f361fee969
Snapshots the current development tree, headlined by proper load combinations (user request): a reusable LoadCombination entity of weighted completed static-case results (e.g. 1.2xDead + 1.6xLive). - core: LoadCombination/LoadCombinationItem entities, Project integration (lookup, unique ids, reference validation) - services: combinations.py (linear superposition + envelope), exported via services __init__ - commands: undoable Add/Delete/Update for combinations - GUI: Load Combinations manager dialog, Run-dialog evaluation, envelope display in Results panel, Combinations tab in Table dock - tests: unit coverage (validation, math, error paths) + integration superposition check vs a single factored run
94 lines
4.2 KiB
Text
94 lines
4.2 KiB
Text
# --------------------------------------------------------------------------------------------------
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# Example 1. portal frame in 2D
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# static pushover analysis of Portal Frame, with gravity.
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# all units are in kip, inch, second
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# elasticBeamColumn ELEMENT
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# Silvia Mazzoni & Frank McKenna, 2006
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#
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# ^Y
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# |
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# 3_________(3)________4 __
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# | | |
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# | | |
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# | | |
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# (1) (2) LCol
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# | | |
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# | | |
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# | | |
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# =1= =2= _|_ -------->X
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# |----------LBeam------------|
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#
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# SET UP ----------------------------------------------------------------------------
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wipe; # clear opensees model
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model basic -ndm 2 -ndf 3; # 2 dimensions, 3 dof per node
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file mkdir Data; # create data directory
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# define GEOMETRY -------------------------------------------------------------
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# nodal coordinates:
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node 1 0 0; # node#, X Y
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node 2 504 0
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node 3 0 432
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node 4 504 432
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# Single point constraints -- Boundary Conditions
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fix 1 1 1 1; # node DX DY RZ
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fix 2 1 1 1; # node DX DY RZ
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fix 3 0 0 0
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fix 4 0 0 0
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# nodal masses:
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mass 3 5.18 0. 0.; # node#, Mx My Mz, Mass=Weight/g.
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mass 4 5.18 0. 0.
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# Define ELEMENTS -------------------------------------------------------------
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# define geometric transformation: performs a linear geometric transformation of beam stiffness and resisting force from the basic system to the global-coordinate system
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geomTransf Linear 1; # associate a tag to transformation
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# connectivity: (make A very large, 10e6 times its actual value)
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element elasticBeamColumn 1 1 3 3600000000 4227 1080000 1; # element elasticBeamColumn $eleTag $iNode $jNode $A $E $Iz $transfTag
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element elasticBeamColumn 2 2 4 3600000000 4227 1080000 1
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element elasticBeamColumn 3 3 4 5760000000 4227 4423680 1
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# Define RECORDERS -------------------------------------------------------------
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recorder Node -file Data/DFree.out -time -node 3 4 -dof 1 2 3 disp; # displacements of free nodes
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recorder Node -file Data/DBase.out -time -node 1 2 -dof 1 2 3 disp; # displacements of support nodes
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recorder Node -file Data/RBase.out -time -node 1 2 -dof 1 2 3 reaction; # support reaction
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recorder Drift -file Data/Drift.out -time -iNode 1 2 -jNode 3 4 -dof 1 -perpDirn 2 ; # lateral drift
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recorder Element -file Data/FCol.out -time -ele 1 2 globalForce; # element forces -- column
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recorder Element -file Data/FBeam.out -time -ele 3 globalForce; # element forces -- beam
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# define GRAVITY -------------------------------------------------------------
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pattern Plain 1 Linear {
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eleLoad -ele 3 -type -beamUniform -7.94 ; # distributed superstructure-weight on beam
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}
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constraints Plain; # how it handles boundary conditions
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numberer Plain; # renumber dof's to minimize band-width (optimization), if you want to
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system BandGeneral; # how to store and solve the system of equations in the analysis
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test NormDispIncr 1.0e-8 6 ; # determine if convergence has been achieved at the end of an iteration step
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algorithm Newton; # use Newton's solution algorithm: updates tangent stiffness at every iteration
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integrator LoadControl 0.1; # determine the next time step for an analysis, # apply gravity in 10 steps
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analysis Static # define type of analysis static or transient
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analyze 10; # perform gravity analysis
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loadConst -time 0.0; # hold gravity constant and restart time
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# define LATERAL load -------------------------------------------------------------
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# Lateral load pattern
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pattern Plain 2 Linear {
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load 3 2000. 0.0 0.0; # node#, FX FY MZ -- representative lateral load at top nodes
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load 4 2000. 0.0 0.0; # place 1/2 of the weight for each node to get shear coefficient
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}
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# pushover: diplacement controlled static analysis
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integrator DisplacementControl 3 1 0.1; # switch to displacement control, for node 11, dof 1, 0.1 increment
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analyze 100; # apply 100 steps of pushover analysis to a displacement of 10
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puts "Done!"
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