Hello Sir,
I am designing steel frame building using ASD method but during analysis staad is giving me the error " Each load combination must be followed by perfom cable analysis then change". unfortunately i am unable to solve this error. please help me with that.
This structure is buckling even under the selfweight loading. If you run a first order analysis ( PERFORM ANALYSIS with just the selfweight ) you will see large displacements in Y. So I would suggest that you first do a basic first order analysis with the loads and ensure that displacements are within reasonable limits for all cases. You will need to add lateral supports as otherwise the structure does not have any lateral stability with the frame hanging from four pinned supports and suspended using axial only cable elements. Stabilizing the structure even against vertical loads would require addition of weak lateral springs. Try adding weak translational springs in FX and FZ at four corners. If you need to analyze this structure for lateral loads, you would definitely need to have additional lateral supports besides these springs. Also for any nonlinear type analysis you will need to use REPEAT LOADs and not LOAD COMBINATIONs.
Can any one find the solution for this
STAAD SPACESTART JOB INFORMATIONENGINEER DATE 9/19/2018JOB NAME Load at 4m from center of lifting frameJOB NO 123JOB REV R1END JOB INFORMATIONINPUT WIDTH 79UNIT METER KNJOINT COORDINATES1 0 0 0; 2 0.740001 0 0; 3 1.74 0 0; 4 2.74001 0 0; 5 3.74001 0 0;7 5.68001 0 0; 8 6.68001 0 0; 9 7.68002 0 0; 10 8.68002 0 0; 11 9.42002 0 0;13 0.740001 0 8.40002; 14 1.74 0 8.40002; 15 2.74001 0 8.40002;16 3.74001 0 8.40002; 17 5.68001 0 8.40002; 18 6.68001 0 8.40002;19 7.68002 0 8.40002; 20 8.68002 0 8.40002; 21 0 0 8.40002;22 9.42002 0 8.40002; 25 0.740001 0 2; 32 8.68002 0 2; 33 0 0 2;34 9.42002 0 2; 37 0.740001 0 6.40001; 44 8.68002 0 6.40001; 45 0 0 6.40001;46 9.42002 0 6.40001; 48 3.56001 0 2; 49 3.56001 0 6.40001; 50 5.86001 0 2;51 5.86001 0 6.40001; 52 4.71001 0 0; 53 4.71001 0 8.40002;56 4.43501 5.75101 0; 57 4.43501 5.75101 8.40002; 58 4.98501 5.75101 0;59 4.98501 5.75101 8.40002;MEMBER INCIDENCES1 1 33; 2 33 45; 3 45 21; 4 2 1; 5 13 21; 6 25 33; 7 37 45; 8 2 3; 9 13 14;10 25 48; 11 37 49; 12 3 4; 13 14 15; 16 4 5; 17 15 16; 18 48 50; 19 49 51;20 5 52; 21 16 53; 22 7 8; 23 17 18; 26 8 9; 27 18 19; 28 50 32; 29 51 44;30 9 10; 31 19 20; 32 10 11; 33 20 22; 34 32 34; 35 44 46; 36 11 34; 37 34 46;38 46 22; 39 52 7; 40 53 17; 45 2 56; 46 10 58; 47 13 57; 48 20 59;DEFINE MATERIAL STARTISOTROPIC STEELE 1.99947e+08POISSON 0.3DENSITY 76.8191ALPHA 6.5e-06DAMP 0.03TYPE STEELSTRENGTH FY 248210 FU 399894 RY 1.5 RT 1.2END DEFINE MATERIALCONSTANTSMATERIAL STEEL ALLMEMBER PROPERTY BRITISH1 TO 13 16 TO 23 26 TO 40 TABLE ST PIP40616.0MEMBER PROPERTY BRITISH45 TO 48 PRIS YD 0.08SUPPORTS56 TO 59 PINNEDMEMBER CABLE45 TO 48 TENSION 1LOAD 1 LOADTYPE Dead TITLE DLSELFWEIGHT Y -1 PERFORM CABLE ANALYSIS BASICCHANGELOAD 2 LOADTYPE Live TITLE 4M VERTICALMEMBER LOAD8 9 CON GY -1200 030 31 CON GY -1200 1PERFORM CABLE ANALYSIS BASICCHANGELOAD 3 LOADTYPE Live TITLE 4M HORIZONTALMEMBER LOAD30 31 CON GZ -120 18 9 CON GZ -120 0PERFORM CABLE ANALYSIS BASICCHANGELOAD COMB 4 COMBINATION LOAD CASE 41 1.1 2 1.0 3 1.0 PERFORM CABLE ANALYSIS BASICCHANGEPERFORM ANALYSIS PRINT ALLPARAMETER 1CODE BS5950RATIO 1 ALLTRACK 2 ALLCHECK CODE ALLFINISH
You were attempting to do a Nonlinear Cable Analysis but there was no pretension load defined which is essential. I added a pretension of 10KN ( you may change as needed). The bigger question is whether the nonlinear cable analysis is required or not. Are these members that you assigned as cables, really cable members or are these rods ? If these are rods you may as well model these as TRUSS. Also when you are using a nonlinear cable analysis, each load case has to be a complete case by itself with selfweight and all components. You should not do a cable analysis with just the wind load ( for example load case 7 to 14 ). Also if you go with a nonlinear cable analysis, your load combinations should be replaced by REPEAT LOADs. These can be very easily handled through the command editor as explained for the load case 15 below
LOAD COMBINATION :
…
LOAD COMB 15 DL+RL
5 1.0 6 1.0
REPEAT LOAD :
LOAD 15 DL+RL
REPEAT LOAD
A partly modified file is attached for your reference. Hop this will give you some direction.
2068.Structure1.std