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 -oecho no >inmodel Time To perform Inmodel : CP= 0.13 >&apply @ >&instate -cond 300 0 90 >medit +++ M O D E L E D I T I N G +++ ================================= >~fix fix x y z >~rx fix rx >rest ~rx *br1 >sp_beam ~sp -eleme su@ *spf *sps >end +++ M A I N +++ =============== >&status config +++ C U R R E N T S Y S T E M C O N F I G U R A T I O N +++ =============================================================== Process is DEFAULT: Units Are Degrees, Feet, and Kips Unless Specified Location and Net Force at Body Origin Body X Y Z RX RY RZ -------- --------- --------- --------- --------- --------- --------- SPAR Location 0.00 0.00 -300.00 0.00 90.00 0.00 N Force 0.00 0.00 -0.01 0 0 0 >&status force +++ F O R C E S A C T I N G O N S P A R +++ ================================================= Process is DEFAULT: Units Are Degrees, Feet, and Kips Unless Specified Results Are Reported In Body System Type of Force X Y Z MX MY MZ ------------------ --------- --------- --------- --------- --------- --------- Weight 3000.00 0.00 0.00 0 0 0 Buoyancy -1.1965E5 0.00 0.00 0 -17948096 5982347 Rigid Connectors 116653.95 0.00 -0.01 0 17948096 -5982346 ======= ======= ======= ======= ======= ======= Total 0.00 0.00 -0.01 0 0 0 >&event 1 >struct +++ S T R U C T U R A L S O L U T I O N +++ ============================================= >lcase -process 1 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= 0.03 Time to Form Global Stiffness Matrix : CP= 0.01 Time to Form Global Load Matrix : CP= 0.00 *** WARNING: 3.1 Sig. Figures Lost At **IN0241 In Direction Y ============================================================== *** WARNING: 3.0 Sig. Figures Lost At **IN0235 In Direction Y ============================================================== *** WARNING: 3.2 Sig. Figures Lost At **IN0240 In Direction Y ============================================================== *** WARNING: 3.1 Sig. Figures Lost At **IN0236 In Direction Y ============================================================== *** WARNING: 3.2 Sig. Figures Lost At **IN0239 In Direction Y ============================================================== *** WARNING: 3.2 Sig. Figures Lost At **IN0237 In Direction Y ============================================================== *** WARNING: 3.1 Sig. Figures Lost At **IN0238 In Direction X ============================================================== *** WARNING: 3.6 Sig. Figures Lost At **IN0238 In Direction Y ============================================================== Time to Factor Stiffness Matrix : 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= 0.01 >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 +++ =========================================================== >beam load stress -detail -ele s@ >end +++ M A I N +++ =============== MOSES Finished Normally ========================= CP Time 0.26 ======================== Total Units 0.26 ========================