CalME Design and Analysis Software for Pavement Design and Analysis, and Analysis of HVS Results
Presented by D Jones, UCPRC Prepared by J Harvey, UCPRC On behalf of many at UCPRC, Dynatest, CSIR and other collaborators around the world
CalME Design and Analysis Software for Pavement Design and - - PowerPoint PPT Presentation
CalME Design and Analysis Software for Pavement Design and Analysis, and Analysis of HVS Results Presented by D Jones, UCPRC Prepared by J Harvey, UCPRC On behalf of many at UCPRC, Dynatest, CSIR and other collaborators around the world
Presented by D Jones, UCPRC Prepared by J Harvey, UCPRC On behalf of many at UCPRC, Dynatest, CSIR and other collaborators around the world
Flexible, composite and semi-rigid pavements Emphasis on rehabilitation and preservation
Interfaces for analysis of HVS instrumentation Models set up for HVS and other APT data
Models the entire damage and distress
Permits calibration using instrumentation and
Developed by Per Ullidtz, Dynatest Focus of rest of presentation
Incremental – simulation runs at one
Recursive – output from one increment as
Pavement response calculated from wheel
Damage and permanent deformation
Same format as MEPDG but
some parameters are identified differently
aT ref
lt tr × = η η
δ, α, β, γ, aT, A, VTS = model parameters tr = reduced loading time lt = actual loading time η= viscosity T= loading temperature
Rankine
Basic approach implemented to account for
Needs local calibration
Temporary stiffness decrease when small rest
Considered in shift factor based on average
May include some healing effects
× − − × = actor StiffnessF S S E E
ref ref n n 3 3 ,
1 1
−
1 1 3 n i i
kN P
40
α
α, StiffnessFactor = model param. Sref = normalizing constant E = stiffness P = Wheel load S = Combined bending stiffness h = Layer thickness Second type of nonlinearity from confinement effect of overlying layers First type of nonlinearity, classic stress harden or soften
Section N1
y = 56.288x + 61.232 R2 = 0.5902 y = 35.536x + 18.118 R2 = 0.733 20 40 60 80 100 120 140 0.2 0.4 0.6 0.8 1 1.2 Stiffness ratio, S/Sref Modulus, MPa AB SG Linear (AB) Linear (SG)
30 Years of pre-calculated Surface temperature 1-D FEM to calculate in-depth temperature
Axle load spectra in database based on axle
Includes extrapolation to all locations on state
Spectra and extrapolation approach can be
Simulates HVS loading
Odemark-Bousinesq OpenPave Layer Elastic Analysis program
Regression equation based on FEM analysis 2-d to develop sensitivity to parameters 3-d to get realistic values
CalME designed to work with layer stiffness back-
calculation program CalBack
Recommend FWD testing repeated two times of the day:
characterization of HMA master stiffness curve
Database of typical new materials in software
Updated with each new project
Lab testing protocols for new materials Stiffness variability for Monte
Carlo from back-calculation within project
Asphalt and asphalt stabilized recycled
Aggregate base, subbase and subgrade
Cement/asphalt stabilized stiffness, cracking,
15
i HMA
e i
γ β α
ref ref p
Α, α, β, γ = model parameters εref , Eref = normalizing constant dp = permanent deformation MN = number of load repetitions in million ε = vertical strain at the top of the unbound layer E = Layer stiffness
tr E log exp 1 ) 1 ( log γ β ω α δ + + − × + =
α
ω ⋅ =
p FAT MN
SF MN
° × + = C t 1 exp
1
α α α
δ γ β
ε ε × × × =
ref i ref ref p
E E E E A MN
Α, α0, α1, β, γ, δ = model parameters εref , Eref = normalizing constant MN = N in millions MNp = Allowable N ε = bending strain E = Damaged stiffness Ei = Intact stiffness
Surface crack
density is related to damage in deterministic analysis:
α
ω ω + =
2
1 m/m .0 10 CR
a ref HMA initiation
h h + = 1 1 ω
1 2 3 4 5 6 7 8 9 10 0.2 0.4 0.6 0.8 1 Damage Surface Crack Density (m/m^2) HMA = 150mm HMA = 100mm HMA = 50mm
α, a = calibration parameters hHMA = HMA thickness, href = normalizing const. ωinitiation = damage at crack initiation
HMA/HMA overlay: average maximum tensile
HMA/PCC overlay: bending strain at the crack
Two damages are calculated, one for fatigue
Deterministic Within project variability (Monte Carlo simulation) Between projects variability (sensitivity analysis)
sensitivity analysis if warranted
Random selection of initial year and day used to
Damage to surface layer Cracking of surface layer, m/m2
Permanent deformation of each layer Down rut on surface
Thicknesses Stiffnesses (default or from back-calculation) Materials constants for permanent deformation,
fatigue and cracking
Calculate the standard deviation of rut Generate 300-mm of longitudinal profile using
Calculate IRI based on the profile Roughness from standard deviation on rut depth
0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 5 10 15 20 25 30 35 40 45 Age, years Stdev on rut, mm 1 2 3 4 5 6 7 IRI, m/km Stdev on rut IRI
M&R strategies designated by designer, or Other strategies can be implemented
Rehabilitation only (RRR) Rehabilitation, 2
preservations, then rehab (RPPR)
Rehabilitation and then
perpetual pavement preservation (RPPP)
27 Heavy Vehicle Simulator
(HVS) test sections
26 Westrack sections; NCAT, MnROAD validation
Calibrate damage models with deflections, strains, back-
calculated stiffness
Once damage process through entire life of pavement is
match, calibrate cracking and rutting
M = measured C = calculated
Shift factor, SF, for damage evolution All parameters for relating damage to surface
WesTrack: beam frequency sweep and
HVS tests from UCPRC: beam frequency
NCAT, MnROAD sections used for validation Further calibration with other HVS, APT and
Step 1: Shift Factor for damage
Back-calculate AC stiffness from FWD => stiffness
history
Back-calculate AC damage history Predict AC damage history with CalME Adjust shift factor to match
Step 2: Damage to surface crack density
Back-calculated damage history Measured surface crack density history Adjust parameters to match
Final shift factors:
Fatigue and reflection cracking 1.0 HMA rutting 1.0, other asphalt mixes 0.5
Wes02 in wheel tracks
0.00 0.05 0.10 0.15 0.20 0.25 0.30 0.35 0.40 0.45 0.50 01-Jan-96 01-Jul-96 31-Dec-96 01-Jul-97 31-Dec-97 Date Damage 10 20 30 40 50 60 70 80 90 100 Cracking % FWD CalME damage LWP % Fatigue Cracking RWP % Fatigue Cracking Calculated RWP Calculated LWP
Empirical Cumulative Distribution Function
10 20 30 40 50 60 70 80 90 100 0.01 0.1 1 10 100 Damage Shift Factor Cumulative Probability (%)
HVS WesTrack
Caltrans to design long-life rehab projects
UCPRC for HVS section analysis (adding new
Email jtharvey@ucdavis.edu Requirements: give us your feedback
for HVS and design Languages other than English
Assistance with updating databases with local
Perpetual license to source code of improved