The output message is shown here.
=================output message============================================
RELEASE= Release 18.0 BUILD= 18.0 UP20161219 VERSION=WINDOWS x64
CURRENT JOBNAME=file 13
3:55 JUN 27, 2019 CP= 0.125
PARAMETER _DS_PROGRESS = 999.0000000
/INPUT FILE= ds.dat LINE= 0
DO NOT WRITE ELEMENT RESULTS INTO DATABASE
*GET _WALLSTRT FROM ACTI ITEM=TIME WALL VALUE= 13.5652778
TITLE=
test1--Static Structural (F5)
SET PARAMETER DIMENSIONS ON _WB_PROJECTSCRATCH_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_PROJECTSCRATCH_DIR(1) = C:Users1155049058Desktopmiddle testAnsys FEA_ProjectScratchScr2180
SET PARAMETER DIMENSIONS ON _WB_SOLVERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_SOLVERFILES_DIR(1) = C:Users1155049058Desktopmiddle testAnsys FEAtest1_filesdp0SYS-5MECH
SET PARAMETER DIMENSIONS ON _WB_USERFILES_DIR
TYPE=STRI DIMENSIONS= 248 1 1
PARAMETER _WB_USERFILES_DIR(1) = C:Users1155049058Desktopmiddle testAnsys FEAtest1_filesuser_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 Release 18.0 18.0 ***
ANSYS Multiphysics
00000000 VERSION=WINDOWS x64 133:55 JUN 27, 2019 CP= 0.203
test1--Static Structural (F5)
***** ANSYS ANALYSIS DEFINITION (PREP7) *****
*********** Nodes for the whole assembly ***********
*********** Elements for Body 1 "fiber_Line Body" ***********
*********** Elements for Body 2 "mid" ***********
*********** Elements for Body 3 "top" ***********
*********** Elements for Body 4 "btm" ***********
*********** Elements for Body 5 "spring_line" ***********
*********** Send User Defined Coordinate System(s) ***********
*********** Set Reference Temperature ***********
*********** Send Materials ***********
*********** Send Beam Properties ***********
*********** Create Contact "Contact Region" ***********
Real Constant Set For Above Contact Is 7 & 6
*********** Create Contact "Contact Region 2" ***********
Real Constant Set For Above Contact Is 9 & 8
*********** Create Contact "Bonded - fiber_Line Body To mid" ***********
Real Constant Set For Above Contact Is 11 & 10
*********** Create Contact "Bonded - spring_line To mid" ***********
Real Constant Set For Above Contact Is 13 & 12
*********** Create Contact "Bonded - spring_line To btm" ***********
Real Constant Set For Above Contact Is 15 & 14
*********** Create Contact "Bonded - spring_line To top" ***********
Real Constant Set For Above Contact Is 17 & 16
*********** Create Contact "Contact Region" ***********
Real Constant Set For Above Contact Is 19 & 18
*********** Create Contact "Contact Region 2" ***********
Real Constant Set For Above Contact Is 21 & 20
*********** Fixed Supports ***********
*********** Define Pressure Using Surface Effect Elements ***********
LIST DATA TABLE HYPE FOR MATERIAL 5
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE Release 18.0 18.0 ***
ANSYS Multiphysics
00000000 VERSION=WINDOWS x64 133:55 JUN 27, 2019 CP= 0.469
test1--Static Structural (F5)
HYPER EL (HYPE) Table For Material 5
Hyperelastic mat. Option - NEO-HOOKEAN
1
Temps 0.0000000e+000
mu 2.4000000e-001
d 0.0000000e+000
***** ROUTINE COMPLETED ***** CP = 0.469
--- Number of total nodes = 38522
--- Number of contact elements = 7770
--- Number of spring elements = 0
--- Number of bearing elements = 0
--- Number of solid elements = 6906
--- Number of total elements = 16891
*GET _WALLBSOL FROM ACTI ITEM=TIME WALL VALUE= 13.5652778
****************************************************************************
************************* SOLUTION ********************************
****************************************************************************
***** ANSYS SOLUTION ROUTINE *****
PERFORM A STATIC ANALYSIS
THIS WILL BE A NEW ANALYSIS
LARGE DEFORMATION ANALYSIS
USE SPARSE MATRIX DIRECT SOLVER
CONTACT INFORMATION PRINTOUT LEVEL 1
NLDIAG: Nonlinear diagnostics CONT option is set to ON.
Writing frequency : each ITERATION.
DEFINE RESTART CONTROL FOR LOADSTEP LAST
AT FREQUENCY OF LAST AND NUMBER FOR OVERWRITE IS 0
DELETE RESTART FILES OF ENDSTEP
****************************************************
******************* SOLVE FOR LS 1 OF 1 ****************
SELECT FOR ITEM=TYPE COMPONENT=
IN RANGE 22 TO 22 STEP 1
1832 ELEMENTS (OF 16891 DEFINED) SELECTED BY ESEL COMMAND.
SELECT ALL NODES HAVING ANY ELEMENT IN ELEMENT SET.
5622 NODES (OF 38522 DEFINED) SELECTED FROM
1832 SELECTED ELEMENTS BY NSLE COMMAND.
GENERATE SURFACE LOAD PRES ON SURFACE DEFINED BY ALL SELECTED NODES
SET ACCORDING TO TABLE PARAMETER = _LOADVARI61
NUMBER OF PRES ELEMENT FACE LOADS STORED = 1832
ALL SELECT FOR ITEM=NODE COMPONENT=
IN RANGE 1 TO 38522 STEP 1
38522 NODES (OF 38522 DEFINED) SELECTED BY NSEL COMMAND.
ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 16891 STEP 1
16891 ELEMENTS (OF 16891 DEFINED) SELECTED BY ESEL COMMAND.
ALL SELECT FOR ITEM=ELEM COMPONENT=
IN RANGE 1 TO 16891 STEP 1
16891 ELEMENTS (OF 16891 DEFINED) SELECTED BY ESEL COMMAND.
PRINTOUT RESUMED BY /GOP
USE AUTOMATIC TIME STEPPING THIS LOAD STEP
USE 5 SUBSTEPS INITIALLY THIS LOAD STEP FOR ALL DEGREES OF FREEDOM
FOR AUTOMATIC TIME STEPPING:
USE 1000 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 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
PRINTOUT RESUMED BY /GOP
WRITE MISC ITEMS TO THE DATABASE WITH A FREQUENCY OF ALL
FOR THE ENTITIES DEFINED BY COMPONENT _ELMISC
NONLINEAR STABILIZATION CONTROL:
KEY=OFF
NLDIAG: Nonlinear diagnostics NRRE option is set to ON.
The number of files/iterations to be saved for NRRE nonlinear diagnostics has been set to 4
*GET ANSINTER_ FROM ACTI ITEM=INT VALUE= 0.00000000
*IF ANSINTER_ ( = 0.00000 
NE
0 ( = 0.00000 THEN
*ENDIF
***** ANSYS SOLVE COMMAND *****
*** WARNING *** CP = 0.500 TIME= 133:55
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** NOTE *** CP = 0.516 TIME= 133:55
The model data was checked and warning messages were found.
Please review output or errors file (
C:Users1155049058Desktopmiddle testAnsys
FEA_ProjectScratchScr2180file.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(3) IS ALREADY SET AS SUGGESTED AND NO
RESETTING IS NEEDED.
ELEMENT TYPE 1 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
RESETTING IS NEEDED.
ELEMENT TYPE 2 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED. SINCE IT IS
ASSOCIATED WITH FULLY INCOMPRESSIBLE HYPERELASTIC MATERIALS, KEYOPT(6)=1
MUST BE USED. THEY HAVE BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 1 0 0 0 0 0 0
ELEMENT TYPE 3 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0
ELEMENT TYPE 4 IS SOLID186. KEYOPT(2)=0 IS SUGGESTED AND HAS BEEN RESET.
KEYOPT(1-12)= 0 0 0 0 0 0 0 0 0 0 0 0
ELEMENT TYPE 5 IS BEAM188 . KEYOPT(3) IS ALREADY SET AS SUGGESTED AND NO
RESETTING IS NEEDED.
ELEMENT TYPE 5 IS BEAM188 . KEYOPT(15) IS ALREADY SET AS SUGGESTED AND NO
RESETTING IS NEEDED.
*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE Release 18.0 18.0 ***
ANSYS Multiphysics
00000000 VERSION=WINDOWS x64 133:55 JUN 27, 2019 CP= 0.516
test1--Static Structural (F5)
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
NONLINEAR GEOMETRIC EFFECTS . . . . . . . . . .ON
EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE
PLASTIC MATERIAL PROPERTIES INCLUDED. . . . . .YES
NEWTON-RAPHSON OPTION . . . . . . . . . . . . .PROGRAM CHOSEN
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC
*** ERROR *** CP = 0.531 TIME= 133:55
BEAM188 element number 6276 does not support hyperelastic material 5.
*** WARNING *** CP = 0.547 TIME= 133:55
Material number 22 (used by element 15060 ) should normally have at
least one MP or one TB type command associated with it. Output of
energy by material may not be available.
*** ERROR *** CP = 0.562 TIME= 133:55
The step data was checked and there were errors found.
Please check output or errors file (
C:Users1155049058Desktopmiddle testAnsys
FEA_ProjectScratchScr2180file.err ) for messages.
*** NOTE *** CP = 0.562 TIME= 133:55
This nonlinear analysis defaults to using the full Newton-Raphson
solution procedure. This can be modified using the NROPT command.
*** NOTE *** CP = 0.562 TIME= 133:55
The conditions for direct assembly have been met. No .emat or .erot
files will be produced.
NUMBER OF WARNING MESSAGES ENCOUNTERED= 2
NUMBER OF ERROR MESSAGES ENCOUNTERED= 2
***** PROBLEM TERMINATED BY INDICATED ERROR(S) OR BY END OF INPUT DATA *****
+
A N S Y S S T A T I S T I C S
+
Release: Release 18.0 Build: 18.0 Update: UP20161219 Platform: WINDOWS x64
Date Run: 06/27/2019 Time: 133 Process ID: 2700
Operating System: Windows 10 (Build: 17763)
Processor Model: Intel(R) Core(TM) i5-7400 CPU @ 3.00GHz
Compiler: Intel(R) FORTRAN Compiler Version 15.0.7 (Build: 20160518)
Intel(R) C/C++ Compiler Version 15.0.7 (Build: 20160518)
Intel(R) Math Kernel Library Version 11.3.3 Product Build 20160413
Number of machines requested : 1
Total number of cores available : 4
Number of physical cores available : 4
Number of processes requested : 1
Number of threads per process requested : 2
Total number of cores requested : 2 (Shared Memory Parallel)
GPU Acceleration: Not Requested
Job Name: file
Working Directory: C:Users1155049058Desktopmiddle testAnsys FEA_ProjectScratchScr2180
Total CPU time for main thread : 0.6 seconds
Total CPU time summed for all threads : 0.6 seconds
Elapsed time spent pre-processing model (/PREP7) : 0.2 seconds
Elapsed time spent solution - preprocessing : 0.1 seconds
Elapsed time spent computing solution : 0.0 seconds
Elapsed time spent solution - postprocessing : 0.0 seconds
Elapsed time spent post-processing model (/POST1) : 0.0 seconds
Maximum total memory used : 37.0 MB
Maximum total memory allocated : 2112.0 MB
Total physical memory available : 8 GB
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