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Impact of Accelerated Pavement Testing (APT)
on Pavement Engineering
Jean-Maurice BalayJean-Michel Piau
Pierre HornychChantal de La Roche
LCPC - FranceTRB 2008 - Worshop 110 - Validation of advanced flexible pavement modeling
with accelerated Pavement testing data - Sunday 13 January 2008.
Contents
1 LCPC - January 13, 2008
• Introduction• LCPC activities on pavement design and modeling
• Presentation of LCPC APT facilities
• Use of APT for pavement engineering• Advantages, Limits and important rules
• Examples of APT experiments and their impacts– Fatigue experiments
– Airbus Pavement Experimental Program
– Use of APT for pavement structure innovation
• Conclusion
Introduction
LCPC activities on pavement design and modeling
3 LCPC - January 13, 2008
• Contribution to the development and evaluation of French pavement design methodology
• Development of models for :• Low trafic pavements : Non linear behaviour of soils and unbound
granular materials, prediction of rutting
• Bituminous pavements : visco-elastic behaviour, fatigue, visco-plastic behaviour (rutting)
• Rigid pavements : study and modelling of reflective cracking
• Airfield pavements ; impact of multi peak loading
• Design of innovative pavement structures
Presentation of LCPC APT facilities
4 LCPC - January 13, 2008
Fatigue test track – large circular test track (pavement length 120 m)
“FABAC” Machines : mobile machines – simulation of full wheel loading on small length (2m)
LCPC Fatigue test track
5 LCPC - January 13, 2008
• Circular outdoor facility, built in 1984• Track width up to 6 m - length 122 m (radius 19.5m)• Radius of rotation : adjustable from 15 m to 20 m• Maximum speed 13.5 rpm (100 km/h at radius 19.5 m)• Simulation Transverse wandering of real traffic can be
reproduced• Various types of loads from 8-ton single-axle to 30-ton
multiple-axle (only a half-axle per arm)• 3 test sites - one including a water table
control system (pumping station)
Experiments performed in partnership withRoad authorities, public or private companies,European research program
Use of APT for pavement engineering
7 LCPC - January 13, 2008
Performance models – Two main different approaches, almost disconnected today ?
• Extensive survey campaigns of road networks (ex: at national scale) & global statistical approach
• Tool: statistical analysis of broad data base, including equivalent pavement structures at different ages and supporting different traffic
• Efficient way to derive “evolution laws” for PMS (maintenance & reinforcement planification) on standard pavement techniques
• Local mechanistic approach on test sections, looking more deeply to the nature of pavement materials and structures and to their behaviors
• Tools: Real loading test, APT, laboratory testing, constitutive laws, structural models
• More “introspective” approach ; specially recommended for innovation testing (materials, structures)
Advantages and limits of APT
8 LCPC - January 13, 2008
Advantages• Well controlled pavement construction and experimentation conditions
(load, traffic, temperature,…)
• Internal instrumentation and detailed monitoring of pavements
• Response in relatively short time owing to the acceleration of traffic
• Possibility to make comparative tests
• Good quantitative knowledge of the resilient behavior of the structures and damaging mechanisms
Limits
• Not representative of real traffic & climatic variations
• No long term ageing of materials
• Obtained results more comparative than intrinsic
Important rule for APT success
9 LCPC - January 13, 2008
• Build a pavement dedicated to the distress to be studied and trynot to mix pavement distresses
• Examples :• permanent deformation of bituminous layers
use hydraulically bound base and sub base• fatigue of bituminous materials
avoid using surface layer that could hide bottom to top cracks• ….
Examples of APT experiments and their impacts
Experimenton fatigue behaviour
Objectives of the experiments
12 LCPC - January 13, 2008
• Comparison of fatigue behaviour of different bituminous materials, with different binders
- in the laboratory, using different fatigue tests- in pavements
• Evaluation of the French fatigue design approach for bituminous pavements
• Determination of shift factor to be applied to High Modulus Mixtures (French EME)
• 3 full scale experiments on the LCPC test track (between 1990 and 1994)
Third “fatigue” experiment
13 LCPC - January 13, 2008
4 structures : 8 or 10 cm thick bituminous layer40 cm thick granular baseclayey subgrade : E = 30 to 40 MPa
3 bituminous materials:BBB : Bituminous concrete with 50/70 grade bitumen (reference)BBS : Bituminous concrete with 50/70 polymer modified bitumenEME : high modulus bituminous mix, with 10/20 grade bitumen
2 structures – 8 and 10 cm thick
Loading conditions :65 kN dual wheel load, 72 km/h3.2 million loads applied
In situ performance of the 4 structures
14 LCPC - January 13, 2008
Cracking extent
010
2030
4050
6070
8090
100
0 500000 1000000 1500000 2000000 2500000 3000000 3500000
Number of loads
Exte
nt o
f cra
ckin
g (%
)
Struct. 1 - BBB
Struct. 2 - BBS
Struct. 3 - EMEStruct. 4 - EME
Laboratory fatigue tests
15 LCPC - January 13, 2008
5 different test procedures
Procedure Type of loading
Fatigue design method
16 LCPC - January 13, 2008
Criterion on maximum tensile strain :
( ) ( ) k10NEf,b6
6adt ⋅⋅θε=ε
ε6(θ,f) : Strain leading to failure for 106 cycles,depending on temperature θ and frequency f
NE : number of standard axle loadsb : slope of the fatigue linek : shift factor, taking into account the risk of failure, the bearing capacity of the soil, the difference between the model and observed pavement behaviour
Predicted pavement life: ( )b1
6
t6f,k
10NE ⎟⎟⎠
⎞⎜⎜⎝
⎛θε⋅
ε⋅=
Comparison of design predictions and field performance
17 LCPC - January 13, 2008
Calculation of shift factor k (k = 1 exact prediction of pavement life) ( )
b1
6
t6f,k
10NE ⎟⎟⎠
⎞⎜⎜⎝
⎛θε⋅
ε⋅=
k
Fatigue test procedure S1BBB
S2BBs
S3EME 8 cm
S4EME 10cm
3 – strain control Continuous
1,58 1,28 1,14
0,8
1,10
1,20
5 – strain control, with rest periods
1,04 1,03 0,8
6 – stress control, continuous
3,21 2,57
10 – stress control, with rest periods
1,73 1,49 1,08
Conclusions – “fatigue experiments”
18 LCPC - January 13, 2008
• Large differences in fatigue life predictions from different fatigue test procedures,
• Fatigue tests with rest periods seem more representative of in situ behaviour
• For the high modulus material (EME), the stress controlled fatigue test seems more representative of in situ behaviour.
more research needed on intrinsic characterisation of fatigue in laboratory
• Correction between in situ and lab behaviour dependent on the type of material (BB/EME)
Shift factor for EME = 1,0
[De la Roche et al, TRB 94, ISAP 98] [Rivière et al, ISAP 98
Airbus Pavement Experimental Program
Airbus experimental program on flexible pavements – 1998-2003
20 LCPC - January 13, 2008
30m 30m 30m 30m
Section DAC 8 cm
BAC24 cmUGA 1.40 m
CBR 3
Section CAC 8 cm
BAC 24 cmUGA 0.60 m
CBR 6
Section BBBSG 8 cmGB3 24 cmGNT 20 cmSol CBR 10
Section ABBSG 8 cmGB3 24 cmSol CBR 15
Objectives of the Airbus experimental program
21 LCPC - January 13, 2008
Tests on 4 instrumented pavement structures with soils of different bearing capacity (CBR 3 to 15)
Simulation of loads of different aircrafts , using a load simulator
Objectives :
Study of the behaviour of flexible airfield pavements under heavy aircraft loading conditions
Evaluation of the possibility of applying the French road pavement design method to flexible airfield pavements
Observed pavement performance
22 LCPC - January 13, 2008
Main mode of distress of the flexible pavements = ruttingNo fatigue cracking - densification of the bituminous layers under heavy loading
-1.80
-1.60
-1.40
-1.20
-1.00
-0.80
-0.60
-0.40
-0.20
0.00
1000/2000 1000/3000 1000/4000 1000/5000
Max
rut d
epth
(cm
)Load 1
Load 2
Load 3
Load 4
Evolution of rutting Section C – CBR 6
Number of loads
Linear elastic calculations (ALIZE Software)
23 LCPC - January 13, 2008
XX XX
A380 Load configuration
Prediction of vertical strains at top of subgrade (structure C)
0
200400
600
8001000
1200
-14 -12 -10 -8 -6 -4 -2 0 2Transversal profile XX (m)
µdé
f
4 wheels 4 wheels6 wheels 6 wheelsMeasurement Alizé software
Results of linear elastic calculations
24 LCPC - January 13, 2008
Good prediction of vertical strains in granular layers and subgrade
Poor prediction of maximum tensile strains at bottom of bituminous layers :• Maximum values poorly simulated
• Discordance in directions of maximum tensile strains εt:
Measurements : εt transversal > εt longitudinal
Calculations : εt longitudinal > εt transversal
⇒ Attempt to take into account viscoelastic behaviour
ACεtrans.
εlong.
Visco-elastic model for bituminous materials
25 LCPC - January 13, 2008
HUET - SAYEGH MODEL (1965)
10
100000
060phase angle, (°)
E0
E∞δ, k
h E MPa E MPak h
∞ = == = =
25000 452 7 0 27 0 7
0; ;, ; , ; ,δ
Black space
E E E Ei ik h*( , )
( ( )) ( ( ))ω θ
δ ωτ θ ωτ θ= +
−
+ +∞− −0
01
Huet-Sayegh’s model measurements
E*
, MP
a
3000
0 5000 25000
Cole & Cole axes
Real(E*), MPa
Im(E
*), M
Pa
Finite element model : module CVCR of CESAR-LCPC
26 LCPC - January 13, 2008
Modelling of a pavement under moving wheel load (in 3D)
Hypotheses : Constant speed V
Constant properties along x
V zy
O' O x
σ( , y, z) ε(X, y, z)
X’
V zy
O' O x
σ( , y, z) ε(X, y, z)
Calculation in the referential of the moving load (O’, X’, y ,z) X’ = x +VtStatic mechanical problem - no time stepsModification of the visco -elastic law : becomes a non - local law
Models available in CVCR :Linear and non linear elasticity ( Boyce model, k-θ model)Huet-Sayegh visco-elastic model
27 LCPC - January 13, 2008
- 2 0 0
- 1 5 0- 1 0 0
- 5 0
05 0
1 0 0
2 0 3 0 4 0 5 0 6 0 7 0 8 0
measurementmeasurement
calculations
εtlongitudinalbase AC
µµstrainstrain
time (s)time (s)
-6 0 0
-4 0 0
-2 0 0
0
2 0 0
2 0 3 0 4 0 5 0 6 0 7 0 8 0
measurement
calculations
εttransversalbase AC
µµstrainstrain
time (s)time (s)
Viscoelastic modelling of strains at bottom of bituminous layers
Load : 6 wheel bogie 240 kN per wheel
First conclusions of the Airbus experiment
28 LCPC - January 13, 2008
Main mode of distress of the flexible pavements = ruttingNo detectable fatigue of bituminous layers, despite high tensile strains
Modelling of resilient behaviour
- Reasonable prediction of vertical strains in subgrade with linear elastic calculations.
- Visco-elastic modelling necessary to predict correctly strains in bituminous layers
Modelling of fatigue- Need to adapt the fatigue tests to aeronautical loading conditions
(high strain levels ≈ 400 µstrain, lower number of cycles (104))
Rutting :
Need to develop suitable design criteria and specifications for resistance to rutting of materials (bituminous and unbound)
Use of APT for pavement structure innovation
Grave-Mousse test at LCPC’s APT facility
30 LCPC - January 13, 2008
Grave-Mousse ®- new material for treated road bases developed by EJL Contractor (now EUROVIA) since about 10 years. - bitumen-foam treated aggregates, used for new pavement as for overlay construction
- New pavement structure and innovative concept using Grave-Mousse in the middle part of a three-layer structure design model to be defined and validated- In overlay, functioning and endurance of this new material under heavy traffic to be checked.
Grave-Mousse test at LCPC’s APT facility
31 LCPC - January 13, 2008
Experiment with LCPC’s APT facility :
• Partners : Private contractor EJL• Fatigue test performed from July 1995 to March 1996• 3 overlays and 1 new pavement, 28 m long x 3.5 m width• 2.87 millions single axle load from 45 kN to 85 kN /twinned
wheels, equivalent to 4.3 millions of the French standard load (130 kN/single axle) ie about 15 years of service on average trafic national network
• Load speed: - 44 km/h until 70 000 loadings (consolidation stage)- 68 km/h for all the other loadings.
The 4 structures tested
32 LCPC - January 13, 2008
BFTA 10 cmCracked AC 7cm
UGA 40 cm
Spoilt micaschist 2 m
Overlay structure 3
AC 8 cm (reference)Cracked AC 7cmUGA 40 cm
Spoilt micaschist 2 m
Overlay structure 1
HMAC 6 cmBFTA 10 cmHMAC 6 cm
Spoilt micaschist 2 m
New pavement structure 4
ESA 10 cmCracked AC 7cmUGA 40 cm
Spoilt micaschist 2 m
Overlay structure 2
Rotation radius of loads : 18 m
3.5 m
AC : asphat concrete BFTA : bitumen-foam treated aggregatesESA : emulsion stabilised aggregates HMAC : high modulus asphalt concreteUGA : untreated graded aggregates
Cracking and rutting vs traffic
33 LCPC - January 13, 2008
0
20
40
60
80
100
0.00 0.50 1.00 1.50 2.00 2.50 3.00
Equivalent traffic - 130 kN standard loads (millions)
Crac
king
exte
nt (%
)
Overlay structure 1 (AC) Overlay structure 2 (ESA) Overlay structure 3 (BTFA) New structure 4 (BFTA)
05
1015202530
0.00 1.00 2.00 3.00 4.00Equivalent traffic - 130 kN standard loads (millions)
Ruttin
g de
pth
(mm)
New structure 4: dammage mechanism
34 LCPC - January 13, 2008
Typical horizontal strains profiles measured under the 65 kN standard load
HMAC
BFTA
HMAC
-25
-20
-15
-10
-5
0-150 -100 -50 0 50 100
Horizontal strains (µstrains)
Dept
h (c
m)
Untrafficked areas
Longitudinal strain Transversal strain
Trafficked areas
-25
-20
-15
-10
-5
0-150 -100 -50 0 50 100
Horizontal strains (µstrains)
Dept
h (c
m)(tensile strains are positive)
failure area (?)
New structure 4: dammage mechanism
35 LCPC - January 13, 2008
Trench in the new structure 4 at the end of the experiment
HMAC 6 cm
BFTA 10 cm
HMAC 6 cm
Subgrade (spoilt micaschist)
Failure areahorizontal shear crack
Wheel path
Numerical modeling: main results
36 LCPC - January 13, 2008
Theoritical modeling:• multilayer elastic model (Burmister). Young moduli are back-
calculated from deflections, curvature radii and strains measured.Young modulus (15°C, 10Hz)
- reference AC : 10 000 Mpa- BFTA : 4 000- ESA : 2 500- Cracked AC : 2 000
• Fatigue behavior evaluated from fatigue laboratory tests, and calibrated by ajustement with experimental results.
• Scattering of the fatigue parameters are taken into account, leading to a probabilist determination of the pavement dammagedue to the traffic.
• The theoretical risk of failure is assimilated to the cracking extent.• New structure 4 : shear failure plane is modelized by a low
modulus thin layer (2 cm thick, at 2 cm above the BFTA/HMAC interface, Young modulus 750 MPa).
Numerical modeling: main results
37 LCPC - January 13, 2008
New structure 4 : internal shear en tensile stresses
Shear stresses at the midlepart of the BFTA layer
Vertical distribution of stresses in the BFTA
-16
-14
-12
-10
-8
-6
0 0.05 0.1 0.15 0.2 0.25 0.3Stresses (MPa)
Depth
(cm)
Major stress S1Maximal shear stress
(tensile stresses are positive)
-0.3
-0.2
-0.1
0
0.1
0.2
0.3
-1.5 -1 -0.5 0 0.5 1 1.5Distance to the load axle (m)
Shea
r stre
ss σ
xz (M
Pa)
Standard twinned wheel load (65kN)
Numerical modeling: main results
38 LCPC - January 13, 2008
Measured and calculated evolution of cracked area
0
20
40
60
80
100
0.00 0.50 1.00 1.50 2.00 2.50 3.00Equivalent traffic - 130 kN standard loads (millions)
Crac
king
exte
nt (
%)
ST1 reference AC - measures
ST2 ESA - measures
ST3 BFSA - measures
ST4 HMAC/BFSA/HMAC measures
ST1 reference AC - model
ST2 ESA - model
ST3 BFSA - model
ST4 HMAC/BFSA/HMAC model
General Conclusions
39 LCPC - January 13, 2008
APT is a useful tool for :• Identification of pavement deterioration mechanisms, and suitable
models • Validation of models• Experimentation of innovative structural design• Improvement of laboratory test proceduresBut validation on real pavement sections is also necessary
Recent research at LCPC on design /performance models focuses in particular on :
• Prediction of rutting
• Design of airfield pavements or special pavements (ex: industrial platforms) subject to heavy, complex loads
• Viscoelastic behavior of bituminous pavements and development softwares based on analytical models such as Viscoroute-LCPC.
References – Research on pavement modelling
40 LCPC - January 13, 2008
•Bitumen Cracking modeling (Nguyen, 2006) (Chailleux, ICAP2006)
•Damage modeling (Bodin, 2002) (Bodin et al., ASCE2004), ….
•Visco-elastic structural model (Duhamel et al., BLCPC2005) (Chabot et al, ICAP2006), …
•Cracking structural model (Tran, 2004) (Chabot et al., BLPC2005), ….
•Visco-plastic modeling (Nguyen, 2006) (Nguyen et al., ICAP2006), …
•Non linearity modeling for GNT and soil material (El Abd, 2006) (Hornych et al., RMPD2006 or 2007) …
Additionnal not presented
Model for the prediction of rutting in unbound pavement layers
Developed in European project SAMARIS (2002-2006)
SAMARIS
42 LCPC - January 13, 2008
• SAMARIS : European project of the 5th PCRD• 2002-March 2006• Pavement and Structure Streams
• Task 5 : Development of a performance-based approach for the prediction of rutting of unbound pavement materials
• Selection of permanent deformation models for unbound granular materials
• Development of a structural method of calculation of rutting of unbound pavement layers
• Comparison with results of ALT full scale pavement experiment
Laboratory study of permanent deformations
43 LCPC - January 13, 2008
Test method : cyclic triaxial test Advantages : realistic simulation of « stress paths » due to traffic loading
Test proceduresTest equipment
p = (σ1+2σ3)/3 q = (σ1-σ3)
0
100
200
300
400
500
600
0 100 200 300 400
q/p = 1
q/p = 1,5
q/p = 2
q/p = 2,5
P (kPa)
q (kPa)
0
20
40
60
80
100
120
0 50000 100000 150000 200000
Number of cyclesPe
rman
ent
axia
l str
ain
(10-
4 )
Selected permanent deformation models
44 LCPC - January 13, 2008
2 modelling approaches :
• Routine level : utilizable for designEmpirical permanent deformation model
• Advanced level : for research or analysisElasto-plastic model with isotropic and kinematic hardening Chazallon (2000)
)q,p(g).N(f)N( maxmaxp =ε 1 Gidel (2001)
45 LCPC - January 13, 2008
Example of calibration of empirical permanent deformation model
[ ])(
1.1.)(
max
max
max
011
pq
psmp
LNNn
a
Bpp
−+⎥⎦
⎤⎢⎣
⎡⋅−= −εε Gidel (2001)
0
50
100
150
200
250
300
0 50000 100000 150000 200000 Number of cycles
ε 1p (1
0-4)
∆q/∆p = 1
∆q/∆p = 2
∆q/∆p = 2,5
Empirical model
Maraichère UGM
Cyclic Triaxial Tests atw = 5 %
Structural modeling approach
46 LCPC - January 13, 2008
Main hypothesis : For one cycle
Separate modelling of resilient behaviour and permanent deformations
Three steps :
1. 3D Finite Element calculation of the stress fields in the pavement structure using the resilient behaviour (non linear elastic, visco-elastic models)
2. Use of the stress fields and stress path to calculate permanent strains at the different points of the pavement in the vertical transversal plane
3. Calculation of the displacement field (rutting)
ep ε<<εδ
- FEM method (program ORNI) : 3D structural calculation.- Simplified method: integration of ε1
p in the vertical direction
Modelling of a full scale experiment
47 LCPC - January 13, 2008
5 low traffic pavement structures (each 25 m long)Full scale loading conditions : 65 kN dual wheel load, 72 km/h1.5 million loads appliedLow water table level ( –2.6 m)
Experiment performed in 2003 on the LCPC fatigue test track
Modelling of structure 4
48 LCPC - January 13, 2008
14
6
10
1821
18
10
64
10
5
10
15
20
25
-50 -40 -30 -20 -10 0 10 20 30 40 50position (cm)
perc
enta
geof
load
s(%
) Lateral load distribution
0
5
10
15
20
25
30
0 500000 1000000 1500000 2000000Number of loads
rut
dept
h(m
m)
0
20
40
60
80
100
120
perc
enta
geof
sur
face
cr
acke
d(%
)
mean rut depthmin. rut depthmax. rut depthextent of cracking (%)
UGM
Soil
Structure 46.5 cm
50 cm
2.24 m
Evolution of rutting and cracking
Modelling hypotheses
49 LCPC - January 13, 2008
Modelling of rutting of UGM layer and subgrade (empirical model)Simulation of load wandering and variations of temperature with traffic
Temperature distribution used for calculations
Per
cen
tage
of a
pplie
dlo
ads
(%)
0
6
18
31 29
16
0 00 0
5
17
60
19
0 00 0
42
24
16 16
200
4
42
26
8
2 20 1
34 33
29
2 1 0
11
21
52
13
30 0 0
16
0
10
20
30
40
50
60
70
7-10 10-15 15-20 20-25 25-30 30-35 35-40 40-45
0-50.000 Loads
50.000-100.000 Loads
100.000-200.000 Loads
200.000-500.000 Loads
500.000-1.000.000 Loads
1.000.000-2.000.000 Loads
Temperature (°C)
Examples of rut depth calculations
50 LCPC - January 13, 2008
220cm
• Bituminous concrete : linear elastic• UGM : non linear elastic+ empirical permanent deformation model• Soil : linear leastic E = 100 MPa, n = 0,35
Pavement structure Loading : 65 kN load (single or dual wheel)
1.5 million loads - Constant temperature8cm
50cmUGM
SOIL
Stress paths in UGM layer
0
100
200
300
400
500
600
0 50 100 150 200 250p (kPa)
q (k
Pa)
z = -0.18 m
z = -0.43 m
3D mesh modelling of resilient behaviour
Calculation : influence of lateral load wandering
51 LCPC - January 13, 2008
0
0.5
1
1.5
2
2.5
3
0 400000 800000 1200000 1600000
Number of loads
Max
imu
m r
ut
dept
h(m
m)
With wanderingWithout wandering
Low influence of lateral wandering
No lateral Lateral wandering wandering (11 positions )
Evolution of maximum rut depth
Rut profiles after 1.5 million loads (single wheel) :
52 LCPC - January 13, 2008
0123456789
10
0 400000 800000 1200000 1600000Number of loads
Max
imu
m r
ut
dept
h(m
m)
T=27,5°
T=23°
T=35°
T=15°
-1400
-1200
-1000
-800
-600
-400
-200
0
-1.5 -1.0 -0.5 0.0 0.5 1.0 1.5
Lateral position y (m)
w (
mm
/10
0)
Rut profiles for different Temperatures (8.5 to 42.5°C)
Large influence of temperature
Evolution of maximum rut depth for different temperatures :
Influence of wearing course temperature
Comparison of model with experiment
53 LCPC - January 13, 2008
0
2
4
6
8
10
12
0 500000 1000000 1500000 2000000Number of Loads
max
imum
rut d
epth
(mm
)
ORNI - w = 5 %ORNI - w = 4 %Min. Mean experimentMax.
0
2
4
6
8
10
12
0 500000 1000000 1500000 2000000Number of loads
Max
imum
rut d
epth
(mm
)
Max. Mean experimentMin. ORNI w = 4 % + soilRoutine method
Rutting of UGM only
Rutting of UGM + soil
Conclusions – Modelling of rutting
54 LCPC - January 13, 2008
• First results encouraging but difficulty to simulatereal in situ conditions (temperature and moisture variations…)
• Models predict a too fast stabilisation of permanent deformations
Perspectives :
- more detailed evaluation of ORNI
- Improvement of the models for unbound materials
- Modelling of permanent deformations of bituminous materials