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 +++ =============== >&device -oecho no >inmodel Time To perform Inmodel : CP= 0.09 >&apply -force -percent @ 100 -load -percent @ >&instate -loc 0 0 0 0 0 0 >&summary +++ & S U M M A R Y +++ ======================= >class >point_sum >beam >plate >categ >end +++ M A I N +++ =============== >STRUCT +++ S T R U C T U R A L S O L U T I O N +++ ============================================= >lc_doit CASE #LOAD .5 Generating Loads on MODEL at Time 0.000 ======================================= Total Global Force 137.50 0.00 -1505.36 0 1500 0 Time To Generate Load Cases : CP= 0.00 >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= 0.01 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 Solving Residual Model ====================== Time to Define Model Topology : CP= 0.00 Load Case CASE Converged in 6 Iterations ======================================== Time to Solve Boundary Relations of DEFAULT : CP= 0.01 Expanding Results of DEFAULT ============================ Time For Backward Substitution : CP= 0.01 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 displ >REST loads pile -detail -standard -summary >end +++ M A I N +++ =============== MOSES Finished Normally ========================= CP Time 0.18 ======================== Total Units 0.18 ========================