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Part 12 Final

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    Civl512/Mech 539Finite Element MethodsFinite Element Modeling of Building Structures

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    Overall Design ProcessOverall Design Process

    Conception

    Modeling

    Analysis

    Design

    Detailing

    Drafting

    Costing

    IntegratedIntegratedDesignDesign

    ProcessProcess

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    Building Systems

    Building is an assemblage of various Systems

    Basic Functional System

    Structural System

    Plumbing and Drainage System

    Electrical, Electronic and CommunicationSystem

    Security System Other specialized systems

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    Beams, Columns, One-way/Two-way Slabs, Flat Slabs,

    Transfer Plates, Shear Walls, Deep Beams

    Sub-structure and Member Design

    Frame and Shear WallsLateral Load Resisting System

    Floor Slab SystemGravity Load Resisting System

    Building Structure

    Floor Diaphragm

    The Building Structural System - Physical

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    The Building Structural System - Conceptual

    The Gravity Load Resisting System (GLRS)

    The structural system (beams, slab, girders, columns, etc)that act primarily to support the gravity or vertical loads

    The Lateral Load Resist ing System (LLRS)

    The structural system (columns - tubular structure, shear

    walls, bracing, etc) that primarily acts to resist the lateralloads

    The Floor Diaphragm (FD)

    The structural system that transfers lateral loads to thelateral load resisting system and provides in-plane floorstiffness

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    Building Response

    Objective: To determine the load path for gravity and lateral loads

    For Gravity Loads - How Gravity Loads are Distributed

    Analysis of Gravity Load Resisting System for:

    Dead Load, Live Load, Cladding Loads, temperature,

    shrinkage, creep

    Important Elements: Floor slabs, beams, columns, openings,J oists, etc.

    For Lateral LoadsHow Lateral Loads are Distributed

    Analysis of Lateral Load Resisting System for:

    Wind Loads, Seismic Loads, Structural Un-symmetry

    Important elements: Columns, shear walls, bracing , beams

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    Structural Response To LoadsStructural Response To Loads

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    STRUCTURE

    pv

    EXCITATION

    Loads

    Vibrations

    SettlementsThermal Changes

    RESPONSES

    Displacements

    Strains

    StressStress Resultants

    Structural System

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    Analysis of Structures

    pv

    xx yy zzvxx y z

    p+ + + = 0

    Real Structure is governed by Partial

    Differential Equations of various order

    Direct solution is only possible for:

    Simple geometry Simple Boundary

    Simple Loading.

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    We would like to predict the structural response before

    the structure is being constructed

    Real structure are not available for analysis

    We therefore need tools to Model the

    Structure and to Analyze the Model

    The Need for Modeling

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    StructuralModel

    The Need for Structural Model

    EXCITATION

    Loads

    Vibrations

    SettlementsThermal Changes

    RESPONSES

    Displacements

    Strains

    StressStress Resultants

    STRUCTURE

    pv

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    Finite Element Analysis (FEA)

    A discretized solution to a continuum

    problem using FEM

    Finite Element Method (FEM)

    A numerical procedure for solving (partial)

    differential equations associated with fieldproblems, with an accuracy acceptable to

    engineers

    Throughout the semester, you have alreadylearnt the foundation of FEM:-

    - The matrix structural analysis technique

    - Different element types for FEM

    Finite Element Method: The Analysis Tool

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    (Governed by partial

    differential equations)

    CONTINUOUS MODEL

    OF STRUCTURE

    (Governed by either

    partial or total

    differential equations)

    DISCRETE MODEL

    OF STRUCTURE

    (Governed by algebraic

    equations)

    3D-CONTINUM

    MODEL

    Continuum to Discrete Model

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    xx yy zz

    vxx y zp+ + + =0

    t

    v

    t

    s

    t

    vdV p udV p uds

    _ _ _

    = +

    Assumptions

    Equilibrium

    Compatibility

    Stress-Strain Law

    (Principle of Virtual Work)

    Partial

    Differential

    Equations

    Classical

    Actual Structure

    Kr R=

    Algebraic

    Equations

    K = Stiffness

    r = Response

    R = Loads

    FEM

    Structural Model

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    Simplified Structural System

    Loads (F) Deformations (D)

    Fv

    F = K DF = K D

    FF

    KKDD

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    EXCITATION RESPONSES

    STRUCTURE

    pv

    Static

    Dynamic

    Static

    Dynamic

    Elastic

    Inelastic

    Elastic

    Inelastic

    Linear

    Nonlinear

    Linear

    Nonlinear

    Simplified Structural System

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    Static Vs Dynamic Static Excitation

    When the Excitation (Load) does not vary rapidly with Time When the Load can be assumed to be applied Slowly

    Dynamic Excitation

    When the Excitation varies rapidly with Time

    When the Inertial Force becomes significant

    Most Real Excitation are Dynamic but are consideredQuasi Static

    Most Dynamic Excitation can be converted toEquivalent Static Loads

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    Elastic Vs Inelastic Elastic Material

    Follows the same path during loading and unloading andreturns to initial state of deformation, stress, strain etc.after removal of load/ excitation

    Inelastic Material

    Does not follow the same path during loading andunloading and may not returns to initial state ofdeformation, stress, strain etc. after removal of load/excitation

    Most materials exhibit both, elastic and inelastic behaviordepending upon level of loading.

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    Linear Vs Nonlinear Linearity

    The response is directly proportional to excitation

    (Deflection doubles if load is doubled)

    Non-LinearityThe response is not directly proportional to excitation

    (deflection may become 4 times if load is doubled)

    Non-linear response may be produced by:

    Geometric Effects (Geometric non-linearity) Material Effects (Material non-linearity)

    Both

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    Action

    Deformation

    Action

    Deformation

    Action

    Deformation

    Action

    Deformation

    Linear-Elastic Linear-Inelastic

    Nonlinear-Elastic Nonlinear-Inelastic

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    Basic Steps in FEAasic Steps in FEAEvaluate Real Structure

    Create Structural Model

    Discretize Model in FE

    Solve FE Model

    Interpret FEA Results

    Physical significance of Results

    Engineer

    Engineer + Software

    Software

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    X

    Z

    Y

    Membrane/ PanelIn-Plane, Only Axial

    ShellIn-Plane and Bending

    Plate/ SlabOut of Plane, Only Bending

    General Solid

    Regular Solid

    Plate/ Shell

    ( T small compared to Lengths )

    ( Orthogonal dimensions)

    Beam ElementSolid Element

    H, B much less than L

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    Global Modeling of StructuralGeometry

    (b) Solid Model (c) 3D Plate-Frame (d) 3D Frame

    (a) Real Structure

    (e) 2D Frame

    Fig. 1 Various Ways to Model a Real Struture

    (f) Grid-Plate

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    1 D Elements (Beam type)

    Can be used in 1D, 2D and

    2D

    2-3 Nodes. A, I etc.

    2 D Elements (Plate type)

    Can be used in 2D and 3DModel

    3-9 nodes. Thickness

    3 D Elements (Brick type)

    Can be used in 3D Model

    6-20 Nodes.

    Truss and Beam Elements (1D,2D,3D)

    Plane Stress, Plane Strain, Axisymmetric , Plate and Shell Elements (2D,3D)

    Brick Elements

    Dimensions of Elements

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    11

    33

    22

    33

    22

    ++

    PP+V2+V2

    +V3+V3

    +V3+V3

    +V2+V2+P+P

    11

    33

    22

    33

    22

    ++

    TT+M2+M2

    +M+M

    33

    +M+M

    33

    +M+M

    22 +T+T

    Frame Six DOF at Both Ends

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    Ignore bending stiffness

    Tension / Compression

    In- plane Shear

    For in plane loads

    Principle Stresses

    suitable for very thinstructures / members

    Thin Walled Shells,

    Specially Suitable for FerroCement Structure

    Membrane

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    Membrane ElementGeneral

    Total DOF per Node = 3 (or 2)

    Total Displacements per Node = 2

    Total Rotations per Node = 1 (or 0)Membranes are modeled for flat surfaces

    Application

    For Modeling surface elements carryingin-plane loads

    Building Specific Application

    For representing floor slabs for Lateral

    Load Analysis.

    Model Shear walls, Floor Diaphragm

    etc

    Membrane

    U1

    Node 1

    R3U2

    U1

    Node 3

    R3 U2

    U1

    Node 4

    R3

    U2

    U1

    Node 2

    U2

    3 2

    1

    Membrane

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    1 unit

    330

    230

    130

    22

    12

    11

    x1

    x3

    x2

    3D Problem

    2D Problem

    Plain-Strain

    Assumptions

    12

    22

    11

    x2

    x1

    Plane Stress ProblemPlane Strain Problem

    Plane Stress and Plane Strain

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    Primarily Bending mode

    Moment and Shear arepredominant

    Suitable for moderately

    thick slabs and plates

    For Out-of-plane loads only

    Can be used in 3D or 2D

    models

    Suitable for planks andrelatively flat structures

    Plate

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    Plate ElementGeneral

    Total DOF per Node = 3

    Total Displacements per Node = 1

    Total Rotations per Node = 2

    Plates are for flat surfaces

    Application

    For Modeling surface elementscarrying

    out of plane loads

    Building Specific ApplicationFor representing floor slabs for

    Vertical

    Load Analysis

    Model slabs

    R1

    Node 1

    U3R2

    1

    23

    R1

    Node 2

    U3R2

    R1

    Node 3

    U3 R2

    R1

    Node 4

    U3 R2

    Plate

    Plate

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    Combined Membrane andPlate

    Suitable for general applicationto surface structures

    Suitable for curved structures

    Thick shell and thin shell

    implementations available Membrane thickness and plate

    thickness can be specifiedseparately

    Numerous results generated.Difficult to design the sectionfor combined actions

    Plate-Shell

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    General

    Total DOF per Node = 6 (or 5)

    Total Displacements per Node = 3

    Total Rotations per Node = 3

    Used for curved surfaces

    Application

    For Modeling surface elementscarrying general loads

    Building Specific Application

    May be used for modeling of generalslabs systems. But not used generally

    1

    23

    U1, R1Node 3

    U3, R3

    U2, R2

    U1, R1

    Node 1

    U3, R3 U2, R2

    U1, R1

    Node 4

    U3, R3

    U2, R2

    U1, R1

    Node 2

    U3, R3

    U2, R2

    Shell

    Shell

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    Shear Axial deformation mode

    in 3D

    Suitable for micro-models Suitable for very thick plates /

    solids

    May not be applicable much toferocement structures

    Use 6 to 20 node

    elements

    Solid

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    Simple Supports

    Fix, Pin, Roller etc.

    Support Settlement

    Elastic Supports

    Spring to represent soil

    Using Modulus of Sub-grade

    reaction

    Full Structure-Soil Model Use 2D plane stress elements

    Use 3D Solid Elements

    Soil-Structure Interaction

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    OKOKDx, DzDzOKOKSolid

    Rx, RzOKDx, DzRx, Ry,

    Rz, DzOK

    Rx, Ry,

    Rz

    Shell

    Rx, RzOKOKRx, RzOKRx, RzPlate

    OKOKDx, DyOKOKOKMembrane

    Rx, Ry,

    RzRx ?

    Rx ?

    Dx, Dy

    Rx, Ry,

    Rz, DzOK

    Rx, Ry,

    Rz

    Frame

    OKOKOKDzOKOKTruss

    SolidShellPlateMembr

    ane

    FrameTruss

    0

    Orphan Degrees Of Freedom:

    1 2 3 4

    Connecting Different Types of Elements

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    Vertical Load Resisting SystemsVertical Load Resisting Systems

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    Purpose

    To Transfer Gravity Loads Applied at the Floor Levels

    down to the Foundation Level

    Direct Path Systems

    Slab Supported on Load Bearing Walls

    Slab Supported on Columns

    Indirect Multi Path Systems

    Slab Supported on Beams

    Beams Supported on Other Beams

    Beams Supported on Walls or Columns

    Gravity Load Resisting Systems

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    1. Slabs supported on Long Rigid Supports

    Supported on stiff Beams or Walls

    One-way and Two-way Slabs Main consideration is flexural reinforcement

    2. Slab-System supported on Small Rigid Supports

    Supported on Columns directly Flat Slab Floor systems

    Main consideration is shear transfer, moment distribution invarious parts, lateral load resistance

    3. Slabs supported on soi l

    Slabs on Grade: Light, uniformly distributed loads

    Footings, Mat etc. Heavy concentrated loads

    Vertical Load Resisting Systems

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    Direct Load Transfer Systems (Single load transfer path)

    Flat Slab and Flat Plate

    Beam-Slab

    Waffle Slab

    Wall J oist

    Indirect Load Transfer System (Multi step load transfer

    path)

    Beam, Slab

    Girder, Beam, Slab Girder, J oist

    Popular Gravity Load Resting Systems

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    For Wall Supported Slabs

    Assume load transfer in One-Way or Two-Waymanner

    Uniform, Triangular or Trapezoidal Load on Walls

    For Beam Supported Slabs

    Assume beams to support the slabs in similar waysas walls

    Design slabs as edge supported on beams

    Transfer load to beams and design beams for slab

    load

    For Flat-Slabs or Columns Supported Slabs

    Assume load transfer in strips directly to columns

    Conventional Approach

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    Popular Gravity Load Resting Systems

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    Single PathSlab On Walls

    Single PathSlab on Columns

    Dual PathSlab On Beams,

    Beams on Columns

    Gravity Load Transfer Paths

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    Mixed PathSlab On Walls

    Slab On Beams

    Beams on Walls

    Complex PathSlab on Beams

    Slab on Walls

    Beams on Beams

    Beams on Columns

    Three Step PathSlab On Ribs

    Ribs On Beams

    Beams on Columns

    Gravity Load Transfer Paths

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    Simplified Load Transfer

    Transfer of Area Load

    To Lines To Points To Lines and Points

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    Load Transfer Through Slab and Beam

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    Slab Deformation and Beams

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    5.0m

    Slab T = 200 mmBeam Width, B = 300 mmBeam Depth, Da) 300 mmb) 500 mmc) 1000 mm

    D

    B

    Slab System Behavior

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    Effect of Beam Size

    on

    MomentDistribution

    a) Beam Depth = 300 mm

    b) Beam Depth = 500 mmc) Beam Depth = 1000 mm

    Moment Distribution in Beam-Slab

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    Effect of Beam Size on Moment Distribution

    a) Beam Depth = 300 mm b) Beam Depth = 500 mm c) Beam Depth = 1000 mm

    Moment Distribution in Beam-Slab

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    By default uses two-way load transfer

    mechanism

    Simple RC solid slab

    Can also be used to model one way slabs

    Area Objects: Slab

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    Use one-way load transfer mechanism

    Metallic Composite SlabsIncludes shear studs

    Generally used in association with

    composite beams

    Deck slabs may be

    o Filled Deck

    o Unfilled Deck

    o Solid Slab Deck

    Area Objects: Deck

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    Lateral Load Resisting SystemsLateral Load Resisting SystemsLateral Load Resisting Systems

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    Purpose

    To Transfer Lateral Loads Applied at any location in the structure

    down to the Foundation Level

    Single System

    Moment Resisting Frames

    Braced Frames

    Shear Walls Tubular Systems

    Outrigger System

    Dual System Shear Wall + Frames

    Tube + Frame + Shear Wall

    Lateral Load Bearing Systems

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    Primary Lateral Loads

    Load generated by Wind Pressure

    Load generated due to Seismic Excitation

    Other Lateral Loads

    Load generated due to horizontal component ofGravity Loads in Inclined Systems and in Un-symmetrical structures

    Load due to lateral soil pressure, liquid and materialretention

    Lateral Load

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    Bearing wall system

    Light frames with shear panels

    Load bearing shear walls

    Fully Braced System (FBS)

    Shear Walls (SW)

    Diagonal Bracing (DB)

    Moment Resisting Frames (MRF) Special Moment-Resisting Frames (SMRF)

    Concrete Intermediate Moment-Resisting Frame (IMRF)

    Ordinary Moment-Resisting Frame (OMRF)

    Dual Systems (DS) Shear Walls + Frames (SWF)

    Ordinary Braced Frame (OBF)

    Special Braced Frame (SBF)

    Sample Lateral Load ResistanceSystems

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    The Load is transferred by

    shear in columns, that

    produces moment in columns

    and in beams

    The Beam-Column

    connection is crucial for the

    system to work

    The moments and shear fromlater loads must be added to

    those from gravity loads

    Moment Resisting Frame

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    Structural Form Rigid frame structure

    Low rise buildings

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    The Walls are part of the

    frame and act together with

    the frame members

    The lateral loads is primarily

    resisted by the shear in the

    walls, in turn producing

    bending moment.

    Partial loads is resisted by the

    frame members in moment

    and shear

    Shear Wall - Frame

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    Structural Form Wall frame structure

    Low to medium rise buildings

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    The lateral loads is primarily

    resisted by the Axial Force in

    the braces, columns and beamsin the braced zone.

    The frame away from the

    braced zone does not have

    significant moments

    Bracing does not have to be

    provided in every bay, but

    should be provided in every

    story

    Braced Frame

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    The system is formed by using

    closely spaced columns and deep

    spandrel beams

    The lateral loads is primarilyresisted by the entire building

    acting as a big cantilever with a

    tubular/ box cross-section

    There is a shear lag problembetween opposite faces of the tube

    due to in-efficiency of column beam

    connection

    The height to width ratio should bemore than 5

    Tubular Structure

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    Structural Form Tubular Structure

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    Diagonal Braces are added to

    the basic tubular structure This modification of the

    Tubular System reduces shear

    lag between opposite faces

    Braced Tube Systems

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    Structural Form Out-rigger Structure

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    1. 2D Frame Models

    Convert building in to several 2D frames in each direction Suitable for symmetrical loads and geometry

    2. 3D Frame Model

    Make a 3D frame model of entire building structure

    Can be open floor model or braced floor model3. Full 3D Finite Element Model

    A full 3D Finite Element Model using plate and beamelements

    4. Rigid Diaphragm Model

    A special model suitable for buildings that uses theconcept of Rigid Floor Diaphragm

    Modeling for Lateral Loads

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    Convert 3D Building to an assemblage of 2D Frames

    Using Independent Frames

    Using Linked Frames Using Sub-Structuring Concept

    Advantages

    Easier to model, analyze and interpret

    Fairly accurate for Gravity Load Analysis Main Problems:

    Center of Stiffness and Center of Forces my notcoincide

    Difficult to consider building torsional effects

    Several Frames may need to be modeled in eachdirection

    Difficult to model non-rectangular framing system

    Modeling as 2D Frame

    Create a Simple 2D ModelCreate a Simple 2D Model

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    1. Consider the

    Structure Plan and 3D

    View

    2. Select and

    isolate

    Typical 2D

    Structure

    4. Obtain results

    3. Discretize

    the Model,

    apply loads

    Using Linked FramesUsing Linked Frames

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    Plan

    Modeling

    Shear Wall

    Typical Frame

    Elevation

    Linked Elements

    Link Element can allow only to transmit the shear

    and axial force from one end to other end. It has

    moment discontinuity at both ends

    Link Element act as a member which links the forces

    of one frame to another frame, representing the effect

    of Rigid Floor.

    F3

    F2

    F1

    F1

    F2 F3

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    The columns and beams are modeled by using beamelements

    The slabs and shear walls are modeled by using shellelements

    Enough elements in each slab panel must be

    used if gravity loads are applied to the slabs If the model is only for lateral analysis, one

    element per slab panel may be sufficient to modelthe in-plane stiffness

    Shear walls may be modeled by plate or panel orplane stress element. The out of plane bending isnot significant

    Full 3D Finite Element Model

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    Example:

    Uses more than 4000beam and plate elements

    Suitable for analysis for

    gravity and lateral loads

    Results can be used fordesign of columns and

    beams

    Slab reinforcement

    difficult to determinefrom plate results

    Full 3D Finite Element Model

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    Use Plate

    Elements

    Use Diagonal

    Bracing Use Plate Elements

    Panels, Plane Stress

    Use Diagonals

    In 3D Frame Models

    Use Conceptual Rigid Diaphragm

    Link Frames in 2D

    Master DOF in 3D

    Use Approximately

    Modeling of Floor Diaphragm

    The Rigid Floor Diaphragm

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    Combines the simplicity and advantages of the 2D Frame

    models with the accuracy of the 3D models

    Basic Concept:

    The building structure is represented by vertical units (2DFrames, 3D Frames and Shear Walls), connected by the

    invisible rigid diaphragmThe lateral movement of all vertical units are connected to

    three master degree of freedom

    This takes into account the building rotation and its effect

    on the vertical units.The modeling and analysis is greatly simplified and made

    efficient

    The Rigid Floor Diaphragm

    Rigid Floor Diaphragm Concept

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    Modeled as Rigid Horizontal Plane of infinite

    in-plane stiffness (in X-Y plane) Assumed to have a hinge connection with

    frame member or shear wall, so flexural

    influence of all floors to lateral stiff ness is

    neglected

    All column lines of all frames at particular

    level can not deform independent of each

    other

    The floor levels of all frames must be at the

    same elevation and base line, but they need

    not have same number of stories

    Rigid Floor Diaphragm Concept

    How RFD Concept Works

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    UL

    UL1

    UL2

    UL3

    X

    Y

    F3 , 2

    F1 ,1

    F3 ,3

    uilding d.o.f.s

    F2 , 1

    r x

    r rY

    Local Frame DOF

    How RFD Concept Works

    When Single Rigid Floor Cannot be Used

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    When Single Rigid Floor Cannot be Used

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    MeshingMeshingMeshing

    Basic Floor Modeling Object

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    Points

    Columns

    Load Points Boundary Point

    Lines

    Beams

    Areas Deck: Represents a Steel Metal Deck, One way Load Transfer

    Slab: Represents one-way or two-way slab portion

    Opening: Represents Openings in Floor

    Basic Floor Modeling Object

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    Meshing Slabs and Walls

    In general the mesh in the slabshould match with mesh in the

    wall to establish connection

    Some software automaticallyestablishes connectivity by

    using constraints or Zipper

    elements

    ZipperZipper

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    ETABS automatically meshes all line objects with frame sectionproperties into the analysis model

    ETABS meshes all floor type (horizontal) area objects (deck or slab)into the analysis model

    Meshing does not change the number of objects in the model

    To mesh line objects with section properties use Edit menu > DivideLines

    To mesh area objects with section properties use Edit menu > MeshAreas

    Basic Floor Modeling Object

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    Automatic Meshing of Line Objects

    Frame elements are meshed at locations where other frameelements attach to or cross them and at locations where point

    objects lie on them.

    Line objects assigned link properties are never automatically

    meshed into the analysis model by ETABS

    ETABS automatically meshes (divides) the braces at the point

    where they cross in the analysis model

    No end releases are introduced.

    Automatic Meshing

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    ETABS automatically meshes a floor-type area object up into four-sided (quadrilateral) elements

    Each side of each element of the mesh has a beam (Real orImaginary) or wall running along it

    ETABS treats a wall like two columns and a beam where the

    columns are located at the ends of the wall and the beam connectsthe columns.

    Each column is assumed to have four beams connecting to it

    The floor is broken up at all walls and all real and imaginary beamsto create a mesh of four-sided elements

    Automatic Meshing of Area Objects

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    LoadingLoadingLoading

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    Load Transfer Path For Gravity Loads Most loads are basically Volume Loads generated due to

    mass contained in a volume

    Mechanism and path must be found to transfer these loadsto the Supports through a Medium

    All types of Static Loads can be represented as:

    Point Loads

    Line Loads Area Loads

    Volume Loads

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    The Load Transfer Path The Load is transferred through a medium which may be:

    A Point

    A Line An Area

    A Volume

    A system consisting of combination of several mediums

    The supports may be represented as:

    Point Supports

    Line Supports

    Area Supports Volume Supports

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    Graphic Object RepresentationObject

    Line

    Area

    Volume

    Point LoadConcentrated Load

    Beam Load

    Wall Load

    Slab Load

    Slab Load

    Wind Load

    Seismic LoadLiquid Load

    Node

    Beam / Truss

    Connection Element

    Spring Element

    Plate Element

    Shell Element

    Panel/ Plane

    Solid Element

    Point SupportColumn Support

    Line Support

    Wall Support

    Beam Support

    Soil Support

    Soil Support

    Point

    LoadGeometry

    Medium

    Support

    Boundary

    ETABS uses graphic object modeling concept

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    ETABSETABSETABS

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    ETABS Nonlinear For nearly 30 years ETABS has been recognized as the

    industry standard for Building Analysis and DesignSoftware.

    ETABS is the solution, whether you are designing asimple 2D frame or performing a dynamic analysis of acomplex high-rise that utilizes non-linear dampers forinter-story drift control.

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    Objective By performing a finite element analysis on a structure:-

    Predict the top drift of the structure under differentload cases.

    Predict the critical forces acting on a particularelement.

    Predict the natural frequencies of the structure.

    Predict the dynamic performance.

    Design the member sizes to comply with the codesrequirement.

    Etc.

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    IntroductionGeneral procedure for computerized FEM

    modeling and analysis

    Study the structure Propose aims/objectives of structural analysis

    Select the type of analysis Select the computer package to perform the

    analysis Define materials, element/section properties

    Draft the model Assign load cases Run the analysis and extract the useful data

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    ETABS Key Characteristics

    A wide variety of automated templates allow a quickstart for almost any building.

    Units that can be changed at any time.

    Fully integrated Section Designer allows definition ofcomplex sections.

    Static and dynamic, linear and nonlinear analysisoptions.

    Fully interactive design for American, Canadian andBritish design codes.

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    ETABS

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    AnalysisStaged construction(construction sequence loading)

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    AnalysisStatic Analysis

    Dynamic Analysis(Modal Analysis)

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    AnalysisDynamic response spectrum analysis

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    AnalysisTime history analysis

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    AnalysisNonlinear element analysis

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    OutputDeformed Shape

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    OutputBending moment, shear force, axial force diagrams

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    OutputStress contours

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    DesignSteel frame design(BS 5950)

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    DesignConcrete frame/ Composite beam/ Shear wall design(BS 8110)

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    Assumption in ETABSTo avoid instabilities and to reduce computational demand,

    ETABS assume some ideal conditions. These assumptionshave been proved to be valid in most cases but one shouldalways check against these assumptions when dealing withspecial structures.

    Rigid Floor Diaphragm

    End Pier

    P-delta Effect

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    Rigid Floor DiaphragmIn ETABS a rigid diaphragm translates within its own plane (global X-Y plane) androtates about an axis perpendicular to its own plane (global Z-axis) as a rigid body.Designating point objects as a rigid diaphragm has no effect on the out-of-plane

    behavior of the point objects.

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    End Pier

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    P-delta Effect

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    ETABS Example on using ETABS

    4 story building

    Steel frame structure

    1st story = 4.5m

    Remaining stories = 3.8m/story All slabs = 75mm thk.

    Cladding load =3.5kN/m

    Dead load = 1.5kN/m 2 Live load = 5kN/m 2

    Open New Model by selecting file -> New Model, select the unit KN,m,Cand select the

    template Grid Only. You are recommended to change the view to help yourselfidentify/draw your members, this can be done by selecting the appropriate view iconlocated along the top edge of the interface window

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    located along the top edge of the interface window.

    Introduction to interface

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    Introduction to interface

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    Drafting Commands

    Set Select ModeToggle to selection modeClick on element to selectDrag from left to right to select elements enclosed by the drag areaDrag from right to left to select elements touched by the drag areaClick on selected element to unselect

    Draw Frame/CableClick on the main window to assign ends of frame element(s)Select the pre-defined element from the Propertieswindow

    Quick Draw Frame/Cable

    Click on any grid line to assign frame element to the grid sectionDrag to assign frame elements to all enclosed empty grid lines

    Introduction to interface

    D fti C d

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    Drafting Commands

    Quick Draw Braces

    Quick Draw Secondary BeamsSelect the number of Secondary Beams assigned within the selectedarea, theconnection type and the orientation from the Propertieswindow

    Draw Quad AreaSelect 4 points to assign area element

    Draw Rectangular Area ElementSelect 2 corners to assign rectangular area element

    Quick Draw Area ElementSelect any point to assign area element enclosed by the nearest gridlines

    Introduction to interface

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    Drafting Commands

    The Selection Tools

    Select All (Ctrl + A)Get Previous SelectionClear SelectionSelect Using Intersecting Line

    Snap Tools

    Snap to Points and Grid IntersectionSnap to Ends and Midpoints

    Import UB & UC for BS Standard by selecting the Define -> Frame Sections.Select. Choose add auto-select list from the right and add all the available members to

    the list.

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    One can draw columns and beams one by one. However, for building structures, thesame floor plan usually applies to multi-stories. To draw elements on similar stories,select Edit -> Edit story data -> Edit story to open the window below, select story 4 asmaster story and all remaining stories as similar to story 4.

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    Add columns by selecting the create columns at click button on the left, make sure that theproperties of the columns have been set to the auto-select list. You may change the majoraxis direction by selecting Assign Frame/Lines Local Axis

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    Add beams by selecting the create lines at click button on the left, make sure that the

    properties of the beams have been set to the auto-select list.

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    Add secondary beams by selecting the create secondary beams at click button on the left,you make change the number of secondary beams with each bay on the properties window.

    To add the slab, select the Define -> Deck sections. Select Deck 1 and click on Modify.Change the type to solid slab and adjust the slab depth to 75mm

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    Add slab by selecting the draw area button on the left, you make change the number ofsecondary beams with each bay on the properties window. Make sure that the properties ofthe slab have been set to Deck 1

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    Before applying the load to the structure, one should create the load cases first, select thedefine static load case button on the top and define 3 types of loading, dead load, live load

    and the cladding load. Click on the plan view and make sure that the similar stories buttonis on, select the slab and choose assign -> shell area loads -> uniform command. Selectthe dead load and change the dead load to 1.5kN/m 2 and click on OK. Replete for the

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    the dead load and change the dead load to 1.5kN/m 2 and click on OK. Replete for the5kN/m 2 live load.

    Select the perimeter beams and select the assign -> frame/line load -> distributed load to

    assign the cladding loads.

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    After adding all the loads to the structure, you may now click the run analysis button to start

    your analysis.

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    Example

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    Example

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    Example

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    Example

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    Example

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    Example

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    Example

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    Example

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    Example

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