Page 1 of 4
European Journal of Business &
Social Sciences
Available at https://ejbss.org/
ISSN: 2235-767X
Volume 07 Issue 05
May 2019
Available online: https://ejbss.org/ P a g e | 971
Effect of Thickness of a Sandwiched Layer of Bitumen
Between Two Aggregate on the Bond Strength
N. Ezhilarasi, PG Student
Dept. of Civil Engineering
PRIST University
Thanjavur, India
Abstract—The research was also to evaluate tack coat
materials and application rates for the Alabama Department of
Transportation (ALDOT). The project included a laboratory
phase and a field phase. For the laboratory work, the experiment
included two types of emulsion (CRS-2 and CSS-1) and a PG 64-
22 asphalt binder that are allowed by ALDOT’s specifications.
Bond strengths were measured with a shear type device at three
temperatures and three normal pressure levels. Three
application rates that encompassed the specification range were
investigated for each tack coat.
Laboratory prepared mixture samples included a coarse- graded blend and a fine-graded blend to represent two different
surface textures. The effects of tack coat type, application rate,
mixture type, testing temperature and normal pressure on the
bond strength were evaluated. In the laboratory phase, it was
found that all of the main factors used in the test plan affected
bond strength. Testing temperature had the most significant
impact on bond strength. As the temperature increases, bond
strength decreases significantly. Testing normal pressure affected
bond strength differently for high, intermediate, and low
temperatures.
Based on the laboratory work, a draft procedure was
developed for determining the bond strength between pavement
layers. An easy to use procedure was selected that was believed to
provide a good indication of the quality of the bond. The
procedure utilizes the simple shear device developed by NCAT
which is similar to bond strength devices used in several
European countries.
Index Terms — Asphalt binder; Polymer; Rheology;
Morphology; Nanomaterial; Bio-oil
I. INTRODUCTION (HEADING 1)
Bituminous mix is composed of aggregates, bitumen and
air-voids. A good bonding between the aggregates and bitumen
is important for satisfactory performance of the bituminous mix
in terms of proper load transfer and resistance to fatigue,
ravelling, moisture sensitivity etc. A large number of studies
have been conducted to understand the bond between
aggregate and bitumen. Contact angle measurement, inverse
gas chromatography, micro-calorimetry methods have been
used to estimate surface energy of aggregates-bitumen
bonding. Some research studies report tensile strength testing
between bitumen and aggregate or bitumen and other materials.
Marek and Herrin conducted tensile strength test on
bitumen film and found that with the increase in bitumen film
thickness, tensile strength first increases to a peak value and
then decreases and almost becomes constant. In their study, the
peak strength was observed at bitumen film thickness of about
20 μm. Frolov et al. found that for higher values of film
thickness, cohesive strength is independent of film thickness.
Canestrari et al. performed a number of tests with
Pneumatic Adhesion Tensile Testing Instrument (PATTI) test
set-up on different types of asphalt binders and aggregates.
They found that samples under dry condition primarily showed
cohesive failure and water conditioned samples showed
adhesive or cohesive failure depending on the affinity between
aggregate bitumen systems. Pouli kakos and Partl conducted
tensile strength testing on bituminous film placed between steel
or aggregates.
In their study, cohesive failure was observed at 23oC and
primarily adhesive-failure was observed at -10oC. As can be
seen from the above discussions that limited literature is
available on study of tensile strength between aggregate and
bitumen. This has motivated the present researchers to initiate a
further study in this direction.
II. LITERATURE STUDY
Scarpas et al., (1996) developed the CAPA (Computer
Aided Pavement Analysis) system using both 2-D and 3-D
finite element routines to study the contribution of
reinforcement layers to the overlay system, with the 2-D
program being capable of simulating crack propagation. This
program was eventually upgraded through the implementation
of a constitutive model for the material response of viscoplastic
Page 2 of 4
European Journal of Business &
Social Sciences
Available at https://ejbss.org/
ISSN: 2235-767X
Volume 07 Issue 05
May 2019
Available online: https://ejbss.org/ P a g e | 972
materials and elasto-viscoplastic-fracturing model. The new
system has since been used to evaluate different reinforcement
materials and the affect of bonding of the reinforcement
materials.
Owusu-Antwi et al., (1998) developed a mechanistic-based
reflective cracking model for HMA/PCC pavements, which
was developed to be used by practicing engineers.
The procedure used 2-D plain strain finite element
modeling for stress intensity computations and 3-D finite
element modeling for computing the required mathematical
expressions to determine the “J-integral” for temperature and
traffic loadings. The authors used 33 LTPP HMA overlaid
PCC pavement sections for their analysis and finally derived a
mechanistic-empirical model for predicting reflective cracks by
using optimization techniques.
Kohale and Lytton (2000) also developed a mechanistic- based reflective cracking model for evaluating different
reflective cracking mitigation techniques. The computer
program was used to develop design equations for flexible
overlays with Stress Absorbing Membrane Interlayers
(SAMI‟s) and Reinforcing Grids. The equations were then
calibrated using in-service data from the Florida Department of
Transportation. In 2000, identifying the lack of research
focused on the issue of reflective cracking in bituminous
overlays, the RILEM group of Europe sponsored the first
international conference solely dedicated to reflective cracking.
III. EXPERIMENTAL STUDY
Locally available sand-stone aggregates and bitumen of
grade VG30 (penetration value obtained between 60 and 70)
are used in the present study. Irregular shaped aggregates are
cut into small cubes (approximately 25 mm each side) by using
a diamond cutter. The surface of the aggregate is polished
thoroughly by using a polishing equipment with abrasive
silicon carbide powder (of size 180 mesh) and water. Followed
by polishing, the samples are rinsed with water to remove any
abrasive powder stuck onto the polished surface. Roughness of
polished surface of five representative aggregate samples are
measured at the Manufacturing Sciences
Fig. 1. Sand-witched layer of bitumen between two polished aggregate
Laboratory, IIT K. The arithmetic mean parameter (Ra) is
obtained as 6.78 μm. In order to form a thin sandwiched layer
of bitumen, two aggregate samples are heated in an oven to
about 110oC and the polished surface of one of them is dipped
inside a pool of hot and molten bitumen maintained at a
temperature of about 150oC.
The aggregates are brought closer (with the bitumen dipped
surface facing the polished surface of the other aggregate) and
they are mildly pressed. Excess bitumen is removed using a
blade.
A. Failure Mechanism
The interaction between vehicle tyres and the pavement
surface is complex (Horak et al. 2009b). Despite significant
research efforts in this area, there remains no routine method to
account for tyre contact stress in pavement design (Al-Qadi &
Wang, 2011). The general forces and mechanisms acting on a
pavement from a passing tyre are, however, commonly
accepted as including normal and shear forces. Shear forces are
present under free-wheeling tyres but increase significantly
during braking and turning operations (Yoo et al. 2006). Raab
& Partl (2004) presented a simple diagrammatic description of
the stresses induced in a surface layer by a moving tyre and this
is reproduced
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Page 3 of 4
European Journal of Business &
Social Sciences
Available at https://ejbss.org/
ISSN: 2235-767X
Volume 07 Issue 05
May 2019
Available online: https://ejbss.org/ P a g e | 973
Fig. 2. Stress in a surface layer from a moving tyre
B. Achieved Bond Strength
A number of asphalt overlays were recently cored and the
interfaces with the underlying pavement tested in the
laboratory for direct shear strength. All overlays tested were
constructed following the standard practices outlined above
and all included asphalt designed to the typical airport
specification. Shear strength results and the calculated Mohr- Coulomb type envelopes are presented in Figure 6. At zero
normal stress the shear strength is provided solely by the
interface‟s cohesion, which is the tensile strength provided by
the tack coat. For the overlays tested, the cohesion values range
from 223-366 kPa with an average of 274 kPa. The slope of the
shear strength envelope represents the combined mechanical
interlock and friction contribution. This is characterised by the
friction angle. For the overlays tested, the friction angles
ranged from 33-55° with an average of 42°. For the nine cores
tested, the regression coefficients for the calculated shear
strength envelopes averaged 94% indicating a highly reliable
and linear relationship between normal stress and shear
strength.
C. Potential Improvements
Construction processes currently adopted for airport
overlays in Australia already take precautions to minimise the
risk of poor bond leading to delamination failures. Possible
additional improvements include the texturing of the surface in
a direction that is perpendicular to the direction of aircraft
movement as well as dry texturing of the existing surface. Both
of these initiatives are possible but impractical. Unless
texturing is allowed a few shifts in advance of the paving
operation, transverse texturing would have significant impact
on overlay productivity and therefore cost/duration of
resurfacing works. Dry texturing reduces the service life of
cold planing machine teeth and is resisted by contractors. It has
been performed on airports in the USA following bond-related
failures but is not widely adopted. Improved tack coat
performance is the primary improvement that could practically
be made.
Fig. 3. Jet Bond and CRS emulsion Interface Shear Strengths
IV. EFFECT OF BOND ON PAVEMENT PERFORMANCE
Several recent studies have evaluated the effect of the bond
on pavement performance using mechanistic pavement models.
In 2004, King and May presented an analysis of the effect of
bond between HMA layers using the program BISAR (11).
They analyzed a pavement structure with two 4-inch (100
mm) HMA layers over a 6- inch (150 mm) aggregate base and
two subgrade stiffnesses. Two load levels were used, 9 kip (40
kN) dual tire and 12 kip (53.4 kN) dual tire. The interface
between HMA layers was modeled in separate runs from a no
slip condition to full slip between (no bond) layers.
Program outputs analyzed included maximum stress and
strain at various locations and numbers of load repetitions to
failure. All of the outputs show a dramatic increase in stresses
and strains or decrease in pavement life when the interface
drops from full bond to about 90 percent bond. Figure 3 shows
fatigue life decreasing by about 50 percent for each
load/subgrade condition when the bond is reduced by 10
percent. Roffe and Chaignon (3) conducted a similar analysis
using the French pavement design program ALIZE. They
analyzed a pavement structure consisting of a 2.4 inch (60 mm)
surface layer, a 5.1 inch (130 mm) HMA intermediate layer
and 7.9 inch (200 mm) aggregate base. The program was run
with full bond and no bond between the HMA layers. Their
analysis showed that the service life of the pavement was
reduced from 20 years to between 7 and 8 years due to the lack
of bond between the HMA layers.
V. RESULTS AND DISCUSSIONS
T Failure of sample occurs due to development of crack at
the weakest point of the aggregate-bitumen-aggregate junction.
The crack may develop either at the aggregate bitumen
interface (i.e. adhesive failure) or within the bitumen (i.e.
cohesive failure) or combination of both. As the vertical
deformation increases the size of crack also increases. These
results in separation of two aggregates from each other and the
material fail to carry any further load.
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