
 ANSYS Academic Teaching Advanced                  


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 |   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     |
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 ***************************************************************
 *            ANSYS 2019 R3          LEGAL NOTICES             *
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 * Copyright 1971-2019 ANSYS, Inc.  All rights reserved.       *
 * Unauthorized use, distribution or duplication is            *
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 * documentation CD or online help for the complete Legal      *
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 * THIS ANSYS SOFTWARE PRODUCT AND PROGRAM DOCUMENTATION       *
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 2019 R3 
     
 Point Releases and Patches installed:   
     
 ANSYS, Inc. Products 2019 R3
 SpaceClaim 2019 R3  
 AIM 2019 R3 
 Live (includes SpaceClaim) 2019 R3  
 Autodyn 2019 R3 
 LS-DYNA 2019 R3 
 Customization Files for User Programmable Features 2019 R3  
 Mechanical Products 2019 R3 
 Additive 2019 R3
 Viewer 2019 R3  
 ACIS Geometry Interface 2019 R3 
 AutoCAD Geometry Interface 2019 R3  
 Catia, Version 5 Geometry Interface 2019 R3 
 Catia, Version 6 Geometry Interface 2019 R3 
 Creo Elements/Direct Modeling Geometry Interface 2019 R3
 Creo Parametric Geometry Interface 2019 R3  
 Inventor Geometry Interface 2019 R3 
 JTOpen Geometry Interface 2019 R3   
 NX Geometry Interface 2019 R3   
 Parasolid Geometry Interface  2019 R3   
 Solid Edge Geometry Interface 2019 R3   
 SOLIDWORKS Geometry Interface 2019 R3   
 ANSYS, Inc. License Manager 2019 R3 


          *****  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
  DESIGNXPLORER REQUESTED
  INPUT FILE NAME              = C:\Users\201285_Abdul_moghni\Desktop\Train_Faze_4\_ProjectScratch\ScrE68E\dummy.dat
  OUTPUT FILE NAME             = C:\Users\201285_Abdul_moghni\Desktop\Train_Faze_4\_ProjectScratch\ScrE68E\solve.out
  START-UP FILE MODE           = NOREAD
  STOP FILE MODE               = NOREAD

 RELEASE= 2019 R3              BUILD= 19.5      UP20190805   VERSION=WINDOWS x64 
 CURRENT JOBNAME=file0  01:11:00  APR 30, 2021 CP=      0.219


 PARAMETER _DS_PROGRESS =     999.0000000    

 /INPUT FILE= ds.dat  LINE=       0



 *** NOTE ***                            CP =       0.328   TIME= 01:11:00
 The /CONFIG,NOELDB command is not valid in a Distributed ANSYS          
 solution.  Command is ignored.                                          

 *GET  _WALLSTRT  FROM  ACTI  ITEM=TIME WALL  VALUE=  1.18333333    

 TITLE= 
 my_3d_Bc--Static Structural (A5)                                              


 SET PARAMETER DIMENSIONS ON  _WB_PROJECTSCRATCH_DIR
  TYPE=STRI  DIMENSIONS=      248        1        1

 PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\201285_Abdul_moghni\Desktop\Train_Faze_4\_ProjectScratch\ScrE68E\

 SET PARAMETER DIMENSIONS ON  _WB_SOLVERFILES_DIR
  TYPE=STRI  DIMENSIONS=      248        1        1

 PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\201285_Abdul_moghni\Desktop\Train_Faze_4\my_3d_Bc_files\dp0\SYS\MECH\

 SET PARAMETER DIMENSIONS ON  _WB_USERFILES_DIR
  TYPE=STRI  DIMENSIONS=      248        1        1

 PARAMETER _WB_USERFILES_DIR(1) = C:\Users\201285_Abdul_moghni\Desktop\Train_Faze_4\my_3d_Bc_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     ***
 DISTRIBUTED ANSYS Academic Teaching Advanced                  

 00292481  VERSION=WINDOWS x64   01:11:00  APR 30, 2021 CP=      0.328

 my_3d_Bc--Static Structural (A5)                                              



          ***** ANSYS ANALYSIS DEFINITION (PREP7) *****
 *********** Nodes for the whole assembly ***********
 *********** Nodes for all Remote Points ***********
 *********** Elements for Body 1 "Line Body" ***********
 *********** Elements for Body 2 "Line Body" ***********
 *********** Elements for Body 3 "Line Body" ***********
 *********** Elements for Body 4 "Line Body" ***********
 *********** Elements for Body 5 "Line Body" ***********
 *********** Elements for Body 6 "Line Body" ***********
 *********** Elements for Body 7 "Line Body" ***********
 *********** Elements for Body 8 "Line Body" ***********
 *********** Elements for Body 9 "Line Body" ***********
 *********** Elements for Body 10 "Line Body" ***********
 *********** Elements for Body 11 "Line Body" ***********
 *********** Elements for Body 12 "Line Body" ***********
 *********** Elements for Body 13 "Line Body" ***********
 *********** Elements for Body 14 "Line Body" ***********
 *********** Elements for Body 15 "Line Body" ***********
 *********** Elements for Body 16 "Line Body" ***********
 *********** Elements for Body 17 "Line Body" ***********
 *********** Elements for Body 18 "Line Body" ***********
 *********** Elements for Body 19 "Line Body" ***********
 *********** Elements for Body 20 "Line Body" ***********
 *********** Elements for Body 21 "Line Body" ***********
 *********** Elements for Body 22 "Line Body" ***********
 *********** Elements for Body 23 "Line Body" ***********
 *********** Elements for Body 24 "Line Body" ***********
 *********** Elements for Body 25 "Line Body" ***********
 *********** Elements for Body 26 "Line Body" ***********
 *********** Elements for Body 27 "Line Body" ***********
 *********** Elements for Body 28 "Line Body" ***********
 *********** Elements for Body 29 "Line Body" ***********
 *********** Elements for Body 30 "Line Body" ***********
 *********** Elements for Body 31 "Line Body" ***********
 *********** Elements for Body 32 "Line Body" ***********
 *********** Elements for Body 33 "Line Body" ***********
 *********** Elements for Body 34 "Line Body" ***********
 *********** Elements for Body 35 "Line Body" ***********
 *********** Elements for Body 36 "Line Body" ***********
 *********** Elements for Body 37 "Line Body" ***********
 *********** Elements for Body 38 "Line Body" ***********
 *********** Elements for Body 39 "Line Body" ***********
 *********** Elements for Body 40 "Line Body" ***********
 *********** Elements for Body 41 "Line Body" ***********
 *********** Elements for Body 42 "Line Body" ***********
 *********** Elements for Body 43 "Line Body" ***********
 *********** Elements for Body 44 "Line Body" ***********
 *********** Elements for Body 45 "Line Body" ***********
 *********** Elements for Body 46 "Line Body" ***********
 *********** Elements for Body 47 "Line Body" ***********
 *********** Elements for Body 48 "Line Body" ***********
 *********** Elements for Body 49 "Line Body" ***********
 *********** Elements for Body 50 "Line Body" ***********
 *********** Elements for Body 51 "Line Body" ***********
 *********** Elements for Body 52 "Line Body" ***********
 *********** Elements for Body 53 "Line Body" ***********
 *********** Elements for Body 54 "Line Body" ***********
 *********** Elements for Body 55 "Line Body" ***********
 *********** Elements for Body 56 "Line Body" ***********
 *********** Elements for Body 57 "Line Body" ***********
 *********** Elements for Body 58 "Line Body" ***********
 *********** Elements for Body 59 "Line Body" ***********
 *********** Elements for Body 60 "Line Body" ***********
 *********** Elements for Body 61 "Line Body" ***********
 *********** Elements for Body 62 "Line Body" ***********
 *********** Elements for Body 63 "Line Body" ***********
 *********** Elements for Body 64 "Line Body" ***********
 *********** Elements for Body 65 "Line Body" ***********
 *********** Elements for Body 66 "Line Body" ***********
 *********** Elements for Body 67 "Line Body" ***********
 *********** Elements for Body 68 "Line Body" ***********
 *********** Elements for Body 69 "Line Body" ***********
 *********** Elements for Body 70 "Line Body" ***********
 *********** Elements for Body 71 "Line Body" ***********
 *********** Elements for Body 72 "Line Body" ***********
 *********** Elements for Body 73 "Line Body" ***********
 *********** Elements for Body 74 "Line Body" ***********
 *********** Elements for Body 75 "Line Body" ***********
 *********** Elements for Body 76 "Line Body" ***********
 *********** Elements for Body 77 "Line Body" ***********
 *********** Elements for Body 78 "Line Body" ***********
 *********** Send User Defined Coordinate System(s) ***********
 *********** Set Reference Temperature ***********
 *********** Send Materials ***********
 *********** Send Beam Properties ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Define Vertex Force Using Follower Elements ***********
 *********** Create Remote Point "Internal Remote Point" ***********
 *********** Create Remote Point "Internal Remote Point 3" ***********
 *********** Create Remote Point "Internal Remote Point 4" ***********
 *********** Create Remote Point "Internal Remote Point 5" ***********
 *********** Construct Remote Displacement ***********
 *********** Construct Remote Displacement ***********
 *********** Construct Remote Displacement ***********
 *********** Construct Remote Displacement ***********
 *** Create a component for all remote displacements ***


 ***** ROUTINE COMPLETED *****  CP =         0.781


 --- Number of total nodes = 152
 --- Number of contact elements = 0
 --- Number of spring elements = 0
 --- Number of bearing elements = 0
 --- Number of solid elements = 104
 --- Number of condensed parts = 0
 --- Number of total elements = 244

 *GET  _WALLBSOL  FROM  ACTI  ITEM=TIME WALL  VALUE=  1.18333333    
 ****************************************************************************
 *************************    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

 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.

 DO NOT SAVE ANY RESTART FILES AT ALL
 ****************************************************
 ******************* SOLVE FOR LS 1 OF 1 ****************

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        79 TO         79 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        80 TO         80 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -10485.        -10485.        -10485.        -10485.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        81 TO         81 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        82 TO         82 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        83 TO         83 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14815.        -14815.        -14815.        -14815.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        84 TO         84 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        85 TO         85 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        86 TO         86 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14318.        -14318.        -14318.        -14318.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        87 TO         87 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        88 TO         88 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        89 TO         89 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -15354.        -15354.        -15354.        -15354.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        90 TO         90 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        91 TO         91 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        92 TO         92 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -15477.        -15477.        -15477.        -15477.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        93 TO         93 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        94 TO         94 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        95 TO         95 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -15025.        -15025.        -15025.        -15025.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        96 TO         96 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        97 TO         97 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        98 TO         98 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -15477.        -15477.        -15477.        -15477.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        99 TO         99 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       100 TO        100 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       101 TO        101 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -15354.        -15354.        -15354.        -15354.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       102 TO        102 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       103 TO        103 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       104 TO        104 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14318.        -14318.        -14318.        -14318.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       105 TO        105 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       106 TO        106 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       107 TO        107 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14815.        -14815.        -14815.        -14815.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       108 TO        108 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       109 TO        109 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       110 TO        110 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -10485.        -10485.        -10485.        -10485.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       111 TO        111 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       112 TO        112 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       113 TO        113 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12716.        -12716.        -12716.        -12716.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       114 TO        114 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       115 TO        115 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       116 TO        116 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14705.        -14705.        -14705.        -14705.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       117 TO        117 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       118 TO        118 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       119 TO        119 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14851.        -14851.        -14851.        -14851.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       120 TO        120 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       121 TO        121 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       122 TO        122 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14590.        -14590.        -14590.        -14590.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       123 TO        123 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       124 TO        124 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       125 TO        125 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -13546.        -13546.        -13546.        -13546.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       126 TO        126 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       127 TO        127 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       128 TO        128 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -13324.        -13324.        -13324.        -13324.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       129 TO        129 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       130 TO        130 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       131 TO        131 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -13546.        -13546.        -13546.        -13546.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       132 TO        132 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       133 TO        133 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       134 TO        134 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14590.        -14590.        -14590.        -14590.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       135 TO        135 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       136 TO        136 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       137 TO        137 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14851.        -14851.        -14851.        -14851.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       138 TO        138 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       139 TO        139 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       140 TO        140 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -14705.        -14705.        -14705.        -14705.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       141 TO        141 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       142 TO        142 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       143 TO        143 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12716.        -12716.        -12716.        -12716.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE       144 TO        144 STEP          1

          2  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =     0.0000         0.0000         0.0000         0.0000    

 ALL SELECT   FOR ITEM=ELEM COMPONENT=    
  IN RANGE         1 TO        248 STEP          1

        244  ELEMENTS (OF        244  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED CONSTRAINT UX   FOR SELECTED NODES          149 TO         149 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UY   FOR SELECTED NODES          149 TO         149 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UZ   FOR SELECTED NODES          149 TO         149 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES          149 TO         149 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTY FOR SELECTED NODES          149 TO         149 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UX   FOR SELECTED NODES          150 TO         150 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UY   FOR SELECTED NODES          150 TO         150 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UZ   FOR SELECTED NODES          150 TO         150 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES          150 TO         150 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTY FOR SELECTED NODES          150 TO         150 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UY   FOR SELECTED NODES          151 TO         151 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UZ   FOR SELECTED NODES          151 TO         151 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES          151 TO         151 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTY FOR SELECTED NODES          151 TO         151 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UY   FOR SELECTED NODES          152 TO         152 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UZ   FOR SELECTED NODES          152 TO         152 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES          152 TO         152 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTY FOR SELECTED NODES          152 TO         152 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 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

 *** NOTE ***                            CP =       0.797   TIME= 01:11:00
 The automatic domain decomposition logic has selected the MESH domain   
 decomposition method with 2 processes per solution.                     

 *****  ANSYS SOLVE    COMMAND  *****

 *** WARNING ***                         CP =       0.797   TIME= 01:11:00
 Element shape checking is currently inactive.  Issue SHPP,ON or         
 SHPP,WARN to reactivate, if desired.                                    

 *** NOTE ***                            CP =       0.797   TIME= 01:11:00
 The model data was checked and warning messages were found.             
  Please review output or errors file (                                  
 C:\Users\201285_Abdul_moghni\Desktop\Train_Faze_4\_ProjectScratch\ScrE6 
 68E\file0.err ) for these warning messages.                             

 *** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
      --- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---

 ELEMENT TYPE    1 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE    1 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE    2 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE    2 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE    3 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE    3 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE    4 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE    4 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE    5 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE    5 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE    6 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE    6 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE    7 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE    7 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE    8 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE    8 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE    9 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE    9 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   10 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   10 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   11 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   11 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   12 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   12 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   13 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   13 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   14 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   14 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   15 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   15 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   16 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   16 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   17 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   17 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   18 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   18 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   19 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   19 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   20 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   20 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   21 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   21 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   22 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   22 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   23 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   23 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   24 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   24 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   25 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   25 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   26 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   26 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   27 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   27 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   28 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   28 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   29 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   29 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   30 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   30 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   31 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   31 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   32 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   32 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   33 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   33 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   34 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   34 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   35 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   35 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   36 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   36 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   37 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   37 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   38 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   38 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   39 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   39 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   40 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   40 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   41 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   41 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   42 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   42 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   43 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   43 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   44 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   44 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   45 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   45 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   46 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   46 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   47 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   47 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   48 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   48 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   49 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   49 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   50 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   50 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   51 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   51 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   52 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   52 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   53 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   53 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   54 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   54 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   55 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   55 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   56 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   56 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   57 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   57 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   58 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   58 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   59 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   59 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   60 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   60 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   61 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   61 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   62 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   62 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   63 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   63 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   64 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   64 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   65 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   65 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   66 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   66 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   67 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   67 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   68 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   68 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   69 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   69 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   70 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   70 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   71 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   71 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   72 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   72 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   73 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   73 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   74 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   74 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   75 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   75 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   76 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   76 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   77 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   77 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.

 ELEMENT TYPE   78 IS BEAM188 . KEYOPT(1)=1 IS SUGGESTED FOR NON-CIRCULAR CROSS
 SECTIONS AND KEYOPT(3) IS ALREADY SET AS SUGGESTED. KEYOPT(1) CAN NOT BE RESET
 HERE. PLEASE RESET IT MANUALLY ACCORDING TO CROSS SECTION TYPES IF NECESSARY.

 ELEMENT TYPE   78 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
 RESETTING IS NEEDED.



 *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2019 R3          19.5     ***
 DISTRIBUTED ANSYS Academic Teaching Advanced                  

 00292481  VERSION=WINDOWS x64   01:11:00  APR 30, 2021 CP=      0.797

 my_3d_Bc--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 =       0.812   TIME= 01:11:00
 Material number 79 (used by element 109) 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 =       0.812   TIME= 01:11:00
 The step data was checked and warning messages were found.              
  Please review output or errors file (                                  
 C:\Users\201285_Abdul_moghni\Desktop\Train_Faze_4\_ProjectScratch\ScrE6 
 68E\file0.err ) for these warning messages.                             

 *** NOTE ***                            CP =       0.812   TIME= 01:11:00
 Internal nodes from 153 to 260 are created.                             
 4 internal nodes are used for handling degrees of freedom on pilot      
 nodes of rigid target surfaces.                                         
 104 internal nodes are used for quadratic and/or cubic options of       
 BEAM188, PIPE288, and/or SHELL208.                                      

 *** NOTE ***                            CP =       0.812   TIME= 01:11:00
 Internal nodes from 153 to 166 are created.                             
 4 internal nodes are used for handling degrees of freedom on pilot      
 nodes of rigid target surfaces.                                         
 10 internal nodes are used for quadratic and/or cubic options of        
 BEAM188, PIPE288, and/or SHELL208.                                      

 *** NOTE ***                            CP =       0.812   TIME= 01:11:00
 Rigid target surface identified by real constant set 145.  The degrees  
 of freedom of the rigid surface are driven by the pilot node 149.       
 Internal MPC will be built.                                             
 Boundary conditions can be applied on any target node.
 The rigid surface does not overlap other elements.                      
 The used degrees of freedom set is  UX   UY   UZ   ROTX ROTY ROTZ
 ****************************************
  

 *** NOTE ***                            CP =       0.812   TIME= 01:11:00
 Rigid target surface identified by real constant set 146.  The degrees  
 of freedom of the rigid surface are driven by the pilot node 150.       
 Internal MPC will be built.                                             
 Boundary conditions can be applied on any target node.
 The rigid surface does not overlap other elements.                      
 The used degrees of freedom set is  UX   UY   UZ   ROTX ROTY ROTZ
 ****************************************
  

 *** NOTE ***                            CP =       0.812   TIME= 01:11:00
 Rigid target surface identified by real constant set 147.  The degrees  
 of freedom of the rigid surface are driven by the pilot node 151.       
 Internal MPC will be built.                                             
 Boundary conditions can be applied on any target node.
 The rigid surface does not overlap other elements.                      
 The used degrees of freedom set is  UX   UY   UZ   ROTX ROTY ROTZ
 ****************************************
  

 *** NOTE ***                            CP =       0.812   TIME= 01:11:00
 Rigid target surface identified by real constant set 148.  The degrees  
 of freedom of the rigid surface are driven by the pilot node 152.       
 Internal MPC will be built.                                             
 Boundary conditions can be applied on any target node.
 The rigid surface does not overlap other elements.                      
 The used degrees of freedom set is  UX   UY   UZ   ROTX ROTY ROTZ
 ****************************************
  
  
  

 *** NOTE ***                            CP =       0.812   TIME= 01:11:00
 Internal nodes from 153 to 260 are created.                             
 4 internal nodes are used for handling degrees of freedom on pilot      
 nodes of rigid target surfaces.                                         
 104 internal nodes are used for quadratic and/or cubic options of       
 BEAM188, PIPE288, and/or SHELL208.                                      

  
  
     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: 244
  ...Number of nodes:    260
  ...Decompose to 2 CPU domains
  ...Element load balance ratio =     2.008


                      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 =       0.844   TIME= 01:11:00
 Rigid target surface identified by real constant set 145.  The degrees  
 of freedom of the rigid surface are driven by the pilot node 149.       
 Internal MPC will be built.                                             
 Boundary conditions can be applied on any target node.
 The used degrees of freedom set is  UX   UY   UZ   ROTX ROTY ROTZ
 ****************************************
  

 *** NOTE ***                            CP =       0.844   TIME= 01:11:00
 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.                            

  
 The FEA model contains 0 external CE equations and 24 internal CE       
 equations.                                                              


                         ***********  PRECISE MASS SUMMARY  ***********

   TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
               Translational mass               |   Coupled translational/rotational mass
         50.857        0.0000        0.0000     |     0.0000        76286.      -0.10629E+06
         0.0000        50.857        0.0000     |    -76286.        0.0000       0.10527E+07
         0.0000        0.0000        50.857     |    0.10629E+06  -0.10527E+07    0.0000    
     ------------------------------------------ | ------------------------------------------
                                                |         Rotational mass (inertia)
                                                |    0.60931E+09  -0.22002E+10  -0.15791E+10
                                                |   -0.22002E+10   0.29948E+11  -0.15944E+09
                                                |   -0.15791E+10  -0.15944E+09   0.30116E+11

   TOTAL MASS =  50.857    
     The mass principal axes coincide with the global Cartesian axes

   CENTER OF MASS (X,Y,Z)=    20700.        2090.0        1500.0    

   TOTAL INERTIA ABOUT CENTER OF MASS
        0.27273E+09   0.95367E-06  -0.30994E-05
        0.95367E-06   0.80418E+10  -0.26822E-06
       -0.30994E-05  -0.26822E-06   0.81017E+10
     The inertia principal axes coincide with the global Cartesian axes


  *** MASS SUMMARY BY ELEMENT TYPE ***

  TYPE      MASS
     1  0.301440    
     2  0.301440    
     3   1.37276    
     4   1.42996    
     5  0.577760    
     6  0.370559    
     7  0.325369    
     8   1.42996    
     9  0.370559    
    10  0.577760    
    11   1.37276    
    12  0.301440    
    13  0.325369    
    14  0.301440    
    15  0.433320    
    16  0.433320    
    17  0.226080    
    18  0.226080    
    19  0.226080    
    20  0.226080    
    21  0.301440    
    22  0.301440    
    23  0.301440    
    24  0.301440    
    25  0.301440    
    26  0.301440    
    27  0.301440    
    28   1.37276    
    29   4.43026    
    30  0.844974    
    31  0.844974    
    32   3.76988    
    33   1.42996    
    34  0.577760    
    35  0.370559    
    36  0.325369    
    37  0.325369    
    38  0.325369    
    39  0.280179    
    40  0.280179    
    41  0.560357    
    42  0.301440    
    43  0.844974    
    44  0.325369    
    45  0.301440    
    46  0.301440    
    47   4.43026    
    48  0.280179    
    49  0.301440    
    50  0.560357    
    51   3.76988    
    52  0.301440    
    53  0.280179    
    54  0.325369    
    55  0.844974    
    56  0.301440    
    57  0.325369    
    58   1.42996    
    59  0.370559    
    60   1.37276    
    61  0.301440    
    62  0.577760    
    63  0.433320    
    64  0.433320    
    65  0.226080    
    66  0.226080    
    67  0.226080    
    68  0.226080    
    69  0.226080    
    70  0.226080    
    71  0.226080    
    72  0.226080    
    73  0.226080    
    74  0.226080    
    75  0.226080    
    76  0.226080    
    77  0.226080    
    78  0.226080    

 Range of element maximum matrix coefficients in global coordinates
 Maximum = 4.497997653E+12 at element 69.                                
 Minimum = 5.568202818E+11 at element 64.                                

   *** ELEMENT MATRIX FORMULATION TIMES
     TYPE    NUMBER   ENAME      TOTAL CP  AVE CP

        1         1  BEAM188       0.000   0.000000
        2         1  BEAM188       0.000   0.000000
        3         2  BEAM188       0.000   0.000000
        4         2  BEAM188       0.000   0.000000
        5         1  BEAM188       0.000   0.000000
        6         1  BEAM188       0.000   0.000000
        7         1  BEAM188       0.000   0.000000
        8         2  BEAM188       0.000   0.000000
        9         1  BEAM188       0.000   0.000000
       10         1  BEAM188       0.000   0.000000
       11         2  BEAM188       0.000   0.000000
       12         1  BEAM188       0.000   0.000000
       13         1  BEAM188       0.000   0.000000
       14         1  BEAM188       0.000   0.000000
       15         1  BEAM188       0.000   0.000000
       16         1  BEAM188       0.000   0.000000
       17         1  BEAM188       0.000   0.000000
       18         1  BEAM188       0.000   0.000000
       19         1  BEAM188       0.000   0.000000
       20         1  BEAM188       0.000   0.000000
       21         1  BEAM188       0.000   0.000000
       22         1  BEAM188       0.000   0.000000
       23         1  BEAM188       0.000   0.000000
       24         1  BEAM188       0.000   0.000000
       25         1  BEAM188       0.000   0.000000
       26         1  BEAM188       0.000   0.000000
       27         1  BEAM188       0.000   0.000000
       28         2  BEAM188       0.000   0.000000
       29         6  BEAM188       0.000   0.000000
       30         1  BEAM188       0.000   0.000000
       31         1  BEAM188       0.000   0.000000
       32         4  BEAM188       0.000   0.000000
       33         2  BEAM188       0.000   0.000000
       34         1  BEAM188       0.000   0.000000
       35         1  BEAM188       0.000   0.000000
       36         1  BEAM188       0.000   0.000000
       37         1  BEAM188       0.000   0.000000
       38         1  BEAM188       0.000   0.000000
       39         1  BEAM188       0.000   0.000000
       40         1  BEAM188       0.000   0.000000
       41         2  BEAM188       0.000   0.000000
       42         1  BEAM188       0.000   0.000000
       43         1  BEAM188       0.000   0.000000
       44         1  BEAM188       0.000   0.000000
       45         1  BEAM188       0.000   0.000000
       46         1  BEAM188       0.000   0.000000
       47         6  BEAM188       0.000   0.000000
       48         1  BEAM188       0.000   0.000000
       49         1  BEAM188       0.000   0.000000
       50         2  BEAM188       0.000   0.000000
       51         4  BEAM188       0.000   0.000000
       52         1  BEAM188       0.000   0.000000
       53         1  BEAM188       0.000   0.000000
       54         1  BEAM188       0.000   0.000000
       55         1  BEAM188       0.000   0.000000
       56         1  BEAM188       0.000   0.000000
       57         1  BEAM188       0.000   0.000000
       58         2  BEAM188       0.000   0.000000
       59         1  BEAM188       0.000   0.000000
       60         2  BEAM188       0.000   0.000000
       61         1  BEAM188       0.000   0.000000
       62         1  BEAM188       0.000   0.000000
       63         1  BEAM188       0.000   0.000000
       64         1  BEAM188       0.000   0.000000
       65         1  BEAM188       0.000   0.000000
       66         1  BEAM188       0.000   0.000000
       67         1  BEAM188       0.000   0.000000
       68         1  BEAM188       0.000   0.000000
       69         1  BEAM188       0.000   0.000000
       70         1  BEAM188       0.000   0.000000
       71         1  BEAM188       0.000   0.000000
       72         1  BEAM188       0.000   0.000000
       73         1  BEAM188       0.000   0.000000
       74         1  BEAM188       0.000   0.000000
       75         1  BEAM188       0.000   0.000000
       76         1  BEAM188       0.000   0.000000
       77         1  BEAM188       0.000   0.000000
       78         1  BEAM188       0.000   0.000000
       79         6  CLOAD201      0.000   0.000000
       82         6  CLOAD201      0.000   0.000000
       85         6  CLOAD201      0.000   0.000000
       88         6  CLOAD201      0.000   0.000000
       91         6  CLOAD201      0.000   0.000000
       94         6  CLOAD201      0.000   0.000000
       97         6  CLOAD201      0.000   0.000000
      100         6  CLOAD201      0.000   0.000000
      103         6  CLOAD201      0.000   0.000000
      106         6  CLOAD201      0.000   0.000000
      109         6  CLOAD201      0.000   0.000000
      112         6  CLOAD201      0.000   0.000000
      115         6  CLOAD201      0.000   0.000000
      118         6  CLOAD201      0.000   0.000000
      121         6  CLOAD201      0.000   0.000000
      124         6  CLOAD201      0.000   0.000000
      127         6  CLOAD201      0.000   0.000000
      130         6  CLOAD201      0.000   0.000000
      133         6  CLOAD201      0.000   0.000000
      136         6  CLOAD201      0.000   0.000000
      139         6  CLOAD201      0.000   0.000000
      142         6  CLOAD201      0.000   0.000000
      145         2  TARGE170      0.000   0.000000
      146         2  TARGE170      0.000   0.000000
      147         2  TARGE170      0.000   0.000000
      148         2  TARGE170      0.000   0.000000
 Time at end of element matrix formulation CP = 0.84375.                 

 DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
  Number of equations =         870,    Maximum wavefront =      6

  Local memory allocated for solver              =      0.501 MB
  Local memory required for in-core solution     =      0.440 MB
  Local memory required for out-of-core solution =      0.440 MB

  Total memory allocated for solver              =      1.347 MB
  Total memory required for in-core solution     =      1.212 MB
  Total memory required for out-of-core solution =      1.212 MB

 *** NOTE ***                            CP =       0.859   TIME= 01:11:00
 The Distributed Sparse Matrix Solver is currently running in the        
 in-core memory mode.  This memory mode uses the most amount of memory   
 in order to avoid using the hard drive as much as possible, which most  
 often results in the fastest solution time.  This mode is recommended   
 if enough physical memory is present to accommodate all of the solver   
 data.                                                                   
 curEqn=    432  totEqn=    432 Job CP sec=      0.875
      Factor Done= 100% Factor Wall sec=      0.006 rate=      55.4 Mflops
 Distributed sparse solver maximum pivot= 2.809091858E+11 at node 34     
 ROTZ.                                                                   
 Distributed sparse solver minimum pivot= 1517.2398 at node 37 UZ.       
 Distributed sparse solver minimum pivot in absolute value= 1517.2398 at 
 node 37 UZ.                                                             

   *** ELEMENT RESULT CALCULATION TIMES
     TYPE    NUMBER   ENAME      TOTAL CP  AVE CP

        1         1  BEAM188       0.000   0.000000
        2         1  BEAM188       0.000   0.000000
        3         2  BEAM188       0.000   0.000000
        4         2  BEAM188       0.000   0.000000
        5         1  BEAM188       0.000   0.000000
        6         1  BEAM188       0.000   0.000000
        7         1  BEAM188       0.000   0.000000
        8         2  BEAM188       0.000   0.000000
        9         1  BEAM188       0.000   0.000000
       10         1  BEAM188       0.000   0.000000
       11         2  BEAM188       0.000   0.000000
       12         1  BEAM188       0.000   0.000000
       13         1  BEAM188       0.000   0.000000
       14         1  BEAM188       0.000   0.000000
       15         1  BEAM188       0.000   0.000000
       16         1  BEAM188       0.000   0.000000
       17         1  BEAM188       0.000   0.000000
       18         1  BEAM188       0.000   0.000000
       19         1  BEAM188       0.000   0.000000
       20         1  BEAM188       0.000   0.000000
       21         1  BEAM188       0.000   0.000000
       22         1  BEAM188       0.000   0.000000
       23         1  BEAM188       0.000   0.000000
       24         1  BEAM188       0.000   0.000000
       25         1  BEAM188       0.000   0.000000
       26         1  BEAM188       0.000   0.000000
       27         1  BEAM188       0.000   0.000000
       28         2  BEAM188       0.000   0.000000
       29         6  BEAM188       0.000   0.000000
       30         1  BEAM188       0.000   0.000000
       31         1  BEAM188       0.000   0.000000
       32         4  BEAM188       0.000   0.000000
       33         2  BEAM188       0.000   0.000000
       34         1  BEAM188       0.000   0.000000
       35         1  BEAM188       0.000   0.000000
       36         1  BEAM188       0.000   0.000000
       37         1  BEAM188       0.000   0.000000
       38         1  BEAM188       0.000   0.000000
       39         1  BEAM188       0.000   0.000000
       40         1  BEAM188       0.000   0.000000
       41         2  BEAM188       0.000   0.000000
       42         1  BEAM188       0.000   0.000000
       43         1  BEAM188       0.000   0.000000
       44         1  BEAM188       0.000   0.000000
       45         1  BEAM188       0.000   0.000000
       46         1  BEAM188       0.000   0.000000
       47         6  BEAM188       0.000   0.000000
       48         1  BEAM188       0.000   0.000000
       49         1  BEAM188       0.000   0.000000
       50         2  BEAM188       0.000   0.000000
       51         4  BEAM188       0.000   0.000000
       52         1  BEAM188       0.000   0.000000
       53         1  BEAM188       0.000   0.000000
       54         1  BEAM188       0.000   0.000000
       55         1  BEAM188       0.000   0.000000
       56         1  BEAM188       0.000   0.000000
       57         1  BEAM188       0.000   0.000000
       58         2  BEAM188       0.000   0.000000
       59         1  BEAM188       0.000   0.000000
       60         2  BEAM188       0.000   0.000000
       61         1  BEAM188       0.000   0.000000
       62         1  BEAM188       0.000   0.000000
       63         1  BEAM188       0.000   0.000000
       64         1  BEAM188       0.000   0.000000
       65         1  BEAM188       0.000   0.000000
       66         1  BEAM188       0.000   0.000000
       67         1  BEAM188       0.000   0.000000
       68         1  BEAM188       0.000   0.000000
       69         1  BEAM188       0.000   0.000000
       70         1  BEAM188       0.000   0.000000
       71         1  BEAM188       0.000   0.000000
       72         1  BEAM188       0.000   0.000000
       73         1  BEAM188       0.000   0.000000
       74         1  BEAM188       0.000   0.000000
       75         1  BEAM188       0.000   0.000000
       76         1  BEAM188       0.000   0.000000
       77         1  BEAM188       0.000   0.000000
       78         1  BEAM188       0.000   0.000000
       79         6  CLOAD201      0.000   0.000000
       82         6  CLOAD201      0.000   0.000000
       85         6  CLOAD201      0.000   0.000000
       88         6  CLOAD201      0.000   0.000000
       91         6  CLOAD201      0.000   0.000000
       94         6  CLOAD201      0.000   0.000000
       97         6  CLOAD201      0.000   0.000000
      100         6  CLOAD201      0.000   0.000000
      103         6  CLOAD201      0.000   0.000000
      106         6  CLOAD201      0.000   0.000000
      109         6  CLOAD201      0.000   0.000000
      112         6  CLOAD201      0.000   0.000000
      115         6  CLOAD201      0.000   0.000000
      118         6  CLOAD201      0.000   0.000000
      121         6  CLOAD201      0.000   0.000000
      124         6  CLOAD201      0.000   0.000000
      127         6  CLOAD201      0.000   0.000000
      130         6  CLOAD201      0.000   0.000000
      133         6  CLOAD201      0.000   0.000000
      136         6  CLOAD201      0.000   0.000000
      139         6  CLOAD201      0.000   0.000000
      142         6  CLOAD201      0.000   0.000000

   *** NODAL LOAD CALCULATION TIMES
     TYPE    NUMBER   ENAME      TOTAL CP  AVE CP

        1         1  BEAM188       0.000   0.000000
        2         1  BEAM188       0.000   0.000000
        3         2  BEAM188       0.000   0.000000
        4         2  BEAM188       0.000   0.000000
        5         1  BEAM188       0.000   0.000000
        6         1  BEAM188       0.000   0.000000
        7         1  BEAM188       0.000   0.000000
        8         2  BEAM188       0.000   0.000000
        9         1  BEAM188       0.000   0.000000
       10         1  BEAM188       0.000   0.000000
       11         2  BEAM188       0.000   0.000000
       12         1  BEAM188       0.000   0.000000
       13         1  BEAM188       0.000   0.000000
       14         1  BEAM188       0.000   0.000000
       15         1  BEAM188       0.000   0.000000
       16         1  BEAM188       0.000   0.000000
       17         1  BEAM188       0.000   0.000000
       18         1  BEAM188       0.000   0.000000
       19         1  BEAM188       0.000   0.000000
       20         1  BEAM188       0.000   0.000000
       21         1  BEAM188       0.000   0.000000
       22         1  BEAM188       0.000   0.000000
       23         1  BEAM188       0.000   0.000000
       24         1  BEAM188       0.000   0.000000
       25         1  BEAM188       0.000   0.000000
       26         1  BEAM188       0.000   0.000000
       27         1  BEAM188       0.000   0.000000
       28         2  BEAM188       0.000   0.000000
       29         6  BEAM188       0.000   0.000000
       30         1  BEAM188       0.000   0.000000
       31         1  BEAM188       0.000   0.000000
       32         4  BEAM188       0.000   0.000000
       33         2  BEAM188       0.000   0.000000
       34         1  BEAM188       0.000   0.000000
       35         1  BEAM188       0.000   0.000000
       36         1  BEAM188       0.000   0.000000
       37         1  BEAM188       0.000   0.000000
       38         1  BEAM188       0.000   0.000000
       39         1  BEAM188       0.000   0.000000
       40         1  BEAM188       0.000   0.000000
       41         2  BEAM188       0.000   0.000000
       42         1  BEAM188       0.000   0.000000
       43         1  BEAM188       0.000   0.000000
       44         1  BEAM188       0.000   0.000000
       45         1  BEAM188       0.000   0.000000
       46         1  BEAM188       0.000   0.000000
       47         6  BEAM188       0.000   0.000000
       48         1  BEAM188       0.000   0.000000
       49         1  BEAM188       0.000   0.000000
       50         2  BEAM188       0.000   0.000000
       51         4  BEAM188       0.000   0.000000
       52         1  BEAM188       0.000   0.000000
       53         1  BEAM188       0.000   0.000000
       54         1  BEAM188       0.000   0.000000
       55         1  BEAM188       0.000   0.000000
       56         1  BEAM188       0.000   0.000000
       57         1  BEAM188       0.000   0.000000
       58         2  BEAM188       0.000   0.000000
       59         1  BEAM188       0.000   0.000000
       60         2  BEAM188       0.000   0.000000
       61         1  BEAM188       0.000   0.000000
       62         1  BEAM188       0.000   0.000000
       63         1  BEAM188       0.000   0.000000
       64         1  BEAM188       0.000   0.000000
       65         1  BEAM188       0.000   0.000000
       66         1  BEAM188       0.000   0.000000
       67         1  BEAM188       0.000   0.000000
       68         1  BEAM188       0.000   0.000000
       69         1  BEAM188       0.000   0.000000
       70         1  BEAM188       0.000   0.000000
       71         1  BEAM188       0.000   0.000000
       72         1  BEAM188       0.000   0.000000
       73         1  BEAM188       0.000   0.000000
       74         1  BEAM188       0.000   0.000000
       75         1  BEAM188       0.000   0.000000
       76         1  BEAM188       0.000   0.000000
       77         1  BEAM188       0.000   0.000000
       78         1  BEAM188       0.000   0.000000
       79         6  CLOAD201      0.000   0.000000
       82         6  CLOAD201      0.000   0.000000
       85         6  CLOAD201      0.000   0.000000
       88         6  CLOAD201      0.000   0.000000
       91         6  CLOAD201      0.000   0.000000
       94         6  CLOAD201      0.000   0.000000
       97         6  CLOAD201      0.000   0.000000
      100         6  CLOAD201      0.000   0.000000
      103         6  CLOAD201      0.000   0.000000
      106         6  CLOAD201      0.000   0.000000
      109         6  CLOAD201      0.000   0.000000
      112         6  CLOAD201      0.000   0.000000
      115         6  CLOAD201      0.000   0.000000
      118         6  CLOAD201      0.000   0.000000
      121         6  CLOAD201      0.000   0.000000
      124         6  CLOAD201      0.000   0.000000
      127         6  CLOAD201      0.000   0.000000
      130         6  CLOAD201      0.000   0.000000
      133         6  CLOAD201      0.000   0.000000
      136         6  CLOAD201      0.000   0.000000
      139         6  CLOAD201      0.000   0.000000
      142         6  CLOAD201      0.000   0.000000
 *** LOAD STEP     1   SUBSTEP     1  COMPLETED.    CUM ITER =      1
 *** TIME =   1.00000         TIME INC =   1.00000      NEW TRIANG MATRIX


 *** ANSYS BINARY FILE STATISTICS
  BUFFER SIZE USED= 16384
        0.062 MB WRITTEN ON ELEMENT MATRIX FILE: file0.emat
        0.062 MB WRITTEN ON ELEMENT SAVED DATA FILE: file0.esav
        0.062 MB WRITTEN ON ASSEMBLED MATRIX FILE: file0.full
        0.750 MB WRITTEN ON RESULTS FILE: file0.rst
 *************** Write FE CONNECTORS *********

 WRITE OUT CONSTRAINT EQUATIONS TO FILE= file.ce                                                                                                                                                                                                                                                             
 ****************************************************
 *************** FINISHED SOLVE FOR LS 1 *************

 *GET  _WALLASOL  FROM  ACTI  ITEM=TIME WALL  VALUE=  1.18333333    

 PRINTOUT RESUMED BY /GOP

 FINISH SOLUTION PROCESSING


 ***** ROUTINE COMPLETED *****  CP =         0.969



 *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2019 R3          19.5     ***
 DISTRIBUTED ANSYS Academic Teaching Advanced                  

 00292481  VERSION=WINDOWS x64   01:11:00  APR 30, 2021 CP=      0.969

 my_3d_Bc--Static Structural (A5)                                              



          ***** ANSYS RESULTS INTERPRETATION (POST1) *****

 *** NOTE ***                            CP =       0.969   TIME= 01:11:00
 Reading results into the database (SET command) will update the current 
 displacement and force boundary conditions in the database with the     
 values from the results file for that load set.  Note that any          
 subsequent solutions will use these values unless action is taken to    
 either SAVE the current values or not overwrite them (/EXIT,NOSAVE).    

 Set Encoding of XML File to:ISO-8859-1

 Set Output of XML File to:
     PARM,     ,     ,     ,     ,     ,     ,     ,     ,     ,     ,     ,
         ,     ,     ,     ,     ,     ,     ,

 DATABASE WRITTEN ON FILE  parm.xml                                                                                                                                                                                                                                                            

 EXIT THE ANSYS POST1 DATABASE PROCESSOR


 ***** ROUTINE COMPLETED *****  CP =         0.969



 PRINTOUT RESUMED BY /GOP

 *GET  _WALLDONE  FROM  ACTI  ITEM=TIME WALL  VALUE=  1.18333333    

 PARAMETER _PREPTIME =     0.000000000    

 PARAMETER _SOLVTIME =     0.000000000    

 PARAMETER _POSTTIME =     0.000000000    

 PARAMETER _TOTALTIM =     0.000000000    

 *GET  _DLBRATIO  FROM  ACTI  ITEM=SOLU DLBR  VALUE=  2.00847458    

 *GET  _COMBTIME  FROM  ACTI  ITEM=SOLU COMB  VALUE= 0.515913000E-01
 --- Number of total nodes = 152
 --- Number of total elements = 244
 --- Element load balance ratio = 2.00847458
 --- Time to combine distributed files = 5.15913E-02

 EXIT ANSYS WITHOUT SAVING DATABASE


 NUMBER OF WARNING MESSAGES ENCOUNTERED=          2
 NUMBER OF ERROR   MESSAGES ENCOUNTERED=          0

+--------- D I S T R I B U T E D   A N S Y S   S T A T I S T I C S ------------+

Release: 2019 R3            Build: 19.5       Update: UP20190805   Platform: WINDOWS x64 
Date Run: 04/30/2021   Time: 01:11     Process ID: 10148
Operating System: Windows 10  (Build: 17763)

Processor Model: AMD Ryzen 5 1500X Quad-Core Processor

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         :    8
Number of physical cores available      :    4
Number of processes requested           :    2
Number of threads per process requested :    1
Total number of cores requested         :    2 (Distributed Memory Parallel)               
MPI Type: INTELMPI
MPI Version: Intel(R) MPI Library 2018 Update 3 for Windows* OS


GPU Acceleration: Not Requested

Job Name: file0
Input File: dummy.dat

  Core                Machine Name   Working Directory
 -----------------------------------------------------
     0   FME-V3U0BM8U219.fme.vutbr   C:\Users\201285_Abdul_moghni\Desktop\Train_Faze_4\_ProjectScratch\ScrE68E
     1   FME-V3U0BM8U219.fme.vutbr   C:\Users\201285_Abdul_moghni\Desktop\Train_Faze_4\_ProjectScratch\ScrE68E
 
Latency time from master to core     1 =    0.817 microseconds
 
Communication speed from master to core     1 =  4753.39 MB/sec

Total CPU time for main thread                    :        1.0 seconds
Total CPU time summed for all threads             :        1.2 seconds

Elapsed time spent pre-processing model (/PREP7)  :        0.2 seconds
Elapsed time spent solution - preprocessing       :        0.0 seconds
Elapsed time spent computing solution             :        0.1 seconds
Elapsed time spent solution - postprocessing      :        0.1 seconds
Elapsed time spent post-processing model (/POST1) :        0.0 seconds
 
Equation solver used                              :            Sparse (symmetric)

Maximum total memory used                         :       86.0 MB
Maximum total memory allocated                    :     3136.0 MB
Total physical memory available                   :         16 GB

Total amount of I/O written to disk               :        0.0 GB
Total amount of I/O read from disk                :        0.0 GB

+------ E N D   D I S T R I B U T E D   A N S Y S   S T A T I S T I C S -------+


 *---------------------------------------------------------------------------*
 |                                                                           |
 |                       DISTRIBUTED ANSYS RUN COMPLETED                     |
 |                                                                           |
 |---------------------------------------------------------------------------|
 |                                                                           |
 | Ansys 2019 R3               Build 19.5         UP20190805     WINDOWS x64 |
 |                                                                           |
 |---------------------------------------------------------------------------|
 |                                                                           |
 | Database Requested(-db)  1024 MB    Scratch Memory Requested      1024 MB |
 | Maximum Database Used       1 MB    Maximum Scratch Memory Used     42 MB |
 |                                                                           |
 |---------------------------------------------------------------------------|
 |                                                                           |
 |        CP Time      (sec) =          1.250       Time  =  01:11:01        |
 |        Elapsed Time (sec) =          3.000       Date  =  04/30/2021      |
 |                                                                           |
 *---------------------------------------------------------------------------*
