ACECOMS, AIT 1
Analysis and Design of Buildings
Using ETABS 9.5
Dr. Naveed Anwar, Keerati Tunthasuwat, Thuang Htut Aung
Asian Institute of Technology
Users’ Forum
Manila, 2009
About ACECOMS and AIT
The Asian Center for Engineering Computations and Software
(ACECOMS) is a part of the Structural Engineering Field in the School of Engineering and Technology (SET) at the Asian Institute of Technology (AIT), Thailand.
AIT is a postgraduate international institute established in 1959 with the mission “to develop highly qualified and committed professionals who play leading roles in the region's sustainable development and its integration into the global economy”.
The Structural Engineering Field is one of the first programs to be established at AIT and has been as a strong academic and research program for almost fifty years. The program is well known for
excellence in academic, research and industry partnership.
About ACECOMS and AIT
ACECOMS was established in 1995 as one of
the first not-for-profit, self-sustaining outreach
center in then the School of Civil Engineering to
provide and interface between academic and
research activities and the professional practice.
Since its establishment., ACECOMS has been
contributing significantly in the development and
effective applications of computational
technologies in structural and civil engineering
through its activities
ACECOMS
Carry-out research and development in engineering
computational technology and software.
Carry-out research and provide consultancy for the
applications of computing tools on the real world problems
Provide general and specialized consulting services and
support for project design, system development, review and investigation etc.
Provide trainings and technical support for development
of knowledge, information and skills
Establish networks and associations with regional
academic institutions and professional organizations
Disseminate practical information and knowledge
ACECOMS, AIT 3
Agenda
Overview
Handling Materials, Sections, Loads
Handling Special Behavior
Creating Complex Models
Analysis for various purposes
Interpreting and evaluating results
Specific Questions
What is Coming Next?
Discussion
Software Discussed
ETABS
SAP2000
SAFE
CSICOL
GEAR
GRASP
Overall Process
Define the Parameters and Properties
Quick Modeling
Import, Draw and Edit
Select and Assign
Analyze and Understand
Design and Check
Define and Preferences
ACECOMS, AIT 5
Define Coordinate System/Grids
For a regular or general system, the coordinate system is defined using an origin and orientation relative to the Global coordinate system.
All coordinate systems follow the right-hand rule. The grid lines for a regular system are defined relative to X and Y (Cartesian) or r and theta (cylindrical). The grid lines for a general system are defined relative to X and Y only.
A regular system is any coordinate/grid system having a Cartesian (rectangular) or cylindrical grid system.
A general system is a system comprised of arbitrarily defined grid lines.
The Global coordinate system always exists, and has its own grid. All other systems are user defined with respect to the Global system.
Define Coordinate System/Grids
Configuration of alternate coordinate systems
Define Coordinate System/Grids
Configuration of alternate coordinate systems
Define Coordinate System/Grids
How to determine regular system or general system
To determine if a previously defined system is a regular or general system, access the Coordinate/Grid Systems form and highlight the system name in the Systems display area. If the
Convert to General Grid check box is NOT checked (with the
ACECOMS, AIT 7
Define Coordinate System/Grids
General System
In general system, we can draw the arbitrary grid lines which does not need to perpendicular each other.
Define Coordinate System/Grids
General System
Functions
Response Spectrum
Time History
Functions
Response Spectrum Function
For Seismic Analysis
From Code (IBC2006, AASHTO, EuroCode 8 …etc.)
User Define from File
ACECOMS, AIT 9
Functions
Time History Function
From Built-in (Sine, Cosine, Ramp, Sawtooth…etc.)
User Define from File
Time History Function for Sine Function
Quick Modeling
Templates
ACECOMS, AIT 11
Staggered Truss System
Flat Slab with Perimeter Beams
ACECOMS, AIT 13
Ribbed Slab System
Template
Add template to existing model
Able to add the components from template to
Export, Draw and Edit
Creating Complex Geometry Efficiently
Import & Export
Capability to import data from many
structural engineering software to create
the model
Export the model to SAFE and other
drawing software
ACECOMS, AIT 15
Export to AutoCAD .dxf File
Drawing and Editing
Points
Nodes, Supports etc.
Lines
Frames, Beams, Trusses Cables Areas
Plate, Shell, Membrane Move
Replicate
Extrude
Edit Points
Divide
Mesh
Replicate
Generating a large model from a small model when the
objects and/or joints form a linear or radial pattern or are symmetrical about a plane or story.
Different from Cut, Copy and Paste commands.
Replicate command replicated the assignments and
loads on the objects but Cut, Copy and Paste commands are NOT capable of copying the assignments or loads.
Four types of replication
Linear
Radial
Mirror
ACECOMS, AIT 17
Extrude
Sweep selected objects through space to
create new objects of higher dimension
Extrude points to lines
Model circular-shaped beam
Extrude lines to areas
Model the ramp
Extrude
Extrude
Model circular shaped ramp by radial extrusion of line object
Edit Point
Merge joints
Merge the joints outside the auto merge tolerance.
To eliminate the extraneous joints that may occur if
the elements are drawn with snap turned off.
Align points
If the floor area is manually meshed in irregular
pattern and the different pattern loading is to be assigned, the edge of area elements should be aligned along the border of the pattern loading.
ACECOMS, AIT 19
Edit Point - Merge
Select the points to merge
Merge tolerance must be greater than distance between the points
Edit Point - Align
Live load = 2 kN/m2 Live load = 5 kN/m2
To assign different pattern loading on irregular shaped
meshed floor
Draw the line along the border of pattern
loading. Select the line and the points to
be aligned
The floor elements are aligned along the
border of different pattern loading
Edit Lines
Divide frames
Join frames
Trim/Extend frames
Edit curved frame geometry
Edit cable geometry
Edit tendon profile
Edit Lines
Divide frames
Divide the frame intersect with selected frames.
Select the frame object to bed divided and select the
intersecting objects
Join frames
ACECOMS, AIT 21
Edit Areas - Divide
Divide into the number of objects specified
using the edit box for each edge.
Edit Areas - Divide
Divide area into objects of given maximum
size
Edit Areas - Divide
Divide area based on points on area edges
Divide based on specified lines and points. Program will not extend the selected line to make it intersect an edge; the selected line must already intersect an edge of the selected area object. The selected point must also intersect an edge of the selected object, not inside the selected object.
Edit Areas - Divide
Divide area using cookie cut based on selected straight
line objects
The selected line object does not need to intersect with the edge of the selected area object .
ACECOMS, AIT 23
Edit Areas - Divide
Divide area into given number of objects
The selected point object must lie either on the edge or inside the selected area object. The rotation in degrees of dividing lines can be specified from original local 1 and 2 axes.
Edit Areas - Divide
Divide area using general divide tool based on selected
points and lines
Divide the area object based on specified maximum dimension. The division lines intersect the selected points and concurrent
Edit Areas - Divide
Local axes for added points
Specify that the local axes definitions for new
points added along the edges of an area
object are the same as an adjacent area
object corner point if the local axes definition
for the adjacent corners are identical.
Specify that the local axes definition for the
new points on the face of the area object are
set the same as a corner point of the area
object if the local axes definitions for all of the
corner points of the area object are identical.
Edit Areas - Divide
Added points on the edge of original element have the same local axes with original element. If the second check box is checked, local axes of added points on the face of original element will be same.
ACECOMS, AIT 25
Edit Areas - Divide
Restraints and constraints for added points
Specify that a restraint degree of freedom (or
constraint) is added to new points on the edges of the area object if both adjacent corners have that degree of freedom restrained (constrained) and the local axes definitions for the adjacent corners and the new point are identical.
Specify that a restraint degree of freedom (or
constraint) is added to new points on the face of the area object if all area object corners have that degree of freedom restrained (constrained) and the local axes definitions of all corners and the new points are
identical.
Edit Areas - Divide
Added points on the edge of original element have the same restraints with original element. If the second check box is checked, restraints of added points on the face of original element will be same.
Edit Areas-Merge
Selected areas essentially in the same plane and sharing a common edge or with overlapping area edges will be merged.
Areas that lie one on top of the other or that share no common or overlapping edges will not be merged.
Choose an area that has assignments suitable for the merged area.
Edit Areas-Merge
Area 6
Area 7
Maintain the assignments for Area 7
ACECOMS, AIT 27
Edit Areas
Expand/Shrink areas
A positive value expands the area and a negative value shrinks the area.
The offset distance is measured perpendicular to the area edge.
100 100
100
100
Offset all area edges
Select the edge or whole area
Edit Areas
Offset selected area edges only Select the edge
Edit Areas
Offset selected points of selected areas only 100
Select the point and area The offset for points is measured along a bisector angle formed by the area edges adjacent to the
selected point(s).
Edit Areas
Add point to area edge
Add points to the edges at the midpoint between the
existing points of the selected object.
This procedure can do repeatedly as many times as
ACECOMS, AIT 29
Edit Areas
Remove points from area
Select the area and the point to be removed.
If the point was not colinear with the remaining points,
the area object will be reshaped.
Special Tools
Basic Modeling Techniques
-Behavior
Constraints
Restraints
Springs
Nonlinear Links
Nonlinear Hinges
Element End Conditions
Dummy elements
Link/Support Element
A Link element is a two-joint connecting link.
A Support element is a one-joint element
Support Element Link Element
ACECOMS, AIT 31
Link/Support Element
Type of Link/Support Element available in ETABS
Linear Damper Gap Hook Plastic1 Isolate1 Isolate2
Link/Support Element
Damper Element
Gap Element
Compression only (for example Spread Footing)
Hook Element
Diaphragms
In ETABS: Only diaphragms is available as
constraint option for joint and shell element
Diaphragms
Rigid Option
ACECOMS, AIT 33
Diaphragms
Semi Rigid Option:
The in-plane rigidity of the diaphragm comes
from the stiffness of the objects that are part of
the diaphragm
Used to calculate the dimension of diaphragm in
application of the wind/static equivalent
earthquake loading
Select and Assign
Select and Assign
Many tools to select the drawn objects
Many types of assignments
Sections
Loads, Temperature, Joint Patters
Constraints, Restraints, Releases
Special modifications
Axis, Insertion Points, Offsets
Local material changes
Analyze and Understand
ACECOMS, AIT 35
Analysis Case
Static
Linear Static
Nonlinear Static (Included Push Over)
Staged Construction
Response Spectrum
Time History
Linear Time History
Nonlinear Time History
Analysis Case
Static
:
Linear: The most common type of analysis.
Loads are applied without dynamical effects.
Nonlinear: Loads are applied without
dynamical effects. May be used for pushover
analysis, and other types of nonlinear
problems. (Pushover + P-Delta)
Nonlinear Staged Construction: The definition
of a nonlinear direct-integration time-history
analysis case for staged construction.
Analysis Case
1 2 3 Nonlinear Staged ConstructionAnalysis Case
Modal:
Calculation of dynamic modes of the structure using the Eigenvector or Ritz-vector method. Loads are not actually applied, although they can be used to generate Ritz vectors.
ACECOMS, AIT 37
Analysis Case
Response Spectrum
.
Statistical calculation of the response caused by
acceleration loads. Requires response-spectrum
functions.
Response Spectrum Function
Analysis Case
Time History:
Linear Time History. Time-varying loads are applied.
Requires time-history functions. All objects behave linearly.
Period. Specify a single cycle of the periodic function
and assumes that the specified cycle continues indefinitely. All objects behave linearly.
Nonlinear Time History. Time-varying loads are
applied. Requires time-history functions. Nonlinear dynamic properties assigned to link elements are considered.
Pushover Analysis
Pushover Analysis
Available Hinge Properties
Axial P
Shear V2
Shear V3
Moment M2
Moment M3
Torsion T
Interaction P-M2-M3
ACECOMS, AIT 39
Pushover Analysis
Hinge Property Data
Displacement Controlled
Pushover Analysis
Pushover Curve Resultant Base Shear vs Monitored DisplacementPushover Analysis
Pushover Curve
ATC-40 Capacity Spectrum ATC-40 Capacity Spectrum
Show Response Spectrum Curve
Create from Time History Case at Particular
Joint
Frequency or Period
Versus
Spectral Displacement
Spectral Velocity
Pseudo Spectral Velocity
Spectral Acceleration
ACECOMS, AIT 41
Show Plot Function
Energy Function
Input, Kinetic, Potential Modal Damping
Link Damper, Energy Error
Base Function
Joint Displacement/Forces
Frame Forces
Pier Forces
Spandrel Forces
Show Plot Function
Displacement Function Base Function
Energy/ Virtual Work Function
Figure "a," that has lateral loads P1 and P2 at the Roof and Second story levels, respectively. Also note the displaced shape, D, associated with this structure and loading, which is shown as a dashed line.
Energy/ Virtual Work Function
Figure "b", with a single load P (typically a unit load) applied to it and a resulting displaced shape, d, shown as a dashed line. Maxwell's Reciprocal Theorem states that:
ACECOMS, AIT 43
Energy/ Virtual Work Function
In this very simple example, the equation above could be reduced to an element level where the elements are illustrated in Figure "c" as:
P δ= [P1δ roof- P1δ second] + [(P1 + P2)δ second]
Energy/ Virtual Work Function
P δ= [P1δ roof - P1δ second] + [(P1 + P2)δ second] ETABS show the energy diagram, it reports the equivalent of the values shown in brackets in the above equation of the background information for each element in the structure.
Note the following about the energy values that ETABS reports:
Energy/ Virtual Work Function
P δ= [P1δ roof - P1δ second] + [(P1 + P2)δ second] They are based on all six degrees of freedom of the element, not just the one degree of freedom described in the Figure and the associated equations in the background information.
They are determined as follows:
ETABS determines the energy per unit volume
associated with each element in the structure.
ETABS normalizes all of the calculated energy values
such that the largest one has a value of 100.
Energy/ Virtual Work Function
ACECOMS, AIT 45
Time History Traces
Available Functions for Time History Traces
Input Function
Energy Function
Base Function
Point Displacement/ Forces
Line Element Forces
Pier Forces
Spandrel Forces
Time History Traces
Time History Traces
Energy Function
Time History Traces
ACECOMS, AIT 47
Time History Traces
Base Function = Total Base Reaction Function
Time History Traces
Point Displacement/ Forces
Line Element Forces
Pier Forces
Spandrel Forces
Displacement/ Forces at Particular Element and
Location
Time History Traces
Point Displacement/ Forces
Line Element Forces
Pier Forces
Spandrel Forces
Displacement/ Forces at Particular Element and
Location Element ID Force Component Location
Outrigger System
Outrigger No OutriggerACECOMS, AIT 49
Shear Force in Beams due to Lateral
Load (No Outrigger Wall)
3.14 T 3.25 T 4.24 T
Shear Force in Beams due to Lateral
Load (Outrigger Wall)
Axial Force in Columns due to
Lateral Load (No Outrigger Wall)
623 T 350 T 383 T
Axial Force in Columns due to
Lateral Load (Outrigger Wall)
ACECOMS, AIT 51
Bending Moment due to Lateral Load
(No Outrigger Wall)
8.3 8.6 11.3
40.2 38.3 36.9
Bending Moment due to Lateral Load
(Outrigger Wall)
6.9 6.4 7.9
Top Displacement due to Lateral
Load
Top Displacement = 75 cm Top Displacement = 40 cm
ACECOMS, AIT 53
Construction Sequence Analysis
Deflected Shape due to DL
(Linear Analysis) Deflected Shape due to DL (Construction Sequence Analysis)
Construction Sequence Analysis
Axial Force due to DL at the Base (Linear Analysis)
Axial Force due to DL at the Base (Construction Sequence Analysis)
Construction Sequence Analysis
Bending Moment due to DL (Linear Analysis)
Bending Moment due to DL (Construction Sequence Analysis)
11.3 12.4