
 ANSYS Academic Teaching Introductory              


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 *            ANSYS 2020 R2          LEGAL NOTICES             *
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 2020 R2 
     
 Point Releases and Patches installed:   
     
 Academic Student 2020 R2
 Aqwa 2020 R2
 EnSight 2020 R2 
 FENSAP-ICE 2020 R2  


          *****  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\Abdulrahman Moghni\Desktop\varianta_urcita_soustava\Ansys_Train_faze_2_s=0\Ansys- version_2\_ProjectScratch\ScrF8F6\dummy.dat
  OUTPUT FILE NAME             = C:\Users\Abdulrahman Moghni\Desktop\varianta_urcita_soustava\Ansys_Train_faze_2_s=0\Ansys- version_2\_ProjectScratch\ScrF8F6\solve.out
  START-UP FILE MODE           = NOREAD
  STOP FILE MODE               = NOREAD

 RELEASE= 2020 R2              BUILD= 20.2      UP20200601   VERSION=WINDOWS x64 
 CURRENT JOBNAME=file0  12:52:07  APR 01, 2021 CP=      0.266


 PARAMETER _DS_PROGRESS =     999.0000000    

 /INPUT FILE= ds.dat  LINE=       0



 *** NOTE ***                            CP =       0.359   TIME= 12:52:07
 The /CONFIG,NOELDB command is not valid in a Distributed ANSYS          
 solution.  Command is ignored.                                          

 *GET  _WALLSTRT  FROM  ACTI  ITEM=TIME WALL  VALUE=  12.8686111    

 TITLE= 
 Ansys- version_2--Static Structural (B5)                                      


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

 PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:\Users\Abdulrahman Moghni\Desktop\varianta_urcita_soustava\Ansys_Train_faze_2_s=0\Ansys- version_2\_ProjectScratch\ScrF8F6\

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

 PARAMETER _WB_SOLVERFILES_DIR(1) = C:\Users\Abdulrahman Moghni\Desktop\varianta_urcita_soustava\Ansys_Train_faze_2_s=0\Ansys- version_2\Ansys- version_2_files\dp0\SYS-5\MECH\

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

 PARAMETER _WB_USERFILES_DIR(1) = C:\Users\Abdulrahman Moghni\Desktop\varianta_urcita_soustava\Ansys_Train_faze_2_s=0\Ansys- version_2\Ansys- version_2_files\user_files\
 --- Data in consistent NMM units. See Solving Units in the help system for more

 MPA UNITS SPECIFIED FOR INTERNAL    
  LENGTH      = MILLIMETERS (mm)
  MASS        = TONNE (Mg)
  TIME        = SECONDS (sec)
  TEMPERATURE = CELSIUS (C)
  TOFFSET     = 273.0
  FORCE       = NEWTON (N)
  HEAT        = MILLIJOULES (mJ)

 INPUT  UNITS ARE ALSO SET TO MPA 

 *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2020 R2          20.2     ***
 DISTRIBUTED ANSYS Academic Teaching Introductory              

 01055371  VERSION=WINDOWS x64   12:52:07  APR 01, 2021 CP=      0.359

 Ansys- version_2--Static Structural (B5)                                      



          ***** 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" ***********
 *********** Send User Defined Coordinate System(s) ***********
 *********** Set Reference Temperature ***********
 *********** Send Materials ***********
 *********** Send Beam Properties ***********
 ******* Constant Zero Displacement Z *******
 *********** 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 ***********
 *********** 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 2" ***********
 *********** Construct Remote Displacement ***********
 *********** Construct Remote Displacement ***********
 *** Create a component for all remote displacements ***


 ***** ROUTINE COMPLETED *****  CP =         0.391


 --- Number of total nodes = 65
 --- Number of contact elements = 0
 --- Number of spring elements = 0
 --- Number of bearing elements = 0
 --- Number of solid elements = 41
 --- Number of condensed parts = 0
 --- Number of total elements = 132

 *GET  _WALLBSOL  FROM  ACTI  ITEM=TIME WALL  VALUE=  12.8686111    
 ****************************************************************************
 *************************    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        29 TO         29 STEP          1

          1  ELEMENTS (OF        132  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        30 TO         30 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -9097.9        -9097.9        -9097.9        -9097.9    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        31 TO         31 STEP          1

          1  ELEMENTS (OF        132  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        32 TO         32 STEP          1

          1  ELEMENTS (OF        132  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        33 TO         33 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12223.        -12223.        -12223.        -12223.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        34 TO         34 STEP          1

          1  ELEMENTS (OF        132  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        35 TO         35 STEP          1

          1  ELEMENTS (OF        132  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        36 TO         36 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12226.        -12226.        -12226.        -12226.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        37 TO         37 STEP          1

          1  ELEMENTS (OF        132  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        38 TO         38 STEP          1

          1  ELEMENTS (OF        132  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        39 TO         39 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12320.        -12320.        -12320.        -12320.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        40 TO         40 STEP          1

          1  ELEMENTS (OF        132  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        41 TO         41 STEP          1

          1  ELEMENTS (OF        132  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        42 TO         42 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -11950.        -11950.        -11950.        -11950.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        43 TO         43 STEP          1

          1  ELEMENTS (OF        132  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        44 TO         44 STEP          1

          1  ELEMENTS (OF        132  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        45 TO         45 STEP          1

          1  ELEMENTS (OF        132  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        46 TO         46 STEP          1

          1  ELEMENTS (OF        132  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        47 TO         47 STEP          1

          1  ELEMENTS (OF        132  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        48 TO         48 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -9097.9        -9097.9        -9097.9        -9097.9    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        49 TO         49 STEP          1

          1  ELEMENTS (OF        132  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        50 TO         50 STEP          1

          1  ELEMENTS (OF        132  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        51 TO         51 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12223.        -12223.        -12223.        -12223.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        52 TO         52 STEP          1

          1  ELEMENTS (OF        132  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        53 TO         53 STEP          1

          1  ELEMENTS (OF        132  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        54 TO         54 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12226.        -12226.        -12226.        -12226.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        55 TO         55 STEP          1

          1  ELEMENTS (OF        132  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        56 TO         56 STEP          1

          1  ELEMENTS (OF        132  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        57 TO         57 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12320.        -12320.        -12320.        -12320.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        58 TO         58 STEP          1

          1  ELEMENTS (OF        132  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        59 TO         59 STEP          1

          1  ELEMENTS (OF        132  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        60 TO         60 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -11950.        -11950.        -11950.        -11950.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        61 TO         61 STEP          1

          1  ELEMENTS (OF        132  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        62 TO         62 STEP          1

          1  ELEMENTS (OF        132  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        63 TO         63 STEP          1

          1  ELEMENTS (OF        132  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        64 TO         64 STEP          1

          1  ELEMENTS (OF        132  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        65 TO         65 STEP          1

          1  ELEMENTS (OF        132  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        66 TO         66 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -11197.        -11197.        -11197.        -11197.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        67 TO         67 STEP          1

          1  ELEMENTS (OF        132  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        68 TO         68 STEP          1

          1  ELEMENTS (OF        132  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        69 TO         69 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -11835.        -11835.        -11835.        -11835.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        70 TO         70 STEP          1

          1  ELEMENTS (OF        132  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        71 TO         71 STEP          1

          1  ELEMENTS (OF        132  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        72 TO         72 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12729.        -12729.        -12729.        -12729.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        73 TO         73 STEP          1

          1  ELEMENTS (OF        132  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        74 TO         74 STEP          1

          1  ELEMENTS (OF        132  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        75 TO         75 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -13207.        -13207.        -13207.        -13207.    

 SELECT       FOR ITEM=REAL COMPONENT=    
  IN RANGE        76 TO         76 STEP          1

          1  ELEMENTS (OF        132  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        77 TO         77 STEP          1

          1  ELEMENTS (OF        132  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        78 TO         78 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -11833.        -11833.        -11833.        -11833.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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        81 TO         81 STEP          1

          1  ELEMENTS (OF        132  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        82 TO         82 STEP          1

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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        84 TO         84 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -11197.        -11197.        -11197.        -11197.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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        87 TO         87 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -11835.        -11835.        -11835.        -11835.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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        90 TO         90 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12729.        -12729.        -12729.        -12729.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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        93 TO         93 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -13207.        -13207.        -13207.        -13207.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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        96 TO         96 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12383.        -12383.        -12383.        -12383.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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        99 TO         99 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -31749.        -31749.        -31749.        -31749.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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       102 TO        102 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -31749.        -31749.        -31749.        -31749.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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       105 TO        105 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -24765.        -24765.        -24765.        -24765.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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       108 TO        108 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -31749.        -31749.        -31749.        -31749.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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       111 TO        111 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -31749.        -31749.        -31749.        -31749.    

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

          1  ELEMENTS (OF        132  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

          1  ELEMENTS (OF        132  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       114 TO        114 STEP          1

          1  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED SURFACE LOAD PRES FOR ALL SELECTED ELEMENTS  LKEY =  1   KVAL = 1
     VALUES =    -12383.        -12383.        -12383.        -12383.    

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

          1  ELEMENTS (OF        132  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        138 STEP          1

        132  ELEMENTS (OF        132  DEFINED) SELECTED BY  ESEL  COMMAND.

 SPECIFIED CONSTRAINT UX   FOR SELECTED NODES           72 TO          72 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UY   FOR SELECTED NODES           72 TO          72 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UZ   FOR SELECTED NODES           72 TO          72 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES           72 TO          72 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTY FOR SELECTED NODES           72 TO          72 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UY   FOR SELECTED NODES           73 TO          73 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT UZ   FOR SELECTED NODES           73 TO          73 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTX FOR SELECTED NODES           73 TO          73 BY           1
 REAL=  0.00000000       IMAG=  0.00000000    

 SPECIFIED CONSTRAINT ROTY FOR SELECTED NODES           73 TO          73 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 =       0.422   TIME= 12:52:07
 The automatic domain decomposition logic has selected the MESH domain   
 decomposition method with 2 processes per solution.                     

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

 *** WARNING ***                         CP =       0.422   TIME= 12:52:07
 Element shape checking is currently inactive.  Issue SHPP,ON or         
 SHPP,WARN to reactivate, if desired.                                    

 *** NOTE ***                            CP =       0.422   TIME= 12:52:07
 The model data was checked and warning messages were found.             
  Please review output or errors file ( C:\Users\Abdulrahman             
 Moghni\Desktop\varianta_urcita_soustava\Ansys_Train_faze_2_s=0\Ansys-   
 version_2\_ProjectScratch\ScrF8F6\file0.err ) for these warning         
 messages.                                                               

 *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2020 R2          20.2     ***
 DISTRIBUTED ANSYS Academic Teaching Introductory              

 01055371  VERSION=WINDOWS x64   12:52:07  APR 01, 2021 CP=      0.422

 Ansys- version_2--Static Structural (B5)                                      



                       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 =       0.422   TIME= 12:52:07
 Material number 29 (used by element 48) 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 =       0.422   TIME= 12:52:07
 The step data was checked and warning messages were found.              
  Please review output or errors file ( C:\Users\Abdulrahman             
 Moghni\Desktop\varianta_urcita_soustava\Ansys_Train_faze_2_s=0\Ansys-   
 version_2\_ProjectScratch\ScrF8F6\file0.err ) for these warning         
 messages.                                                               

 *** NOTE ***                            CP =       0.422   TIME= 12:52:07
 Internal nodes from 74 to 75 are created.                               
 2 internal nodes are used for handling degrees of freedom on pilot      
 nodes of rigid target surfaces.                                         

 *** NOTE ***                            CP =       0.422   TIME= 12:52:07
 Internal nodes from 74 to 75 are created.                               
 2 internal nodes are used for handling degrees of freedom on pilot      
 nodes of rigid target surfaces.                                         

 *** NOTE ***                            CP =       0.422   TIME= 12:52:07
 Rigid target surface identified by real constant set 116.  The degrees  
 of freedom of the rigid surface are driven by the pilot node 72.        
 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
 *WARNING*: Boundary conditions, coupling, and/or constraint equations   
 have been applied on certain target nodes (for example 14).             
 ****************************************
  

 *** NOTE ***                            CP =       0.422   TIME= 12:52:07
 Rigid target surface identified by real constant set 117.  The degrees  
 of freedom of the rigid surface are driven by the pilot node 73.        
 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
 *WARNING*: Boundary conditions, coupling, and/or constraint equations   
 have been applied on certain target nodes (for example 17).             
 ****************************************
  

 *** WARNING ***                         CP =       0.422   TIME= 12:52:07
 Overconstraint may occur for Lagrange multiplier or MPC based contact   
 algorithm.                                                              
 The reasons for possible overconstraint are:                            

 *** WARNING ***                         CP =       0.438   TIME= 12:52:07
 Boundary conditions, coupling, and/or constraint equations have been    
 applied on certain contact nodes (for example 17).                      
 ****************************************
  
  

 *** NOTE ***                            CP =       0.438   TIME= 12:52:07
 Internal nodes from 74 to 75 are created.                               
 2 internal nodes are used for handling degrees of freedom on pilot      
 nodes of rigid target surfaces.                                         

  
  
     D I S T R I B U T E D   D O M A I N   D E C O M P O S E R
  
  ...Number of elements: 132
  ...Number of nodes:    67
  ...Decompose to 2 CPU domains
  ...Element load balance ratio =     1.969


                      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                                                                                                                                                                                                                                                           


 *** WARNING ***                         CP =       0.453   TIME= 12:52:07
 Multiple constraints have been applied on degree of freedom 3 of        
 contact node 14.  The program will remove certain internal MPCs.        
 Please check the model carefully.                                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 48.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 49.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 50.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 81.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 83.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 114.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 115.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 116.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 82.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 52.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 51.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 53.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 84.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 85.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 86.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 117.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 118.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 119.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 55.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 54.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 56.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 87.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 88.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 89.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 120.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 121.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 122.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 58.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 57.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 59.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 90.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 91.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 92.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 123.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 124.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 125.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 61.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 60.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 62.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 93.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 94.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 95.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 126.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 127.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 128.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 64.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 63.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 65.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 96.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 97.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 98.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 129.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 130.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 131.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 79.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 78.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 80.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 111.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 112.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 113.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 132.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 133.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 134.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 77.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 75.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 76.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 108.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 109.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 110.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 74.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 72.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 73.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 105.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 106.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 107.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 71.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 69.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 70.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 102.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 103.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 104.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 67.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 66.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 68.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 99.                       

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 101.                      

 *** WARNING ***                         CP =       0.484   TIME= 12:52:07
 A boundary condition has been applied on 1 degrees of freedom of the    
 node belonging to the FOLLW201 element number 100.                      


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

   TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
               Translational mass               |   Coupled translational/rotational mass
         22.527        0.0000        0.0000     |     0.0000        0.0000       -47343.    
         0.0000        22.527        0.0000     |     0.0000        0.0000       0.46632E+06
         0.0000        0.0000        22.527     |     47343.      -0.46632E+06    0.0000    
     ------------------------------------------ | ------------------------------------------
                                                |         Rotational mass (inertia)
                                                |    0.17062E+09  -0.97999E+09    0.0000    
                                                |   -0.97999E+09   0.13017E+11    0.0000    
                                                |     0.0000        0.0000       0.13187E+11

   TOTAL MASS =  22.527    
     The mass principal axes coincide with the global Cartesian axes

   CENTER OF MASS (X,Y,Z)=    20700.        2101.6        0.0000    

   TOTAL INERTIA ABOUT CENTER OF MASS
        0.71125E+08  -0.95947E-07    0.0000    
       -0.95947E-07   0.33638E+10    0.0000    
         0.0000        0.0000       0.34350E+10
     The inertia principal axes coincide with the global Cartesian axes


  *** MASS SUMMARY BY ELEMENT TYPE ***

  TYPE      MASS
     1   1.42996    
     2   1.42996    
     3  0.844974    
     4  0.844974    
     5   3.76988    
     6   1.37276    
     7   1.37276    
     8   4.43026    
     9  0.370559    
    10  0.370559    
    11  0.325369    
    12  0.325369    
    13  0.325369    
    14  0.325369    
    15  0.280179    
    16  0.280179    
    17  0.560357    
    18  0.577760    
    19  0.577760    
    20  0.301440    
    21  0.301440    
    22  0.301440    
    23  0.301440    
    24  0.301440    
    25  0.301440    
    26  0.301440    
    27  0.301440    
    28  0.301440    

 Range of element maximum matrix coefficients in global coordinates
 Maximum = 1471014.49 at element 10.                                     
 Minimum = 116974.386 at element 39.                                     

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

        1         2  LINK180       0.000   0.000000
        2         2  LINK180       0.000   0.000000
        3         1  LINK180       0.000   0.000000
        4         1  LINK180       0.000   0.000000
        5         4  LINK180       0.000   0.000000
        6         2  LINK180       0.000   0.000000
        7         2  LINK180       0.000   0.000000
        8         6  LINK180       0.000   0.000000
        9         1  LINK180       0.000   0.000000
       10         1  LINK180       0.000   0.000000
       11         1  LINK180       0.000   0.000000
       12         1  LINK180       0.000   0.000000
       13         1  LINK180       0.000   0.000000
       14         1  LINK180       0.000   0.000000
       15         1  LINK180       0.000   0.000000
       16         1  LINK180       0.000   0.000000
       17         2  LINK180       0.000   0.000000
       18         1  LINK180       0.000   0.000000
       19         1  LINK180       0.000   0.000000
       20         1  LINK180       0.000   0.000000
       21         1  LINK180       0.000   0.000000
       22         1  LINK180       0.000   0.000000
       23         1  LINK180       0.000   0.000000
       24         1  LINK180       0.000   0.000000
       25         1  LINK180       0.000   0.000000
       26         1  LINK180       0.000   0.000000
       27         1  LINK180       0.000   0.000000
       28         1  LINK180       0.000   0.000000
       29         3  CLOAD201      0.000   0.000000
       32         3  CLOAD201      0.000   0.000000
       35         3  CLOAD201      0.000   0.000000
       38         3  CLOAD201      0.000   0.000000
       41         3  CLOAD201      0.000   0.000000
       44         3  CLOAD201      0.000   0.000000
       47         3  CLOAD201      0.000   0.000000
       50         3  CLOAD201      0.000   0.000000
       53         3  CLOAD201      0.000   0.000000
       56         3  CLOAD201      0.000   0.000000
       59         3  CLOAD201      0.000   0.000000
       62         3  CLOAD201      0.000   0.000000
       65         3  CLOAD201      0.000   0.000000
       68         3  CLOAD201      0.000   0.000000
       71         3  CLOAD201      0.000   0.000000
       74         3  CLOAD201      0.000   0.000000
       77         3  CLOAD201      0.000   0.000000
       80         3  CLOAD201      0.000   0.000000
       83         3  CLOAD201      0.000   0.000000
       86         3  CLOAD201      0.000   0.000000
       89         3  CLOAD201      0.000   0.000000
       92         3  CLOAD201      0.000   0.000000
       95         3  CLOAD201      0.000   0.000000
       98         3  CLOAD201      0.000   0.000000
      101         3  CLOAD201      0.000   0.000000
      104         3  CLOAD201      0.000   0.000000
      107         3  CLOAD201      0.000   0.000000
      110         3  CLOAD201      0.000   0.000000
      113         3  CLOAD201      0.000   0.000000
      116         2  TARGE170      0.000   0.000000
      117         2  TARGE170      0.000   0.000000
 Time at end of element matrix formulation CP = 0.515625.                

 DISTRIBUTED SPARSE MATRIX DIRECT SOLVER.
  Number of equations =          41,    Maximum wavefront =      6

  Local memory allocated for solver              =      0.184 MB
  Local memory required for in-core solution     =      0.176 MB
  Local memory required for out-of-core solution =      0.176 MB

  Total memory allocated for solver              =      0.372 MB
  Total memory required for in-core solution     =      0.355 MB
  Total memory required for out-of-core solution =      0.355 MB

 *** NOTE ***                            CP =       0.531   TIME= 12:52:07
 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.                                                                   
 Distributed sparse solver maximum pivot= 3059003.37 at node 9 UX.       
 Distributed sparse solver minimum pivot= 16679.7614 at node 20 UY.      
 Distributed sparse solver minimum pivot in absolute value= 16679.7614   
 at node 20 UY.                                                          

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

        1         2  LINK180       0.000   0.000000
        2         2  LINK180       0.000   0.000000
        3         1  LINK180       0.000   0.000000
        4         1  LINK180       0.000   0.000000
        5         4  LINK180       0.000   0.000000
        6         2  LINK180       0.000   0.000000
        7         2  LINK180       0.000   0.000000
        8         6  LINK180       0.000   0.000000
        9         1  LINK180       0.000   0.000000
       10         1  LINK180       0.000   0.000000
       11         1  LINK180       0.000   0.000000
       12         1  LINK180       0.000   0.000000
       13         1  LINK180       0.000   0.000000
       14         1  LINK180       0.000   0.000000
       15         1  LINK180       0.000   0.000000
       16         1  LINK180       0.000   0.000000
       17         2  LINK180       0.000   0.000000
       18         1  LINK180       0.031   0.031250
       19         1  LINK180       0.000   0.000000
       20         1  LINK180       0.000   0.000000
       21         1  LINK180       0.000   0.000000
       22         1  LINK180       0.000   0.000000
       23         1  LINK180       0.000   0.000000
       24         1  LINK180       0.000   0.000000
       25         1  LINK180       0.000   0.000000
       26         1  LINK180       0.000   0.000000
       27         1  LINK180       0.000   0.000000
       28         1  LINK180       0.000   0.000000
       29         3  CLOAD201      0.000   0.000000
       32         3  CLOAD201      0.000   0.000000
       35         3  CLOAD201      0.000   0.000000
       38         3  CLOAD201      0.000   0.000000
       41         3  CLOAD201      0.000   0.000000
       44         3  CLOAD201      0.000   0.000000
       47         3  CLOAD201      0.000   0.000000
       50         3  CLOAD201      0.000   0.000000
       53         3  CLOAD201      0.000   0.000000
       56         3  CLOAD201      0.000   0.000000
       59         3  CLOAD201      0.000   0.000000
       62         3  CLOAD201      0.000   0.000000
       65         3  CLOAD201      0.000   0.000000
       68         3  CLOAD201      0.000   0.000000
       71         3  CLOAD201      0.000   0.000000
       74         3  CLOAD201      0.000   0.000000
       77         3  CLOAD201      0.000   0.000000
       80         3  CLOAD201      0.000   0.000000
       83         3  CLOAD201      0.000   0.000000
       86         3  CLOAD201      0.000   0.000000
       89         3  CLOAD201      0.000   0.000000
       92         3  CLOAD201      0.000   0.000000
       95         3  CLOAD201      0.000   0.000000
       98         3  CLOAD201      0.000   0.000000
      101         3  CLOAD201      0.000   0.000000
      104         3  CLOAD201      0.000   0.000000
      107         3  CLOAD201      0.000   0.000000
      110         3  CLOAD201      0.000   0.000000
      113         3  CLOAD201      0.000   0.000000

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

        1         2  LINK180       0.000   0.000000
        2         2  LINK180       0.000   0.000000
        3         1  LINK180       0.000   0.000000
        4         1  LINK180       0.000   0.000000
        5         4  LINK180       0.000   0.000000
        6         2  LINK180       0.000   0.000000
        7         2  LINK180       0.000   0.000000
        8         6  LINK180       0.000   0.000000
        9         1  LINK180       0.000   0.000000
       10         1  LINK180       0.000   0.000000
       11         1  LINK180       0.000   0.000000
       12         1  LINK180       0.000   0.000000
       13         1  LINK180       0.000   0.000000
       14         1  LINK180       0.000   0.000000
       15         1  LINK180       0.000   0.000000
       16         1  LINK180       0.000   0.000000
       17         2  LINK180       0.000   0.000000
       18         1  LINK180       0.000   0.000000
       19         1  LINK180       0.000   0.000000
       20         1  LINK180       0.000   0.000000
       21         1  LINK180       0.000   0.000000
       22         1  LINK180       0.000   0.000000
       23         1  LINK180       0.000   0.000000
       24         1  LINK180       0.000   0.000000
       25         1  LINK180       0.000   0.000000
       26         1  LINK180       0.000   0.000000
       27         1  LINK180       0.000   0.000000
       28         1  LINK180       0.000   0.000000
       29         3  CLOAD201      0.000   0.000000
       32         3  CLOAD201      0.000   0.000000
       35         3  CLOAD201      0.000   0.000000
       38         3  CLOAD201      0.000   0.000000
       41         3  CLOAD201      0.000   0.000000
       44         3  CLOAD201      0.000   0.000000
       47         3  CLOAD201      0.000   0.000000
       50         3  CLOAD201      0.000   0.000000
       53         3  CLOAD201      0.000   0.000000
       56         3  CLOAD201      0.000   0.000000
       59         3  CLOAD201      0.000   0.000000
       62         3  CLOAD201      0.000   0.000000
       65         3  CLOAD201      0.000   0.000000
       68         3  CLOAD201      0.000   0.000000
       71         3  CLOAD201      0.000   0.000000
       74         3  CLOAD201      0.000   0.000000
       77         3  CLOAD201      0.000   0.000000
       80         3  CLOAD201      0.000   0.000000
       83         3  CLOAD201      0.000   0.000000
       86         3  CLOAD201      0.000   0.000000
       89         3  CLOAD201      0.000   0.000000
       92         3  CLOAD201      0.000   0.000000
       95         3  CLOAD201      0.000   0.000000
       98         3  CLOAD201      0.000   0.000000
      101         3  CLOAD201      0.000   0.000000
      104         3  CLOAD201      0.000   0.000000
      107         3  CLOAD201      0.000   0.000000
      110         3  CLOAD201      0.000   0.000000
      113         3  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
        0.375 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=  12.8686111    

 PRINTOUT RESUMED BY /GOP

 FINISH SOLUTION PROCESSING


 ***** ROUTINE COMPLETED *****  CP =         0.609



 *** ANSYS - ENGINEERING ANALYSIS SYSTEM  RELEASE 2020 R2          20.2     ***
 DISTRIBUTED ANSYS Academic Teaching Introductory              

 01055371  VERSION=WINDOWS x64   12:52:07  APR 01, 2021 CP=      0.641

 Ansys- version_2--Static Structural (B5)                                      



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

 *** NOTE ***                            CP =       0.641   TIME= 12:52:07
 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 =         0.641



 PRINTOUT RESUMED BY /GOP

 *GET  _WALLDONE  FROM  ACTI  ITEM=TIME WALL  VALUE=  12.8686111    

 PARAMETER _PREPTIME =     0.000000000    

 PARAMETER _SOLVTIME =     0.000000000    

 PARAMETER _POSTTIME =     0.000000000    

 PARAMETER _TOTALTIM =     0.000000000    

 *GET  _DLBRATIO  FROM  ACTI  ITEM=SOLU DLBR  VALUE=  1.96875000    

 *GET  _COMBTIME  FROM  ACTI  ITEM=SOLU COMB  VALUE= 0.822620000E-02
 --- Total number of nodes = 65
 --- Total number of elements = 132
 --- Element load balance ratio = 1.96875
 --- Time to combine distributed files = 8.2262E-03

 EXIT ANSYS WITHOUT SAVING DATABASE


 NUMBER OF WARNING MESSAGES ENCOUNTERED=         92
 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: 2020 R2            Build: 20.2       Update: UP20200601   Platform: WINDOWS x64 
Date Run: 04/01/2021   Time: 12:52     Process ID: 48892
Operating System: Windows 10  (Build: 19042)

Processor Model: Intel(R) Core(TM) i5-7300HQ CPU @ 2.50GHz

Compiler: Intel(R) FORTRAN Compiler Version 19.0.0  (Build: 20190206)
          Intel(R) C/C++ Compiler Version 19.0.0  (Build: 20190206)
          Intel(R) Math Kernel Library Version 2020.0.0 Product Build 20191125

Number of machines requested            :    1
Total number of cores available         :    4
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             DESKTOP-B14K7L0   C:\Users\Abdulrahman Moghni\Desktop\varianta_urcita_soustava\Ansys_Train_faze_2_s=0\Ansys- version_2\_ProjectScratch\ScrF8F6
     1             DESKTOP-B14K7L0   C:\Users\Abdulrahman Moghni\Desktop\varianta_urcita_soustava\Ansys_Train_faze_2_s=0\Ansys- version_2\_ProjectScratch\ScrF8F6
 
Latency time from master to core     1 =    1.970 microseconds
 
Communication speed from master to core     1 =  4700.74 MB/sec

Total CPU time for main thread                    :        0.6 seconds
Total CPU time summed for all threads             :        0.7 seconds

Elapsed time spent obtaining a license            :        0.9 seconds
Elapsed time spent pre-processing model (/PREP7)  :        0.0 seconds
Elapsed time spent solution - preprocessing       :        0.0 seconds
Elapsed time spent computing solution             :        0.1 seconds
Elapsed time spent solution - postprocessing      :        0.0 seconds
Elapsed time spent post-processing model (/POST1) :        0.0 seconds
 
Equation solver used                              :            Sparse (symmetric)

Maximum total memory used                         :       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 2020 R2               Build 20.2         UP20200601     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) =          0.672       Time  =  12:52:08        |
 |        Elapsed Time (sec) =          3.000       Date  =  04/01/2021      |
 |                                                                           |
 *---------------------------------------------------------------------------*
