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UCBCALTRANS Shaking Table Test of Concrete Bridge Columns

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Compare performance for near-fault and long-duration excitations ... Design Level Earthquake (aftershock) Maximum Level Earthquake. Repeat Maximum Until Failure! ... – PowerPoint PPT presentation

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Title: UCBCALTRANS Shaking Table Test of Concrete Bridge Columns


1
UCB/CALTRANS Shaking Table Test of Concrete
Bridge Columns
U.C. Berkeley / Caltrans
2
RC Column Research
  • Main research focus is on Circular Reinforced
    Concrete Bridge Columns

Steel Bar
BRIDGE
COLUMN
SECTION
3
Earthquake Shaking
4
PEER/Caltrans Bridge Research
  • Research Focus
  • Monolithic reinforced concrete bridge
    construction
  • New rather than older construction detailing
  • Representative of
  • Viaducts
  • Overcrossings
  • Major interchanges

5
Shaking Table Tests Objectives
  • Data to validate analytical models
  • Compare performance for near-fault and
    long-duration excitations
  • Assess effects of multiple components of ground
    motion
  • Assess cumulative damage models

6
(No Transcript)
7
Specimen Design - Summary
  • Aspect Ratio 6 (to center of mass)
  • Scale 4.5
  • Diametermodel 16
  • Use actual mass for axial load
  • Unidirectional and bidirectional Input
  • Total 4 columns
  • longitudinal steel ratio of 1.2 (12 4 bars)
  • Spiral reinforcement ratio of 0.54
  • Designed according to Caltrans BDS

8
Section Details
9
Earthquake Histories
  • Investigate the response to Unidirectional Vs.
    Bidirectional Loading
  • Investigate the effects of Directivity and
    Duration

Near fault record (directivity, short duration)
Large magnitude earthquake (long duration, more
cycles)
Vs
10
Test Matrix
11
Loading History
Design Level Earthquake (aftershock)
Free Vibration Test
Low Level Testing up to Yield
Maximum Level Earthquake
Design Level Earthquake
Repeat Maximum Until Failure!
Maximum Level Earthquake
12
Specimen A2 - Before Testing
13
Specimen A2
Design Level 1
Maximum Level 1
14
Specimen A2
4th Run at the Maximum Level
dground 4.7,1.3
dmax 7.5, 2.4
aground 1.02g,1.09g
amax 0.24g,0.41g
15
Specimen A2 - Final Run
16
Damage - Spec A2
After sixth repetition of Maximum Run - Olive View
Fractured Bar
17
All Column Exhibited Stable Ductile Behavior
18
No Deterioration of Reponse Under Bidirectional
Loading
19
Second Mode Effects Due to Mass Rotational Inertia
20
Bidirectional Moment Interaction
21
Evaluation of Damage Indices
22
Column Stiffness Deteriorates Significantly Due
to Shaking
23
Verification of Analytical Models
  • Response quantities
  • Analytical Models
  • Elastic Analysis with equivalent sectional
    Stiffness (EI e)
  • Concentrated hinge models with equivalent plastic
    hinge properties
  • Fiber models with distributed section properties
    with equivalent material properties
  • Global
  • Displacements,
  • Residual Displacements,
  • Forces, Moments
  • Local
  • Curvatures,
  • Strains,
  • Slip Rotations,
  • Cumulative Damage

24
Elastic Models
  • Various assumptions for approximating effective
    section stiffness EI
  • EIe as defined by Caltrans gives reasonable
    results for maximum displacement

EIe
Test
Maximum Credible
25
Elastic Models
  • Various assumptions for approximating effective
    section stiffness EI
  • EIe as defined by Caltrans gives reasonable
    results for maximum displacement
  • Not always

EIe
Test
Maximum Credible
26
Elastic Models
  • Various assumptions for approximating effective
    section stiffness EI
  • EIe as defined by Caltrans gives reasonable
    results for maximum displacement
  • Not always

EIe
Test
Maximum Credible
27
Elastic Models
  • Various assumptions for approximating effective
    section stiffness EI
  • EIe as defined by Caltrans gives reasonable
    results for maximum displacement
  • Not always
  • No information on residual displacements
  • Other engineering demand parameters inferred from
    pushover analyses

EIe
Test
Maximum Credible
Design Level
28
Concentrated Plastic Hinge Models
  • Various methods for estimating equivalent
    properties for concentrated plastic hinge (Lp,
    M-f, etc.)
  • Various idealized hysteretic models
  • Bilinear vs. Stiffness Degrading
  • Coupled and uncoupled

Bilinear Stiffness Degrading
Maximum Credible
29
Concentrated Plastic Hinge Models
  • Most models provide adequate estimate of maximum
    displacement

Bilinear Stiffness Degrading
Maximum Credible
Bilinear Stiffness Degrading
Design Level
30
Concentrated Plastic Hinge Models
  • Most models provide adequate estimate of maximum
    displacement
  • Nonlinear models provide indication of yielding
    and degradation on wave form and residual
    displacement
  • Estimates are often poor
  • Stiffness degrading models generally better

Bilinear Stiffness Degrading
Maximum Credible
Lateral Direction
Stiffness Degrading Bilinear
31
Concentrated Plastic Hinge Models
Bilinear Stiffness Degrading
Maximum Credible
Lateral Direction
Stiffness Degrading Bilinear
32
Concentrated Plastic Hinge Models
  • Local information on strains, bar buckling,
    fatigue, etc. must be inferred from detailed
    analysis of member
  • Problem under cyclic loads?

33
Fiber Models
  • Useful for well confined members controlled by
    ductile yielding
  • Approximations at material level, number of
    fibers used to model section, manner in which
    member is discretized longitudinally

Concentrated Hinge Models
Bilinear Stiffness Degrading
Fiber Model
Maximum Credible
34
Fiber Models
Fiber Model
Maximum Credible
  • Generally, much better fidelity
  • Results, especially for residual displacement and
    local deformations (strain) sensitive to modeling
    of section
  • Fixed end rotations due to bar pullout not yet
    accounted for in OpenSees

35
Parametric Study
  • Design multiple columns with varying
  • Diameter (Dcol)
  • Axial Load (Pr)
  • Aspect Ratio (ar)

36
Design Procedure
Sa
Z?? BDS Z4 for all T ATC-32 Z1 to 4
Tlt1 sec Z4 Tgt1 sec SDC
Sa gt 0.1g DcapacitygtDdemand
Elastic ARS Spectrum
Z
Sadesign Sa/Z
0.1g
Period, T
37
Automated Design Using Section Properties Database
38
Designed Columns with Dcol60
39
Ground Motions
  • Used 20 LMSR motions

40
Hysteretic Model Used
41
Performance Evaluation
  • Damage Indices
  • Park Ang
  • Bar Fatigue Damage Index

where 2Nf is the number of half cycles to
failure at a plastic strain
42
Mean Results
43
Mean1 SD Results
44
Comparison of displacement demand
45
Low-Cycle Fatigue Index
46
Fragility Curves
  • For a single column, run suite of ground motions.
  • Ground motions are scaled to have a spectral
    acceleration at the period of the column ranging
    from zero to 2 SaARS(Tcol)
  • Compute Fragility curves for
  • Park Ang Index (Minor and Significant damage)
  • Fatigue Index
  • Spalling (ecu gt 0.009)

47
Fragility Curves for Events with Large Magnitude
at Small Distance
48
Fragility Curves for Events with Large Magnitude
at Large Distance
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