Good day, I would like to ask for assistance regarding my disjointed model. I would like to model and analyse the structure as seen in its 3D rendered view.
Here are the inputs as per the editor.
STAAD SPACESTART JOB INFORMATIONENGINEER DATE 14-Jun-16END JOB INFORMATIONINPUT WIDTH 79UNIT MMS KNJOINT COORDINATES1 0 0 0; 2 4000 0 0; 3 0 2560 0; 4 4000 2560 0; 5 200 2560 200;6 200 2560 -200; 7 -200 2560 200; 8 -200 2560 -200; 13 0 2560 400;15 0 2560 -400; 18 -570 2560 0; 19 4570 2560 0; 20 4000 2560 400;21 4000 2560 -400; 26 4200 2560 200; 27 4200 2560 -200; 28 3800 2560 200;29 3800 2560 -200;MEMBER INCIDENCES2 1 3; 3 2 4; 71 15 13; 72 21 20; 73 18 19;ELEMENT INCIDENCES SHELL22 8 6 5 7; 42 29 27 26 28;ELEMENT PROPERTY22 42 THICKNESS 16DEFINE MATERIAL STARTISOTROPIC STEELE 205POISSON 0.3DENSITY 7.68195e-008ALPHA 1.2e-005DAMP 0.03TYPE STEELSTRENGTH FY 0.2532 FU 0.4078 RY 1.5 RT 1.2END DEFINE MATERIALMEMBER PROPERTY AMERICAN2 3 TABLE ST HSSP8.625X0.18871 72 TABLE D C4X7 SP 24773 TABLE D C4X7 SP 587CONSTANTSMATERIAL STEEL ALLSUPPORTS1 2 PINNEDMEMBER OFFSET71 START 0 58.7995 071 END 0 58.7995 072 START 0 58.7995 072 END 0 58.7995 073 START 0 160.4 073 END 0 160.4 0LOAD 1 LOADTYPE Dead TITLE DEADSELFWEIGHT Y -1 LIST ALLMEMBER LOAD73 CON GY -6.8 12073 CON GY -6.8 257073 CON GY -6.8 5020LOAD 2 LOADTYPE Wind TITLE WIND +XMEMBER LOAD2 3 TRAP GX 0 1.37 0 2560LOAD 3 LOADTYPE Wind TITLE WIND +ZMEMBER LOAD2 3 TRAP GZ 0 1.37 0 256073 UNI GZ 1.37 0 5140LOAD 4 LOADTYPE Wind TITLE WIND +X +ZMEMBER LOAD2 3 TRAP GX 0 1.37 0 25602 3 TRAP GZ 0 1.37 0 256073 UNI Z 1.37 0 5140LOAD 5 LOADTYPE Wind TITLE WIND +X -ZMEMBER LOAD2 3 TRAP GX 0 1.37 0 25602 3 TRAP GZ 0 -1.37 0 256073 UNI GZ -1.37 0 5140LOAD 6 LOADTYPE Wind TITLE WIND -X +ZMEMBER LOAD2 3 TRAP GX 0 -1.37 0 25602 3 TRAP GZ 0 1.37 0 2560LOAD 7 LOADTYPE Wind TITLE WIND -X -ZMEMBER LOAD2 3 TRAP GX 0 -1.37 0 25602 3 TRAP GZ 0 -1.37 0 2560LOAD COMB 8 COMBINATION LOAD CASE 81 1.2 2 1.6 LOAD COMB 9 COMBINATION LOAD CASE 91 1.2 3 1.6 LOAD COMB 10 COMBINATION LOAD CASE 101 1.2 4 1.6 LOAD COMB 11 COMBINATION LOAD CASE 111 1.2 5 1.6 LOAD COMB 12 COMBINATION LOAD CASE 121 1.2 6 1.6 LOAD COMB 13 COMBINATION LOAD CASE 131 1.2 7 1.6 PERFORM ANALYSISPARAMETER 1CODE AISC UNIFIED 2010CHECK CODE MEMB 2 3FINISH
Thank you all in advance for any assistance you may provide.
You need to first rectify beam plate connectivity issues and then intersect the members. Please refer to the attached rectified model.
6746.a5.std