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 >&dimen -dimen feet kips >inmodel Time To perform Inmodel : CP= 0.08 >&set fact = .125 >&apply @ .125*100 >&instate -con 10 >&weight -compute temp 0. >&equi +++ 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 -------- --------- --------- --------- --------- --------- --------- TEMP Location 0.00 0.00 -10.00 0.00 0.00 0.00 N Force -0.00 0.00 0.00 0 0 0 Equilibrium Converged in 1 Iterations >&event 1 >&data env +++ & D A T A +++ ================= >env env -sea issc 90 50 10 -use_mean yes >env env1 -sea issc 90 50 10 -use_mean yes >end_&data +++ M A I N +++ =============== >medit +++ M O D E L E D I T I N G +++ ================================= >~rest1 fix >connect r1 ~rest1 *2 >end +++ M A I N +++ =============== >struct +++ S T R U C T U R A L S O L U T I O N +++ ============================================= >s_part jacket >s_rest ~rest1 >lcase -process static 1 -note Static Load Case Time To Generate Load Cases : CP= 0.01 >ssolve Reducing Stiffness of DEFAULT ============================= 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 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 +++ =============== >&status note +++ D E S C R I P T I O N O F C A T E G O R I E S +++ ========================================================= Name Tag /---------------------- Description ---------------------/ EXTRAS EXTRAS Additional Things +++ DESCRIPTION OF STRUCTURAL REPORT CASES +++ ============================================== Name Tag /---------------------- Description ---------------------/ STATIC STATIC Static Load Case +++ DESCRIPTION OF STRUCTURAL SOLUTION CASE +++ =============================================== Name Tag /---------------------- Description ---------------------/ STATIC STATIC Static Load Case >medit +++ M O D E L E D I T I N G +++ ================================= >~rest2 fix >rest ~rest2 *2 >end +++ M A I N +++ =============== >hydro +++ H Y D R O _ D Y N A M I C S +++ =================================== >g_press -period 5 7 9 11 13 15 17 -heading 90 Setting Pressure Name for TEMP to TEMP ====================================== Time for Strip Theory For TEMP : CP= 0.00 Setting Drift Name for TEMP to TEMP =================================== Time to Sum Pressures For 45 Panels on TEMP : CP= 0.00 Time To Set Up Convolution For TEMP : CP= 0.01 >end +++ M A I N +++ =============== >freq_resp +++ F R E Q U E N C Y R E S P O N S E +++ =========================================== >rao Time To Compute RAOs : CP= 0.01 >fr_point 200 0 38.33 RAOs Moved to X = 200.0 Y = 0.0 Z = 38.3 =============================================== +++ D I S P O S I T I O N +++ ============================= >report >end +++ F R E Q U E N C Y R E S P O N S E +++ =========================================== >fr_fcargo 2*25500*.125 32 120 120 Forces with WT = 6375.0 RX = 32.0 RY = 120.0 RZ = 120.0 ============================================================= +++ D I S P O S I T I O N +++ ============================= >report >end +++ F R E Q U E N C Y R E S P O N S E +++ =========================================== >st_fcargo env THE FOLLOWING DATA WILL BE USED =============================== Spectrum Type = ISSC Sign. Wave Height = 50.00 Mean Period = 10.00 Mean Heading = 90.00 Spreading Coef. = 200.00 Statistics = MAX +++ D I S P O S I T I O N +++ ============================= >report >end +++ F R E Q U E N C Y R E S P O N S E +++ =========================================== >end +++ M A I N +++ =============== >struc +++ S T R U C T U R A L S O L U T I O N +++ ============================================= >lcase -rao Time To Generate Load Cases : CP= 0.02 >s_part jacket >s_rest ~rest2 >ssolve 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 Expanding Results of DEFAULT ============================ Time For Backward Substitution : CP= 0.00 Time to Store Deflections : CP= 0.01 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 +++ =========================================================== >cases -spec env >&select :load -s static frqmean@ env >restraint -load :load -detail >end +++ M A I N +++ =============== MOSES Finished Normally ========================= CP Time 0.27 ======================== Total Units 0.27 ========================