Nonlinear Analysis of Reinforced Concrete Structures in ... · CERVENKA CONSULTING PRAGUE, CZECH...
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CERVENKA CONSULTING
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October 2008
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Nonlinear Analysis
of Reinforced Concrete Structures
in Design and Structural Assessment
Jan Cervenka
Červenka Consulting, Prague, Czech Republic
Outline:
Červenka Consulting - Computer simulation (virtual testing) of concrete structures
Finite element system ATENA – theoretical background, structure, practical applications
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Contents
1. What is simulation?
1. Numerical models for the simulation of reinforced concrete:
1. Nonlinear finite element analysis
2. Material models, fracture-plastic, microplane
3. Special FE for reinforced concrete modeling
• Validation:
• Tension stiffening
• Round robin predictions
• Full scale structural tests
• Applications:
• Bridges
• Tunnels
• Nuclear containment
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Why nonlinear simulation of structures?
Supports expert engineering knowledge
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E 2 E 3 E 10 E 15 E 18 E 27
low strength
high strength
Nonlinear simulation of reinforced concrete structures obrazy trhlin při provozním zatížení
bez oslabení
kulaté otvory
plné vyztužení
kulaté otvory
pouze třmínky
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ATENA:
reinforcement modeling
realistic crack display
run-time visualization
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Nonlinear Finite Element Analysis
ATENA analysis
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Nonlinear constitutive models in ATENA
variety of nonlinear material models:
for concrete
plain
reinforced
pre-stressed
fibre reinforced
other quasi-brittle materials
masonry
rock
soil
metals
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Material Models for Concrete
Uniaxial law Bi-axial criterion 3D failure surface
Menetrey Willam, ACI 1995 Kupfer 1969
Plasticity
Damage mechanics
Microplane models
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Program ATENA
Crack band method – correct energy dissipation during the fracturing process
concrete in tension
tensile cracks
post-peak behavior
fracture energy
crack band method
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Demonstration Examples – mesh objectivity
Importance of Fracture mechanics x Stress-strain laws
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Exponential Model
0,00E+00
2,00E-04
4,00E-04
6,00E-04
8,00E-04
1,00E-03
1,20E-03
1,40E-03
1,60E-03
0,00E+00 1,00E-04 2,00E-04 3,00E-04 4,00E-04 5,00E-04 6,00E-04 7,00E-04 8,00E-04
Deformation [m]
Su
pp
ort
Re
actio
n [M
N]
Coarse Mesh (80x16.7mm)
Fine Mesh (26.7x16.7mm)
Finest Mesh (15.4x16.7mm)
Theory of Elasticity
Experiment
Local Strain Model
0,00E+00
2,00E-04
4,00E-04
6,00E-04
8,00E-04
1,00E-03
1,20E-03
1,40E-03
1,60E-03
0,00E+00 1,00E-04 2,00E-04 3,00E-04 4,00E-04 5,00E-04 6,00E-04 7,00E-04 8,00E-04
Deformation [m]
Support
Reactio
n [M
N]
Coarse Mesh (80x16.7mm)
Fine Mesh (26.7x16.7mm)
Finest Mesh (15.4x16.7mm)
Theory of Elasticity
Experiment
Fracture mech.:
Local model:
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Program ATENA
Numerical core - nonlinear material models
concrete in tension
tensile cracks
post-peak behavior
crack band method
fracture energy
fixed or rotated cracks
crack localization
deterministic size-effect
is captured
Crack band size: L
e = w
L
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Special elements for reinforced concrete analysis
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VALIDATION: Simulation of laboratory experiments
Reality
Simulation
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Validation and Reliability
Blind Predictions
Toronto Panel (Collins, Melhorn) 1986
competition results (Panel C).
a) Variations in predicted shear
strength
b) Variations in predicted
load-deformation
response
winner Vladimir Cervenka
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Validation: Round Robin Competition, Marti 2005
ATENA predictions
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Validation: Field Test – Örnsköldsvik, Sweden
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Validation: Field Test
Örnsköldsvik, Sweden
Final failure Step 40, Cracks: in elements, <5.000E-03; ...), openning: <-4.092E-04;4.226E-02>[m], Sigma_n: <-1.912E+01;2.009E+00>[MPa], Sigma_T: <-2.535E+00;2.151E+00>[MPa]
ATENA analysis Field test
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0
2
4
6
8
10
12
14
0 20 40 60 80 100 120 140
Deflection [mm]
Lo
ad
[M
N]
Exper. side 1 Exper. side 2
Initial ATENA w/o CFRP Initial ATENA w. CFRP
Eurocode 2 ATENA final
Analysis with stirrups
Örnsköldsvik Bridge – shear strength
comparison, experiment, ATENA calculation
Stirrups not modelled in the initial analyses
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0 20 40 60 80 10010 30 50 70 90
Displacement [mm]
0
2
4
6
8
10
12
0.5
1
1.5
2.5
3
3.5
4.5
5
5.5
6.5
7
7.5
8.5
9
9.5
10.5
11
11.5
Loa
d [M
N]
West beam mid-span displacement
East beam mid-span displacement
ATENA
3D analysis by LTU
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Foundation slab – cracks due to underground water pressure
forensic investigation
crack
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ATENA numerical simulation
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Foundation slab
Measured cracks
FE analysis
Results due
to water
pressure
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Foundation slab
Measured cracks
FE analysis
Results due
to shrinkage
Constant shrinkage
based on EC2
Conclusion:
Cracks not due to shrinkage
but due to water pressure
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Measured
deflections
Analyzed
deflections
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Construction 514, bridge crossing river Berounky
near Prague, Czech Rep., design Novák & Partner, Ing. M. Šístek
Global verification
of safety during
construcion stages
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Double console
Pier n. 39
112 m
50 m 50 m
35 m
1,4 m
R = 750 m
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Special continuum 3D layered
shell elements, concrete C35/45
výztuž
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Loading Cases
ZS16 vertical wind pressures
ZS17 concreting vehicle
ZS18 longitudinal wind
ZS19 cross-wind
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0
20
40
60
80
100
120
140
160
180
-1.00-0.80-0.60-0.40-0.200.000.20
Maximal deflection [m]
Rela
tive lo
ad
[%
]
Structural capacity
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Optimization of precast structures
precast prestressed hollow core slabs without shear reinforcement
shear failure test in laboratory … and in nonlinear computer simulation
(crack widths)
0.000866
0.000812
0.000758
0.000704
0.00065
0.000596
0.000541
0.000487
0.000433
0.000379
0.000325
0.000271
0.000217
0.000162
0.000108
0.0000541
-3.02E-12
V1
L1
Output Set: Load Step ID 40
Contour: C:COD CRACK_ATTRIBUTES
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ATENA applications
plain concrete lining
railway tunnel in Prague
typical cross section
outer diameter 6 m
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New Railway Connection in Prague
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New Railway Connection in Prague – tunnels under the Vítkov Hill
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Nonlinear analysis of the tunnel profile
finite element model
5000 elements
1 m longitudinal section
plane stress state
supported by nonlinear springs
reflect soil properties
variants:
various upper vault thickness
plain or reinforced
with or without bottom vault
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Nonlinear analysis of the tunnel profile
finite element model
1 m longitudinal section
plane stress state
supported by nonlinear springs
reflect soil properties
Drucker-Prager ground
variants:
various upper vault thickness
plain or reinforced
with or without bottom vault
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Step 26, NSf-UZL - nevyztuzene osteni 300, MSU, zima, liniove pruzne ulozeni Scalars:iso-areas, Basic material, in nodes, Principal Stress, Max., <-5.027E-01;9.964E-01>[MPa]
-5.027E-01
-4.500E-01
-3.000E-01
-1.500E-01
0.000E+00
1.500E-01
3.000E-01
4.500E-01
6.000E-01
7.500E-01
9.000E-01
9.964E-01
Results from NLA
Iso-areas of
principal stress
maximal (tensile)
unreinforced
ultimate limit state
dead load
creep
shrinkage
temperature in winter
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Results from NLA
normal forces
bending moments
unreinforced
ultimate limit state
dead load
creep
shrinkage
temperature in winter
Step 26, NSf-UZL - nevyztuzene osteni 300, MSP, zima, liniove pruzne ulozeni Cracks: in elements, openning: <-1.544E-04;1.592E-03>[m], Sigma_n: <-1.237E+00;9.998E-01>[MPa], Sigma_T: <1.017E-16;5.182E-01>[MPa]
-5
.03
7E
-04
1
.78
4E
-02
8.0
76E
-03
8.516E-03
-2.745E-02
-1.0
06E-03 -
8.3
30
E-0
3 5.324E
-03
-2.763E-02
1.7
52E
-02
-5
.09
9E
-04
1
.25
2E
-04
-1.248E-01
-4.2
36E
-02
-4.7
66
E-0
2
-4.4
27E
-02
-6.749E-02
-6.697E-02
-1.258E-01 1
.08
1E
-04
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Results from NLA
Crack pattern
unreinforced
ultimate limit state
dead load
creep
shrinkage
temperature in winter
Step 26, NSf-UZL - nevyztuzene osteni 300, MSP, zima, liniove pruzne ulozeni Cracks: in elements, openning: <-1.544E-04;1.592E-03>[m], Sigma_n: <-1.237E+00;9.998E-01>[MPa], Sigma_T: <1.017E-16;5.182E-01>[MPa]
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Results from NLA
Main crack
description
of crack width
max. 1.6 mm
unreinforced
ultimate limit state
dead load
creep
shrinkage
temperature in winter
Step 26, NSf-UZL - nevyztuzene osteni 300, MSP, zima, liniove pruzne ulozeni Cracks: in elements, <2.000E-04; ...), openning: <-1.544E-04;1.592E-03>[m], Sigma_n: <-1.237E+00;9.998E-01>[MPa], Sigma_T: <1.017E-16;5.182E-01>[MPa]
7.4
23E
-04
9.7
72
E-0
4
1.2
69E
-03
1.5
92E
-03
4.4
93E
-04
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BARC, Indie, Containment Pressure Test
Model 1:4
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ATENA
3D shell element
geometry
layers
reinforcement
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3D Analysis – 3.00 design pressure, P = 0.4239 MPa
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0
0.5
1
1.5
2
2.5
3
3.5
4
-0.005 0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 0.04
Radial Displacement [m]
Inte
rna
l P
ressu
re [
MP
a]
Axi-symmetric
3D old
3D new
2D - 3D Analysis – Comparison
Design Pressure 0.1413 MPa
3.2 – 3.5 Pd
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New 3D Model based on BARCOM 2009 workshop – corrected cover of openings
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Safety formats for non-linear analysis - 4 methods
Example:
• bending
• shear - deep beam
• bridge pier – geometric nonlin.
• railway tunnel
Comparative study of different safety formats
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Safety Formats for Nonlinear Analysis
xd
R
RE
Rx - is the structural resistance
obtained by nonlinear analysis
gR - is the global safety factor of the
structural resistance
Ed - is the factorized load effect as in
the case of partial safety factor method
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Safety Format (1), PSF Method
Partial safety factors , ,( ) ( )d G i dd jE R
Use design value of material
parameter to calculate Rd:
design val.= characteristic val.
partial safety factor
30
120
.5
ckcd
c
ff MPa
Action Resistance
Med < Mrd
fyd
fcd
1.0
dd
RE
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Safety Format (2), EN1992-2
,( ) /d G i m RE R
Adjusted “mean” values of material parameters:
0.85cm ckf f 1.1ym ykf f
1.27R All failure modes:
Global safety factor
1.1 x 1.15/1.5
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Safety Format (3), ECOV
Estimate of Coefficient of Variation
Coefficient of variation, assuming lognormal distribution of resistance
Global resistance factor
1ln
1.65
mR
k
RV
R
exp( )m
R R RV 4.7 0.8R
Reliability index Resistance sensitivity
exp( )d m R RR R V
exp( 1.65 )k m RR R V we need
2 analyses
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Safety Format (4), Probabilistic Analysis
Reliability index:
( )P E R
Probability of failure:
( )Z
( 0)P Z
Z E R (1) (2)
EN 1990: Basis of structural design, 2002
~ 4.7
~ 10-6
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Safety and Reliability Factors
Safety factors
scatter – not considered
Probabilistic approach
scatter - considered
Z
Z
m
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Results – probabilistic, SARA+ATENA 120 samples
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Bending Beam
300 6000 (t=1000 mm) 300
300 5f14
77.9 93Ed RdM kNm M kNm
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Example: Deep beam
Tested by: Melvin Asin, Delft University, 1999
Nonlinear, probabilistic analysis by: ATENA, 2006
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Reinforced Concrete Bridge Pier
Horizontal deflection [mm]
Lo
ad facto
r
Interaction diagram
PSF
Mean
EN 1992-2
Characteristic
w/o geom. nonlin.
PSF
Mean
Charact.
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Safety Formats Comparison
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Types of Nonlinear Analysis
Ultimate Limit State – max load
(ULS)
Service Limit State – deflection
(SLS) crack width
Seismic Assessment
(SA) pushover
accelerogram
0.0
0.2
0.4
0.6
0.8
1.0
1.2
1.4
1.6
1.8
2.0
-100 0 100 200 300 400 500 600
Radial Displacement [mm]
Inte
rnal P
ress
ure
[M
Pa]
Radial displ @ z=23 m
Radial displ @ z=10 m
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Types of Nonlinear Analysis
Structural details
reinforcement detailing
special details
problems with
boundary conditions
Overall structural behaviour
redistribution due to cracking
ULS, SLS, SA
bending OK
shear or other local effects
not modelled??
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Modelling Issues
for nonlinear analyses of RC
Columns
bending failure
expected
Use beam
elements with
fibres
Shear + bending
failure
Use solid
elements
Bending
failure
expected
Use shell
elements
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Conclusions
Simulation by nonlinear analysis is used as a standard tool in design practice or for the evaluation of existing structures
• Removes inconsistency in standard design process between linear analysis and non-linear cross-section check
• Provides insight into the structural behavior
• Helps to discover critical locations and failure modes
• May discover additional load-carrying capacity
• Ideal tool for checking reinforcement detailing in complicated D-regions
State of art:
• “Complexity” -> old myth from the 20th century
• Available in many commercial finite element codes
• Computationally more demanding than linear analysis
• Supplement standard design based on linear analysis and section design