.8 at element 258813. Minimum = 666298.556 at element 23274. *** ELEMENT MATRIX FORMULATION TIMES TYPE NUMBER ENAME TOTAL CP AVE CP 1 182624 SHELL281 61.547 0.000337 2 75908 SHELL281 25.078 0.000330 3 36 BEAM189 0.000 0.000000 4 36 BEAM189 0.000 0.000000 5 36 BEAM189 0.000 0.000000 6 36 BEAM189 0.000 0.000000 7 36 BEAM189 0.000 0.000000 8 36 BEAM189 0.000 0.000000 9 36 BEAM189 0.000 0.000000 10 36 BEAM189 0.000 0.000000 11 36 BEAM189 0.062 0.001736 12 36 BEAM189 0.000 0.000000 13 36 BEAM189 0.000 0.000000 14 36 BEAM189 0.000 0.000000 15 36 BEAM189 0.000 0.000000 16 36 BEAM189 0.000 0.000000 17 36 BEAM189 0.000 0.000000 18 36 BEAM189 0.000 0.000000 19 36 BEAM189 0.062 0.001736 20 36 BEAM189 0.000 0.000000 21 36 BEAM189 0.000 0.000000 22 36 BEAM189 0.000 0.000000 23 36 BEAM189 0.000 0.000000 24 36 BEAM189 0.000 0.000000 25 36 BEAM189 0.000 0.000000 26 36 BEAM189 0.000 0.000000 27 36 BEAM189 0.062 0.001736 28 36 BEAM189 0.000 0.000000 29 36 BEAM189 0.000 0.000000 30 36 BEAM189 0.016 0.000434 31 28 CONTA175 0.000 0.000000 32 700 TARGE170 0.125 0.000179 33 28 CONTA175 0.016 0.000558 34 928 TARGE170 0.000 0.000000 35 182624 SURF154 23.969 0.000131 Time at end of element matrix formulation CP = 77.375. SPARSE MATRIX DIRECT SOLVER. Number of equations = 4744398, Maximum wavefront = 132 *** ERROR *** CP = 123.516 TIME= 17:57:59 There is not enough memory for the Sparse Matrix Solver to proceed using the out-of-core memory mode. The total memory required by all processes = 10924 MB. The total physical memory that is available on the system = 7092 MB. Please decrease the model size, or run this model on another system with more physical memory. NUMBER OF WARNING MESSAGES ENCOUNTERED= 3 NUMBER OF ERROR MESSAGES ENCOUNTERED= 1 ***** PROBLEM TERMINATED BY INDICATED ERROR(S) OR BY END OF INPUT DATA ***** *** WARNING *** CP = 128.422 TIME= 17:58:32 During this session the elapsed time exceeds the CPU time by 124%. Often this indicates either a lack of physical memory (RAM) required to efficiently handle this simulation or it indicates a particularly slow hard drive configuration. This simulation can be expected to run faster on identical hardware if additional RAM or a faster hard drive configuration is made available. For more details, please see the ANSYS Performance Guide which is part of the ANSYS Help system. +--------------------- A N S Y S S T A T I S T I C S ------------------------+ Release: 2019 R3 Build: 19.5 Update: UP20190805 Platform: WINDOWS x64 Date Run: 09/20/2019 Time: 17:58 Process ID: 4196 Operating System: Windows 10 (Build: 18362) Processor Model: Intel(R) Core(TM) i5-4300M CPU @ 2.60GHz Compiler: Intel(R) FORTRAN Compiler Version 17.0.6 (Build: 20171215) Intel(R) C/C++ Compiler Version 17.0.6 (Build: 20171215) Intel(R) Math Kernel Library Version 2017.0.3 Product Build 20170413 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 Input File: dummy.dat Working Directory: C:\Users\Admin\Documents\ansys\_ProjectScratch\Scr6808 Total CPU time for main thread : 89.9 seconds Total CPU time summed for all threads : 128.4 seconds Elapsed time spent pre-processing model (/PREP7) : 3.0 seconds Elapsed time spent solution - preprocessing : 9.0 seconds Elapsed time spent computing solution : 156.6 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 : 7572.0 MB Maximum total memory allocated : 8256.0 MB Total physical memory available : 8 GB Total amount of I/O written to disk : 2.1 GB Total amount of I/O read from disk : 0.0 GB +------------------ E N D A N S Y S S T A T I S T I C S -------------------+ *---------------------------------------------------------------------------* | | | ANSYS RUN COMPLETED | | | |---------------------------------------------------------------------------| | | | Ansys 2019 R3 Build 19.5 UP20190805 WINDOWS x64 | | | |---------------------------------------------------------------------------| | | | Database Requested(-db) 1024 MB Scratch Memory Requested 1024 MB | | Maximum Database Used 528 MB Maximum Scratch Memory Used 7044 MB | | | |---------------------------------------------------------------------------| | | | CP Time (sec) = 128.391 Time = 17:58:32 | | Elapsed Time (sec) = 201.000 Date = 09/20/2019 | | | *---------------------------------------------------------------------------*