WELCOME TO  MOSES Rev devlop
                         ============================
 
              This Program is licensed for the exclusive use of
 
                               Ultramarine inc.
 
              Copying of this program or use  by  anyone  other
              than  an  employee  of  the  above  firm  without
              written  consent  of  Ultramarine   is   strictly
                                 prohibited.
 
 
 
                               +++ M A I N +++
                               ===============
 
 
>&dimen -dimen feet kips
>&device    -auxin plate1.dat -oecho no
>&set lname = axix bndy bndz
>&set xrefine = 10
>&set yrefine =  5
>inmodel
    Time To perform Inmodel                         : CP=     0.11
>&title Plate Cantelever
>&subtitle x-refine=10 ; y-refine=5
>&apply -load @ 100 -force @ 100
>struct
                +++ S T R U C T U R A L   S O L U T I O N +++
                =============================================
 
 
                   Generating Loads on MODEL at Time 0.000
                   =======================================
                              Total Global Force
          1000.00      0.00      0.00         0         0         0
    Time To Generate Load Cases                     : CP=     0.02
                   Generating Loads on MODEL at Time 0.000
                   =======================================
                              Total Global Force
            0.00    100.00      0.00         0         0      1000
    Time To Generate Load Cases                     : CP=     0.01
                   Generating Loads on MODEL at Time 0.000
                   =======================================
                              Total Global Force
            0.00      0.00      1.00         0        -9         0
    Time To Generate Load Cases                     : CP=     0.00
>ssolve
                        Reducing Stiffness of DEFAULT
                        =============================
    Time to Define Model Topology                   : CP=     0.01
    Time to Complete Nodal Loads                    : CP=     0.00
    Time to Define Stiffness Blocks                 : CP=     0.00
    Time to Form Element Matricies                  : CP=     0.01
    Time to Form Global Stiffness Matrix            : CP=     0.00
    Time to Form Global Load Matrix                 : CP=     0.00
        *** WARNING: 4.3 Sig. Figures Lost At **IN0117 In Direction  Z
        ==============================================================
    Time to Factor Stiffness Matrix                 : CP=     0.00
                         Expanding Results of DEFAULT
                         ============================
    Time For Backward Substitution                  : CP=     0.00
    Time to Store Deflections                       : CP=     0.00
    Time to Store Element Internal Loads            : CP=     0.00
>end
                               +++ M A I N +++
                               ===============
 
 
>strpost
         +++ S T R U C T U R A L   P O S T - P R O C E S S I N G +++
         ===========================================================
 
 
>end
                               +++ M A I N +++
                               ===============
 
 
>&device -g_default device -oecho no
>&picture iso -type struc
 
 
                          MOSES   Finished Normally
                          =========================
                           CP Time             0.26
                           ========================
                           Total Units         0.26
                           ========================