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 -g_default device -oecho no >&dimen -dimen feet kips >inmodel Time To perform Inmodel : CP= 0.08 >&title Rectangle with No Refinement >&subtitle Same Problem as rect_ref >&selec :p -sel *a@ *b@ *c@ *d@ *e@ *f@ **R@ >&summ +++ & S U M M A R Y +++ ======================= >point coor >plate >cat >end +++ M A I N +++ =============== >&pict top -type struct -point :p -ano point >struct +++ S T R U C T U R A L S O L U T I O N +++ ============================================= >lc_doit load #load Generating Loads on TEST at Time 0.000 ====================================== Total Global Force -2000.00 0.00 0.00 0 0 0 Time To Generate Load Cases : CP= 0.01 >ssolve 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 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 -node *@ >rest load >plate stress -detail -node @ >end +++ M A I N +++ =============== >&pict top -type struct -color stress MOSES Finished Normally ========================= CP Time 0.15 ======================== Total Units 0.15 ========================