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    Development of the Strut-and-Tie Method for A endix A of

    James K. Wight

    the Building Code (ACI 318-08)

    University of Michigan

    Strut and Tie Modeling

    be designed by idealizing the concrete

    and reinforcement as an assembly of

    axially loaded members, inter-

    connected at nodes, to form a truss

    capable of carrying loads across aregion or member.

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    Components of Strut and Tie Models

    Steps to Build Strut & Tie Model

    -

    Compute forces or distribution of

    stresses on boundary

    Represent stress distributions as forces

    forces across the member or D-region

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    Concept of D-Regions

    (force discontinuities)

    h

    h 2h

    Concept of D-Regions(geometric discontinuities)

    h2h1

    1 2

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    Basic Requirements

    Model approximates stress flow

    Define component dimensions and

    strengths

    Define and factors

    Select reinforcement details

    Modeling Stress Flow

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    Modeling Stress Flow in D-Regions(Dapped Beam)

    How to Select the CorrectStrut-and-Tie Model

    Some researchers suggest using a finite

    element model to determine stress

    trajectories, then selecting a STM to

    model the stress flow.

    ,required amount or reinforcement is

    close to an ideal model.

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    Required Definitions for Code

    Geometric rules to follow when creating

    a strut-and-tie model.

    Component strengths for determining

    members sizes and final geometry of

    .

    Other Codes with Rules for Useof Strut-and-Tie Models

    AASHTO LRFD Specification

    Canadian Code for Design of Concrete

    Structures (CSA Standard, 2004)

    ecommen a ons orPractical Design of Structural Concrete

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    Strength of Compression Struts

    (what to consider)

    Longitudinal cracking due to transverse

    tension strain

    Transverse tension forces

    Sustained loads

    Reinforcement grid crossing strut

    Confinement by concrete or steel

    Lateral Expansion of Strut

    (bottle-shaped strut)

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    Effective Compressive Strength of Struts

    ns uF F

    0.75 =

    ns cu cF f A=

    min. cross-sectional area of strutcA =

    s .cu c=

    AASHTO and CSA Evaluation ofEffective Concrete Strength

    Trans. tension strain,1= (s + 0.002) cot2s

    1

    0.850.8 170

    cs c c

    ff f

    =

    +

    s = angle between strut and tie (steel)

    s = strain in steel tie

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    FIP Recommendations fors in

    Cracked Struts

    0.80 - struts with longitudinal cracking

    (splitting), but crossed by minimum

    reinforcement grid

    0.75 - struts crossed by normal width

    0.60 - struts crossed by wide cracks

    ACI Recommended s Values for Struts

    1.0 prismatic shape (constant width) over its,

    in a B-region

    0.75 inclined (bottle-shaped) strut crossedby minimum reinforcement grid

    0.60 inclined bottle-shaped strut notcrossed by minimum reinforcement grid;

    where accounts for lightweight concrete 0.40 struts in flexural tension zones

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    Struts in a Flexural Tension Zone

    A

    A

    Sect. A-A

    Minimum Reinforcement Grid (fc

    6000 psi)

    Strut centerline2

    12

    1

    sii

    i

    A in 0.003b s

    s (A 4)

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    Reinforcement Grid

    (only horizontal bars)

    Min. Reinf. Grid in other Codes

    AASHTO 0.003 EW

    CSA 0.002 EW

    FIP 0.001 EF, EW

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    Modification for Higher

    Strength Concrete

    (41 MPa), must calculate required

    amount of transverse reinforcement

    crossing strut.

    This procedure can result in a

    significant difference when compared to

    requirements of ACI Eq. (A-4).

    Modification for HigherStrength Concrete

    =

    2 longitudinal/1 transverse

    equ re ransversetie capacity = 50%

    of strut strength

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    Tie Dimensions

    Full width (out or plane) of member

    Width (in plane) of tie is function ofeffective compression strength ofconcrete in nodes where tie is anchored

    dimensions

    Tie - Dimensions and Strength

    Asfy

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    Strength of Ties

    Strength = As fy, where = 0.75*

    Anchorage of ties at nodes is a major

    concern

    *A constant value of = 0.75 is to be used for

    sizing the strut-and-tie model, but the use of

    = 0.75 to also select the reinforcement mayneed further examination within the appropriate

    Code subcommittee.

    Anchorage Check

    Definition of Extended Nodal Zone

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    Nodal Zone Shape and Dimensions

    Width of compression face is same as

    width of strut connecting to nodal zone

    (smaller allowable strength governs)

    Height (width of face perpendicular to

    tie force) of nodal zone is equal to tie

    force divided by effective compressivestrength of the concrete in the node

    Node Shape and Size

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    Effective Strength of Nodal Zones

    Function of type of members connected

    to the node

    Possible combinations are CCC, CCT

    and CTT

    Strength can be enhanced by addition

    of confinement reinforcement

    Examples of CCC and CCT Nodes

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    Examples of CCT and CTT Nodes

    Examples of CCT and CTT Nodes

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    Strength of Nodes

    nn uF F

    0 75 0.75 =

    nn cu nF f A=

    n uA area of node face to force F=

    n0.85

    cu cf f =

    Recommended n Values (Nodes)

    1.0 - CCC node

    . -

    0.6 - CTT node

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    Use of STM in the ACI Code

    - .However,

    Is listed as alternate procedure inseveral sections of the code (e.g.corbels, short shear walls).

    Currently required for shear strength

    design of deep beams.

    640 k (includes member weight)

    All member widths = 20 in.

    Example: ACI Concrete International

    Magazine, May 2003

    dv60 in.

    .

    53 in. 107 in. 212 k428 k

    16 in. 16 in.

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    640 k

    All member widths = 20 in.

    Beam Dimensions and Initial Truss Model

    dv60 in.

    .

    53 in. 107 in. 212 k428 k

    16 in. 16 in.

    Check Max. Allowable Shear Force

    =.

    Max. All. Shear Force = 10

    4000(max) 0.75 10 20 54 512 k (o.k.)

    1000

    c w

    n

    f b d

    V

    = =

    Assumed thatd0.9h

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    212 k428 k

    Splitting of Node 2

    dv

    =

    ?

    1

    2

    3

    4 51 = 42.2

    o2 = ? 2

    49.7 in. 50.2 in. 50.2 in.

    10 in.428 k 212 k

    Establish Truss Geometry: Start withleft portion of the beam

    Assumes heights of Nodes 1 & 2 = 15 in.

    Thus, dv= 60 in. 2(7.5 in.)

    = 45 in. (1140 mm)

    From eometr :

    tan 1 = (45in./49.7in.),

    And thus 1 = 42.2 deg.

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    212 k428 k

    Initial Truss Geometry

    dv

    =

    45

    in.

    1

    2

    3

    4 51 = 42.2

    o2 = ? 2

    49.7 in. 50.2 in. 50.2 in.

    10 in.428 k 212 k

    Establish Equilibrium at Node 1

    12

    F14Fy = 428 - F12sin 1 = 0

    F12 = 637 k

    428 kFx = F14 F12cos 1 = 0

    F14 = 472 k

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    Geometry and dimensions of Node 1

    and Strut 1-2

    14

    b1

    1

    Establish/Check Dimensions at Node 1

    fcu(1) = (0.85) n fc'= 0.750.850.804

    1

    428( ) 1.34 ksi (o.k.)

    20 16w b

    Rf base

    b= = =

    l

    l

    = 2.04 ksi

    1414

    472 11.6 12 in.(1) 20 0.75 2.72w cu

    Fwb f

    = = =

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    Establish/Check Width and Strength of

    Strut 1-2

    ( ) ( )12 14 1 1 1

    12

    cos sin

    8.89 10.8 19.7 in.

    bw w

    w

    = +

    = + =

    l

    (1-2) 0.85 0.85 0.75 4 2.55 ksicu s cf f = = =

    12(1-2) (1-2)(1-2) 0.75 2.55 19.6 20 757 k 637 k (o.k.)

    ns cu w

    ns

    F f w bF

    = = =

    Modified Truss Geometryand Member Forces

    Thus, height of Node 1 = 12 in.

    Because Node 2 is a CCC node, assume

    it has a total height of 10 in.

    , v= = .

    Reestablish truss geometry and member

    forces!

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    212 k428 k

    Final truss geometry and member forces

    dv

    =

    49

    in.

    434 k 217 k

    217 k

    1

    2

    3

    4 51 = 44.6

    o 2 = 44.3o

    2

    212

    k

    49.7 in. 50.2 in. 50.2 in.

    10 in.428 k 212 k

    Select Reinforcement for Tie 1-4

    214434

    ( .) 9.64 in.sF

    A req d = = =.

    y

    Select 13 No. 8 bars,

    As = 10.3 in.2

    3 in.

    20 in.

    3 in.

    3 in.

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    Check Anchorage at Node 1

    Tie 1-4

    a = 6 in./tan1a = 6.09 in.

    b1 = 16in. a

    Critical section

    1 6in.

    Length 22.1 in.

    Check Anchorage at Node 1

    0.02 0.02 1 60, 0001.0 in.

    e yf

    d

    = = l

    b

    1 4000

    19.0 in. (> 8d and > 6 in.)

    c

    dh

    f

    =l

    Although dh is less than 22 in., this would be a tight fit if

    only 90 hooks were used. In-plane 180 hooks could be

    used for some bars to partially relieve this rebar detailingproblem. The use of mechanical anchorage devices could

    also be considered.

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    Minimum Reinforcement Crossing Strut 1-2

    Strut centerline2

    12

    1

    sii

    i

    A in 0.003b s

    s

    Minimum Reinforcement CrossingStrut 1-2 for s = 0.75

    and width of cracks crossing the strut.

    Because this is a deep beam, I recommend

    that you also satisfy ACI Code Sections

    11.7.4 and 11.7.5.

    , ,the minimum skin reinforcement requirements

    of ACI Code Section 10.6.7 must be satisfied.

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    2 #4

    per layer

    3 in.Final design

    in left span

    Four #4 legs6 at 8 in.

    3 at 3 in.

    20 in.

    13 #8

    212 k428 k

    Comments on right half of truss

    dv

    =

    49

    in.

    434 k 217 k

    217 k

    1

    2

    3

    4 51 = 44.6

    o 2 = 44.3o

    2

    212

    k

    49.7 in. 50.2 in. 50.2 in.

    10 in.428 k212 k

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    22in.60in.

    Analysis of fan-shaped struts 2-4

    and 3-5, and tie 3-4

    2

    49in.

    25o

    25o

    3

    5

    104 in.

    22in. six stirrups at s = 10 in.

    4

    Section A

    Final design of longitudinal andtransverse steel

    5 at 10 in. 15 at 6 in.

    2 in. 2 in.

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    Gracias

    Preguntas?