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 >&title AISC BEAM EXAMPLES 1 TO 3 >&m_act str_basic lcase >inmodel Time To perform Inmodel : CP= 0.08 >&apply -force -percen #live 100 >&env basic >&status force +++ F O R C E S A C T I N G O N M O D E L +++ =================================================== 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 ------------------ --------- --------- --------- --------- --------- --------- Buoyancy 0.00 0.00 0.23 0 -4 0 Applied 0.00 0.00 -52.72 0 1162 0 Added Inertia 0.00 0.00 52.49 0 -1155 0 ======= ======= ======= ======= ======= ======= Total 0.00 0.00 -0.00 0 0 0 >RESIZE UPDOWN 3 str_basic +++ S T R U C T U R A L S O L U T I O N +++ ============================================= Generating Loads on MODEL at Time 0.000 ======================================= Total Global Force 0.00 0.00 -52.49 0 1156 0 Time To Generate Load Cases : CP= 0.01 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= 0.00 Time to Store Element Internal Loads : CP= 0.00 +++ M A I N +++ =============== +++ S T R U C T U R A L P O S T - P R O C E S S I N G +++ =========================================================== resize 1 - resized 1 classes : CP= 0.01 +++ M A I N +++ =============== +++ S T R U C T U R A L S O L U T I O N +++ ============================================= Generating Loads on MODEL at Time 0.000 ======================================= Total Global Force 0.00 0.00 -52.47 0 1156 0 Time To Generate Load Cases : CP= 0.01 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= 0.01 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 +++ M A I N +++ =============== +++ S T R U C T U R A L P O S T - P R O C E S S I N G +++ =========================================================== resize 2 - resized 0 classes : CP= 0.01 +++ M A I N +++ =============== end of resize loop 0 classes overstressed ========================================= +++ S T R U C T U R A L P O S T - P R O C E S S I N G +++ =========================================================== +++ M A I N +++ =============== MOSES Finished Normally ========================= CP Time 0.18 ======================== Total Units 0.18 ========================