Sfran
Subscriber

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.