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FINITE ELEMENT ANALYSIS OF THE MECHANICS OF VISCOELASTIC<br />

ASPHALTIC PAVEMENTS SUBJECTED TO VARYING TIRE CONFIGURATIONS<br />

by<br />

Roberto Firmeza Soares<br />

A THESIS<br />

Presented to <strong>the</strong> Faculty <strong>of</strong><br />

The Graduate College at <strong>the</strong> University <strong>of</strong> Nebraska<br />

In Partial Fulfillment <strong>of</strong> Requirements<br />

For <strong>the</strong> Degree <strong>of</strong> Master <strong>of</strong> Science<br />

Major: Engineering Mechanics<br />

Under <strong>the</strong> Supervision <strong>of</strong> Pr<strong>of</strong>essor David H. Allen<br />

Lincoln, Nebraska<br />

November, 2005


FINITE ELEMENT ANALYSIS OF THE MECHANICS OF VISCOELASTIC<br />

ASPHALTIC PAVEMENTS SUBJECTED TO VARYING TIRE CONFIGURATIONS<br />

by<br />

Roberto Firmeza Soares<br />

A THESIS<br />

Presented to <strong>the</strong> Faculty <strong>of</strong><br />

The Graduate College at <strong>the</strong> University <strong>of</strong> Nebraska<br />

In Partial Fulfillment <strong>of</strong> Requirements<br />

For <strong>the</strong> Degree <strong>of</strong> Master <strong>of</strong> Science<br />

Approved as to style and content by:<br />

_______________________________<br />

David H. Allen<br />

Chair <strong>of</strong> Committee<br />

_______________________________<br />

Mehrdad Negahban<br />

Member<br />

_______________________________<br />

Yuris A. Dzenis<br />

Member<br />

_______________________________<br />

Yong R. Kim<br />

Member<br />

November, 2005


FINITE ELEMENT ANALYSIS OF THE MECHANICS OF VISCOELASTIC<br />

ASPHALTIC PAVEMENTS SUBJECTED TO VARYING TIRE CONFIGURATIONS<br />

Roberto Firmeza Soares, MS<br />

University <strong>of</strong> Nebraska, 2005<br />

Advisor: David H. Allen<br />

This <strong>the</strong>sis proposes a model for predicting <strong>the</strong> mechanical behavior and<br />

performance life <strong>of</strong> asphalt pavements subjected to various tire configurations, layer<br />

geometries and material properties. A <strong>viscoelastic</strong> two-dimensional <strong>finite</strong> <strong>element</strong> model<br />

is formulated in order to predict which combination <strong>of</strong> design variables increase and<br />

improve pavement life.<br />

The formulation utilizes recently proposed advanced algorithms to produce a<br />

time-marching computational algorithm capable <strong>of</strong> predicting <strong>the</strong> spatial and temporal<br />

variations in stresses, strains and displacements in <strong>viscoelastic</strong> roadways subjected to<br />

various configurations <strong>of</strong> loads, geometry and material properties.<br />

In this study, <strong>the</strong> effects <strong>of</strong> truck loads on <strong>the</strong> pavement performance are<br />

simulated by a cyclic load. Three tire configurations are included in <strong>the</strong> study, including<br />

two types <strong>of</strong> <strong>the</strong> new generation, wide-base single tire and one conventional dual tire<br />

configuration. Also, two different types <strong>of</strong> hot mix asphalt and three variations <strong>of</strong> <strong>the</strong><br />

asphalt layer thickness are evaluated.


The results presented here show that <strong>the</strong> use <strong>of</strong> conventional dual tires produces<br />

approximately 50% more service life when compared to <strong>the</strong> use <strong>of</strong> wide tires. Also, by<br />

increasing <strong>the</strong> asphalt layer thickness, <strong>the</strong> service life is increased. For instance, a 15 cm<br />

thick asphalt layer provides a 15% better life than a 10 cm thick layer. However, if a 20<br />

cm thick layer is compared with a 15 cm layer, <strong>the</strong> life goes up about 18%. Comparisons<br />

<strong>of</strong> two different asphalt mixtures, shows that one produces a lifespan six times that <strong>of</strong> <strong>the</strong><br />

o<strong>the</strong>r. These results indicate that <strong>the</strong> model proposed herein can play a fundamental role<br />

in pavement design and hot mix selection.


i<br />

Dedication<br />

to God for my health;<br />

to my wife Marilena;<br />

to my parents Aroldo and Laís.


ii<br />

Acknowledgments<br />

I wish to express my sincere gratitude to Dr. David H. Allen, chair <strong>of</strong> my graduate<br />

advisory committee for <strong>the</strong> time invested on me, for his guidance and all <strong>the</strong><br />

opportunities during my Master’s program. Without his expert knowledge this work<br />

would not have been possible. Also I would like to thank all <strong>the</strong> members <strong>of</strong> my<br />

committee, Dr. Mehrdad Negahban, Dr. Yong Rak Kim and Dr. Yuris Dzenis for all <strong>the</strong><br />

assistance that I have received in so many ways and for being available to share <strong>the</strong>ir<br />

knowledge every time I had questions.<br />

I also would like to thank pr<strong>of</strong>essor Jorge B. Soares from <strong>the</strong> Federal University<br />

<strong>of</strong> Ceará (Brasil) for introducing me to <strong>the</strong> research field <strong>of</strong> asphalt pavement.<br />

I wish to acknowledge <strong>the</strong> financial support provided by <strong>the</strong> Army Research<br />

Office with <strong>the</strong> contract number is W911NF-04-2-0011.<br />

Special thanks are due to my classmates Mr. Philip Yuya, Mr. Ashwani Goel and<br />

Mr. Kitti Ratatanadit for <strong>the</strong>ir friendship and shared knowledge; to Mr. Felipe Freitas,<br />

Mr. Victor Teixeira and Mr. Sávio Câmara for all <strong>the</strong> technical support; Mr. James Nau<br />

for setting up <strong>the</strong> supercomputer; Ms. Michelle Sitorius for taking <strong>the</strong> time to read<br />

through my <strong>the</strong>sis; and my friends Ms. Jamilla Lutif and Mr. Thiago Aragão for <strong>the</strong>ir<br />

friendship.<br />

Finally, I wish to thank my family. My wife, Marilena, for all <strong>the</strong> support, love,<br />

patience and encouragement throughout this effort and also for making all <strong>the</strong> pictures in<br />

this work. There are not enough words to describe my appreciation. My mo<strong>the</strong>r and


iii<br />

fa<strong>the</strong>r whom I love so much for encouraging me to pursue my education; and to my<br />

bro<strong>the</strong>r Paulo and my sister Renata, just for being part <strong>of</strong> my life.<br />

But very special thanks are due to God for giving me my life back.


iv<br />

List <strong>of</strong> Tables<br />

Table 1: Viscoelastic material properties.................................................................... 54<br />

Table 2: Prony series coefficients <strong>of</strong> relaxation modulus for AC I.......................... 70<br />

Table 3: Prony series coefficients <strong>of</strong> relaxation modulus for AC II......................... 71<br />

Table 4: Material properties for <strong>the</strong> road elastic layers............................................ 71


v<br />

Figure Index<br />

Figure 1: Pavement structure......................................................................................... 3<br />

Figure 2: Typical asphalt pavement structure.............................................................. 3<br />

Figure 3: Loads in Pavement ......................................................................................... 4<br />

Figure 4: Aggregates ....................................................................................................... 6<br />

Figure 5: Mixing ................................................................................................................ 7<br />

Figure 6: Pouring mix into <strong>the</strong> mold .............................................................................. 7<br />

Figure 7: Gyratory compactor......................................................................................... 8<br />

Figure 8: Cracking.......................................................................................................... 11<br />

Figure 9: Cracking.......................................................................................................... 11<br />

Figure 10: Thermal cracking......................................................................................... 13<br />

Figure 11: Rutting........................................................................................................... 14<br />

Figure 12: Rutting........................................................................................................... 14<br />

Figure 13: Tandem axle – wide tires (Courtesy <strong>of</strong> Michelin American)................. 16<br />

Figure 14: Tandem axle ................................................................................................ 16<br />

Figure 15: 18 wheeler truck .......................................................................................... 17<br />

Figure 16: Tridem axle................................................................................................... 17<br />

Figure 17: European truck ............................................................................................ 18<br />

Figure 18: Truck with dual tires or wide tires configuration ..................................... 19<br />

Figure 19: Dual tire vs. Wide base .............................................................................. 20<br />

Figure 20: Types <strong>of</strong> tires ............................................................................................... 22<br />

Figure 21: Measured tire pressure distribution. Courtesy Tekscan, Inc................ 23<br />

Figure 22: Tire footprints – Hua and White, 2002..................................................... 24


vi<br />

Figure 23: General three dimensional body............................................................... 33<br />

Figure 24: T3 triangular <strong>element</strong> representation....................................................... 46<br />

Figure 25: Wiechert model............................................................................................ 53<br />

Figure 26: Rectangular bar subjected to a tip load................................................... 56<br />

Figure 27: Loading history and response <strong>of</strong> example 1........................................... 57<br />

Figure 28: Loading history and response <strong>of</strong> example 2........................................... 58<br />

Figure 29: Cylinder with Internal Pressure................................................................. 59<br />

Figure 30: Finite <strong>element</strong> mesh used in example 3.................................................. 60<br />

Figure 31: Loading history and response for example 3.......................................... 61<br />

Figure 32: Beam problem <strong>of</strong> example 4 ..................................................................... 63<br />

Figure 33: Loading history and response for example 4.......................................... 64<br />

Figure 34: Typical two-lane roadway cross section.................................................. 65<br />

Figure 35: Right half side to be modeled.................................................................... 66<br />

Figure 36: Boundary conditions on <strong>the</strong> pavement .................................................... 67<br />

Figure 37: Side slopes <strong>of</strong> roadways (NDor, 2005).................................................... 67<br />

Figure 38: Pavement structure and all layers ............................................................ 69<br />

Figure 39: Comparison between AC I and AC II....................................................... 72<br />

Figure 40: Weight distribution ...................................................................................... 73<br />

Figure 41: Tire pressure distribution (Blackman, Halliday, and Merrill, 2000)...... 75<br />

Figure 42: Pavement 3-D with forces.......................................................................... 76<br />

Figure 43: Pavement 2-D with forces.......................................................................... 76<br />

Figure 44: Comparison between 3D and 2D loads................................................... 77<br />

Figure 45: First cyclic load – axle loads...................................................................... 78


vii<br />

Figure 46: Cyclic load .................................................................................................... 79<br />

Figure 47: Convergence <strong>of</strong> maximum displacement for 29.5 tire........................... 81<br />

Figure 48: Mesh for <strong>the</strong> dual configuration tire – 29.5 cm ....................................... 81<br />

Figure 49: Convergence <strong>of</strong> maximum displacement for 44.5 tire........................... 82<br />

Figure 50: Mesh for <strong>the</strong> wide configuration tire – 44.5 cm ...................................... 82<br />

Figure 51: Convergence <strong>of</strong> maximum displacement for 49.5 tire........................... 83<br />

Figure 52: Mesh for <strong>the</strong> wide configuration tire – 49.5 cm ...................................... 83<br />

Figure 53: Pavement with side slope 1:6 ................................................................... 84<br />

Figure 54: Pavement with side slope 1:3 ................................................................... 84<br />

Figure 55: Pavement with side slope 1:1 ................................................................... 84<br />

Figure 56: Pavement with side slope 0.5:1 ................................................................ 84<br />

Figure 57: Displacement on <strong>the</strong> surface for different side slopes .......................... 85<br />

Figure 58: Failure criterion............................................................................................ 87<br />

Figure 59: Displacement versus time.......................................................................... 88<br />

Figure 60: Displacement versus time in log scale .................................................... 88<br />

Figure 61: Different tire configurations for HMA thickness <strong>of</strong> 10cm....................... 89<br />

Figure 62: Different tire configurations for HMA thickness <strong>of</strong> 15cm....................... 90<br />

Figure 63: Different tire configurations for HMA thickness <strong>of</strong> 20cm....................... 90<br />

Figure 64: Different HMA thicknesses for dual tires 29.5 cm.................................. 91<br />

Figure 65: Different HMA thicknesses for dual tires 44.5 cm.................................. 93<br />

Figure 66: Different HMA thicknesses for dual tires 49.5 cm.................................. 93


viii<br />

Table <strong>of</strong> Contents<br />

CHAPTER 1 .......................................................................................................................1<br />

Introduction.................................................................................................................... 1<br />

Asphalt Pavement Structures..................................................................................... 4<br />

Asphalt Materials........................................................................................................ 4<br />

Asphalt Pavement Distress ......................................................................................... 9<br />

Truck Loading........................................................................................................... 15<br />

Pavement Design ...................................................................................................... 24<br />

Research Objective.................................................................................................... 29<br />

CHAPTER 2 ..................................................................................................................... 31<br />

Solution Method.......................................................................................................... 31<br />

CHAPTER 3 ..................................................................................................................... 38<br />

Finite Element Formulation....................................................................................... 38<br />

Incrementalization <strong>of</strong> <strong>the</strong> Constitutive Equations..................................................... 38<br />

Method <strong>of</strong> Weight Residuals ..................................................................................... 40<br />

Displacement Formulation ....................................................................................... 44<br />

CHAPTER 4 ..................................................................................................................... 50<br />

Code Description and Verification ........................................................................... 50<br />

Code Description ...................................................................................................... 50<br />

Code Verification...................................................................................................... 52<br />

CHAPTER 5 ..................................................................................................................... 65<br />

Asphalt Concrete Roadway Analysis ...................................................................... 65<br />

Roadway Geometry................................................................................................... 65


ix<br />

Pavement Layer Characterization ............................................................................ 67<br />

Overestimation Between 3-D and 2-D...................................................................... 74<br />

Mesh Convergence.................................................................................................... 79<br />

Results ......................................................................................................................... 85<br />

CONCLUSION................................................................................................................. 94<br />

BIBLIOGRAPHY............................................................................................................. 97


1<br />

CHAPTER 1<br />

The interstates and highways connecting cities and sustaining economic exchange<br />

are integral to <strong>the</strong> infrastructure <strong>of</strong> a country. Accordingly, <strong>the</strong> characteristics—<br />

durability, safety, and comfort—<strong>of</strong> <strong>the</strong>se structures are vital not only for those who travel<br />

on roadways but also for those involved in <strong>the</strong> actual construction. This paper evaluates<br />

<strong>the</strong> effectiveness <strong>of</strong> <strong>the</strong> current use <strong>of</strong> asphalt surfaces and proposes to develop a model<br />

for predicting mechanical behavior and performance life <strong>of</strong> pavements.<br />

I begin with a general overview <strong>of</strong> pavement structures, looking at <strong>the</strong> benefits<br />

and drawbacks <strong>of</strong> different methods <strong>of</strong> paving. Then, a comparison between wide base<br />

tires and dual tire configurations is presented. The second section explores <strong>the</strong> solution<br />

method. The third section develops <strong>the</strong> model for mechanical behavior and performance<br />

prediction based on <strong>the</strong> <strong>finite</strong> <strong>element</strong> formulation. The fourth section evaluates <strong>the</strong> code<br />

description and verification, determining <strong>the</strong> effectiveness <strong>of</strong> <strong>the</strong> entire system. The fifth<br />

and final segment analyzes <strong>the</strong> research results from <strong>the</strong> different computational analyses<br />

performed.<br />

Introduction<br />

Pavements are structures built as layered systems to sustain traffic and to diminish<br />

environmental effects. The most common paving methods are: asphalt concrete (or<br />

flexible pavements), Portland cement concrete (or rigid pavements) and composite<br />

pavements. Establishing which method to use is usually determinate upon cost; however,<br />

o<strong>the</strong>r variables such as durability, i.e. maintenance, and <strong>the</strong> purpose <strong>of</strong> <strong>the</strong> roadway also<br />

play a role, necessitating a delicate balance between road life and road utility. As <strong>of</strong>


2<br />

today, <strong>the</strong>re are 2.27 million miles <strong>of</strong> paved roadways in <strong>the</strong> United States, where 94%<br />

have surfaces <strong>of</strong> asphalt concrete. 1 Correspondingly, an evaluation <strong>of</strong> <strong>the</strong> sustainability <strong>of</strong><br />

<strong>the</strong>se surfaces necessitates fur<strong>the</strong>r research.<br />

Asphalt concrete is a mixture <strong>of</strong> asphalt and mineral aggregate mixed toge<strong>the</strong>r,<br />

spread and compacted at high temperatures. Asphalt concrete is also known as hot mix<br />

asphalt or HMA. The asphalt layer is built on top <strong>of</strong> several o<strong>the</strong>r layers, finishing <strong>the</strong><br />

paving process. With less rigid materials used at <strong>the</strong> bottom, <strong>the</strong> lowest layer in <strong>the</strong><br />

structure is <strong>the</strong> subgrade or natural terrain. The next layer is <strong>the</strong> subbase, consisting <strong>of</strong><br />

specified, compacted material placed on top <strong>of</strong> <strong>the</strong> subgrade to serve as a foundation for<br />

<strong>the</strong> pavement. On top <strong>of</strong> <strong>the</strong> subbase is <strong>the</strong> base, ano<strong>the</strong>r compacted material layer, lying<br />

directly beneath <strong>the</strong> concrete or asphalt. Figure 1 and Figure 2 show <strong>the</strong> pavement<br />

structure, differentiating <strong>the</strong> various layers. This configuration can vary from case to<br />

case. In some instances, <strong>the</strong>se structures require additional reinforced layers to provide<br />

sufficient total pavement thickness and to prevent pavement distress.<br />

1 National Asphalt Pavement Association, retrieved November 10, 2005, from:<br />

http://www.hotmix.org/history.php


3<br />

Figure 1: Pavement structure<br />

Figure 2: Typical asphalt pavement structure<br />

A basic factor in pavement design, and integral to this <strong>the</strong>sis, is <strong>the</strong> vertical<br />

traction on <strong>the</strong> top <strong>of</strong> <strong>the</strong> subgrade (see Figure 3). Traction can be minimized by a


4<br />

properly designed pavement structure, reducing <strong>the</strong> traction to one tenth <strong>of</strong> <strong>the</strong> tire<br />

pressure applied at <strong>the</strong> surface <strong>of</strong> <strong>the</strong> pavement. In turn, <strong>the</strong> strain level is very low,<br />

limiting long term deformations. ideas<br />

Figure 3: Loads in Pavement<br />

Asphalt Pavement Structures<br />

Asphalt Materials<br />

Hot mix asphalt (HMA) is composed <strong>of</strong> three components: aggregates, asphalt<br />

binder and air voids. The interaction <strong>of</strong> <strong>the</strong>se components and <strong>the</strong> <strong>viscoelastic</strong> behavior <strong>of</strong><br />

<strong>the</strong> binder define <strong>the</strong> <strong>the</strong>rmomechanical behavior <strong>of</strong> <strong>the</strong> mixture.


5<br />

Historically, determining which asphalt cement or binder to use has been based on<br />

(i) phenomenological tests developed over time and (ii) experience with asphalt<br />

pavements. Since empirical results work only when all <strong>the</strong> conditions for all <strong>the</strong> tests are<br />

satisfied, penetration and viscosity tests are slowly being replaced by tests that more fully<br />

characterize asphalt binders. For instance, two binders might have <strong>the</strong> same viscosity at<br />

<strong>the</strong> test temperature, but behave differently at a very low temperature. As a result, it can<br />

be difficult to select a binder that will consistently work under varying conditions.<br />

In 1987, <strong>the</strong> U.S. Congress authorized <strong>the</strong> Strategic Highway Research Program<br />

(SHRP) — a five-year, applied research initiative — to develop and evaluate techniques<br />

and technologies to combat <strong>the</strong> deteriorating conditions <strong>of</strong> <strong>the</strong> nation's highways and to<br />

improve <strong>the</strong>ir performance, durability, safety, and efficiency. The final product <strong>of</strong> <strong>the</strong><br />

SHRP asphalt research program is a system referred to as Superpave, which stands for<br />

Superior Performing Asphalt Pavements. The objectives <strong>of</strong> Superpave are: to investigate<br />

why some pavements perform well, while o<strong>the</strong>rs do not; to develop tests and<br />

specifications for materials that will outperform and outlast <strong>the</strong> pavements being<br />

constructed today; and to work with highway agencies and industry to have <strong>the</strong> new<br />

specifications put to use. This enables reduction in maintenance costs, and minimization<br />

on <strong>the</strong> number <strong>of</strong> premature pavement failures. This program actually proposes a new<br />

system <strong>of</strong> specifying asphalt materials, providing a new asphalt binder specification, new<br />

tests and a new mix design and <strong>analysis</strong> system.<br />

In this system, asphalt binders are classified based on <strong>the</strong>ir performance in a range<br />

<strong>of</strong> climates and pavement temperatures, relating <strong>the</strong> properties <strong>of</strong> <strong>the</strong> asphalt mixture to


6<br />

<strong>the</strong> conditions under which <strong>the</strong>y will be used. 2<br />

Those binders are classified by a “PG”<br />

(Performance Grade) rating, where <strong>the</strong> first number indicates <strong>the</strong> high temperature grade<br />

and <strong>the</strong> second number corresponds to <strong>the</strong> low temperature grade. Thus, a PG 58-22 is<br />

intended for use where <strong>the</strong> average, seven-day, maximum pavement temperature is 58°C<br />

and <strong>the</strong> expected minimum pavement temperature is -22°C. 3<br />

By selecting quality<br />

aggregates and <strong>the</strong> correct Superpave performance graded (PG) asphalt binder, it is<br />

possible to make high quality, hot mix asphalt for a variety <strong>of</strong> conditions. Figure 4,<br />

Figure 5, Figure 6 and Figure 7 show <strong>the</strong> Superpave procedure to produce <strong>the</strong> mixture in<br />

<strong>the</strong> laboratory.<br />

Figure 4: Aggregates<br />

2 CDot, 2005.<br />

3 Note that <strong>the</strong>se numbers are pavement temperatures and not air temperatures.


7<br />

Figure 5: Mixing<br />

Figure 6: Pouring mix into <strong>the</strong> mold


8<br />

Figure 7: Gyratory compactor<br />

Although <strong>the</strong> character <strong>of</strong> <strong>the</strong> asphalt binder is influential to a hot mix asphalt, air<br />

voids and aggregates can also influence pavement performance. Factors like gradation<br />

and type <strong>of</strong> aggregates and/or high permeability to air or water play an important role in<br />

pavement durability. Asphalt binders exposed to air become brittle due to oxidation and<br />

tend to undergo cracking. High permeability to water enables stripping <strong>of</strong> <strong>the</strong> binder from<br />

<strong>the</strong> aggregates, making it possible for <strong>the</strong> lower layers to be carried away.<br />

In addition, ano<strong>the</strong>r important factor to keep in mind when determining pavement<br />

materials and structure is traffic loads. Heavy vehicles, such as trucks, significantly<br />

influence pavement distresses and failure. Currently, <strong>the</strong> importance <strong>of</strong> roadway


9<br />

transportation has grown as vehicles are heavier with greater load-carrying capacity and<br />

high tire pressures. Consequently, pavement loadings have significantly increased along<br />

with <strong>the</strong> number <strong>of</strong> heavy vehicles traveling roads across <strong>the</strong> globe, resulting in<br />

premature failure. As a primary variable <strong>of</strong> pavement design, accurate configuration <strong>of</strong><br />

<strong>the</strong> truck loading and investigations on <strong>the</strong> impact <strong>of</strong> heavy traffic on pavement<br />

performance is an important issue and, indeed, remains an issue. Although truck loads are<br />

important, pavements are complex systems involving interaction <strong>of</strong> o<strong>the</strong>r variables. Their<br />

performance is also influenced by material properties, <strong>the</strong> environment, construction<br />

practices and geometry <strong>of</strong> tires and/or layers.<br />

Asphalt Pavement Distress<br />

Determining <strong>the</strong> expected service life <strong>of</strong> a pavement system is an important<br />

parameter to be considered in <strong>the</strong> design <strong>of</strong> a pavement. Pavements constructed <strong>of</strong> hot<br />

mix asphalt are typically designed to last at least 20 years and perform well under stress,<br />

from <strong>the</strong> extremes <strong>of</strong> high and low temperatures to heavy traffic loads. However, it is not<br />

unusual to see severe deterioration in those pavements well before <strong>the</strong> expected service<br />

life is met, resulting in irregular roadways and high maintenance and rehabilitation costs.<br />

Loads, geometry and material properties contribute to declines or increases in this<br />

expected life, some <strong>of</strong> <strong>the</strong>ses factors include, thickness <strong>of</strong> pavement layers, material<br />

properties, tire pressures, axle loads, tire configuration and volume <strong>of</strong> traffic. The major<br />

causes <strong>of</strong> asphalt pavement failures are cracking and rutting.<br />

Cracking<br />

One possibility leading to cracking occurs due to excessive traffic load, causing<br />

pavement failure by fatigue cracking, and introducing openings on <strong>the</strong> surface allowing


10<br />

moisture to penetrate and accelerating pavement deterioration. These cracks start as<br />

microcracks and propagate with time due to tensile or shear stresses or both. These<br />

cracks <strong>the</strong>n form macrocracks. To accurately predict fatigue is a complex task and for <strong>the</strong><br />

past several decades, significant research has been done in this area to develop reliable<br />

models.<br />

Castell, Ingraffea and Irwin focus on identifying <strong>the</strong> differences in crack<br />

propagation between a common laboratory fatigue test specimen - beam and layered<br />

pavement using a 2-D <strong>finite</strong> <strong>element</strong> with fracture <strong>mechanics</strong> capabilities. 4 Lee and Kim<br />

present a mechanistic approach to uniaxial <strong>viscoelastic</strong> constitutive modeling <strong>of</strong> asphalt<br />

concrete mixtures, accounting for <strong>the</strong> rate-dependent damage growth. 5 Lee also<br />

developed a fatigue performance prediction model <strong>of</strong> asphalt concrete based on <strong>the</strong><br />

elastic-<strong>viscoelastic</strong> correspondence principle and continuum damage <strong>mechanics</strong>.<br />

Schapery developed a so-called work potential <strong>the</strong>ory applicable to describing <strong>the</strong><br />

mechanical behavior <strong>of</strong> elastic media with growing damage and o<strong>the</strong>r structural changes. 6<br />

He also developed a <strong>the</strong>ory for predicting <strong>the</strong> time-dependent size and shape <strong>of</strong> cracks in<br />

linear <strong>viscoelastic</strong>, isotropic media. 7 A number <strong>of</strong> studies involving <strong>the</strong>ory <strong>of</strong> crack<br />

initiation and growth in <strong>viscoelastic</strong> media can be found in <strong>the</strong> literature. 8<br />

4 Castell, M.A., A. R. Ingraffea, L. H. Irwin. “Fatigue Crack Growth in Pavements.” Journal <strong>of</strong><br />

Transportation Engineering. Volume 126, Number 4 (July 2000): 283-290.<br />

5 Lee, Hyun-Jong, Kim, Y. Richard. “Viscoelastic Constitutive Model for Asphalt Concrete Under Cyclic<br />

Loading.” Journal <strong>of</strong> Engineering Mechanics. Vol. 124, No. 1 (January 1998): 32-40.; Lee, Hyun-Jong;<br />

Kim, Y. Richard. “Viscoelastic Continuum Damage Model <strong>of</strong> Asphalt Concrete With Healing.” Journal <strong>of</strong><br />

Engineering Mechanics. Vol. 124 Issue 11 (Nov98): 1224, 9<br />

6 Schapery, R.A. ‘‘A <strong>the</strong>ory <strong>of</strong> mechanical behavior <strong>of</strong> elastic media with growing damage and o<strong>the</strong>r<br />

changes in structure.’’ Journal <strong>of</strong> Mech.Phys. Solids. 38 (1990): 215–253.<br />

7 Schapery, R.A. A <strong>the</strong>ory <strong>of</strong> crack initiation and growth in <strong>viscoelastic</strong> media (Part I), International<br />

Journal <strong>of</strong> Fracture, 11, 1975. 141–59.; Schapery, R.A. A <strong>the</strong>ory <strong>of</strong> crack initiation and growth in<br />

<strong>viscoelastic</strong> media (Part II), International Journal <strong>of</strong> Fracture, 11, 1975b. 369–88.<br />

8 See (Schapery, 1975a; Schapery, 1975b; Schapery, 1978; Schapery, 1986; Schapery 1990; Park and<br />

Schapery, 1997; Kim, 1995, Costanzo and Allen, 1993).


11<br />

Figure 8: Cracking<br />

Figure 9: Cracking


12<br />

Cracking can also be caused by temperature, ei<strong>the</strong>r from very large temperature<br />

variations or very cold temperatures. Those <strong>the</strong>rmal cracks occur because <strong>the</strong> shrinkage<br />

<strong>of</strong> <strong>the</strong> surface is restrained; <strong>the</strong>refore, tensile stress is developed until it reaches <strong>the</strong><br />

tensile strength, forming <strong>the</strong> crack. 9<br />

Not only is <strong>the</strong> asphalt surface subjected to this<br />

phenomenon, but also <strong>the</strong> base, subbase and subgrade, that can potentially propagate up<br />

to <strong>the</strong> asphalt layer by reflective cracking. In this case, tensile stress is greatest in <strong>the</strong><br />

longitudinal direction, explaining <strong>the</strong> fact that <strong>the</strong>rmal cracks are usually transverse. Easa<br />

provided a reliability-based model which predicts <strong>the</strong>rmal cracking <strong>of</strong> pavements and<br />

relates it to cold winters, spring thaws, and daily cyclic <strong>the</strong>rmal loading. 10 and Shen and<br />

Kirkner 11 developed a multiscale model to simulate <strong>the</strong> distributed <strong>the</strong>rmal cracking<br />

primarily for asphalt concrete pavement structures. They used this model to study <strong>the</strong><br />

interaction between multiple cracks and predict <strong>the</strong> crack spacing. They assumed <strong>the</strong>re is<br />

a set <strong>of</strong> fictitious cracks on <strong>the</strong> pavement. When temperature drops, some fictitious cracks<br />

become predominant to <strong>the</strong> o<strong>the</strong>rs and turn out to be major cracks.<br />

9 See (Al-Qadi, I. L., et al., 2004).<br />

10 Easa, Said M. “Reliability-Based Model for Predicting Pavement Thermal Cracking.” Journal <strong>of</strong><br />

Transportation Engineering. Volume 122, Number 5 (September 1996): 374-380.<br />

11 Shen, Weixin, David J. Kirkner. “Distributed Thermal Cracking <strong>of</strong> AC Pavement with Frictional<br />

Constraint.” Journal <strong>of</strong> Engineering Mechanics. Volume 125, Number 5 (May 1999): 554-560.


13<br />

Figure 10: Thermal cracking<br />

Rutting<br />

The o<strong>the</strong>r cause <strong>of</strong> asphalt pavement failures is rutting. Rutting is characterized by<br />

depressions along <strong>the</strong> wheel path caused by <strong>the</strong> permanent deformation <strong>of</strong> <strong>the</strong> asphalt<br />

concrete mixture, base, or subgrade materials. Highway rutting is common due to high<br />

canalizations and higher repetition traffic. Ramsamooj presented a new elastoplastic<br />

model for predicting <strong>the</strong> stress/strain response <strong>of</strong> asphalt concrete under cyclic loading,<br />

incorporating a complete description <strong>of</strong> <strong>the</strong> plastic deformation <strong>of</strong> asphalt concrete and<br />

including <strong>the</strong> elastic, <strong>viscoelastic</strong>, and plastic components. 12 The plastic deformation is<br />

calculated by a computer program and compared with experimental results. Douglas,<br />

1997; Collop, 1995; and Chen, 2004 also studied several effects <strong>of</strong> rutting in asphalt<br />

pavements.<br />

12 Ramsamooj, D.V., J. Ramadan, G. S. Lin. “Model Prediction <strong>of</strong> Rutting in Asphalt Concrete.” Journal <strong>of</strong><br />

Transportation Engineering. Volume 124 Number 5 (September 1998): 448-456.


14<br />

Figure 11: Rutting<br />

Figure 12: Rutting


15<br />

In <strong>the</strong> past 20 years traffic load as well as truck tire pressures have increased in<br />

<strong>the</strong> US and impacted <strong>the</strong> pavement long-term life and performance; consequently, <strong>the</strong><br />

roadways have experienced premature failure <strong>of</strong> <strong>the</strong> asphalt layer. The effect <strong>of</strong> tire<br />

configurations and pressure are not <strong>the</strong> only variables <strong>of</strong> interest in pavement design.<br />

Varying material properties, such as size <strong>of</strong> <strong>the</strong> aggregate, percentage <strong>of</strong> binder in <strong>the</strong><br />

asphalt concrete mixture, and <strong>the</strong> thickness <strong>of</strong> asphalt layer, impact <strong>the</strong> service life <strong>of</strong><br />

pavement. Fur<strong>the</strong>rmore, by increasing <strong>the</strong> thickness <strong>of</strong> <strong>the</strong> asphalt layer, <strong>the</strong> pavement<br />

becomes less vulnerable to high pressure tires. It should be noted that with load,<br />

geometry and material property variation, expected pavement life is altered. Given that<br />

<strong>the</strong> major part <strong>of</strong> paved roadways have hot mix asphalt surface, those issues are <strong>of</strong> great<br />

interest for <strong>the</strong> Departments <strong>of</strong> Transportation around <strong>the</strong> country. Among <strong>the</strong> primary<br />

factors that contribute to pavement deterioration are changes in truck loading, which<br />

include axle weight and configuration, tire type, and suspension systems.<br />

Truck Loading<br />

Wide base tires x dual tires<br />

Currently, a wide-base single tire has been proposed as a replacement for<br />

conventional dual tires. They are more commonly used in Europe and Canada; however,<br />

<strong>the</strong>se configurations are slowly appearing in <strong>the</strong> US market and are intended to replace<br />

<strong>the</strong> dual tire configuration for a larger tire. In <strong>the</strong> United States <strong>the</strong> most common type <strong>of</strong><br />

truck is <strong>the</strong> 18-wheeler, which is has 5 axles. The front, steer axle has one wheel at each<br />

side and <strong>the</strong> rear has two tandem axles. Each tandem axle is composed by two pairs <strong>of</strong><br />

double wheels at each side. Figure 13 and Figure 14 shows a tandem axle and Figure 15<br />

shows an 18-wheeler.


16<br />

Figure 13: Tandem axle – wide tires (Courtesy <strong>of</strong> Michelin American)<br />

Figure 14: Tandem axle


17<br />

Figure 15: 18 wheeler truck<br />

Europe uses <strong>the</strong> wide tire configuration on <strong>the</strong> majority <strong>of</strong> trucks. There, <strong>the</strong> most<br />

common configuration also has 5 axles, again with <strong>the</strong> front, steer having two wheels,<br />

and <strong>the</strong> rear, instead <strong>of</strong> having two tandem axles, has one single and one tridem axle with<br />

three axles at <strong>the</strong> rear with single wheels, or 6 wheels in total. Thus, whatever <strong>the</strong><br />

configuration, <strong>the</strong> entire vehicle usually has 12 wheels in total. Figure 16 shows a tridem<br />

axle and Figure 17 shows an European truck.<br />

Figure 16: Tridem axle


18<br />

Figure 17: European truck<br />

Even though wide tire configuration is used more <strong>of</strong>ten in Europe, it is being<br />

introduced in <strong>the</strong> US and Canada by simply replacing <strong>the</strong> dual tires by wide ones and still<br />

carrying equal loads. This research project investigates <strong>the</strong> effect <strong>of</strong> wide base tires and<br />

dual tires assemblies in <strong>the</strong> US and Canada. 13<br />

Replacing both sides <strong>of</strong> dual tires with<br />

larger tires results in a smaller total contact area with <strong>the</strong> pavement. The load weight<br />

remains <strong>the</strong> same with <strong>the</strong> larger tires, yet, <strong>the</strong> pressure is larger in <strong>the</strong> wide tire case. 14<br />

13 Figure 18 shows <strong>the</strong> types <strong>of</strong> truck analyzed for this research project.<br />

14 Figure 19 shows a dual configuration compared with a wide base tire.


19<br />

Figure 18: Truck with dual tires or wide tires configuration<br />

While a single wide tire <strong>of</strong>fers advantages for fuel efficiency, productivity and<br />

vehicle stability, 15 its pavement wear characteristics are still being examined. Even<br />

though <strong>the</strong> market for wide-base tires does not surpass 5% <strong>of</strong> truck applications, <strong>the</strong>re is<br />

potential for an increase in demand.<br />

15 (Giles, 1979; John and Glauz, 1995; Sebaaly, 1998)


20<br />

Figure 19: Dual tire vs. Wide base<br />

Research in <strong>the</strong> past has shown that <strong>the</strong> wide-base tire can cause significantly<br />

more damage to <strong>the</strong> pavement compared to conventional dual tires. The damage is related<br />

to tire width and tire pressure. Sebaaly and Tabatabaee investigated <strong>the</strong> response <strong>of</strong><br />

various flexible pavement structures in terms <strong>of</strong> tensile strain on <strong>the</strong> bottom <strong>of</strong> <strong>the</strong> asphalt<br />

layer, <strong>the</strong> compressive stress at <strong>the</strong> asphalt layer interface and <strong>the</strong> surface deflection. 16<br />

For all asphalt concrete thicknesses, <strong>the</strong> tensile strain under <strong>the</strong> wide-base tires was 50%<br />

greater than those under <strong>the</strong> dual tires. Compressive stresses at <strong>the</strong> interface were lower<br />

for <strong>the</strong> dual tires. The wide-base tires are designed with narrow tread width, causing high<br />

16 Sebaaly, P., N. Tabatabaee. Effect <strong>of</strong> Tire Pressure and Type on Response <strong>of</strong> Flexible Pavement.<br />

Transportation Research Record. (1989): (1227) 115-127.


21<br />

vertical and contact stresses between <strong>the</strong> road and tire. The US Department <strong>of</strong><br />

Transportation performed a comprehensive truck size and weight study showing that <strong>the</strong><br />

wide-base tires appear to cause 1.5 times more rutting than dual tires on flexible<br />

pavements. This is an indication that those tires were designed with greater concern for<br />

non-pavement costs, thus, resulting in restrictions on allowable weight on axles equipped<br />

with wide-base single tires. Most <strong>of</strong> <strong>the</strong> studies performed comparing dual tires versus<br />

wide tires, concluded that wide tires are more damaging to <strong>the</strong> pavement than are<br />

conventional dual tires. 17<br />

Recent advances in materials and tire design have led to <strong>the</strong> development <strong>of</strong> a new<br />

generation <strong>of</strong> wide-base tires with <strong>the</strong> claim that <strong>the</strong>ir new technology causes no<br />

additional infrastructure wear as compared to dual tires. This new design resulted in a<br />

wider flatter transverse pr<strong>of</strong>ile, providing a uniform pressure distribution (See Figure 20).<br />

Ponniah analyzed <strong>the</strong> impact <strong>of</strong> this new technology on pavements by using <strong>the</strong> methods<br />

<strong>of</strong> equivalent single axle loads and showed that <strong>the</strong> current axle load limit <strong>of</strong> 6000 kg in<br />

Canada for single tires can be increased up to 8000 kg for wide-base tires with no more<br />

damage than dual tires at 10000 kg. 18<br />

17 (Akram, Scullion, Smith, Fernando, 1992; Huhtala, Pihlajamaki, Pienimaki, 1989; Perdomo, Nokes,<br />

1993, Al-Qadi, Pyeong, Elseifi, 2005; Myers; Roque, Ruth, Drakos, 1999; Priest, 2005)<br />

18 (Ponniah et al., 2003)


22<br />

Figure 20: Types <strong>of</strong> tires<br />

Al-Qadi developed an experimental program performed under different loading<br />

and environmental conditions and at different speeds in order to understand <strong>the</strong> behavior<br />

<strong>of</strong> <strong>the</strong> new tire. 19<br />

The conclusions showed that <strong>the</strong> newly developed tires and <strong>the</strong><br />

conventional dual tire produce approximately <strong>the</strong> same horizontal strains under <strong>the</strong><br />

asphalt concrete layer. Fur<strong>the</strong>rmore, <strong>the</strong> fatigue damage is <strong>the</strong> same as that produced by<br />

dual tires. However, <strong>the</strong> vertical compressive stresses induced by <strong>the</strong> wide-base are<br />

greater on <strong>the</strong> upper asphalt concrete layers <strong>of</strong> <strong>the</strong> tested pavement. Recently, Al-Qadi<br />

performed a three-dimensional <strong>analysis</strong> using a <strong>viscoelastic</strong> constitutive model to<br />

simulate <strong>the</strong> pavement responses to different vehicular loadings. They used two newgeneration<br />

wide-tires, and, in general, <strong>the</strong> wider one produced less damage than <strong>the</strong><br />

narrower one. For this <strong>analysis</strong>, damage was defined by four failure parameters: fatigue<br />

cracking, primary and secondary rutting, and top-down cracking. It was noted that by<br />

using <strong>the</strong> wide-base tires, <strong>the</strong> truck’s overall weight would be reduced by approximately<br />

450 kg and <strong>the</strong> truck has a 4% reduction in fuel consumption. 20<br />

19 Al-Qadi, Imad L., Pyeong J. Yoo, and Mostafa A. Elseifi. “Characterization <strong>of</strong> Pavement Damage Due to<br />

Different Tire Configurations.” Journal <strong>of</strong> <strong>the</strong> Association <strong>of</strong> Asphalt Paving Technologists. (March 7-9,<br />

2005).<br />

20 (Markstaller et al., 2000)


23<br />

The tire-pavement contact area is ano<strong>the</strong>r concern when considering pavement<br />

<strong>analysis</strong>. In <strong>the</strong> last decade, a series <strong>of</strong> sophisticated measuring systems have been<br />

developed to measure <strong>the</strong>se tire-pavement contact stresses. 21<br />

It has been found that tirepavement<br />

stress distribution is significantly affected by tire inflation pressure, tire type,<br />

and tire load. Figure 21 depicts different pressure distributions from different tires and<br />

Figure 22 shows different tire-pavement contact areas. Different tires have different<br />

contact areas on <strong>the</strong> pavement, requiring sophisticated instrumentation to measure and,<br />

consequently, to apply <strong>the</strong>m. In this study, tire-pavement contact area and tire pressure<br />

are not treated as variables, as this is a subject to be incorporated in 3D <strong>finite</strong> <strong>element</strong>s.<br />

Papers by Blab and Harvey, 2002; Hua and White, 2002; Greer and Palazotto, 1998;<br />

Blackman, Halliday, and Merrill, 2000; Huhtala, Pihlajamaki and Pienimaki, 1989<br />

provide comprehensive studies <strong>of</strong> tire pressure distribution, tire contact area.<br />

Figure 21: Measured tire pressure distribution. Courtesy Tekscan, Inc.<br />

21 See (Siddharthan, 2002)


24<br />

Figure 22: Tire footprints – Hua and White, 2002<br />

Pavement Design<br />

The primary goal <strong>of</strong> pavement engineering is to predict pavement performance. In<br />

<strong>the</strong> past, pavement design was almost totally driven by empirical relationships based on<br />

long-term experience and field tests, such as <strong>the</strong> American Association <strong>of</strong> State Highway<br />

and Transportation Officials (AASHTO) Road Test. These procedures, however, are<br />

applicable only to similar load conditions (tire types and tire pressures), pavement<br />

materials, and environment, making this model very limited. It would require a large<br />

number <strong>of</strong> empirically-based models to predict <strong>the</strong> roadway performance for each<br />

different road structure subjected to variable traffic loads.<br />

To overcome <strong>the</strong> limitations <strong>of</strong> <strong>the</strong> empirical methods, mechanistic procedures<br />

were introduced, allowing pavement engineers to undertake design at a site taking into<br />

consideration loading, materials and environmental conditions, o<strong>the</strong>r than at <strong>the</strong> road test<br />

sites. Such procedures provide <strong>the</strong> pavement response in terms <strong>of</strong> stress, strains, and<br />

displacements in a multilayer pavement system when subjected to a vehicle load. In<br />

1943, solutions for a two-layered system were developed by Burmister and <strong>the</strong>n extended


25<br />

to three-layered systems and <strong>the</strong>n multiple-layered systems by 1945. 22<br />

Burmister’s<br />

<strong>the</strong>ory can be applied to a system with any arbitrary number <strong>of</strong> layers with <strong>the</strong> help <strong>of</strong><br />

computers. This <strong>the</strong>ory is <strong>the</strong> first analytical solution to calculate layered systems<br />

response.<br />

Phenomenological-empirical methods, developed in <strong>the</strong> 1950’s, are <strong>the</strong> basis for<br />

most pavement design procedures that use <strong>the</strong> AASHTO method <strong>of</strong> axle load equivalency<br />

factor. 23 This design method is used to convert mixed traffic axle loads into standard (18-<br />

kip) equivalent single axle loads (ESALs) and is based on <strong>the</strong> total number <strong>of</strong> passes <strong>of</strong><br />

an equivalent axle load factor during <strong>the</strong> design period. 24<br />

Many load equivalency factors<br />

have been proposed in <strong>the</strong> past, based on pavement response to load (deflection, stress,<br />

strain) or distress manifestations (rutting, fatigue, cracking), however, <strong>the</strong> AASHTO load<br />

equivalency factor are <strong>the</strong> most widely used conversions in <strong>the</strong> world. Some researchers<br />

and agencies advocate <strong>the</strong> mechanistic approach, in which LEFs are defined in terms <strong>of</strong><br />

pavement response to load such as stress or strain 25 . O<strong>the</strong>rs prefer empirical models (such<br />

as AASHTO), in which LEFs are subjectively defined in terms <strong>of</strong> user acceptance <strong>of</strong> <strong>the</strong><br />

pavement ride quality and fatigue or distress manifestations (See Huhtala, 1992 and<br />

Southgate 91).<br />

In 1995, Hajek conducted a study that proposed a general axle load equivalency<br />

factors – LEFs, that are independent <strong>of</strong> pavement variables. Such LEFs are valid based on<br />

22 Burmister, D. M. (1945). "The General Theory <strong>of</strong> Stresses and Displacements in Layered Soil Systems,"<br />

Journal <strong>of</strong> Applied Physics, Vol. 16, pp. 84-94, 126- 127,296-302.<br />

23 Helwany, Sam, John Dyer Joe Leidy. “Finite-Element Analyses <strong>of</strong> Flexible Pavements.” Journal <strong>of</strong><br />

Transportation Engineering. Volume 124, Issue 5 (September/October 1998): 491-499.<br />

24 AASHTO - American Association <strong>of</strong> State Highway and Transportation Officials. AASHTO Guide for<br />

design <strong>of</strong> Pavements Structures. Washington, D.C. 1993.<br />

25 See (Southgate 1993; Ioannides 1991; Ioannides 1993; Papagiannakis 1990)


26<br />

<strong>the</strong> argument that uncertainties resulting from traffic volume variables and projections are<br />

much larger than those inherent to LEF estimates.<br />

The methods <strong>of</strong> equivalency factor can be empirical or mechanistic and although<br />

mechanistic based, <strong>the</strong>se methods used elastic material constitutive <strong>the</strong>ory and assume no<br />

induced damage or healing during loading and unloading. 26 Many recent pavement<br />

<strong>analysis</strong> procedures such as <strong>the</strong> SHRP Superpave use <strong>the</strong> pavement response as an input.<br />

In order to design a pavement based on a mechanistic approach it is necessary to<br />

use a structural <strong>analysis</strong> tool or computer program to predict <strong>the</strong> stress-strain response.<br />

Computer programs based on <strong>the</strong> multilayered elasticity method (MLE) have been<br />

developed and are widely used for structural <strong>analysis</strong> <strong>of</strong> asphalt pavements because <strong>of</strong><br />

<strong>the</strong>ir simplicity, but <strong>the</strong>y <strong>of</strong>ten simplify <strong>the</strong> problem, making it unrealistic. The success <strong>of</strong><br />

<strong>the</strong> mechanistic approach mainly depends on how realistically it can model <strong>the</strong> pavement<br />

materials behavior and tire-pavement interaction loading. As a result <strong>of</strong> introducing more<br />

realistic variables, such as inelastic material behavior, as well as complex geometries and<br />

loading conditions, <strong>the</strong> analytical solution for this problem is extremely difficult if not<br />

impossible. Thus, numerical techniques are needed to solve it. Currently, <strong>the</strong> most<br />

commonly used technique is <strong>the</strong> Finite Element Method (FEM), which is a method for<br />

solving partial differential equations governing <strong>the</strong> response <strong>of</strong> objects with complicated<br />

geometries and boundary conditions. 27<br />

Chen’s review and evaluation <strong>of</strong> five computer<br />

programs, including <strong>finite</strong> <strong>element</strong> and MLE programs, sought to establish <strong>the</strong> most<br />

appropriate one for pavement structural <strong>analysis</strong>. 28 He showed that <strong>the</strong> results from<br />

26 See (Ber<strong>the</strong>lot, C.F., 1998)<br />

27 See (Allen, David H., and Walter Haisler, 1985).<br />

28 Chen D.H., M. Zaman, J. Laguros, and A. Soltani. “Assessment <strong>of</strong> computer programs for <strong>analysis</strong> <strong>of</strong><br />

flexible pavement structure.” Transportation Research Record. TRB, 1482:123-133 (1995).


27<br />

ABAQUS program, a commercial <strong>finite</strong> <strong>element</strong> modeling program that has been widely<br />

applied for pavement <strong>analysis</strong> were comparable to those from o<strong>the</strong>r programs.<br />

Programs like ELSYM5 and BISAR also make unrealistic assumptions; <strong>the</strong>y treat<br />

<strong>the</strong> tire interaction as static, uniform and stationary circular load. Papagiannakis 29 and<br />

Sousa 30 attempted to model loadings more realistically; however, <strong>the</strong>se models still suffer<br />

limitations. Siddharthan proposed a continuum-based <strong>finite</strong>-layer model to evaluate<br />

pavement response, incorporating factors such as noncircular contact area, <strong>viscoelastic</strong><br />

material characterization and vehicle speed. 31 They document important pavement<br />

response parameters generated from <strong>the</strong> <strong>finite</strong>-layer analytical model, 3D-moving load<br />

<strong>analysis</strong>, under a variety <strong>of</strong> loading conditions. The loading conditions include two types<br />

<strong>of</strong> tires (conventional and wide base) and different contact stress distributions (uniform<br />

and nonuniform). These studies also reveal that <strong>the</strong>re is a significant difference between<br />

<strong>the</strong> responses computed with uniform (conventional assumption) and nonuniform contact<br />

tire-pavement stress distributions. Finite <strong>element</strong> <strong>analysis</strong> <strong>of</strong> pavements is a well-studied<br />

topic and references can be found in a simple literature review. 32<br />

For a model to be realistic it must consider all major effects that influence <strong>the</strong><br />

materials response. Additional effects can also contribute to <strong>the</strong> pavement performance<br />

and may be used as inputs in <strong>the</strong> model, such as temperature, 33 or moisture and aging <strong>of</strong><br />

29 Papagiannakis, A.T., N. Amoah, R. Taha. “Formulation for Viscoelastic Response <strong>of</strong> Pavements under<br />

Moving Dynamic Loads.” Journal <strong>of</strong> Transportation Engineering. Vol. 122, No. 2 (March/April 1996):<br />

140-145.<br />

30 Sousa, J. B, J. Lysmer, S. S. Chen, and C. L. Monismith. “Effects <strong>of</strong> Dynamic Loads on Performance <strong>of</strong><br />

Asphalt Concrete Pavements.” Transportation Research Record 1207. National Research Council. (1988).<br />

31 Siddharthan, R.V., Krishnamenon, N., and Sebaaly, P.E. “Pavement Response Evaluation using Finite-<br />

Layer Approach.” Transportation Research Record. No. 1709 (2000): 43-49; Siddharthan, Raj V.<br />

“Pavement Strain from Moving Dynamic 3D Load Distribution.” Journal <strong>of</strong> Transportation Engineering.<br />

Volume 124, Number 6 (November 1998).<br />

32 See (Mun, 2003; wang, 2001; Helwany, 1998; Erkens, Liu and Scarpas, 2002)<br />

33 See (Park, Sun Woo and Y. Richard Kim, 1998)


28<br />

<strong>the</strong> asphalt layer. 34 The long term response <strong>of</strong> a pavement involves reduction in stiffness<br />

<strong>of</strong> <strong>the</strong> asphalt material throughout <strong>the</strong> life <strong>of</strong> <strong>the</strong> pavement. Collop shows that an<br />

exponential relationship exists between <strong>the</strong> reduction in asphalt layer stiffness and<br />

cumulative fatigue damage. 35<br />

In a separate study, Harvey addressed one aspect <strong>of</strong> <strong>the</strong><br />

performance <strong>of</strong> asphalt concrete pavements—rutting <strong>of</strong> <strong>the</strong> asphalt mix under high<br />

temperature loading conditions for both highway and airfield pavements. 36<br />

Erik showed<br />

that <strong>the</strong> effect <strong>of</strong> climate on pavement structures is a major contributor to pavement<br />

deterioration in cold regions, caused by seasonal freezing and thawing. 37<br />

Although <strong>the</strong>se studies have advanced <strong>the</strong> general knowledge <strong>of</strong> pavement design,<br />

a more accurate characterization <strong>of</strong> paving material is essential in order to develop a<br />

comprehensive model. A time-domain model for <strong>the</strong> <strong>viscoelastic</strong> pavement response<br />

under dynamic load should be developed, taking into account <strong>the</strong> time-dependency <strong>of</strong> <strong>the</strong><br />

load-frequency and material behavior, including <strong>the</strong> stress-strain-time constitutive law.<br />

By designing a roadway without time effects, <strong>the</strong> main evaluation mechanisms <strong>of</strong><br />

structural performance are disregarded and <strong>the</strong> energy dissipated due to loading and<br />

unloading during <strong>the</strong> years <strong>of</strong> service will not be counted. In addition, dynamic vehiclepavement<br />

interaction effects are well known to be significant for <strong>the</strong> <strong>analysis</strong> <strong>of</strong> dynamic<br />

response <strong>of</strong> pavement subjected to moving loads. 38 Computing pavement response using<br />

34 See (Krishnan, J. Murali, and K.R. Rajagopal, 2005)<br />

35 Collop, A. C. “Stiffness Reductions <strong>of</strong> Flexible Pavements due to Cumulative Fatigue Damage.” Journal<br />

<strong>of</strong> Transportation Engineering. Volume 122, Number 2 (March 1996): 131-139.<br />

36 Harvey, J.T., T.P. Hoover, N.F. Coetzee and C.L. Monismith. "Rutting Evaluation <strong>of</strong> Asphalt Pavements<br />

Using Full-Scale Accelerated Load and Laboratory Performance Tests," 2002 FAA Airport Technology<br />

Transfer Conference. (May 2002).<br />

37 Simonsen, Erik. “Prediction <strong>of</strong> Pavement Response during Freezing and Thawing Using Finite Element<br />

Approach.” Journal <strong>of</strong> Cold Regions Engineering. Volume 11, Number 4 (December 1997): 308-324.;<br />

Simonsen, Erik. “Prediction <strong>of</strong> Temperature and Moisture Changes in Pavement Structures.” Journal <strong>of</strong><br />

Cold Regions Engineering. Volume 11, Number 4 (December 1997): 291-307.<br />

38 See (Wu, Chih-Ping, 1996).


29<br />

dynamic models provides more accurate field measurements than those computed using<br />

static models. 39<br />

Research Objective<br />

The objective <strong>of</strong> <strong>the</strong> present research project is to develop a model for predicting<br />

mechanical behavior and performance life <strong>of</strong> pavements by focusing on tire<br />

configurations and also including loading configurations, layer geometry, and material<br />

properties. Based on <strong>the</strong> test results, <strong>the</strong> model is utilized to predict which pavement<br />

configuration <strong>of</strong>fers <strong>the</strong> greater life. These results play a fundamental role in pavement<br />

design as <strong>the</strong>y provide important information about pavement service life. For example,<br />

by using a certain mixture A, pavement life will be reduced by X number <strong>of</strong> years,<br />

compared against <strong>the</strong> use <strong>of</strong> a certain mixture B. It also can be used to compare pavement<br />

life by applying a truck load with dual tires or a truck load with wide-base tires. In this<br />

particular case, it can be shown that by using one specific set <strong>of</strong> tires in opposition to <strong>the</strong><br />

o<strong>the</strong>r, <strong>the</strong> pavement life will be reduced. Various types <strong>of</strong> results are possible with this<br />

model that will be useful in selecting materials and designing pavement structures with<br />

improved performance.<br />

This model also employs nonlinear inelastic <strong>finite</strong> <strong>element</strong> methods to layered<br />

structures <strong>of</strong> pavements. Computational results for various tire loading conditions are also<br />

investigated to monitor <strong>the</strong> impact <strong>of</strong> loading conditions on pavement failure and life.<br />

Fur<strong>the</strong>rmore, <strong>the</strong> influence <strong>of</strong> layer thickness <strong>of</strong> pavement structure and <strong>the</strong> variation <strong>of</strong><br />

pavement material properties are also evaluated.<br />

39 See (Mamlouk, Michael S., 1997)


30<br />

In order to fully develop <strong>the</strong> potential <strong>of</strong> this model, <strong>the</strong> next section will<br />

formulate <strong>the</strong> statement <strong>of</strong> <strong>the</strong> problem. Then, all <strong>the</strong> variables involved in <strong>the</strong> <strong>analysis</strong><br />

will be described and <strong>the</strong> governing field equations will be stated, based on <strong>the</strong><br />

continuum <strong>mechanics</strong> approach. The 2D problem here is composed <strong>of</strong> a linear<br />

<strong>viscoelastic</strong> layer (asphalt concrete) and three elastic layers (sub-grade, sub-base and<br />

base), constituting <strong>the</strong> initial boundary value problem (IBVP). Subsequently, <strong>the</strong> <strong>finite</strong><br />

<strong>element</strong> formulation will be posed and finally <strong>the</strong> results from this <strong>analysis</strong> will be<br />

shown.


31<br />

CHAPTER 2<br />

Solution Method<br />

Complex geometry and mixed boundary conditions with heterogeneous and nonelastic<br />

materials are normally present in roadway problems, making <strong>the</strong> solution<br />

sometimes only feasible by numerical computation. The problem to be solved in this<br />

research may be described as a linear, two-dimensional, quasistatic initial boundary value<br />

problem (IBVP). It can be considered quasistatic since <strong>the</strong> cyclic motion <strong>of</strong> vehicles on<br />

<strong>the</strong> roadway is not enough to reach <strong>the</strong> fundamental frequency <strong>of</strong> <strong>the</strong> pavement, or <strong>the</strong><br />

lowest frequency at which <strong>the</strong> pavement can vibrate. Also, even though we are treating<br />

with a 2-D problem, a more general case <strong>of</strong> a three dimensional domain will be<br />

presented.<br />

In developing <strong>the</strong> solution technique, I will first describe <strong>the</strong> complete problem<br />

statement with all <strong>the</strong> variables involved in <strong>the</strong> <strong>analysis</strong> and <strong>the</strong> governing field<br />

equations. This formulation follows a continuum <strong>mechanics</strong> approach, where a body is<br />

considered to be a continuum or without any microstructure when analyzed on a small<br />

scale. A number <strong>of</strong> variables are known a priori while o<strong>the</strong>rs need to be determined by<br />

field equations, which are provided by kinetics, kinematics, and material constitutive<br />

behavior. 40 A concise formulation is shown here, similar to that found in most continuum<br />

<strong>mechanics</strong> textbooks. 41<br />

40 Kinetics is a field <strong>of</strong> <strong>mechanics</strong> that studies loads on a body relating force and mass. Kinematics is <strong>the</strong><br />

field that considers motions <strong>of</strong> bodies without regard to force and mass. The material constitutive equations<br />

are used to relate kinetics and kinematics and provide additional equations to complete <strong>the</strong> statement <strong>of</strong> a<br />

well posed problem.<br />

41 (Malvern, 1969).


32<br />

Consider a general three dimensional body Ω and its boundary∂Ω as shown in<br />

Figure 23. Consider a small volume ∆Ω from this body, where:<br />

∂Ω<br />

∪ ∂Ω =∂Ω<br />

(2.1)<br />

1 2<br />

∂Ω1∩ ∂Ω<br />

2<br />

=∅<br />

(2.2)<br />

Boundary ∂Ω<br />

1<br />

is subjected to known tractions (natural boundary conditions) and<br />

boundary ∂Ω 2 is subjected to known displacements (essential boundary conditions).<br />

To solve <strong>the</strong> IBVP we need to derive <strong>the</strong> governing equations from <strong>the</strong> kinetics<br />

equations (conservation <strong>of</strong> mass, conservation <strong>of</strong> linear and angular momentum),<br />

kinematics equations (strain-displacement) and constitutive equations. Additional<br />

constraints can be obtained from <strong>the</strong> boundary conditions and initial conditions. The<br />

standard summation convention and range convention are observed in <strong>the</strong> equations<br />

shown below.


33<br />

Figure 23: General three dimensional body<br />

The purpose <strong>of</strong> solving an IBVP is to know how <strong>the</strong> body will deform with a load<br />

applied on it. These mechanical responses are given in terms <strong>of</strong> stresses, strains and<br />

displacements at each point <strong>of</strong> <strong>the</strong> body. Those variables, known as state or field<br />

variables, may be functions <strong>of</strong> space and time and are represented by <strong>the</strong> stress tensor<br />

σ ( x <br />

<br />

, t)<br />

, strain tensor ε ij<br />

( x, t)<br />

and displacement vector u ( x, t)<br />

. Twenty-one unknown<br />

ij<br />

i


34<br />

variables are identified, consequently making necessary <strong>the</strong> same number <strong>of</strong> field<br />

equations to solve <strong>the</strong> problem.<br />

The global statement <strong>of</strong> conservation <strong>of</strong> linear momentum is given by three parts:<br />

<strong>the</strong> rate <strong>of</strong> addition <strong>of</strong> momentum to region Ω , plus <strong>the</strong> forces acting on region Ω ,<br />

equals <strong>the</strong> rate <strong>of</strong> change <strong>of</strong> momentum in region Ω . Or it can be expressed by:<br />

∂ <br />

−∫ ρvv ( ⋅ ndS ) + ∫ tdS+ ∫ρ fdΩ= ∫ ( ρvd<br />

) Ω<br />

∂t<br />

∂Ω ∂Ω Ω Ω<br />

(2.3)<br />

where v is <strong>the</strong> velocity vector, ρ is <strong>the</strong> density, n is <strong>the</strong> unit outer normal, t is traction<br />

applied on surface and f is <strong>the</strong> body force. To obtain a local statement in index notation,<br />

first dot with base vector e i<br />

and apply <strong>the</strong> divergence <strong>the</strong>orem, which gives <strong>the</strong> local<br />

form <strong>of</strong> <strong>the</strong> conservation <strong>of</strong> linear momentum:<br />

dv<br />

σ<br />

ji,<br />

j<br />

ρ f ρ<br />

dt<br />

i<br />

+<br />

i<br />

= (2.4)<br />

where ρ is <strong>the</strong> mass, f<br />

i<br />

is <strong>the</strong> body force per unit area and vi<br />

is <strong>the</strong> velocity vector and<br />

d<br />

dt<br />

is relative to material derivative. It was noted before that <strong>the</strong> quasistatic conditions<br />

apply in this research, meaning <strong>the</strong> cyclic loads are applied slowly compared to <strong>the</strong><br />

fundamental frequency <strong>of</strong> <strong>the</strong> pavement. As a result, <strong>the</strong> dynamic effects <strong>of</strong> <strong>the</strong><br />

acceleration are negligible and can be eliminated<br />

σ + ρ f = (2.5)<br />

ji, j i<br />

0<br />

Conservation <strong>of</strong> angular momentum must be satisfied at all points in a body or <strong>the</strong><br />

rate <strong>of</strong> change <strong>of</strong> angular momentum crossing boundary <strong>of</strong> region Ω plus moments<br />

applied to region Ω must equal <strong>the</strong> rate <strong>of</strong> change <strong>of</strong> angular momentum in region Ω .


35<br />

Satisfying <strong>the</strong> conservation <strong>of</strong> angular momentum assures equilibrium <strong>of</strong> <strong>the</strong> body. The<br />

general form <strong>of</strong> <strong>the</strong> conservation <strong>of</strong> angular momentum is given by:<br />

e<br />

σ + ρm<br />

= 0<br />

(2.6)<br />

ijk ij k<br />

where eijk<br />

is <strong>the</strong> permutation symbol and ρmk<br />

is body moment. If no body moments are<br />

assumed, <strong>the</strong> conservation <strong>of</strong> angular momentum reduces to:<br />

σ = σ<br />

(2.7)<br />

ij<br />

ji<br />

stating that <strong>the</strong> stress tensor is symmetric, 42 reducing <strong>the</strong> number <strong>of</strong> unknown stresses<br />

from nine to six.<br />

Kinematics constraints are satisfied by <strong>the</strong> strain tensor and it can be expressed in<br />

terms <strong>of</strong> <strong>the</strong> displacement field in a body. This is called <strong>the</strong> strain-displacement tensor<br />

and is given by:<br />

1<br />

ε<br />

ij<br />

= ( ui, j<br />

+ uj, i<br />

− uk , iuk , j )<br />

(2.8)<br />

2<br />

When <strong>the</strong> displacement is in<strong>finite</strong>simal, or no large deformation is considered, <strong>the</strong><br />

term uki<br />

,<br />

uk,<br />

jcan be neglected. As a result, <strong>the</strong> strain tensor becomes <strong>the</strong> in<strong>finite</strong>simal<br />

linear strain tensor:<br />

1<br />

ε<br />

ij<br />

= ( ui, j<br />

+ uj,<br />

i )<br />

(2.9)<br />

2<br />

The in<strong>finite</strong>simal tensor is symmetric by simple observation, reducing <strong>the</strong> number<br />

<strong>of</strong> strain unknowns from nine to six.<br />

A material is said to possess <strong>viscoelastic</strong> behavior when <strong>the</strong> stress is a single value<br />

function <strong>of</strong> <strong>the</strong> entire history <strong>of</strong> <strong>the</strong> strain. Thus, ma<strong>the</strong>matically,<br />

42 (Malvern,1969)


36<br />

τ<br />

σ () t = σ ε( = t<br />

τ )<br />

(2.10)<br />

{ }<br />

τ =−∞<br />

where braces denote history dependence.<br />

Asphalt concrete is a material that exhibits <strong>viscoelastic</strong> mechanical behavior; thus,<br />

<strong>the</strong> material constitutive equations are given for a general orthotropic, linear <strong>viscoelastic</strong><br />

material and can be expressed in hereditary integral form or convolution integral:<br />

t<br />

<br />

<br />

∂εkl<br />

( xk<br />

, τ)<br />

σ ( x , t) = ∫ C ( t−τ)<br />

dτ<br />

∂τ<br />

ij k ijkl<br />

0<br />

t<br />

<br />

<br />

∂σkl<br />

( xk<br />

, τ)<br />

ε ( x , t) = ∫ D ( t−τ)<br />

dτ<br />

∂τ<br />

ij k ijkl<br />

0<br />

(2.11)<br />

(2.12)<br />

where:<br />

C ( t− τ ) is <strong>the</strong> fourth order tensor <strong>of</strong> relaxation moduli, relating stress to strain,<br />

ijkl<br />

D ( t− τ ) is <strong>the</strong> fourth order tensor <strong>of</strong> creep compliances, relating strain to stress.<br />

ijkl<br />

Constraints imposed by boundary conditions can be applied on <strong>the</strong> body as natural<br />

(Neumann) or essential (Dirichlet). The first case refers to traction applied on <strong>the</strong><br />

boundary and is given by:<br />

<br />

t ( x, t ) = known on ∂Ω<br />

i<br />

<br />

t ( x, t)<br />

= σ n<br />

i ji j<br />

1<br />

(2.13)<br />

(2.14)<br />

where t i<br />

is <strong>the</strong> traction per unit area on <strong>the</strong> surface and n<br />

j<br />

is <strong>the</strong> unit outer normal. The<br />

second one is when displacement is applied. Essential boundary conditions are given by:<br />

<br />

u ( x, t ) = known on ∂Ω<br />

(2.15)<br />

where ui<br />

are displacements known a priori on <strong>the</strong> surface.<br />

The initial conditions are:<br />

i<br />

2


37<br />

<br />

σ<br />

ij<br />

( xt , ) = 0⎫ ⎪ <br />

εij<br />

( xt , ) = 0 ⎬ ∀xinΩ+∂Ω<br />

<br />

ui<br />

( x, t) = 0 ⎪ ⎭<br />

(2.16)<br />

The above problem introduces all <strong>the</strong> unknown variables and equations, providing<br />

<strong>the</strong> solution to <strong>the</strong> IBVP. Our goal is to find σ ( x <br />

, t)<br />

, u ( x, t)<br />

and ε ij<br />

( x, t)<br />

. The equations<br />

provided are given by Equation (2.5), Equation (2.9), and Equation (2.11) with<br />

constraints imposed by boundary conditions in Equation (2.13) and Equation (2.15) and<br />

initial conditions Equation (2.16).<br />

ij<br />

i


38<br />

CHAPTER 3<br />

Finite Element Formulation<br />

After formulating a brief statement <strong>of</strong> <strong>the</strong> IBVP, it is necessary to develop <strong>the</strong><br />

method for obtaining a numerical solution.<br />

Incrementalization <strong>of</strong> <strong>the</strong> Constitutive Equations<br />

The constitutive equation for a linear <strong>viscoelastic</strong> material is shown in Equation<br />

(2.11). This equation cannot be implemented into <strong>the</strong> <strong>finite</strong> <strong>element</strong> formulation in <strong>the</strong><br />

integral form; <strong>the</strong>refore, a numerical incrementalization is necessary. Equation (2.11) is<br />

restated here:<br />

t<br />

<br />

<br />

∂εkl<br />

( xk<br />

, τ)<br />

σ ( x , t) = ∫ C ( t−τ)<br />

dτ<br />

∂τ<br />

ij k ijkl<br />

0<br />

(3.1)<br />

where<br />

Cijkl<br />

is <strong>the</strong> fourth order tensor <strong>of</strong> relaxation moduli relating stress to strain. The<br />

procedure described here was developed by Zocher, Groves and Allen, 1995 and it is<br />

shown in a concise form. In fact, in <strong>the</strong> original method developed by Zocher, Groves and<br />

Allen, <strong>the</strong>rmo<strong>viscoelastic</strong>ity was considered differently from this research where<br />

temperature terms are not included.<br />

They subdivided <strong>the</strong> timeline into discrete intervals, such that tn+ 1<br />

= tn<br />

+∆ t, where<br />

t +<br />

corresponds to current time plus <strong>the</strong> time step. Also, <strong>the</strong> stress at current time is<br />

n 1<br />

assumed to be known. The goal is to express stress at t<br />

n + 1<br />

in a way suitable for an<br />

incremental <strong>finite</strong> <strong>element</strong> formulation. Rewriting Equation (3.1), representing <strong>the</strong> state<br />

<strong>of</strong> stress at time t<br />

n + 1<br />

, becomes:


39<br />

<br />

<br />

σ x t C t τ dτ C t τ dτ<br />

tn<br />

tn+<br />

1<br />

∂εkl<br />

( x, τ) ∂εkl<br />

( x, τ)<br />

ij<br />

( ,<br />

n+ 1) = ∫ ijkl<br />

(<br />

n+ 1− ) +<br />

ijkl<br />

(<br />

n+<br />

1−<br />

)<br />

∂τ<br />

∫<br />

∂τ<br />

0<br />

tn<br />

(3.2)<br />

Let us define<br />

∆ Cijkl<br />

as follows:<br />

∆C ≡C ( t −τ<br />

) −C ( t − τ )<br />

(3.3)<br />

ijkl ijkl n+<br />

1<br />

ijkl n<br />

Substituting Equation (3.3) in Equation (3.2), becomes:<br />

<br />

∆ σ = − τ τ +∆σ<br />

tn+<br />

1<br />

∂εkl<br />

( x, τ)<br />

R<br />

ij ∫ Cijkl ( tn+<br />

1<br />

) d<br />

ij<br />

∂τ<br />

tn<br />

(3.4)<br />

where<br />

R<br />

ij<br />

t n<br />

∫<br />

∆ σ = ∆C<br />

0<br />

ijkl<br />

<br />

∂εkl<br />

( x, τ)<br />

dτ<br />

∂τ<br />

(3.5)<br />

And<br />

∆σ<br />

ji<br />

is defined to be:<br />

∆σ ≡σ − σ<br />

(3.6)<br />

t+∆t t<br />

ji ji ji<br />

Now, considering that each <strong>element</strong> <strong>of</strong><br />

Cijkl<br />

can be represented by <strong>the</strong> Wiechert model:<br />

Mijkl<br />

ijkl<br />

C () t = C +∑ C e ρ m<br />

(3.7)<br />

ijkl ijkl∞<br />

ijklm<br />

m=<br />

1<br />

−<br />

t<br />

where<br />

η<br />

ρ = (with no sum on i, j, k and l) and<br />

ijklm<br />

ijklm<br />

C ijkl m<br />

ηijkl m<br />

are <strong>the</strong> dashpots coefficients<br />

and<br />

Cijkl<br />

are <strong>the</strong> spring constants.<br />

ρijkl m<br />

is referred as <strong>the</strong> relaxation time.<br />

Also, suppose ε ( t, τ ) can be approximated over <strong>the</strong> interval t ≤τ ≤t<br />

+ 1<br />

by:<br />

kl<br />

ε (, t τ) = ε + ε ι× ( t− t ) × H( t−t<br />

)<br />

(3.8)<br />

kl kln<br />

kl n n<br />

where ε<br />

kl<br />

is a constant representing <strong>the</strong> time rate <strong>of</strong> change over <strong>the</strong> interval, Ht ( − t n<br />

) is<br />

<strong>the</strong> Heaviside step function and <strong>the</strong> symbol “×” represents a multiplication.<br />

Substituting Equation (3.3) in Equation (3.2), results in:<br />

n<br />

n


40<br />

∆ σ = C ∆ ε +∆ σ<br />

(3.9)<br />

'<br />

R<br />

ij ijkl kl ij<br />

where,<br />

C<br />

Mijkl<br />

' 1<br />

ijkl<br />

= Cijkl + η<br />

∞<br />

ijkl<br />

t<br />

m<br />

m=<br />

1<br />

∆t<br />

−<br />

( ρijkl m )<br />

∑ (3.10)<br />

∆ 1−<br />

e<br />

∆ ε = ∆<br />

(3.11)<br />

kl<br />

ε<br />

kl<br />

t<br />

The final steps in <strong>the</strong> incrementalization <strong>of</strong> <strong>the</strong> constitutive equation involve writing an<br />

expression for<br />

where,<br />

R<br />

∆σ ij<br />

in a convenient form. Only <strong>the</strong> final equations are shown here:<br />

∆t<br />

−<br />

( ijkl m )<br />

Mijkl<br />

R<br />

ij<br />

Sijkl 1<br />

m<br />

tn<br />

− e ρ<br />

m=<br />

1<br />

∆ σ =−∑ ( )<br />

(3.12)<br />

ijkl m n ijkl m<br />

0<br />

t<br />

tn<br />

−τ<br />

−<br />

( ρijkl m )<br />

n<br />

∂εkl<br />

( x, τ)<br />

S ( t ) ≡ ∫ C dτ<br />

(3.13)<br />

e ∂τ<br />

Now <strong>the</strong> constitutive equation can be implemented to an incremental formulation.<br />

The approach shown here is a brief review; a more complete and detailed formulation is<br />

detailed by Zocher et al. 1995.<br />

Method <strong>of</strong> Weight Residuals<br />

A <strong>finite</strong> <strong>element</strong> formulation can be found in open literature such as Yang, 1986;<br />

Reddy, 1993; Hughes, 1987; Zienkiewicz, 1971. The methodology shown here is a<br />

concise formulation and it is introduced by integrating <strong>the</strong> conservation <strong>of</strong> linear<br />

momentum over <strong>the</strong> volume against a test function v<br />

i<br />

. The governing differential<br />

equation treated herein is specified by Equation (2.5), transforming it to integral form<br />

gives


41<br />

∫ ( σ<br />

ji,<br />

j<br />

+ ρ fi ) vdV<br />

i<br />

= 0<br />

(3.14)<br />

Ωi<br />

where<br />

Ω<br />

i<br />

is <strong>the</strong> sub domain and vi<br />

is a weight function or any arbitrary admissible<br />

displacement vector. Equation (3.14) can be rewritten as:<br />

∫ ( σ<br />

jivi ), j<br />

− σ<br />

jivi,<br />

j<br />

+ ρ fvdV<br />

i i<br />

= 0<br />

(3.15)<br />

Ωi<br />

by applying <strong>the</strong> relations in <strong>the</strong> equation above<br />

( σ v ) = σ v + σ v<br />

ji i , j ji, j i ji i,<br />

j<br />

σ v = ( σ v ) −σ<br />

v<br />

ji, j i ji i , j ji i,<br />

j<br />

or<br />

∫( σ v ) dV − ∫σ v dV + ∫ ρ f v dV = 0<br />

(3.16)<br />

ji i , j ji i,<br />

j i i<br />

Ωi Ωi Ωi<br />

Now, applying Gauss divergence <strong>the</strong>orem, Equation (3.16) can be rewritten as:<br />

∫ ∫ ∫ (3.17)<br />

σ<br />

jivn i jdV− σ<br />

jivi , jdV+ ρ fvdV<br />

i i<br />

= 0<br />

∂Ωi Ωi Ωi<br />

or<br />

∫σ v dV = ∫ σ vn dV + ∫ ρ fvdV<br />

(3.18)<br />

ji i,<br />

j ji i j i i<br />

Ωi ∂Ωi Ωi<br />

where, n<br />

j<br />

is <strong>the</strong> unit outer normal. Inserting Cauchy’s Formula (Equation (2.14)),<br />

Equation (3.18) can be rewritten as:<br />

∫σ<br />

v dV = ∫ tvdV+<br />

∫ ρ fvdV<br />

(3.19)<br />

ji i,<br />

j i i i i<br />

Ωi ∂Ωi Ωi<br />

Note:


42<br />

1 1<br />

σ<br />

jivi , j<br />

= σ<br />

ji[ ( vi, j<br />

+ vj, i<br />

) + ( vi, j<br />

−vj,<br />

i<br />

)]<br />

2 2<br />

σ v = σ [ ε + ϖ ]<br />

ji i,<br />

j ji ij ij<br />

where ϖ<br />

ij<br />

is <strong>the</strong> linear rotation tensor and σ<br />

jiϖ ij<br />

is <strong>the</strong> product <strong>of</strong> a symmetric and skewsymmetric<br />

tensors, which results in zero, so:<br />

σ v<br />

= σ ε<br />

(3.20)<br />

ji i,<br />

j ji ij<br />

Now inputting Equation (3.20) in Equation (3.19), gives:<br />

∫σ ε dV = ∫ t v dS + ∫ ρ f v dV<br />

(3.21)<br />

ji ij i i i i<br />

Ωi ∂Ωi Ωi<br />

If we add <strong>the</strong> traction boundary conditions applied on boundary ∂Ω<br />

2<br />

, Equation (3.21)<br />

becomes:<br />

∫σ ε dV = ∫ t v dS + ∫ ρ f v dV<br />

(3.22)<br />

ji ij i i i i<br />

Ω ∂Ω2<br />

Ω<br />

which is <strong>the</strong> principle <strong>of</strong> virtual work.<br />

Up to this point, <strong>the</strong> variable time had not imposed influence on <strong>the</strong> development<br />

and <strong>the</strong> procedure presented is similar for an elastic formulation problem. By introducing<br />

time dependency behavior, Equation (3.22) takes <strong>the</strong> form:<br />

∫σ ε dV = ∫ t v dS + ∫ ρ f v dV<br />

(3.23)<br />

t +∆ t t +∆ t t +∆ t t +∆ t t +∆ t t +∆ t<br />

ji ij i i i i<br />

Ωi ∂Ωi Ωi<br />

where <strong>the</strong> superscript “t<br />

+∆ t” means “at reduced time t+ ∆ t”. It is necessary to<br />

incrementalize Equation (3.23), since <strong>the</strong> stress-strain relations (Equation (3.9)) are<br />

incrementalized. Let us define <strong>the</strong> following relations:


43<br />

∆σ ≡σ −σ<br />

t+∆t t<br />

ji ji ji<br />

∆ε ≡ε −ε<br />

t+∆t t<br />

ij ij ij<br />

∆u ≡u −u<br />

t+∆t t<br />

i i i<br />

∆v ≡v −v<br />

t+∆t t<br />

i i i<br />

(3.24)<br />

or rearranging:<br />

σ = σ +∆σ<br />

t+∆t t<br />

ji ji ji<br />

ε = ε +∆ε<br />

t+∆t t<br />

ij ij ij<br />

u = u +∆u<br />

t+∆t t<br />

i i i<br />

v = v +∆v<br />

t+∆t t<br />

i i i<br />

(3.25)<br />

ε (t) and v ( t)<br />

are zero, as a consequence <strong>of</strong> u ( t)<br />

being known. Now substituting<br />

ij<br />

i<br />

Equations (3.25) in Equation (3.23), yields:<br />

or reorganizing terms:<br />

i<br />

t t+∆ t t+∆t<br />

∫( σ<br />

ji<br />

+∆σ ji)<br />

∆ εijdV = ∫ ti ∆ vidS + ∫ ρ fi ∆vidV<br />

(3.26)<br />

Ωi ∂Ωi Ωi<br />

∫∆σ ∆ ε dV = ∫ t ∆ v dS + ∫ ρ f ∆v dV −∫ σ ∆ε<br />

dV (3.27)<br />

t+∆ t t+∆t t<br />

ji ij i i i i ji ij<br />

Ωi ∂Ωi Ωi Ωi<br />

Introducing Equation (3.9) in Equation (3.27), yields:<br />

∫ C dV ∫ t vdS ∫ f vdV ∫ dV (3.28)<br />

'<br />

R t t t t t<br />

(<br />

ijkl<br />

∆ εkl +∆σij ) ∆ εij = +∆ i<br />

∆<br />

i<br />

+ ρ +∆<br />

i<br />

∆<br />

i<br />

− σ<br />

ji<br />

∆εij<br />

Ωi ∂Ωi Ωi Ωi<br />

Rearranging Equation (3.27), it can be referred to as incremental variational initial<br />

boundary value problem:<br />

∫C ∆ε ∆ ε dV = ∫ t ∆ vdS+ ∫ ρ f ∆vdV−∫σ ∆ε dV−∫ ∆σ ∆ε<br />

dV (3.29)<br />

'<br />

t +∆ t t +∆ t t R<br />

ijkl kl ij i i i i ji ij ij ij<br />

Ωi ∂Ωi Ωi Ωi Ωi<br />

Notice that <strong>the</strong> term<br />

∆εij<br />

is a function <strong>of</strong> vi<br />

and<br />

∆ε<br />

kl<br />

is a function <strong>of</strong> u<br />

i<br />

.


44<br />

Displacement Formulation<br />

Let us now convert <strong>the</strong> problem to a matrix notation that is easily programmed.<br />

Notice that this research is treating a plane strain problem, which considers <strong>the</strong> third<br />

dimension in<strong>finite</strong>ly long. In this notation we could write <strong>the</strong> following matrices:<br />

The change in displacement vector:<br />

⎡∆u⎤<br />

[ ∆ u]<br />

= ⎢<br />

∆v<br />

⎥<br />

⎣ ⎦<br />

(3.30)<br />

The change in strain tensor:<br />

⎡∆ε<br />

⎤<br />

xx<br />

[ ε ]<br />

⎢ ⎥<br />

∆ = ⎢ ∆ε<br />

yy ⎥<br />

⎢ ε ⎥<br />

⎣∆<br />

xy ⎦<br />

(3.31)<br />

The change in stress during<br />

∆ t :<br />

⎡∆σ<br />

⎤<br />

xx<br />

[ σ]<br />

⎢ ⎥<br />

∆ = ⎢ ∆σ<br />

yy ⎥<br />

⎢ σ ⎥<br />

⎣∆<br />

xy ⎦<br />

(3.32)<br />

The stress-strain relationship can be written for a general anisotropic material as:<br />

R<br />

⎧∆σ ⎫<br />

xx ⎡C' 11<br />

C' 12<br />

C'<br />

13 ⎤⎧∆ε ⎫ ⎧<br />

xx<br />

∆σ<br />

⎫<br />

xx<br />

⎪ ⎪ R<br />

σ<br />

⎢<br />

yy<br />

C' 21<br />

C' 22<br />

C'<br />

⎥⎪ ⎪ ⎪ ⎪<br />

⎨∆ ⎬= ⎢<br />

23<br />

⎥⎨∆ εyy ⎬+ ⎨∆σ<br />

yy ⎬<br />

⎪ R<br />

σ ⎪<br />

xy<br />

C' 31<br />

C' 32<br />

C'<br />

⎪<br />

33<br />

γ ⎪ ⎪<br />

xy<br />

σ ⎪<br />

⎩∆ ⎭<br />

⎢⎣<br />

⎥⎦⎩∆ ⎭ ⎩∆<br />

xy ⎭<br />

(3.33)<br />

or in symbolic form:<br />

R<br />

{ σ} [ C ']{ ε} { σ }<br />

The body forces (per unit mass) at reduced time t<br />

∆ = ∆ + ∆ (3.34)<br />

+ ∆ t<br />

⎡ f<br />

⎤<br />

t+∆t<br />

t+∆t<br />

x<br />

⎡⎣f<br />

⎤ ⎦ = ⎢ t+∆t⎥<br />

f<br />

y<br />

⎢⎣<br />

⎥⎦<br />

(3.35)


45<br />

The surface tractions at reduced time t<br />

+ ∆ t<br />

t+∆t<br />

[ ]<br />

t<br />

t+∆t<br />

⎡t<br />

⎤<br />

x<br />

= t+∆t<br />

⎢⎣<br />

ty<br />

⎥⎦<br />

(3.36)<br />

The stresses at reduced time t<br />

t<br />

[ σ ]<br />

t<br />

⎡σ<br />

⎤<br />

xx<br />

⎢ t ⎥<br />

= ⎢ σ<br />

yy ⎥<br />

⎢<br />

t<br />

σ ⎥<br />

⎣ xy ⎦<br />

(3.37)<br />

The terms defined in Equation (3.12)<br />

R<br />

[ ∆ σ ]<br />

R<br />

⎡∆σ<br />

⎤<br />

xx<br />

⎢ R ⎥<br />

= ⎢ ∆σ<br />

yy ⎥<br />

⎢<br />

R<br />

σ ⎥<br />

⎣∆<br />

xy ⎦<br />

(3.38)<br />

The term<br />

∆ and term ∆ε<br />

kl<br />

can be written in matrix form:<br />

εij<br />

1<br />

∆ ε ( [ ][ ]<br />

ij<br />

= ∆ vi , j<br />

+∆vj,<br />

i ) →∆ εij<br />

= B ∆ v<br />

(3.39)<br />

2<br />

1<br />

∆ ε ( [ ][ ]<br />

kl<br />

= ∆ uk , l<br />

+∆ul,<br />

k ) →∆ εkl<br />

= B ∆ u<br />

(3.40)<br />

2<br />

The principle <strong>of</strong> virtual work is in Equation (3.29) may be written as:<br />

∫∆ε C ∆ ε dV = ∫ ∆ vt dS+ ∫∆vρ f dV −∫∆ε σ dV −∫ ∆ε σ dV (3.41)<br />

'<br />

t+∆ t t+∆t t R<br />

ij ijkl kl i i i i ij ji ij ij<br />

Ωi ∂Ωi Ωi Ωi Ωi<br />

The <strong>element</strong> matrices are derived for a triangular T3 <strong>element</strong>. Element T3 is<br />

shown in Figure 24.


46<br />

y<br />

u<br />

3<br />

3<br />

v<br />

3<br />

2<br />

v<br />

2<br />

v<br />

1<br />

1<br />

u<br />

2<br />

u<br />

1<br />

x<br />

Figure 24: T3 triangular <strong>element</strong> representation<br />

For a 3 node <strong>element</strong>, let:<br />

∆uxyt<br />

( , , )<br />

⎡<br />

⎢<br />

i i<br />

⎡ ⎤ i=<br />

1<br />

∆ u = ⎢ ⎥ =⎢ ⎥<br />

3<br />

3<br />

∑<br />

⎤<br />

N ∆u () t ⎥<br />

⎣∆vxyt<br />

( , , ) ⎦ ⎢ ⎥<br />

⎢∑<br />

Ni∆vi()<br />

t ⎥<br />

⎣ i=<br />

1 ⎦<br />

(3.42)<br />

where<br />

Ni<br />

are <strong>the</strong> shape functions. A linear displacement function <strong>of</strong> x and y is assumed<br />

and <strong>the</strong> shape functions can be described as:<br />

where:<br />

Ni = ai + bx<br />

i<br />

+ ciy<br />

(3.43)


47<br />

1<br />

ai = ( xjyk −xkyj<br />

)<br />

2A<br />

1<br />

bi = ( yj − yk<br />

)<br />

2A<br />

1<br />

ci = ( xk −xj<br />

)<br />

2A<br />

(3.44)<br />

where i, j, k are a permutation <strong>of</strong> 1, 2, 3. So, <strong>the</strong> displacements on <strong>the</strong> <strong>element</strong> can be<br />

written as:<br />

e<br />

u uiNi ujN j<br />

ukNk<br />

∆ =∆ +∆ +∆<br />

e<br />

v vN<br />

i i<br />

vjN j<br />

vkNk<br />

∆ =∆ +∆ +∆<br />

(3.45)<br />

can be rewritten as:<br />

[ ][ ]<br />

e e e<br />

∆ u = H ∆ U<br />

(3.46)<br />

where:<br />

0 0 0<br />

e ⎡N N N ⎤<br />

H = ⎢<br />

0 N1 0 N2 0 N ⎥<br />

⎣<br />

3⎦<br />

[ ]<br />

1 2 3<br />

(3.47)<br />

is <strong>the</strong> shape function matrix for <strong>the</strong> <strong>element</strong>, and:<br />

e<br />

[ ]<br />

⎡∆u1<br />

⎤<br />

⎢<br />

v<br />

⎥<br />

⎢<br />

∆<br />

1<br />

⎥<br />

⎢∆u<br />

⎥<br />

2<br />

∆ U =⎢ ⎥<br />

∆v2<br />

⎢ ⎥<br />

⎢∆u<br />

⎥<br />

3<br />

⎢ ⎥<br />

⎢⎣<br />

∆v3<br />

⎥⎦<br />

(3.48)<br />

is <strong>the</strong> nodal displacement matrix. Also,


48<br />

⎡ ∂∆u<br />

⎤<br />

⎢ ⎥<br />

⎡∆ε<br />

⎤<br />

⎢ ∂x<br />

⎥<br />

xx<br />

⎢ ⎥ e e ⎢<br />

[ ][ ]<br />

∂∆v<br />

⎥<br />

∆ ε = ⎢∆ εyy<br />

⎥ = B ∆ U = ⎢<br />

=<br />

∂y<br />

⎥<br />

⎢ γ ⎥<br />

⎢ ⎥<br />

⎣∆<br />

xy ⎦ ⎢∂∆u<br />

∂∆v⎥<br />

⎢ + ⎥<br />

⎣ ∂y<br />

∂x<br />

⎦<br />

∆u<br />

⎡∂N<br />

1<br />

1<br />

∂N2<br />

∂N<br />

⎤⎡ ⎤<br />

3<br />

⎢ 0 0 0 ⎥⎢<br />

x x x v<br />

⎥<br />

∂ ∂ ∂ ⎢ ∆<br />

1<br />

⎥<br />

⎢ ⎥<br />

⎢ ∂ N ∂ N ∂ N ⎥⎢∆<br />

u ⎥<br />

0 0 0<br />

⎢ ∂ ∂ ∂<br />

⎥⎢ ⎥<br />

⎢∂N ∂N ∂N ∂N<br />

∂N<br />

∂N<br />

⎥ ⎢ ∆u<br />

⎥<br />

1 2<br />

3 2<br />

= ⎢<br />

⎥⎢ ⎥<br />

y y y ∆ v2<br />

1 1 2 2 3 3 3<br />

⎢ ⎥⎢ ⎥<br />

⎣ ∂y ∂x ∂y ∂x ∂y ∂x ⎦⎣⎢<br />

∆v3<br />

⎥⎦<br />

(3.49)<br />

or<br />

⎡b 0 b 0 b 0⎤<br />

B c c c<br />

1 2 3<br />

e<br />

=<br />

⎢<br />

0<br />

1<br />

0<br />

2<br />

0<br />

⎥<br />

⎢<br />

3 ⎥<br />

⎢⎣<br />

c1 b1 c2 b2 c3 b ⎥<br />

3⎦<br />

(3.50)<br />

Equation (3.41) can be rewritten in <strong>the</strong> form:<br />

∫<br />

T T T T<br />

e e e e e e<br />

⎡<br />

⎣∆U ⎤<br />

⎦<br />

⎡<br />

⎣B ⎤<br />

⎦<br />

⎡<br />

⎣ C'<br />

⎤⎡<br />

⎦⎣B ⎤⎡<br />

⎦⎣∆ U ⎤<br />

⎦dV = ⎡<br />

⎣∆U ⎤<br />

⎦<br />

⎡<br />

⎣H ⎤<br />

⎦ tdS2<br />

Ωi<br />

∂Ωi<br />

(3.51)<br />

e<br />

T<br />

e<br />

T<br />

e<br />

T<br />

e<br />

T<br />

R e<br />

T<br />

e<br />

T<br />

t<br />

+ ⎡<br />

⎣∆U ⎤<br />

⎦<br />

⎡<br />

⎣H ⎤<br />

⎦ ρ fdV − ⎡<br />

⎣∆U ⎤<br />

⎦<br />

⎡<br />

⎣B ⎤<br />

⎦<br />

⎡<br />

⎣σ ⎤<br />

⎦dV − ⎡<br />

⎣∆U ⎤<br />

⎦<br />

⎡<br />

⎣B ⎤<br />

⎦<br />

⎡<br />

⎣σ<br />

⎤<br />

⎦dV<br />

∫ ∫ ∫<br />

Ωi Ωi Ωi<br />

∫<br />

and <strong>the</strong> <strong>element</strong> stiffness matrix can be defined as:<br />

e e<br />

T<br />

e<br />

⎡<br />

⎣k ⎤<br />

⎦ = ∫<br />

⎡<br />

⎣B ⎤<br />

⎦<br />

⎡<br />

⎣ C'<br />

⎤⎡<br />

⎦⎣B ⎤<br />

⎦dV<br />

(3.52)<br />

Ωi<br />

and <strong>the</strong> <strong>element</strong> force vector, which has contributions from specified displacement<br />

boundary conditions, concentrated nodal forces, traction boundary conditions, body<br />

forces, stresses at start <strong>of</strong> time step and change <strong>of</strong> stresses during time step, can be<br />

defined as:


49<br />

∫<br />

e<br />

e<br />

T<br />

1<br />

=<br />

2<br />

∂Ωi<br />

⎡<br />

⎣f ⎤<br />

⎦<br />

⎡<br />

⎣H ⎤<br />

⎦<br />

⎡<br />

⎣ t ⎤<br />

⎦dS<br />

∫<br />

e<br />

e<br />

T<br />

f2<br />

= H ρ f dV<br />

Ωi<br />

⎡<br />

⎣<br />

⎤<br />

⎦<br />

⎡<br />

⎣<br />

⎤<br />

⎦<br />

⎡<br />

⎣<br />

⎤<br />

⎦<br />

∫<br />

e e<br />

T<br />

R<br />

3<br />

= σ<br />

Ωi<br />

⎡<br />

⎣f ⎤<br />

⎦<br />

⎡<br />

⎣B ⎤<br />

⎦<br />

⎡<br />

⎣<br />

⎤<br />

⎦dV<br />

(3.53)<br />

∫<br />

e e<br />

T<br />

t<br />

4<br />

= σ<br />

Ωi<br />

⎡<br />

⎣f ⎤<br />

⎦<br />

⎡<br />

⎣B ⎤<br />

⎦<br />

⎡<br />

⎣<br />

⎤<br />

⎦dV<br />

e<br />

where ⎡<br />

⎣f<br />

⎤<br />

1 ⎦ , e<br />

⎡<br />

⎣f<br />

⎤<br />

2 ⎦ , e<br />

⎡<br />

⎣f<br />

⎤<br />

3 ⎦ and e<br />

⎡<br />

⎣f<br />

⎤<br />

4 ⎦are <strong>element</strong> contributions to <strong>the</strong> force vector. Now<br />

Equation (3.51) can be rewritten as:<br />

⎡ ⎤⎡ ⎤ ⎡ ⎤ ⎡ ⎤ ⎡ ⎤ ⎡ ⎤<br />

e e e e e e<br />

⎣k ⎦⎣∆ U ⎦ = ⎣f1 ⎦+ ⎣f2 ⎦+ ⎣f3 ⎦+<br />

⎣f4<br />

⎦ (3.54)<br />

And <strong>the</strong> summation <strong>of</strong> contributions from all <strong>element</strong>s yields,<br />

[ K]{ ∆ U} = { F}<br />

(3.55)<br />

where [ K ] is <strong>the</strong> global stiffness matrix, { F } is <strong>the</strong> global force vector and { U}<br />

change in <strong>the</strong> displacement vector during <strong>the</strong> time step.<br />

∆ is <strong>the</strong><br />

Note that solving <strong>the</strong> linear system in Equation (3.55) results in <strong>the</strong> displacement<br />

contribution. Thus, one can find <strong>the</strong> stresses and strains contributions by using Equation<br />

(3.34) and Equation (3.49) respectively.


50<br />

CHAPTER 4<br />

Code Description and Verification<br />

Code Description<br />

Our main objective is to predict <strong>the</strong> maximum displacement when a load is<br />

applied. To conduct <strong>the</strong> <strong>analysis</strong>, two codes were used: <strong>the</strong> first code was written by <strong>the</strong><br />

author, to create roadway meshes – Road Mesh, and <strong>the</strong> second code is <strong>the</strong> Structural<br />

Analysis <strong>of</strong> Damage Induced Stresses in Thermo-Inelastic Composites – SADISTIC<br />

(Allen, 1994), to perform <strong>finite</strong> <strong>element</strong> <strong>analysis</strong>. The mesh generator provides for <strong>the</strong><br />

roadway geometry, loads and material properties as an input, and <strong>the</strong> resulting code gives<br />

you, as an output, <strong>the</strong> input file for <strong>the</strong> <strong>finite</strong> <strong>element</strong> code. Both codes were written in<br />

FORTRAN, in addition, commercial s<strong>of</strong>tware was used as a postprocessor to visualize<br />

<strong>the</strong> meshes, both deformed and undeformed cases. The purpose <strong>of</strong> <strong>the</strong> roadway mesh<br />

generator code is to perform discretization <strong>of</strong> <strong>the</strong> roadway domain into triangular subdomains,<br />

and was developed in such a way that it can be divided in three parts: i) input<br />

roadway geometry, loads and material properties; ii) output used as input for <strong>the</strong> <strong>finite</strong><br />

<strong>element</strong> code; and iii) output used as input for mesh visualization. The chart below shows<br />

how <strong>the</strong> mesh generator works in combination with <strong>the</strong> <strong>finite</strong> <strong>element</strong> code.


51<br />

Start<br />

Input loads<br />

Input roadway geometry<br />

Input material properties<br />

• Elastic<br />

• Viscoelastic<br />

• Roadway width<br />

• Tire width<br />

• Axle dimension<br />

Number <strong>of</strong> divisions horizontally<br />

• Under <strong>the</strong> truck<br />

• On <strong>the</strong> shoulder<br />

• Number <strong>of</strong> layers<br />

• Layer thickness<br />

Number <strong>of</strong> divisions vertically<br />

• In each layer<br />

Output<br />

Create input file for <strong>finite</strong><br />

<strong>element</strong> code<br />

Create input file for mesh<br />

visualization<br />

SADISTIC solves two and three dimensional <strong>the</strong>rmomechanical continuum<br />

problems using <strong>the</strong> <strong>finite</strong> <strong>element</strong> method. Linear <strong>the</strong>rmoelastic (both isotropic and<br />

orthotropic), elastic-plastic, <strong>the</strong>rmoviscoplastic, and linear <strong>the</strong>rmo<strong>viscoelastic</strong> are<br />

included as material models. In addition, interface <strong>element</strong>s can be used to simulate crack<br />

growth. The code has a broad variety <strong>of</strong> options that include: plane stress, plane strain,<br />

generalized plane strain, and penalty constraints. 43 The combination <strong>of</strong> <strong>the</strong>se two codes<br />

provides <strong>the</strong> necessary tools to perform <strong>the</strong> pavement analyses.<br />

43 A more detailed description <strong>of</strong> <strong>the</strong> program is beyond our interest here and can found in (ZOCHER,<br />

1995).


52<br />

Our roadway problem involves several different materials with a total <strong>of</strong> four<br />

layers; one layer is treated as <strong>viscoelastic</strong> and <strong>the</strong> o<strong>the</strong>r three as elastic. Traction (natural)<br />

boundary conditions and displacement (essential) boundary conditions were specified<br />

throughout <strong>the</strong> domain Ω. The temperature was considered to be constant for <strong>the</strong> entire<br />

<strong>analysis</strong> and was not taken into consideration. A triangular <strong>element</strong> was used in <strong>the</strong> <strong>finite</strong><br />

<strong>element</strong> discretization.<br />

Code Verification<br />

In this chapter <strong>the</strong> computer program SADISTIC is verified with several two<br />

dimensional problems. Four problems were chosen to verify <strong>the</strong> code with <strong>the</strong> purpose <strong>of</strong><br />

investigating <strong>the</strong> response <strong>of</strong> several <strong>viscoelastic</strong> bodies to mechanical loadings. The<br />

verification is obtained by solving simple problems with a known analytical solution and<br />

comparing <strong>the</strong> solutions with numerical results from <strong>the</strong> code. The roadway is modeled as<br />

a plane strain problem, since <strong>the</strong> third dimension is considered to be in<strong>finite</strong>. Thus, <strong>the</strong><br />

three problems solved are also plane strain problems. This procedure verifies <strong>the</strong> code<br />

and confirms <strong>the</strong> code output is correct, while also ensuring that more complex cases are<br />

accurate. The examples will be presented with two graphics each, <strong>the</strong> first one showing<br />

loading and <strong>the</strong> second one detailing <strong>the</strong> <strong>viscoelastic</strong> response (displacement). All<br />

examples are modeled using a hypo<strong>the</strong>tical <strong>viscoelastic</strong> material. The uniaxial relaxation<br />

modulus is given in <strong>the</strong> form <strong>of</strong> <strong>the</strong> standard linear solid (a 1-<strong>element</strong> Wiechert model)<br />

with one term in <strong>the</strong> Prony series. Below, Figure 25 shows <strong>the</strong> Wiechert model.


53<br />

E<br />

1<br />

E<br />

2<br />

E<br />

n−1<br />

E<br />

n<br />

E ∞<br />

η<br />

1<br />

η<br />

2<br />

η<br />

n−1<br />

η<br />

n<br />

ε<br />

σ<br />

Figure 25: Wiechert model<br />

The Wiechert model can have as many spring-dashpot Maxwell <strong>element</strong>s as are<br />

needed to approximate <strong>the</strong> distribution satisfactorily, and are given by:<br />

n<br />

i<br />

Et () = E +∑ Ee ρ<br />

(4.1)<br />

∞<br />

i=<br />

1<br />

i<br />

t<br />

−<br />

however, to make <strong>the</strong> verification simpler, only one Maxwell <strong>element</strong> was used. The total<br />

stress σ transmitted by <strong>the</strong> model is <strong>the</strong> stress in <strong>the</strong> isolated spring (<strong>of</strong> stiffness E ∞<br />

) plus<br />

that in each <strong>of</strong> <strong>the</strong> Maxwell spring-dashpot arms. The uniaxial relaxation modulus is<br />

given by:<br />

t<br />

−<br />

1<br />

=<br />

∞<br />

+<br />

1<br />

(4.2)<br />

Et () E Ee ρ<br />

In <strong>the</strong> examples that follow, values <strong>of</strong> 0.1 MPa and 0.4 MPa were assigned<br />

to E ∞<br />

and E 1<br />

respectively: ρ<br />

1<br />

, which is <strong>the</strong> relaxation time, is 1.0, and <strong>the</strong> Poisson’s ratio


54<br />

is 0.3. The material description <strong>of</strong> <strong>the</strong> Wiechert model (C ij in Voigt notation) is given in<br />

Table 1.<br />

ij<br />

q<br />

C<br />

ij q<br />

η<br />

ij q<br />

11,22 ∞ 0.1346150D+06<br />

1 0.5384620D+06 0.5384620D+06<br />

12,23 ∞ 0.1346150D+06<br />

1 0.2307690D+06 0.2307690D+06<br />

44,66 ∞ 0.3846150D+05<br />

1 0.1538460D+06 0.1538460D+06<br />

Table 1: Viscoelastic material properties<br />

The first two solutions are obtained for a two dimensional rectangular bar with<br />

length 2 m as shown in Figure 26. The bar has zero displacement in <strong>the</strong> x-direction at<br />

x = 0 . Evenly distributed load is applied to <strong>the</strong> bar at x = 2 . The input to be considered is<br />

<strong>the</strong> load P and <strong>the</strong> output is <strong>the</strong> time-dependent displacement ux= ( 2) . Since <strong>the</strong> stresses<br />

and strains can be shown to be spatially homogeneous, <strong>the</strong> bar is modeled exactly with<br />

two triangular <strong>element</strong>s.<br />

Example 1. (Creep test) The bar is subjected to a tip load<br />

P<br />

0<br />

= P H()<br />

t in a test<br />

called a creep test, where<br />

0<br />

P is <strong>the</strong> load P at time equals to zero and Ht () is <strong>the</strong> Heaviside<br />

function. The exact analytical solution to <strong>the</strong> displacement for an elastic bar under plane<br />

strain condition is:


55<br />

2<br />

−(1 −ν ) PL<br />

ux ( = Lt , ) = (4.3)<br />

EA<br />

whereν is Poisson’s ratio, P is <strong>the</strong> load on <strong>the</strong> end <strong>of</strong> <strong>the</strong> bar, at ( x = 2 ), E is <strong>the</strong> elastic<br />

modulus, L is <strong>the</strong> bar length and A is <strong>the</strong> cross sectional area <strong>of</strong> <strong>the</strong> bar. The bar has a<br />

width b. Using <strong>the</strong> <strong>viscoelastic</strong> correspondence principle it is easy to show that <strong>the</strong><br />

solution to <strong>the</strong> <strong>viscoelastic</strong> problem is given by:<br />

ν<br />

ux ( = Lt , ) = ⎜ ⎟<br />

( )<br />

2<br />

−(1 − ) P ⎛ L⎞<br />

−<br />

E Ee t ∞<br />

+<br />

1 ⎝ A⎠<br />

(4.4)<br />

The response <strong>of</strong> <strong>the</strong> bar from 0 to 40 seconds to a load <strong>of</strong> 2000 N is shown in<br />

Figure 27. By using a time step ∆t<br />

<strong>of</strong> 0.1 seconds, <strong>the</strong> <strong>finite</strong> <strong>element</strong> solution produces an<br />

error considered small or hardly noticeable in <strong>the</strong> graphic.<br />

tip load<br />

Example 2. (Ramp creep test) In this example <strong>the</strong> uniaxial bar is subjected to <strong>the</strong><br />

P=<br />

0<br />

P tH t<br />

()<br />

The analytical solution for <strong>the</strong> <strong>viscoelastic</strong> problem can be shown to be<br />

ν<br />

ux ( = Lt , ) = ⎜ ⎟<br />

( )<br />

2<br />

−(1 − ) Pt ⎛ L ⎞<br />

−<br />

E Ee t<br />

∞<br />

+<br />

1 ⎝ A⎠<br />

(4.5)<br />

Figure 28 shows <strong>the</strong> result for this problem.


Figure 26: Rectangular bar subjected to a tip load<br />

56


57<br />

INPUT<br />

4000<br />

3000<br />

Load P (N)<br />

2000<br />

1000<br />

0<br />

0 5 10 15 20 25 30 35 40<br />

Time (s)<br />

OUTPUT<br />

Displacement u at x = 2 (m)<br />

4.00E-02<br />

3.00E-02<br />

2.00E-02<br />

1.00E-02<br />

0.00E+00<br />

0 5 10 15 20 25 30 35 40<br />

Time (s)<br />

Analytical<br />

FEM<br />

Figure 27: Loading history and response <strong>of</strong> example 1


58<br />

INPUT<br />

20000<br />

16000<br />

Load P (N)<br />

12000<br />

8000<br />

4000<br />

0<br />

0 2 4 6 8 10<br />

Time (s)<br />

OUTPUT<br />

Displacement (x = 2) (m)<br />

0.25<br />

0.2<br />

0.15<br />

0.1<br />

0.05<br />

0<br />

0 2 4 6 8 10<br />

Time (s)<br />

FEM<br />

Analytical<br />

Figure 28: Loading history and response <strong>of</strong> example 2


59<br />

Example 3. This example is a 2-D problem and treats a thick-wall <strong>viscoelastic</strong><br />

cylinder problem with an internal pressure p applied to <strong>the</strong> inner diameter, as shown in<br />

Figure 29. Consider <strong>the</strong> internal pressure to be given by<br />

P<br />

0<br />

= P H()<br />

t , similar to <strong>the</strong> creep<br />

test. The elasticity solution can be employed along with <strong>the</strong> <strong>viscoelastic</strong> correspondence<br />

principle and <strong>the</strong> radial displacement is given by:<br />

0 2<br />

Pab(1 + ν)(1−2 ν)<br />

⎛b r⎞<br />

ur<br />

(,) r t = D()<br />

t<br />

2 2 ⎜ − ⎟<br />

a + (1−2 ν ) b ⎝r b⎠<br />

(4.6)<br />

Figure 29: Cylinder with Internal Pressure


60<br />

For this problem, a = 2 m, b = 4 m, and<br />

0<br />

P = 100 Pa. Figure 29 shows <strong>the</strong> radial<br />

displacement at x = 3.00 m up to 50 seconds. The mesh used here contains 120 <strong>element</strong>s<br />

and is shown in Figure 30. Due to symmetry conditions only one quarter <strong>of</strong> <strong>the</strong> cylinder<br />

needed to be modeled. The analytical and <strong>finite</strong> <strong>element</strong> solutions are presented in Figure<br />

31 for <strong>the</strong> mid-thickness displacement.<br />

Figure 30: Finite <strong>element</strong> mesh used in example 3


61<br />

INPUT<br />

200<br />

Internal Pressure (Pa)<br />

150<br />

100<br />

50<br />

0<br />

0 10 20 30 40 50<br />

Time (s)<br />

OUTPUT<br />

5.0E-04<br />

Displacement (r = 3) (m)<br />

4.0E-04<br />

3.0E-04<br />

2.0E-04<br />

1.0E-04<br />

0.0E+00<br />

0 10 20 30 40 50<br />

Time (s)<br />

FEM<br />

ANALYTICAL<br />

Figure 31: Loading history and response for example 3


62<br />

Example 4: (Beam with tip load) This last example treats a 3-D cantilever beam shown<br />

in Figure 32 has length L = 10m and cross-sectional area <strong>of</strong> 1 m 2 . The beam is subjected<br />

to a load at x = 10 m<br />

P=<br />

PH<br />

0<br />

() t<br />

Where P<br />

0<br />

is 1 Newton. We seek <strong>the</strong> displacement v at x = 10m. This problem has<br />

spatially varying stress and strain as opposed to <strong>the</strong> first two bar problems.<br />

The analytical solution is derived by applying <strong>the</strong> <strong>viscoelastic</strong> correspondence<br />

principle to <strong>the</strong> elastic solution for <strong>the</strong> tip deflection from strength <strong>of</strong> materials. This<br />

procedure results in:<br />

PL<br />

= (4.7)<br />

3I<br />

3<br />

0<br />

v [ Dt ( )]<br />

where I is <strong>the</strong> area moment <strong>of</strong> inertia <strong>of</strong> <strong>the</strong> beam and it is 1/12.<br />

The results are calculated from o to 10 seconds. Note that <strong>the</strong> results shown in<br />

Figure 33 are not exact, but are a good approximation, since <strong>the</strong>y produce a maximum<br />

difference <strong>of</strong> 3% between <strong>the</strong> analytical solution and <strong>the</strong> <strong>finite</strong> <strong>element</strong> code. A time step<br />

<strong>of</strong> 0.1 seconds was used for this example.


Figure 32: Beam problem <strong>of</strong> example 4<br />

63


64<br />

INPUT<br />

2.0<br />

1.5<br />

Load P (N)<br />

1.0<br />

0.5<br />

0.0<br />

0 2 4 6 8 10<br />

Time (s)<br />

OUTPUT<br />

Displacement (x = 10) (m)<br />

0.04<br />

0.03<br />

0.02<br />

0.01<br />

0.00<br />

0 2 4 6 8 10<br />

Time (s)<br />

FEM<br />

ANALYTICAL<br />

Figure 33: Loading history and response for example 4


65<br />

CHAPTER 5<br />

Asphalt Concrete Roadway Analysis<br />

As described before, <strong>the</strong> purpose <strong>of</strong> this <strong>analysis</strong> is to show a comparison between<br />

different configurations in a pavement structure. Correspondingly, in this section,<br />

pavement geometry, pavement layer characterization, overestimation between 3-D and 2-<br />

D, and mesh convergence are evaluated.<br />

Roadway Geometry<br />

Consider a typical two-lane asphalt roadway described in <strong>the</strong> Roadway Design<br />

Manual <strong>of</strong> <strong>the</strong> Nebraska Department <strong>of</strong> Roads (shown in Figure 34) that contains a<br />

symmetry line down <strong>the</strong> middle <strong>of</strong> it. For simplicity, roadway symmetry for only <strong>the</strong> right<br />

half <strong>of</strong> <strong>the</strong> lane will be modeled (See Figure 35).The road is 12 meters wide with two<br />

3.50 meters traffic lanes and two shoulders <strong>of</strong> 2.50 meters. Figure 36 shows <strong>the</strong> boundary<br />

conditions <strong>of</strong> <strong>the</strong> pavement used in <strong>the</strong> model.<br />

Figure 34: Typical two-lane roadway cross section<br />

A pavement design must include means <strong>of</strong> surface drainage–removal <strong>of</strong> all water<br />

present on <strong>the</strong> pavement surface, shoulder surface or any o<strong>the</strong>r surface from which it may


66<br />

flow onto <strong>the</strong> pavement. This is important to ensure a high-quality, long-lasting<br />

pavement. Moisture accumulation is always problematic in any pavement structural<br />

layers, and if not systematically removed, can cause problems by weakening <strong>the</strong><br />

pavement structure. When rutting—<strong>the</strong> permanent deformation along <strong>the</strong> wheel path—is<br />

present, <strong>the</strong> pavement becomes more vulnerable to pooling water on <strong>the</strong> surface. When<br />

this happens, 90% <strong>of</strong> <strong>the</strong> pavement life is depleted. Some <strong>of</strong> <strong>the</strong> ways to prevent water<br />

infiltration and accumulation include: impermeable HMA, roadside ditch and slope. The<br />

only one considered in this <strong>analysis</strong> is <strong>the</strong> slope <strong>of</strong> <strong>the</strong> cross section that allows rainwater<br />

to flow to <strong>the</strong> side <strong>of</strong> <strong>the</strong> pavement where it is collected in a roadside ditch.<br />

Figure 35: Right half side to be modeled


67<br />

Figure 36: Boundary conditions on <strong>the</strong> pavement<br />

Typically, <strong>the</strong> travel lane has slopes to both shoulders usually at 2% grade while<br />

paved shoulders have slopes <strong>of</strong> 4%. The side slope grade varies according to <strong>the</strong><br />

classification <strong>of</strong> <strong>the</strong> roadway. It can be 1:3, 1:4 or 1:6, depending on whe<strong>the</strong>r <strong>the</strong> roadway<br />

is a rural state highway, a municipal state highway or an interstate. Figure 37 shows <strong>the</strong><br />

different possibilities <strong>of</strong> side slopes.<br />

Figure 37: Side slopes <strong>of</strong> roadways (NDor, 2005)<br />

Pavement Layer Characterization<br />

The pavement in this research is composed <strong>of</strong> four layers. The top layer is <strong>the</strong><br />

asphalt concrete, which varies from 10cm to 20cm for this <strong>analysis</strong>. The subsequent


68<br />

layers with <strong>the</strong> multiple <strong>element</strong>s involved in <strong>the</strong> hot mix asphalt are shown in Figure 38,<br />

detailing <strong>the</strong> pavement structure and all layers. This figure shows <strong>the</strong> variety <strong>of</strong><br />

aggregates sizes in each layer and how <strong>the</strong> asphalt matrix works as a binder with <strong>the</strong><br />

aggregates embedded in <strong>the</strong> asphalt matrix.


Figure 38: Pavement structure and all layers<br />

69


70<br />

The asphalt concrete layer is <strong>the</strong> final layer to be built on top <strong>of</strong> <strong>the</strong> o<strong>the</strong>r layers.<br />

Even though <strong>the</strong> pavement geometry can vary from case to case and require additional<br />

layers if necessary, for our <strong>analysis</strong>, <strong>the</strong> selected pavement contains four layers: a 10 cm<br />

HMA, a 40 cm granular base, a 30 cm granular sub-base and a in-situ sub-grade, which is<br />

<strong>the</strong> graded natural terrain and has a depth <strong>of</strong> 1.10 m in <strong>the</strong> model. The asphaltic layer is<br />

modeled as an isotropic <strong>viscoelastic</strong> medium defined by a generalized Maxwell model<br />

and represented by:<br />

n<br />

i<br />

Et () = E +∑ Ee ρ<br />

(4.8)<br />

∞<br />

i=<br />

1<br />

i<br />

t<br />

−<br />

The remaining layers are treated as linear elastic media. Table 2 and Table 3 list <strong>the</strong><br />

Prony series coefficients <strong>of</strong> relaxation modulus for <strong>the</strong> two different types <strong>of</strong> hot asphalt<br />

mixtures: AC I and AC II. All HMA are asphalt concrete type and mixed with different<br />

binders. The Prony series constants for AC I were obtained from <strong>the</strong> study <strong>of</strong> Mun (2003)<br />

and AC II were obtained from Wen, 2001.<br />

AC I<br />

Poisson ration = 0.30 E i (kPa) ρ i (s)<br />

∞ 5.83E+04 -<br />

1 4.91E+09 2.00E-02<br />

2 5.74E+09 2.00E-01<br />

3 4.96E+09 2.00E+00<br />

4 2.96E+09 2.00E+01<br />

5 1.26E+09 2.00E+02<br />

6 4.47E+08 2.00E+03<br />

7 1.58E+05 2.00E+04<br />

Table 2: Prony series coefficients <strong>of</strong> relaxation modulus for AC I


71<br />

AC II<br />

Poisson ration = 0.35 E i (kPa) ρ i (s)<br />

∞ 9.90E+04 -<br />

1 -7.50E+05 1.00E-05<br />

2 2.17E+06 1.00E-04<br />

3 -5.39E+06 1.00E-03<br />

4 8.47E+06 1.00E-02<br />

5 4.08E+06 1.00E-01<br />

6 1.05E+06 1.00E+00<br />

7 1.16E+05 1.00E+01<br />

8 5.06E+04 1.00E +02<br />

9 3.10E+03 1.00E+03<br />

10 1.70E+03 1.00E+04<br />

11 -2.00E+02 1.00E+05<br />

Table 3: Prony series coefficients <strong>of</strong> relaxation modulus for AC II<br />

Base Sub-base Sub-grade<br />

E (MPa) ν E (MPa) ν E (MPa) ν<br />

4000 0.35 800 0.35 200 0.35<br />

Table 4: Material properties for <strong>the</strong> road elastic layers<br />

The mixture AC I was obtained at temperature 5°C and <strong>the</strong> relaxation modulus data for<br />

mixture AC II was obtained at temperature 20°C. Figure 39 shows a comparison between<br />

AC I and AC II.


72<br />

AC I<br />

1.E-07 1.E-04 1.E-01 1.E+02 1.E+05 1.E+08 1.E+11 1.E+14<br />

1.00E+05<br />

1.00E+04<br />

1.00E+03<br />

1.00E+02<br />

1.00E+01<br />

1.00E+00<br />

Relaxation Modulus (MPa)<br />

Time (s)<br />

AC II<br />

1.00E+05<br />

1.00E+04<br />

1.00E+03<br />

1.00E+02<br />

1.00E+01<br />

1.00E+00<br />

1.E-07 1.E-04 1.E-01 1.E+02 1.E+05 1.E+08 1.E+11 1.E+14<br />

Relaxation Modulus (MPa)<br />

Time (s)<br />

Figure 39: Comparison between AC I and AC II


73<br />

The loads applied to a pavement are regulated. Most US states have limitations<br />

for <strong>the</strong> maximum weight per axle limit and overall weight. Nebraska Department <strong>of</strong><br />

Roads sets limits for 34,000 lb for tandem axles and a maximum gross-vehicle weight <strong>of</strong><br />

80,000 lb. The 34,000 lb in a tandem axle applies a load <strong>of</strong> 151kN on <strong>the</strong> roadway<br />

surface, where a uniform distribution to each side <strong>of</strong> <strong>the</strong> axle is considered. The front,<br />

steer axle has 12,000 lb and applies a load <strong>of</strong> 53.4kN. Figure 40 shows <strong>the</strong> load<br />

distribution on each axle.<br />

Figure 40: Weight distribution<br />

In order to accommodate for <strong>the</strong>se limitations, different tire configurations are<br />

used. Conventional dual tires are being replaced by only one wide-base single tire. By<br />

replacing both sides <strong>of</strong> dual tires by one wide result in a smaller total contact area with<br />

<strong>the</strong> pavement. Since <strong>the</strong>y are still carrying <strong>the</strong> same load as <strong>the</strong> dual tires, <strong>the</strong> pressure is<br />

larger in <strong>the</strong> wide tire case. In addition to this, <strong>the</strong> axle distance is not treated as a variable<br />

and it is fixed at 1.80 meters.<br />

The analyses performed here include three different tire types with different<br />

overall widths: 29.5 cm (295/80R22.5) for <strong>the</strong> dual configuration and 44.5 cm<br />

(445/50R22.5) and 49.5 cm (495/45R22.5) for <strong>the</strong> wide base configuration. As mentioned


74<br />

before, tire inflation pressures and contact areas are not treated as variables. The standard<br />

inflation pressure was <strong>the</strong> same for <strong>the</strong> each tire at 100 psi. One o<strong>the</strong>r design variable<br />

included in <strong>the</strong> analyses is <strong>the</strong> change in <strong>the</strong> asphaltic layer thickness, using values <strong>of</strong> 10,<br />

15 and 20 cm. In addition to tire configuration and thickness <strong>of</strong> asphalt layer, changes in<br />

hot mix asphalt were also evaluated. The goal is to compare <strong>the</strong> pavement service life for<br />

one variable parameter.<br />

The analyses are done in <strong>the</strong> following way. Three parameters are treated as<br />

variables: tire width, type <strong>of</strong> hot mix asphalt and thickness <strong>of</strong> asphaltic layer. However,<br />

only one parameter is varied each time and all o<strong>the</strong>rs are held fixed. For example, if<br />

different tire widths are <strong>the</strong> selected variable, <strong>the</strong>n only one type <strong>of</strong> hot mix asphalt and<br />

one thickness <strong>of</strong> asphaltic layer are selected. Afterwards, it is possible to predict which<br />

one gives <strong>the</strong> best service life <strong>of</strong> a pavement. Similarly, by selecting a type <strong>of</strong> tire and a<br />

thickness <strong>of</strong> asphaltic layer would be possible to conclude which one will give <strong>the</strong> best<br />

service life.<br />

Overestimation Between 3-D and 2-D<br />

The analyses are run in a plane strain configuration, assuming <strong>the</strong> configurations<br />

shown in Figure 34 are in<strong>finite</strong>ly long in <strong>the</strong> third dimension. Therefore, in <strong>the</strong>se types <strong>of</strong><br />

analyses, <strong>the</strong> loading is applied as a strip load in <strong>the</strong> third dimension. The 2D plane strain<br />

analyses have advantages over a 3D <strong>analysis</strong> in that <strong>the</strong> computational time is<br />

considerably reduced. By running a 2D problem and applying a strip <strong>of</strong> load in <strong>the</strong> third<br />

dimension, an overestimation <strong>of</strong> load is induced. Since a tire applies a non-uniform load<br />

to a pavement, <strong>the</strong> consideration <strong>of</strong> a uniform load is considered as an approximation.


75<br />

Figure 41 shows a real pressure distribution on a tire, showing pressure is higher in <strong>the</strong><br />

center and lower in <strong>the</strong> corners.<br />

Figure 41: Tire pressure distribution (Blackman, Halliday, and Merrill, 2000)<br />

A reasonable 3-D approximation for this pressure would be a sinusoidal curve in<br />

both directions. By doing a 2-D <strong>analysis</strong>, only one dimension can be treated as a<br />

sinusoidal curve, since <strong>the</strong>re is no variation on <strong>the</strong> third dimension. Figure 42 shows a 3-<br />

D pavement with a dual tire configuration load, and Figure 43 shows a 2-D with <strong>the</strong> same<br />

load. The comparison between <strong>the</strong> two types <strong>of</strong> loads is shown in Figure 44.


76<br />

Figure 42: Pavement 3-D with forces<br />

Figure 43: Pavement 2-D with forces


77<br />

Figure 44: Comparison between 3D and 2D loads<br />

To solve this problem, a factor showing <strong>the</strong> ration between 3D and 2D has to be<br />

found. This factor is <strong>the</strong>n multiplied by <strong>the</strong> maximum displacements in <strong>the</strong> 2D to correct<br />

and make a more realistic prediction. Two analyses are necessary to find this factor. The<br />

first <strong>analysis</strong> is a 3-D <strong>finite</strong> <strong>element</strong> mesh with only one tire load and elastic materials as<br />

shown in Figure 42. The o<strong>the</strong>r <strong>analysis</strong> shows a 2-D mesh with <strong>the</strong> same material<br />

properties, loads and geometry. Only one time step is necessary. A maximum<br />

displacement <strong>of</strong> 4.46E-01 m was <strong>the</strong> result for <strong>the</strong> 3-D <strong>analysis</strong> and 6.34E-01 was <strong>the</strong><br />

maximum displacement for <strong>the</strong> 2-D <strong>analysis</strong>. With <strong>the</strong>se numbers, it is shown that <strong>the</strong><br />

displacements are overestimated by a factor <strong>of</strong> 1.42x and, as a result, <strong>the</strong> displacements<br />

used in <strong>the</strong> <strong>analysis</strong> are corrected by being divided by this factor.<br />

For this <strong>analysis</strong>, <strong>the</strong> response <strong>of</strong> a cyclic load imposed by <strong>the</strong> truck on <strong>the</strong><br />

pavement is simulated. The truck applies a static load <strong>of</strong> 151kN with a tandem axle. A 60<br />

feet truck traveling at 70 mph takes less than one second to pass through a fixed point in<br />

<strong>the</strong> pavement. However, for simplicity, one second <strong>of</strong> simulation was considered to<br />

simulate <strong>the</strong> passage <strong>of</strong> all five axles, being 0.2 seconds <strong>the</strong> time that each axle loads <strong>the</strong>


78<br />

pavement. Ramp functions for axle loading and unloading were implemented in <strong>the</strong> code,<br />

with a period <strong>of</strong> 0.2 seconds for each axle passing or 0.1 seconds for loading and 0.1<br />

seconds for unloading and a peak <strong>of</strong> 18,900kPa. The truck takes a total five cycles <strong>of</strong> 0.2<br />

seconds or 1 second for passing all five axles followed by a 19 second interval <strong>of</strong> rest,<br />

which is <strong>the</strong> time until <strong>the</strong> next truck passes, totaling a period <strong>of</strong> 20 seconds. Three trucks<br />

per minute or 180 trucks per hour are considered. Figure 45 shows <strong>the</strong> five axle load and<br />

a rest period up to 5 seconds, although <strong>the</strong> rest period still goes up to 20 seconds. For<br />

scale reasons it would be hard to see <strong>the</strong> five cycles with a larger scale. Figure 46 shows<br />

<strong>the</strong> first 3 cycles <strong>of</strong> trucks passing over <strong>the</strong> pavement.<br />

0.0<br />

0 1 2 3 4 5<br />

-4.0<br />

Load (KPa)<br />

-8.0<br />

-12.0<br />

-16.0<br />

-20.0<br />

Time (s)<br />

Figure 45: First cyclic load – axle loads


79<br />

0.0<br />

0 10 20 30 40 50 60<br />

-4.0<br />

Load (KPa)<br />

-8.0<br />

-12.0<br />

-16.0<br />

-20.0<br />

Time (s)<br />

Figure 46: Cyclic load<br />

The load is applied on <strong>the</strong> pavement by increments <strong>of</strong> time and this requires an<br />

<strong>analysis</strong> <strong>of</strong> <strong>the</strong> minimum time step that will produce accurate results. This can be<br />

accomplished by simply running <strong>the</strong> code for a few cycles <strong>of</strong> loading and increasing <strong>the</strong><br />

time step for each run until <strong>the</strong> results start to change with <strong>the</strong> time step, Giving <strong>the</strong><br />

minimum allowable time step. After running <strong>the</strong> code with different time steps, making<br />

<strong>the</strong>m smaller and smaller, <strong>the</strong> minimum allowable time step is found to be 0.125 seconds<br />

for <strong>the</strong> loading part and 1.0 second for <strong>the</strong> rest part.<br />

Mesh Convergence<br />

The process <strong>of</strong> discretizing <strong>the</strong> roadway into <strong>element</strong>s is known as mesh<br />

generation. Fine meshes have <strong>the</strong> disadvantage <strong>of</strong> increasing <strong>the</strong> number <strong>of</strong> equations that<br />

must be subsequently solved. However, choosing a relatively coarse mesh will result in<br />

an inaccurate numerical solution. Therefore, in order to decide <strong>the</strong> size <strong>of</strong> <strong>the</strong> triangular<br />

<strong>element</strong>s, an <strong>analysis</strong> <strong>of</strong> mesh convergence must be conducted.


80<br />

The first step is to create a mesh using <strong>the</strong> fewest, reasonable number <strong>of</strong> <strong>element</strong>s<br />

and analyze <strong>the</strong> model. Then, recreate <strong>the</strong> mesh with a denser <strong>element</strong> distribution, reanalyze<br />

it and compare <strong>the</strong> results to those <strong>of</strong> <strong>the</strong> previous mesh. The mesh density is<br />

increased and <strong>the</strong> model is re-analyzed until <strong>the</strong> results converge satisfactorily. One<br />

method <strong>of</strong> establishing mesh convergence requires a curve <strong>of</strong> a result parameter (in this<br />

case maximum displacement on <strong>the</strong> surface was used) to be plotted against some measure<br />

<strong>of</strong> mesh density (number <strong>of</strong> <strong>element</strong>s was used). To determine when results have<br />

converged satisfactorily and accurately, we used at least three runs to plot a curve which<br />

can <strong>the</strong>n be used to indicate when convergence is achieved or how far away <strong>the</strong> most<br />

refined mesh is from full convergence. Notice that each tire used in <strong>the</strong> <strong>analysis</strong><br />

employed a different mesh and, consequently, a mesh convergence study had to be<br />

performed for each <strong>of</strong> <strong>the</strong>m.<br />

The first step was to keep all layers with <strong>the</strong> minimum reasonable number <strong>of</strong><br />

<strong>element</strong>s. The subdivision was performed at each layer. A total <strong>of</strong> 5 steps were necessary<br />

to obtain convergence with <strong>the</strong> mesh. The first one was to vertically subdivide <strong>the</strong> first<br />

layer. When convergence was achieved, <strong>the</strong> first layer was <strong>the</strong>n horizontally subdivided<br />

completing <strong>the</strong> second step. Now, <strong>the</strong> first layer has <strong>the</strong> adequate number <strong>of</strong> <strong>element</strong>s, so<br />

no fur<strong>the</strong>r divisions were necessary in this layer. After this, only horizontal subdivisions<br />

were necessary, since <strong>the</strong>y share <strong>the</strong> same vertical lines. The third, fourth and fifth steps<br />

were accomplished by keeping fixed <strong>the</strong> previous layers that already achieved<br />

convergence and varying <strong>the</strong> horizontal divisions in each corresponding one. Figure 47<br />

shows <strong>the</strong> mesh convergence for dual tire configuration. The final number <strong>of</strong> <strong>element</strong>s is<br />

1423. Figure 48 shows <strong>the</strong> final mesh.


81<br />

29.5 cm tire<br />

1.38E-04<br />

Maximum Displacement (m)<br />

1.37E-04<br />

1.37E-04<br />

1.36E-04<br />

1.35E-04<br />

1.34E-04<br />

1100 1150 1200 1250 1300 1350 1400 1450 1500 1550<br />

Number <strong>of</strong> Elements<br />

Figure 47: Convergence <strong>of</strong> maximum displacement for 29.5 tire<br />

Figure 48: Mesh for <strong>the</strong> dual configuration tire – 29.5 cm<br />

Figure 49 shows <strong>the</strong> mesh convergence for <strong>the</strong> 44.5 cm wide tire and Figure 50 shows its<br />

respective mesh with 920 <strong>element</strong>s.


82<br />

44.5 cm tire<br />

1.32E-04<br />

Maximum Displacement (m)<br />

1.31E-04<br />

1.31E-04<br />

1.30E-04<br />

1.29E-04<br />

1.28E-04<br />

750 800 850 900 950 1000 1050 1100<br />

Number <strong>of</strong> Elements<br />

Figure 49: Convergence <strong>of</strong> maximum displacement for 44.5 tire<br />

Figure 50: Mesh for <strong>the</strong> wide configuration tire – 44.5 cm<br />

Figure 51 shows <strong>the</strong> mesh convergence for <strong>the</strong> 49.5 cm wide tire and Figure 52 its<br />

respective mesh with 901 <strong>element</strong>s. So, for each tire configuration used, a different mesh<br />

must be selected.


83<br />

49.5 cm tire<br />

1.34E-04<br />

Maximum Displacement (m)<br />

1.33E-04<br />

1.32E-04<br />

1.31E-04<br />

1.31E-04<br />

1.30E-04<br />

700 750 800 850 900 950 1000<br />

Number <strong>of</strong> Elements<br />

Figure 51: Convergence <strong>of</strong> maximum displacement for 49.5 tire<br />

Figure 52: Mesh for <strong>the</strong> wide configuration tire – 49.5 cm<br />

After <strong>the</strong> mesh convergence study was performed, ano<strong>the</strong>r convergence had to be<br />

done. A real roadway does not have a side slope like <strong>the</strong> one shown on Figure 52, but a<br />

smoo<strong>the</strong>r one. As mentioned before, <strong>the</strong> side slope varies according to <strong>the</strong> classification<br />

<strong>of</strong> <strong>the</strong> roadway. It can be 1:3, 1:4 or 1:6, all depending if <strong>the</strong> roadway is a rural state


84<br />

highway, a municipal state highway or an interstate. As a result, different meshes with<br />

<strong>the</strong> different side slopes had to be created in order to verify <strong>the</strong> accuracy <strong>of</strong> each one.<br />

Each mesh was treated with <strong>the</strong> same materials <strong>of</strong> Table 4 and <strong>the</strong> HMA layer was also<br />

treated as an elastic material, for simplicity purposes, with Young’s modulus <strong>of</strong><br />

E = 8000MPa<br />

. Also, one tire configuration <strong>of</strong> 44.5 cm width was considered. The<br />

purpose <strong>of</strong> this study is to show that a mesh with a side slope 1:6 does not produce a<br />

considerable difference in <strong>the</strong> results compared to a mesh with side slope 0.5:1. Four<br />

meshes were created, with side slopes 1:6, 1:3, 1:1 and 0.5:1 and are shown below. Note<br />

that <strong>the</strong> pavement shown in Figure 56 is <strong>the</strong> one used in all analyses.<br />

Figure 53: Pavement with side slope 1:6<br />

Figure 54: Pavement with side slope 1:3<br />

Figure 55: Pavement with side slope 1:1<br />

Figure 56: Pavement with side slope 0.5:1


85<br />

Figure 57 shows a graphic with <strong>the</strong> displacement on <strong>the</strong> surface for each side slope. The<br />

<strong>analysis</strong> shows that <strong>the</strong> maximum difference between displacements in similar locations<br />

is less than 0.1%, which gives support to use <strong>the</strong> mesh presented in Figure 50.<br />

Different Slopes - Displacement on <strong>the</strong> surface<br />

Displacements (m)<br />

-5.0E-05<br />

-7.0E-05<br />

-9.0E-05<br />

-1.1E-04<br />

-1.3E-04<br />

-1.5E-04<br />

0 10 20 30 40 50<br />

Node #<br />

0.5:1 1:01 1:03 1:06<br />

Figure 57: Displacement on <strong>the</strong> surface for different side slopes<br />

Results<br />

The results <strong>of</strong> this <strong>analysis</strong> and <strong>the</strong> value <strong>of</strong> this research project provide a new<br />

potentially more reliable way to predict <strong>the</strong> life <strong>of</strong> asphalt pavements subjected to cyclic<br />

loads, involving different variables, such as, tire widths, hot mix asphalt and thicknesses<br />

<strong>of</strong> asphalt layer. What makes this <strong>analysis</strong> unique is <strong>the</strong> possibility to predict which<br />

combination <strong>of</strong> design variables gives <strong>the</strong> best service life. One limitation to this <strong>analysis</strong><br />

is that no damage is considered. Since no damage is taken in consideration, an empirical


86<br />

but physically meaningful criterion is adopted. In addition, <strong>the</strong> actual number obtained as<br />

a result from <strong>the</strong> <strong>finite</strong> <strong>element</strong> code does not represent <strong>the</strong> real life <strong>of</strong> a pavement.<br />

We start <strong>the</strong> <strong>analysis</strong> by defining <strong>the</strong> failure criterion used. The failure criterion is<br />

not <strong>the</strong> main thrust <strong>of</strong> this research and we have chosen a simple one in order to<br />

demonstrate <strong>the</strong> technique. A more accurate failure criterion will be a subject to be<br />

incorporated as a future work. All pavements involved have <strong>the</strong> same base and sub-base<br />

thicknesses, <strong>the</strong> only possibility <strong>of</strong> variation is <strong>the</strong> top layer composed by <strong>the</strong> HMA.<br />

However, <strong>the</strong> overall thickness remains <strong>the</strong> same by changing <strong>the</strong> subgrade thickness.<br />

The pavement is said to fail when <strong>the</strong> difference between <strong>the</strong> asphalt layer thickness and<br />

<strong>the</strong> maximum displacement on <strong>the</strong> surface becomes less than <strong>the</strong> average size <strong>of</strong> <strong>the</strong><br />

aggregate in <strong>the</strong> mixture. Figure 58 shows two simple cases with different asphalt layer<br />

thicknesses to explain <strong>the</strong> failure criterion. Consider <strong>the</strong> roadway in case b with thickness<br />

b<br />

h greater than <strong>the</strong> roadway in case a with thickness<br />

a<br />

h . Note that at time t = 0 a force<br />

F( x, t)<br />

is applied to <strong>the</strong> surface in both cases and <strong>the</strong> displacement are measured at<br />

b<br />

a<br />

time = t 1<br />

. In case b, <strong>the</strong> displacement ( δ ) is greater than in case a ( δ ), but<br />

where,<br />

Also, when<br />

h<br />

−δ<br />

≤h<br />

− δ<br />

b b a a<br />

( h −δ<br />

or h −δ<br />

) ≤ D<br />

a a b b MAX<br />

MAX<br />

D is <strong>the</strong> maximum size <strong>of</strong> <strong>the</strong> aggregate in <strong>the</strong> mixture, which in this case is<br />

considered to be 2 cm, <strong>the</strong> pavement is considered to fail. Note also that <strong>the</strong> picture is<br />

exaggerating <strong>the</strong> displacement, however δ is not greater than <strong>the</strong> thickness ( h ) <strong>of</strong> <strong>the</strong><br />

roadway.


87<br />

Figure 58: Failure criterion<br />

This computer simulation requires an extraordinary amount <strong>of</strong> computer<br />

processing and would make <strong>the</strong> work practically unachievable to conduct over a longer<br />

period <strong>of</strong> time, such as one full year. Since our prediction does not involve damage, we<br />

show that it is possible to extrapolate <strong>the</strong> results after a certain number <strong>of</strong> cycles. This can<br />

be done by 1) running <strong>the</strong> problem up to 3000 seconds or 150 cycles <strong>of</strong> 20 seconds,<br />

instead <strong>of</strong> <strong>the</strong> full year, and 2) adding a trend line to <strong>the</strong> data. Figure 59 and Figure 60<br />

clarify this idea, by showing <strong>the</strong> graphic with <strong>the</strong> maximum displacement on <strong>the</strong> surface<br />

versus time and followed by <strong>the</strong> same graphic in log scale, making it easier to see <strong>the</strong><br />

tendency.


88<br />

0.00018<br />

0.00016<br />

Maximum Displacement (m<br />

0.00014<br />

0.00012<br />

0.0001<br />

0.00008<br />

0.00006<br />

0.00004<br />

0.00002<br />

0<br />

0 500 1000 1500 2000 2500<br />

Time (s)<br />

Figure 59: Displacement versus time<br />

Maximum Displacement (m)<br />

0.01 0.1 1 10 100 1000 10000<br />

0.00018<br />

0.00016<br />

0.00014<br />

0.00012<br />

0.0001<br />

0.00008<br />

0.00006<br />

0.00004<br />

0.00002<br />

0<br />

Time (s)<br />

Trend line<br />

Figure 60: Displacement versus time in log scale<br />

As it can be seen in both graphics, <strong>the</strong> displacements are varying in a cyclic way<br />

according to <strong>the</strong> load. The top part reflects <strong>the</strong> pavement being loaded and <strong>the</strong> lowest<br />

part where <strong>the</strong> trend line is positioned corresponds to <strong>the</strong> pavement being unloaded. The


89<br />

trend line is placed where a permanent deformation is observed. Notice in Figure 60 that<br />

after around 500 seconds a linear approximation makes an appropriate choice for <strong>the</strong><br />

extrapolation. This choice is based on <strong>the</strong> R 2 value for each graphic. A trendline is most<br />

reliable when its R 2 value is at or near 1. 44<br />

The first <strong>analysis</strong> is done by keeping <strong>the</strong> HMA thickness in 10 cm and two types<br />

<strong>of</strong> mixtures. The design variable to be compared in <strong>the</strong> next three graphics is <strong>the</strong> different<br />

tire widths.<br />

HMA Thickness 10 cm<br />

250<br />

211.4<br />

Time (year)<br />

200<br />

150<br />

100<br />

50<br />

34.8<br />

26.2<br />

140.9<br />

28.8<br />

158.5<br />

0<br />

29.5 cm 44.5 cm 49.5 cm<br />

Tire Width<br />

AC I (See Table 2) AC II (See Table 3)<br />

Figure 61: Different tire configurations for HMA thickness <strong>of</strong> 10cm<br />

44 R 2 value is a number from 0 to 1 that reveals how closely <strong>the</strong> estimated values for <strong>the</strong> trendline<br />

correspond to your actual data. A trendline is most reliable when its R 2 value is at or near 1. It is also<br />

known as <strong>the</strong> coefficient <strong>of</strong> determination.


90<br />

HMA Thickness 15 cm<br />

Time (year)<br />

300<br />

250<br />

200<br />

150<br />

100<br />

50<br />

0<br />

257.6<br />

187.1<br />

164.9<br />

40.8<br />

29.2<br />

32.0<br />

29.5 cm 44.5 cm 49.5 cm<br />

Tire Width<br />

AC I (See Table 2) AC II (See Table 3)<br />

Figure 62: Different tire configurations for HMA thickness <strong>of</strong> 15cm<br />

HMA Thickness 20 cm<br />

Time (year)<br />

350<br />

300<br />

250<br />

200<br />

150<br />

100<br />

50<br />

0<br />

300.4<br />

190.3<br />

203.8<br />

46.0<br />

31.9<br />

34.6<br />

29.5 cm 44.5 cm 49.5 cm<br />

Tire Width<br />

AC I (See Table 2) AC II (See Table 3)<br />

Figure 63: Different tire configurations for HMA thickness <strong>of</strong> 20cm


91<br />

As it can be seem from Figure 61, Figure 62 and Figure 63 a comparison between<br />

tires widths is presented and <strong>the</strong> tire width 29.5 cm gives <strong>the</strong> best pavement life for all <strong>the</strong><br />

thicknesses and <strong>the</strong> two mixtures. The wide tires 44.5 cm always gives <strong>the</strong> least life, and<br />

49.5 cm is always intermediate. The 29.5 cm tire width gives a pavement life<br />

approximately 50% better than if <strong>the</strong> wide tire 44.5 cm is used and around 40% better life<br />

if <strong>the</strong> comparison is between <strong>the</strong> dual tire 29.5 cm and wide tire 49.5 cm. If <strong>the</strong> two wide<br />

tires are compared, <strong>the</strong> wide tire 49.5 cm gives a better life <strong>of</strong> around 10% more than <strong>the</strong><br />

44.5 cm wide tire. It is a good point to notice that among <strong>the</strong> wide tires, <strong>the</strong> wider <strong>the</strong> tire,<br />

<strong>the</strong> better <strong>the</strong> pavement life. Note also, if you compare in one graphic, <strong>the</strong> AC II gives a<br />

better life in all cases compared to AC I, as a result <strong>of</strong> being a stiffer mixture.<br />

Tire Width 29.5 cm<br />

Time (year)<br />

350<br />

300<br />

250<br />

200<br />

150<br />

100<br />

50<br />

0<br />

300.4<br />

257.6<br />

211.4<br />

34.8<br />

40.8<br />

46.0<br />

10 cm 15 cm 20 cm<br />

HMA Thickness<br />

AC I (See Table 2) AC II (See Table 3)<br />

Figure 64: Different HMA thicknesses for dual tires 29.5 cm<br />

Now we turn our attention to comparing life for different thicknesses <strong>of</strong> asphalt<br />

layer. Three thicknesses are presented in each graphic for two different mixtures. Three


92<br />

graphics are presented, each one with applied from a different tire configuration. By<br />

looking at Figure 64 with dual tire configurations, it can be seem that by increasing <strong>the</strong><br />

thickness <strong>of</strong> <strong>the</strong> asphalt layer, <strong>the</strong> life increases for both mixtures. If a 15 cm thick layer<br />

is used as opposed to a 10 cm, <strong>the</strong> life goes up by 22% for AC II and 18% if AC I is used.<br />

Figure 65 shows if a 44.5 cm wide tire is used and a 15 cm is used, instead <strong>of</strong> a 10 cm,<br />

<strong>the</strong> life goes up about 17% for AC II and 12% for AC I. On <strong>the</strong> o<strong>the</strong>r hand if a 49.5 cm is<br />

used it only increases life about 14% for AC II and 11% for AC I.<br />

If <strong>the</strong> thickness is increases from 10 cm to 20 cm, <strong>the</strong> life increases for all cases<br />

and mixtures. In <strong>the</strong> case <strong>of</strong> AC II it gives a better life <strong>of</strong> 42% for dual tires 29.5 cm; 35%<br />

for 44.5 cm wide tires and 29% for 49.5 cm wide tires. Note that <strong>the</strong> dual tires always<br />

give <strong>the</strong> better increase <strong>of</strong> life if <strong>the</strong> thickness is increased.<br />

Overall, dual tire configurations with 29.5 cm give <strong>the</strong> best pavement life in terms<br />

<strong>of</strong> all parameter and 44.5 cm gives <strong>the</strong> shortest pavement life. A 10 cm thickness <strong>of</strong><br />

asphalt layer gives <strong>the</strong> shortest life for all types <strong>of</strong> tire configurations and a 20 cm layer<br />

gives <strong>the</strong> best life. AC II gives <strong>the</strong> best life as opposed to AC I for all cases. This is a<br />

strong tool to be improved and used in pavement design, since it gives a reasonable<br />

comparison <strong>of</strong> how <strong>the</strong> pavement response will over <strong>the</strong> years and how to helps to make a<br />

decision <strong>of</strong> which geometry and materials use.


93<br />

Tire Width 44.5 cm<br />

200<br />

164.9<br />

190.3<br />

Time (year)<br />

150<br />

100<br />

50<br />

26.2<br />

140.9<br />

29.2<br />

31.9<br />

0<br />

10 cm 15 cm 20 cm<br />

HMA Thickness<br />

AC I (See Table 2) AC II (See Table 3)<br />

Figure 65: Different HMA thicknesses for dual tires 44.5 cm<br />

Tire Width 49.5 cm<br />

250<br />

200<br />

158.5<br />

180.7<br />

203.8<br />

Time (year)<br />

150<br />

100<br />

50<br />

28.8<br />

32.0<br />

34.6<br />

0<br />

10 cm 15 cm 20 cm<br />

HMA Thickness<br />

AC I (See Table 2) AC II (See Table 3)<br />

Figure 66: Different HMA thicknesses for dual tires 49.5 cm


94<br />

CONCLUSION<br />

A <strong>finite</strong> <strong>element</strong> <strong>viscoelastic</strong> model has been developed for <strong>the</strong> purpose <strong>of</strong><br />

analyzing service life <strong>of</strong> asphalt pavements subjected to different tire configurations,<br />

layer geometries and material properties. The primary motivations for this study is to<br />

model asphalt pavements and predict which combination <strong>of</strong> design variables increases<br />

and improves pavement life. The model gives a comparison <strong>of</strong> predicted lives for various<br />

roadway and tire configurations.<br />

The model compares <strong>the</strong> relative effect <strong>of</strong> wide base single tires and dual<br />

assemblies for equal inflation pressures and equal loads. Since this new generation <strong>of</strong><br />

tires is already approaching <strong>the</strong> US market and is intended to replace <strong>the</strong> dual tire<br />

configuration for a larger tire, <strong>the</strong> likelihood <strong>of</strong> damage to U.S. roadways must be<br />

evaluated. This technique is very powerful for designing pavement, allowing engineers to<br />

choose <strong>the</strong> best hot mix asphalt to be used. Also in pavement design, <strong>the</strong> model is able to<br />

predict how much longer <strong>the</strong> roadway will last if a thicker layer <strong>of</strong> hot mix asphalt is<br />

chosen.<br />

As expected, dual tire configurations give <strong>the</strong> best life if compared to <strong>the</strong> o<strong>the</strong>r<br />

two wide tire configurations for all mixtures and for all thicknesses. Additionally, for <strong>the</strong><br />

wide tire case, as tire size increases, <strong>the</strong> damage potential from tandem axles decreases.<br />

By analyzing pavement response to different thicknesses, it is observed that <strong>the</strong> thicker<br />

asphalt layer <strong>of</strong> 20 cm gives <strong>the</strong> best life for all mixtures and tire configurations<br />

compared to <strong>the</strong> thinner layers <strong>of</strong> 10cm and 15 cm. Ano<strong>the</strong>r advantage <strong>of</strong> this model is<br />

<strong>the</strong> capability <strong>of</strong> minimizing <strong>the</strong> need <strong>of</strong> extensively laboratory work, since <strong>the</strong><br />

predictions rely upon <strong>the</strong> fundamental structural properties <strong>of</strong> each layer. However,


95<br />

because <strong>the</strong> current generation <strong>of</strong> <strong>the</strong> model does not provide any source <strong>of</strong> energy<br />

dissipation in <strong>the</strong> form <strong>of</strong> cracks, it has certain limitations that are left as future work.


96<br />

FUTURE WORK<br />

It has been shown that computational modeling for pavements has great potential and can<br />

provide substantial benefits; however, many possibilities exist to continue to improve this<br />

research, such as:<br />

i. Extend <strong>the</strong> <strong>analysis</strong> capabilities to three dimensions. Even though <strong>the</strong><br />

computational effort will be much greater, <strong>the</strong> results will be more accurate;<br />

ii.<br />

Incorporate and model damage, in <strong>the</strong> form <strong>of</strong> discrete cracks, at any length scale<br />

by incorporating a type <strong>of</strong> fracture <strong>mechanics</strong> model to <strong>the</strong> <strong>analysis</strong>;<br />

iii.<br />

Introduce more realistic tire inflation pressures and contact areas and <strong>the</strong>ir effect<br />

on wide base single tires and dual tire configurations;<br />

iv.<br />

Analyze <strong>the</strong> effect on pavement life <strong>of</strong> possible under- and over- inflation in tires;<br />

v. Perform a qualitative field validation, to compare life <strong>of</strong> wide tires against dual<br />

tires;<br />

vi.<br />

Incorporate <strong>the</strong> effect <strong>of</strong> dynamic loading in <strong>the</strong> code.


97<br />

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