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Research Research carried carried out out within within the the context context of PBEE of PBEE Paolo Franchin Paolo Franchin A relaxed workshop on PBEE Capri, July 2 nd -4 th 2009

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Page 1: Research carried out within the context of PBEE › doc › pdf › EEBTB › Franchin_EEBTB_Presentation.pdf · – Rajeev Pathmanathan – Fatemeh Jalayer – Fabrizio Noto –

ResearchResearch carriedcarried out out withinwithin the the contextcontext of PBEEof PBEE

Paolo FranchinPaolo Franchin

A relaxed workshop on PBEECapri, July 2nd-4th 2009

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AcknowledgementsAcknowledgements

• People I learnt from, I had fun with, I owe much (I’m not going to quote each and every one when neededlater on, hence I just thank them all now):

– Paolo E. Pinto– Armen Der Kiureghian– Ove Ditlevsen– Filip C. Filippou– Alessio Lupoi– Marko IJke Schotanus– Giorgio Lupoi– Rajeev Pathmanathan– Fatemeh Jalayer– Fabrizio Noto– Terje Haukaas

• Introduction• Topic 1• Topic 2

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ResearchResearch areasareas

• Probabilistic methods in earthquake engineering– Seismic risk for intact and damaged structures (collapse & progressive

collapse risk)• FORM• Response surface• IM-based methods• Simulations with fully probabilistic models

– Performance of hospital systems– Performance of infrastructural systems (road networks)

• Seismic assessment of existing structures– Epistemic uncertainty– Non-linear static methods– Masonry and reinforced concrete

• Seismic design and analysis of bridges– Non-uniform support excitation

• Modelling– Nonlinear frame elements, response sensitivities– Soil-structure interaction: retaining structures

• Introduction• Topic 1• Topic 2

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FocusFocus themesthemes

• Today, focus on:– Earth-retaining structures, simplified non-linear

dynamic modelling• Relevance

– Structural and geotechnical communities traditionally havedifferent language/approach

– Typically structures are “lollipops” for geotechnical engineers, while the soil is “some springs” for their structural counterparts

– Consistent seismic performance evaluation of foundations & retaining structures is thus challenging, given the “boundary”nature of the topic

– Probability of collapse for sequential shocks• Relevance

– key to emergency response management, both for buildingsand for infrastructure

• Some open questions

• Introduction• Topic 1• Topic 2

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TopicTopic 11

BD

AE

F

C(a)

BD

AE

F

C

BD

AE

F

C(a)

(a)

αcosu

uhff =

α2coskkh = u

f

αcos0

0ff h =

α

(a)

αcosu

uhff =

α2coskkh = u

f

αcos0

0ff h =

αα

hε(Tensile)(Compressive)

Bha ,σBh ,0σ

Ah ,0σ

Ahp ,σ

(b)BhE ,

AhE ,

hε(Tensile)(Compressive)

Bha ,σBh ,0σ

Ah ,0σ

Ahp ,σ

(b)BhE ,

AhE ,

A

B

A

B

τ

γ

( )b ( )c(a)

αcosu

uhff =

α2coskkh = u

f

αcos0

0ff h =

α

(a)

αcosu

uhff =

α2coskkh = u

f

αcos0

0ff h =

αα

hε(Tensile)(Compressive)

Bha ,σBh ,0σ

Ah ,0σ

Ahp ,σ

(b)BhE ,

AhE ,

hε(Tensile)(Compressive)

Bha ,σBh ,0σ

Ah ,0σ

Ahp ,σ

(b)BhE ,

AhE ,

A

B

A

B

τ

γ

( )b ( )c

0 5 10 15 20 25-1

0

1

ac

ce

lera

tion

(g

)

0 10 20-20

-15

-10

-5

0

top wall settlement (mm)

0 10 20

-60

-40

-20

0

horizontal displacement (mm)

SeismicSeismic performance performance evaluationevaluation ofofflexibleflexible retainingretaining structuresstructures::

1D 1D nonlinearnonlinear dynamicdynamic modellingmodelling

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RetainingRetaining structuresstructures: : motivationmotivation

• Several hundreds km of highways currentlyundergoing upgrading (including seismic)

• Large number of non-seismically designedearth-retaining structures in existing road networks

• Current analysis based (99%) on pseudo-staticmethods

– FEA/FDA still too demanding and unwarranted foruse in the profession

• Shift in focus from forces to displacement(maximum and residual)

• This situation stimulates the development of simple non linear dynamic models satisfying the requirements of:

– Being affordable and sufficiently accurate– Allowing evaluation of residual (cumulative)

displacements

• Introduction• Topic 1• Topic 2

m5

m8

3/20 mkN=γ°=°= 23 35 δφ

( )kPazE s ⋅= 13000GPaEc 31=mtw 80.0=

( )a( )b( )c

g2.0g1.0

200400600800Bending moment M (kNm/m)

Dep

thz

(m)

13−

11−

9−

5−

3−

m5

m8

3/20 mkN=γ°=°= 23 35 δφ

( )kPazE s ⋅= 13000GPaEc 31=mtw 80.0=

( )a( )b( )c

g2.0g1.0

200400600800Bending moment M (kNm/m)

Dep

thz

(m)

13−

11−

9−

5−

3−

FLACSRMM-O

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AvailableAvailable modelsmodels//methodsmethods

• Pseudo-static methods (Woods, Mononobe-Okabe)

• Newmark method

• Inelastic (usually some brand of plasticity) dynamicfinite element/difference methods (DYNAFLOW, GEFDYN, FLAC, PLAXIS, OPENSEES, etc)– Violate the requirement of affordability (computationally and

in terms of required background)

• Viscoelastic solutions (Wood, Veletsos and co-workers)– Cannot assess inelastic displacements

• Winkler-type analysis– Crude but practical, applied to a variety of linear/nonlinear,

static and dynamic problems– Apparently not yet employed for nonlinear dynamic analysis of

flexible retaining structures

• Introduction• Topic 1• Topic 2

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ProposedProposed 1D model 1D model (1/2)(1/2)

The problem is one of imposed displacements, characterised bythe lack of symmetry

BD

AE

F

C(a)

BD

AE

F

C

BD

AE

F

C(a)

bedrock

Model base (absorbent boundary)

Common base

Far-field(undisturbed)Far-field

(undisturbed)Interface soil(disturbed)

Interface soil(disturbed)

(b)

(b)

A B

C D E

F

Dampercb = ρbVsb

Input forcef(t)=cbv(t)

“Uphill”(layered)

soilcolumn

Mas

s-sp

ring

mod

elof

soi

lcol

umn

Non-symmetricWinkler springs“Downhill”

(layered)soil

column

• Introduction• Topic 1• Topic 2

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ProposedProposed 1D model 1D model (2/2)(2/2)

(a)

αcosu

uhff =

α2coskkh = u

f

αcos0

0ff h =

α

(a)

αcosu

uhff =

α2coskkh = u

f

αcos0

0ff h =

αα

hε(Tensile)(Compressive)

Bha,σBh ,0σ

Ah ,0σ

Ahp,σ

(b)BhE ,

AhE ,

hε(Tensile)(Compressive)

Bha,σBh ,0σ

Ah ,0σ

Ahp,σ

(b)BhE ,

AhE ,

A

B

A

B

τ

γ

( )b ( )c(a)

αcosu

uhff =

α2coskkh = u

f

αcos0

0ff h =

α

(a)

αcosu

uhff =

α2coskkh = u

f

αcos0

0ff h =

αα

hε(Tensile)(Compressive)

Bha,σBh ,0σ

Ah ,0σ

Ahp,σ

(b)BhE ,

AhE ,

hε(Tensile)(Compressive)

Bha,σBh ,0σ

Ah ,0σ

Ahp,σ

(b)BhE ,

AhE ,

A

B

A

B

τ

γ

( )b ( )c

Non-symmetric:Elastic-plastic

shifted in tension

Non-symmetric:Elastic-plastic

shifted in compression

Symmetric:Bouc-Wen

Tie-backs Soil-wall interfaceSoil columns

Force-displacement laws for the model components

(England et al, 2001)

• Introduction• Topic 1• Topic 2

Soil springs for both columns and interface elements are functionsof the overburden pressure as well as the OCR, they are updatedduring excavation

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The The nextnext slidesslides

• Sample results– Unanchored diaphragm wall– Tie-back wall (retrofitted abutment)

• Limited/preliminary validation through:– Comparison with 2D-FE analysis (PLAXIS), good– Comparison with shake-table test performed in

Pavia, not bad– Both of the above can’t be used to validate all the

features of the model

• Further research

• Introduction• Topic 1• Topic 2

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11SampleSample resultsresults, , unanchoredunanchored wallwall

(1/3)(1/3)

mtGPaE

mkN

c

c

50.02.0 30

/25 3

=

==

=

ν

γ

φδ

φ

ν

γ

32

0' 353.0 /250

/6.19 3

=

=°=

==

=

kPacsmVmkN

s

s

m 0.6

m 0.5

m 0.9

mtGPaE

mkN

c

c

50.02.0 30

/25 3

=

==

=

ν

γ

φδ

φ

ν

γ

32

0' 353.0 /250

/6.19 3

=

=°=

==

=

kPacsmVmkN

s

s

m 0.6

m 0.5

m 0.9

Dry cohesion-less soil!

• Introduction• Topic 1• Topic 2

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12SampleSample resultsresults, , unanchoredunanchored wallwall

(2/3)(2/3)

0 5 10 15

-0.2

-0.1

0

0.1

0.2

0.3

time (s)

acc.

(g)

Outcropping

0 5 10 15

-0.2

-0.1

0

0.1

0.2

0.3

time (s)

acc.

(g)

Deconvolved

0 1 2 30

0.1

0.2

0.3

0.4

0.5

0.6

period (s)

Sa (g

)

( )ta

( )ta

sbb Vρ , space-half

( )tvde

conv

olut

ion

integration

ss Vρ ,deposit

sbbsb VAc ρ⋅= 2

( ) ( )tvctf b=

Model response

0 05

-0.045

-0.04

-0.035

-0.03

-0.025

-0.02

-0.015

-0.01

-0.005

0

( )tu( )ta

( )ta

sbb Vρ , space-half

( )tvde

conv

olut

ion

integration

ss Vρ ,deposit

sbbsb VAc ρ⋅= 2

( ) ( )tvctf b=

Model response

0 05

-0.045

-0.04

-0.035

-0.03

-0.025

-0.02

-0.015

-0.01

-0.005

0

( )tu

Outcropping Deconvolved Spectra

• Introduction• Topic 1• Topic 2

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13SampleSample resultsresults, , unanchoredunanchored wallwall

(3/3)(3/3)

Bending moment distr. Top displacement TH

• Introduction• Topic 1• Topic 2

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SampleSample resultsresults, , tietie--backback wallwall

-200 0 200 400 600 800 1000-12

-10

-8

-6

-4

-2

0

Bending moment (kNm/m)

Dep

th (m

)

Fixed bearingSliding bearingSlidingbearing,anchored

0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15-0.07

-0.06

-0.05

-0.04

-0.03

-0.02

-0.01

0

Time (s)

Top

disp

lacem

ent (

m)

Sliding bearing, anchored

Sliding bearing

Fixed bearing

-0.07 -0.06 -0.05 -0.04 -0.03 -0.02 -0.01 0 0.01-12

-10

-8

-6

-4

-2

0

Displacement (m)

Dep

th (m

)

Fixedbearing

Slidingbearing

Slidingbearing,anchored

H=

6.0m

D=

6.0m

2.0m

8.0m

L=10.0m

α=15°

L=30.0m

3.0m/s 250

kPa 0'

32 35kN/m 6.19

30,

3

=

==

=

°=°=

=

ν

φφ

γ

ss

cvpeak

s

VVc

t=0.7m

H=

6.0m

D=

6.0m

2.0m

8.0m

L=10.0m

α=15°

L=30.0m

3.0m/s 250

kPa 0'

32 35kN/m 6.19

30,

3

=

==

=

°=°=

=

ν

φφ

γ

ss

cvpeak

s

VVc

t=0.7m

• Introduction• Topic 1• Topic 2

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Model Model validationvalidation ((partialpartial!) !) (1/3)(1/3)

• 2D plane strain model in the commercial code PLAXIS– Elastic-plastic with Mohr-Coulomb failure criterion (small “stability”

cohesion 1kPa)– Non-rigid interface with R = tanδ/tanφ = 0.62 (δ/φ = 0.67)– Newmark damping α = 0.6 and β = 0.3025– (Use of large model width and fixed base due to lack of

transparent boundaries)

• Introduction• Topic 1• Topic 2

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Model Model validationvalidation ((partialpartial!) !) (2/3)(2/3)

Artificial signalRicker wavelet

Recorded motionColfiorito (Italy)

Response spectraA

ccel

erat

ion

Dis

plac

emen

t

• Introduction• Topic 1• Topic 2

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Model Model validationvalidation ((partialpartial!) !) (3/3)(3/3)

1D modelPlaxis

• Introduction• Topic 1• Topic 2

Ricker wavelet

Colfiorito recorded GM

• Note:– High-frequency

content, model isfixed-base

– Largedisplacements and moments, no radiation damping

– (Too) good match with “higher-order”method

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ComparisonComparison withwith experimentalexperimental testtest

• Large scale shake-table test of an unanchored diaphragm wall in dry cohesionless soil

• Data kindly made available from the EUCENTRE researchfoundation in Pavia, Italy (Carlo Lai and co-workers)– Details can be found in “Large scale 1-g shaking table test of an

unanchored earth-retaining RC diaphragm” Borg et al 2009• Our simulation

– Constant unit weight, fixed soil columns, no degradation and average value of friction angle between φ’ and φCV

Laminar box Pluviation device Instrument scheme

But… But…

• Introduction• Topic 1• Topic 2

But…

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Model Model vsvs ExperimentExperiment

0 5 10 15 20 25-1

0

1

ac

ce

lera

tion

(g

)

0 10 20-20

-15

-10

-5

0

top wall settlement (mm)

0 10 20

-60

-40

-20

0

horizontal displacement (mm)

• Introduction• Topic 1• Topic 2

+NAT4 NAT5=-NAT4 +NAT6 NAT7=-NAT6 +NAT8 NAT9=-NAT8

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FurtherFurther developmentsdevelopments

• Include interface-soil cyclic degradation (φ’→φCV)

• Cantilever retaining wall with direct and indirect foundation(abutments)

• Introduction• Topic 1• Topic 2

Active φ’

Active φCV

Passive φ’

Passive φCVDecreasein restraint

at base

Increasein uphillpressure

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SummarySummary & & conclusionsconclusions of of TopicTopic 11

• A simple 1D nonlinear dynamic model is developed to be:– Capable of capturing the main features of the problem (lack of

symmetry, imposed motion, cumulative inelasticdisplacements)

– Computationally affordable– Sufficiently accurate, as compared to other computational

tools

• What is still needed:– A more “robust” validation, for tie-back walls, with compliant

base, more records and parameters sets

• Uses:– Preliminary design– Reliability analysis (as for instance the base model in a Model

Correction Factor Method)

• Open questions– In the pursue for more reliable performance estimates is it still

feasible to separate the design tasks between structural and geotechnical engineers? Or shouldn’t SSI analysis become a more widespread tool?

• Introduction• Topic 1• Topic 2

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0 5 10 15 20 25 30 35 40-4

time (s)

0 5 10 15 20 25 30 35 40-0.15

-0.1

-0.05

0

0.05

0.1

time (s)

disp

lacem

ent (

m)

-4

-2

0

2

4

acce

lerat

ion

(m/s

2 )

0 1

0 1 20

5

10

15

Y

Sa (m

/s2 )

0 5 10 150

2

4

6

8

SaY=1 (m/s2)

0 5 10 150

0.2

0.4

0.6

0.8

Sa (m/s2)

P(D

S3|D

S2,S

a)

0 1 20

5

10

15

Y

Sa (m

/s2 )

0 5 10 150

5

10

15

SaY=1 (m/s2)

η β

0 5 10 150

0.2

0.4

0.6

0.8

Sa (m/s2)

P(D

S3|S

a)

100 101 102 10310-3

10-2

10-1

t (days)

λ3m

λ1,3a T = 365 days

λ2,3a T = 365 days

λ1,3a T = 180 days

λ2,3a T = 180 days

Mm = 5.5

TopicTopic 22

RiskRisk of of aftershockaftershock--inducedinduced collapsecollapseasas a a criterioncriterion forfor

closureclosure//rere--openingopening of of bridgesbridges

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Statement of the Statement of the problemproblem

• Decision on transitability of bridges in the aftermath of a damaging mainshock currently based on expert judgementon damage state

• Expert judgement not replaceable but could be usefully complemented by pre-analysis of bridges in the network

• Proposed criterion: transitability decision based on collapse risk due to aftershocks

• Implemented method requires– Aftershock hazard– Capability of assessing state of damage of each bridge: linking

visual observation with mechanical damage

• The idea was inspired by Gee Like Yeo PhD work (Stanford, 2005), and more generally by work carried out in California for PGE on the topic of building tagging

• Introduction• Topic 1• Topic 2

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DifficultiesDifficulties withwith DamageDamage

Actual

Visual Numerical

Damageas assessed

during field visit

Damage assimulated by FE analysis

Real damageexperienced

by the structure

• Introduction• Topic 1• Topic 2

Both visual inspection and FEA have limitations. Evaluation of true damage and of residual capacity is a challenging task.

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MainshockMainshock vsvs AftershocksAftershocks

Seismichazard

Structuralfragility

Risk orMAF of DS

(e.g. collapse)

( ) ( )xx SaSa λλ =year 1

PSHA

( ) ( )xSDSPxF aii ==

Fragility analysis

( ) ( )∫∞

=0

xdxF Saii λλ

Mainshock Aftershock

APSHA

( )txSa ,λ

Fragility analysis (damaged)

( ) ( )xSDSDSPxF ajiij =→=

( ) ( ) ( ) ( )∫∞

=0, dxxfxFtt Saijji αλ

• Introduction• Topic 1• Topic 2

IM-based approach: Risk from hazard and fragility

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APSHA and APSHA and AftershockAftershock riskrisk

( ) ( ) ( ) nilma

T

t

ai

ylm

ai PMMtd

tTT

MMt ,

3,1

3, ,,~,,~⋅=

−= ∫ αττλλ

( ) ( ) ( ) ( ) ( ) nilmaaSailma

ai PMMtdxxfxFMMtt ,0 3,3, ,,,, ⋅== ∫

∞ααλ

( )( )

( )pMMba

ma ctMMt

m

+=

−+10,,λ

Instantaneous rate of aftershocks(Modified Omori-law, Reasenberg and Jones 1989)

Instantaneous Collapse Frequency due to aftershocks

Equivalent Mean Annual Collapse Frequency due to aftershocks

• Introduction• Topic 1• Topic 2

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StructuralStructural fragilityfragility curvecurve

( )( )tCtDY DS

k

kIkNjt

DS

jm ∈== minmaxmax

,,1K

Global scalar index of structural performance, Jalayer et al 2007

minmin

max

( ) ⎟⎟⎠

⎞⎜⎜⎝

⎛ −Φ=≤=

21 lnln

i

iYa

xxSPβ

ηY

1

aSIDA

Y1

aSIDA ( ) ( ) ( )xSPxSaYPxF Y

aDSi

i ≤==>= =11

Median ηi, dispersion βi

• Introduction• Topic 1• Topic 2

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ModellingModelling forfor cycliccyclic degradationdegradation

crackV

peakV

.resV

.resγpeakγcrackγ

sres

scrackpeak

Nccrack

VV

VVVVVV

=

+=

+=

( )*arctan GA

( )a

-0.01 -0.005 0 0.005 0.01-2000

-1000

0

1000

2000

shear deformation γ

shea

r for

ce V

(kN

)

( )b

peakV≈crackV

.resV≈

crackV

peakV

.resV

.resγpeakγcrackγ

sres

scrackpeak

Nccrack

VV

VVVVVV

=

+=

+=

( )*arctan GA

( )a

-0.01 -0.005 0 0.005 0.01-2000

-1000

0

1000

2000

shear deformation γ

shea

r for

ce V

(kN

)

( )b

peakV≈crackV

.resV≈

⎥⎥⎥

⎢⎢⎢

∂∂

∂∂∂∂

∂∂∂∂

=

γ

φε

φε

VMMNN

s

0000

0

0

k

Opensees, flexibility-based element, section aggregator

Fiber section

Uniaxial material

Cyclic degradationBackbone curve

• Introduction• Topic 1• Topic 2

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The The HansuiHansui viaductviaduct, , KobeKobe 19951995

(from Marini and Spacone, ACI Struct. Jnl 2006)

• Introduction• Topic 1• Topic 2

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0 5 10 15 20 25 30 35 40-4

time (s)

0 5 10 15 20 25 30 35 40-0.15

-0.1

-0.05

0

0.05

0.1

time (s)

disp

lacem

ent (

m)

Sample model Sample model responseresponse 1/21/2

-4

-2

0

2

4ac

celer

atio

n (m

/s2 )

0 1

Mainshock Aftershock

Input ground acceleration

Output top displacement

• Introduction• Topic 1• Topic 2

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Sample model Sample model responseresponse 2/22/2

5 0 5

-5 0 5

x 10-3

-5 0 5

x 10-4

-2 0 2

x 10-4

-2 0 2

x 10-4

-2 0 2

x 10-4

-5 0 5

x 10-4

-1000

0

1000

2000

-5 0 5

x 10-4

-1000

0

1000

2000

-2 0 2

x 10-4

-1000

0

1000

-2 0 2

x 10-4

-1000

0

1000-2 0 2

x 10-4

-1000

0

1000-2 0 2

x 10-4

-1000

0

1000

2 0 2-1000

0

1000-2 0 2

x 10-4

-1000

0

1000-2 0 2

x 10-4

-1000

0

1000

-1 0 1

x 10-3

-1000

0

1000

2000

-5 0 5

x 10-4

-1000

0

1000

2000

-5 0 5

x 10-4

-2000

0

2000

05 0 0 05

2 0 2

x 10-3

2 0 2

x 10-3

5 0 5

x 10-3

1 0 1

x 10-3

5 0 5

x 10-3

-0.05 0 0.05-5000

0

5000

0 1 2

x 10-4

0

100

200

-0.05 0 0.05-5000

0

5000

-5 0 5

x 10-3

-2000

0

2000-1 0 1

x 10-3

-1000

0

1000-0.01 0 0.0-5000

0

5000

0 05 0 0 0-5000

0

5000-2 0 2

x 10-3

-2000

-1000

0

1000-5 0 5

x 10-3

-2000

0

2000

4000

-0.05 0 0.05-5000

0

5000

-5 0 5

x 10-4

-200

0

200

400

-0.05 0 0.05-5000

0

5000

Flexural (M-φ) Shear (V-γ)

• Introduction• Topic 1• Topic 2

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DefinitionDefinition of of limitlimit statesstates• Introduction• Topic 1• Topic 2

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Site, Site, seismogeneticseismogenetic areasareas, , hazardhazard

-200 -150 -100 -50 0 50 100-150

-100

-50

0

50

100

Zone 904

Zone 905

Zone 906

km

km

44.75

45

45.25

45.5

45.75

46

46.25

46.5

46.75

47

10.2510.510.7511 11.2511.511.7512 12.2512.512.7513 13.2513.513.7514 14.25

Site

100 10210110110-6

10-5

10-4

10-3

10-2

10-1

Sa (m/s2)

λSa

α = 0.14β = 1.12Ml = 4.76Mu = 6.14

α = 0.37β = 1.06Ml = 4.76Mu = 6.60

α = 0.11β = 1.14Ml = 4.76Mu = 6.14

NE Italy - Friuli region1976 M = 6.4 event

Three seismogeneticareas

MAF of Sa at T=0.45s

Lolli and Gasperini, 2003:

a = -2, b = 1, log10c = -1.65 and p = 0.9,

• Introduction• Topic 1• Topic 2

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IntactIntact structurestructure fragilitiesfragilities

0 1 20

5

10

15S

a (m/s

2 )

0 5 10 150

5

10

15η β

0 5 10 150

0.2

0.4

0.6

0.8

P(D

S1|S

a)

LDη=1.89 β=0.30

0 1 20

5

10

15

Sa (m

/s2 )

0 5 10 150

5

10

15

0 5 10 150

0.2

0.4

0.6

0.8

P(D

S2|S

a)

SDη=3.05 β=0.42

0 1 20

5

10

15

Y

Sa (m

/s2 )

0 5 10 150

5

10

15

SaY=1 (m/s2)

η β

0 5 10 150

0.2

0.4

0.6

0.8

Sa (m/s2)

P(D

S3|S

a)COη=4.01 β=0.41

• Introduction• Topic 1• Topic 2

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DamagedDamaged structurestructure fragilitiesfragilities

0 1 20

5

10

15S

a (m/s

2 )

0 5 10 150

5

10

0 5 10 150

0.2

0.4

0.6

0.8

P(D

S3|D

S1,S

a)

0 1 20

5

10

15

Y

Sa (m

/s2 )

0 5 10 150

2

4

6

8

SaY=1 (m/s2)

0 5 10 150

0.2

0.4

0.6

0.8

Sa (m/s2)

P(D

S3|D

S2,S

a)

LD to COη=3.98 β=0.38

SD to COη=2.86 β=0.48

0 1 20

5

10

15

Y

Sa (m

/s2 )

0 5 10 150

5

10

15

SaY=1 (m/s2)

η β

0 5 10 150

0.2

0.4

0.6

0.8

Sa (m/s2)

P(D

S3|S

a)CO η=4.01 β=0.41

• Introduction• Topic 1• Topic 2

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EquivalentEquivalent MAFMAF

100 101 102 10310-3

10-2

10-1

t (days)

λ3m

λ1,3a M

m = 5.5

λ2,3a M

m = 5.5

λ1,3a M

m = 6.0

λ2,3a M

m = 6.0

100 101 102 10310-3

10-2

10-1

t (days)

λ3m

λ1,3a T = 365 days

λ2,3a T = 365 days

λ1,3a T = 180 days

λ2,3a T = 180 days

T = 365 days Mm = 5.5

• Introduction• Topic 1• Topic 2

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SummarySummary & & ConclusionsConclusions of of TopicTopic 22

• An aftershock-risk-based bridge opening/closurecriterion is proposed. It requires:– Pre-analysis of bridges for intact and damaged conditions– APSHA immediately after the mainshock

• Pre-analysis, possibly with data acquired frominstruments (SMA) at the brigdes sites and network emergency traffic analysis, can better direct inspections and rationally support closure decision

• Still need considerable improvements:– In analysis tools (correct simulation of damage) and in

particular shear-flexure cyclic interaction– In correlation between visual observation and actual damage

• Introduction• Topic 1• Topic 2

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ContributionContribution toto generalgeneral discussiondiscussion

• As far as I know the role/weight of computer modelsand analysis is increasing and is likely to do even more as we press towards realistic performance estimation

– Is this an illusory step towards better/safer structures?

• Engineering has always relied on sound engineeringjudgement

– Is there a way to develop it in students?– Shouldn’t we invest more on finding more effective ways of

teaching?– I personally teach Structures to architects (yes, I know…):

succeding in teaching them an intimate understanding of structural behaviour isn’t going to make a larger differencethan all my research?

– What about dynamics? How to develop intuition aboutdynamic behaviour?