Two issues about output objects
Moderators: silvia, selimgunay, Moderators
Two issues about output objects
Hi all!
I have two issues..
First: there are commands like ‘nodeDisp’ or ‘nodeVel’ to check other parameters of the structure like stiffness, local deformations, etc.?
If not, how can I check them?
For ex. if I want to stop the analysis when a target deformation is reached by concrete or steel, how can I do that?
Second: in the section fiber deformation output file the three columns are : load factor , axial def. and rotation. Isn’t it? The last is the chord rotation?
Thank you for the attention and for your assistance!
Best regards.
I have two issues..
First: there are commands like ‘nodeDisp’ or ‘nodeVel’ to check other parameters of the structure like stiffness, local deformations, etc.?
If not, how can I check them?
For ex. if I want to stop the analysis when a target deformation is reached by concrete or steel, how can I do that?
Second: in the section fiber deformation output file the three columns are : load factor , axial def. and rotation. Isn’t it? The last is the chord rotation?
Thank you for the attention and for your assistance!
Best regards.
getStrain, getStress
How do getStrain or getStress commands work?.
I have not seen anything about it in the manual.
I have not seen anything about it in the manual.
getStrain?
Is there a getStrain command or is it a function in the material implementation code? If such command exist is there an example on how to use it. If no such command exist, is there a command to extract strain component during the analysis to check the values rather than from the output files.
-
- Posts: 71
- Joined: Sat Nov 29, 2008 10:18 am
- Location: -
Re: getStrain?
Try with eleResponse command... (see the online manual)
Hope it helps you.
Hope it helps you.
Hugo Esquivel
it is the eleResponse command, here is an example usage.
[code]
model basic -ndm 2 -ndf 2
node 1 0.0 0.0
node 2 0.0 10.0 -mass 0.0 1.0
uniaxialMaterial Elastic 3 300.0
element truss 1 1 2 10.0 3
fix 1 1 1
fix 2 1 0
set Fy -50. ;# magnitude
set SineSeries "Trig 0. 1000. 1."
pattern Plain 2 $SineSeries {
load 2 0.0 $Fy
}
system BandGen
constraints Plain
test NormDispIncr 1.0e-12 10 0
algorithm Newton
numberer RCM
integrator Newmark 0.5 0.25
analysis Transient
for {set i 1} {$i < 1000} {incr i 1} {
analyze 1 0.01
set stress [eleResponse 1 material stress]
puts "[getTime] $stress"
}
[/code]
[code]
model basic -ndm 2 -ndf 2
node 1 0.0 0.0
node 2 0.0 10.0 -mass 0.0 1.0
uniaxialMaterial Elastic 3 300.0
element truss 1 1 2 10.0 3
fix 1 1 1
fix 2 1 0
set Fy -50. ;# magnitude
set SineSeries "Trig 0. 1000. 1."
pattern Plain 2 $SineSeries {
load 2 0.0 $Fy
}
system BandGen
constraints Plain
test NormDispIncr 1.0e-12 10 0
algorithm Newton
numberer RCM
integrator Newmark 0.5 0.25
analysis Transient
for {set i 1} {$i < 1000} {incr i 1} {
analyze 1 0.01
set stress [eleResponse 1 material stress]
puts "[getTime] $stress"
}
[/code]