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
>inmodel
    Time To perform Inmodel                         : CP=     0.10
>&apply -load @ 100 -force @ 100
>&summary
                           +++ & S U M M A R Y +++
                           =======================
 
 
>class
>point
>beam
>plate
>categ
>end
                               +++ M A I N +++
                               ===============
 
 
>struc
                +++ S T R U C T U R A L   S O L U T I O N +++
                =============================================
 
 
>lc_doit  lc1 #lc1
                   Generating Loads on MODEL at Time 0.000
                   =======================================
                              Total Global Force
           10.00      0.00    -10.00         0       300         0
    Time To Generate Load Cases                     : CP=     0.01
>s_part three
>s_rest none
>reduce part3 *c1 *c2 *c3 *c4
                         Reducing Stiffness of PART3
                         ===========================
    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=     0.00
    Time to Form Global Stiffness Matrix            : CP=     0.00
    Time to Form Global Load Matrix                 : CP=     0.00
    Time to Factor Stiffness Matrix                 : CP=     0.00
>s_part part3 super two
>s_rest none
>reduce part2 *b1 *b2 *b3 *b4
                         Reducing Stiffness of PART2
                         ===========================
    Time to Define Model Topology                   : CP=     0.00
    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
    Time to Factor Stiffness Matrix                 : CP=     0.00
>s_part part2 super one
>s_rest ~@
>ssolve model
                         Reducing Stiffness of model
                         ===========================
    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=     0.00
    Time to Form Global Stiffness Matrix            : CP=     0.00
    Time to Form Global Load Matrix                 : CP=     0.00
    Time to Factor Stiffness Matrix                 : CP=     0.00
                          Expanding Results of model
                          ==========================
    Time For Backward Substitution                  : CP=     0.00
    Time to Store Deflections                       : CP=     0.01
    Time to Store Element Internal Loads            : CP=     0.00
>expand part2
                          Expanding Results of part2
                          ==========================
    Time For Backward Substitution                  : CP=     0.00
    Time to Store Deflections                       : CP=     0.00
    Time to Store Element Internal Loads            : CP=     0.00
>expand part3
                          Expanding Results of part3
                          ==========================
    Time For Backward Substitution                  : CP=     0.00
    Time to Store Deflections                       : CP=     0.00
    Time to Store Element Internal Loads            : CP=     0.00
>end
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                               ===============
 
 
>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 +++
         ===========================================================
 
 
>joint disp
>rest -detail
>beam loads
>end
                               +++ M A I N +++
                               ===============
 
 
 
 
                          MOSES   Finished Normally
                          =========================
                           CP Time             0.20
                           ========================
                           Total Units         0.20
                           ========================