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=     0.09
>&apply -load @ 100 -force @ 100
>&summary
                           +++ & S U M M A R Y +++
                           =======================
 
 
>beam ud_for
>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
            0.00      0.00    -10.00         0       100         0
    Time To Generate Load Cases                     : CP=     0.01
>s_rest ~one ~twoa
>ssolve -n
                        Reducing Stiffness of DEFAULT
                        =============================
    Time to Define Model Topology                   : CP=     0.00
    Time to Complete Nodal Loads                    : CP=     0.01
    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
                            Solving Residual Model
                            ======================
    Time to Define Model Topology                   : CP=     0.00
                   Load Case LC1 Converged in 2 Iterations
                   =======================================
    Time to Solve Boundary Relations of DEFAULT     : CP=     0.01
                         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 +++
         ===========================================================
 
 
>joint disp
>rest -detail
>beam loads
>end
                               +++ M A I N +++
                               ===============
 
 
>struc -init
                +++ 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
            0.00      0.00    -10.00         0       100         0
    Time To Generate Load Cases                     : CP=     0.01
>lc_doit        lc2 #lc1 #lc2
                   Generating Loads on MODEL at Time 0.000
                   =======================================
                              Total Global Force
           -0.50      0.00    -10.00         0       100         0
    Time To Generate Load Cases                     : CP=     0.01
>s_rest ~one ~twob
>ssolve -nonlinear
                        Reducing Stiffness of DEFAULT
                        =============================
    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=     0.00
    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
                            Solving Residual Model
                            ======================
    Time to Define Model Topology                   : CP=     0.00
                   Load Case LC1 Converged in 1 Iterations
                   =======================================
                   Load Case LC2 Converged in 1 Iterations
                   =======================================
    Time to Solve Boundary Relations of DEFAULT     : CP=     0.01
                         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 +++
         ===========================================================
 
 
>joint disp
>rest -detail
>beam loads
>end
                               +++ M A I N +++
                               ===============
 
 
 
 
                          MOSES   Finished Normally
                          =========================
                           CP Time             0.23
                           ========================
                           Total Units         0.23
                           ========================