dissipated energy study of fatigue in airport pavements phd candidate: shihui shen advisor: prof. s....
DESCRIPTION
DISSIPATED ENERGY CONCEPT REVIEW Ratio of Dissipated Energy Change (RDEC) STRAIN STRESS Initial Load Cycle Second Load Cycle Different Dissipated Energy Between First And Second Load CycleTRANSCRIPT
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DISSIPATED ENERGY STUDY OF
FATIGUE IN AIRPORT
PAVEMENTSPHD Candidate: Shihui ShenAdvisor: Prof. S. H. Carpenter
FAA Project ReviewNov. 9, 2005
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INTRODUCTIONDissipated Energy (RDEC)– Unifying Concept
Load Modes, Gear Configurations, Load Pulse Duration, Load Levels
Fatigue Endurance LimitThick airport pavementsThickness below which no damage occurs
Healing is the Recovery from Damage Impacts total loads to failure
Damage Concept is Amenable to a Thickness Design Procedure
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DISSIPATED ENERGY CONCEPT REVIEW
Ratio of Dissipated Energy Change (RDEC)
STRAINSTRAIN
STR
ESS
STR
ESS
Initial Load CycleInitial Load Cycle
Second Load CycleSecond Load Cycle
Different Dissipated Energy Between First And Second Load Cycle
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RDEC REVIEW
IIIIII
IIIIII
Plateau Value
Ratio
of D
issip
ated
Ene
rgy
Chan
ge, L
og
Load Repetitions, Log
Dissipated Envergy Vs. Loading cyclesIDOT Mix 6-7-1A 1000 Microstrain
00.002
0.0040.006
0.0080.01
0.0120.014
0.016
10 510 1,010 1,510 2,010 2,510 3,010 3,510 4,010
Number of Load Cycles
DER
Plateau Value50% Stiffness
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PV CALCULATIONIDOT03 mix 3N704B
DE vs. Loading cycles 800microstrain
y = 3.4255x-0.1638
R2 = 0.9512
00.20.40.60.8
11.21.4
0 1000 2000 3000 4000 5000Loading cycles
DE
Nf50
Slope f = - 0.1638
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UNIQUE PV-Nf RELATIONSHIPy = 0.4428x -1.1102
R2 = 0.996
1.E-09
1.E-08
1.E-07
1.E-06
1.E-05
1.E-04
1.E-03
1.E-02
1.E+02 1.E+03 1.E+04 1.E+05 1.E+06 1.E+07 1.E+08
loading cycles @ 50% stiffness reduction (Nf50), log
plat
eau
valu
e (P
V), l
og
Normal strain/damage
Data Points: 546Mixture types: 98Loading modes: 2Frequency: 0.5-10 HzRest period: 0- 0.4 sec.
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UNIQUE PV-Nf RELATIONSHIP
1.E-36
1.E-31
1.E-26
1.E-21
1.E-16
1.E-11
1.E-06
1.E-01
1.E+04
1.E+00 1.E+04 1.E+08 1.E+12 1.E+16 1.E+20 1.E+24 1.E+28 1.E+32
loading cycles @ 50% stiffness reduction, log
Plat
eau
Valu
e, lo
g Normal PVLow PV
Nf=1.10E+7
PVL=6.74E-9
Fatigue Endurance Fatigue Endurance LimitLimit
Unique energy level at which no fatigue damage exists
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APPLY RDEC IN HEALING STUDY
Researchers suggest healing can be better understood by carefully considering energy behavior and viscoelastic properties of an HMA PV, energy based, can provide a unique indication of the impact of a load pulse followed by a rest periodResearch hypothesis:
Rest periods promote healing effect and make it quantifiable through lab testHealing reduces the damageReduced damage produces a lower PV, which translates into a longer fatigue life
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FATIGUE-HEALING TEST
Four Point Bending Beam (SHRP T321-03)Mode of Loading: Constant Strain @ 500 microstrainWave Shape: HaversineLoad Pulse Width: 100ms (10 Hz)Rest Period: 0~9 secondTemperature: 20℃
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FATIGUE-HEALING TEST
ε
Loading time, second
No rest period, 0.1 second load pulse
1 second
3 second
9 second
Haversine Load Pulse Sequence A short rest period after each load pulse ~ to simulate rest between loads; An intermediate strain level, 500 microstrain, is used ~ relatively high damage level and shorter tests.
The whole nature of energy change during a test is still continuous, thus the dissipated energy and the PV can be obtained for each test to perform the RDEC analysis,
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PV-Nf FOR HEALING TEST
395950
114700
21010
33070y = 0.4429x-1.1102
1.E-07
1.E-06
1.E-05
1.E-04
1.E+04 1.E+05 1.E+06
Nf 50 , log
PV, l
og
neat binder mix polymer binder mix
(RP=0 sec.)-neat
(RP=0 sec.)-polymer
Unique PV-Nf relationship for healing test With 9 second rest
period, the fatigue life is extended 5 times for neat binder mix and 10 times for polymer binder mix
neat
polymer
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HEALING TEST ~ PV vs. (RP+1) FOR NEAT BINDER
70 microstrain
500microstrainPV = 1.018E-05(RP+1)-0.9069
R2 = 0.8944
1.E-09
1.E-08
1.E-07
1.E-06
1.E-05
1.E-04
1.E-03
1 10 100 1000 10000 100000(RP+1), (second), log
PV, l
og
PVL
3127 741584 44600
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HEALING TEST ~ PV vs. (RP+1) FOR POLYMER BINDER
500 microstrain
200 microstrain
500microstrain
y = 4.302E-06x-1.347
R2 = 0.7957
1.E-09
1.E-08
1.E-07
1.E-06
1.E-05
1.E-04
1 10 100 1000(RP+1), (second), log
PV, l
og
PVL
121
1000 microstrain
800 microstrain
300 microstrain
399 5406
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HEALING AND FELHealing study using RDEC approach helps to understand the existence of FEL
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PV-IDE AT NORMAL STRAIN (DAMAGE)
y = 1.137E-05x2.416E+00
R2 = 7.934E-01
1.E-09
1.E-08
1.E-07
1.E-06
1.E-05
1.E-04
1.E-03
1.E-02
0 0.5 1 1.5 2 2.5 3Initial Dissipated Energy
Plat
eau
Val
ue, l
og
At normal strain/damage condition and continuous loading, the PV is found has good correlation with Initial Dissipated Energy (IDE).
IDE, initial energy capacityPV, total effect of fatigue behavior (material fatigue resistance and load effect)
Under normal condition, load effect is dominant, while healing is negligible
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PV-IDE FOR WHOLE LOADING RANGE
y = 38.221x0.3288
R2 = 0.7947
1.E-03
1.E-02
1.E-01
1.E+00
1.E+01
1.E-41 1.E-36 1.E-31 1.E-26 1.E-21 1.E-16 1.E-11 1.E-06 1.E-01 1.E+04PV, log
IDE
, log
Normal damage low damageNf LowHigh
PVL
Normal DamageLow Damage
With decreased damage level, the role of healing becomes more significant: healing starts to dominate the performance comparing to damage
At low damage level when PV reaches threshold PVL, the PV-IDE curve start to flatten, leading to extended fatigue life
PV, combined healing effect, can no longer be represented by initial loading status, IDE, starting from the endurance limit, PVL
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PAVEMENT DESIGNRequires Relation to Standard ParametersLoad LevelSpeedRepetition IntervalMix VariablesAsphalt Grade
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PRELIMINARY PV PREDICTION MODELBased on 19 IDOT mix Including neat binder and polymer binder mix; various gradations; 2 air voids levels; Rich bottom binder mixes are included
2.6812.6763.7505.3295 C)VbAV
AV(Sε104.598PV
Where:ε: controlled tensile strainS : the flexural stiffness of HMA mix, MPa AV : the air voids of mixtureVb : the asphalt content by volumeC : the aggregate gradation parameter, C=(PNMS-PPCS)/P#200PNMS : the percent of agg. passing nominal maximum size sievePPCS : the percent of agg. passing primary control sieve (PCS = NMS * 0.22)P#200 : the percent of agg. passing #200 sieve
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PV PREDICTION
1.E-08
1.E-07
1.E-06
1.E-05
1.E-04
1.E-03
1.E-02
1.E-08 1.E-07 1.E-06 1.E-05 1.E-04 1.E-03 1.E-02
PV tested
PV p
redi
cted
Line of equality
R2 = 0.902
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BINDER FATIGUE TEST - DSR
DSR Testing Geometry Schematic Gemini 200 Dynamic Shear Rheometer
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TYPICAL BINDER DE-Nf CURVE
50 Pen Bitumen with 65% limestone, 1% Controlled strain
50% complexmodulusreduction
0.E+00
2.E+07
4.E+07
6.E+07
8.E+07
1.E+08
0 50000 100000 150000 200000 250000
Loading Cycles
DE
0.00E+00
4.00E+03
8.00E+03
1.20E+04
1.60E+04
2.00E+04
G*
G*DEI
III
II
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TYPICAL BINDER RDCE CURVE
50Pen Pure Bitumen, 15% Controlled Strain
0
0.0001
0.0002
0.0003
0.0004
0.0005
0.0006
0 50000 100000 150000 200000 250000 300000loading cycles
RD
EC
Plateau StageFailure Point
Plateau Stage, IIIII
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COMPARE PV-Nf CURVES FOR BINDER AND MIXTUREBinder (Mastic):y = 1.7663x-0.9598
R2 = 0.9819
Mix: y = 0.5787x-1.101
R2 = 0.988
1.E-07
1.E-06
1.E-05
1.E-04
1.E-03
1000 10000 100000 1000000 10000000Nf @ 50% stiffness reduction
Plat
eau
Val
ue (
PV)
Binder: con-strain Binder: con-stress Mixture
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CONCLUSIONSRDEC provides a successful way to study HMA, fatigue, healing, and its role on fatigue endurance limitHealing does exist and its effect on fatigue behavior can be observed through lab accelerated fatigue-healing test:
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CONCLUSIONS (cont.)The occurrence of healing is highly related to the level of damage; healing effect can be dominant under low load damage condition.Healing under the low damage condition is a key to understand the existence of a fatigue endurance limit (FEL).
Healing potential exceeds damage potential for any one load cycle.
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RECOMMENDATIONSPV can be predicted based on material properties, which can be integrated into pavement structural design.
Combine this with PVL, the energy based FEL established before, provides a simple way to estimate the strain level that can reach “unlimited” fatigue life.
The fatigue-healing test can be extended to different temperature, load levels, and more diversity of mix types.Asphalt binders’ energy recovery rates and healing capacity can be studied using the RDEC approach. It should provide an insight of the healing kinetics derived from the existing fatigue-healing study for mixture.
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THANK YOU !!
QUESTIONS ?