Stress strain recorder problem

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rcsoul
Posts: 17
Joined: Mon Jun 13, 2005 4:27 am
Location: Integer Engineering Consultants, Ltd.

Stress strain recorder problem

Post by rcsoul »

Hi, everyone:
I've tested stressStrain recorder on example 3.1. I only add one recorder to record stress-strain relationship but got an empty file. Did I miss something?


# OpenSees Example 3.1
# OpenSees Primer
#
# Units: kips, in, sec
# ------------------------------
# Start of model generation
# ------------------------------
# Create ModelBuilder (with two-dimensions and 3 DOF/node)
model basic -ndm 2 -ndf 3
# Create nodes
# ------------
# Set parameters for overall model geometry
set width 360
set height 144
# Create nodes
# tag X Y
node 1 0.0 0.0
node 2 $width 0.0
node 3 0.0 $height
node 4 $width $height
# Fix supports at base of columns
# tag DX DY RZ
fix 1 1 1 1
fix 2 1 1 1
# Define materials for nonlinear columns
# ------------------------------------------
# CONCRETE tag f'c ec0 f'cu ecu
# Core concrete (confined)
uniaxialMaterial Concrete01 1 -6.0 -0.004 -5.0 -0.014
# Cover concrete (unconfined)
uniaxialMaterial Concrete01 2 -5.0 -0.002 0.0 -0.006
# STEEL
# Reinforcing steel
set fy 60.0; # Yield stress
set E 30000.0; # Young's modulus
# tag fy E0 b
uniaxialMaterial Steel01 3 $fy $E 0.01
# Define cross-section for nonlinear columns
# ------------------------------------------
# set some paramaters
set colWidth 15
set colDepth 24
set cover 1.5
set As 0.60; # area of no. 7 bars
# some variables derived from the parameters
set y1 [expr $colDepth/2.0]
set z1 [expr $colWidth/2.0]
section Fiber 1 {
# Create the concrete core fibers
patch rect 1 10 1 [expr $cover-$y1] [expr $cover-$z1] [expr $y1-$cover] [expr $z1-$cover]
# Create the concrete cover fibers (top, bottom, left, right)
patch rect 2 10 1 [expr -$y1] [expr $z1-$cover] $y1 $z1
patch rect 2 10 1 [expr -$y1] [expr -$z1] $y1 [expr $cover-$z1]
patch rect 2 2 1 [expr -$y1] [expr $cover-$z1] [expr $cover-$y1] [expr $z1-$cover]
patch rect 2 2 1 [expr $y1-$cover] [expr $cover-$z1] $y1 [expr $z1-$cover]
# Create the reinforcing fibers (left, middle, right)
layer straight 3 3 $As [expr $y1-$cover] [expr $z1-$cover] [expr $y1-$cover] [expr $cover-$z1]
layer straight 3 2 $As 0.0 [expr $z1-$cover] 0.0 [expr $cover-$z1]
layer straight 3 3 $As [expr $cover-$y1] [expr $z1-$cover] [expr $cover-$y1] [expr $cover-$z1]
}
# Define column elements
# ----------------------
# Geometry of column elements
# tag
geomTransf Linear 1
# Number of integration points along length of element
set np 5
# Create the coulumns using Beam-column elements
# tag ndI ndJ nsecs secID transfTag
element nonlinearBeamColumn 1 1 3 $np 1 1
element nonlinearBeamColumn 2 2 4 $np 1 1
# Define beam elment
# -----------------------------
# Geometry of column elements
# tag
geomTransf Linear 2
# Create the beam element
# tag ndI ndJ A E Iz transfTag
element elasticBeamColumn 3 3 4 360 4030 8640 2
# Define gravity loads
# --------------------
# Set a parameter for the axial load
set P 180; # 10% of axial capacity of columns
# Create a Plain load pattern with a Linear TimeSeries
pattern Plain 1 "Linear" {
# Create nodal loads at nodes 3 & 4
# nd FX FY MZ
load 3 0.0 [expr -$P] 0.0
load 4 0.0 [expr -$P] 0.0
}
# ------------------------------
# End of model generation
# ------------------------------
# ------------------------------
# Start of analysis generation
# ------------------------------
# Create the system of equation, a sparse solver with partial pivoting
system BandGeneral
# Create the constraint handler, the transformation method
constraints Transformation
# Create the DOF numberer, the reverse Cuthill-McKee algorithm
numberer RCM
# Create the convergence test, the norm of the residual with a tolerance of
# 1e-12 and a max number of iterations of 10
test NormDispIncr 1.0e-12 10 3
# Create the solution algorithm, a Newton-Raphson algorithm
algorithm Newton
# Create the integration scheme, the LoadControl scheme using steps of 0.1
integrator LoadControl 0.1
# Create the analysis object
analysis Static
# initialize in case we need to do an initial stiffness iteration
initialize
# ------------------------------
# End of analysis generation
# ------------------------------
# ------------------------------
# Start of recorder generation
# ------------------------------
# Create a recorder to monitor nodal displacements
recorder Node -file nodeGravity.out -time -node 3 4 -dof 1 2 3 disp
recorder Element -file teststrain.out –time -ele 1 section 3 fiber 0. 0. 1 stressStrain

# --------------------------------
# End of recorder generation
# ---------------------------------
# ------------------------------
# Finally perform the analysis
# ------------------------------
# perform the gravity load analysis, requires 10 steps to reach the load level
analyze 10
# Print out the state of nodes 3 and 4
print node 3 4
# Print out the state of element 1
print ele 1 2
Chia-hung Lin, Ph.D. Candidate, National Taiwan University
fmk
Site Admin
Posts: 5884
Joined: Fri Jun 11, 2004 2:33 pm
Location: UC Berkeley
Contact:

Post by fmk »

you had some garbage in the recorder command .. there was a space between 0. and 1 (and ppossibly some other garbage in there around -time, though that could be just the copy & paste i did). The command should be:

recorder Element -file teststrain.out -time -ele 1 section 3 fiber 0. 0.1 stressStrain
rcsoul
Posts: 17
Joined: Mon Jun 13, 2005 4:27 am
Location: Integer Engineering Consultants, Ltd.

Post by rcsoul »

Thank you very much fmk. But the number "1" I I've put after 0. was referred to $matID. Even though I tried your suggestion deleted the space between 0. and 1 it still not work. Can you give me some more help?
Chia-hung Lin, Ph.D. Candidate, National Taiwan University
silvia
Posts: 3909
Joined: Tue Jan 11, 2005 7:44 am
Location: Degenkolb Engineers
Contact:

Post by silvia »

on that same line, replace the long dash before time with a short dash.

some editors (which one are you using?) automatically replace the short dash with a long one.
Silvia Mazzoni, PhD
Structural Consultant
Degenkolb Engineers
235 Montgomery Street, Suite 500
San Francisco, CA. 94104
rcsoul
Posts: 17
Joined: Mon Jun 13, 2005 4:27 am
Location: Integer Engineering Consultants, Ltd.

Post by rcsoul »

Thank you silvia. Yes, it's my error for that dash. My editor is wordpad. But even I corrected the dash it still cannot work. Very strange... I haven't resolved it.
Chia-hung Lin, Ph.D. Candidate, National Taiwan University
silvia
Posts: 3909
Joined: Tue Jan 11, 2005 7:44 am
Location: Degenkolb Engineers
Contact:

Post by silvia »

what do you get?
Silvia Mazzoni, PhD
Structural Consultant
Degenkolb Engineers
235 Montgomery Street, Suite 500
San Francisco, CA. 94104
silvia
Posts: 3909
Joined: Tue Jan 11, 2005 7:44 am
Location: Degenkolb Engineers
Contact:

Post by silvia »

it might be that you don't have a fiber of material ID 1 near the 0. 0. coordinates you are asking for!
Silvia Mazzoni, PhD
Structural Consultant
Degenkolb Engineers
235 Montgomery Street, Suite 500
San Francisco, CA. 94104
rcsoul
Posts: 17
Joined: Mon Jun 13, 2005 4:27 am
Location: Integer Engineering Consultants, Ltd.

Post by rcsoul »

Thank u fmk and silvia. I made a mistake opening a wrong file to check the output results. It had already worked after correction following your above suggestions. Thank you very much.
Chia-hung Lin, Ph.D. Candidate, National Taiwan University
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