March 31, 2020 at 7:11 am
santrondela
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*** ANSYS - ENGINEERING ANALYSIS SYSTEM RELEASE Release 16.0 16.0 ***
ANSYS Multiphysics
00000000 VERSION=WINDOWS x64 11:51:56 MAR 31, 2020 CP= 57.922
without wire--Static Structural (A5)
S O L U T I O N O P T I O N S
PROBLEM DIMENSIONALITY. . . . . . . . . . . . .3-D
DEGREES OF FREEDOM. . . . . . UX UY UZ
ANALYSIS TYPE . . . . . . . . . . . . . . . . .STATIC (STEADY-STATE)
OFFSET TEMPERATURE FROM ABSOLUTE ZERO . . . . . 273.15
NONLINEAR GEOMETRIC EFFECTS . . . . . . . . . .ON
EQUATION SOLVER OPTION. . . . . . . . . . . . .PCG
MEMORY SAVING OPTION. . . . . . . . . . . .ON
TOLERANCE. . . . . . . . . . . . . . . . . . 1.00000E-08
PLASTIC MATERIAL PROPERTIES INCLUDED. . . . . .YES
NEWTON-RAPHSON OPTION . . . . . . . . . . . . .PROGRAM CHOSEN
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC
*** WARNING *** CP = 59.734 TIME= 11:51:58
Material number 23 (used by element 682037 ) 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 = 66.375 TIME= 11:52:06
The step data was checked and warning messages were found.
Please review output or errors file ( G:thesis
solidansys26.3.20203.57_ProjectScratchScr20AAfile.err ) for
these warning messages.
*** NOTE *** CP = 66.375 TIME= 11:52:06
This nonlinear analysis defaults to using the full Newton-Raphson
solution procedure. This can be modified using the NROPT command.
*** NOTE *** CP = 66.375 TIME= 11:52:06
The conditions for direct assembly have been met. No .emat or .erot
files will be produced.
L O A D S T E P O P T I O N S
LOAD STEP NUMBER. . . . . . . . . . . . . . . . 1
TIME AT END OF THE LOAD STEP. . . . . . . . . . 1.0000
AUTOMATIC TIME STEPPING . . . . . . . . . . . . ON
INITIAL NUMBER OF SUBSTEPS . . . . . . . . . 5
MAXIMUM NUMBER OF SUBSTEPS . . . . . . . . . 1000
MINIMUM NUMBER OF SUBSTEPS . . . . . . . . . 1
MAXIMUM NUMBER OF EQUILIBRIUM ITERATIONS. . . . 15
STEP CHANGE BOUNDARY CONDITIONS . . . . . . . . NO
STRESS-STIFFENING . . . . . . . . . . . . . . . ON
TERMINATE ANALYSIS IF NOT CONVERGED . . . . . .YES (EXIT)
NODAL DOF SOLUTION LIMIT. . . . . . . . . . . . 0.78886E-30
CONVERGENCE CONTROLS. . . . . . . . . . . . . .USE DEFAULTS
INERTIA LOADS X Y Z
ACEL . . . . . . . . . . . ._ACELX _ACELY _ACELZ
COPY INTEGRATION POINT VALUES TO NODE . . . . .YES, FOR ELEMENTS WITH
ACTIVE MAT. NONLINEARITIES
PRINT OUTPUT CONTROLS . . . . . . . . . . . . .NO PRINTOUT
DATABASE OUTPUT CONTROLS
ITEM FREQUENCY COMPONENT
ALL NONE
NSOL ALL
RSOL ALL
STRS ALL
EPEL ALL
EPPL ALL
AESO ALL
SOLUTION MONITORING INFO IS WRITTEN TO FILE=
file.mntr
*** NOTE *** CP = 742.922 TIME= 12:03:28
It is highly recommended to use the auto contact setting option by
issuing CNCHECK,AUTO command for this problem in order to achieve
better convergence.
*** NOTE *** CP = 742.922 TIME= 12:03:28
Symmetric Deformable- deformable contact pair identified by real
constant set 22 and contact element type 22 has been set up. The
companion pair has real constant set ID 23. Both pairs should have
the same behavior.
ANSYS will deactivate the current pair and keep its companion pair,
resulting in asymmetric contact.
Contact algorithm: Augmented Lagrange method
Contact detection at: Gauss integration point
Contact stiffness factor FKN 10.000
The resulting initial contact stiffness 0.14457E+06
Default penetration tolerance factor FTOLN 0.10000
The resulting penetration tolerance 0.49471
Default opening contact stiffness OPSF will be used.
Default tangent stiffness factor FKT 1.0000
Default elastic slip factor SLTOL 0.50000E-02
The resulting elastic slip 0.45970E-01
Update contact stiffness at each iteration
Default Max. friction stress TAUMAX 0.10000E+21
Average contact surface length 9.1939
Average contact pair depth 4.9471
Default pinball region factor PINB 0.50000
The resulting pinball region 2.4736
Initial penetration/gap is excluded.
Bonded contact (always) is defined.
*** NOTE *** CP = 742.922 TIME= 12:03:28
No contact was detected for this contact pair.