【免费下载】用OpenSees进行截面弯矩 曲率分析

Tcl Basics

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Here is the file: MomentCurvature.tcl

Moment Curvature Example用OpenSees进行截面弯矩-曲率分析,分析结果可用于SAP2000自定义铰属性

This next example covers the moment-curvature analysis of a rectangular reinforced concrete section. In this example a Zero

Length element with the fiber discretization of the cross section is used. In addition to providing understanding as to the creation of a fiber section, the example introduces Tcl language features such as variable and command substitution, expression evaluation and the use of procedures.

1.The lines in the dashed boxes are lines that appear in the input file.

2.all lines that begin with # are comments, they are ignored by the program (interpreter) but are useful for documenting the code. When creating your own input scripts you are highly encouraged to use comments.

In the tcl script that is to be presented, variables, expressions and procedures are used.

A variable is a symbolic name given to some known or unknown quantity or information, for the purpose of allowing the name to be used independently of the information it represents. In Tcl a variable once set (with the set command) can then be subsequently using the syntax of $variable. The following tcl example sets the variable v to be 2.0, and then prints to the screen a message saying what the value of v is.

set v 3.0

puts \"v equals $v\"

Expressions can be evaluated using the expr command. When using the

expr command, most mathematical functions found in any programming language can be used, e.g. sin(), cos(), max(), min(), abs(),... It is also typical to combine an expression command, with a set command. To do this, the expr command is enclosed in square brackets []'s. The following example demonstrates the setting of a variable v to be 3.0, the setting of another variable sum to be the result of adding whatever the value of the variable v is to 2.0, and finally the

printing to the screen of a message saying what the current value of sum is.

Typically, the result of an expression is then set to another

variable. A simple example to add 2.0 to a parameter and print the result is shown below:

set v 3.0

set sum [expr $v + 2.0]

puts \"sum equals $sum\"; # print the sum

MomentCurvature.tcl Script

The file contains 2 parts. The first part contains a procedure named MomentCurvature, and the second part contains the creation of the section and the subsequent calling of the procedure. NOTES:

1.Typically useful procedures such as MomentCurvature would be placed in a separate file. This is done so that other scripts

can also use them. It is only placed in the same file here to limit the number of downloads for the reader of this article. 2.In the referenced file, the procedure proceeds the calling of the procedure. It must always be thus. In this article we discuss the section generation first.

Section Definition

For the zero length element, a section discretized by concrete and steel is created to represent the behaviour. UniaxialMaterial objects are created which define the fiber stress-strain relationship's. There is confined concrete in the core, unconfined concrete in the cover region, and reinforcing steel.

The dimension of the section are as shown in the figure. The section

depth is 24 inches, the width 15 inches, and there is 1.5inch cover all around. Strong axis bending is about the z-axis. The section is separated into confined and unconfined concrete regions, for which separate discretizations will be generated, Reinforcing steel is

placed around the boundary of th confined and unconfined regions. The fiber discretization is shown below:

The following are the commands that generate the section and perform the moment curvature analysis. The model and analysis commands are contained in the MomentCurvature procedure. These are contained in a seperate file which are \"sourced\"\" by the main script. # units: kip, in# Remove existing modelwipe

# Create ModelBuilder (with two-dimensions and 3 DOF/node)model BasicBuilder -ndm 2 -ndf 3

# 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 stressset E 30000.0; # Young's modulus

# tag fy E0 buniaxialMaterial Steel01 3 $fy $E 0.01# ------------------------------------------

# set some paramatersset colWidth 15set colDepth 24

set cover 1.5

set As 0.60; # area of no. 7 bars# some variables derived from the parametersset y1 [expr $colDepth/2.0]set z1 [expr $colWidth/2.0]

# Define cross-section for nonlinear columnssection 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]}

# Estimate yield curvature

# (Assuming no axial load and only top and bottom steel)set d [expr $colDepth-$cover];# d -- from cover to rebarset epsy [expr $fy/$E];# steel yield strainset Ky [expr $epsy/(0.7*$d)]

# Print estimate to standard outputputs \"Estimated yield curvature: $Ky\"

# Set axial load set P -180set mu 15;

set numIncr 100;

# Target ductility for analysis# Number of analysis increments

# Call the section analysis procedure

MomentCurvature 1 $P [expr $Ky*$mu] $numIncr

Moment Curvature Procedure

The Tcl procedure to perform the moment-curvature analysis follows.

The procedure takes as input the tag of the section to be analyzed, the axial load, P, to be applied, the max curvature to be evaluated and the number of iterations to achieve this max curavature. The procedure first creates the model which consists of two nodes, boundary conditions, and a ZeroLengthSection element. A depiction of the geometry is as shown in the top most figure above. The image on the left shows an edge view of the element, with local z-axis coming out of the page. Node 1 is completely restrained, with the applied loads acting at Node 2. An axial load, P, is applied to the section during the moment curvature analysis.

After the model has been created, the analysis is performed. A single load step is first performed for the axial load, then the integrator is changed to DisplacementControl to impose nodal displacements,

which map directly to section deformations. A reference moment of 1.0 is defined in a Linear time series. For this reference moment, the DisplacementControl integrator will determine the load factor needed to apply the imposed displacement. A node recorder is defined to

track the momentcurvature results. The load factor is the moment, and the nodal rotation is in fact the curvature of the element with zero thickness.

proc MomentCurvature {secTag axialLoad maxK {numIncr 100} } {

# Define two nodes at (0,0)node 1 0.0 0.0node 2 0.0 0.0

# Define analysis parametersintegrator LoadControl 0.0system SparseGeneral -piv;

pivoting!

test NormUnbalance 1.0e-9 10numberer Plainconstraints Plainalgorithm Newtonanalysis Static

}

# Define constant axial loadpattern Plain 1 \"Constant\" {

load 2 $axialLoad 0.0 0.0

}

# Do one analysis for constant axial loadanalyze 1

# Define element

# tag ndI ndJ secTagelement zeroLengthSection 1 1 2 $secTag

# Create recorder

recorder Node -file section$secTag.out -time -node 2 -dof 3

# Overkill, but may need the

disp

# Do the section analysisanalyze $numIncr

# Compute curvature incrementset dK [expr $maxK/$numIncr]

# Fix all degrees of freedom except axial and bendingfix 1 1 1 1fix 2 0 1 0

# Use displacement control at node 2 for section analysisintegrator DisplacementControl 2 3 $dK

# Define reference moment

pattern Plain 2 \"Linear\" {

load 2 0.0 0.0 1.0

}

Results

will produce the following:

In addition, your directory should contain the following a file

section1.out. A plot of this file using the following matlab commands

When you run this script, you should see the following printed to the screen:

load section1.out

plot(section1(:,2),sections1(:,1)xlabel(\"Curvature 1/in\")ylabel(\"Moment kip-in\")