FATIGUE BEHAVIOR AND HIGH TEMPERATURE EFFECTS Valter Carvelli - - PowerPoint PPT Presentation

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FATIGUE BEHAVIOR AND HIGH TEMPERATURE EFFECTS Valter Carvelli - - PowerPoint PPT Presentation

GFRP REINFORCED CONCRETE STRUCTURAL ELEMENTS: FATIGUE BEHAVIOR AND HIGH TEMPERATURE EFFECTS Valter Carvelli Politecnico di Milano SOME APPLICATIONS OF GFRP (Glass Fiber Reinforced Polymer) REBARS IN CONCRETE STRUCTURAL ELEMENTS Some


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SLIDE 1

GFRP REINFORCED CONCRETE STRUCTURAL ELEMENTS: FATIGUE BEHAVIOR AND HIGH TEMPERATURE EFFECTS

Valter Carvelli

Politecnico di Milano

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SLIDE 2

SOME APPLICATIONS OF GFRP (Glass Fiber Reinforced Polymer) REBARS IN CONCRETE STRUCTURAL ELEMENTS

Some advantages:

  • No rebars corrosion;
  • Electrical insulation.
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SLIDE 3

AVAILABLE STANDARDS AND GUIDES FOR DESIGN OF FRP REINFORCED CONCRETE STRUCTURES

CHBDC - Canadian Highway Bridge Design Code – CSA “Fibre Reinforced Structures ” ACI 440.1R - American Concrete Institute “Guide for the design and construction of concrete reinforced with FRP bars” JSCE - Japan Society of Civil Engineer’s “Recommendations for design and construction of concrete structures using continuous fiber reinforcing materials” IStructE - British Institution of Structural Engineers “Interim guidance on the design of reinforced concrete structures using fibre composite reinforcement” CNR-DT 203 - Italian National Research Council “Guide for design and construction of concrete structures reinforced with fiber-reinforced polymer bars” ………..……

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SLIDE 4

 High temperature effects on beams  Materials features

Cycle period Load jack A jack B 500000 1000000 1500000 cycles number 2 4 6 8 10 displacement [mm] slab S1 - max load 140kN Jack A: max Jack A: min Jack B: max Jack B: min

 Fatigue behaviour of slabs

OUTLINE

23 200 500 Temperature bottom [oC] 50 100 150 200 Load max [kN] no overlap 55cm overlap bent rebars 35cm overlap 24cm overlap

 Open discussion

Numerical and analytical modelling

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SLIDE 5

MATERIALS FEATURES

Carvelli V, Fava G, Pisani M A. ASCE Journal of Composites for Construction, 2009 Fava G, Carvelli V, Pisani M A. Composites Part B, 2012

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SLIDE 6

Unidirectional pultruded bars (E-glass fibre / vynilester) External surface: sanding of quartz and wrapping of aramidic yarn

Experimental static tensile properties Ø16mm: E ≈ 39 GPa sult ≈ 885 MPa

MATERIALS FEATURES

(Fibre volume fraction ≈ 60%) test of rebars: Ø 16÷40mm

GFRP REBARS

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SLIDE 7

TENSILE STRENGTH VS. TEMPERATURE

MATERIALS FEATURES

GFRP REBARS

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SLIDE 8

MATERIALS FEATURES

Nigro et al., CICE 2008 Conference (CFRP bars)

GFRP REBARS

Wang et al., Composite Structures, 2007 (GFRP + CFRP bars)

TENSILE STRENGTH VS. TEMPERATURE

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SLIDE 9

MATERIALS FEATURES

Experimental measurements of concrete C55/67

STRENGTH VS. TEMPERATURE

CONCRETE

23 200 500 23 200 500

Temperature [oC]

1 2 3 4 5

Tensile strength [MPa]

4.0 2.8 1.1 (indirect tensile test, EN 12390-6) (cylinder strength)

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SLIDE 10

MATERIALS FEATURES

Design quality: C55/67 characteristic cubic strength = 67 MPa Experimental cubic strength (average of 16 samples) ≈ 66 MPa FATIGUE LIFE IN COMPRESSION European Codes: Palmgren-Miner rule

m i i i

N n

1

1

number of intervals with constant amplitude actual number of constant amplitude cycles ultimate number of constant amplitude cycles

The ultimate number of constant amplitude cycles, for max cyclic load of 140 kN applied on a 200x300mm contact area, should be

N = 1.138.000

CONCRETE

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SLIDE 11

GFRP REBARS - CONCRETE ADHESION

MATERIALS FEATURES

6 8 10 12 14 16 18 20 22 24 26 nominal diameter Ø [mm] 5 10 15 20 tmax [MPa] GFRP rebar Steel rebar

PULL-OUT Test BEAM- Test

5 10 15 20 tmax [MPa] Pull-out Beam-test GFRP Ø12mm

Steel rebar Fava G., Carvelli V., Pisani M.A., to appear

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SLIDE 12

Personal knowledges Lack or very few investigations on

  • Fatigue behaviour of the FRP REBARS
  • Fatigue behaviour of the FRP REBARS-CONCRETE ADHESION

MATERIALS FEATURES

Fatigue life domain of fibre–glass sucker rods

(FIBEROD Info Catalog. TX, USA)

Load level in our experiment of slabs for a max load of 140 kN

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SLIDE 13

FATIGUE BEHAVIOUR OF SLABS

Carvelli V, Pisani M A, Poggi C. Composites Part B, 2010

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SLIDE 14

FATIGUE BEHAVIOUR OF SLABS

LOAD CONDITIONS FOR TRAFFIC ON BRIDGES European Codes define five fatigue load models.

Among those the most heavy condition is for a twinned wheel:

  • maximum load of 95 kN,
  • contact area of 40x60cm.

To accelerate the failure of the slabs in the experimental fatigue tests: minimum load in cycles 140 kN (+48%) contact area 20x30cm (-400%) European Code 1 and 2 as guidelines for slab design

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SLIDE 15

Length L = 500 cm Width W = 248 cm Thickness t = 20 cm Span length S = 150 cm

BRIDGE SLABS GEOMETRY

5 . 7  t W 37 . 1  S D D

small influence of free edges minimize the arch effect

FATIGUE BEHAVIOUR OF SLABS

S W t L

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SLIDE 16

Transverse Longitudinal

Longitudinal Reinforcement Transverse Reinforcement

GFRP REINFORCEMENT OF THE SLABS

Ø12/20cm Ø16/10cm Ø16/10cm Ø16/20cm

The bottom reinforcement was designed to reduce the slab deformability: maximum displacement < Span/250 = 6mm bottom top

FATIGUE BEHAVIOUR OF SLABS

Manufacturing

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SLIDE 17

CONSTRAINS SIMULATION

Cylindrical support (Ø 50mm) Layer of rubber (5mm thick)

Service condition

Bilateral constrain (as connectors)

FATIGUE BEHAVIOUR OF SLABS: experimental setup

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SLIDE 18

5 displacement transducers LVDT (max 50 mm)

DISPLACEMENT MEASUREMENT DEVICES

FATIGUE BEHAVIOUR OF SLABS: experimental setup

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SLIDE 19

LOADING SETUP

Hydraulic Jack A Hydraulic Jack B Contact area for European code is 40x60cm. Contact area

20cm 30cm

FATIGUE BEHAVIOUR OF SLABS: experimental setup

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SLIDE 20

Hydraulic Jack A

Spherical Hinge Laminated neoprene plate

LOADING SETUP

FATIGUE BEHAVIOUR OF SLABS: experimental setup

Hydraulic Jack B

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SLIDE 21

FEATURES OF THE LOADING CYCLE

Maximum load for European code is 95 kN

Reproducing a moving wheel

FATIGUE BEHAVIOUR OF SLABS: experimental setup

Slab Test Max load in cycles Frequency [kN] [Hz] S1 cyclic + static 140 1 S2 cyclic + static 290 0.7 S3 cyclic 440 0.2 S4 static

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SLIDE 22

SLAB 1 : max load = 140kN

Max displacement ≈2.5mm < 6mm = Span/250

No failure after 1.500.000 cycles

European codes predict concrete failure after 1.138.000 cycles

FATIGUE BEHAVIOUR OF SLABS

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SLIDE 23

SLAB 2 : max load = 290kN

1 2 3 4 5

Test stopped: excessive deformation after 140.000 cycles

Max displacement ≈12mm

FATIGUE BEHAVIOUR OF SLABS

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SLIDE 24

SLAB 3 : max load = 440kN Failure after 400 cycles

FATIGUE BEHAVIOUR OF SLABS

No bilateral constrain (as damaged connectors)

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SLIDE 25

SUMMARY OF THE FATIGUE TESTS

FATIGUE BEHAVIOUR OF SLABS

Fatigue life prediction > 3 x 108 95 kN

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SLIDE 26

QUASI-STATIC THREE-POINTS BENDING TEST

POST-FATIGUE RESIDUAL PROPERTIES OF SLABS

Reduction with respect to S4 Stiffness Strength S1 45,9% 1,2% S2 76,4% 3,4%

(140 kN) (290 kN)

LOADING-UNLOADING up to 200kN and 400kN RAMP TO FAILURE

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SLIDE 27

QUASI-STATIC FAILURE MECHANISMS S4 S2 S1

POST-FATIGUE RESIDUAL PROPERTIES OF SLABS

UNFATIGUED Post-fatigue 140.000 cycles max load 290 kN Post-fatigue 1.500.000 cycles max load 140 kN

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SLIDE 28

HIGH TEMPERATURE EFFECTS ON BEAMS

Carvelli V, Pisani M A, Poggi C. Composites Part B, 2013

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SLIDE 29

BEAM GEOMETRY

HIGH TEMPERATURE EFFECTS ON BEAMS

Bridge slab for cyclic loading

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SLIDE 30

Longitudinal Reinforcement

GFRP REINFORCEMENTS

(no shear reinforcement)

Continuous rebars (no overlap) Overlap with bent rebars Overlap 56 cm Overlap 40 cm Overlap 24 cm

FIVE CONFIGURATIONS OF REINFORCEMENT

HIGH TEMPERATURE EFFECTS ON BEAMS

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SLIDE 31

HEATING FEATURES

Heating device (max 800 oC)

HIGH TEMPERATURE EFFECTS ON BEAMS

Bottom heating zone

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SLIDE 32

QUASI-STATIC 3-POINTS BENDING after heating

LVDTs Spherical hinge

HIGH TEMPERATURE EFFECTS ON BEAMS

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SLIDE 33

EXPERIMENTAL PROGRAM

LOADING HISTORY

  • Loading up to 10 kN and unload
  • Loading up to 20 kN and unload
  • Loading up to 40 kN and unload
  • Loading up to failure

5 10 15 20 25 LVDT displacement [mm] 50 100 150 200 Load [kN] LVDT 1 LVDT 2

0.2 0.4 0.6 0.8 1 LVDT displacement [mm] 10 20 30 40 50 Load [kN] LVDT 1 LVDT 2

HIGH TEMPERATURE EFFECTS ON BEAMS

Number of specimens Sample Temperature Type 23oC 230oC 550oC 1 2 2 2 2 2 1 3 2 2 1 4 2 5 1 1

Continuous rebars Overlap with bent rebars Overlap 56 cm Overlap 40 cm Overlap 24 cm

Heating time Imposed bottom Temperature [hours] 23oC (RT) 1+1.5 230oC 1+1.5 550oC

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SLIDE 34

HEATING PHASE: TEMPERATURE RECORDING

30 60 90 120 150 Time [min] 50 100 150 200 250 300 Temperature [oC] TC1 TC2 TC3 30 60 90 120 150 180 Time [min] 100 200 300 400 500 600 Temperature [oC] TC1 TC2 TC3

HIGH TEMPERATURE EFFECTS ON BEAMS

Heating time Imposed bottom Temperature [hours] 23oC (RT) 1+1.5 230oC 1+1.5 550oC

Resin Tg ≈ 180 °C ≈400°C ≈130°C Rebars temperature

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SLIDE 35

T T T T T continuous rebars bent rebars 56cm overlap 40cm overlap 24cm overlap

HIGH TEMPERATURE EFFECTS ON BEAMS

LOADING RESPONSE

56cm

  • verlap

RT continuous rebars

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SLIDE 36

HIGH TEMPERATURE EFFECTS ON BEAMS

LOADING RESPONSE

T T T T T continuous rebars bent rebars 56cm overlap 40cm overlap 24cm overlap

56cm

  • verlap

continuous rebars

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SLIDE 37

Overlap 56 cm

Room Temperature tests: FAILURE MECHANISM

Continuous rebars (no overlap) Overlap with bent rebars Overlap 40 cm Overlap 24 cm

HIGH TEMPERATURE EFFECTS ON BEAMS

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SLIDE 38

550oC tests: FAILURE MECHANISM

Continuous rebars Overlap with bent rebars

HIGH TEMPERATURE EFFECTS ON BEAMS

Overlap 56 cm

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SLIDE 39

HIGH TEMPERATURE EFFECTS ON BEAMS Numerical and analytical modelling

Pagani R, Bocciarelli M, Carvelli V, Pisani M A. Engineering Structures, 2014

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SLIDE 40

HIGH TEMPERATURE EFFECTS ON BEAMS: Modelling

Analytical model: constitutive behaviour of materials GFRP REBARS

Hypotheses  linear elastic behaviour of GFRP and elasto-“plastic” of concrete  perfect bond between concrete and GFRP rebars  planarity of the cross-section after bending throughout temperature exposure

Elastic modulus vs. temperature

   

12 4.3

0.28 20 0.28 6 10

g g

E T E C T

     

Nigro et al. Composites Part B, 2014

     

 

   

3 4

20 tanh 7.91 10 320.35 0.525 0°C T 400°C 20 0.25 4.17 10 400 T 400°C

 

                       

g g g

E C T if E T E C T if

Yu et al. Composite Structures, 2013

Thermal strain

   

6

6.58 10 20

th g T

T C

     

coefficient of thermal expansion

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SLIDE 41

HIGH TEMPERATURE EFFECTS ON BEAMS: Modelling

CONCRETE

EN 1992-1-2:2005, Euro Code 2 Stabler J. The University of Queensland, 2000

Elastic modulus vs. temperature Thermal strain

 

4 6 11 3 3

1.8 10 9 10 2.3 10 20 700 14 10 700 1200

th c

T T if C T C T if C T C

   

                      

     

 

 

2

1 0.2 0.01 0.2 0.01 0.01 0.2 20 20 800 800                   

c c

T T E C if C T C E T if T C

Tensile strength vs. temperature

     

20 20 100 100 1.0 20 100 600 500

ct ct ct

f C if C T C f T T f C if C T C                        

EN 1992-1-2:2005, Euro Code 2

Analytical model: constitutive behaviour of materials

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SLIDE 42

HIGH TEMPERATURE EFFECTS ON BEAMS: Modelling

CONCRETE

Sargin M. University of Waterloo, 1971 Carreira D C, Chu K H. ACI Journal 1986

Tensile stress-strain relationship Compressive stress-strain relationship

EN 1992-1-2:2005, Euro Code 2

     

2 2 2 2 2

2 1 1

el el c c el el c c el el c c cu c el c el c

D f T if T D              s                

2

0.002

el c

 

         

10 1

el c ct el ct el el el c ct c ct el c el ct

f T T if T T T

           s                       

el ct ct c

T f T E T   1.5  

Analytical model: constitutive behaviour of materials

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SLIDE 43

HIGH TEMPERATURE EFFECTS ON BEAMS: Modelling

ANALYTICAL MODEL

     

( ) el el el c g cj cj cj cj cj gi gi gi gi j i A

M y dA y w b y A   s    s   s 

  

weights of the Gaussian integration

moment M corresponding to the curvature

GFRP reinforcement area section width at integration point

tot

non-linear equation solved by an iterative Newton–Raphson scheme

Position of the neutral axis

tot G tot

X y    

total axial strain in the centre of gravity

* * tot tot j j j j beam

M dx w M     

 

Section displacement

bending moment distribution due to a single unit virtual force

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SLIDE 44

HIGH TEMPERATURE EFFECTS ON BEAMS: Modelling

NUMERICAL FE MODELLING of beam with continuous rebars

Plane stress model (2D) Three-dimensional model (3D)

reinforcement modelled as strips having equivalent area of the GFRP bars

d.o.f. n° CPS4T elements 7239 2268 d.o.f. concrete n° C3D8T elements rebars n° C3D4T elements 170796 31992 23178

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SLIDE 45

HIGH TEMPERATURE EFFECTS ON BEAMS: Modelling

NUMERICAL FE MODELLING of beam with continuous rebars

HEATING PHASE SIMULATION (adopted in the analytical model)

Concrete moisture content

2D model 3D model Prediction of the temperature distribution

Experimental imposed temperature

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SLIDE 46

HIGH TEMPERATURE EFFECTS ON BEAMS: Modelling

ANALYTICAL and NUMERICAL RESULTS

Beam with continuous rebars - ROOM TEMPERATURE

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SLIDE 47

HIGH TEMPERATURE EFFECTS ON BEAMS: Modelling

ANALYTICAL MODEL RESULTS

Beam with continuous rebars - MAX TEMPERATURE 550°C

   

12 4.3

0.28 20 0.28 6 10

g g

E T E C T

     

     

 

   

3 4

20 tanh 7.91 10 320.35 0.525 0°C T 400°C 20 0.25 4.17 10 400 T 400°C

 

                       

g g g

E C T if E T E C T if Nigro et al. Composites Part B, 2014 Yu et al. Composite Structures, 2013

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SLIDE 48

HIGH TEMPERATURE EFFECTS ON BEAMS: Modelling

ANALYTICAL and NUMERICAL RESULTS

Beam with continuous rebars - MAX TEMPERATURE 550°C