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Publication Number:  FHWA-HRT-16-011    Date:  December 2017
Publication Number: FHWA-HRT-16-011
Date: December 2017

 

Using Falling Weight Deflectometer Data With Mechanistic-Empirical Design and Analysis, Volume III: Guidelines for Deflection Testing, Analysis, and Interpretation

CHAPTER 3. General Backcalculation Guidelines

Because the most common use of deflection data is in the backcalculation of the fundamental engineering parameters of the paving layers, this chapter has been prepared to provide general guidance on performing backcalculation. The guidelines are intended to assist the pavement engineer in conducting the backcalculation process, evaluating the results, and ensuring that those results are reasonable; however, they should be used only as general guidance because considerable engineering judgment and expertise is still required.

In addition to the guidelines on pavement backcalculation, this chapter describes the results of studies that have verified backcalculated results with instrumented pavement sections and also presents an example illustrating the interpretation of results from a backcalculation program.

Backcalculation Versus Forwardcalculation

In the backcalculation process, pavement deflections are determined using layer elastic theory, layer thickness, and assumed layer moduli (e.g., HMA layer, unbound base layer, and subgrade). An iterative approach is used to vary layer moduli until the calculated deflection basin matches the FWD-measured deflection basin. A solution is found when the difference between the measured and calculated deflection basin is minimized (discussed in the following sections).

In forwardcalculation, load and deflection data are entered into closed-form equations for estimating layer moduli. Forwardcalculation can be used to estimate layer moduli for the subgrade and bound surface layers, while intermediate layer (e.g., unbound base) moduli are estimated using modular ratios.(24)

The primary difference between backcalculation and forwardcalculation is that the former uses specific equations, while the latter uses an iterative procedure in estimating layer moduli.

Backcalculation Guidelines

Over the years, researchers and practitioners have developed numerous approaches to backcalculate pavement layer and subgrade moduli, as well as numerous software programs to perform the calculations. Table 8 summarizes available software programs that can be used for backcalculation of pavement deflection data that the research team was able to identify during the conduct of this research study.

Table 8. Summary of available backcalculation programs.
Program Name Public Domain Pavement Type Maximum Number of Layers Convergence Scheme Error Weighting Function
BAKFAA
Yes Flexible/rigid Five Sum of squares of absolute error Yes
BISDEF©
No Flexible Number of deflections; best for three unknowns Sum of squares of absolute error Yes
BOUSDEF 2.0
No Flexible At least four Sum of percent errors Varies
CHEVDEF
Yes Flexible Number of deflections; best for three unknowns Sum of squares of absolute error Yes
COMDEF
No Composite Three Various No
DBCONPAS
No Rigid Two N/A N/A
DIPLOBACK
No Composite Three Closed form solution N/A
ELMOD®/ ELCON 5
No Flexible/rigid Four (exclusive of rigid layer) Relative error of five sensors No
ELSDEF
No Flexible Number of deflections; best for three unknowns Sum of squares of absolute error Yes
EMOD
No Flexible Three Sum of relative squared error No
EVERCALC©
Yes Flexible Three (exclusive of rigid layer) Sum of absolute error No
FPEDD1
No Flexible Three- or four-layer model Relative deflection error No
ISSEM4
No Flexible Four Relative deflection error No
MICHBACK©
Yes Flexible/ composite Three + rigid layer Least squares Yes
MODTAG©
Yes Flexible Two to 15 layers; maximum of five unknown layers Relative deflection error at sensors No
MODULUS 6.0
Yes Flexible Four plus rigid layer Sum of relative squared error Yes
PADAL 2
No Flexible Four plus rigid layer Sum of relative squared error Yes
PCASE 2.08
Yes Rigid/flexible/ composite 5 Sum of squares of absolute error Yes
RPEDD1
No Rigid Three- or four-layer model Relative deflection error No
WESDEF
Yes Flexible Four + rigid layer Sum of squares of absolute error Yes

N/A = Not applicable.

Inputs Needed for Backcalculation Analysis

The following inputs are needed to perform a backcalculation analysis:

Backcalculation Pavement Model

A number of different factors must be considered in establishing a model of the pavement section for backcalculation, as described in the following sections.

Number of Layers

Ideally, no more than three (preferable) or four layers with unknown moduli should be used in the backcalculation process. If the backcalculation results produce unrealistic weak base moduli, it may be advantageous to eliminate the base layer and evaluate the pavement structure as a two-layer system. In this case, the lower base moduli may indicate contamination from the underlying subgrade, resulting in weaker base moduli owing to the presence of finer material.(25) If unrealistic results persist, then the analysis should consider the presence of a stiff layer.

When a pavement structure consists of a stiff layer between two weak layers, the backcalculation process may produce unrealistic moduli.(25) If this is the case, other means (e.g., laboratory testing) may be required for determining layer moduli.

Thickness of Layers

The following subsections provide guidelines for setting the layer thickness for each pavement layer.

HMA

It can be difficult to obtain reasonably backcalculated moduli for bituminous surface layers less than 75 mm (3 inches) thick. If the total thickness of the bituminous layer is less than 75 mm (3 inches), the modulus of the bituminous layer should be fixed (see table 9 for guidance) to allow backcalculation of the base and subgrade moduli.

Table 9. HMA moduli versus temperature.(26)
Temperature
(°C (°F))
HMA Modulus
(MPa (lbf/inch2))
-7 (20)
17,852 (2,589,138)
-1 (30)
15,066 (2,185,115)
4 (40)
11,881 (1,723,141)
10 (50)
8,754 (1,269,682)
16 (60)
6,027 (874,172)
21 (70)
3,878 (562,375)
27 (80)
2,331 (338,052)
32 (90)
1,309 (189,875)
38 (100)
687 (99,651)

Theoretically, backcalculation of each individual bituminous layer is possible, but this is generally not advised because of the complexity of evaluating more than three or four pavement layers. Ideally, all bituminous layers (seal coats, chip seals, and HMA) should be combined into a single layer unless there is evidence of an HMA layer exhibiting a unique distress.(27) In general, the presence of stripping or debonding of HMA layers reduces the backcalculated HMA moduli. In these cases, coring may be required to confirm the presence of stripping or debonding.

PCC

There are no thickness limitations associated with the backcalculation of modulus values for concrete pavements.

Unstabilized Base/Subbase Course

The presence of a thin base course beneath a thick HMA or PCC surface layer often results in low base moduli. This can occur because of the insignificant effects of a thin base beneath a very stiff thick layer, or it may be that the base modulus is low due to the stress sensitivity of granular materials.(25) In this case, it is advisable to combine the base with the subgrade and conduct the backcalculation as a two-layer system. If consideration of the base layer is desired, including a stiff layer in the backcalculation process may improve the base/subbase layers modulus estimate.

Subgrade

If an unusually high subgrade modulus is determined from the backcalculation results, the site should be investigated for the possible presence of a shallow bedrock/stiff layer or a high water table.

Initial and Moduli Ranges

The following subsections provide guidelines for the typical range of layer moduli that should be considered in establishing a pavement section model for backcalculation.

HMA

Generally, new HMA is observed to have backcalculated moduli ranging from 2,000 to 4,000 MPa (300,000 to 600,000 lbf/inch2), while a fatigue-cracked HMA is often observed to have backcalculated moduli between 700 and 1,400 MPa (100,000 to 200,000 lbf/inch2) at about 25 °C (77 °F). In some cases, areas of severe alligator cracking can result in backcalculated HMA layer moduli that significantly exceed the expected moduli values. If the HMA layer is known to have severe alligator cracking and results in high backcalculated layer moduli, it is recommended that either the HMA layer moduli be fixed at 700 to 1,400 MPa (100,000 to 200,000 lbf/inch2) or the testing location not be used in the backcalculation analysis. However, the presence of severe alligator cracking represents an area of structural deficiency and may require repair before overlay or at least should be taken into account during the overlay thickness design process.

If an HMA modulus range is required, an initial estimate of the HMA modulus should be made and then the range can be selected as 0.25 to five times that value.(27) For example, if the initial HMA modulus estimate is 2,800 MPa (400,000 lbf/inch2), then a range of 700 to 14,000 MPa (100,000 to 2 million lbf/inch2) is selected.

PCC

The modulus of an uncracked concrete pavement typically ranges from about 10,000 to 70,000 MPa (1.5 million to 10 million lbf/inch2).(28) An initial modulus ranging from 28,000 to 40,000 MPa (4 million to 6 million lbf/inch2) is typical.

Unstabilized Bases and Subbases

Initial modulus and moduli ranges are listed in Table 10 for a variety of unstabilized base and subbase materials.

Table 10. Typical layer moduli for unstabilized materials.(27-29)
Material Type Initial Modulus
(MPa (lbf/inch2))
Moduli Range
(MPa (lbf/inch2))
Uncrushed gravel
140-200 (20,000-30,000)
50-750 (7,000-110,000)
Crushed stone or gravel
200-345 (30,000-50,000)
70-7,000 (10,000-150,000)
Sand
100-140 (15,000-20,000)
35-550 (5,000-80,000)
Soil-aggregate mixture (predominantly fine-grained)
100-140 (15,000-20,000)
50-700 (7,000-100,000)
Soil-aggregate mixture (predominantly coarse-grained)
140-200 (20,000-30,000)
60-800 (9,000-120,000)

Note: Data in this table were taken from references 27-29.

Stabilized Bases and Subbases

Initial modulus and moduli ranges are presented in table 11 for a variety of stabilized base and subbase materials.

Table 11. Typical layer moduli for stabilized materials.(28,29)
Material Type Initial Modulus
(MPa (lbf/inch2))
Moduli Range
(MPa (lbf/inch2))
Asphalt treated 700-1,400 (100,000-200,000) 700-25,000 (100,000-3.5 million)
Sand asphalt 700-1,400 (100,000-200,000) 700-25,000 (100,000-3.5 million)
Fractured PCC 3,000-3,500 (400,000-500,000) 700-20,000 (100,000-3 million)
Cement aggregate mixture 3,000-3,500 (400,000-500,000) 2,000-20,000 (300,000-3 million)
Lean concrete 4,000-5,000 (600,000-700,000) 4,500-45,000 (650,000-6.5 million)
Cement treated 1,400-2,000 (200,000-300,000) 700-3,000 (100,000-400,000)
Lime stabilized 200-300 (30,000-40,000) 35-1,500 (5,000-200,000)
Soil cement 2,000-3,500 (300,000-500,000) 1,000-7,000 (150,000-1 million)

Note: Data in this table were taken from references 28 and 29.

Subgrade

Table 12 includes suggested values for subgrade moduli by soil type and climate condition.

Table 12. Typical moduli values of various subgrade materials for climate conditions.(30)
Material Dry
(MPa(lbf/inch2))
Wet-No Freeze
(MPa(lbf/inch2))
Wet-Freeze Unfrozen
(MPa(lbf/inch2))
Wet-Freeze Frozen
(MPa(lbf/inch2))
Clay 103 (15,000) 41 (6,000) 41 (6,000) 345 (50,000)
Silt 103 (15,000) 41 (6,000) 34 (5,000) 345 (50,000)
Silty or clayey sand 138 (20,000) 69 (10,000) 34 (5,000) 345 (50,000)
Sand 172 (25,000) 172 (25,000) 172 (25,000) 345 (50,000)
Silty or clayey gravel 276 (40,000) 207 (30,000) 138 (20,000) 345 (50,000)
Gravel 345 (50,000) 345 (50,000) 276 (40,000) 345 (50,000)

Poisson’s Ratio

Table 13 provides recommendations for Poisson’s ratio for various paving and subgrade materials.

Table 13. Typical Poisson’s ratio values.(31)
Material Type Poisson’s Ratio
HMA 0.35
PCC 0.15-0.20
Stabilized base or subbase 0.25-0.35
Unstabilized base or subbase 0.35
Cohesive (fine grain) subgrade soils 0.45
Cohesion less (coarse grain) subgrade soils 0.35-0.40
Stiff layer 0.35 or less

Depth to Bedrock/Stiff Layer or Water Table

The presence of shallow bedrock, a stiff clay layer, or high groundwater table can have a significant effect on backcalculated layer moduli. Assuming the subgrade layer to be a semi-infinite halfspace, while in reality the subgrade layer is only a few meters (feet) thick, causes the backcalculated moduli for the upper pavement layers to be incorrect. Generally, when the stiff layer is deeper than about 12 m (39 ft), its presence has little or no influence on the backcalculated moduli. The depth to the stiff layer can be evaluated by using a relationship between the deflection, δZ, and 1/r, where r is the corresponding offset of the measured surface deflection (see figure 20).(32)

This graph shows a plot of the inverse of deflection offset versus the measured deflection. The x-axis is 1 divided by r (inverse of deflection offset), with no units or data labels given. The y-axis is measured deflection, with no units or data labels given. The graph depicts an s-shaped curve for the deflection as a function of 1 divided by r. The curve starts at the origin, increases slowly at first, and then increases sharply before leveling off.

©Washington State Department of Transportation

Figure 20. Graph. Inverse of deflection offset versus measured deflection.(31)

The determination of the depth to the stiff layer using the offset of inverse deflection uses the following regression equations (see figure 21 through figure 24) for various HMA layer thicknesses:(32)

The quotient of 1 divided by B, end quotient, equals 0.0362 minus the product of 0.3242 times r subscript 0, end product, plus the product of 10.2717 times r subscript 0 cubed, end product, minus the product of 23.6609 times r subscript 0 superscript 3, end product, minus the product of 0.0037 times BCI, end product.

Figure 21. Equation. Determination of depth to stiff layer, HMA less than 50 mm (2 inches) thick (R2 = 0.98).

The quotient of 1 divided by B, end quotient, equals 0.0065 plus the product of 0.1652 times r subscript 0, end product, plus the product of 5.4290 times r subscript 0 squared, end product, minus the product of 11.0026 times r subscript 0 cubed, end product, minus the product of 0.0004 times BDI, end product.

Figure 22. Equation. Determination of depth to stiff layer, HMA 50 to 100 mm
(2 to 4 inches) thick (R2 = 0.98).

The quotient of 1 divided by B, end quotient, equals 0.0413 plus the product of 0.9929 times r subscript 0, end product, plus the product of 0.0012 times SCI, end product, plus the product of 0.0063 times BDI, minus the product of 0.0778 times BCI, end product.

Figure 23. Equation. Determination of depth to stiff layer, HMA 100 to 150 mm
(4 to 6 inches) thick (R2 = 0.94).

The quotient of 1 divided by B, end quotient, equals 0.0409 plus the product of 0.5669 times r subscript 0, end product, plus the product of 3.0137 times r subscript 0 squared, end product, plus the product of 0.0033 times BDI, minus the product of 0.0665 log BCI, end product.

Figure 24. Equation. Determination of depth to the stiff layer, HMA greater than 150 mm (6 inches) thick (R2 = 0.97).

Where:

B = Depth to rigid layer, measured from pavement surface (ft).
r0 = 1/r intercept (extrapolate steepest section of Dr versus 1/r plot) in units of 1/ft.
BCI = D24 - D36 BCI (i.e., MLI) (mil).
BDI = D12 - D24 BDI (i.e., LLI) (mil).
SCI = D0 - D12 SCI (i.e., BLI) (mil).

Example of Calculating Depth to Stiff Layer(31)

Typical deflection data for an HMA pavement section with an asphalt layer thickness of 194 mm (7.65 inches) are shown in table 14. In addition, soil borings indicate a stiff layer may be present at 5.0 m (198 inches). The corresponding values of 1/r (expressed in terms of 1/ft) are shown in table 15 for each sensor offset.

Table 14. Typical and normalized deflection.(31)
Load Level D0
(μm (mil))
D200
(8 inches)
(μm (mil))
D300
(12 inches)
(μm (mil))
D450
(18 inches)
(μm (mil))
D600
(24 inches)
(μm (mil))
D900
(36 inches)
(μm (mil))
D1500
(60 inches)
(μm (mil))
29.1 kN
(6,534 lbf)
83
(3.28)
68
(2.69)
59
(2.33)
48
(1.88)
40
(1.56)
28
(1.09)
17
(0.68)
42.3 kN
(9,512 lbf)
129
(5.07)
110
(4.32)
93
(3.67)
76
(2.99)
61
(2.40)
43
(1.69)
26
(1.01)
Normalized to 40 kN
(9,000 lbf)
121
(4.76)
103
(4.04)
87
(3.44)
71
(2.80)
57
(2.26)
40
(1.59)
24
(0.95)
Table 15. Values for 1/r values (at 40-kN (9,000-lbf) load level).
Dr (mil) R (inch) 1/r (1/ft)
4.76 0 N/A
4.04 8 1.50
3.44 12 1.00
2.80 18 0.67
2.26 24 0.50
1.59 36 0.33
0.95 60 0.20

N/A = Not applicable.

With this information, the equation in figure 24, repeated here as figure 25, (for HMA thickness > 150 mm (6 inches)) is used to calculate B.

The quotient of 1 divided by B, end quotient, equals 0.0409 plus the product of 0.5669 times r subscript 0, end product, plus the product of 3.0137 times r subscript 0 squared, end product, plus the product of 0.0033 times BDI, minus the product of 0.0665 log BCI, end product.

Figure 25. Equation. Determination of depth to the stiff layer, HMA greater than 150 mm (6 inches) thick (R2 = 0.97).

Where:

r0 = 1/r intercept (refer to figure 26) ≅ 0 (steepest part of deflection basin for deflections at 36 and 60 inches).

This graph shows measured deflection on the vertical scale as a function of 1 divided by r on the horizontal scale, where r is defined as the inverse of the deflection offset. The x-axis, expressed in units of 1 divided by inches, ranges from 0 to 1.5, while the y-axis, expressed in units of mils, ranges from 0 to 6. A general curving trend is observed in which the deflection increases at increasing (1 divided by r) values, as defined from the point of (0,0) to the point (1.5,4). (1 mil = 0.0254 mm.)

©Washington State Department of Transportation
1 mil = 0.0254 mm.
1 inch = 25.4 mm.

Figure 26. Graph. Measured deflection versus 1/r.(31)

Therefore, the depth to the stiff layer in this case is calculated as shown in figure 27.

The quotient of 1 divided by B, end quotient, equals the sum of 0.0409 plus the product of 0.5669 times 0, end product, plus the product of 3.0137 times 0 squared, end product, plus the product of 0.003 times 1.18, minus the product of 0.0665 times 0.67, end product, end sum equals 0.0564. B equals 17.7 ft (5.4 m).

Figure 27. Equation. Sample computation of depth to the stiff layer with HMA greater than 150 mm (6 inches) thick (R2 = 0.97).

Recalling that the soil boring indicated the potential of a stiff layer at 5.0 m (16.5 ft), the estimate for the depth to the stiff layer using the inverse of deflection offset agrees reasonably well. An alternative way to determine the depth to the stiff layer is to use the free vibration response from FWD deflection sensor measurements and one-dimensional wave propagation theory.(33) Chatti, Ji, and Harichandran modified Roesset’s equations to account for different conditions, as shown in figure 28.(34)

(a) D subscript b equals the quotient of the product of V subscript s times T subscript d, end product, divided by 1.35, end quotient. (b) D subscript b equals the quotient of the product of V subscript s times T subscript d, end product, divided by the difference pi minus 2.24 times u, end difference, end quotient.

Figure 28. Equation. Determination of depth to the stiff layer using modified Roesset’s equations.

Where:

Vs = Shear-wave velocity of subgrade = [(Esg/(2(1 − u2))/ρ]0.5.
Esg = Modulus of the subgrade.
ρ = Unit weight of the subgrade.
u = Poisson’s ratio of subgrade.
Td = Natural period of free vibration (see figure 29).

This graph illustrates the natural period, T subscript d, from sensor deflection time histories. The deflections from seven sensors are graphed. The x-axis is time from 0 to 140 ms. The y-axis is deflection from -10 to 30 mils. The sensors show that the natural period occurs between 40 and 80 ms. (1 mil = 0.0254 mm)

©Chatti, K., Ji, Y., Harichandran, R.S., and Hyung, S.L.
1 mil = 0.0254 mm.

Figure 29. Graph. Illustration of natural period, Td, from sensor deflection time histories.(34)

In the backcalculation process, the stiffness of a stiff layer is often fixed at modulus values ranging from 700 to 6,900 MPa (100,000 to 1 million lbf/inch2). When a stiff layer is included, the subgrade must have a specified thickness, and the bedrock/stiff layer is assumed to have an indefinite depth. If a stiff layer is believed to exist, but exact depth data are not available, the depth in the backcalculation process should be varied (e.g., depths of 6, 9, or 15 m (20, 30, or 50 ft)) to determine whether reasonable results can be obtained. Ideally, the depth to the stiff layer should be verified by subsurface borings.

If the layer is due to the presence of a water table (or saturated soil), then a modulus value of about 345 MPa (50,000 lbf/inch2) should be used. If rock or stiff soils (e.g., glacial till) are present, then a modulus value of about 6,900 MPa (1 million lbf/inch2) may be more appropriate.

PCC Pavement Interface Conditions

The ability to account for the interface condition between a PCC slab and the underlying base/subbase layer can have a significant effect on the backcalculated results.(35) This was demonstrated on an evaluation of two LTPP Program General Pavement Studies rigid pavement sections: section 105004, consisting of a 225-mm (8.8-inch) continuously reinforced concrete pavement (CRCP) over a 100-mm (4-inch) cement-aggregate mixture, and section 204052, consisting of a 225-mm (8.8-inch) jointed plain concrete pavement (JPCP) over a 100-mm (4-inch) lean concrete base. Backcalculation scenarios include the following:

The results of the analysis, shown in table 16, indicate that the PCC layer moduli for the no base scenario are unreasonably high for both LTPP Program sections. The full bond assumption produces more reasonable results for section 204052, whereas the no bond scenario provides more reasonable results for section 105004.

Table 16. Effects of interface condition.(35)
LTPP
Program Section
No BaseEPCC
(MPa (lbf/inch2))
No Bond EPCC
(MPa (lbf/inch2))
No Bond EBase
(MPa (lbf/inch2))
Full Bond EPCC
(MPa (lbf/inch2))
Full Bond EBase
(MPa (lbf/inch2))
105004
31,034
(4,501,101)
30,501
(4,423,796)
6,100
(884,730)
20,283
(2,941,800)
4,056
(588,273)
204052
8,203
(1,189,745)
79,569
(11,540,508)
19,892
(2,885,090)
49,871
(7,233,177)
12,468
(1,808,330)

EPCC = PCC layer moduli.
EBase = Base layer moduli.

Stabilized Base Under PCC Pavements

It is difficult to precisely determine the layer modulus of a stabilized base beneath a concrete slab from surface deflection data. Given that the bending stiffness of multiple pavement layers (plates) can be represented by an equivalent plate with an effective thickness (he) and modulus (Ee), it is not possible to resolve the backcalculated effective modulus into component moduli without having additional information on the interface bonding condition and the relative stiffness of the slab and stabilized base (also known as the modular ratio). However, these can be estimated and used iteratively to obtain reasonable estimates of the slab and base modulus values. The two equations in figure 30 can be used to determine the slab modulus value for the unbonded and bonded conditions; the stiffness of the stabilized base, E2, can be found by multiplying the stiffness of the slab by the modular ratio, β.(35)

(a) E subscript 1 equals the product of the quotient of h subscript 1 cubed divided by the sum of h subscript 1 cubed plus Beta times h subscript 2 cubed, end sum, end quotient, times E subscript e, end product. (b) E subscript 1 equals the product of the quotient of h subscript 1 cubed, divided by the sum of h subscript 1 cubed plus Beta times h subscript 2 cubed plus the product of 12h subscript 1 times the difference x minus the quantity h subscript 1 divided by 2, end quotient, end quantity, squared, end product, plus the product of 12 Beta times h subscript 2 times the quantity h subscript 1 minus x plus the quotient of h subscript 2 divided by 2, end quantity, squared, end sum, end quotient, all times E subscript e, end product; where x equals the sum of the quotient of h subscript 1 squared divided by 2 plus the product of h subscript 2 times Beta times the quantity the sum of h subscript 1 plus the quotient of h subscript 2 divided by 2, end quotient, end sum, end quantity, end product, end sum, all divided by the sum of h subscript 1 plus Beta h subscript 2; and where Beta equals the quotient of E subscript 2 divided by E subscript 1.

Figure 30. Equation. Determination of slab modulus values for (a) unbonded and (b) bonded conditions.

Where:

E1 = Modulus of upper plate, i.e., the PCC layer (MPa (lbf/inch2)).
E2 = Modulus of lower plate, i.e., the base layer (MPa (lbf/inch2)).
h1 = Thickness of upper plate, i.e., the PCC slab (mm (inches)).
h2 = Thickness of lower plate, i.e., the base layer (mm (inches)).
β = Modular ratio (see table 17 for selection).

Table 17. Typical modular ratios (β).(28)
Base Type β
HMA, dense graded 0.1000
Asphalt-treated base 0.0200
Lime-treated soil 0.0100
Cement aggregate mixture 0.2000
Lean concrete 0.5000
Econocrete 0.2500
Cement-treated soil 0.0200
Crushed rock 0.0070
Gravel, uncrushed 0.0050
Gravel, crushed 0.0060
Crushed stone 0.0070
Sand 0.0040
Soil-aggregate mixture (fine grained) 0.0025
Soil-aggregate mixture (coarse grained) 0.0040
Soil cement 0.1000

Modeling and Response Issues

The pavement responses to loading can be modeled and interpreted in different ways as part of the backcalculation process. Some of these issues, and how they are often addressed, are described in the following subsections.

Static Versus Dynamic Response

The difference between static response and dynamic response can be defined in terms of the internal forces involved. In a static analysis, only elastic forces are considered, and it is assumed that the peak deflection at each sensor occurs at the same time as the peak load. In actually, viscous and inertial forces are at work in the pavement system, and there is a significant time lag between the peak load and the peak deflection for each sensor. A dynamic analysis tries to capture these time lag effects.

Many engineers argue that backcalculation is an exercise that determines pavement parameters, and not properties, to use within a given mechanistic framework. Therefore, it is acceptable to use static analysis and to backcalculate parameters that are compatible with the current mechanistic-empirical design framework grounded in static and not dynamic analysis. However, dynamic analysis advocates maintain that it takes advantage of more information provided by the test, which allows backcalculating more parameters such as layer thicknesses or the modulus versus frequency curve of the HMA layer. (See references 34 and 36-38.) Also, in certain cases, such as the existence of a stiff layer or water table at shallow depth, the effect of dynamics of pavement response may become more important.

Linear Versus Nonlinear Behavior

When pavement structures are thin enough or the applied loads and corresponding stresses are high enough, fine-grained subgrade materials often exhibit stress-softening, nonlinear behavior (i.e., the subgrade material response increases at a higher rate than the load or stress increases). This means that the subgrade modulus changes with depth and with radial distance from the load. If the modeling approach assumes linear behavior, then only a single modulus value can be assigned to the subgrade, typically an averaged value that matches the measured deflections. For fine-grained materials, the backcalculated subgrade modulus is commonly higher than the laboratory-based measurement by a factor of two to three.

On the other hand, granular (cohesionless) materials used in bases and subbases are stress dependent in a different way, in that their modulus increases with increasing confinement. Similar to the subgrade modulus, this leads to a base/subbase modulus that varies with depth and radial distance from the load, and any linear backcalculation exercise can only lead to an averaged modulus value. The combination of the above phenomena often leads to a base modulus lower than the subgrade modulus even through the base material is of higher quality than the subgrade. Although one way of addressing this problem is to introduce an artificial layer, a more direct way of addressing the problem is to treat the subgrade as a nonlinear elastic material with stress-dependent modulus as shown in figure 31.(39)

E equals the product of C times the quotient of lowercase sigma subscript 1 divided by p, end quotient to the n power, end product.

Figure 31. Equation. Stress-dependent modulus determination.

Where:

E = Modulus value (MPa (lbf/inch2)).
C = Positive constant.
n = Negative constant.
p = Reference stress (atmospheric pressure of 0.1 MPa (14.5 lbf/inch2)).

Ullidtz argues that the effect of the positive non-linearity in granular base/subbase layers is less important to the backcalculation results.(39)

Although finite element modeling (FEM) can be used to evaluate the variation of modulus with depth and radial distance, models based on layered elastic theory can also handle nonlinear behavior (e.g., NELAPAVE and KENPAVE). For example, Ullidtz combines the method of equivalent thickness with a stress-dependent subgrade modulus (see figure 31 equation) to handle material nonlinearity and reports that this approach is superior to FEM.(39)

A number of backcalculation programs, such as BOUSDEF, EVERCALC©, FPEDD1, MODTAG©, and RPEDD1, include a nonlinear analysis component. Others, such as ELMOD®/ELCON, EMOD, ISSEM4, and PADAL, incorporate a nonlinear analysis for the subgrade only.

Temperature and Moisture Effects

Temperature and moisture conditions in the pavement vary over time, both daily and seasonally. A pavement is generally stiffer (stronger) during the winter months because of the frozen state of the underlying materials and is typically at its weakest during the spring thaw period when the foundation materials are saturated.

Several State transportation departments have conducted FWD testing on multiple locations over consecutive seasons to determine the seasonal variation in the unbound layer moduli.(40) Based on the results of the studies, these agencies have developed a range of seasonal factors (see table 18) for adjusting layer moduli for use in a HMA overlay design procedure. In addition, the Enhanced Integrated Climatic Model (EICM), which is incorporated in the MEPDG, provides an analytical tool for predicting temperature, resilient modulus adjustment factors, pore water pressure, water content, frost and thaw depths, frost heave, and drainage performance for a given pavement.(1)

Table 18. Seasonal moduli adjustment factors for unbound materials.(40,41)
State Layer Spring Summer Fall Winter
Idaho Base/subbase 0.65-0.85 1.00 1.00 0.65-1.00
Subgrade 0.43-0.90 1.00 1.00 0.27-11.20
Nevada Base 0.68-0.70 1.00 0.93-0.98 0.87-0.95
Subgrade 0.70-0.79 1.00 0.85-1.02 0.77-0.81
Minnesota Base 0.54-1.20 0.84-1.17 1.00 1.00-35.00
Subgrade 0.73-2.50 0.68-1.10 1.00 13.00-33.00
Washington Base 0.65-0.85 1.00 0.90 0.75-1.10
Subgrade 0.85-0.90 1.00 0.90 0.85-1.10
Indiana Subgrade 0.79-0.87 1.00

—Indicates no data.

Temperature and moisture effects are also critical for PCC pavements because slab curling (caused by temperature gradients) and slab warping (caused by moisture gradients) significantly influence the deflection response of PCC pavements. For example, Khazanovich, Tayabji, and Darter showed backcalculated k-values at one location to be up to three times as high because of temperature gradients.(35) In addition, temperature effects are more critical on backcalculated k-values for thinner slabs compared with thicker slabs.(42) However, it is primarily large temperature fluctuations (temperatures outside of 7 to 32 °C (45 to 90 °F)) that influence the backcalculated slab modulus and k-values.(43)

None of the existing analysis methods directly accounts for the effects of temperature or moisture in the backcalculation process. Therefore, it is recommended that FWD testing be performed when there is no significant temperature gradient present (e.g., when the ambient air temperature is below 27 °C (80 °F)) to avoid the effects of slab curling on the backcalculated results. Note, however, that avoiding the temperature gradient will not address any built-in curling that may be present in the pavement. Crovetti presents a way of differentiating slab curling from poor foundation support using an incremental analysis.(44)

Slab Size Effects

PCC pavement backcalculation procedures based on Westergaard’s solutions assume an infinite plate, but in actuality, pavements have a finite length and width. The following approach can be used to correct for slab size effects on a bare PCC pavement during the backcalculation process:(45)

  1. Compute AREA (units of inches) for the seven-sensor configuration (sensors spaced at
    (0, 203, 305, 457, 610, 914, and 1,524 mm (0, 8, 12, 18, 24, 36, and 60 inches)), as described in chapter 2.
  2. Compute the estimated radius of relative stiffness (est) (units of mm (inches)) for an infinite slab using the equation in figure 32 for the seven-sensor configuration:
Lowercase l subscript est equals the quantity of, the quotient of the log of the quotient of, the difference of 60 minus AREA, end difference, divided by 289.708, end log, divided by negative 0.698, end quotient, end quantity, to the 2.566 power.

Figure 32. Equation. Estimate of radius of relative stiffness for an infinite slab.

  1. Estimate the modulus of subgrade reaction (k-value) for an infinite slab using figure 33.
k equals quotient of the product of P times d subscript 0 superscript asterisk, end product, divided by the product of d subscript 0 times lower l subscript est superscript squared, end product, end quotient.

Figure 33. Equation. Estimate of modulus of subgrade reaction for an infinite slab.

Where:

kest = Modulus of subgrade reaction (MPa/mm (lbf/inch2/inch)).
P = Applied load (N (lbf)).
d0* = Nondimensional deflection coefficient of deflection at center of load plate = 0.1245e superscript minus 14707 e times superscript minus 07565 lowercase l subscript est.
d0 = Measured deflection at radial distance r from the load (mm (inches)).
est = Estimated radius of relative stiffness (mm (inches)).

  1. Calculate finite slab size adjustment factors for the deflection directly under the load plate (AFd0) and radius of relative stiffness (AFℓest) using figure 34 and figure 35 equations.
AF subscript lowercase l subscript est equals 1.89434e superscript negative 0.61662 times the quotient of L divided by lowercase l subscript est, end quotient, to the 1.04831 power, end product.

Figure 34. Equation. Adjustment factor for radius of relative stiffness.

. AF subscript d subscript 0 equals 1 minus 1.15085e superscript negative 0.71878 times the quotient of L divided by lowercase l subscript est, end quotient, to the 0.80151 power, end product.

Figure 35. Equation. Adjustment factor for deflection directly under load plate.

Where:

L = (Ll × Lw) × 0.5 (if the slab length, Ll, is less than or equal to twice the slab width, Lw).
L = 1.414 × Ll (if the slab length, Ll, is greater than twice the slab width, Lw).

  1. Calculate the adjusted k-value that accounts for slab size effects as shown in figure 36):
k equals the quotient of k subscript est divided by the product of the quantity AF subscript l subscript est end quantity squared, times AF subscript d subscript 0, end quotient.

Figure 36. Equation. Adjusted k-value calculation for slab size.

Although the slab size correction procedure is relatively simple and straightforward, it is not always used because of the difficulty in defining the effective length and width of the slab, which are a function of the LTE at the adjacent joints.(35)

Measures of Convergence

In the backcalculation process, the goodness of fit between the calculated deflection basin and the measured deflection basin is referred to as the measure of convergence. The root mean square (RMS) error is one of the more common measures of convergence and can be used to provide a measure of the magnitude of the difference between the calculated and measured deflection basin; it is computed as shown in figure 37.

RMS percentage equals the square root of the product of, the quotient of 1 divided by n subscript d, end quotient, times the summation of the range from n to i equals 1 of the quantity the quotient of the difference d subscript ci minus d subscript mi, end difference, divided by d subscript mi, end quotient, end quantity, squared, end square root, times 100.

Figure 37. Equation. Determination of RMS error.

Where:

nd = Number of deflection sensors used in the backcalculation process.
dci = Calculated pavement surface deflection at sensor i.
dmi = Measured pavement surface deflection at sensor i.

Figure 38 illustrates an example calculation for RMS using the summary of measured and computed deflections provided in table 19.(27)

RMS percentage equals the square root of quotient of 1 divided by 7, end quotient, times the quantity quotient of, the difference 4.90 minus 5.07, end difference divided by 5.07, end quotient, end quantity squared plus the quantity quotient of, the difference 3.94 minus 4.32, end difference, divided by 4.32, end quotient, end quantity, squared, plus ... plus the quantity the quotient of the difference 0.95 minus 1.01, end difference, divided by 1.01, end quotient, end quantity, squared, times 100 equals 6.9 percent.

Figure 38. Equation. Example RMS calculation.

Table 19. Example measured and computed pavement deflection data.
nd Measured deflections
(μm (mil))
Calculated deflections
(μm (mil))
1 129 (5.07) 125 (4.90)
2 109 (4.32) 100 (3.94)
3 93 (3.67) 89 (3.50)
4 75 (2.99) 78 (3.06)
5 61 (2.40) 67 (2.62)
6 43 (1.69) 47 (1.86)
7 26 (1.01) 24 (0.95)

Based on analysis of LTPP Program data, Von Quintus and Killingsworth suggested that an error term of 2 percent or less was considered reasonable.(46,47) The EVERCALC© and MODTAG© user manuals indicate a RMS error of less than 1 percent will result in credible estimates of the layer moduli, whereas layer moduli results with a RMS error greater than 3 percent should be considered questionable.(31,48) Based on these guidelines, the resulting RMS error from the example described in figure 38 and table 19 is considered higher than normally accepted, and therefore resulting layer moduli should be scrutinized.

Modulus Convergence

In addition to the deflection convergence measure, some backcalculation programs also include convergence criteria based on changes in the estimated moduli. If the change in layer moduli between subsequent iterations is less than a user-specified limit, the backcalculation process will terminate. Figure 39 shows the general form of the modulus convergence equation.(27)

Modulus Tolerance is greater than or equal to the quantity, the absolute value of the quotient of the difference E subscript i superscript the quantity k plus 1 end quantity, minus E subscript i superscript k, end difference, divided by E subscript i superscript k, end absolute value, end quantity, times 100.

Figure 39. Equation. Determination of modulus convergence.

Where:

MT = Difference in layer moduli from one iteration (k) to the next (k + 1).
Ei(k) = Specific layer modulus for the i-th layer at the kth iteration.
Ei(k+1) = Specific layer modulus for the i-th layer at the (k + 1)-th iteration.

In general, a modulus convergence of 1 percent is considered acceptable. Large convergence errors suggest that there is a fundamental problem with a specific backcalculation effort. The problem could be within the deflection data (e.g., check that the sensor location in the backcalculation program corresponds to the FWD sensor locations and the precision of the deflection measurement), layer types and thicknesses, or lack of material homogeneity (e.g., cracked and uncracked conditions). Although low convergence errors are desirable, higher convergence errors do not always imply that the backcalculated layer moduli are unreasonable. In this instance, having a good understanding of material properties will greatly assist in balancing the convergence error and reasonable layer moduli.

Identifying Outliers

One of the more challenging aspects of backcalculation is deciding whether the determined layer modulus values are reasonable. Although evaluating the value of the calculated error is helpful, it does not necessarily guarantee that the results are reasonable. Ultimately, being able to assess the reasonableness of the results is based on knowledge of material parameters and behavior and is gained with experience in the backcalculation process. However, the following items are recommended for investigation when evaluating the validity of the backcalculated modulus values:

If investigation of these items does not provide any insight regarding the high error term, the data should be considered an outlier and removed from the analysis.

Other Effects

Several other issues may arise during the backcalculation analysis that can affect the results, including the following:(49)

Verification of Backcalculation Results

There are potentially two ways to verify the reasonableness of backcalculated modulus values. One way is to compare measured strains with calculated strains, and the other way is to compare backcalculated modulus values with laboratory-based values. These are described in the following subsections.

Comparison Based on Strain

A number of studies have compared strains levels induced by an FWD with those of an instrumented HMA pavement. In one study, Winters conducted an evaluation at a test track pavement consisting of a 140-mm (5.5-inch) HMA layer over a 330-mm (13-inch) granular base.(50) HMA cores were instrumented with horizontal and transverse strain gauges and inserted into the existing HMA surface material. An FWD load was applied to induce the strain response (measured by the strain gauges mounted on the cores). The EVERCALC© backcalculation program was then used to determine layer moduli from the measured deflection basins and the corresponding strains.(27) The relative agreement between the measured and calculated strains was fairly good, as indicated in figure 40 and figure 41.

This graph shows measured versus calculated strain for axial core bottom longitudinal gauges. The x-axis is measured microstrains from 0 to 250. The y-axis is calculated microstrains from 0 to 250. This graph shows that the correlation between the measured and calculated strains was fairly good. Data points all fall reasonably close to the line of equality.

©J.P. Mahoney.

Figure 40. Graph. Measured versus calculated strain for axial core bottom longitudinal gauges.(50)

This graph shows measured versus calculated strain for axial core bottom transverse gauges. The x-axis is measured microstrains from 0 to 300. The y-axis is calculated microstrains from 0 to 300. This graph shows that the correlation between the measured and calculated strains was fairly good. Data points all fall reasonably close to the line of equality.

©J.P. Mahoney.

Figure 41. Graph. Measured versus calculated strain for axial core bottom transverse gauges.(50)

In a study conducted by Lenngren, backcalculated layer moduli, determined using a modified version of EVERCALC©, were used to estimate tensile strain at the bottom of the HMA for two in-place pavement sections.(51) In situ tensile strains were measured using strain gauges attached to HMA cores and tested using the FWD. The pavement sections of that study consisted of either 80 or 150 mm (3.1 or 5.9 inches) of HMA over a 550- to 620-mm (22- to 24-inch) gravel and sand base and granular subgrade. The results of the study are shown in figure 42 and figure 43, again showing good agreement between measured and calculated tensile strains.

This graph shows backcalculated versus measured tensile strains-80 mm (3.1 inches) hot-mix asphalt. The x-axis is measured tensile strain from 0 to 350. The y-axis is backcalculated tensile strain from 0 to 350. This graph shows that the correlation between the measured and calculated tensile strains was very good. The data points all fall very close to the line of equality.

©C.A. Lenngren.

Figure 42. Graph. Backcalculated versus measured tensile strains (80-mm (3.1-inch) HMA).(51)

This graph shows backcalculated versus measured tensile strains-150 mm (5.9 inches) hot-mix asphalt. The x-axis is measured tensile strain from 0 to 200. The y-axis is backcalculated tensile strain from 0 to 200. This graph shows that the correlation between the measured and calculated tensile strains was very good. The data points all fall very close to the line of equality.

©C.A. Lenngren.

Figure 43. Graph. Backcalculated versus measured tensile strains (150-mm (5.9-inch) HMA).(51)

In a study conducted by the Minnesota Department of Transportation, in situ strain gauges were monitored during FWD testing and compared with backcalculated strain values from each of several backcalculation programs evaluated (EVERCALC©, WESDEF, and MODCOMP©).(52) The Mn/ROAD analysis concluded that the agreement between the expected and backcalculated strain (figure 44 and figure 45) was good for all programs evaluated, especially for the horizontal strain in the asphalt concrete (AC) layer.

This graph is a comparison of backcalculated (EVERCALC©) and measured asphalt concrete strain. The x axis is measured strain from 0 to 250 microstrains. The y-axis is backcalculated strain from 0 to 300 microstrains. This graph shows that the correlation between the measured and backcalculated strains was fairly good. The data points all fall reasonably close to the line of equality. A regression line relating calculated strain to measured strain is also given.

©D. Van Deusen.

Figure 44. Graph. Comparison of backcalculated (EVERCALC©) and measured AC strain.(52)

This graph is a comparison of backcalculated (WESDEF) and measured asphalt concrete strain. The x axis is measured strain from 0 to 250 microstrains. The y-axis is backcalculated strain from 0 to 300 microstrains. This graph shows that the correlation between the measured and backcalculated strains was fairly good. The data points all fall reasonably close to line of equality. A regression line relating calculated strain to measured strain is also given.

©D. Van Deusen.

Figure 45. Graph. Comparison of backcalculated (WESDEF) and measured AC strain.(52)

Timm and Priest also conducted a study that measured the strain response due to FWD loading and compared it with the layer moduli estimates from the WESLEA pavement analysis program.(53) Conclusions from this analysis determined that the field-measured strain was very similar to the predicted strains using the backcalculated layer moduli (see figure 46).

This graph shows a hot-mix asphalt strain comparison. The x-axis is measured strain from −800 to 400 microstrains. The y-axis is theoretical strain from −800 to 400 microstrains. This graph shows that the correlation between the field-measured and theoretical strains was fairly good. The data points all fall reasonably close to line of equality, indicating that the layer elastic analysis generally gives a reasonable approximation of pavement response under dynamic loadings.

©D.H. Timm.

Figure 46. Graph. HMA strain comparison.(53)

Appea, Flintsch, and Al-Qadi compared pavement responses (from in situ pressure cells and strain gauges) from the Virginia Smart Road with backcalculated layer moduli from measured FWD deflections.(54) Conclusions from this study indicate that, in general, the calculated stresses were comparable to the measured stresses.(54)

Laboratory Versus Backcalculated Moduli

There have been a number of attempts to relate laboratory-based modulus values to those determined from backcalculation, but such comparisons can be problematic for a number of reasons, including the following:(27)

In a study of LTPP Program rigid pavement sections, the backcalculated slab modulus values did not correlate well with the static chord modulus measured in the laboratory under ASTM C469, “Standard Test Method for Static Modulus of Elasticity and Poisson’s Ratio of Concrete in Compression.”(35,55) The backcalculated modulus values were substantially higher than the measured static values, part of which was attributed to curling/warping of the slab and also differences in the loading condition.

A number of studies have been conducted to compare backcalculated and laboratory-determined HMA layer moduli. In a study conducted by Zhou, it was determined that backcalculated HMA layer moduli were generally 20 to 30 percent lower than laboratory-measured moduli (tested at the same temperature).(56) More recently, Kim, Ji, and Siddiki noted that on average, the modulus determined from FWD testing was approximately two times higher than the laboratory-determined modulus.(57) A study by Dawson et al. found a reasonable relationship (see table 20) between laboratory and backcalculated modulus values for the following Unified Soil Classification System (USCS) soil types: gravelly sand (SP1, and SP2), poorly graded sand - silty sand (SP-SM), and clayey sand - silty sand (SC-SM), while noting that differences existed with finer grained soils types.(58) In a study on the effects of reflective cracking, researchers found a reasonable match between backcalculated modulus values and laboratory-based values.(59)

Table 20. Backcalculated versus laboratory-obtained subgrade moduli and recommended values for use in the MEPDG.(58)
USCS AASHTO
Soil Type(60)
Laboratory Backcalculation MEPDG Recommendations(1)
No. of
Tests
Average MR
(MPa (lbf/inch2))
No. of
Tests
Average MR
(MPa (lbf/inch2))
Range
(MPa (lbf/inch2))
Typical
(MPa (lbf/inch2))
SP1 A-1-a
A-3
16 199.5
(28,942)
1,241 179.8
(26,073)
169-290
(24,500-42,000)
228
(33,000)
SP2 A-1-b
A-3
10 177.1
(25,685)
542 173.6
(25,178)
169-276
(24,500-40,000)
221
(32,000)
SP-SM A-1-b
A-2-4
A-3
8 145.8
(21,147)
383 143.1
(20,760)
169-259
(24,500-37,500)
214
(31,000)
SC-SM A-2-4
A-4
7 160.4
(23,258)
1,829 140.7(20,402) 148-259
(21,500-37,500)
200
(29,000)
SM A-2-4
A-4
17 117.4
(17,028)
182 176.4
(25,583)
148-259
(21,500-37,500)
200
(29,000)
SC A-2-6
A-6
A-7-6
16 129.3
(18,756)
1,450 158.9
(23,052)
93-214
(13,500-31,000)
152
(22,000)
CL A-4
A-6
A-7-6
9 256.7
(37,225)
99 156.8
(22,746)
34-200
(5,000-29,000)
117
(17,000)
ML A-4 4 169.5
(24,578)
23 110.2
(15,976)
117-200
(17,000-29,000)
159
(23,000)

SM = Silty sand.
SC = Low plasticity clay.
ML = Low plasticity silt.

Van Deusen, Lenngren, and Newcomb compared laboratory to backcalculated layer moduli for subgrade soils at the Mn/ROAD facility.(61) This study suggested that the laboratory samples and backcalculated layer moduli compared well, within the encountered variability.(61) Finally, a study conducted by Houston, Mamlouk, and Perera went a step farther by adding an assessment of quality related to laboratory testing costs.(62) That study concluded the following:(62)

The intent of this discussion is not to resolve the conflict between laboratory-determined and backcalculated layer moduli. Instead, the intent is to demonstrate potential issues with laboratory test results from field samples (cores of bound materials and remolded unbound materials) and to provide results of a few studies that have compared laboratory and backcalculated layer moduli. The issue of laboratory-based versus backcalculated modulus values commonly comes up in HMA overlay design with regard to whether the backcalculated layer moduli should be “corrected” to laboratory conditions. Although most HMA overlay design procedures rely on the conversion of backcalculated values to those based on laboratory conditions, an understanding of the principles and processes of both laboratory testing and backcalculation are essential for determining appropriate input values. Ultimately, the need for a correction should be based on the experience of the design engineer in concert with knowledge of the local materials and climatic conditions.

Backcalculation Example

This section provides an example of the backcalculation process using actual field data (coring, pavement condition assessment, and FWD testing results) from the Washington State Department of Transportation.(31)

Project Description

FWD testing was performed on a section of State Route 395 near Chewelah, WA, located in the northeast corner of the State. The pavement at the time of FWD testing (performed in mid-April) exhibited 5 to 15 percent of low- to medium-severity alligator cracking and 30 percent medium- to high-severity longitudinal cracking.

The subgrade was very deep and moderately well drained and classified as a silty loam (i.e., ML). From February to April, a perched water table was present and located at a depth of 600 to 900 mm (24 to 35 inches) beneath the surface. The base material consisted of a silty sandy gravel or sandy gravel and varied in thickness from 300 to 450 mm (12 to 18 inches). The wearing surface was composed of multiple layers of HMA and chip seal overlays with a total thickness ranging from 100 to 300 mm (3.9 to 11.8 inches). Table 21 presents a summary of the pavement cross section information based on cores taken at various points throughout the project.

Table 21. Summary of pavement cross section information.
Core
MP Location
Thickness HMA
(mm (inches))
Thickness Base
(mm (inches))
Comments
207.85
135 (5.3) 457 (18.0) Core taken at a crack; crack was full depth
208.00
152 (6.0) 457 (18.0) Core taken at a crack; core not intact
208.50
119 (4.7) 305 (12.0) Core taken at a crack; crack was full depth
209.00
117 (4.6) 305 (12.0) Very fatigued; core broke into several pieces
209.05
107 (4.2) 305 (12.0) Fatigued area; crack was full depth
209.40
150 (5.9) 335 (13.2) Core taken at a crack; crack was full depth
209.80
165 (6.5) 396 (15.6) HMA core intact
210.00
112 (4.4) 366 (14.4) Fatigue in both wheel paths; crack was full depth
210.50
249 (9.8) 366 (14.4) Core taken at a crack; crack was full depth
211.00
229 (9.0) 366 (14.4) Core broke into several pieces
211.50
282 (11.1) 366 (14.4) HMA core intact
212.00
300 (11.8) 366 (14.4) HMA core intact
212.50
229 (9.0) 366 (14.4) Top 183 mm (7.2 inches) in good condition

Because of the presence of the perched water table, there was the potential for a stiff layer to be encountered as part of the backcalculation process. Therefore, the following three backcalculation approaches were considered:

Input Values

The number of layers to be modeled for this problem ranged from three (if a stiff layer did not exist) to four (if a stiff layer existed). Table 22 summarizes the layer information and initial assumptions/ranges for modulus values. The FWD testing employed a six-sensor configuration with sensor spacings of 0, 203, 305, 610, 914, and 1219 mm (0, 8, 12, 24, 36, and 48 inches). FWD data were normalized to a standard loading of 40 kN (9,000 lbf), with the resultant normalized deflection data presented in table 23. The pavement temperature at the time of FWD testing was between 8 and 10 °C (46 and 50 °F).

Table 22. Input values to represent pavement layers.
Layer Description Poisson’s Ratio Modulus (MPa (lbf/inch2))
Initial Minimum Maximum
1
HMA 0.35 2,700
(400,000)
690
(100,000)
13,800
(2 million)
2
Base 0.40 170
(25,000)
35
(5,000)
3,500
(500,000)
3
Subgrade 0.45 100
(15,000)
35
(5,000)
3,500
(500,000)
4a
Stiff layer (water) 0.35 345
(50,000)
4a
Stiff layer (rock) 0.30 6,900
(1 million)

aDenotes the use of a stiff layer.
—Indicates not applicable.

Backcalculation Results

The EVERCALC© program was used in the backcalculation analysis of the FWD data collected for this project. It is briefly described in this subsection along with a presentation and discussion of the overall results.

EVERCALC©

EVERCALC© uses the Levenberg-Marquardt minimization algorithm that seeks to minimize an objective function formed as the sum of squared relative differences between the calculated and measured surface deflections.(63) EVERCALC© employs the WESLEA computer program for forward calculations; has the option for including stress sensitivity of unstabilized materials and stresses and strains at various depths; and optionally normalizes HMA modulus to a standard temperature. The program uses an iterative approach in changing the moduli to match theoretical and measured deflections and was specifically developed to backcalculate layer moduli of flexible pavements.

Discussion of Results

The backcalculation results obtained from the EVERCALC© program are shown in table 24. The Eadj columns are the backcalculated HMA modulus values adjusted to a standard temperature of 25 °C (77 °F), while the EHMA columns are the backcalculated HMA modulus values at the actual field testing temperatures.

Table 23. FWD deflections and normalized deflection to 40 kN (9,000 lbf).
MP Location Load
(kN (lbf))
D0
(μm (mil))
D200 mm (8 in)
(μm (mil))
D305 mm (12 in)
(μm (mil))
D610 mm (24 in)
(μm (mil))
D915 mm (36 in)
(μm (mil))
D1220 mm (48 in)
(μm (mil))
207.85 75 (16,940) 795 (31.30) 665 (26.18) 589 (23.19) 350 (13.78) 231 (9.09) 169 (6.65)
54 (12,086) 615 (24.21) 516 (20.31) 460 (18.11) 263 (10.35) 173 (6.81) 126 (4.96)
42 (9,421) 494 (19.45) 416 (16.38) 370 (14.57) 206 (8.11) 134 (5.28) 101 (3.98)
28 (6,218) 335 (13.19) 286 (11.26) 252 (9.92) 130 (5.12) 86 (3.39) 72 (2.83)
Normalized Deflection 467 (18.39) 394 (15.51) 350 (13.78) 193 (7.60) 127 (5.00) 97 (3.82)
208.00 76 (16,987) 687 (27.04) 547 (21.53) 472 (18.58) 286 (11.26) 186 (7.32) 134 (5.28)
54 (12,070) 540 (21.26) 431 (16.97) 371 (14.61) 220 (8.66) 141 (5.55) 101 (3.98)
42 (9,405) 445 (17.52) 354 (13.94) 304 (11.97) 178 (7.01) 113 (4.45) 82 (3.23)
28 (6,186) 313 (12.32) 248 (9.76) 211 (8.31) 118 (4.65) 73 (2.87) 52 (2.05)
Normalized Deflection 421 (16.57) 336 (13.23) 288 (11.34) 167 (6.57) 106 (4.17) 76 (2.99)
208.50 75 (16,829) 379 (14.92) 302 (11.89) 260 (10.23) 150 (5.91) 81 (3.19) 58 (2.28)
54 (12,245) 296 (11.65) 236 (9.29) 202 (7.95) 114 (4.49) 54 (2.13) 44 (1.73)
42 (9,533) 244 (9.61) 194 (7.63) 166 (6.53) 92 (3.62) 46 (1.81) 33 (1.30)
28 (6,297) 171 (6.73) 136 (5.35) 114 (4.49) 61 (2.40) 32 (1.26) 22 (0.87)
Normalized Deflection 229 (9.01) 182 (7.17) 155 (6.10) 86 (3.39) 43 (1.69) 32 (1.26)
209.00 73 (16,305) 1,505 (59.25) 1,234 (48.58) 1,080 (42.52) 541 (21.30) 242 (9.53) 130 (5.12)
52 (11,737) 1,172 (46.14) 953 (37.52) 827 (32.56) 396 (15.59) 170 (6.69) 91 (3.58)
41 (9,247) 938 (36.93) 757 (29.8) 651 (25.63) 299 (11.77) 126 (4.96) 68 (2.68)
27 (6,154) 635 (25.00) 505 (19.88) 426 (16.77) 185 (7.28) 77 (3.03) 44 (1.73)
Normalized Deflection 902 (35.51) 728 (28.66) 625 (24.61) 290 (11.42) 123 (4.84) 67 (2.64)
209.05 71 (15,972) 1,426 (56.14) 1,140 (44.88) 969 (38.15) 556 (21.89) 344 (13.54) 236 (9.29)
51 (11,531) 1,118 (44.02) 894 (35.20) 751 (29.57) 415 (16.34) 254 (10.00) 174 (6.85)
40 (9,088) 905 (35.63) 718 (28.27) 597 (23.50) 321 (12.64) 191 (7.52) 128 (5.04)
27 (5,995) 644 (25.35) 488 (19.21) 392 (15.43) 190 (7.48) 118 (4.65) 710 (2.80)
Normalized Deflection 893 (35.16) 702 (27.64) 581 (22.87) 311 (12.24) 189 (7.44) 125 (4.92)
209.40 71 (16,004) 1,597 (62.87) 1,316 (51.81) 1,106 (43.54) 631 (24.84) 377 (14.84) 244 (9.61)
52 (11,610) 1,268 (49.92) 1,044 (41.10) 871 (34.29) 491 (19.33) 293 (11.54) 189 (7.44)
40 (9,104) 1,020 (40.16) 846 (33.31) 696 (27.40) 382 (15.04) 227 (8.94) 145 (5.71)
30 (6,733) 725 (28.54) 581 (22.87) 466 (18.35) 241 (9.49) 145 (5.71) 94 (3.70)
Normalized Deflection 1,002 (39.45) 821 (32.32) 675 (26.57) 369 (14.53) 220 (8.66) 142 (5.59)
209.80 77 (17,257) 677 (26.65) 548 (21.57) 475 (18.70) 286 (11.26) 182 (7.17) 126 (4.96)
54 (12,229) 528 (20.79) 429 (16.89) 371 (14.61) 220 (8.66) 137 (5.39) 94 (3.70)
42 (9,533) 426 (16.77) 347 (13.66) 298 (11.73) 171 (6.73) 107 (4.21) 72 (2.83)
28 (6,265) 298 (11.73) 240 (9.45) 203 (7.99) 111 (4.37) 69 (2.72) 44 (1.73)
Normalized Deflection 402 (15.83) 326 (12.83) 280 (11.02) 160 (6.30) 100 (3.94) 67 (2.64)
210.00 74 (16,718) 914 (35.98) 742 (29.21) 639 (25.16) 426 (16.77) 285 (11.22) 197 (7.76)
53 (12,023) 706 (27.80) 650 (25.60) 490 (19.29) 323 (12.72) 213 (8.39) 145 (5.71)
42 (9,422) 567 (22.32) 457 (17.99) 388 (15.28) 250 (9.84) 162 (6.38) 111 (4.37)
27 (6,170) 385 (15.16) 307 (12.09) 256 (10.08) 160 (6.30) 101 (3.98) 70 (2.76)
Normalized Deflection 538 (21.18) 434 (17.09) 367 (14.45) 236 (9.29) 154 (6.06) 105 (4.13)
210.50 76 (17,162) 568 (22.36) 488 (19.21) 423 (16.65) 265 (10.43) 175 (6.89) 120 (4.72)
54 (12,213) 441 (17.36) 380 (14.96) 329 (12.95) 201 (7.91) 128 (5.04) 89 (3.50)
42 (9,437) 355 (13.98) 306 (12.05) 264 (10.39) 159 (6.26) 100 (3.94) 68 (2.68)
27 (6,170) 244 (9.61) 210 (8.27) 179 (7.05) 104 (4.09) 63 (2.48) 42 (1.65)
Normalized Deflection 336 (13.22) 289 (11.38) 249 (9.80) 149 (5.87) 93 (3.66) 64 (2.52)
211.00 76 (17,178) 344 (13.54) 300 (11.81) 278 (10.94) 204 (8.03) 154 (6.06) 116 (4.57)
55 (12,324) 264 (10.39) 226 (8.90) 209 (8.23) 155 (6.10) 116 (4.57) 85 (3.35)
43 (9,628) 203 (7.99) 181 (7.13) 166 (6.54) 122 (4.80) 90 (3.54) 66 (2.60)
28 (6,392) 144 (5.67) 121 (4.76) 109 (4.29) 80 (3.15) 58 (2.28) 43 (1.69)
Normalized Deflection 194 (7.64) 168 (6.61) 153 (6.02) 113 (4.45) 83 (3.27) 61 (2.40)
211.50 78 (17,463) 320 (12.60) 266 (10.47) 239 (9.41) 169 (6.65) 119 (4.69) 82 (3.23)
56 (12,626) 234 (9.21) 195 (7. 68) 175 (6.89) 123 (4.84) 87 (3.42) 59 (2.32)
44 (9,881) 179 (7.05) 150 (5.91) 134 (5.28) 93 (3.66) 65 (2.56) 44 (1.73)
29 (6,487) 113 (4.45) 94 (3.70) 83 (3.27) 57 (2.24) 40 (1.57) 27 (1.06)
Normalized Deflection 162 (6.38) 135 (5.31) 121 (4.76) 84 (3.31) 59 (2.32) 40 (1.57)
212.00 79 (17,717) 570 (22.44) 519 (20.43) 483 (19.01) 362 (14.25) 269 (10.59) 199 (7.83)
56 (12,626) 431 (16.97) 392 (15.43) 364 (14.33) 272 (10.71) 201 (7.91) 149 (5.87)
45 (10,024) 340 (13.39) 310 (12.20) 187 (7.36) 215 (8.46) 158 (6.22) 118 (4.65)
29 (6,582) 218 (8.59) 204 (8.03) 188 (7.40) 139 (5.47) 103 (4.06) 76 (2.99)
Normalized Deflection 306 (12.04) 278 (10.94) 257 (10.11) 192 (7.56) 142 (5.59) 105 (4.13)
212.5 81 (18,193) 495 (19.49) 441 (17.36) 407 (16.02) 316 (12.44) 242 (9.53) 177 (6.97)
58 (12,927) 382 (15.04) 337 (13.27) 310 (12.20) 241 (9.49) 183 (7.20) 135 (5.31)
46 (10,294) 296 (11.65) 267 (10.51) 244 (9.61) 191 (7.52) 144 (5.67) 102 (4.02)
30 (6,789) 206 (8.11) 178 (7.01) 161 (6.34) 125 (4.92) 93 (3.66) 64 (2.52)
Normalized Deflection 266 (10.47) 235 (9.26) 214 (8.42) 167 (6.57) 125 (4.92) 89 (3.50)
Table 24. Summary of EVERCALC© backcalculation results.
FWD/
Core
MP Location
No Stiff Layer Depth
to Stiff
Layer
(m (inches))
Stiff Layer at 345 MPa (50 ksi) Stiff Layer at 6,900 MPa (1,000 ksi)
Eadj
(MPa(ksi))
Ehma
(MPa(ksi))
Ebase
(MPa(ksi))
Esub
(MPa(ksi))
RMS Eadj
(MPa(ksi))
Ehma
(MPa(ksi))
Ebase
(MPa(ksi))
Esub (MPa(ksi)) RMS Eadj
(MPa(ksi))
Ehma
(MPa(ksi))
Ebase
(MPa(ksi))
Esub
(MPa(ksi))
RMS
207.85 1,138
(165)
3,640
(528)
117
(17)
83
(12)
3.09 4.95
(195)
981
(142)
3,137
(455)
152
(22)
69
(10)
4.12 931
(135)
2,972
(431)
165
(24)
62
(9)
4.53
208.00 903
(131)
2,882
(418)
124
(18)
103
(15)
0.70 4.04
(159)
738
(107)
2,351
(341)
165
(24)
83
(12)
1.80 676
(98)
2,165
(314)
193
(28)
69
(10)
2.52
208.50 3,654
(530)
1,703
(247)
117
(17)
248
(36)
3.39 1.55
(61)
2,537
(368)
8,115
(1,177)
296
(43)
152
(22)
5.37 1,400
(203)
4,482
(650)
758
(110)
34
(9)
10.73
209.00 607
(88)
1,951
(283)
34
(5)
90
(13)
13.40 1.19
(47)
1,733
(251)
5,550
(805)
117
(17)
34
(5)
24.56 2,530
(367)
8,418
(1,221)
34
(5)
34
(5)
41.88
209.05 1,165
(169)
3737
(542)
41
(6)
62
(9)
2.04 2.49
(98)
621
(90)
1,979
(287)
131
(19)
34
(5)
5.29 1,276
(185)
4,082
(592)
83
(12)
34
(5)
10.12
209.40 414
(60)
1,331
(193)
34
(5)
55
(8)
2.00 2.16
(85)
648
(94)
2,068
(300)
34
(5)
34
(5)
14.39 655
(95)
2,089
(303)
34
(5)
34
(5)
21.76
209.80 979
(142)
3,123
(453)
83
(12)
117
(17)
0.96 3.61
(142)
779
(113)
2,503
(363)
145
(21)
90
(13)
1.60 689
(100)
2,213
(321)
179
(26)
76
(11)
2.41
210.00 2,048
(297)
6,557
(951)
97
(14)
69
(10)
2.29 3.23
(127)
1,138
(165)
3,640
(528)
200
(29)
48
(7)
0.83 1,000
(145)
3,199
(464)
228
(33)
41
(6)
0.99
210.50 4,868
(706)
17,037
(2,471)
117
(17)
117
(17)
0.64 8.64
(340)
4,406
(639)
15,417
(2,236)
145
(21)
117
(17)
0.76 4,151
(602)
14,534
(2,108)
165
(24)
110
(16)
0.85
211.00 1,882
(273)
6,578
(954)
145
(21)
138
(20)
0.76 5.69
(224)
1,903
(276)
6,660
(966)
193
(28)
124
(18)
0.63 1,793
(260)
6,288
(912)
262
(38)
103
(15)
0.68
211.50 1,317
(191)
4,606
(668)
83
(12)
255
(37)
0.66 3.05
(120)
1269
(184)
4,447
(645)
124
(18)
207
(30)
0.67 1,158
(168)
4,054
(588)
269
(39)
110
(16)
1.13
212.00 827
(120)
2,889
(419)
34
(5)
97
(14)
2.08 7.98
(314)
876
(127)
3,061
(444)
34
(5)
90
(13)
1.88 896
(130)
3,130
(454)
34
(5)
83
(12)
1.86
212.50 1,965
(285)
6,888
(999)
34
(5)
124
(18)
1.23 5.13
(202)
1,924
(279)
1,924
(279)
69
(10)
90
(13)
0.97 1,834
(266)
6,426
(932)
103
(15)
76
(11)
0.86

No Stiff Layer Scenario

In general, the adjusted HMA modulus values appear to be reasonable (within the expected moduli range for a fatigued HMA) for this aged and distressed HMA pavement. At MP location 210.50, the resulting adjusted HMA moduli was very high considering that the HMA was cracked full depth at this location. Reviewing the results for the base layer, it is noted that for the most part, the base layer moduli were higher than those determined for the subgrade, which was an expected outcome (although it may occasionally be possible for the backcalculated subgrade moduli to be equal to or slightly higher than the backcalculated base moduli). The backcalculated moduli of 35 MPa (5,000 lbf/inch2) for the base and subgrade moduli was the minimum value specified in the EVERCALC© program, which was the result at several locations for the base layer. The RMS error for more than half of the locations (54 percent) was below the recommended 2-percent threshold.

Stiff Layer at 345 MPa (50,000 lbf/inch2)

In this scenario (in which a stiff layer was assumed with a fixed modulus of 345 MPa (50,000 lbf/inch2)), the HMA modulus still appears reasonable and the base layer modulus, for the most part, increased slightly to more reasonable values. The subgrade modulus was lowered a bit from the first scenario but is still in the reasonable range for this soil type. In this scenario, 62 percent (or one more location than the first scenario) of the backcalculated moduli resulted in an RMS error below 2 percent.

Stiff Layer at 6,900 MPa (1 million lbf/inch2)

This scenario assumed a stiff layer with a fixed modulus of 6,900 MPa (1 million lbf/inch2). This analysis produces generally reasonable HMA modulus values and yields base layer moduli within the expected range for about half of the locations; it also produces slightly lower subgrade moduli but ones that are still within the range of expected values. Under this scenario, fewer than half (approximately 46 percent) of the locations had a resulting RMS error below 2 percent.

Selection of Moduli

Of the 13 locations evaluated, only 1 location, MP 209.00, consistently resulted in a very high RMS error under all three scenarios. Consequently, that point was considered an outlier and should not be considered as representative of the typical conditions. Several other locations produced RMS errors above the 2 percent criterion, but in most of those cases, one of the two stiff layer scenarios produced reasonable values. Ultimately, it is up to the engineer to decide which set of backcalculated modulus values is the most reasonable for each location, based on experience and knowledge of the in situ conditions. In general, the backcalculated moduli using a stiff layer at 345 MPa (50,000 lbf/inch2) appears to have the most locations in the range of expected values for this roadway section. Based on the information provided in this example, table 25 summarizes recommended moduli and provides a brief discussion on the reasoning behind the selection of the particular layer moduli results.

Table 25. Summary of selected layer moduli.
MP Location EHMA
MPa
(lbf/inch2)
EBase
MPa
(lbf/inch2)
ESub
MPa
(lbf/inch2)
RMS Scenario1 Discussion
207.85 981
(142,000)
152
(22,000)
69
(10,000)
4.12 1 High RMS. Results in realistic base moduli. Stiff layer at 6,900 MPa (1 million lbf/inch2) would also be appropriate, but higher RMS.
208.00 738
(107,000)
165
(24,000)
83
(12,000)
1.80 1 Realistic layer moduli. No stiff layer results in base moduli a bit low for this roadway section. High stiff layer case results in higher RMS.
208.50 2,537
(368,000)
296
(43,000)
152
(22,000)
5.37 1 High RMS. No stiff layer results in too low base moduli though lower RMS. High stiff layer case results in too high base moduli.
209.00 Unreasonable layer moduli and RMS considerably higher than 2 percent. Results not recommended for use.
209.05 621
(90,000)
131
(19,000)
34
(5,000)
5.29 1 High RMS; layer moduli look reasonable. No stiff layer results in low base moduli. High stiff layer results in high RMS.
209.40 No stiff layer has good RMS, but layer moduli all too low. Results not recommended for use.
209.80 779
(113,000)
145
(21,000)
90
(13,000)
1.60 1 No stiff layer and stiff layer result in reasonable RMS. Stiff layer has more reasonable base layer moduli.
210.00 1,138
(165,000)
200
(29,000)
48
(7,000)
0.83 1 Stiff and high stiff layer result in reasonable RMS. Either could be used, stiff layer selected because of lower RMS.
210.50 4,151
(602,000)
165
(24,000)
110
(116,000)
0.85 2 All scenarios result in low RMS. High stiff layer results in more reasonable base moduli for this roadway section.
211.00 1,903
(276,000)
193
(28,000)
124
(18,000)
0.63 1 All scenarios result in low RMS. High stiff layer results in higher base moduli than expected for this roadway section.
211.50 1,158
(168,000)
269
(39,000)
110
(16,000)
1.13 2 All scenarios result in low RMS. No stiff layer and stiff layer result in too low base moduli for this roadway section.
212.00 896
(130,000)
34
(5,000)
83
(12,000)
1.86 2 Stiff and high stiff scenarios result in low RMS. All scenarios result in too low base moduli.
212.50 1,834
(266,000)
103
(15,000)
76
(11,000)
0.86 2 All scenarios result in low RMS. High stiff layer results in more reasonable base moduli for this roadway section.

1Scenario 1 = Stiff layer at 345 MPa (50,000 lbf/inch2)—stiff layer. Scenario 2 = Stiff layer at 6,900 MPa
(1 million lbf/inch2)—high stiff layer.
—Indicates results not recommended for use.

Summary

This chapter provides an overview of the backcalculation process and recommended guidelines for backcalculation of flexible, rigid, and composite pavements. General backcalculation recommendations are summarized as follows:

In addition, table 26 provides a summary of guidance for dealing with a number of specific issues in the backcalculation of flexible, rigid, and composite pavement systems.

Table 26. Addressing specific conditions in pavement backcalculation analysis.
Pavement Type Situation Issue(s) Recommendation(s)
Flexible Multiple bituminous lifts/layers
  • Many backcalculation programs limit the total number of layers to five (including a stiff layer).
  • Typically, backcalculation programs are insensitive to differentiating moduli values between adjacent similar stiffness bituminous layers.
  • Combine adjacent bituminous lifts/layers.
  • If total thickness is less than 75 mm (3 inches), assume a fixed modulus for the combined layer.
More than five structural layers
  • Many backcalculation programs limit the total number of layers to five (including a stiff layer).
  • As the number of layers increases, the error level may increase and result in an unreasonable solution.
  • Combine adjacent layers of similar materials or stiffness (e.g., bituminous layers, granular base and subbase).
  • Ideally, no more than four layers (surfacing, base, subgrade, and stiff layer, when applicable) should be modeled.
Thin surfacing layers (< 75 mm (3 inches))
  • Thin bituminous layers have minimal influence on the surface deflection.
  • Unreasonable moduli for the thin bituminous layer may result.
  • A high error level may result.
  • Combine thin surface layer with adjacent bituminous layer(s).
  • Assume a fixed modulus for the bituminous layer.
Highly distressed surface (e.g., alligator cracking, stripping)
  • Highly distressed pavements violate the layered-elastic theory of homogeneity.
  • Deflection basin may not produce the smooth basin predicted by layered-elastic theory.
  • Assume a fixed layer modulus for the bituminous layer.
  • Consider using only the backcalculated results for the unbound layer moduli.
  • Remove data points from analysis (condition should be well documented during testing).
Bonding condition Significant debonding/ delamination of adjacent bituminous lifts/layers can result in unreasonable modulus values and higher error levels.
  • Confirm bond condition (coring) where delamination may be an issue.
  • Assume a fixed layer modulus for the bituminous layer.
Elevated testing temperatures
  • Bituminous layers are very sensitive to changes in temperature.
  • On extremely hot days, the bituminous layer will have a significantly lower modulus.
  • Increased error levels may result.
  • Do not conduct deflection testing when pavement temperatures are above 32 °C (90 °F).
  • Apply temperature correction factor for bituminous layer.
  • Assume a fixed layer modulus for the bituminous layer.
Saturated soils In the backcalculation process, saturated soils can have a similar affect as a stiff layer. If a saturated layer is known to exist, consider evaluating this layer as a stiff layer (see comments for a stiff layer).
Frozen subgrade See discussion on presence of rigid layer.
  • Conduct deflection testing during unfrozen conditions.
  • Include use of seasonal moduli in pavement design process.
Non-decreasing layer stiffness with depth
  • Some backcalculation programs include a built-in assumption that layer moduli decrease with depth.
  • Deflection of lower stiffness layer has minimal influence on deflection.
  • Unreasonable moduli for the layer above the stiffer layer may result.
  • Confirm backcalculation program assumptions.
  • Review results for reasonable moduli and RMS values.
  • Assume a fixed modulus for the bituminous layer.
Compacted subgrade layers (sub-layering subgrade)
  • Treated materials often have higher moduli than the underlying subgrade.
  • If unaccounted for, these layers can result in unreasonable layer moduli and higher error levels.
For treated materials (e.g., lime- or cement-stabilized subgrade), consider as a base/subbase layer; may need to combine with base/subbase course if results in more than three layers to analyze.
Presence of stiff layer (e.g., bedrock, saturated layer, water table) Stiff layers located at a shallow depth (< 12 m (40 ft)) may result in unreasonable backcalculated moduli in the upper layers and higher error levels.
  • When possible, confirm location of bedrock, stiff layer, or shallow water table (borings, soil surveys).
  • Run multiple backcalculation analyses that include stiff layer at varying depths and stiffnesses.
Rigid Cement-treated or lean concrete base
  • A bonding condition between base and slab affects backcalculated modulus.
  • AREA-based methods compute effective modulus of bound (stiffer) layers, and a layer ratio is used to determine individual layer moduli.
  • Review results for reasonable moduli.
  • Conduct investigation to determine bonding conditions.
  • Conduct materials testing to validate assumed layer ratio.
Presence of stiff layer (e.g., bedrock, saturated layer, water table) A composite k-value is determined, which includes the influence of any stiff layer, if present. Ensure the use of a compatible model in the design method.
Elevated testing temperatures
  • Curling of the slab may increase variability of backcalculated values.
  • Joint LTE values may be artificially high.
Conduct deflection testing when ambient air temperature is below 30 °C (85 °F).
Small PCC slab sizes Joint (or crack) discontinuity near the applied load influences results.
  • Review results for reasonable moduli.
  • Assess impact of the use of slab size adjustments on the reasonableness of moduli.
More than two structural layers Procedure is limited to two structural layers and subgrade. Combine adjacent layers of similar materials or stiffness.
Thin stabilized layer beneath PCC surface
  • Thin layer has a minimal influence on the surface deflection.
  • Unreasonable moduli for the thin stabilized layer may result.
  • A high error level may result.
  • Review results for reasonable moduli.
  • Neglect the moduli of this layer and add thickness to the underlying layer.
Composite More than two structural layers Procedure is limited to two structural layers and subgrade. Combine adjacent layers of similar materials or stiffness.
Bonding condition Significant debonding/ delamination between HMA surface and underlying PCC pavement can result in unreasonable modulus values and higher error levels.
  • Confirm bond condition (coring) where debonding may be an issue.
  • Model using appropriate bonding condition.
  • Convert to equivalent thickness of PCC assuming layers are unbonded.
Small PCC slab size (e.g., thin whitetopping) Joint (or crack) discontinuity near the applied load influences results.
  • Review results for reasonable moduli.
  • Assess impact of the use of slab size adjustments on reasonableness of moduli.
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Turner-Fairbank Highway Research Center | 6300 Georgetown Pike | McLean, VA | 22101