I saved the project per above. Below is what the "file.err" file had and last part of the "solve.out" file. I didn't see any errors in either file so not sure where to go from here.
Contents of "file.err".
/COM,ANSYS RELEASE 2022 R2 BUILD 22.2 UP20220516 13:23:33
*** WARNING *** CP = 3.094 TIME= 13:23:37
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** WARNING *** CP = 3.453 TIME= 13:23:37
Material number 2 (used by element 2583) should normally have at least
one MP or one TB type command associated with it. Output of energy by
material may not be available.
Partial contents of "solve.out"
***** MAPDL SOLVE COMMAND *****
*** WARNING *** CP = 3.094 TIME= 13:23:37
Element shape checking is currently inactive. Issue SHPP,ON or
SHPP,WARN to reactivate, if desired.
*** NOTE *** CP = 3.297 TIME= 13:23:37
The model data was checked and warning messages were found.
Please review output or errors file (
C:\Users\lastname\AppData\Local\Temp\WB_lastname_9764_2\_ProjectScratch\S
Scr7CDD\file.err ) for these warning messages.
*** SELECTION OF ELEMENT TECHNOLOGIES FOR APPLICABLE ELEMENTS ***
--- GIVE SUGGESTIONS AND RESET THE KEY OPTIONS ---
ELEMENT TYPE 1 IS SOLID187. IT IS NOT ASSOCIATED WITH FULLY INCOMPRESSIBLE
HYPERELASTIC MATERIALS. NO SUGGESTION IS AVAILABLE AND NO RESETTING IS NEEDED.
*** MAPDL - ENGINEERING ANALYSIS SYSTEM RELEASE 2022 R2 22.2 ***
Ansys Mechanical Enterprise Academic Student
00000000 VERSION=WINDOWS x64 13:23:37 JAN 02, 2023 CP= 3.359
wbnew--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 . . . . . 459.67
EQUATION SOLVER OPTION. . . . . . . . . . . . .SPARSE
GLOBALLY ASSEMBLED MATRIX . . . . . . . . . . .SYMMETRIC
*** WARNING *** CP = 3.453 TIME= 13:23:37
Material number 2 (used by element 2583) 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 = 3.516 TIME= 13:23:37
The step data was checked and warning messages were found.
Please review output or errors file (
C:\Users\lastname\AppData\Local\Temp\WB_lastname_9764_2\_ProjectScratch\S
Scr7CDD\file.err ) for these warning messages.
*** NOTE *** CP = 3.562 TIME= 13:23:37
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
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
SOLUTION MONITORING INFO IS WRITTEN TO FILE= file.mntr
*********** PRECISE MASS SUMMARY ***********
TOTAL RIGID BODY MASS MATRIX ABOUT ORIGIN
Translational mass | Coupled translational/rotational mass
0.55957E-04 0.0000 0.0000 | 0.0000 0.61305E-09 -0.27292E-04
0.0000 0.55957E-04 0.0000 | -0.61305E-09 0.0000 -0.46874E-08
0.0000 0.0000 0.55957E-04 | 0.27292E-04 0.46874E-08 0.0000
------------------------------------------ | ------------------------------------------
| Rotational mass (inertia)
| 0.16809E-04 0.26878E-08 -0.60965E-10
| 0.26878E-08 0.15910E-05 -0.61394E-09
| -0.60965E-10 -0.61394E-09 0.16810E-04
TOTAL MASS = 0.55957E-04
The mass principal axes coincide with the global Cartesian axes
CENTER OF MASS (X,Y,Z)= -0.83769E-04 0.48773 0.10956E-04
TOTAL INERTIA ABOUT CENTER OF MASS
0.34980E-05 0.40158E-09 -0.61016E-10
0.40158E-09 0.15910E-05 -0.31494E-09
-0.61016E-10 -0.31494E-09 0.34985E-05
The inertia principal axes coincide with the global Cartesian axes
*** MASS SUMMARY BY ELEMENT TYPE ***
TYPE MASS
1 0.559568E-04
Range of element maximum matrix coefficients in global coordinates
Maximum = 15489976.9 at element 1201.
Minimum = 506190.43 at element 674.
*** ELEMENT MATRIX FORMULATION TIMES
TYPE NUMBER ENAME TOTAL CP AVE CP
1 1654 SOLID187 1.875 0.001134
2 52 SURF154 0.000 0.000000
Time at end of element matrix formulation CP = 4.828125.
SPARSE MATRIX DIRECT SOLVER.
Number of equations = 9030, Maximum wavefront = 288
Memory allocated for solver = 26.376 MB
Memory required for in-core solution = 25.390 MB
Memory required for out-of-core solution = 12.757 MB
*** NOTE *** CP = 5.719 TIME= 13:23:39
The 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.