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  • 5/18/2018 PushOver

    1/30Push-over analysis for seismic performance evaluation of RC frame structures. Computer programsPush-over analysis for seismic performance evaluation of RC frame structures. Computer programs

    22ooCiclo de Palestras em Engenharia Civil-2003Ciclo de Palestras em Engenharia Civil-2003

    12 de Novembro de 200312 de Novembro de 2003

    niversidade Nova de !isboa-Centro de "nvestiga#ao em $struturas e Constru#%o-N"Cniversidade Nova de !isboa-Centro de "nvestiga#ao em $struturas e Constru#%o-N"C

    Push-over analysis for seismicPush-over analysis for seismic

    performance evaluation of RC frameperformance evaluation of RC framestructures. Computer programsstructures. Computer programs

    Dr. C. G. ChioreanDr. C. G. Chiorean

    Technical University of Cluj-Napoca, RomaniaTechnical University of Cluj-Napoca, Romania

    Bolseiro na UNL!CT, Lis"oa, #ortu$alBolseiro na UNL!CT, Lis"oa, #ortu$al

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    Part "".Part "".Computer programsComputer programs

    N$&C'(N$&C'( Computer program for large deflection elasto-plasticComputer program for large deflection elasto-plastic

    analysis of spatial frame structuresanalysis of spatial frame structures

    ')$P')$P Computer program for inelastic analysis of arbitraryComputer program for inelastic analysis of arbitrary

    reinforced and composite concrete sectionsreinforced and composite concrete sections

    OutlineOutline

    Part ".Part ".Push-over analysis for seismic performancePush-over analysis for seismic performance

    evaluation of spatial RC frame structuresevaluation of spatial RC frame structures

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    )tatic Nonlinear)tatic Nonlinearanalysis -analysis -Push-over 'nalysisPush-over 'nalysis*apro+imative solution,*apro+imative solution,

    Seismic performanceSeismic performance InelasticInelastic TypesTypes

    of analysisof analysis

    Nonlinear dynamic analysis- time history *final solution,Nonlinear dynamic analysis- time history *final solution,

    Vb

    !

    Push-over Curve

    "oadvs #eflection! $

    Vb

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    Nonlinear static procedure: constant gravitational loads and

    monotonically increasing lateral loads Plastic mechanisms and P-effects: diplacement or arc length

    control

    Capacity curve: Control node displacement vs base shear force

    Lateral load patterns: uniform, modal, SRSS, L! force

    distribution

    stimation of the target displacement: elastic or inelastic response

    spectrum for e"uivalent S#$! system

    Performance evaluation: global and local seismic demands %ith

    capacities of performance level&

    Key elements of the push-over analysisKey elements of the push-over analysis

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    Concentrated plasticity #istributed plasticity

    #imensionless plastic hinge

    'nteraction surface

    Return mapping plasticity

    algorithms Computationally efficient but limitedaccuracy

    Plastic (ones

    !orce-strain curves: "uasi plastic hingeapproach

    Stress-strain curves: fiber element approach Plastic flo% rules

    )igh accuracy but computational e*pensive

    Plastic hingePlastic (ones

    lastic lastic

    Inelastic analysis modelsInelastic analysis models

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    IP4IP3

    IP2

    j=IP5

    iPI1

    L+,

    L+,

    x

    z

    y

    ConcreteSteel

    Z

    Yx

    vi, Tiy

    wi, Tiz

    zj,Mzj

    xj,Mxj

    uj, Njvj, Tjy

    yi,Myi

    xi,Mxi

    ui, Ni

    zi,Mzi

    wj, Tjz

    z

    y

    N

    y

    !le*ibility-based nonlinear beam column element

    'terative method to compute inelastic response at cross-sectional level inelasatic

    fle*ural and a*ial rigidity.

    /radual yielding along the member length and %ithin the cross sections

    #istributed loads

    0niform or nonuniform tapered. members

    1ariation of reinforcement bars along the member

    $ne element+

    member

    3D RC Fier !eam Column "lement3D RC Fier !eam Column "lement

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    N2

    .

    y

    x

    ,,

    yx

    yxuxyu

    +=

    +=++=

    2rbitrary cross-sections under bia*ial bending moments and a*ial force

    2rc length icremental iterative method %ith tangent stiffness strategy/reen3s theorem: domain integrals are evaluated in terms of boundary integrals

    4-N-curves, N-4*-4y interaction diagrams and a*ial force ultimate curvature

    Inelastic analysis of cross-sectionsInelastic analysis of cross-sections

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    Large deflection and large rotations

    /eometrical local effects P-. including bo%ing effect, shear deformations

    Concentrated and distributed plasticity fiber and 4-N-aproaches.

    Consistency bet%een linear and nonlinear models one element+member.

    Local geometrical and material imperfections

    !le*ible semi-rigid. and finite 5oints

    Complete non-linear behavior pre and post crtical response: snap-bac6

    and snap-through.

    #odel capailities#odel capailities

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    lastic spectrum response: 7ype 8

    /round 7ype: 2

    Desi$n $roun% acceleration& #G'().*$

    +ass() )/ toneslevel

    Case study $Si% story RC frame uildin&'Case study $Si% story RC frame uildin&'

    9 *9

    ; *

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    Push-over analysis for seismic performance evaluation of RC frame structures. Computer programsPush-over analysis for seismic performance evaluation of RC frame structures. Computer programs

    Pushover loads =mode 8 transv&>

    ffective modal mass?9

    ffective modal mass?A9@

    Base shear forces:7ransversal mode 8.: !(? ;D 6N

    Longitudinal mode 8.:!*? D 6N

    78?8&

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    Plastic hinge analysis Plastic (one analysis

    'nteraction surface e"uation: Stress-strain curves for concrete andsteel bars urocodes.

    A /auss-Lobatto 'P+member

    %nteraction !-&

    -2000

    0

    2000

    4000

    6000

    8000

    10000

    12000

    0 200 400 600 800 1000 1200

    Bendi ng moment (kNm)

    -2000

    0

    2000

    4000

    6000

    8000

    10000

    12000

    0 .0 0 0. 01 0. 02 0. 03 0. 04 0 .0 5

    ltimate curvature

    '(ialforce)*!+

    -1000.00

    0.00

    1000.00

    2000.00

    3000.00

    4000.00

    5000.00

    0 .0 0 10 0.0 0 2 00 .0 0 3 00 .0 0 4 00 .0 0

    Bending Moment (kNm)

    ajor axis

    bending

    Minor axis

    bending

    0.00

    50.00

    100.00

    150.00

    200.00

    250.00

    300.00

    350.00

    400.00

    0.00 0.05 0.10 0.15 0.20

    Ultimate curvature

    Major axis

    bending

    Minor axis

    bending

    :8

    9&89&8

    =

    +

    zp

    z

    py

    y

    M

    M

    M

    M

    D

    ;*

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    Plastic (one analysis Plastic hinge analysis

    Pushover curves-"ongitudinal direction

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    0.00 20.00 40.00 60.00 80.00 100.00 120.00#isplacement , )cm+

    'pliedloadfactor

    Plastic zone, Plim1.12

    Plastic !inge, Plim1.11

    (ushover analysis) *on&itudinal direction(ushover analysis) *on&itudinal direction

    Plastic hinge: CP0 time: 8&< min

    8 load cycles.

    Plastic (one: CP0 time: D&; min

    8

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    Plastic hinge analysisPlastic (one analysisPushover curves-ransversal direction

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    1.40

    0.00 20.00 40.00 60.00 80.00#isplacement )cm+

    'plied

    load

    factor Plastic zone, Plim1.21

    Plastic !inge, Plim1.11

    (ushover analysis) Transversal direction(ushover analysis) Transversal direction

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    Bending moments !le*ural rigidities

    (lastic +one analysis) *on&itudinal direction(lastic +one analysis) *on&itudinal direction

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    Bending moments !le*ural rigidities

    (lastic +one analysis) Transversal direction(lastic +one analysis) Transversal direction

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    Pushover curves-ransversal direction

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    1.40

    0.00 20.00 40.00 60.00 80.00#isplacement )cm+

    'pliedloa

    dfactor Plastic zone "modal #attern$, #lim1.21

    Plastic zone "%ni&orm acceleration$, #lim1.1'

    #odal vs ,niform force distriution#odal vs ,niform force distriution

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    Push-over analysis for seismic performance evaluation of RC frame structures. Computer programsPush-over analysis for seismic performance evaluation of RC frame structures. Computer programs

    Pushover curves-"ongitudinal direction

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    1.40

    0.00 20.00 40.00 60.00 80.00 100.00 120.00#isplacement , )cm+

    'pliedloa

    dfactor

    Plastic zone "modal #attern$, Plim1.12

    Plastic zone "%ni&orm #attern$,Plim1.28

    #odal vs ,niform force distriution#odal vs ,niform force distriution

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    "uivalent SDOF and tar&et displacement"uivalent SDOF and tar&et displacement

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    Push-over analysis for seismic performance evaluation of RC frame structures. Computer programsPush-over analysis for seismic performance evaluation of RC frame structures. Computer programs

    arget displacements )Plastic /one+-ransversal direction

    (t).80 cm

    (t15.)) cm

    (t31.54 cm

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    1.40

    0.00 20.00 40.00 60.00 80.00

    #isplacement . )cm+

    'pliedlo

    adfactor *om#%ted #%s!o+er c%r+e "#lastic zone$

    dealized elaso-#er&ectl #lastic "*8$

    Tar&et displacements) transversal directionTar&et displacements) transversal direction

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    Push-over analysis for seismic performance evaluation of RC frame structures. Computer programsPush-over analysis for seismic performance evaluation of RC frame structures. Computer programs

    arget displacem ents )plastic hinge+-ransversal direction

    ).45

    14.'1

    2'.83

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    0.00 10.00 20.00 30.00 40.00 50.00 60.00#isplacement )cm+

    'pliedlo

    adfactor

    *om#%ted #%s!o+er c%r+e "#lastic !inge$

    dealized elasto-#er&ectl #lastic "*8$

    P/0.15g

    P/0.3g

    P/0.6g

    Tar&et displacements) transversal directionTar&et displacements) transversal direction

    T t di l t l it di l di ti

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    Push-over analysis for seismic performance evaluation of RC frame structures. Computer programsPush-over analysis for seismic performance evaluation of RC frame structures. Computer programs

    arget displacements )plastic /one+-"ongitudinal direction

    11.65 cm

    23.3 cm

    46.64 cm

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    0.00 20.00 40.00 60.00 80.00 100.00 120.00#isplacement , )cm+

    'pliedloadfactor

    *om#%ted #%s!o+er c%r+e "#lastic zone$

    dealized elasto-#er&ectl #lastic "*8$

    P/0.15g

    P/0.3g

    P/0.6g

    Tar&et displacements) lon&itudinal directionTar&et displacements) lon&itudinal direction

    T t di l t l it di l di ti

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    Push-over analysis for seismic performance evaluation of RC frame structures. Computer programsPush-over analysis for seismic performance evaluation of RC frame structures. Computer programs

    arget displacements )plastic hinge+-"ongitudinal direction

    11.2) cm

    22.54 cm

    45.08 cm

    0.00

    0.20

    0.40

    0.60

    0.80

    1.00

    1.20

    0.00 20.00 40.00 60.00 80.00 100.00#isplacement , )cm+

    'pliedloa

    dfactor

    *om#%ted #%s!o+er c%r+e "#lastic !inge$

    dealized elasto-#er&ectl #lastic "*8$

    P/0.15g

    P/0.3g

    P/0.6g

    Tar&et displacementsTar&et displacements lon&itudinal directionlon&itudinal direction

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    Push-over analysis for seismic performance evaluation of RC frame structures. Computer programsPush-over analysis for seismic performance evaluation of RC frame structures. Computer programs

    *ocal seismic demands*ocal seismic demands

    Curvatures along the member length

    -0.0150

    -0.0100

    -0.0050

    0.0000

    0.0050

    0.0100

    0.0150

    0.0200

    0.00 1.00 2.00 3.00 4.00 5.00 6.00 ).00

    Member lengt! "m$

    *%r+at%res

    P/0.15g

    P/0.3g

    P/0.6g

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    Push-over analysis for seismic performance evaluation of RC frame structures. Computer programsPush-over analysis for seismic performance evaluation of RC frame structures. Computer programs

    *ocal seismic demands*ocal seismic demands

    Curvatures along the member length

    -0.00)0

    -0.0060

    -0.0050

    -0.0040

    -0.0030

    -0.0020

    -0.0010

    0.0000

    0.0010

    0.00 0.50 1.00 1.50 2.00 2.50 3.00 3.50

    Member lengt! "m$

    *%r+at%res

    P/0.15g

    P/0.3g

    P/0.6g

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    .loal seismic demands.loal seismic demandsP/2?&8

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    P/2?&;g P/2?&9gP/2?&8

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    P/2?&;g P/2?&9gP/2?&8

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    CollapseP/2?&8

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    P/2?&8

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    Push over analysis for seismic performance evaluation of RC frame structures Computer programsPush over analysis for seismic performance evaluation of RC frame structures Computer programs

    2 computational efficient ;-# RC fiber beam-column element %as

    developed and implemented in a nonlinear inelastic analysis computer

    program Plastic hinge analysis: limited accuracy

    2 pushover e*ample for spatial model %as presented in con5unction

    %ith CD provisions

    Pushover analysis: good estimates of global and local inelastic

    deformations demands

    Limitations: for structures that vibrate primarily in the fundamental

    mode

    $vercomes: adaptive force distribution and modal pushover analysis

    procedures

    Nonlinear dynamic analysis: final solution

    Concludin& remar/sConcludin& remar/s