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Page 1: by - Lehigh University
Page 2: by - Lehigh University

, 'I :

APPLICATION OF LAYERED SYSTEM

ANALYSIS TO THE DESIGN OF FLEXIBLE PAVEMENTS

, ....... , ~

..

\

i

by

Humphrey Chishao Han

A thesis

Presented to the Graduate Faculty

of Lehigh University

in Partial Fulfillment of ~he

Requirements for the Degree of'

Master of Science in Civil Engineering

FRITZ ENGINEERINGLABORATORY LIBRARY

"

Lehigh University

Ap::i;.il 19·jJj""'\.

Page 3: by - Lehigh University
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,

ACKNOWLEDGEMENTS

The work described in this thesis was conducted in

the Geotechnical Engineering Division, Fritz Engineering

Laboratory, Lehigh University .

Special thanks are due for the encouragement from

Professor T. J. Hirst during this study.

The investigation was carried out under sponsor­

ship of the Pennsylvania Department of Transportation.

Sincere appreciation is expressed to this organization for

their support.

-iii-

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TABLE OF CONTENTS

ABSTRACT

I. INTRODUCTION

II. CURRENT STATUS OF KNOWLEDGE

2.1 The AASHO Design Committee's Finding

2.1.1 The AASHO Design Equation

2.1.2 Variables Involved in the AASHO

Design Equation

2.1.3 The Structural Number

2.1.4 Structural Coefficients (Thick­

ness Equivalency)

2.1.5 Evaluation of Structural Coef­

ficients

2.2 Elastic-Layered Theory

2.2.1 Boussinesq Equation

2.2.2 Burmister's Two-Layered System

Theory

2.3 Finite Element Analysis

2.3.1 Method of Analysis

2.3.1a Displacement Function

2.3.1b Strain of Element

2.3.1c Stress and Stiffness

Matrix

2.3.1d Solution of Element

Displacement

2.3.2 Computer Program

Page

1

3

5

5

5

7

8

9

10

11

12

14

16

18

18

19

20

23

23

III. DEVELOPMENT OF FIELD TESTING PROGRAM 26

3.1 Existing Construction Materials used in 26

Pennsylvania Flexible Pavements

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..

3.2

3.3

3.4

TABLE OF CONTENTS (Continued)

Selection of Test Sites

Test Site Layout

Plate Loading Test

27

28

28

,

IV. ANALYSIS OF PLATE LOADING TEST DATA

4.1 Plate Loading Test on Subgrade

4.1.1 Application of Burmister's Theory

4.1.2 Finite Element Analysis

4.1.3 Comparison of Results from Bur­

mister's Theory and Finite Ele­

ment Analysis

4.1.4 Variation of Subgrade Modulus

with Applied Pressure and Plate

Size

4.2 Plate Loading Tests on Layered Systems

4.2.1 Equivalent Two-Layered Theory

Applied to Multi-Layered

Systems

4.2.1a Determination of Upper

Layer Modulus in a Two­

Layered System

4.2.1b Determination of Upper

Layer Modulus in a

Multi-Layered System

4.2.2 Finite Element Analysis

4.2.3 Strength of Pavement Components

4.2.3a Subbase Courses

4.2.3b Base Courses

4.2.3c Surface Course

-v-

29

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30

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31

32

33

33

34

36

37

37

39

40

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..

TABLE OF CONTENTS (Continued)

V. EVALUATION OF STRUCTURAL COEFFICIENTS

5.1 Structural Coefficients for the

Surface, a l5.2 Structural Coefficients for Bases, a 25.3 Structural Coefficients for the

Subbase, a 3

VI. SUMMARY AND CONCLUSIONS

VII. TABLES.

VIII. FIGURES

IX. N.0MENCLATURE

X. BIBLT0GRAPHY

XI. kPPENDTX.

XII. VITA

-vi-

41

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81

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I •

Table

1

2

3

4

5

6

7

8

9

10

LIST OF TABLES

Structural Coefficients Determined in

AASHO Road Test

Plate Sizes and unit Pressures

Comparison of Subgrade Modulus for 12 in.

Plate Obtained from Finite Element Analy-

sis and Burmister's Equation

Comparison of Subgrade Modulus for 30 in.

Plate Obtained from Finite Element Analy-

sis and Burmister's Equation

Variation of Subgrade Modulus with Various

Pressures for 12 in. Plate

Variation of Subgrade Moduluswith Various

Applied Pressures for 30 in. Plate

variation of Subgrade Modulus with Plate

Size

Individual Modulus of Pavement Components

(obtained from equivalent two-layered

system approach)

Individual Modulus of Pavement Components

(obtained from finite element analysis)

Structural Coefficients of Pavement

Material (correlated from Moduli obtained

from finite element analysis)-v~~-

48

49

50

51

52

53

54

55

56

57

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If

Table

11

LIST OF TABLES (Continued)

Structural Coefficients of Pavement

Materials (Correlated fr-om Moduli ob­

tained from Equivalent Two-Layered

System

-viii-

Page

58

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Page

60

61

62

63

Figure

1

2

3

4

5

6

7

8

9

10

11

12

13

14

LIST OF FIGURES

AASHO Design Chart

Values of Deflection Factor, F

Finite Element Idealizat~on of a Cylinder

Triangular Element in an Axisymmetric

Solid

Simplified Flow Diagram of Finite Element 64

Computer Program

Iterative Solution to Layer Moduli 65

Theoretical Experimental Design 66

Deflection vs. Subgrade Modulus for'Various 67

Applied Pressures on ¢12- irt-. ~P.late

Deflection vs. Subgrade Modulus for Various 68

Applied Pressures on ¢30 in. Plate

Finite Element Configuration used for Analy- 69

sis of Homogeneous Subgrade

Determination of Individual Modulus by 70

using Equivalent Two-Layered Theory

Pressure vs. Deflection for ¢12 in. Plate 71

Pressure vs. Deflection for ¢12 in. Plate 72

Finite Element Configuration used for Analy- 73

sis of Layered System - Deep Bottom Boundary

-ix-

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Figure

15

16

17

18

19

20

21

LIST OF FIGURES (Continued)

Point Loads Converted from Unit Pres­

sures Applied on Plates of Various Sizes

(Finite Element Analysis)

Variation of Subbase Modulus with Thick­

ness (Equivalent Two-Layered System

Approach)

Variation of Subbase Modulus with Thick­

ness (Finite Element Analysis)

Variation of Base Moduli with Thickness

(Equivalent Two-Layered System Approach)

Variation of Base Moduli with Thickness

(Finite Element Analysis)

Variation of Surface Moduli with Thick­

ness (Equivalent Two-Layered Approach)

Correlation of Coefficient of Surface

with Marshall Stability (by Illinois)

-x-

Page

74

75

76

77

78

79

80

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ABSTRACT

In 1962, a new flexible pavement design method,

the AASHO Interim Guide for Flexible Pavement Design, was

developed by the AASHO Committee on Design. Although the

method has gained wide acceptance in this country and is

currently used in Pennsylvania to design flexible pave-

-ments, it is limited in precise application to areas where

the soil types and environmental conditions are similar to

those upon which the method is based (the AASHO Road Test

site, Ottawa, Illinois). One limitation of the Interim

Guide is that no guidance is given for selecting structural

coefficients for materials different to those used in the

AASHO Road Test. The objective of this work is to

use existing elastic theories to determine the modulus of

each pavement component from plate loading test data ob­

tained at the surface of each layer and to develop structural

coefficients from the moduli.

Two approaches, an equivalent Burmister's two-

layered theory and a finite element analysis, are used to

determine the individual moduli of pavement components.

It has been found that, within the linear elastic

range, the subgrade modulus is independent of the applied

pressure but dependent on the size of bearing area. A range

-1-

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of effective thickness has been established for the sub-

base in which the subbase modulus increases with increasing

thickness. This effective thickness is approximately equal

to 1.5 times the loaded area. For stabilized base materials,

moduli appear independent of thickness. Tentative values of

structural coefficients of pavement materials based on corre­

lation of their moduli are presented.

-2-

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)

I. INTRODUCTION

In 1962, following completion of the Road Test,

the American Association of state Highway Officials (AASHO)

Design Committee reported the development of the AASHO In­

terim Design Guide for flexible pavements. This Guide was

based on the results of the AASHO Road Test, supplemented by

existing design procedures. Although the method has been

widely accepted, it is limited in precise application to

areas where the soil type and environmental conditions are

similar to those upon which the method is based (the AASHO

Road Test site, Ottawa, Illinois). One limitation of the

Design Guide is that no guidance is given for selection of

structural coefficients of pavement materials which differ

from those used in the AASHO Road Test.

Since flexible pavement design is a layered­

system problem, one of the major inputs is the individual

moduli of the pavement materials. These moduli are usually

determined by laboratory triaxial tests, repeated-load

tests or simply by engineering judgement. However, it was

pointed out by Burmister (1943) in his layered theory, and

confirmed by McLeod (1965), by having analyzed the Hybla

va~ley data, that the values of pavement component moduli

might not be constant and independent of thickness and

-3~

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size of loading area. The modulus may increase as the

loading area increases and thickness of the layer component

remains constant or the modulus may increase as the thick­

ness of the layer component increases and the loading area

remains constant. Therefore, attention has been directed

at determining the individual moduli of pavement components

by using data obtained from a series of field plate loading

tests performed on the surface of each pavement component.

Based on the individual modulus, the relative contribution

(structural coefficient) of each layer of the pavement to

the AASHO design equation can be evaluated.

This thesis includes a brief review of the current

state of knowledge in flexible pavement design, including

the AASHO Design equation, the elastic-layered theory

(Boussinesq equation and Burmister's two-layered system

theory) ,and the axisymmetric finite element theory. De­

scriptions of the field testing program are presented. Out­

lines of the application of both the elastic-layered theory

and the axisymmetric finite element analysis to evaluate

the modulus of each pavement component are described. The

structural coefficients in the AASHO design, determined from

the individual modulus for materials used in Pennsylvania,

are presented.

-4-

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..

II. CURRENT STATUS OF KNOWLEDGE

2.1 The AASHO Design Committee's Finding

In 1962, the American Association of State Highway

Officials (AASHO) Design Committee reported the development

of the AASHO Interim Design Guide for flexible pavements.

This Guide was based on the results of the AASHO Road Test,

supplemented by existing design procedures.

2.1.1 The AASHO Design Equation

For l8-kip single-axle load applications, the

general AASHO Road Test equation for flexible pavement de-

sign is,

logw18 = 9.36

where

Glog(SN+l)-0.20+ 1,094

0.4+ 5 19(SN+l) •

(1)

...

W18 = total equivalent l8-kip single-axle loads

expected during the design life of the

facility.

SN = structural 'numb~r

G = logarithmic expression of initial and

desired terminal serviceability. Frequently,

-5-

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..

..

..

G is assumed to be 2.5 for primary, heavy

duty highways and 2.0 for secondary, low

traffic highways

Equation (1) is a mathematical expression of the

Road Test results and gives the number of l8-kip axle load

applications, w18 ' required to reduce the serviceability to

a certain value for a pavement having a structural number of

SN.

In order to properly account for environmental in­

fluences on the behavior of the pavement materials, a re­

gLonal factor, R, is introduced into the design procedure

to permit variation in design. There is no rational proce­

dure available to evaluate the regional factor for the various

conditions present throughout the country. Although guide­

lines and suggested values were proposed by the Design Com­

mittee (Langsner, Huff, and Liddle, 1962), there has been

very little progress in the development of specific regional

factors.

Due to a wide variety of subgrade soil ty.pes on

which the pavement is constructed, a soil support scale has

been established by correlation with a number of other design

procedures, extending the AASHO Design equation to geographic

-6-

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areas which have soil characteristics different from those

at the test site. It has been found that the correlation

varies with the soil testing procedure used and the manner

in which the test is run. If the regional factor R and the

soil strength, expressed as soil support, SS, are intro-

duced, Eq~, (1) becomes

logwis1= 9.36 log(SN+l)+0.372(SS-3.0)+log(R)

G-0.20+ 1 094o. 4 0 +-~':.....:....:::....;.--::--:­

(SN+l)S.19

(2 )

..

..

Equation (2) has been reduced to nomographic form

for design purposes and is shown in Fig. 1.

2.1.2 Variables Involved in the AASHO Design Equation

From Fig. 1 it is seen that to apply the AASHO

Interim Guide to the design of a flexible pavement, it is

necessary to evaluate each of the parameters in the design

equation, including the soil support value, SS, the regional

factor, R, the estimated average daily traffic Wis' the

value of G for the initial and terminal serviceability de-

sired, and the design life of the pavement. From the knowl-

edge of these variables, the AASHO design chart can be

-7-

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readily used to solve for the required structural number of

the proposed pavement.

2.1.3 The Structural Number

In the 1962 International Conference on Structural

Design of Asphalt Pavements, W. J. Liddle presented a method

of determining layer thickness from the structural number

(SN) developed by the AASHO Operating Committee on Design.

The relationship is expressed by the general equation

(3)

where

a l ,a2 ,a3 = structural coefficients or relative

strength of bituminous surface, base,

and subbase courses respectively

Dl ,D2 ,D 3 = thicknesses of bituminous surface,

base, and subbase courses respec­

tively, in inches

Thus, the structural number expresses a relationship be­

tween the thickness of a component layer in a pavement

structure and the type of material used in constructing

the layer. ~8-

Page 20: by - Lehigh University

Table 1 shows the coefficients established in

the AASHO Road Test for the types of surface course, base

course, and subbase used in the project.

For the same value of structural number, there may

be many combinations of surface, base, and subbase thick­

nesses.

2.1.4 Structural Coefficients (Thickness Equivalency)

The structural coefficient was one of the most

significant parameters to emerge from the Road Test. In the

application of the AASHO design method, the correct coeffi­

cient values of pavement materials are of immediate impor­

tance.

The structural coefficients determined in the AASHO

Road Test (Table 1) are statistically derived from the analy­

sis of the performance data obtained at the Road Test. In

other words, the individual values are evaluated mathema­

tically instead of being determined from physically measured

properties. In addition, the structural coefficients are

valid only for a layered pavement system having the same ar­

rangement of pavement components as those in the Road Test

(surface, base, subbase, and subgrade) .

-9-

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Actually, the structural coefficient can be de­

scribed as a thickness equivalency or an index of the load­

carrying capacity of a material. It may be considered as

the ratio of the strength of a I-in. thickness of the mate­

rial to that of 1 in. of any reference material.

2.1.5 Evaluation of Structural Coefficients

One of the major objectives of the AASHO Road

Test was to determine, under specified ~~. axle loads of

varying magnitude and arrangement, the required thickness of

asphalt concrete surfaces on different thicknesses of base

and subbase for a basement soil of known characteristics.

Although the Road Test has established coefficients

for various surface, base, and subbase courses used at the

Road Test, consideration must be given to determining the

structural coefficients as a function of material types

which are different from those used at the Road Test.

Studies needed fall into four categories:

theoretical studies; (2) major satellite studies;

tests; and (4) laboratory tests.

(I)

(3) field

The simplest and most straight-forward method of

evaluating the structural coefficients is by correlation

-10-

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studies in which laboratory tests measuring the properties

of materials similar to the Road Test are performed. Ratios,

relative scales or graphs are then established.

The studies reported herein use field plate load-

ing test data to determine the individual modulus of each

pavement component through the use of elastic-layered theory

and finite element analysis. From these, the ratios of

modulus of base and subbase to that of asphalt concrete

surfaces may be obtained. The structural coefficients of

each layer canobe~:eva1:\:1:ated~.by:tdetermining-:'the!?t:tuctur.al:~co­

effiG:ient'"for one lay.er, .such as the asphalt concrete surface,

by. direct 'correlati9h.. wi th~~.a~ physical test::such" as-; the Marshall

test.

2.2 Elastic-Layered Theory

Since a flexible pavement is a layered system, it

is logical to apply some form of layered system theory to

the problem. The basic assumption underlying elastic layered

system theory is that the materials which constitute the in­

dividual layers are linearly elastic and:. are charact~rized by

time-independent constants of proportionality between stress

and strain. Generally, along with the assumption of linear

elasticity, each material is assumed to be continuous, homo­

geneous, and isotropic. Although viscoelastic layered sys-

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Page 23: by - Lehigh University

terns have been studied .±n ~so:rn.e detail -anaTytl:cal-1y, and

asphalt concrete is known to possess certain nonlinear pro-

perties, it can be assumed to behave linearly under normal

operating conditions (Sisko and Brunstrum, 1969).

In recent years, there has been considerable

interest in the application of theories of elasticity to

the structural design of asphalt pavements. The theory of

elasticity was first applied to soil problems by Boussinesq

(1885). Burmister (1943) was the first one to develop the

two- and three-layer elastic theory for pavement design.

2.2.1 Boussinesq Equation

Boussinesq assumed that the material is an elas-

tic, isotropic and homogeneous semi-infinite half-space.

with this assumption, those characteristics of the material

which influence the stresses and strains in the system are

the modulus of elasticity E and Poisson's ratio~. The

deflection at the center of a circularly loaded area is~

For flexibly. loaded areas:

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For rigidly loaded areas:

where

(5 )

6 = deflection at the center of the loaded area

associated with the pressure

E = modulus of elasticity of the material

cr = unit pressure applied to the surface of the

loaded area

r = radius of the loaded area

~ = Poisson's ratio of the material

Poisson's ratio for soils generally range from 0

to 0.5. If 0.5 is chosen, Eqs;, 0 (41) and (5) become

For flexibly loaded areas:

6 = l.5~r, E = l.5~r

For rigidly loaded areas:

6 = l.l8~r, E = l.l8~r

-13-

(4a)

(Sa)

Page 25: by - Lehigh University

By knowing the applied unit pressure, the radius

of the loaded area, and the surface deflection, Eqs;o (4a)

and (Sa) can be used to determine the modulus of elasticity.

Equation (Sa) can be used to determine the subgrade modulus

in situ by means of --:; loading tests on the

subgrade.

2.2.2 BurmisterLs Two-Layered System Theory

The two- and three-layer elastic theory, developed

by Burmister (1943 and 1945), considered the pavement as an

elastic layer resting on a semi-infinite elastic subgrade.

Due to the complexity of the mathematics involved, this

theory was once considered to be of limited application and

only a few numerical solutions were pUblished (Fox, 1948; Acum

&~Fdx,19S1). It is only since the advent of high speed digi­

tal computers that the theory has gained increased .L..-;-;' ---.

importance~and has been extended to multilayer systems

(Warren and Dieckman, 1963).

Assumptions made in Burmister's two-layered system

theory are:

(1) The soils of each of two layers are homoge­

neous, isotropic, and linearly elastic.

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(2) The upper layer (layer l) is

weightless and is of infinite extent in the horizontal

direction, but of finite thickness. The lower layer (sub-

grade) is infinite in extent both horizon-

tally and vertically downward.

(3) Boundary conditions

(a) the surface of the upper layer is free

of normal and shearing stress outside the limit of the

loading area.

(b) at infinite depth the stresses and dis­

placements in the subgrade are equal to zero.

(4) The solution of the two-layer problem satis­

fies the continuity condition of stress and displacement

across the interface between the upper and lower layers,

i.e. at the interface, the normal and shearing stresses and

the vertical and horizontal displacements are equal in the

two layers.

(5) The value of the Poisson's ratio is 0.5 •

Based on the above assumptions Burmister has re­

duced the complicated differential equation to simple ex­

pressions as follows:

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For flexibly loaded areas:

(6 )

For rigidly loaded areas:

(7 )

where E2 is the modulus of lower layer (subgrade) and F is

called the deflection factor which is dimensionless and is

a function of both ratio of the modulus of elasticity of

the subgrade to that of the pavement and the depth to bear-

ing radius ratio.

Figure 2 shows values of F for various depth

ratios and moduli of elasticity. Additional tables and

charts have been published by Hank and Scrivner (1948), Fox

(1948), and Jones (1962).

2.3 Finite Element Analysis

There have been many layered-system approaches

based on theory of elasticity to solve the stress and dis-

placement pavement problem. However, due to the complexity

of the mathematics involved, it is rather difficult to ob-

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Page 28: by - Lehigh University

tain an exact solution of the differential equations. The

finite difference method has been the most popular of the

numerical techniques. However, for structures of composite

materials such as highway pavements, this procedure is dif­

ficult to apply.

Clough and Rashid (1965) used an axisymmetric

finite element analysis to solve for the stress distribution

in a semi-infinite elastic solid subjected to a concentrated

load at the surface. The results were in reasonable ~gree­

ment with the well known classic problem of elasticity solved

by Boussinesq (1885).

Recently, the finite element method was applied

to the analysis of a pavement system subjected to axisymme­

tric loads (Duncan, Monismith, and Wilson, 1968). The

stresses and deflections so obtained were found to be in

reasonable agreement with those determined from other lay­

ered system solutions.

The advantage of the finite element method is

that it can be quite generally formulated with respect to

geometry and material properties. This method is parti­

cularly useful for solving problems in layered pavements

composed of many different materials.

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2.3.1 Method of Analysis

In the finite element approximation for axisymme-

tric solids, the continuous structure is replaced by a system

of axisymmetric elements which are interconnected at circum-

ferential joints. Figure 3 illustrates a finite element

idealization of a typical axisymmetric solid cylinder in

which the distribution of stress in the body of revolution

under axisymmetric loading is reduced to a two dimensional

problem.

2.3.la Displacement Function

For a triangular element with nodes i, j, m,

lettered anticlockwise, the nodal point displacement (Fig.

4) may be expressed as:

u.{o.} = { l}

1 V.1

where

o. = nodal point displacement1

U. = displacement of nodal point in radial1

direction

V. = displacement of nodal point in vertical1

direction

-18-

(8)

Page 30: by - Lehigh University

The element displacement is similarly expressed as:

O.~

= . {O· }J

om

(9)

where the position of nodal point i is located by the cylin-

drical coordinate system Rand Z.

Letting the displacements at any point within the

element be defined as a column vector, {F (R, Z) }, the dis-

placement function {F} within the element will be

{F}

O.1

= [N.N.N ]{o.}~ J m J

Om(10)

in which the components of [N] are in general functions of

position.

2.3.1b Strain of Element

•is

The strain function, E, in an axisymmetric system

E: ZE:

= { R} = {E: eYRZ

av/az

ClU/aR

U/R

Cl U/ClZ+ClV/ClR

-19-

}(11)

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With displacements known at all points within

the element from Eq'., (10) ~ the strain at any point can be

determined as

'{s} = [B] {ole = [B. B . B ] { o} e1 J m

(12)

From Eq., (10), with the functions N., N., Nm" 1 J

already determined, the matrix [B] can be obtained. If the

linear form of these functions is adopted then strains will

be constant throughout the element.

2.3.1c Stress and Stiffness Matrix

Assuming general elastic behavior in which the

material is a homogeneous, isotropic, linear elastic solid,

the relationship between stresses and strains will be linear

of the form

{a} = [D] {s} .. _{13)

where [D] is an elasticity matrix containing the appro-

priate material properties. Let

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F.1

= {F.}J

Fm

(14)

define the nodal forces in the Rand Z directions, which

are statically equivalent to the boundary stress and/or dis-

tributed loads on the element.

If a virtual displacement of the element,· {o*}, is

introduced, then Eq. (10) becomes

{f*} = [N] {o*}e

and Equ. (9) becomes

(15)

(16)

Thus, the external work done by the nodal forces, {F.}, will1

be

(17)

and the internal work per unit volume done by the stresses

and/or distributed force will be

(18)

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in which {p} is the body force. By equating the internal

and external work done in the element

T{o*}e • {F}e =' /h:*}T{cr}dV-:-/{f*}T {P}dV

where V is the volume of the element. Since' {o*}e is arbi-

tary,

If the body force is zero, P = 0

If we let

and express the volume in terms of Rand Z then

-22-

(20)

( 21)

(22)

Page 34: by - Lehigh University

(23)

[K] is known as the stiffness matrix, wherein the

[B] matrix is dependent on the cylindrical coordinates Rand

z.

2.3.ld Solution of Element Displacements

The characteristic relationship of applied force

and displacement of an elastic element is

[K] [0] = [F] (24)

where [F] represents the nodal forces required to balance

any distributed loads acting on the element. After the

stiffness has been solved, the displacements can then be

determined.

2.3.2 Computer Program

By using an over-relaxation method, a finite

element computer program for linearly elastic analysis of

an axisymmetric solid with axisymmetric boundary conditions

was used to solve the simultaneous equations in Eq. (24) to

obtain the element displacements.-23-

Page 35: by - Lehigh University

Using this program, the structure to be analyzed

is divided into a series of triangles. The configuration

between elements and nodal points is generated by the compu­

ter program with the input of vertical and horizontal incre-

ments.

The amount of computer time required to solve a

finite element problem depends on the number of nodal points

and elements used to represent the system. For efficient

operation, this should be kept to the minimum necessary for

an accurate representation of the system under study. The

number of elements required is dependent both on the criteria

for element sizes and shapes and on the size of the region

which must be represented for valid simulation of the actual

problem. The way to establish criteria for boundary condi-

tions is either to examine finite element solutions to pro-

blems for which other solutions are available, or to deter-

mine them experimentally.

This program can handle up to 530 nodal points

and 1000 elements. It has been checked exactly against

the program developed by Duncan, Monismith and Wilson (1968)

by applying the same inputs to the program (a 12 in. diame-

ter plate with applied pressure of 100 psi on a subgrade with

modulus ESG = 10,000 psi and Poisson's ratio ~ = 0.4).

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To determine the individual moduli of each pavement

component in a layered system, it is necessary to start with

the deflection measured on the subgrade from which a modulus

can be established (using either Eq.t (5a) or the finite

element program). With the subgrade modulus determined, sub­

base deflections can be used to determine the modulus of the

subbase. This procedure can be repeated for successive lay­

ers working upward. Figures 5 and 6 show a simplified flow

diagram for the finite element program and a pictorial repre­

sentation of the iterative process for determining the modu­

lus of each layer.

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ir '

III. DEVELOPMENT OF FIELD TESTING PROGRAM

In order to evaluate the behavior of Pennsylvania

flexible pavements and to reconcile the Interim Guide to

local conditions, it was decided to set up a field test pro-

gram in which all the tests were similar to those performed

at the AASHO Road Test. The field tests were made in the

eastern part of Pennsylvania over the summers of 1969 and 1970.

3.1 Existing Construction Materials and in PennsylvaniaFlexible Pavements

~ • The majority of flexible pavements tested are con-

structed of seven components. There is one asphalt concrete

surface type, five base types (aggregate bituminous, aggre-

gate cement, aggregate lime pozzolan, bituminous concrete,

and crushed aggregate), and one subbase type; -, (crush aggre-

gate) •

The thicknesses of surfaces ranged from 2.6 in. to

3.7 in., the bases from 5.9 in. to 8.8 in., and the subbases

from 5.2 in. to 12.7 in.

Figure 7 shows the original experimental design of

the test sites. Numbers in blocks are test site identifica-

tions in which the first digit represents the base type and

• the second represents subgrade type.

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3.2 Selection of Test Sites

The experimental program was designed to include

three types of subgrade soil encompassing low, medium, and

high supporting values corresponding to an approximate range

of CBR values of 5-15, 15-40, and 40-100 respectively. In

addition, five pavement types were included (one surface and

one subbase, combined with five base types as described in

Section (3.1». Thus, for a complete factorial, the field

experiment consisted of a combination of fifteen sites. In

addition, four replicate sites were included~d

Because of the extensive nature of the field

testing program, it was decided that the testing program

would be conducted over two summers (1969 and 1970), with

each summer's work being essentially independent of the

other. This procedure provided an additional advantage by

permitting adjustments in the experimental design to be made

during the intervening winter in those cases where the field

tests indicated that the initial experimental design desig­

nations were in error. Error arose mainly from modification

of the support soil classifications following actual field

testing of the support soil.

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I •

3.3 rest Site Layout

Each test site was 1000 feet long. Three test

pits were selected at random in the outer wheel path. De­

tail lists of the field tests performed at each site are

given in the Appendix.

3.4 Plate Loading Test

One of the more satisfactory field tests is the

plate loading test, since the bearing area, the magnitude of

the applied load, and extent of influence on the pavement

system is similar to the actual vehicle loading condition.

A series of plate loading tests were conducted on

the surface of each layer at pit 2 (see Appendix) in every

site. For each test three different unit pressures were ap­

plied and released for measurement of deflection and rebound

movements of the plates. The plate sizes and various unit

pressures used for measurements are given in Table 2. For

the 1970 test sites, it was decided that an additional 12

in. diameter plate loading test should be performed on the

surface of each sublayer at pit 2 in order to obtain more

information concerning the strength properties of pavement

components.

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IV. ANALYSIS OF PLATE LOADING TEST DATA

4.1 Plate Loading Test on Subgrade

A 30 in. diameter plate loading test was conducted

using three cycles of applied loads on the subgrade. It was

felt that additional information would be needed for the

analysis of strength of pavement components in the layered

system, therefore, an additional 12 in. diameter plate load-

ing test was also conducted on the subgrade at pit 2 of the

1970 test sites.

Both the Burmister layered system approach and the

finite element analysis were applied to the data obtained

from these tests.

4.1.1 Application of Burmister's Theory

By setting the settlement factor F equal to unity

(i.e. for a single layer) Eq. (7) may be written for the sub-

•grade modulus as:

ESG = 1.18ar FLl SG ( 25)

This was used to determine the subgrade moduli shown with

dotted lines in Figs. 8 and 9 for 12 in. diameter and 30 in.

diameter plates.

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..

.'

4.1.2 Finite Element Analysis

The finite element computer program was used to

analyze the plate load data on the subgrade. The boundary

conditions were that, (i) the nodal points in the finite

elements were fixed at a depth of 18 radii for the bottom

boundary and (ii), they were constrained from moving radial-

lyon the vertical boundary at a distance of 12 radii from

the center (Fig. 10). It is obvious that the nodal points

on the centerline (left boundary in Fig. 10) can only move

vertically because of the axisymmetric loading condition .

Subgrade moduli computed from finite element analy-

ses are shown with solid lines in Figs. 8 and 9 for 12 in.

and 30 in. diameter plates.

4.1. 3 Comparisons of Results from Burmister' s Theory andFinite Element Analysis

By using the field plate loading data, the sub-

grade moduli obtained from Burmister's theory and from the

finite element analysis for 12 in. diameter and 30 in. dia-

meter plates under applied pressures of 48 psi and 15 psi,

respectively, are shown in Tables 3 and 4. It may be seen

that the deviation between subgrade moduli obtained from

Burmister's theory and from the finite element analysis are

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small. In other words, either the Burmister's theory or

the finite element analysis provide a good determination of

subgrade moduli. However, moduli obtained from the latter

method usually are a little higher than the former. This

might be because of the different boundary conditions of the

two approaches and the selection of Poisson's value ~ (0.5

was assigned to ~ in Eq~r (7) and 0.4 was used for ~ in the

finite element analysis).

4.1.4 Variation of Subgrade Modulus with Applied Pressureand PlateSi~e

Table 5 shows the range of moduli between applied

unit pressures of 16 psi and 48 psi (the usual range of

pressures for routine testing on 12 in. diameter plate load-

ing tests). It is seen that, for constant bearing area,

the moduli tend to keep constant regardless of the change of

applied pressures. This result implies that the subgrade

material does behave elastically.

Table 6 shows the variation of moduli between

applied unit pressures of 5 psi and 15 psi for 30 in. dia-

meter plate loading tests. The agreement is not as good as

in Table 5. It is believed that because the large size

plate loading test was not easy to handle in the field, the

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subgrade moduli obtained from high pressures are more

reliable than those determined at low pressures. It is for

this reason that subgrade moduli obtained from higher pres­

sure are used in later analyses.

Burmister (1943) and McLeod (1963) have shown

that subgrade moduli obtained from plate loading tests in­

crease with the increase of bearing area. This is also the

case in this study. Table 7 shows the variation of subgrade

modulus with plate diameters of 12 in. and 30 in. It may be

seen that subgrade moduli obtained from 30 in. diameter

plate loading tests are generally higher than those from 12

in. diameter tests. However, the variation of subgrade mo­

duli between these two bearing sizes does not seem to be con­

sistent.

4.2 Plate Loading Tests on Layered Systems

To evaluate a representive modulus for a four­

layered pavement system, a series of plate loading tests

was performed on the surface of each layer at pit 2 in every

site. Both the elastic-layered theory and the finite ele­

ment method were used to determine the moduli of each pave~

ment component on various soil subgrades.

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4.2.1 Equivalent Two-Layered Theory Applied to Multi­Layered Systems

Burmister's theory for a two-layered system was

investigated for use in determining the moduli of pavement

components.

4.2.1a Determination of Upper Layer Modulus in a Two-L?yeredSystem

Taking the subbase and subgrade in Fig. 11 as a

two-layered system, the deflection on the surface of the

subbase obtained from Burmister's theory is (using Eq~.c (7)):

~SB (26)

The subgrade deflection is

a r~SG = 1.18 4· 4

ESG(27)

Since, in Pennsylvania and other state$, pavements

are constructed by designing each successive layer stronger

than the layer underneath it, it is a reasonable approxima-

tion to assume that the surface deflection in a two-layered

system is entirely contributed by the lower layer. In other

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words, ~SB can be set to be equal to ~SG. When the same bear­

ing areas are used (r3 = r 4 ), then

(28 )

By knowing the settlement factor F 3 , and the ratio of pave­

ment thickness to radius of bearing area, TSB/r3 , the ratio

of moduli, ESG/ESB ' can be found from Fig. 2. Since ESG

can be calculated from Eq~ (sa), ESB can then be found.

4.2.lb Determination of Upper Layer Modulus in a Multi­Layered Systems

Consider a three-layered system consisting of

base, subbase, and subgrade in Fig. 11.

Taking the base as the upper layer and the combi-

nation of subbase and subgrade as the lower layer to form a

Burmister's two-layered system, the modulus of the lower

layer, ESS ' which actually is the composite modulus of the

combination of subbase and subgrade, can then be calculated

from Eq.,." (Sa). Again, setting ~BB equal to ~SB for r 2 = r 3

then

(29)

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By knowing the settlement factor F 2 , and the ratio

of pavement thickness to radius of bearing area, TBB/r2 , EBB

can be found with the aid of Fig. 2.

Analogously, following the same procedure, the mo­

dulus of the surface can also be found.

The procedure described above is based on the

assumption that if in the "Equivalent" two-layered system,

the settlement factors (F2

and Fl

in Fig. 11) follow an in­

fluence curve shown in Fig. 2 for a two-layered system, then

F l , F 2 , and F3 can be found.

This procedure requires that the size of the plate

on every layer is the same. In the 1970 test sites, a 12 in.

diameter plate load test was performed on every layer at pit

2 in each site. This provides sufficient information for

the analysis. In order to determine F l , F2 , and F3 , it is

also necessary to know the magnitude of the applied unit

pressures for which deflections of a series of plate loading

tests on each layer at every pit are of the same amount.

This can be done by plotting curves of pressures versus de­

flection for the test data. The required applied unit pres­

sure can be interpolated at a specified deflection.

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'.

Figures 12 and 13 show applied unit pressures

at critical pavement deflections of 0.02 in. on the subgrade

and subbase (found by interpolation for 1970 test sites) .

The results of Burmister's analysis are presented

in Table 8 and will be discussed later.

4.2.2 Finite Element Analysis

It has been stated in Section (4.2.1a) that, in

a layered system, the majority of the surface deflection is

contributed by the subgrade when the pavement components are

comparatively stiffer than the subgrade. Therefore, it is

necessary to adjust the boundary conditions in the finite

element analysis for a layered system. According to Duncan

et al (1968), the deflections and stresses obtained by moving

the fixed boundary to a depth of 50 radii while maintaining

the same radial constraints as for the half-space analysis

are in a fairly good agreement with other layered-system

analyses such as that performed by Chevron Research Company

(1963). The finite element configuration used for analysis

of a layered system is shown in Fig. 14 which contains 198

nodal points and 340 elements.

Poisson's ratio, ~ = 0.4 was used for all layers.

The point loads, converted from the unit pressures applied

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on plates of various sizes, are shown in Fig. 15. The

results of the finite element analysis are presented in

Table 9 and will be discussed in detail later.

4.2.3 strength of Pavement Components

4.2.3a Subbase Courses

It is known that for soil material the modulus is

a function of the material thickness and size of loaded

area. The thickness of the subbase courses selected for

field tests ranged from 6 in. to 12 in .

The moduli of subbase courses shown at Column 2

in Table 8 are determined from Burmister's two-layered sys­

tem theory described in Section (4.2.la) at a critical pave­

ment deflection, 0.02 in. (12 in. plate load data only).

The moduli range from 13,806 psi to 43,046 psi as the thick­

ness of subbase varies from 6.8 in. to 10.8 in. Figure 16

shows the variation of subbase modulus (obtained from equi­

valent two-layered system approach) with its thickness. It

may be seen that within the range of subbase thickness from

6 in. to 9 in., the slope is much greater than for subbases

with thicknesses outside this range (less than 6 in. and

more than 9 in.). When the thickness of subbase is less

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than the radius of the loaded area or exceeds approximately

1.5 the radius of the loaded area, the subbase modulus is

no longer a sensitive function of its thickness. This im­

plies that any increase in the thickness of the subbase

above 1.5 the radius of the loading area will not substan­

tially increase the loading strength.

Within the thickness range of 6 in. to 9 in., the

subbase modulus increases effectively with the increase of

its thickness. This range is, therefore, defined as the

"Effective Thickness." It is obvious that the range of ef­

fective thickness depends on the subbase material in use.

In the 1969 and 1970 test sites, the subbase material is

crushed aggregate having laboratory CBR values ranging from

89 to 144 per cent.

The moduli of subbase courses shown in Table 9

are determined from the finite element analysis described

in Section (2.3) by using the subgrade moduli determined

from a 12 in. plate load test. The moduli range from 10,100

psi to 41,000 psi as the subbase thickness varies from 6.8

in. to 10.8 in. By comparing Table 8 and Table 9 it may be

seen that the subbase moduli obtained from Burmister's

theory are generally higher than those from the finite ele­

ment analysis.

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As shown in Fig. 17, the effective thickness

found from the finite element analysis for a 12 in. plate

on both subgrade and subbase is from 6 in. to 9 in. and is

essentially the same as that determined from Burmister's

theory.

4.2.3b Base Courses

The moduli of five base types obtained from the

equivalent two-layered system approach are shown in Fig.. 18.

Tne data were obtained from nine test sites in 1970. There

is insufficient data to suggest if the relationship between

modulus and thickness is similar to that determined for sub­

base material.

It was not possible to determine the base moduli

for the 12 in. plate load test on all layers (subgrade,

subbase, and base) using finite element analysis. It may

be because of the accumulated errors resulting from the

iterative process of determining modulus of each layer by

starting from the subgrade. Any error in measurement data

in the field and the accumulated errors from approximation

of the finite element analysis may result in large errors

at the third and fourth steps in this iterative process.

This is a weakness of the method.

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The variation of the base moduli with thickness

is shown in Fig. 19. It is seen that the moduli appear to

be independent of layer thickness but again there is insuffi­

cient data to draw definite conclusions in this regard.

4.2.3c Surface Course

The moduli of the asphalt concrete surface obtained

from the equivalent two-layered system approach are shown

in Fig. 20. The range in moduli is from 113,280 psi to

191,160 psi. The surface courses of all test sites were

the same, and it may be seen from Fig. 20 that these moduli

appear independent of thickness. The average of these as­

phalt concrete surface moduli is 143,281 psi which is very

close to the value (150,000 psi) summarized and suggested

by McCullough and VanTil (1968).

It was not possible to obtain the asphalt concrete

surface moduli by the use of finite element analysis. The

possible reason was given in Section (4.2.3b).

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V. EVALUATION OF STRUCTURAL COEFFICIENTS

One of the limitations of the Flexible Pavement

Design Guide~ developed by the AASHO Design Committee is

that no guidance is given concerning selection of structural

coefficients for materials different from those of the AASHO

Road Test. In this chapter, the moduli determined for each

layer (by both layered elastic theory and finite element

analysis) are translated into structural coefficients.

Since the structural coefficients of pavements

should represent their stress~strain characteristics at sub­

failure loads, the structural coefficients, aI' a 2 , and a 3

for surface, base, and subbase can be correlated directly

from the individual moduli which are also representative

of the stress-strain characteristics of an elastic material.

5.1 Structural Coefficients for the Surface, a l

The surface course is a hot-mixed and hot-laid

asphalt concrete identified as Pennsylvania ID-2A. The

thickness ranges from 2.6 in. to 3.7 in. It has Marshall

stability values from 874 lb. to 2047 lb. with an average

value of 1512 lb.

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The structural coefficient of the asphalt surface

material has been related to the Marshall Stability test

(Illinois). The coefficient for the surface course (al )

versus Marshall stability values is shown in Fig. 21 in which

the upper value of 0.44 represents the bituminous concrete

used on the Road Test. From Fig. 21 a value of 0.38 is in-

terpreted from the average Marshall stability value for the

Pennsylvania field tests.

5.2 Structural Coefficients. for Bases, a 2

The structural coefficient, a 2 , for base material

may be obtained from

(30)

The structural coefficients, a 2 , obtained from

moduli determined by the equivalent two-layered system for

a l equal to 0.38, and 0.44 are shown in Table 10. Those

obtained by finite element analysis are shown in Table 11.

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5.3 Structural Coefficients for the Subbase, a3

The structural coefficient, a 3 , for subbase

material is obtained from

( 31)

The structural coefficient, a 3 , obtained from

moduli determined by equivalent two-layered system and finite

element analysis are also shown in Tables 10 and 11.

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VI. SUMMARY AND CONCLUSIONS

1. The use of the AASHO design equation, Burmister's

layered system theory, and an axisymmetric finite ele­

ment analysis for flexible pavement design has been

briefly reviewed.

2. Because highway design involves layered systems, in any

elastic approach used, a value of modulus is required

for each layer. The routine method used to determine

the modulus is the laboratory triaxial test in which

conditions are greatly different from the field. This

study has tried to determine the moduli of pavement ma­

terials in situ by using the data obtained from plate

loading tests on each layer.

3. Correlation between the individual moduli of material

and the structural coefficients used in the AASHO design

equation are studied. The determinationofaEtructural

coefficient, aI' for the asphalt surface is based on

Marshall stability.

4. Within the elastic range, the modulus of subgrade appears

to be independent of the applied unit pressure but de­

pendent on the bearing area. The moduli determined from

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large plate sizes tend to be higher than those from

small plate sizes.

5. No matter what plate size is used, the subgrade modulus

determined from the finite element analysis is only a

little higher than that from Burmister's theory.

6. For unstabilized crushed aggregate subbase materials,

there is an effective thickness in which the modulus in­

creases effectively with an increase of thickness. Out­

side of the range of this effective thickness, the modu­

lus remains constant. The upper bound of this effective

thickness is approximately equal to 1.5 times the radius

of the loading area.

7. Theoretically, if the boundary conditions and the ele­

ment configuration can be generated properly, the finite

element technique is a very powerful method for solving

a layered-system problem in pavement design. However,

this study was restricted to determining the individual

modulus of pavement materials from experimental surface

deflections obtained from field plate loading tests (in­

stead of solving for deflection and stresses from known

individual moduli as is usual in a layered pavement de­

sign). To acc?mplish this purpose it was necessary to

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use -an iterative process to determine the modulus of

each layer by starting with the deflections measured on

the subgrade to determine the subgrade modulus. By

knowing the subgrade modulus, the subbase modulus can

be determined from the deflection measured on the sub­

base. Following this procedure, the surface modulus in

a layered pavement can finally be determined. A large

accumulated-: error ~in.this .,'. iterative ..

procedure may result at the surface due to the approxi­

mation in the finite element analysis and to errors of

deflection measurement obtained from plate loading tests

on each layer. One eYI:OIIe'0@l!S-- measurement on the sub­

grade and/or subbase may reflect all the way up to the

surface modulus. It might be for this reason that the

determination of surface modulus was ~not:~-possible.

In the approach of the equivalent two-layered

system, the determination of each modulus uses only the

composite modulus beneath it. In other words, one cal­

culation is independent of the other. Therefore, no

error is accumulated.

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VII TABLES

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COEFFICIENTS OF PAVEMENT COMPONENTS

Pavement Component a l a 2 a 3

Surface course:Roadmix (low sta-

bility) 0.20Plantmix (high

stability) 0.44Sand asphalt 0.40

Base course:0.071Sandy gravel

Crushed stone 0.14*Cement treated

(no-soil-cement):0.23 1650 psi of more 2

400 psi to 650psi 0.20

400 psi or less 0.15Bituminous treated:

0.341Coarse gradedSand asphalt 0.30

Lime treated 0.15-0.30

Subbase:Sandy gravel 0.11Sand or sandy-clay 0.05-0.10

IThis value has been estimated from AASHO Road Testdata, but not to the accuracy of those factorsmarked with an asterisk.

2compressive strength at 7 days.

Table 1 Structural CoefficientsDetermined in AASHO Road Test

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PLATE SIZES AND PRESSURES

Layer Plate Dia. Pressure(in. ) (psi. )

Surface 12 16,32,48

Base 12* 16,32,4818 16,32,48

Subbase 12* 16,32,4824 10,20,28

Subgrade 12* 16,32,4830 5,10,15

*¢12 in. plate loading test performed on base, subbase, andsubgrade only for 1970 test sites.

Table 2 Plate Sizes and Unit Pressures

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Subgrade Modulus ESG

Test (for 12 in. plate)

Site F. E. A. * B. E. *

(10 3 psi) (10 3 psi)

11-0 5.0 4.7

21-0 9.7 9.2

51-0 20.0 17.9

12-0 10.2 9.7

12R-0 8.2 7.8

42-0 7.0 6.8

52-0 11.3 10.8

33-0 5.3 5.1

43-0 27.0 25.4

*F. E. A. = Finite Element AnalysisB. E. = Burmister EquationApplied Pressure: 48 psi

Table 3 Comparison of Subgrade Modulus for 12 in.Plate Obtained from Finite Element Analysisand Burmister's Equation

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Subgrade Modulus ESGTest (For 30 in. Plate) , 10 3 psiSite

F. E. A. * B. E. *

11-9 16.0 14.7

21-9 11.3 10.5

31-9 11. 7 10.9

41-9 B.6 B.O

51-9 15.0 14.0

32-9 9.0 B.3

23-9 16.0 14.5

33-9 9.0 B.3

43-9 5.4 5.0

53-9 20.4 19.2

11-0 6.9 6.3

21-0 13.5 12.6

51-0 30.0 34.1

12-0 16.B 15.6

12R-0 14.6 13.5

42-0 10.1 10.0

52-0 9.2 B.5

33-0 B~7 B.4

43-0 24.4 22.7

*F. E. A. = Finite Element AnalysisB. E. = Burmister EquationApplied Pressure: 15psi

Table 4 Comparison of Subgrade Modulus for 30in. Plate Obtained from Finite ElementAnalysis and Burmister's Equation

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Subgrade Modulus ESGTest (For 12 in. Plate) , 10 3 psiSite

For 16 psi For 48 psi

11-0 4.6 4.7

21-0 9.5 9.2

51-0 17.1 17.9

12-0 8.9 9.7

12R-0 7.1 7.8

42-0 6.4 6.8

52-0 10.7 10.8

33-0 4.8 5.1

43-0 20.2 25.4

table 5 Variation of Subgrade Modulus withVarious Applied Pressures for 12 in. Plate

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..

Subgrade Modulus ESG -

Test (For 30 in. Plate) I 10 3 psiSite

For 5 psi For 15 psi

11-9 11. 2 14.721.:..9 9.9 10.531-9 8.5 10.941-9 7.4 8.051-9 16.7 14.032-9 11. 8 8.323-9 21. 6 14.533-9 7.8 8.343-9 5.4 5.053-9 17.0 19.211-0 6.7 6.321-0 12.5 12.651-0 52.1 34.112-0 17.4 15.6

12R-0 12.8 13.542-0 11. 2 10.052-0 7.14 8.533-0 15.0 8.443-0 19.7 22.7

Table 6 Variation of Subgrade Modu1us~with VariousApplied Pressures for 30 in. Plate

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TestSite

Subgrade Modulus ESG

(10 3 psi)

11-0

21-0

51-0

12-0

12R-0

42-0

52-0

33-0

43-0

</>12" :£L

4.7

9.2

17.9

9.7

7.8

6.8

10.8

5.1

25.4

</>30" f

6.3

12.6

~4.1

15.6

13.5

10.0

8.5

8.4

22.7

Table 7 Variation of SubgradeModulus with Plate Size

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IU1U1I

(I) subgrade (II) Subbase (III)Base (IV) Surface(¢12 11 p..) (¢121~ p..) , (¢12 11 p..) (¢12 11 p..)

Site No.ESB* TBB EBB* TSF

ESF*ESG*

TSB(in) (psi) (in) (psi) (in) (psi)

11-0** 4,602 6.8 13,806 5.6 672,600 3.4 122,661

21-0 9,204 10.2 36,816 5.9 1,062,000 2.6 191,160

51-0 16,992 8.5 37,382 9.1 61,207 3.0 148,680

12-0 9,558 8.9 38,232 6.2 67,968 2.8 119,475

12R-0 7,257 7.9 29,038 6.1 183,195 2.6 150,893

42-0 6.726 10.8 43,046 3.2 67,968 3.6 181,602

52-0 10,620 7.3 26,550 9.3 87,084 2.7 113,280

33-0 5,841 7.3 29,205 9.3 849,600 2.8 127,440

43-0 21,240 8.9 25,488 5.0 74,7.65. 3.7 134,343

*Critica1 Deflection in each layer 0.02 11

Plate size: 12 in. diameter plate loading test on each layer**xx-O indicated 1970 test sites

Table 8 Individual Modulus of Pavement Components(obtained from equivalent two-layered system approach)

Page 67: by - Lehigh University

IU1mI

Subgrade Subbase Base Surface(<P12" I.L) (<P12 " ~) (<P12" ~) (<P12" ~)

Site No. ESG TSB ESB TBB EBB TSF ESF(psi) (in) (psi) (in) (psi) (in) (psi)

11-0** 5,000 6.8 10,100 5.6 ---* 3.4 ---

21-0 9,700 10.2 38,000 5.9 --- 2.6

51-0 20,000 8.5 26,000 9.1 --- 3.0 ---12-0 10,200 8.9 36,500 6.2 --- 2.8 ---

l2R-0 8,200 7.9 25,000 6.1 --- 2.6 ---

42-0 7,000 10.8 41,000 3.2 --- 3.6 ---52-0 11,300 7.3 23,500 9.3 --- 2.7 ---

33-0 5,300 7.3 25,000 9.3 --- 2.8 ---

43-0 27,000 8.9 19,800 5.0 --- 3.7 ---

*Short solid line in blocks indicates no modulus determinedPlate size: 12 in. diameter plate loading test on each layer

**xx-O indicates 1970 test sites

Table 9 Individual Modulus of Pavement Components(obtained from finite element analysis)

Page 68: by - Lehigh University

IlT1-....JI

Material structural Coefficients

(I) Surface Course a l 0.38 2 0.44 2

(II) Base Course

1. ABBC 0.11-0.66 0.12-0.77

2. ACBC 0.13-1.10 0.15-1.28

3. ALP 0.43-1. 32 0.50-1.53

4. BCBCa 2 0.07-0.25 0.08-0.29

5. CABC 0.17-0.42 0.20-0.48

(III) Subbase Course

(crushed AggregateThickness from 6.8" to 10.8") a 0.01-0.13 0.01-0.15

.3.

1. Since no surface modulus could be obtained from finite elementanalysis the structural coefficient is determined from subgradeup to base by assuming a3 is 1.0 and then fing the ratios ofESB/ESG and EBB/ESG for a2 and a3'

2. Correlated from Marshall "stability.

3. Value determined in AASHO Road Test.

* Moduli are obtained from ¢30", ¢24", ¢18", and ¢12" plate leadtest on subgrade, subbase, base, and surface respectively.

Table 10 Structural Coefficients of Pavement Materials (correlatedfrom Moduli obtained from finite element analysis*)

Page 69: by - Lehigh University

IU100I

Material Structural Coefficients

(I) Surface Course0.38 1 0.44 2(Asphalt concrete I-D2A) a 1

(II) Base Course

1. ABBC 0.18-1.78 0.21-2.06

2. ACBC 2.81 3.26

3. ALP a 2 2.25 2.60

4. BCBC 0.18-0.20 0.21-0.23

5. CABC 0.16-0.23 0.19-0.27

(III) Subbase Course(Crushed aggregatethickness from 6.8 11 to 10.8 11

) a 3 0.04-0.11 0.04-0.13

1. Correlated from Marshall Stability

2. Value determined in AASHO Road Test

* Muduli based on critical pavement deflection 0.02 11 and ¢12 11

plate load test on all layers

Table 11 Structural Coefficients of PavementMaterials (Correlated from Moduli obtainedfrom Equivalent Two-Layered System*)

Page 70: by - Lehigh University

VIII FIGURES

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Page 71: by - Lehigh University

".!!JI"'.~.",' It

510

0::(f) WZ CD

9 0 0:: ~

W~ w 4 :J

:J CD z 2-.J 8 u ~ -.J~ -.J :J 0: «

.::.t:. a.. z 0 0::I- 7 COo.. I- :J0: -« 1000 -.J U I-0 ~o 500 « 3

~r5ua.. 6 -« 0:: :Ja.. «0 :J

-.J 1.0 0::I :J o-.J l- I-

m (f) :> 100 u « 2.0 (f) 30 -.J 5 -W 50 :J 6 5.0I :J-.J 0:: 00 ax I- (!) w

(f)4

w«10

(f) W l-I. W I

0: I(f) -.J 5 z

2 I (!)(f) (!) (f) 0:: W 43 z 3:(f)

z2 (f)

DESIGN CHARTFLEXIBLE PAVEMENTS 5

20 YEARTRAFFIC ANALYSIS

P=2.0

Fig. 1 AASHO Design Chart.

Page 72: by - Lehigh University

6rIr 2r 3r 4r 5 r

TH ICKNESS OF REINFORCING LAYER( MULTIPLES OF RADIUS OF CONTACT)

(AFTER BURMISTER (~))

1\ ....l\ ~ r-.. V<

:\ ~ ,'\ ~i\ ... ....1'-., ~ .... i"o v5 Ratio E2 /E,\\ \

"\.... ...~ I-. ----~~ ~ ... YIO

\\ ,\'

......~ " ~~\r\ ~, ......

...... -----, ~ ---\~ \1\

" " :... .... ... ....... 1/50 --""""-------~r\ \, ....

~ \' ~ ... "',~ '------\~" .... .... ...

~~ \ i'. ........ ----- -," .... .!Ieoo~ -~1\ \ "

,~ ~ ----~ " 1/5, ............... --- ---, ... ,

1 00 """"'-- ----~ , .:t.!.00~ ---. ----" ... ' ....Yeooo ----- -----" ..... -:... .... " ' ...

y. ~-~ ---~ 5000, .......~~::------ -------"""---

0.2

0.8

0.4

0.02o

0.08

0.06

0.04

LL

0::0I-u<tLL

Z0

I I-C!' UI-' WI -I

LLW0

0::W>-<t-II

0;:I-

Fig. 2 values of Deflection Factor, F

Page 73: by - Lehigh University

iII

Ip p

HALF - SECTION

OBLIQUE VIEW

Fig. -3 Finite Element Idealization' of a -Cylinder

-62-

Page 74: by - Lehigh University

z (V)

1

~~ .

. j , m

Axis of Symmetry

R (U)

Fig. 4 Tr~angular Element in an Axisymm~tric Solid

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I •

(I) INPUT DATA

1. Diameter of Plate

2. Point Load Convertedfrom unit Pressure

3. Plate Deflection, ~

4. Boundary Conditions

I(II) ASSUME

Assign Initial Modulus, E

I(III) FINITE ELEMENT ANALYSIS

1. Form Stiffness Matrix for CompleteStructure

2. Solve for Plate Deflection, 0

I(IV) TEST

1. If lo-~I > Error,E=E~~E, go to (III)

2. If Io-~ I < Error,E found

Fig. 5 Simplified Flow Diagram of Finite ElementComputer Program

"'64-

Page 76: by - Lehigh University

Surface

Base

.~ ...

E SF -b.;LEBB

-~BB

I0'1111I

Subbase

Subgrade

E SB

-~SG

PROCEDURE KNOWN COMPUTE

1- Subgrade 6 ESGsg

2. Subbase 6SB ,ESG ESB

3. Base 6BB,ESG,ESB EBB

4. Surface 6SF,ESG,ESB,EBB ESF

Fig. 6 ITERATIVE SOLUTION TO LAYER MODULI

Page 77: by - Lehigh University

I

I

I

I

I

~ LOW MEDIUM HIGH

BASE TYPE

(1) Aggregate 11 12 13Bituminous l2R

(2) Aggregate 21 22 23Cement 22R

(3 ) Aggregate 32Lime 31 33Pozzolan 32R

( 4)Bituminous 41 42 43Concrete 42R

(5 ) Crushed 51 52 53Aggregate 52R

Note: 1. Total No. of Test Sites (includingreplicates) = 19

2. The first digit of site identifica­tion represents base type, the second,subgrade type.

Fig. 7 Theoretical Experimental Design

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Page 78: by - Lehigh University

------- ........ _--

o 10 20

SUBGRADE MODULUS ESG (10 3 psi)Fig. 8 ..Deflection vs. Subgrade Modul-us for Various

Applied Pressures on ¢l2" Plate":;'67-

Page 79: by - Lehigh University

--- -------

Subgrade Soil

Appl ied Pressure: 5, 10 ~ 15 psi;

7

2

P6

!15"wa:/d-c 5(\J Subgrade E SGI

0 Modulus......z Finite Element0 4- Solution.....uw --- Burmister's Solution-.Jl.L.W

3Q

o 10 20

SUBGRADE MODULUS E SG (10 3 psi)Fig ° 9· ,Deflection vs 0, Subgrade Modulus for Various

Applied Pre~sure 6n ¢30" Plate-68-

Page 80: by - Lehigh University

12R

'RH

Fig. 10 Finite Element Configuration used forAnalysis of Homogeneous Subgrade

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Page 81: by - Lehigh University

Surface

Base

I Subbase-....JoI

PI (0-,)r,

P2 (0-2)

E SF-~SF r2

TSFF1 =~aa

P3 (0'"3)

Eeer

Tea

F2 =~se

Eess P4 (0-4)

Tsa Esa r4

E ssF3 ~~SG

Subgradea a

E ess : Composite Modulus of Base t Subbase t and Subgrade

E ss : Composite Modulus of Subbase and Subgrade

0-: Unit Pressure Applied on Plate

p: Total Load Applied on Plate

Fig. 11 Determination-of Individual Modulus byusing Equivalent Two-Layered Theory

Page 82: by - Lehigh University

"

50

e:!=(\J"'9-40z0

~ ~wa::::::>C/) 30C/)wa::Q.

20

12 11 Plate On SubgradeCritical PavementDeflection 0.02 11

Pressure vs~ Deflection for ¢12" Plate-71-

5423DEFLECTION 10-2in.

Fig ..12

o

10

70

60

~. .

Page 83: by - Lehigh University

70

60

50

C\J

-&

Z 40oW0::::J

~ 30w0:::a..

20

10211I Plate On Subbase

Critical PavementDeflection 0.02

11

11

o 2 3 4 5DEFLECTION 10-2 in.

Fig. 13 Pressure vs. Deflection for ¢12" Plate

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12R

0::o10

~ vLayer I -.--Layer2- r----

Layer 3 I

r---- V-~

~v1/

~

~

~V

//

Layer 4 v/

/

~V1/

v

vvvvV

~~v~l/~~~l/

/ '///////~ // '//// / / //

Note:

The diagonal

line completing

each triangle is

omitted for clarity.

Fig. 14 Finite Element Configuration used for Analysisof Layered System - Deep Bottom Boundary

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Page 85: by - Lehigh University

I-...J,;,.I

Point LoadDiam. of unit

Plate Size Pressure Pl P2 P 3 P 4 P 5 P6(in. ) (in. ) (lb) . (lb. ) (lb. ) (lb. ) (lb. ) (lb. )

12 48 452.39 2714.33 2261.94 0 0 0

18 48 452.39 2714.33 5428.67 3619.11 0 0

24 28 263.89 1583.36 3166.72 4750.08 2902.83 0

30 15 141.37 848.23 1696.46 2544.69 3392.92 1979.20

I

r =9 II

r= 12 11

r=15 11

Fig. 15 Point Loads Converted from Unit Pressure Appliedon Plates of Various Sizes (Finite Element Analysis)

Page 86: by - Lehigh University

"

1-Effective Thickness

·150P- 6" S

(J) 6"a. •rt>0 40.......

Subbase ESBm •(f)

w Subgrade ESG(f)

::Jr -.J 30 •-....J ::J •U1I 0 •·0 •~

w(f) 20<X:CDCD::J(f)

10

6 8

THICKNESS OF SUBBASE (in.)

10

Fig. 16 Variation of Subbase Modulus With Thickness(Equivalent Two-Layered System Approach)

Page 87: by - Lehigh University

I~"Effective Thickness

•- 40(/)

a. •ro0.......

CD, Subbase ESB T(J)

30w·(f) Subgrade ESG:::>

I -J •--.l :::>

ESG Obtained from0'\ aI0~ ,20 12

11Plate Load Test •

w(f)

c::rCDCD:::>(f) 10

II...,.. ~ --,--I I..- ~I L-6 8 10

THICKNESS OF SUBBASE (in.)

Fig. 17 variation of Subbase Modulus with Thickness(Finite Element Analysis)

Page 88: by - Lehigh University

6 II I

oABBC IXAAA

• ACBCBase EBB

1 TBB... ALP )

o BCBCSubbase

t1 CABC

Subgrade. Ess (CompositeModulus ofSubbase andSubgrade)

100 •80

060-

!J')

a.v 400.......mm

W

(J) 200:::>

-I:::>00~

10w t1(J) 8« 0CD 0 0

6 t1

4

4 6 8 10

. THICKNESS OF BASE (in.)

Fig. 18 VARIATION OF BASE MODULI WITH THICKNESS(EQUIVALENT TWO-LAYERED SYSTEM APPROACH)

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gil

o ABBC I• ACBC I(',( ¥ Y X YXX~ - .....

.. ALP Base EBB4 TBB

o BCBCA CABC Subbase ESB (ep 24" fe..)

Subgrade ESG ( ep 30" fe..)

100•

80

60 A-(J) • ..a.

v 400- 0 •mm

W 0

(J) 20 A A:::J 0-.J:::JQ0 0 0~ 10w A

8 A(J) A<toeD

6 •o·

0

0

4 6 8 10

THICKNESS OF BASE (in.)Fig. 19 variation of Base Moduii with Thickness

(Finite Element Analysis)-78-

\

Page 90: by - Lehigh University

2.0

0

-(/)

c..&0

0-...

(!)Cf)

wCf):J

I ...J 1.5 --.J :J\DI 0

0~

w0<!l.L..a:::::JCf)

0

Average of Surface Modulus

E SF = 143,281psi

o

oo

o

o

o

2.6 3.0 3.5

THICKNESS OF SURFACE (in.)Fig. 20 VARIATION OF SURFACE MODULI WITH THICKNESS

(EQUIVALENT TWO-LAYERED SYSTEM APPROACH)

Page 91: by - Lehigh University

0.4

0 .. . 0.3I-zw-U-lJ..

I lJ..co w 0.20 0I

'U //

/

0.1

o 400 800 1200 1600 2000

MARSHALL STABILITY, Ibs.

2400

Fig. 21 Correlation of Coefficient of Surface withMarshall Stability (By Illinois)

Page 92: by - Lehigh University

I •

E

F

G

p

R

SN

SS

IX. NOMENCLATURE

Design layer thickness in AASHO designequation for surface, base and subbasecourses respectively

Modulus of elasticity

Modulus of elasticity of the bottom layerin a two-layered system

Modulus of elasticity of subgrade, subbase,base and surface courses respectively

Composite modulus of elasticity of subbaseand subgrade

Composite modulus of elasticity of base,subbase and subgrade

Dimensionless settlement factor in a two­layered system

Dimensionless settlement factors in a equi­valent two-layered system

Nodal point forces in radial and vertical 0 . .

direction

Logarithmic value of initial and desiredterminal serviceability

Body force

Regional factor in AASHO design equation;Radial axis in a cylindric coordinate system

Structural number in AASHO design equation

Value of soil support

Layer thickness.of subbase, base and surface

Radial displacements of nodal points in anelement

Vertical displacements of nodal points in anelement

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'.

"

z

r

]J

0.,0,,0,1 J m

Total equivalent 18-kip single axle loads

vertical axis in cylindrica'l'~coordinatesystem

structural coefficients in AASHO designequation for surface, base and subbase coursesrespectively

Radius of circular bearing plate

Various radii of circular bearing plates

Strain

Surface deflection

Surface deflections on the top of surface,base, subbase and subgrade respectively

Applied unit pressure; stress

Poisson's ratio

Nodal point displacements

':"'82-

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..

x. BIBLIOGRAPHY

1. ACUffi, W.E.A., and Fox, L. (1951), "computation of LoadStresses in a Three-Layer Elastic System~ Geotechnique,Vol. 2, pp. 293-300.

2. Benkelman, A.C., and Williams, S. (1959), "A CooperativeStudy of Structural Design of Nonrigid Pavements," High­~ay Research Board, Special Report 46.

3.· Boussinesq, V.J. (1885), "Application des Potentiels al'etude de l'equilibre, et du mouvement des solideselastiques avec des notes etendues sur divers points dephysique nathematique et d'analyse," Gauthier-Villars,Paris.

3. Burmister, D.M. (1943), "The Theory of Stresses and Dis­placements in Layered System and Applications to Designof Airport Runways," Proceedings, Highway Research Board,Vol. 23, pp. 126-149.

5. BurIriister, D.M. (1945), "The General Theory of Stressesand Displacements in Layered Soil Systems,"· Journal ofApplied Physics, Vol. 16, No.2, pp. 89-96; No. 3, p~126-127; ·No. 5, pp. 296-302.

6. Burmister, D.M. (1956), "Stress and Displacement Char­acteristic of a Two-Layered Rigid Base Soil System:Influence Diagrams and Practical Applications," Proceed­ings, Highway Research Board, Vol. 35, pp. 773-814.

7. Chevron Research Co. (1963), "N-Layer Elastic Programfor Determination of Stresses and Strains in LayersSystems," Personal communication.

8. Clough, R.W., and Rashid, Y. (1965), "Finite ElementAnalysis of Axisymmetric Solids," J"ournal of Engineer­ing Mechanics Div., ASCE Proceedings, Vol.9l, February,pp. 71-85.

9. Duncan, J.M., Monismith, C.L., and Wilson, E.L. (1968),"Finite Element Analysis of Pavements," Highway ResearchRecord No. 228, pp.18-33.

10. Fox, L. (1948), "Computation of Traffic Stresses in Sim­ple Road Structures," Proc., 2nd International Conf. onSoil Mechanics and Foundation Engineering, Rotterdam,Vol. II, pp. 236-256 .

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11. Hank, R.J. and Scrivner, F.H. (1948), "Some NumericalSolutions of Stresses in Two and Three-Layered Systems~

Proceedings, Highway Research Board, Vol. 28, pp. 457­468.

12. Housel, W.S. (1929), "A Practical Method for the Selec­tion of Foundations Based on Fundamental Research inSoil Mechanics," Engineering Re~earch Bulletin No. 13,Dept. of Engineering Research, Univ. of Michigan.

13. Jones, A. (1962), "Tables of Stresses in Three-LayerElastic Systems," Highway Research Board Bulletin No.342, pp. 186-214.

14. Langsner, G., Huff, T.S. and Liddle, W.J. (1962), "Useof-:B.oad·r:rest Finding by AASHO Design Committee," High­way Research Board, Special Report No. 73, pp. 399-405.

15. McCullough, B.F. and Van Til, C.J. (1968), "Evaluationof AASHO Interim Guides for Design of Pavement Struc~

tures," National Council of Highway Research ProgressProject 1-11.

16. McLeod, N.W. (1963), "Some Notes on Pavement StructureDesign," HighwS~ Re§earph~Board~Rebord;N~~131 pp. 66r::J.~1. c:=·-: {

17. McLeod, N.W. (1965), "Some Notes on Pavement StructureDesign - Part 2," Highway Research Board Record No. 71,pp. 85-104.

18. Seed, H.B., Mitry, F.G., Monismith, C.L. and Chan, C.K.(1967), " Prediction of Flexible Pavement Deflectionsfrom Laboratory Repeated-Load Tests," National Councilof Highway Research Progress Report 35.

19. Siddiqi, O.S. and Hudson, W.R.Evaluation of Subgrade ModulusModel Slab Studies," ResearchTexas at Austin.

(1970), "Experimentaland its Application inReport 56-16, Univ. of

20. Sisko, A.W. and Brunstrum, L.C. (1969), "Relation ofAsphalt Rheological Properties to Pavement Durability~

National Council of Highway Research Progress Report 67.

21. Timoshenko, s. (1934), "Theory of Elasticity," McGraw­Hill, New York.

22. Vaswani, N.K. (1970), "Optimum Structural Strength ofMaterials in Flexible Pavements," Highway ResearchBoard Record No. 329, pp. 77-97 •

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23. Warren, H. and Dieckmann, W.L. (1963), "Numerical Com­putations of Stresses and Strains in a Multi-Layer As­phalt Pavement System~ Chevron Research Company.

Page 97: by - Lehigh University

·•

r•

'..

..

1.

2.

3.

XL. APPENDIX

Lists of Field Test in Each Site

Length of test section - 1000'

There are 3 pits of random selection in each testsection (all pits located at outer wheelpath)

Pits 1 and 3 (end pits) = 3' x 5'

Pit 2 (center pit) = 5' x 7'

The following tests were performed at all pits:

A. Surface (ID-2)

a. GMR..:.6.::. through the whole section

b. Dynaflect

c. Benkelman Beam

d. CHLOE

e. Rut depth, cracking, and patching (every 100'interval)

f. Surface coring (two ¢4 in. or ¢6 in. asphaltconcrete cores per pit)

g. Pit surface sawing (cut open each pit and ob­tained asphalt block samples)

B. Base (five types)

a. Samples for moisture content taken for crushedaggregate base course (CABC)

b. Four bags of bulk samples taken from CABC forlab tests (2 for PDH and 2 for Lehigh)

c. Nuclear gauge measured density and moisturecontent on non-asphalt stabilized material

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....

C. Subbase (one type)

a. Samples for moisture content

b. Four bags of bulk samples for lab. tests

c. Nuclear gauge for density and moisture content

D. Subgrade (three types)

a. Nuclear gauge for density and moisture content

b. Field density by Balloon method

c. 9 CBR per pit

d. Samples for moisture content measurement

e. Undisturbed samples (¢6 in. and ¢4 in. cores)

f. Four bags of bulk sample taken for lab. tests

g. Layer thickness measurement

4. Tests performed at pit 2 (center pit) only

A. Surface = ¢12 in. plate loading test

B. Base = ¢12 in. and ¢18 in. plate loading test*

C. Subbase = ¢12 in. and ¢24 in. plate loading test*

D. Subgrade = ¢12 in. and ¢30 in. plate loading test*

*No ¢12 in. plate loading test on base, subbase, and subgradein 1969 field test program

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,

XII. VITA

Humphrey Chishao Han was born on April 24, 1942 in

Polo, Canton, China, the first son of Chi-Wang and Te­

Tseng Han. He attended elementary school in his home town

and high school in Taipei, Taiwan, Republic of China and

graduated in 1961.

He received a B.S. degree in Civil Engineering in 1966

from the Cheng-Kung University in Tainan, Taiwan, Republic

of China.

After serving as a teaching and research assistant in

his alma mater for two years, he came to the United States

and enrolled in a Master's program in Civil Engineering at

Lehigh University in 1969, during which time he was employed

as a research assistant.

~88-