SEAUPG 2002 CONFERENCE
1
Top-Down Cracking: Causes and Potential Solutions
Dr. Rey Roque, P.E. University of Florida
352-392-9537
IntroductionSurface-initiated longitudinal wheel path cracking:
Common mode of failure Recently identified Mechanisms now better understoodOccurs primarily under critical conditionsExisting design methods are inadequateUnderstanding leads to more resistant pavements
BackgroundIn the Past, Cracking Assumed to AlwaysStart at Bottom of AC Layer (Structure has a Strong Effect)
Have evaluatedeffects of factorson response atthis location
CRACKING IN WHEEL PATHS
CORE EXTRACTED FROM FIELDObjectives
To Summarize Findings Related to Top-Down Cracking- Mechanisms for Initiation and Propagation- Key Factors Dominating the Mechanisms- Implications for Mitigation and Design (improved guidelines for mixture and pavement design)
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Pavement Surface Stresses
Tire-Pavement Interface Stresses- Including lateral stressesThermal StressesPavement Structure Effects
Layer Stiffness and Thickness
Measured Tire-Pavement Interface Stresses
(Smithers Scientific Services, Inc.)
16 Transducers
Bed Motion
Tire RollingDirection
Bed
σz δz
σy δyσx δx
Tire
Transducer Detail
Transverse Contact Stresses
. . . . .
Radial (R24.5)Truck Tire
Transverse Stress, σxx
Tension
Compression
Transverse Surface Stress Distribution
-10-8-6-4-202468
10
0 50 100 150 200 250 300Transverse Distance, X (mm)
Tran
sver
se S
tres
s,
xx (
MPa
)
Specified Load/Pressure
Tension
Compression
1 3 4 52Tread
Thermal Stress
-1-0.8-0.6-0.4-0.2
00.20.40.60.8
1
0 24 48 72Time (hr)
Ther
mal
Str
ess
(MPa
) 0 mm Depth50 mm Depth100 mm Depth
Aged AC-30
Findings for Crack Initiation
Primary Contributors to Surface-Initiated Longitudinal Wheel Path Cracking- Transverse contact stresses induced by
radial truck tires- Thermal stresses- Age-Hardening near surface
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Propagation of Top-Down Cracks
Surface Contact Stresses (Tire or Thermal) Cannot Explain Propagation of Top-Down Cracks- Continued work to identify mechanisms and factors controlling propagation
RANGE OF FACTORS
• Load Spectra Positioning with respect to crackRealistic tire contact stresses (vertical and lateral)
• Cracks and Discontinuities Crack depth
• Asphalt Pavement ThicknessInterstate highway pavements – thick/stiff
• Surface and Base Layer Stiffness
• Stiffness Gradients Induced in Asphalt Layer Daily temperature and environmental fluctuations
STRUCTURAL PARAMETERS
4, 8”
12”
90”
AC
Complex Vertical LoadPositions: Wide Rib, 7”, 15”, 20”, 25”, 30”
Crack Length0.25”, 0.5”, 0.75”, 1.0”,1.5”
E1 = 800,1200ksiBase
E2 = 20,44.5ksi
SubgradeE3 = 14.5ksi
MODELING SYSTEM – STEP 1
Rollers Applied to Bottom Side
Vertical and Transverse Tire Contact Load
AC Layer
Base Layer
Subgrade Layer
Predict Vertical and Horizontal Reaction Forces
Boundary ConditionApplied to Sides:
Rollers
Pins Applied to Bottom Corners
MODELING SYSTEM – STEP 2
Boundary ConditionApplied on Sides:
Rollers
Predicted Vertical and Horizontal Reaction Forces Applied Along Bottom Nodes
Crack
AC Layer
Vertical and Transverse Tire Contact Load
Spring Constant “k” Applied
Model geometry of crack & increase mesh refinement
USE OF FRACTURE MECHANICS
( )
−+=
EKKJ III
222 1* υ
Crack Depth
Tire Loading
PredictedStressesUnder Crack Tip
Stresses Predicted in Process Zone (Contours) Ahead of Crack TipProvides local
description ofcrack tip region
Mode I Stress Intensity Factor, KI≈ lim σxx ∗ (2πr)1/2
r→0
Mode II Stress Intensity Factor, KII≈ lim τyx ∗ (2πr)1/2
r→0
Fracture Energy Release Rate, J = (KI2 + KII
2) ∗ 1-ν2
E
SEAUPG 2002 CONFERENCE
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PARAMETRIC STUDY - STRUCTURE
-250-225
-200-175
-150-125
-100
-75
-50-25
025
5075
100125
150175
200225
250
0 0.25 0.5 0.75 1 1.25 1.5 1.75 2
Crack Length, a (in)
Mod
e I a
nd II
Fra
ctur
e K I
, K
II (
psi-(
in)0.
5 )
K1 - E1:E2 = 800:20ksiK1 - E1:E2 = 800:44ksiK1 - E1:E2 = 1200:20ksiK1 - E1:E2 = 1200:44ksiK2 - E1:E2 = 800:20ksiK2 - E1:E2 = 800:44ksiK2 - E1:E2 = 1200:20ksiK2 - E1:E2 = 1200:44ksi
• Tension >> Shear failure at crack tip• Higher stiffness ratio increases tension at crack tip
E1:E2= 60
E1:E2= 27E1:E2= 40
E1:E2= 18
Load Position/Crack Length
Undeformed Pavement
CRACK
LOAD
CRACK
LOAD
Deformed Pavement
Transverse Stress DistributionAlong Surface of PavementTensile
Zone (+)
(-)Compressive
Zone
(+)(-)
PARAMETRIC STUDY - LOADING
0
25
50
75
100
125
150
175
200
225
250
0 0.25 0.5 0.75 1 1.25 1.5 1.75 2
Crack Length (in)
Mod
e I F
ract
ure,
KI (
psi-(
in)0.
5 )
Crack Located Under W ide Rib
Crack Located 20" Away From Center of Load
Crack Located 25" Away From Center of Load
Crack Located 30" Away From Center of Load
E1:E2 = 800:20 ksi
Load position – most critical factor for tension at crack tipSTIFFNESS GRADIENTS
Case 1: Uniform temperature distribution (i.e., no stiffness gradient) mean pavement temperature computed at 1/3-depth when
temperature conditions = warm
Case 2: Sharpest temperature gradient near surface - temperatures at 7 PM represent this condition
Case 3: Highest temperature differential between surface & bottomof asphalt concrete layer - temperatures at 5 AM representthis condition
Case 4: Rapid cooling near the surface represent case of suddenrain showers
Temperature differentials, age-hardening, sudden rains induce sub-layers of variable stiffness within asphalt concrete
0
25
50
75
100
125
150
175
200
225
250
275
300
0 0.25 0.5 0.75 1 1.25 1.5 1.75 2
Crack Length, a (in)
Mod
e I F
ract
ure,
K 1
(psi
-(in)
0.5 )
8in AC, Case 1 - Uniform Stiffness E1 = 800 ksi
8in AC, Case 2 - Sharp Gradient
8in AC, Case 3 - Highest TemperatureDifferential8in AC, Case 4 - Sudden Rain
Base Stiffness E2=20ksi
Major increase in tension – key factor in propagation of cracks
STIFFNESS GRADIENTS STAGES OF CRACK GROWTHShort Cracks, a = 0.25”,0.5”
Intermediate Cracks, a = 0.75”,1.0”,1.5”
aWide Rib Load 20”-30”
8” ACd
aLoad 20”-30”
8” ACd
Load 7”
SEAUPG 2002 CONFERENCE
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MPLICATION OF LOAD SPECTRA
Load Wander & Magnitude Instrumental in Mechanism- Critical position not always directly in wheel path on top of crack
- Depends on crack length, pavement structure,type of stiffness gradient
- Need to determine how many loads induce tension @ crack tip
Key FindingsTop-Down Cracks Develop Even in Thick Pavements (Previous Field Studies)Mechanisms Cannot be Captured Without Considering- Realistic Contact Stresses- Temperature Gradients- Load Wander- Presence of Cracks (Fracture Mechanics)
Most Recent Field Test Sections5 pairs of poor and good performing sections throughout Florida
•Location:
Performance:
SR 16-4C
SR 16-6U
US 19-1U
US 19-2C
TPK 1U
TPK 2C
SEAUPG 2002 CONFERENCE
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NW 39-1C
NW 39-2U
NW 39-2U
NW 39-1C
SamplingCoring
Section WP BWP Total
SR 16-4C 3 4 7
SR 16-6U 4 4 8
US 19-1U 18 18 36
US 19-2C 18 18 36
SR 375-1U 12 0 12
SR 375-2C 12 0 12
TPK-1U 12 12 24
TPK-2C 8 12 20
NW 39-1C 18 18 36
NW 39-2U 18 18 36
Total 227
Sample selection: closest to average BSGCrack depth:
Crack Depth (in) Rating< 1/2 101/2 - 1 8
1 - 1 1/2 61 1/2 - 2 4
2 - 3 2> 3 0
Section Performance Rating
SR 16 - 4C 0SR 16 - 6U 6US 19 - 1U 10US 19 - 2C 0SR 375 - 1U 10SR 375 - 2C 2
TPK 1U 10TPK 2C 2
NW 39 - 1C 0
NW 39 - 2U 10
Volumetric Properties
Air Void Content
Effective AsphaltContent
0
1
2
3
4
5
6
7
8
9
10
11
12
SR 16-6U SR 16 -4C US 19-1U US 19-2C SR 3 75-1U SR 375-2C TPK 1U TPK 2 C NW 39-2U NW 39 -1C
Section
% A
ir V
oid
Con
tent
WP
BWP
4.2
4 .4
4 .6
4 .8
5.0
5.2
5.4
5.6
5.8
SR 16-6U SR16-4C US 19-1U US 19-2C SR 375-1U SR 375-2C TP K 1U TP K 2C NW 39-2U NW 39-1C
Section
Effe
ctiv
e A
spha
lt C
onte
n
Aggregate Gradation
SR 16
US 19
0
10
20
30
40
50
60
70
80
90
100
Sieve Sizes
% P
assi
ng
Maximum Density Line SR 16-4C SR 16-6U
0 200 100 50 30 16 8 4 3/8 1/2 3/4 1
0
10
20
30
40
50
60
70
80
90
100
Sieve sizes
% P
assin
g
Maximum Density Line US 19-1U US 19-2C
0 200 100 50 30 16 8 4 3/8 1/2 3/4 1
SR 375
TPK
0
10
20
30
40
50
60
70
80
90
100
Sieve sizes
% P
assi
ng
TPK 1U TPK 2C
0 200 100 50 30 16 8 4 3/8 1/2 3/4 1
0
10
20
30
40
50
60
70
80
90
100
Sieve sizes
% P
assin
g
Maximum Density Line SR 375-1U SR 375-2C
0 200 100 50 30 16 8 4 3/8 1/2
0
10
20
30
40
50
60
70
80
90
100
Sieve sizes
% P
assin
g
Maximum Density Line TPK 1U TPK 2C
0 200 100 50 30 16 8 4 3/8 1/2 3/4
SEAUPG 2002 CONFERENCE
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NW 39
0
10
20
30
40
50
60
70
80
90
100
Sieve sizes
% P
assi
ng
Maximum Density Line NW 39-1C NW 39-2U
0 200 100 50 30 16 8 4 3/8 1/2 3/4 1
Theoretical Film Thickness
Binder Viscosity
0
1
2
3
4
5
6
7
8
9
10
SR 16-6U SR16-4C US 19-1U US 19-2C SR 375-1U S R 375-2C TP K 1U TP K 2C NW 39-2U NW 39-1C
Section
The
oret
ical
Film
Thi
ckne
ss (m
icro
-met
ers)
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
S R 16-6U S R 16-4C US 19-1U US 19-2C SR 375-1U SR 375-2C
TP K 1U TP K 2C NW 39-2U NW 39-1C
Section
Bin
der
Vis
cosi
ty (p
oise
s)
Mixture Testing
Resilient Modulus
Creep Compliance
0
2
4
6
8
10
12
14
16
18
20
S R 16-6U S R 16-4C US 19-1U US 19-2C S R 375-1U S R 375-2C TP K 1U TP K 2C NW 39-2U NW 39-1C
Section
Res
ilien
t Mod
ulus
(GPa
)
0
1
2
3
4
5
6
7
8
9
SR 16-6 U SR 16-4C US 19-1U US 19-2C SR 375-1U SR 375-2C TPK 1U TPK 2C NW 3 9-2 U NW 39-1C
Section
Cre
ep C
ompl
ianc
e at
100
0 se
cond
s (1/
GPa
)
Tensile Strength
m-value
0 .0
0 .5
1.0
1.5
2 .0
2 .5
3 .0
SR 16-6 U SR 16-4C US 19-1U US 19-2C SR 375-1U SR 375-2C TPK 1U TPK 2C NW 39 -2 U NW 39-1C
Section
Indi
rect
Ten
sile
Str
engt
h (M
Pa)
0 .00
0 .10
0 .20
0 .30
0 .40
0 .50
0 .60
0 .70
SR 16-6U SR 16-4 C US 19-1U US 19-2C SR 375-1U SR 375-2 C TPK 1U TPK 2 C NW 39 -2U NW 3 9-1C
Section
m -
Val
ue
Failure Strain
Fracture Energy
0
200
400
600
800
1000
1200
1400
1600
1800
SR 16-6U SR 16 -4 C US 19-1U US 19-2 C SR 375-1U SR 375-2 C TPK 1U TPK 2 C NW 39 -2U NW 3 9-1C
Section
Failu
re S
trai
n (m
icro
stra
in)
0 .0
0 .5
1.0
1.5
2 .0
2 .5
3 .0
SR 16 -6U SR 16-4C US 19 -1U US 19-2C SR 375-1U SR 375-2C TPK 1U TPK 2 C NW 39 -2U NW 3 9-1C
Section
Frac
ture
Ene
rgy
(KJ/
m3 )
• DCSE
0.0
0 .5
1.0
1.5
2 .0
2 .5
SR 16 -6U SR 16-4C US 19 -1U US 19-2C SR 375-1U SR 375-2C TPK 1U TPK 2 C NW 39 -2U NW 3 9-1C
Section
DC
SE (K
J/m
3 )
SEAUPG 2002 CONFERENCE
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FWD Analysis•Geometry
Section Friction Course AC Base Sub-baseSR 16-4C 0.6 3.0 6.7 12.0SR 16-6U 0.6 3.0 6.7 12.0US 19-1U 0.5 9.0 8.0 12.0US 19-2C 0.5 7.0 8.5 12.0SR 375-1U 0.6 6.3 7.5 12.0SR 375-2C 0.6 6.3 7.5 12.0
TPK-1U 0.5 7.0 12.0 12.0TPK-2C 0.5 6.1 12.0 12.0
NW 39-1C 0.8 4.0 12.5 12.0NW 39-2U 1.0 3.3 12.5 12.0
Pavement Structure
Section AC Base Sub-base Sub-gradeUS 19-1U 550 51 37 24US 19-2C 1,000 37 22 28TPK-1U 800 97 39 17TPK-2C 900 34 19 24
NW 39-1C 1,500 28 71 28NW 39-2U 1,500 63 58 30
Section E1/E2US 19-1U 11US 19-2C 27TPK-1U 8TPK-2C 26
NW 39-1C 52NW 39-2U 24
Loading stressesDesign load: 9000 lbs
Thermal StressesCooling rate: 10ºC/hr
0
50
100
150
200
250
300
US 19-1U US 19-2C TPK-1U TPK-2C NW 39-2U NW 39-1C
Section
Loa
ding
Str
esse
s (ps
i)
0
2
4
6
8
10
12
14
16
US 19-1U US 19-2C TPK-1U TPK-2C NW 39-2U NW 39-1C
Section
Ther
mal
Str
esse
s (ps
i)
Crack Growth ModelInitiation
0
2,000
4,000
6,000
8,000
10,000
12,000
14,000
SR 16-6U SR 16-4C US 19-1U US 19-2C SR 375-1U SR 375-2C
TP K 1U TP K 2C NW 39-2U NW 39-1C
Section
DC
SE N
f
7000 9000 11000
0
2,000
4,000
6,000
8,000
10,000
12,000
14,000
SR 16-6U SR 16-4C US 19-1U US 19-2C SR 375-1U SR 375-2C
TP K 1U TP K 2C NW 39-2U NW 39-1C
Section
FE N
f
7000 9000 11000
•Propagation
0
2,00 0
4 ,00 0
6 ,00 0
8 ,00 0
10 ,00 0
12 ,00 0
SR 16 -6 U SR 16-4C US 19-1U US 19 -2C SR 375-1U SR 3 75-2C TPK 1U TPK 2C NW 39-2U NW 3 9-1C
Section
Nf t
o pr
opag
atio
n
7000 9000 11000
Individual Analysis of the SectionsSR 16: high air voids, high m-value, low FEpossible effect of friction course
US 19: stiffness overwhelmed FE, low AC content and film thickness
SR 375: low FE, high m-value, high air voids
SEAUPG 2002 CONFERENCE
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• TPK: low base stiffness, high m-value, lowfilm thickness
• NW 39: high E1/E2 ratio, low compliance, lowtensile strength, low FE, possible effect of friction course
Summary of Findings• Structure has effects on surface-initiated cracking
• Load + Thermal stresses plays significant role
• High MR + Low Compliance / Load and thermal σ
• UF Cracking model properly explained performance differences
• No single property will assure adequate mixtureperformance. Need of conditions and model
Key Findings (Continued)
Design Approach Using Averaged Pavement and Load Conditions Inadequate- Critical Conditions Must Be IdentifiedMitigation Should be Addressed Primarily Through- More Crack-Resistant Surface Materials- Use of Less Damaging Tires
Implications for Design
Focus on Improving Surface MaterialsDialogue With Tire DesignersPavement Design/Management- Realistic contact stresses- Load spectra (magnitude and position)- Temperature gradients- Cracks/discontinuities (fracture mechanics)
Potential SolutionsImproved Mixture Design- Maximize Fracture Resistance of Mixtures- Improved Gradation/Volumetrics- Appropriate Mixture Design Parameters
(e.g. Fracture Energy)- ModifiersSpecialized Thin Surface Layers- Highly Modified, Low Stiffness/Stress
Relief, High Strain Tolerance
Conclusions• Stiffness and Compliance should be limited• Thermal stresses should be considered in structural
design• More attention should be paid to the effect and design of
friction courses• It is critical to identify appropriate design conditions to
evaluate performance using the parameters from thelaboratory
• UF cracking model adequately represents crackingmechanisms
SEAUPG 2002 CONFERENCE
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RecommendationsContinue evaluation of field performance to better understand failure mechanisms
Create database of mixture, traffic, environment and pavement structural characteristics
Concentrate more on friction course and structure
Testing at multiple temperatures for thermal analysis