A A
S H
T O F H
W A
I N D U S T R YSUPERPAVE 2005
SHRP
ASPHALT INSTITUTE
AsphaltAsphaltUU--P GroupsP Groups
SuperpaveSuperpave® ® TodayTodayStatusStatus
ChallengesChallengesOur FutureOur Future
Thomas HarmanThomas HarmanMaterials & Construction Team Leader, R&DMaterials & Construction Team Leader, R&D
Federal Highway AdministrationFederal Highway Administrationwww.TFHRC.govwww.TFHRC.gov
AcknowledgementsAcknowledgements
Thanks to…Thanks to…
ONGOING ONGOING RefinementRefinement
•• Understanding modifiersUnderstanding modifiers•• Understanding acidUnderstanding acid•• Improved moisture testImproved moisture test•• Construction qualityConstruction quality•• Link to pavement designLink to pavement design•• Communication! Communication!
CHALLENGES
Paul MackPaul MackNew York State New York State -- RetiredRetired
Imperfection should never stall implementation.
You can still drink from a chipped cup.
A A
S H
T O F H
W A
I N D U S T R YSUPERPAVE 2005
Question is, “What kind of cup Question is, “What kind of cup do we have?”do we have?”
SuperpaveSuperpave®® Plus 2002Plus 200230% of DOT’s (5 Plus Methods)30% of DOT’s (5 Plus Methods)
•• Elastic recoveryElastic recovery•• Forced ductilityForced ductility•• Toughness and tenacityToughness and tenacity•• Phase anglePhase angle•• Method Method
(mode and dose)(mode and dose)•• CombinationsCombinations
0
10
20
30
40
50
As is Plus Spec.’s
PG Grade Specifications
Num
ber
of S
tate
s14
SHRP Asphalt SHRP Asphalt Program CoordinatorProgram Coordinator
“One of the principal goals of the SHRP asphalt program is to reduce or eliminate the
proliferation of asphalt binder specifications.”
Dr. Thomas Kennedy
Association of Modified Association of Modified Asphalt ProducersAsphalt ProducersAMAPAMAP
Las VegasLas VegasFebruary, 2005
STATE: ARKANSAS MATERIALS: Re: Section 404, Design and Quality Control of Asphalt Mixtures
DATE: 2004 Web Address: www/ahtd.state.ar.us/contract/progcon/general/stdspecs.htm
Materials Engineer: Jerry Westerman Email Address: [email protected]
ASPHALT BINDER:
Description:
Shall comply with requirements of AASHTO M 320, Table 1, except Direct Tension requirements are deleted and shall be from sources that have executed a certification agreement with the Department.
PMA’s: PG 70-22 & PG 76-22 shall be straight run binders that are modified using SB, SBS or SBR
404.01 (b)
Exclusions: None , other than type of polymer modifier
Requirements by Performance Grade, PG (Common Grades)
PROPERTY
Test Method
AASHTO or Other 64-22 70-22 76-22
ORIGINAL:
Flash Point, °C T 48 230 min.
Rotational Viscosity, Pa s 135°C T 316 3.0 max.
Dynamic Shear, kPa (G* /sin , 10 rad./sec.)
1.0 min. T 315 At grade temperature
RTFOT RESIDUE:
Mass Loss, % T 240 1.0 max.
Dynamic Shear, kPa (G* /sin , 10 rad./sec.)
2.20 min. T 315 At grade temperature
PAV RESIDUE R 28 100°C; 20 hrs; 300 psi
Dynamic Shear, kPa (G* sin , 10 rad./sec.)
5,000 max. T 315 25°C 28°C 31°C
S, 300MPa Creep Stiffness
m Value, 0.300
T 313
-12°C
PG PLUS REQUIREMENTS: YES
ORIGINAL:
Elongation Recovery 25°C, % T 301 --- 40 50
Polymer Type -- No SBR, SB, SBS
Notes: 1. If Anti-Strip needed, a heat stable liquid anti-strip additive from QPL shall be added at the rate of 0.5 - 0.75% by weight of asphalt binder as determined by laboratory analysis.
AR Page 1of 1
February, 2005
Ken Ken GrzybowskiGrzybowskiPRI Asphalt Technologies, Inc.PRI Asphalt Technologies, Inc.Tampa, FLTampa, FL
Concerning TrendConcerning Trend
•• 34 States with Plus Specs (67%)34 States with Plus Specs (67%)
•• 13 States Straight M 32013 States Straight M 320
•• 21 Different Pluses21 Different Pluses
•• 4 Duel / Hybrid4 Duel / Hybrid
•• The Winner! The Winner! ––M 320 with 13 PlusesM 320 with 13 Pluses++++++++++++++++++++++++++
05
101520253035
Num
ber
of S
tate
s
As is M320 Plus Spec.'sPG Grade Specifications
20022005
0 5 10 15 20
Polymer Content
Recovered Properties
Chemical Modification
Resilience
Smoke Point
Spot Test
Kinematic Viscosity
Ductility
Absolute Viscosity
Penetration
Softening Point
DTT/BBR
DTT
Phase Angle
DSR
Force Ratio & Ductility
Toughness & Tenacity
Sieve
Solubility
Separation / Compatibility
Elastic Recovery – ORIGINAL
Elastic Recovery – RTFOT
Alkaline
Used Motor Oil
Acid
Air Blown / Oxidized
PRESCRIPTIONS
Number of States
PrescriptionsExclusionsElastomericsConventionalOthers
The MinusesThe Minuses
•• Mostly EmpiricalMostly Empirical•• Varied PurposesVaried Purposes•• Multiple Test Methods Multiple Test Methods
–– Elastic Recover has Elastic Recover has at least 9 methodsat least 9 methods
•• Inconsistent ParametersInconsistent Parameters–– SBR SBR vsvs SBSSBS
The MinusesThe Minuses
•• Increased CostsIncreased Costs–– QC/QA TestingQC/QA Testing
•• Logistical Nightmare for Suppliers!Logistical Nightmare for Suppliers!
The PlussesThe Plusses
•• Great for PRI Asphalt Technologies.Great for PRI Asphalt Technologies.
ACTION ITEMSACTION ITEMS
•• We need regional coordination of We need regional coordination of Superpave Plus specificationsSuperpave Plus specifications
HighHigh--Temperature PerformanceTemperature PerformanceII--80, Nevada80, Nevada
Same gradation Same gradation -- different binders.different binders.
PG 63-22 modified No rutting
PG 67-22 unmodified 15mm of rutting
What do we need?What do we need?
•• Refinement to the Superpave binder Refinement to the Superpave binder purchase specificationpurchase specification to better to better capture the unique benefits of modified capture the unique benefits of modified systems (Step 2)systems (Step 2)
•• Better laboratory accelerated performance Better laboratory accelerated performance prediction toolsprediction tools to evaluate and to evaluate and characterize modified systems (Step 1)characterize modified systems (Step 1)
Purchase SpecificationPurchase Specification
•• Performance CriteriaPerformance Criteria–– Test Procedures, must be…Test Procedures, must be…
•• Easy to set upEasy to set up•• Easy to runEasy to run•• Easy to analyzeEasy to analyze
–– Test Procedures must be…Test Procedures must be…•• RepeatableRepeatable•• Reproducible Reproducible
Research ToolsResearch Tools
•• Performance Measure Performance Measure –– Test Procedures, can be…Test Procedures, can be…
•• Very difficult to set upVery difficult to set up•• Laborious to runLaborious to run•• Subject to interpretationSubject to interpretation
–– Test Procedures should be…Test Procedures should be…•• RepeatableRepeatable•• But not necessarily reproducible But not necessarily reproducible
Superpave® IISuperpave® IIBinder Purchase SpecificationBinder Purchase SpecificationPG PG –– based on degree daysbased on degree days
WHENWHEN WHATWHAT HOWHOW WHEREWHERE
ConstructionConstructionSafetySafety
PumpPump--abilityabilityRuttingRutting
Flash PointFlash PointRotational Rotational ViscVisc
DSR, JDSR, JNRNR
230230°° minmin3 Pa3 Pa--s maxs max
T(high)T(high)
EarlyEarly(RTFO or SAFT)(RTFO or SAFT)
RuttingRutting JJNRNR T(high)T(high)
LateLate(PAV or SAFT)(PAV or SAFT)
FatigueFatigueLowLow--TempTemp
DSRDSRBBR,DT, ABCBBR,DT, ABC
T(T(intint))T(low)T(low)
SuperpaveSuperpave®® IIII
FullFull--Scale Accelerated Scale Accelerated Performance Testing for Performance Testing for
SuperpaveSuperpave®® andandStructural ValidationStructural Validation
TPFTPF--5(019)5(019)
Thomas HarmanThomas HarmanMaterials & Construction Team Materials & Construction Team
Federal Highway AdministrationFederal Highway Administrationwww.TFHRC.govwww.TFHRC.gov
Total Research OrganizationTotal Research Organization
Superpave® Refinement
1993 1999 20032001
SHRP Validation-Laboratory-ALF 5 Binders2 Gradations
NCHRP 90-07-Laboratory
11 Binders1 Gradation
TPF-5(019)-ALF
7+ Binders2 Gradations
PG 67-80 Study-Laboratory
12 Binders1 Gradation
PartnersPartners
ALF TWG Meeting ALF TWG Meeting –– June 2005June 2005
TPFTPF--5(019) / SPR5(019) / SPR--2(174)2(174)State Pooled Fund ParticipantsState Pooled Fund Participants
TPF-5(019)
SPR-2(174)
ALF StudiesALF StudiesTPFTPF--5(019)5(019)SPRSPR--2(174)2(174)
Industry PartnersIndustry Partners
•• CitgoCitgo•• DowDow•• DupontDupont•• KochKoch•• ParamountParamount•• TexParTexPar, BTI, BTI•• TrifineryTrifinery, GCA, GCA•• TrumbullTrumbull•• Wright AsphaltWright Asphalt•• Martin Color Martin Color Fi
•• Bit MatBit Mat•• MathyMathy ConstructionConstruction•• Hot Mix IndustriesHot Mix Industries•• FNF ConstructionFNF Construction•• ConsulpavConsulpav•• Rubber Producers Assoc.Rubber Producers Assoc.•• ISSISS•• RTG RTG •• NAPANAPA
Fi
Collaborative Research PartnersCollaborative Research Partners
•• Asphalt InstituteAsphalt Institute•• National Center for Asphalt TechnologyNational Center for Asphalt Technology•• Western Research InstituteWestern Research Institute•• University of ArkansasUniversity of Arkansas•• Ohio UniversityOhio University•• Queens UniversityQueens University•• Arizona State UniversityArizona State University•• FWD Users GroupFWD Users Group
PTF/ALF EXPERIMENT 6PTF/ALF EXPERIMENT 6
DATA COLLECTION AND INSTRUMENTATIONDATA COLLECTION AND INSTRUMENTATION•• Laboratory TestingLaboratory Testing•• FWDFWD•• Strain GagesStrain Gages•• MultiMulti--Depth Depth DeflectometersDeflectometers•• Weather Station, Weather Station, TDRsTDRs, & Thermocouples, & Thermocouples•• Transverse ProfilingTransverse Profiling•• Crack MappingCrack Mapping
Current Completion DatesCurrent Completion Dates
•• Rutting testing Jan. 2004Rutting testing Jan. 2004•• Fatigue testing (100Fatigue testing (100--mm) Mar. 2006mm) Mar. 2006•• Fatigue testing (150Fatigue testing (150--mm) Dec. 2007mm) Dec. 2007
Two FHWA ALFs with Two FHWA ALFs with 12 Pavement Lanes Constructed in 12 Pavement Lanes Constructed in
the Summer and Fall of 2002the Summer and Fall of 2002
AsAs--Built Pavement Lanes Built Pavement Lanes
CR-AZ----70-22
1
PG70-22Control
2
AirBlown
3
SBSLG
4
CR-TB
5
TP
6
PG70-22
+Fibers
7
PG70-22
8
SBS64-40
9
AirBlown
10
SBSLG
11
TP
12
1 2
3 4
RuttingRuttingTThighhigh = 64= 64°°CC
FatigueFatigueTTintint = 19= 19°°CC
FatigueFatigueTTintint = 28= 28°°CC
ReplicateReplicate
ALF Testing
Rutting Test DataRutting Test Data
(64 (64 ooCC and 45 and 45 kNkN))
ALF HMA RuttingALF HMA RuttingHMA Layer Rutting for All Lanes
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
0 10,000 20,000 30,000 40,000 50,000 60,000
ALF Wheel Passes
HM
A L
ayer
Rut
ting,
in.
L9S1(SBS 64-40 6")
L9S2(SBS 64-40 6")
L6S1(Terpolymer 4")
L8S1(Control 6")
L10S1(Air Blown 6")
L11S1(SBS-lg 6")
L3S1(Air Blown 4")
L2S1(Control 4")
L1S1(CR AZ 4")
L4S1(SBS-lg 4")
L12S1(Terpolymer 6")
L7S1(Fibers 4")
L5S1(TBCR 4")
Fatigue Test DataFatigue Test Data
(19 (19 ooCC and 74 and 74 kNkN))
Lane 1
CR-AZ
300,000
Lane 2
Control
100,000
Lane 3
Air Blown
100,000
Lane 6
TP
200,000
Lane 4
SBS LG
300,000
Lane 5
CR-TB
100,000
Percentage of Area Cracked vs. ALF Wheel Load Passes Percentage of Area Cracked vs. ALF Wheel Load Passes
0.0
20.0
40.0
60.0
80.0
100.0
120.0
0 50000 100000 150000 200000 250000 300000 350000
Number of ALF Passes
Perc
enta
ge o
f Are
a C
rack
ed, %
L2S3 (Control)L3S3 (Air Blown)L5S3 (CR-TB)L6S3 (Terpolymer)L4S3 (SBS LG)L1S2 (CR-AZ)
0
20
40
60
80
100
120
0 100000 200000 300000 400000
Number of ALF Passes
Cum
ulat
ive
Cra
ck L
engt
h (m
) L3S3 (Air Blown)L2S3 (Control)L5S3 (CR-TB)L6S3 (Terpolymer)L4S3 (SBS LG)L7S3 (Fibers)L1S2 (CR-AZ)
Fatigue Cracking Length vs. ALF Wheel Load Passes Fatigue Cracking Length vs. ALF Wheel Load Passes
Rut Depth within HMA vs. ALF Wheel Load Passes(Testing Conditions: 19C & 16,600 lbs)
0
2
4
6
8
10
12
0 50,000 100,000 150,000 200,000 250,000 300,000 350,000
ALF Passes
Rut
Dep
th, m
m
L3S3 HMAL5S3 HMAL6S3 HMAL2S3 HMAL4S3 HMAL1S2 HMA
Strain Response DataStrain Response Data
(Initial and During Fatigue Test)(Initial and During Fatigue Test)
5 Gages Installed in 5 Gages Installed in Site 3 in Each LaneSite 3 in Each Lane
CTL CTL HH--Bar Strain GageBar Strain Gage
0
200
400
600
800
1000
1200
1400
1600
Lane
1 / C
R-AZ
Lane
2 / P
G 70-22
Lane
3 / A
ir-Blow
nLa
ne 4
/ SBS-LG
Lane
5 / C
R-TB
Lane
6 / T
erpoly
merLa
ne 7
/ Fibe
r
Lane
8 / P
G 70-22
Lane
9 / S
BS 64-40
Lane
10 / A
ir-Blow
n
Lane
11 / S
BS-LG
Lane
12 / T
erpoly
mer
Lane Number / Binder
Pea
k st
rain
, mic
rost
rain 19C/53kN 19C/62kN 28C/53kN 28C/62kN
Longitudinal Strains Directly Under LoadLongitudinal Strains Directly Under Load
ALF vs. LabALF vs. Lab
ALF vs. LabALF vs. Lab
•• Permanent Deformation Permanent Deformation –– RUTTINGRUTTING–– Binder (Covered)Binder (Covered)–– Mixture, SPTMixture, SPT
•• Fatigue CrackingFatigue Cracking–– Binder & MixtureBinder & Mixture
•• Other Mixture Challenges & DirectionsOther Mixture Challenges & Directions–– SPTSPT–– GyratoryGyratory–– ImagingImaging
Laboratory Mixture Laboratory Mixture CharacterizationCharacterization
SST FSCH and RSCH TestsSST FSCH and RSCH TestsFrench Permanent Rut TestFrench Permanent Rut TestHamburg WTD TestHamburg WTD TestIDT Resilient Modulus (IDT Resilient Modulus (MMrr) Test) TestSPT Dynamic Modulus (ESPT Dynamic Modulus (E**) and ) and Flow Number (FN) TestsFlow Number (FN) Tests
SST DeviceSST Device
FSCH GFSCH G** vs. 100vs. 100--mm Pavement Rut mm Pavement Rut DepthDepth
RD = - 0.001 G*FSCH + 51.0R2 = 0.84
0.0
5.0
10.0
15.0
20.0
30000 35000 40000 45000 50000
FSCH G* at 74°C (MPa)
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
FSCH GFSCH G** vs. 150vs. 150--mm Pavement Rut mm Pavement Rut DepthDepth
RD = - 0.001 G*FSCH + 41.1R2 = 0.30
0.0
5.0
10.0
15.0
20.0
30000 35000 40000 45000 50000
FSCH G* at 74°C (MPa)
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
RSCH Cycles to Failure vs. 100RSCH Cycles to Failure vs. 100--mm mm Pavement Rut DepthPavement Rut Depth
RD = - 0.003 NRSCH Failure + 15.8R2 = 0.99
0.0
5.0
10.0
15.0
20.0
0 1000 2000 3000 4000 5000
RSCH Cycles to Failure at 74°C
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
Outlier = Terpolymer
RSCH Cycles to Failure vs. 150RSCH Cycles to Failure vs. 150--mm mm Pavement Rut DepthPavement Rut Depth
RD = - 0.004 NRSCH Failure + 19.0R2 = 0.77
0.0
5.0
10.0
15.0
20.0
0 1000 2000 3000 4000 5000
RSCH Cycles to Failure at 74°C
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
French PRT DeviceFrench PRT Device
French Rut Depth vs. 100French Rut Depth vs. 100--mm mm Pavement Rut DepthPavement Rut Depth
RD = 0.525 RDFrench + 7.4R2 = 0.64
0.0
5.0
10.0
15.0
20.0
0.0 5.0 10.0 15.0 20.0 25.0
French Rut Depth at 74°C (mm)
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
French Rut Depth vs. 150French Rut Depth vs. 150--mm mm Pavement Rut DepthPavement Rut Depth
RD = 0.012 RDFrench + 14.9R2 = 0.001
0.0
5.0
10.0
15.0
20.0
0.0 5.0 10.0 15.0 20.0 25.0
French Rut Depth at 74°C (mm)
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
Hamburg Wheel Tracking Device Hamburg Wheel Tracking Device (WTD)(WTD)
685 N80mm
• 10,000 and 20,000 passes
• 10-mm rut depth
Hamburg Rut Depth vs. 100Hamburg Rut Depth vs. 100--mm mm Pavement Rut DepthPavement Rut Depth
RD = 0.0002 RDHamburg + 9.5R2 = 0.22
0.0
5.0
10.0
15.0
20.0
0 5000 10000 15000 20000 25000Hamburg Rut Depth at 64°C (mm)
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
Outlier = Terpolymer
Hamburg Rut Depth vs. 150Hamburg Rut Depth vs. 150--mm mm Pavement Rut DepthPavement Rut Depth
RD = - 0.0001 RDHamburg + 16.3R2 = 0.044
0.0
5.0
10.0
15.0
20.0
0 5000 10000 15000 20000 25000
Hamburg Rut Depth at 64°C (mm)
Pav
emen
t R
ut
Dep
th a
t 64
°C
(mm
)
IDT TestingIDT Testing
IDT Total Resilient Modulus vs. 100IDT Total Resilient Modulus vs. 100--mm Pavement Rut Depthmm Pavement Rut Depth
RD = - 0.006 MrTotal + 17.9R2 = 0.91
0.0
5.0
10.0
15.0
20.0
0 500 1000 1500 2000
IDT Total Resilient Modulus at 40°C (MPa)
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
IDT Total Resilient Modulus vs. 150IDT Total Resilient Modulus vs. 150--mm Pavement Rut Depthmm Pavement Rut Depth
RD = 0.0002 MrTotal + 14.9R2 = 0.003
0.0
5.0
10.0
15.0
20.0
0 500 1000 1500 2000
IDT Total Resilient Modulus at 40°C (MPa)
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
Laboratory Mixture Laboratory Mixture Characterization, RCharacterization, R22
TESTTEST 100mm100mm 150mm150mmSST FSCH SST FSCH 0.840.84 0.300.30SST RSCHSST RSCH 0.990.99 0.770.77French PRTFrench PRT 0.640.64 0.0010.001Hamburg WTD Hamburg WTD 0.220.22 0.040.04IDT IDT MMrr 0.91 (3 pts)0.91 (3 pts) 0.0030.003SPT |ESPT |E**|| on going testing…on going testing…SPT FNSPT FN
New SPTNew SPT
SPT |ESPT |E**| Test| Test
SPT |ESPT |E**| tests were | tests were conducted on …conducted on …•• TruckTruck•• LabLab•• CoresCores
Unconfined |EUnconfined |E**| tests were conducted at | tests were conducted at four temperatures 19, 31, 46, and 58°Cfour temperatures 19, 31, 46, and 58°C
Variability of SPT EVariability of SPT E** and FNand FN
|E*|, CV = 1 to 26|E*|, CV = 1 to 26CV < 15 in most casesCV < 15 in most cases
FN, CV = 1 to 50, howeverFN, CV = 1 to 50, howeverCV ~ 6 to 21 CV ~ 6 to 21 with cycles to 2% strainwith cycles to 2% strain
SamplingSampling
E* Master CurvesE* Master Curves--TruckTruck
1
10
100
1000
10000
100000
1E-05 1E-04 0.001 0.01 0.1 1 10 100 1000 10000Reduced Frequency (Hz)
E* (M
Pa)
PG 70-22Air-BlownCR-TBTerpolymerSBS LGSBS 64-40
E* Master CurvesE* Master Curves--LabLab
1
10
100
1000
10000
100000
1E-05 1E-04 0.001 0.01 0.1 1 10 100 1000 10000Reduced Frequency (Hz)
E* (M
Pa)
PG 70-22Air-BlownCR-TBSBS LGTerpolymerSBS 64-40
E* Master CurvesE* Master Curves--CoresCores
1
10
100
1000
10000
100000
1E-05 1E-04 0.001 0.01 0.1 1 10 100 1000 10000Reduced Frequency (Hz)
E* (M
Pa)
Lane 10/Air-Blown
Lane 8/PG 70-22
Lane 11/SBS LG
Lane 12/Terpolymer
Lane 9/SBS 64-40
Control (PG 70Control (PG 70--22)22)
1
10
100
1000
10000
100000
0.00001 0.001 0.1 10 1000Reduced Frequency (Hz)
E* (M
Pa)
Truck
LabCores
TerpolymerTerpolymer
1
10
100
1000
10000
100000
0.00001 0.001 0.1 10 1000Reduced Frequency (Hz)
E* (M
Pa)
Truck
Lab
Cores
SBS Linear GraftedSBS Linear Grafted
1
10
100
1000
10000
100000
0.00001 0.001 0.1 10 1000Reduced Frequency (Hz)
E* (M
Pa)
Truck
Lab
Cores
Hirsch Model PredictionsHirsch Model PredictionsControl (PG 70Control (PG 70--22)22)--TruckTruck
1
10
100
1000
10000
100000
0.00001 0.001 0.1 10 1000Reduced Frequency (Hz)
E* (M
Pa)
Hirsch Model-PredictedMeasured
Area of Potential Work
Hirsch Model PredictionsHirsch Model PredictionsTerpolymerTerpolymer--Truck Truck
1
10
100
1000
10000
100000
0.00001 0.001 0.1 10 1000
Reduced Frequency (Hz)
E* (M
Pa)
Hirsch Model-PredictedMeasured
Area of Potential Work
Hirsch Model PredictionsHirsch Model PredictionsSBS LGSBS LG--TruckTruck
1
10
100
1000
10000
100000
0.00001 0.0001 0.001 0.01 0.1 1 10 100 1000
Reduced Frequency (Hz)
E*
(MP
a)
Hirsch Model-PredictedMeasured
Area of Potential Work
Hirsch Model vs. Witczak Hirsch Model vs. Witczak ModelModel
Witczak model was not used for Witczak model was not used for the mixture dynamic modulus the mixture dynamic modulus predictions for two reasons:predictions for two reasons:•• It provides similar predictions to It provides similar predictions to
those of the Hirsch model.those of the Hirsch model.•• The mixture volumetric inputs The mixture volumetric inputs
required for the Hirsch model were required for the Hirsch model were available.available.
EE**/sin /sin δ δ vs. 150vs. 150--mm Pavement Rut mm Pavement Rut DepthDepth
RD = 3E+07 (E*sin δ)-2.987
R2 = 0.91
RD = - 0.341 E*sin δ + 58.6R2 = 0.86
0.0
5.0
10.0
15.0
20.0
100 110 120 130 140 150
E*/sin δ at 0.1 Hz (MPa)
Pave
men
t Rut
Dep
th (m
m)
Outlier = Air-Blown
Linear
Power
Flow Number vs. 150Flow Number vs. 150--mm Pavement Rut mm Pavement Rut DepthDepth
RD = - 0.001 FN + 18.5R2 = 0.74
0.0
5.0
10.0
15.0
20.0
0 1000 2000 3000 4000 5000Flow Number at 64°C
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
Outlier = Terpolymer
FN Cycles to Failure vs. 150FN Cycles to Failure vs. 150--mm mm Pavement Rut DepthPavement Rut Depth
RD = - 0.027 N2% Strain + 19.5R2 = 0.81
0.0
5.0
10.0
15.0
20.0
0 100 200 300 400 500FN Cycles to 2% Strain
Pave
men
t Rut
Dep
th a
t 64°
C
(mm
)
Outlier = Terpolymer
SPT ESPT E** RankingRanking
Highest Truck Lab Cores
PG 70-22 PG 70-22 Air-Blown
Air-Blown Air-Blown PG 70-22
CR-TB CR-TB
SBS LG SBS LG SBS LG
Terpolymer Terpolymer Terpolymer
SBS 64-40 SBS 64-40 SBS 64-40Lowest
“Understanding the “Understanding the Performance of Modifiers in Performance of Modifiers in
Asphalt Mixtures” Asphalt Mixtures” ––6767--80 Binder Study80 Binder Study
Revised T.T.S. + Revised T.T.S. + Statistical AnalysisStatistical Analysis
Materials & Construction TeamMaterials & Construction Team
Federal Highway AdministrationFederal Highway Administrationwww.TFHRC.govwww.TFHRC.gov
6767--80 Binder Study80 Binder StudyOutlineOutline
•• 6767--80 Binders80 Binders•• Mixture CharacterizationMixture Characterization•• Research ApproachResearch Approach•• Proposed Binder ParametersProposed Binder Parameters•• ResultsResults•• ObservationsObservations
2001 ALF Pavement Facility2001 ALF Pavement FacilityTarget Grade, AB cTarget Grade, AB c--PG 74PG 74--2828
Binder IDBinder ID cc--PG HTPG HT cc--PG LTPG LT UTIUTI
1: AZ CR1: AZ CR2/8: Control2/8: Control3/10: Air3/10: Air--blownblown4/11: SBS4/11: SBS--lglg5: TBCR5: TBCR6/12: Terpolymer6/12: Terpolymer9: SBS 649: SBS 64--4040
n/an/a727274747474797974747171
n/an/a--2323--2828--2828--2828--3131--3838
n/an/a9595102102102102103103105105109109
UTI – Useful Temperature Index
In situ ALF BindersIn situ ALF Binders
-40
-34
-28
-2258 64 70 76 82
Continous High Temperature Grade, (c-HT) °C
c-LT
, °C
ControlAirblownSBS-lgTBCRTerpolySBS
ETG Concern
6767--80 Binders80 Binderscc--PG based on G*/sin PG based on G*/sin δδ Original/RTFOOriginal/RTFO
Binder IDBinder ID CodeCode cc--PG HTPG HT cc--PG LTPG LT
1: 1: EnviroEnviro. Friendly. Friendly2: EF + SBS2: EF + SBS3: Terpolymer3: Terpolymer4: Terpolymer4: Terpolymer5: Terpolymer5: Terpolymer6: Terpolymer6: Terpolymer
B6308B6308B6309B6309B6310B6310B6311B6311B6312B6312B6316B6316
777780805959686872728282
--2525--2424--3030--2828--3131--2424
6767--80 Binders80 Binderscc--PG based on G*/sin PG based on G*/sin δδ Original/RTFOOriginal/RTFO
Binder IDBinder ID CodeCode cc--PG HTPG HT cc--PG LTPG LT
7: TBCR7: TBCR8: TBCR8: TBCR9: TBCR9: TBCR
10: SBS LG10: SBS LG11: SBS LG11: SBS LG12: SBS LG12: SBS LG
B6313B6313B6314B6314B6315B6315B6324B6324B6325B6325B6326B6326
707076768282686877778484
--2525--2525--2323--2626--2323--2222
6767--80 Binders80 Binders
-40
-34
-28
-2258 64 70 76 82 88
Continous High Temperature Grade, (c-HT) °C
c-LT
, °C
EFEF + SBSTerpolyTBCRSBS lg
58 64 70 76 82 88
Mixture Test at HT cMixture Test at HT c--PGPG
•• Superpave Shear Tester (SST)Superpave Shear Tester (SST)–– Repeated Shear at Constant Height (RSCH)Repeated Shear at Constant Height (RSCH)
Cycles to 2% Strain FailureCycles to 2% Strain Failure•• Strain at 5,000 cyclesStrain at 5,000 cycles•• Strain at 1,000 cyclesStrain at 1,000 cycles
Mixture Test at HT cMixture Test at HT c--PGPG
•• Cycles to 2% Strain FailureCycles to 2% Strain Failure•• Best connection to Full Scale Rutting (ALF)Best connection to Full Scale Rutting (ALF)
RD = - 0.004 NRSCH Failure + 19.0
0.0
5.0
10.0
15.0
20.0
0 1000 2000 3000 4000 5000
RSCH Cycles to Failure at 74°C
150m
m Pa
veme
nt Ru
t Dep
th at
64°C
(mm)
RD = - 0.003 NRSCH Failure + 15.8
0.0
5.0
10.0
15.0
20.0
0 1000 2000 3000 4000 5000
RSCH Cycles to Failure at 74°C
100m
m P
avem
ent R
ut D
epth
at
64°C
(mm
)
Outlier = Terpolymer
R2 = 0.77
R2 = 0.99
150mm
100mm
Summary of 67Summary of 67--80 Mixture Testing80 Mixture TestingCV for Trimmed Mean CV for Trimmed Mean (5(5--2=3)2=3)
•• 6% < COV < 45%6% < COV < 45%•• Most ~ 15%Most ~ 15%
Working Data Set after Trimmed Working Data Set after Trimmed Mean AnalysisMean Analysis
•• Typical ExampleTypical Example
0
250
500
750
1000
1250
1500
68 70 72 74 76 78 80 82 84
SST RSCH Test Temperature, °C
Cyc
les
to 2
% S
trai
n
Trimmed Mean Variability
Much care was taken in this experiment, however, results do not always follow expected decreasing trend
– THIS IS A FACT OF LIFE WITH HT SST.
RR22 Approach…Approach…Understanding R2 behavior as linear slope approaches zero for various qualities of data.
0
0.2
0.4
0.6
0.8
1
0.0001 0.001 0.01 0.1 1 10 100 1000
Data Quality = Standard Deviation about Underlying Linear Function
R2
Slope 100
Slope 10
Slope 1
Slope 0.1
RR22 ApproachApproachUnderstanding R2 behavior as linear slope approaches zero for various qualities of data.
0
0.2
0.4
0.6
0.8
1
0.0001 0.001 0.01 0.1 1 10 100 1000
Data Quality = Standard Deviation about Underlying Linear Function
R2
Slope 100
Slope 10
Slope 1
Slope 0.1
Slope 0.000005
Conclusion – R2 is not the most appropriate method. Essentially R2=1 for a perfect horizontal Model, but HYPERSENSITIVE. Smallest deviation from perfect horizontal causes poor R2 with moderate variability.
Pivotal Question…Pivotal Question…
•• Can we perform SST tests at cooler temperature Can we perform SST tests at cooler temperature where variability is smaller ?where variability is smaller ?
•• Then……relate test data to warmer conditions Then……relate test data to warmer conditions where ETG suggests mixture tests be where ETG suggests mixture tests be performed.performed.
•• WHAT TOOLS ARE AVAILABLE TO DO WHAT TOOLS ARE AVAILABLE TO DO SOMETHING LIKE THIS WITH EXISTING DATA ?SOMETHING LIKE THIS WITH EXISTING DATA ?
Pivotal QuestionPivotal Question(NCHRP 9(NCHRP 9--19)19)
•• Utilization of Utilization of TIME TEMPERATURE TIME TEMPERATURE SUPERPOSTIONSUPERPOSTION–– Creep & Permanent Deformation at Multiple Creep & Permanent Deformation at Multiple
Temperatures…Neat 64Temperatures…Neat 64--22 Dense Graded22 Dense Graded–– It is Feasible to “Shift” Permanent Strains like |G*|It is Feasible to “Shift” Permanent Strains like |G*|
-3
-2.5
-2
-1.5
-1
-0.5
0
0 500 1000 1500 2000Reduced Time, sec
Stra
in, %
Shifted 45oC Avg. 3 ReplicatesUnshifted 35oC Avg. 3 Replicates
-3.5
-3
-2.5
-2
-1.5
-1
-0.5
0
0 1000 2000 3000 4000Reduced Time, sec
Stra
in, %
Shifted 35oC Avg. 3 ReplicatesUnshifted 25oC Avg. 3 Replicates
Current Research ApproachCurrent Research Approach•• Calibrate a SST RSCH Model with integrated Time Calibrate a SST RSCH Model with integrated Time
Temperature SuperpositionTemperature Superposition•• Determine Theoretical SST Test Result at Determine Theoretical SST Test Result at
Temperatures Determined by Candidate Binder Temperatures Determined by Candidate Binder Parameters Parameters
•• Repeat 3 times calibrating on Test DataRepeat 3 times calibrating on Test Data1.1. HIGHERHIGHER2.2. INTERMEDIATEINTERMEDIATE3.3. LOWERLOWER
Calibrate a SST RSCH Model with integrated Calibrate a SST RSCH Model with integrated Time Temperature SuperpositionTime Temperature Superposition
0
500
1000
1500
2000
2500
3000
3500
68 70 72 74 76 78 80 82 84
SST RSCH Test Temperature, oC
# S
ST
RS
CH
Cycle
s to
2%
Pe
rma
ne
nt S
tra
in
High Calib
Measured
( ) ( ) ( ) 213
223
212
23311
23322
22211 666 τττσσσσσσσ +++−+−+−=eq
212
211 3τσσ +=eq
( )( )qvp
peq
R
vp
B
Adtd
12
12
γ
σγ=
From Binder |G*|Trimmed Mean Variability
)(TattR =
Each Binder Parameter for Each Binder Has a Distinct Temperature
Calibrate a SST RSCH Model with integrated Calibrate a SST RSCH Model with integrated Time Temperature SuperpositionTime Temperature Superposition
0
500
1000
1500
2000
2500
3000
3500
68 70 72 74 76 78 80 82 84
SST RSCH Test Temperature, oC
# S
ST
RS
CH
Cycle
s to
2%
Pe
rma
ne
nt S
tra
in
High Calib
Int. Calib
Measured
( ) ( ) ( ) 213
223
212
23311
23322
22211 666 τττσσσσσσσ +++−+−+−=eq
212
211 3τσσ +=eq
( )( )qvp
peq
R
vp
B
Adtd
12
12
γ
σγ=
From Binder |G*|Trimmed Mean Variability
)(TattR =
Each Binder Parameter for Each Binder Has a Distinct Temperature
Calibrate a SST RSCH Model with integrated Calibrate a SST RSCH Model with integrated Time Temperature SuperpositionTime Temperature Superposition
0
500
1000
1500
2000
2500
3000
3500
68 70 72 74 76 78 80 82 84
SST RSCH Test Temperature, oC
# S
ST
RS
CH
Cycle
s to
2%
Pe
rma
ne
nt S
tra
in
High Calib
Int. Calib
Low Calib
Measured
( ) ( ) ( ) 213
223
212
23311
23322
22211 666 τττσσσσσσσ +++−+−+−=eq
212
211 3τσσ +=eq
( )( )qvp
peq
R
vp
B
Adtd
12
12
γ
σγ=
From Binder |G*|Trimmed Mean Variability
)(TattR =
Each Binder Parameter for Each Binder Has a Distinct Temperature
Current Research ApproachCurrent Research ApproachDetermine Proportion of Test Results that Lie
outside Effective Lumped Variability
# C
ycle
s to
2%
Str
ain
Temperature From Parameter
High Spec. Temperature, THigh Spec. Temperature, THSHS
•• |G*|/sin |G*|/sin δ = 2200 Paδ = 2200 Pa at 10 rads/sat 10 rads/s (Superpave)(Superpave)
•• |G*|/(1|G*|/(1--(1/tan(1/tanδδ sinsinδ)) = 50 Paδ)) = 50 Pa at 0.25 rads/sat 0.25 rads/sCriterion 1 Criterion 1 (FHWA)(FHWA)
•• TTE E /(1/(1--(1/tan(1/tanδδ sinsinδ)) where Tδ)) where TEE is when |G*|= 50 is when |G*|= 50 PaPa at 0.25 rads/sat 0.25 rads/sCriterion 2 Criterion 2 (FHWA)(FHWA)
High Spec. Temperature, THigh Spec. Temperature, THSHS
•• η’ = 220 Paη’ = 220 Pa--ss, LSV , LSV at 0.01 rads/sat 0.01 rads/s (Binder ETG)(Binder ETG)
•• ηη00 = 250 Pa= 250 Pa--ss, ZSV , ZSV at 0 rads/sat 0 rads/s (Binder ETG)(Binder ETG)
•• MVR MVR = 50 cc/10min= 50 cc/10min at 1.225 kg loadat 1.225 kg load (FHWA)(FHWA)
High Temperature ParametersHigh Temperature Parameters
•• % γ% γaccacc Repeated Creep Repeated Creep @@300 Pa 300 Pa (NCHRP 9(NCHRP 9--10)10)
•• % γ% γaccacc Repeated Creep Repeated Creep @@25 Pa 25 Pa (NCHRP 9(NCHRP 9--10)10)
Results Results -- ExampleExample
SST Test Results Determined Using Time-Temp Superposition at Different Individual Binder Parameter Temperatures
0
0.001
0.002
0.003
0.004
0.005
0.006
0 500 1000 1500 2000 2500 3000
SST RSCH Cycles to 2% Strain
No
ma
l D
istr
ibu
tio
n F
req
ue
nc
y
B6313 CRTB PG70-25B6314 CRTB PG76-25B6315 CRTB PG82-23B6324 SBS-LG PG68-26B6325 SBS-LG PG77-23B6326 SBS-LG PG84-22B6310 TP PG59-30B6312 TP PG72-31B6316 TP PG82-24Effective Combined
|G*|/sin δ
Intermediate SST Calibration
Results Results ––Lower SST CalibrationLower SST Calibration
|G*| sind
|G*| (1-(1/tandsind))
TE (1-(1/tandsind)) ZSV LSV MVR
B6313 CRTB PG70-25 27.6% 5.3% 1.0% 4.8% 4.4% 24.4%B6314 CRTB PG76-25 30.9% 28.7% 28.6% 29.9% 28.6% 28.6%B6315 CRTB PG82-23 1.0% 0.7% 0.5% 0.6% 1.0% 1.7%B6324 SBS-LG PG68-26 0.0% 0.0% 0.0% 0.0% 0.0% 0.0%B6325 SBS-LG PG77-23 0.0% 0.0% 0.0% 0.0% 0.0% 0.0%B6326 SBS-LG PG84-22 0.1% 0.1% 0.0% 0.1% 0.1% 0.1%B6310 TP PG59-30 5.5% 3.1% 5.3% 0.0% 10.4% 19.4%B6312 TP PG72-31 2.7% 3.2% 3.3% 3.1% 3.4% 3.3%B6316 TP PG82-24 59.6% 59.3% 59.4% 59.3% 59.3% 59.4%
6 of 9 7 of 9 7 of 9 7 of 9 6.5 of 9 5 of 9
Calibration at Lower SST Temperature
Binder\Parameter
Results Results ––Intermediate SST Temp CalibrationIntermediate SST Temp Calibration
|G*| sind
|G*| (1-(1/tandsind))
TE (1-(1/tandsind)) ZSV LSV MVR
B6313 CRTB PG70-25 91.5% 57.0% 17.8% 99.9% 81.6% 98.4%B6314 CRTB PG76-25 72.2% 37.3% 29.1% 93.5% 29.3% 29.6%B6315 CRTB PG82-23 38.4% 21.3% 11.0% 6.3% 34.8% 89.9%B6324 SBS-LG PG68-26 0.0% 0.0% 0.5% 97.3% 99.1% 81.9%B6325 SBS-LG PG77-23 40.9% 0.7% 0.0% 0.0% 0.0% 0.0%B6326 SBS-LG PG84-22 16.3% 5.5% 0.0% 12.2% 0.2% 0.4%B6310 TP PG59-30 100.0% 100.0% 100.0% 100.0% 100.0% 100.0%B6312 TP PG72-31 54.9% 2.8% 6.5% 64.5% 5.3% 35.8%B6316 TP PG82-24 65.8% 60.3% 60.9% 67.2% 59.3% 61.5%
1 of 9 4 of 9 4.5 of 2.5 of 3 of 9 2 of 9
Calibration at Higher SST Temperature
Binder\Parameter
Results Results ––Higher SST Temp CalibrationHigher SST Temp Calibration
|G*| sind
|G*| (1-(1/tandsind))
TE (1-(1/tandsind)) ZSV LSV MVR
B6313 CRTB PG70-25 91.5% 57.0% 17.8% 99.9% 81.6% 98.4%B6314 CRTB PG76-25 72.2% 37.3% 29.1% 93.5% 29.3% 29.6%B6315 CRTB PG82-23 38.4% 21.3% 11.0% 6.3% 34.8% 89.9%B6324 SBS-LG PG68-26 0.0% 0.0% 0.5% 97.3% 99.1% 81.9%B6325 SBS-LG PG77-23 40.9% 0.7% 0.0% 0.0% 0.0% 0.0%B6326 SBS-LG PG84-22 16.3% 5.5% 0.0% 12.2% 0.2% 0.4%B6310 TP PG59-30 100.0% 100.0% 100.0% 100.0% 100.0% 100.0%B6312 TP PG72-31 54.9% 2.8% 6.5% 64.5% 5.3% 35.8%B6316 TP PG82-24 65.8% 60.3% 60.9% 67.2% 59.3% 61.5%
1 of 9 4 of 9 4.5 2.5 3 of 9 2 of 9
Calibration at Higher SST TemperatureBinder\Parameter
ObservationsObservations•• Utilization of the Lower and Intermediate T.T.S. Utilization of the Lower and Intermediate T.T.S.
Calibrations is desired…Calibrations is desired…–– Higher Temp Calibration has strongest potential for Higher Temp Calibration has strongest potential for
variabilityvariability–– Lower and Intermediate compare with each otherLower and Intermediate compare with each other
•• Lower Calibration (7 of 9)Lower Calibration (7 of 9)11--(1/(1/tantanδ δ sinsinδδ) methods and ZSV capture more ) methods and ZSV capture more behaviorbehavior
•• Intermediate Calibration (4~ or 9)Intermediate Calibration (4~ or 9)11--(1/(1/tantanδ δ sinsinδδ) methods and LSV capture more ) methods and LSV capture more behaviorbehavior
ObservationsObservations
•• Cooler tests with less variability are Cooler tests with less variability are needed to further analyze the “tied” needed to further analyze the “tied” parametersparameters
Next Steps… Next Steps… High Temperature ParametersHigh Temperature Parameters
•• NonNon--recovered Compliance after 50 cyclesrecovered Compliance after 50 cyclesRepeated Creep Repeated Creep @ @ 50Pa, 100Pa, 500Pa, 1000Pa, 50Pa, 100Pa, 500Pa, 1000Pa, 1600Pa, 3200Pa 1600Pa, 3200Pa (Binder ETG)(Binder ETG)
•• NonNon--recovered Compliance Multirecovered Compliance Multi--stress after 10 stress after 10 cyclescycles Repeated Creep Repeated Creep @ @ 25Pa, 50Pa, 100Pa, 25Pa, 50Pa, 100Pa, 200Pa, 400Pa, 800Pa, 1600Pa, 3200Pa 200Pa, 400Pa, 800Pa, 1600Pa, 3200Pa
(Binder ETG)(Binder ETG)
Next Steps.Next Steps.•• Revise with FRevise with F--Distribution or Distribution or
ChiChi22--Distribution where 0<x<Distribution where 0<x<•• ActualActual cooler (45cooler (45ooC) SST tests C) SST tests
shifted up to warmer tests shifted up to warmer tests ––i.e. adjust frequency of SST i.e. adjust frequency of SST pulsepulse
OROR•• Revised Flow Number test, of Revised Flow Number test, of
which we have capability to which we have capability to modify test softwaremodify test software
8
ACTION ITEMSACTION ITEMS
•• What additional binder should be What additional binder should be considered? considered? –– Is 7 or 9 good enough?Is 7 or 9 good enough?
•• Should additional aggregate structures be Should additional aggregate structures be considered?considered?
Binder ParametersBinder Parameters
1.1. SuperpaveSuperpave|G*| sin |G*| sin δδ = G” (loss modulus)= G” (loss modulus)
2.2. FHWAFHWA|G*|G*ss|| sinsinδδss = = GG""s s (Strain Sweep)(Strain Sweep)
3.3. EEssential ssential WWork of ork of FFracture (EWF) racture (EWF) Simon Simon Hesp Hesp & Jack Youtcheff
TTISIS is the temperature where |G*|is the temperature where |G*|sinsinδδ = 5 M Pa at = 5 M Pa at ωω = 10 rad/s low strains (0.1= 10 rad/s low strains (0.1--0.4%), PAV0.4%), PAV
& Jack Youtcheff
|G*|sin|G*|sinδδ −− FailureFailure
Bahia, H. U., Hanson, D. I., Zeng, M., Zhai, H., Khatri, M. A. aBahia, H. U., Hanson, D. I., Zeng, M., Zhai, H., Khatri, M. A. and Anderson, M. A. (2001). nd Anderson, M. A. (2001). ““Characterization of modified asphalt binders in Superpave mix deCharacterization of modified asphalt binders in Superpave mix design.sign.”” National Cooperative National Cooperative Highway Research Program NCHRP Report 459, Highway Research Program NCHRP Report 459, Transportation Research Board Transportation Research Board -- National Research National Research Council, National Academy Press, Washington D.C.Council, National Academy Press, Washington D.C.
Gravel Fine Aggregate
R2 = 0.1878
4.0E+06
6.0E+06
8.0E+06
1.0E+07
1.2E+07
0 20000 40000 60000 80000 100000
Mixture Fatigue Life (N50)
Bin
der |
G*|
sin
δ (P
a)
|G*|G*ss|sin|sinδδss −− Strain Sweep Strain Sweep
Shenoy, Aroon (2002). Shenoy, Aroon (2002). ““Fatigue testing and evaluation of asphalt binders using the dynaFatigue testing and evaluation of asphalt binders using the dynamic shear mic shear rheometer.rheometer.”” Journal of Testing and EvaluationJournal of Testing and Evaluation, , 30(4), 30330(4), 303--312. 312.
G" from strain sweep versus Cycles to Failure
750000800000850000900000950000
0 500 1000N f
G" s
=|G
* s|s
inδ
s
B6225 @24CB6226 @29CB6227 @26CB6228 @19CB6229 @23CB6230 @20CB6231 @22CB6232 @25CB6233 @21CB6243 @14CB6251 @23CAC-5 @16CAC-20 @25CStyrelf @24CNovophalt @30CBest Line
R 2=0.82
EWFEWF −− Ductile fracture energy that is Ductile fracture energy that is dissipated during the binder fracture testdissipated during the binder fracture test
(No Criterion Yet)(No Criterion Yet)
L
80 mm
30 mm
Andriescu, A., Hesp, S. A. M. and Youtcheff, J. S. (2004). Andriescu, A., Hesp, S. A. M. and Youtcheff, J. S. (2004). ““On the Essential and Plastic Works of On the Essential and Plastic Works of Ductile Fracture in Asphalt Binders.Ductile Fracture in Asphalt Binders.”” 83rd Annual Meeting of the Transportation Research Board, Washington DC.
•• Ligament lengths (L): 5, 10, 15, 20 and 25 mmLigament lengths (L): 5, 10, 15, 20 and 25 mm
•• Sample thickness (B): 6.5 mmSample thickness (B): 6.5 mm
•• Strain rate = 100 mm/minStrain rate = 100 mm/min
•• T = 25T = 25ooCC
Summary of Binder and ALF Summary of Binder and ALF Fatigue DataFatigue Data
Parameter 1Parameter 1 Parameter 2Parameter 2 Parameter 3Parameter 3 ALF Data
Crack Length (m)
at 100K ALF
Passes
ALF Passes at
50 m Crack Length
90.690.6
115115
00
24.924.9
99
BinderBinder
|G*|sin|G*|sinδ δ value at value at
1919°°C, C, 10 rads/s, 10 rads/s,
0.4% 0.4% strain, PAV strain, PAV
TTISIS when when |G*|sin|G*|sinδδ = =
5 MPa 5 MPa (10 rads/s, (10 rads/s,
0.4% 0.4% strain, strain, PAV)PAV)
|G*|G*ss|sin|sinδδssvalue at value at
1919°°C, C, 10 rads/s, 10 rads/s,
25% strain, 25% strain, RTFOTRTFOT
TTISIS = = TTEEsinsinδδss
where Twhere TEE is is when |G*when |G*ss| |
= 1 MPa = 1 MPa (10 rads/s, (10 rads/s, 25% strain, 25% strain,
RTFOT)RTFOT)
EWF EWF (kJ/m(kJ/m22))
ControlControl 1210000012100000 26.026.0 39400003940000 28.128.1 7.937.93 6627966279
Air Air BlownBlown
68100006810000 22.622.6 23900002390000 24.824.8 7.847.84 4797347973
SBSSBS--lglg 40600004060000 18.118.1 13600001360000 19.219.2 10.810.8 270029270029
TBCRTBCR 42100004210000 17.917.9 12800001280000 19.119.1 4.414.41 154651154651
TerTer--polymerpolymer
26100002610000 14.314.3 910000910000 16.816.8 4.704.70 175171175171
Summary of Binder RankingsSummary of Binder Rankings
Parameter 1Parameter 1 Parameter 2Parameter 2 Parameter 3Parameter 3 ALF Data
Crack Length (m)
at 100K ALF
Passes
DD
EE
AA
CC
BB
ALF Passes at
50 m Crack Length
BinderBinder
|G*|sin|G*|sinδ δ value at value at
1919°°C, C, 10 rads/s, 10 rads/s,
0.4% 0.4% strain, PAV strain, PAV
TTISIS when when |G*|sin|G*|sinδδ = =
5 MPa 5 MPa (10 rads/s, (10 rads/s,
0.4% 0.4% strain, strain, PAV)PAV)
|G*|G*ss|sin|sinδδssvalue at value at
1919°°C, C, 10 rads/s, 10 rads/s,
25% strain, 25% strain, RTFOTRTFOT
TTISIS = = TTEEsinsinδδss
where Twhere TEE is is when |G*when |G*ss| |
= 1 MPa = 1 MPa (10 rads/s, (10 rads/s, 25% strain, 25% strain,
RTFOT)RTFOT)
EWF EWF (kJ/m(kJ/m22))
ControlControl DD DD DD DD BB DDAirAir
BlownBlown CC CC CC CC BB EE
SBSSBS--lglg BB BB BB BB AA AATBCRTBCR BB BB BB BB CC CCTerTer--
polymerpolymer AA AA AA AA CC BB
Binder RankingsBinder RankingsConsistent with ALF Data.Consistent with ALF Data.
Parameter 1Parameter 1 Parameter 2Parameter 2 Parameter 3Parameter 3 ALF Data
Crack Length (m)
at 100K ALF
Passes
DD
EE
AA
CC
BB
ALF Passes at
50 m Crack Length
BinderBinder
|G*|sin|G*|sinδ δ value at value at
1919°°C, C, 10 rads/s, 10 rads/s,
0.4% 0.4% strain, PAV strain, PAV
TTISIS when when |G*|sin|G*|sinδδ = =
5 MPa 5 MPa (10 rads/s, (10 rads/s,
0.4% 0.4% strain, strain, PAV)PAV)
|G*|G*ss|sin|sinδδssvalue at value at
1919°°C, C, 10 rads/s, 10 rads/s,
25% strain, 25% strain, RTFOTRTFOT
TTISIS = = TTEEsinsinδδss
where Twhere TEE is is when |G*when |G*ss| |
= 1 MPa = 1 MPa (10 rads/s, (10 rads/s, 25% strain, 25% strain,
RTFOT)RTFOT)
EWF EWF (kJ/m(kJ/m22))
ControlControl DD DD DD DD BB DDAirAir
BlownBlown CC CC CC CC BB EE
SBSSBS--lglg BB BB BB BB AA AATBCRTBCR BB BB BB BB CC CCTerTer--
polymerpolymer AA AA AA AA CC BB
Binder RankingsBinder RankingsTop , Bottom .Top , Bottom .
Parameter 1Parameter 1 Parameter 2Parameter 2 Parameter 3Parameter 3 ALF Data
Crack Length (m)
at 100K ALF
Passes
DD
EE
AACC
BB
ALF Passes at
50 m Crack Length
BinderBinder
|G*|sin|G*|sinδ δ value at value at
1919°°C, C, 10 rads/s, 10 rads/s,
0.4% 0.4% strain, PAV strain, PAV
TTISIS when when |G*|sin|G*|sinδδ = =
5 MPa 5 MPa (10 rads/s, (10 rads/s,
0.4% 0.4% strain, strain, PAV)PAV)
|G*|G*ss|sin|sinδδssvalue at value at
1919°°C, C, 10 rads/s, 10 rads/s,
25% strain, 25% strain, RTFOTRTFOT
TTISIS = = TTEEsinsinδδss
where Twhere TEE is is when |G*when |G*ss| |
= 1 MPa = 1 MPa (10 rads/s, (10 rads/s, 25% strain, 25% strain,
RTFOT)RTFOT)
EWF EWF (kJ/m(kJ/m22))
ControlControl DD DD DD DD BB DDAir Air
BlownBlown CC CC CC CC BB EE
SBSSBS--lglg BB BB BB BB AA AATBCRTBCR BB BB BB BB CC CCTerTer--
polymerpolymer AA AA AA AA CC BB
Statistical RelationshipsStatistical RelationshipsRR22
Parameter 1Parameter 1 Parameter 2Parameter 2 Parameter 3Parameter 3
ALF Data
R-squared R2
|G*|sin|G*|sinδ δ value value at 19at 19°°C, C,
10 rads/s, 10 rads/s, 0.4% strain, 0.4% strain,
PAV PAV
TTISIS when when |G*|sin|G*|sinδδ = =
5 MPa 5 MPa (10 rads/s, (10 rads/s,
0.4% strain, 0.4% strain, PAV)PAV)
|G*|G*ss|sin|sinδδssvalue at value at
1919°°C, C, 10 rads/s, 10 rads/s,
25% strain, 25% strain, RTFOTRTFOT
TTISIS = T= TEEsinsinδδsswhere Twhere TEEis when is when
|G*|G*ss| = 1 MPa | = 1 MPa (10 rads/s, (10 rads/s, 25% strain, 25% strain,
RTFOT)RTFOT)
EWF (kJ/mEWF (kJ/m22))
Crack Length (m) at100K LoadPasses & 19°C
0.56 0.71 0.61 0.78 0.013
ALF Passes at 50 m Crack Length & 19°C
0.47 0.50 0.50 0.59 0.058
Mixture CharacterizationMixture Characterization
Bending Beam Fatigue TestsBending Beam Fatigue TestsDifferent Analysis Methods and CriteriaDifferent Analysis Methods and CriteriaDynamic Modulus (EDynamic Modulus (E**))IDT Tensile Strength (SIDT Tensile Strength (Stt))
On going testing and analysis…On going testing and analysis…
Bending Beam Fatigue Bending Beam Fatigue DeviceDevice
Fatigue Testing Procedure…Fatigue Testing Procedure…
Bending Beam Fatigue Test:
Conducted according to AASHTO provisional test method TP8-94 (2002).
Strain-controlled mode at a high strain level of 1250 micro-strains.
Test temperature = 19°C.
Fatigue Testing ProcedureFatigue Testing Procedure
Bending Beam Fatigue Test:
A vertical sinusoidal displacement is applied at a frequency of 10 Hz with no rest periods.
Test run up to approximately 300,000 load cycles.
Bending Beam Fatigue Test Schematic Bending Beam Fatigue Test Schematic DiagramDiagram
Two concentrated and symmetrical loads.
Reaction Reaction
Load LoadSpecimenClamp
Deflection
SpecimenRepeated sinusoidal loading at 10 Hz frequency.
Specimen forced back to its original position at the end of each load pulse.
Bending Beam Fatigue Testing Bending Beam Fatigue Testing TheoryTheory
V
M
Specimen subjected to 4-point bending.
P/2 P/2
R R
a=l/3
Shear:
R = P = V
Moment:
M = Pa
a a
l
h
Freedom Conditions of Beam Fatigue TestFreedom Conditions of Beam Fatigue Test
Specimen subjected to 4-point bending.
Free rotation and horizontal translation at all loads and reaction points.
OutlineOutline
ALF and Bending Beam Fatigue TestsALF and Bending Beam Fatigue TestsDifferent Analysis Methods and CriteriaDifferent Analysis Methods and CriteriaLab Fatigue vs. ALF Fatigue and RankingLab Fatigue vs. ALF Fatigue and RankingDynamic Modulus (EDynamic Modulus (E**) vs. ALF Fatigue) vs. ALF FatigueIDT Tensile Strength (SIDT Tensile Strength (Stt) vs. ALF Fatigue) vs. ALF FatigueFuture PlansFuture Plans
Different Fatigue Failure Methods and Different Fatigue Failure Methods and CriteriaCriteria
50% reduction in stiffness adopted by the AASHTO (TP8-94 [2002]).
Ratio of dissipated energy change (Ghuzlan and Carpenter (TRR 1723 [2000]).
Stress-strain Hysteresis loop or sinusoidal waveform progressive distortion (Al-Khateeb and Shenoy (AAPT Journal [2004]).
5050--Percent Reduction in Percent Reduction in StiffnessStiffness
0
220
440
660
880
0 50000 100000 150000 200000
Number of Load Cycles, N
50-percent stiffness reduction
Ratio of Dissipated Energy Ratio of Dissipated Energy Change…Change…
Dissipated energy ratio Rw:
N
NNw w
wwR
−= +1
where:wN+1 = Dissipated energy in (N+1)th
cycle; wN = Dissipated energy in Nth cycle.
Ratio of Dissipated Energy Ratio of Dissipated Energy Change Change
Energy ratio decreases in the first part of the fatigue test, and then fluctuates around a flat plateau, then sharply increases.
The failure point is when the curve shoots up.
Hysteresis Loop CriterionHysteresis Loop Criterion(Before Fatigue Failure)(Before Fatigue Failure)
(a) Before Failure
-500
-300
-100
100
300
500
-0.002 0 0.002 0.004 0.006 0.008 0.01
Strain (m/m)
Stre
ss (k
Pa)
90,000 110,000130,000 170,000150,000
Hysteresis Loop CriterionHysteresis Loop Criterion(First Fatigue Failure)(First Fatigue Failure)
(b) First Failure
-300
-100
100
300
0.008 0.009 0.01 0.011 0.012 0.013 0.014 0.015 0.016
Strain (m/m)
Str
ess (
kP
a)
190,000 210,000 230,000
Hysteresis Loop CriterionHysteresis Loop Criterion(Complete Fatigue Failure)(Complete Fatigue Failure)
(c) Complete Failure
-300
-100
100
300
0.014 0.016 0.018
Strain (m/m)
Stre
ss (k
Pa) 250,000 270,000
OutlineOutline
ALF and Bending Beam Fatigue TestsALF and Bending Beam Fatigue TestsDifferent Analysis Methods and CriteriaDifferent Analysis Methods and CriteriaLab Fatigue vs. ALF Fatigue and RankingLab Fatigue vs. ALF Fatigue and RankingDynamic Modulus (EDynamic Modulus (E**) vs. ALF Fatigue) vs. ALF FatigueIDT Tensile Strength (SIDT Tensile Strength (Stt) vs. ALF Fatigue) vs. ALF FatigueFuture PlansFuture Plans
ALF Load Passes vs. Crack ALF Load Passes vs. Crack LengthLength
0
20
40
60
80
100
120
0 100000 200000 300000 400000
Number of ALF Passes
Cum
ulat
ive
Cra
ck L
engt
h (m
)
L3S3 (Air Blown)L2S3 (Control)L5S3 (CR-TB)L6S3 (Terpolymer)L4S3 (SBS LG)L7S3 (Fibers)L1S2 (CR-AZ)
ALF Load Passes vs. % Area CrackedALF Load Passes vs. % Area Cracked
0
20
40
60
80
100
120
0 100000 200000 300000 400000
Number of ALF Passes
Perc
enta
ge o
f Are
a C
rack
ed, %
L2S3 (Control)L3S3 (Air Blown)L5S3 (CR-TB)L6S3 (Terpolymer)L4S3 (SBS LG)L1S2 (CR-AZ)
ALF Load Passes at 50ALF Load Passes at 50--m Crack m Crack LengthLength
050000
100000150000200000250000300000
ALF
Pas
ses
at 5
0-m
Cra
ck L
engt
h
Lane 3
/Air B
lownLan
e 2/70
-22Lan
e 5/C
R-TB
Lane 6
/Terp
olymer
Lane 4
/SBS LG
Cycles to Failure from Bending Beam Cycles to Failure from Bending Beam Fatigue TestFatigue Test
050,000
100,000150,000200,000250,000
Cyc
les
to
Failu
re
Lanes
3&10
/Air B
lownLan
e 1/A
Z-CR
Lanes
6&12
/Terpo...
Lane 9
/SBS 64-40
OutlineOutline
ALF and Bending Beam Fatigue TestsALF and Bending Beam Fatigue TestsDifferent Analysis Methods and CriteriaDifferent Analysis Methods and CriteriaLab Fatigue vs. ALF Fatigue and RankingLab Fatigue vs. ALF Fatigue and RankingDynamic Modulus (EDynamic Modulus (E**) vs. ALF Fatigue) vs. ALF FatigueIDT Tensile Strength (SIDT Tensile Strength (Stt) vs. ALF Fatigue) vs. ALF FatigueFuture PlansFuture Plans
EE** sin sin δδ vs. ALF Fatigue…vs. ALF Fatigue…
Does EDoes E** sin sin δδ correlate well with the correlate well with the ALF fatigue cracking?ALF fatigue cracking?
If not, what other mixture If not, what other mixture parameters could capture the ALF parameters could capture the ALF fatigue?fatigue?
EE** sin sin δδ vs. ALF Passes at 50vs. ALF Passes at 50--m Crack m Crack Length…Length…
N50-m CL = 1E+19 (E*sin δ) -4.212
R2 = 0.760
100000
200000
300000
0 500 1000 1500 2000 2500 3000
E* sin δ at 10 Hz
ALF
Pas
ses
at 5
0-m
Cra
ck
Leng
th
EE** sin sin δδ vs. ALF Passes at 50vs. ALF Passes at 50--m Crack m Crack LengthLength
N50-m CL = 2E+10 (E*sin δ)-1.827
R2 = 0.850
100000
200000
300000
0 200 400 600 800 1000 1200
E* sin δ at 0.1 Hz
ALF
Pas
ses
at 5
0-m
Cra
ck
Leng
th
EE** sin sin δδ vs. Crack Length at 100,000 ALF vs. Crack Length at 100,000 ALF Passes…Passes…
CL100,000 ALF Passes = 0.150 (E*sin δ) - 256.6R2 = 0.80
0
50
100
150
0 500 1000 1500 2000 2500 3000
E* sin δ at 10 Hz
Cra
ck L
engt
h at
100
,000
ALF
Pa
sses
EE** sin sin δδ vs. Crack Length at 100,000 ALF vs. Crack Length at 100,000 ALF PassesPasses
CL100,000 ALF Passes = 0.184 (E*sin δ) - 83.5R2 = 0.88
0
50
100
150
0 200 400 600 800 1000 1200
E* sin δ at 0.1 Hz
Cra
ck L
engt
h at
100
,000
ALF
Pa
sses
EE** sin sin δδ vs. ALF Fatiguevs. ALF FatigueIt seems that EIt seems that E** sin sin δδ correlate very well correlate very well with the ALF passes at 50with the ALF passes at 50--m fatigue crack m fatigue crack length, Rlength, R22 = 0.76 and 0.85 for 10 Hz and = 0.76 and 0.85 for 10 Hz and 0.1 Hz, respectively (Power Relationship).0.1 Hz, respectively (Power Relationship).
Also EAlso E** sin sin δδ correlate very well with the correlate very well with the ALF fatigue crack length at 100,000 ALF fatigue crack length at 100,000 passes, Rpasses, R22 = 0.80 and 0.88 for 10 Hz and = 0.80 and 0.88 for 10 Hz and 0.1 Hz, respectively (Linear Relationship).0.1 Hz, respectively (Linear Relationship).
OutlineOutline
ALF and Bending Beam Fatigue TestsALF and Bending Beam Fatigue TestsDifferent Analysis Methods and CriteriaDifferent Analysis Methods and CriteriaLab Fatigue vs. ALF Fatigue and RankingLab Fatigue vs. ALF Fatigue and RankingDynamic Modulus (EDynamic Modulus (E**) vs. ALF Fatigue) vs. ALF FatigueIDT Tensile Strength (SIDT Tensile Strength (Stt) vs. ALF Fatigue) vs. ALF FatigueFuture PlansFuture Plans
IDT Tensile Properties vs. ALF IDT Tensile Properties vs. ALF Fatigue…Fatigue…
How well the tensile properties How well the tensile properties from the IDT correlate with the from the IDT correlate with the ALF pavement fatigue cracking?ALF pavement fatigue cracking?
IDT SIDT Stt vs. ALF Passesvs. ALF Passes
ALF Passes = - 244.08 St + 414993R2 = 0.27
0
100000
200000
300000
0 200 400 600 800 1000 1200 1400IDT Tensile Strength (kPa)
ALF
Pas
ses
at 5
0-m
Cra
ck
Leng
th
IDT IDT εεtt vs. ALF Passesvs. ALF Passes
ALF Passes = - 170.63 εt + 448916R2 = 0.52
0
100000
200000
300000
0 500 1000 1500 2000 2500IDT Tensile Strain at Failure (microstrains)
ALF
Pas
ses
at 5
0-m
Cra
ck
Leng
th
IDT SIDT Stt vs. ALF Crack vs. ALF Crack LengthLength
Crack Length = 0.192 St - 164.2R2 = 0.69
0
20
40
60
80
100
0 200 400 600 800 1000 1200 1400
IDT Tensile Strength (kPa)
Cra
ck L
eng
th a
t 10
0,00
0 A
LF
Pas
ses
(m)
IDT IDT εεtt vs. ALF Crack Lengthvs. ALF Crack Length
Crack Length = 0.089 εt - 115.5R2 = 0.58
0
20
40
60
80
100
0 500 1000 1500 2000 2500
IDT Tensile Strain at Failure (microstrains)
Cra
ck L
engt
h at
100
,000
ALF
Pa
sses
(m)
IDT Tensile Properties vs. ALF IDT Tensile Properties vs. ALF Fatigue Fatigue
The IDT tensile strength seems to have The IDT tensile strength seems to have good correlation with the crack length at good correlation with the crack length at 100,000 passes, R100,000 passes, R22 = 0.69.= 0.69.
The IDT tensile strain at failure has good The IDT tensile strain at failure has good correlation with the ALF passes at 50correlation with the ALF passes at 50--m m crack length and the crack length at crack length and the crack length at 100,000 passes with R100,000 passes with R22 = 0.52, and 0.58, = 0.52, and 0.58, respectively.respectively.
OutlineOutline
ALF and Bending Beam Fatigue TestsALF and Bending Beam Fatigue TestsDifferent Analysis Methods and CriteriaDifferent Analysis Methods and CriteriaLab Fatigue vs. ALF Fatigue and RankingLab Fatigue vs. ALF Fatigue and RankingDynamic Modulus (EDynamic Modulus (E**) vs. ALF Fatigue) vs. ALF FatigueIDT Tensile Strength (SIDT Tensile Strength (Stt) vs. ALF Fatigue) vs. ALF FatigueFuture PlansFuture Plans
Future Fatigue Testing And Future Fatigue Testing And Analysis…Analysis…
To complete the full matrix of To complete the full matrix of bending beam fatigue testing (3 bending beam fatigue testing (3 strain levels x 8 mixtures x 3 to 5 strain levels x 8 mixtures x 3 to 5 replicates = 72 to 120 tests).replicates = 72 to 120 tests).
To run uniaxial fatigue tests in To run uniaxial fatigue tests in tension at the same temperature tension at the same temperature 19°C.19°C.
Future Fatigue Testing And Future Fatigue Testing And Analysis…Analysis…
To use the aforementioned fatigue To use the aforementioned fatigue analysis methods and criteria.analysis methods and criteria.
To investigate new methods for To investigate new methods for fatigue data analysis.fatigue data analysis.
Future Fatigue Testing And Future Fatigue Testing And AnalysisAnalysis
To predict the tensile strains at the To predict the tensile strains at the bottom of the asphalt layer using the bottom of the asphalt layer using the solutions of the multisolutions of the multi--layer elastic or layer elastic or viscovisco--elastic theory.elastic theory.
To compare the predicted strains To compare the predicted strains with those measured under the ALF with those measured under the ALF pavements.pavements.
Uniaxial Fatigue Testing…Uniaxial Fatigue Testing…
Uniaxial Fatigue Testing…Uniaxial Fatigue Testing…
Tests will be conducted at a Tests will be conducted at a temperature of 19°C.temperature of 19°C.
A vertical sinusoidal loading will be A vertical sinusoidal loading will be applied at a frequency of 10 Hz with applied at a frequency of 10 Hz with no rest periodsno rest periods. .
Uniaxial Fatigue Testing…Uniaxial Fatigue Testing…
Tests will be conducted in the stressTests will be conducted in the stress--controlled fatigue mode.controlled fatigue mode.
Stresses in uniaxial testing are Stresses in uniaxial testing are uniform.uniform.
NewWarm-MixTechnology
Superpave Performance TesterSuperpave Performance TesterAASHTO TP 62AASHTO TP 62--0303
Performance Sample PreparationPerformance Sample Preparation
Estimation of Modulus Estimation of Modulus WitczakWitczakModelModel
))log(393532.0)log(313351.0603313.0(34
238384
42
200200
100547.0)(000017.0003958.00021.0871977.382208.0
058097.0002841.0)(001767.002923.0249937.1*log
η
ρρρρ
ρρρ
−−−++−+−
++
−
−−−+−=
fabeff
beff
a
eVVV
VE
│E*│= dynamic modulus, 105 psih = viscosity of asphalt binder, 106 psif = loading frequency, Hz
Va = air void content, percentVbeff = effective asphalt binder content, percent by volumer34 = cumulative percent retained on the 19 mm siever38 = cumulative percent retained on the 9.5 mm siever4 = cumulative percent retained on the 4.76 mm siever200 = percent passing 0.075 mm sieve
Hirsch Model (Algorithm)Hirsch Model (Algorithm)
⎥⎥⎥⎥
⎦
⎤
⎢⎢⎢⎢
⎣
⎡
+⎟⎠⎞
⎜⎝⎛ −
−+⎥
⎦
⎤⎢⎣
⎡⎟⎠
⎞⎜⎝
⎛+⎟
⎠⎞
⎜⎝⎛ −=
)(*3000,200,4100
1
1000,10
*3100
1000,200,4|*|
VFAGVMA
VMAPVMAxVFA
GVMAPE
binder
cbindercmix
Where,
58.0
58.0
)(*3650
)(*320
⎟⎟⎠
⎞⎜⎜⎝
⎛+
⎟⎟⎠
⎞⎜⎜⎝
⎛+
=
VMAVFAG
VMAVFAG
Pc
Information needed for estimation Information needed for estimation of |E*|of |E*|
•• Gradation of the hot mixGradation of the hot mix•• Volumetric properties of the hot mixVolumetric properties of the hot mix•• Asphalt Binder propertiesAsphalt Binder properties
Aggregate Shape Properties and Aggregate Shape Properties and Influence on HMA PerformanceInfluence on HMA Performance
AIMS System, Developed Eyad MasadManufacture red by Pine Instruments
Strain @ Flow
y = 0.8685x + 931.09R2 = 0.8795
0
5000
10000
15000
20000
25000
30000
35000
40000
0 5000 10000 15000 20000 25000 30000 35000 40000 45000
Measured, microstrain
Pre
dict
ed, m
icro
stra
in
From Consensus to Performance From Consensus to Performance Based Aggregate CriteriaBased Aggregate Criteria
Superpave Gyratory Superpave Gyratory Compactor CalibrationCompactor Calibration
• Determine the relationship between mix stiffness and eccentricity
• Establish an average mix eccentricity “Standard Stiffness” for calibration
• Compare the RAM and the HMS
• Evaluate Mix-less procedures to DAV
FHWA Paper StudyFHWA Paper StudyIN DOTIN DOT251912.59.54.752.361.180.60.30.075
0 1 2 3 4 5
Sieve Opening Raised to 0.45 Power
0
10
20
30
40
50
60
70
80
90
100
Perc
ent P
assi
ng
SampleMax DensityControl Points
FHWA 0.45 Power ChartColorado Mix - Sampled Aug 2001
19mm CO Production HMA
Normal Distributions
0
5
3.0 3.2 3.4 3.6 3.8 4.0 4.2 4.4 4.6 4.8 5.0
Compacted Air Void Content, %
Dis
trib
utio
n, f(
x, s
)
Pine InstrumentsHMA Lab Supply
Pine Instruments
HMA Lab Supply
24%
FHWA Paper StudyFHWA Paper StudyIN DOTIN DOT251912.59.54.752.361.180.60.30.075
0 1 2 3 4 5
Sieve Opening Raised to 0.45 Power
0
10
20
30
40
50
60
70
80
90
100
Perc
ent P
assi
ng
SampleMax DensityControl Points
FHWA 0.45 Power ChartColorado Mix - Sampled Aug 2001
3 3.5 4 4.5 5 5.5Air Void Content @ 50 Gyrations
HMA-2 Paper Mean = 3.74Std. Dev. = 0.24n=6
Pine Paper Mean = 3.97Std. Dev. = 0.25n=13
No Paper, OilMean = 4.08Std. Dev. = 0.18n=13
HMA-1 PaperMean = 4.39Std. Dev. = 0.29n=13
19mm CO Production HMA
ONGOING ONGOING RefinementRefinement
•• Understanding modifiersUnderstanding modifiers•• Understanding acidUnderstanding acid•• Improved moisture testImproved moisture test•• Construction qualityConstruction quality•• Link to pavement designLink to pavement design•• Communication! Communication!
CHALLENGES
“What kind of cup do we have?”“What kind of cup do we have?”
++++
++++
++ +++