knee braced frame
Moderators: silvia, selimgunay, Moderators
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- Posts: 10
- Joined: Fri Apr 10, 2009 1:37 pm
- Location: t
knee braced frame
i want to model knee braced frames with opensees How should i arrange analysis option "test, integrator ......
do some homework .. look at the examples in the examples manual or those here:
[code]
http://opensees.berkeley.edu/cgi-bin/cv ... leScripts/
[/code]
[code]
http://opensees.berkeley.edu/cgi-bin/cv ... leScripts/
[/code]
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- Posts: 10
- Joined: Fri Apr 10, 2009 1:37 pm
- Location: t
Hi thanks for your attention I have studied example scripts but i could not find any thing for solving the error have been occured during the analysis.
this is my model please help me about that
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wipe
model BasicBuilder -ndm 2 - ndf 3
node 1 0 0
node 2 0 280
node 3 0 280
node 4 259 280
node 5 259 280
node 6 259 280
node 7 320 280
node 8 320 280
node 9 320 210
node 10 320 210
node 11 320 210
node 12 285.39 249.72
node 13 285.39 249.72
node 14 285.39 249.72
node 15 320 0
fix 1 1 1 1
fix 15 1 1 1
mass 3 22.94 0 0
mass 7 22.94 0 0
geomTransf Linear 1
geomTransf PDelta 2
uniaxialMaterial Steel02 1 2400 2.1e6 .02 15 .925 .15 0 0 0 0
uniaxialMaterial Steel01 2 100000000 1e11 0.01
source Wsection.tcl
Wsection 1 1 125e-1 6.5e-1 1.25e-1 9e-1 10 2 10 2
Wsection 2 1 10 6e-1 10 6e-1 10 2 10 2
source doublechannelsection.tcl
Doublechannel 10 1 10 5e-1 5 8.5e-1 1 2 10 2 10
source Hollowsquaresection.tcl
Hollowsquare 20 1 6 4.5e-1 6 4.5e-1 2 10 2 10
section Aggregator 30 1 Vy -section 20
# column
element nonlinearBeamColumn 1 1 2 5 1 1
element nonlinearBeamColumn 3 15 11 5 1 1
element nonlinearBeamColumn 4 10 8 5 1 1
# Beam
element zeroLength 5 2 3 -mat 2 2 2 2 -dir 1 2 3 6
element zeroLength 6 7 8 -mat 2 2 2 2 -dir 1 2 3 6
element nonlinearBeamColumn 8 3 4 5 2 1
element nonlinearBeamColumn 9 5 7 5 2 1
# KneeElement
element zeroLength 10 4 6 -mat 2 2 2 2 -dir 1 2 3 6
element zeroLength 11 10 9 -mat 2 2 2 2 -dir 1 2 3 6
element nonlinearBeamColumn 13 12 6 5 30 1
element nonlinearBeamColumn 14 13 9 5 30 1
# Brace
element zeroLength 15 14 13 -mat 2 2 2 2 -dir 1 2 3 6
element nonlinearBeamColumn 16 1 14 5 10 1
equalDOF 2 4 1
equalDOF 2 8 1
pattern Plain 1 Linear {
eleLoad -ele 1 -type -beamUniform -45.88
}
constraints Transformation
numberer RCM
system BandGeneral
test NormDispIncr 1.0e-6 6
algorithm Newton
integrator LoadControl 0.1
analysis Static
analyze 10
loadConst -time 0.0
this is my model please help me about that
-------------------------------------
wipe
model BasicBuilder -ndm 2 - ndf 3
node 1 0 0
node 2 0 280
node 3 0 280
node 4 259 280
node 5 259 280
node 6 259 280
node 7 320 280
node 8 320 280
node 9 320 210
node 10 320 210
node 11 320 210
node 12 285.39 249.72
node 13 285.39 249.72
node 14 285.39 249.72
node 15 320 0
fix 1 1 1 1
fix 15 1 1 1
mass 3 22.94 0 0
mass 7 22.94 0 0
geomTransf Linear 1
geomTransf PDelta 2
uniaxialMaterial Steel02 1 2400 2.1e6 .02 15 .925 .15 0 0 0 0
uniaxialMaterial Steel01 2 100000000 1e11 0.01
source Wsection.tcl
Wsection 1 1 125e-1 6.5e-1 1.25e-1 9e-1 10 2 10 2
Wsection 2 1 10 6e-1 10 6e-1 10 2 10 2
source doublechannelsection.tcl
Doublechannel 10 1 10 5e-1 5 8.5e-1 1 2 10 2 10
source Hollowsquaresection.tcl
Hollowsquare 20 1 6 4.5e-1 6 4.5e-1 2 10 2 10
section Aggregator 30 1 Vy -section 20
# column
element nonlinearBeamColumn 1 1 2 5 1 1
element nonlinearBeamColumn 3 15 11 5 1 1
element nonlinearBeamColumn 4 10 8 5 1 1
# Beam
element zeroLength 5 2 3 -mat 2 2 2 2 -dir 1 2 3 6
element zeroLength 6 7 8 -mat 2 2 2 2 -dir 1 2 3 6
element nonlinearBeamColumn 8 3 4 5 2 1
element nonlinearBeamColumn 9 5 7 5 2 1
# KneeElement
element zeroLength 10 4 6 -mat 2 2 2 2 -dir 1 2 3 6
element zeroLength 11 10 9 -mat 2 2 2 2 -dir 1 2 3 6
element nonlinearBeamColumn 13 12 6 5 30 1
element nonlinearBeamColumn 14 13 9 5 30 1
# Brace
element zeroLength 15 14 13 -mat 2 2 2 2 -dir 1 2 3 6
element nonlinearBeamColumn 16 1 14 5 10 1
equalDOF 2 4 1
equalDOF 2 8 1
pattern Plain 1 Linear {
eleLoad -ele 1 -type -beamUniform -45.88
}
constraints Transformation
numberer RCM
system BandGeneral
test NormDispIncr 1.0e-6 6
algorithm Newton
integrator LoadControl 0.1
analysis Static
analyze 10
loadConst -time 0.0