Analysis of High Pressure Effects on Wellbore Integrity Using the Distinct Element
Method
by
Stacey J. Amamoo, BSc.
A Thesis
In
PETROLEUM ENGINEERING
Submitted to the Graduate Faculty
of Texas Tech University in
Partial Fulfillment of
the Requirements for
the Degree of
MASTER OF SCIENCES
In
PETROLEUM ENGINEERING
Approved
Dr. Malgorzata Ziaja
Chair of Committee
Dr. Shameem Siddiqui
Dr M. Rafiqul Awal
Peggy Gordon Miller
Dean of the Graduate School
May, 2012
COPYRIGHT 2012, S.J. AMAMOO
Texas Tech University, Stacey J. Amamoo, May 2012
ii
DEDICATION
To my parents Kobina (Dedi) and Alice (Meme) Amamoo and my sisters Mammie and
Effie
Texas Tech University, Stacey J. Amamoo, May 2012
iii
ACKNOWLEDGEMENTS
I would like to thank the Almighty God for being my source of strength and granting me
the gift of perseverance especially during the times I genuinely believed completion of
this thesis was next to impossible.
I would also like to express my heartfelt gratitude to Dr Malgorzata Ziaja, for being my
mentor, professor and mother. I would also like to thank Dr Shameem Siddiqui and Dr.
Rafiqul Awal for accepting to be on the committee as well as providing the much needed
guidance to complete this work.
Sincere appreciation also goes the Texas Tech University Bob E. Herd Petroleum
Engineering Department for giving me the opportunity to obtain a masters degree and to
all the staff and professors for their help and knowledge.
In addition, I would like to express warm gratitude to my colleagues and friends
especially Joshua Momodu and Sarah Alajmi and to Wenjing Li for helping me figure out
the complex parts of the ITASCA Particle Flow Code.
Finally, I would like to thank my dearest aunt Nadia Aloghani for making my stay in the
United States pleasant and always looking out for my wellbeing.
Texas Tech University, Stacey J. Amamoo, May 2012
iv
CONTENTS
DEDICATION .................................................................................................................... ii
ACKNOWLEDGEMENTS ............................................................................................... iii
CONTENTS ....................................................................................................................... iv
ABSTRACT ....................................................................................................................... vi
LIST OF TABLES ............................................................................................................ vii
LIST OF FIGURES ......................................................................................................... viii
NOMENCLATURE ........................................................................................................... x
1 INTRODUCTION ........................................................................................................... 1
1.1 Background ............................................................................................................ 1
1.2 Wellbore Failure .................................................................................................... 4
1.3 Mohr-Coulomb Failure Criterion .......................................................................... 5
2 LITERATURE REVIEW ................................................................................................ 7
2.1 Evaluation of Existing Numerical, Analytical and Experimental Cement-Casing
-Formation Systems ..................................................................................................... 7
2.2 Cement Bonding .................................................................................................... 8
2.3 Factors Affecting Casing-Cement Bond And Casing-Rock Bond ...................... 10
2.4 Experimental Tests Carried Out On Cement ....................................................... 11
2.5 Scope And Objectives ......................................................................................... 15
3 NUMERICAL MODELING OF CEMENT-CASING-FORMATION SYSTEM ........ 18
3.1 Finite Element Method ........................................................................................ 18
3.2 Finite difference Method ..................................................................................... 20
3.3 Boundary Element Method .................................................................................. 22
3.4 Distinct Element Method ..................................................................................... 23
3.5 Using PFC............................................................................................................ 27
4 METHODOLOGY ........................................................................................................ 36
4.1 Determination of Microproperties ....................................................................... 37
4.2 Algorithm for compression testing with PFC ...................................................... 38
4.3 Validation ............................................................................................................ 40
Texas Tech University, Stacey J. Amamoo, May 2012
v
4.4 Analysis of high pressure on Well integrity – A Horizontal well Example ........ 46
5 RESULTS AND ANALYSIS ........................................................................................ 51
6 CONCLUSIONS............................................................................................................ 66
REFERENCES ................................................................................................................. 68
A DATA SET FOR FAILURE TEST 100MPA............................................................... 72
B DATA SET FOR FAILURE TEST 10 MPA ................................................................ 86
C DATA SET FOR FAILURE TEST 1MPA ................................................................. 100
Texas Tech University, Stacey J. Amamoo, May 2012
vi
ABSTRACT
It is a proven fact that the analyses of the casing, cement and rock formation during the
life of a well is of utmost importance in the maintenance of wellbore integrity. This has
been done so far utilizing the continuity numerical methods such as the finite element
method together with experimental methods.
In using the finite element method to analyze wellbore integrity taking into consideration
the formation, cement and casing, the discontinuity of their interaction is lost and as such
fractures and other mechanisms such as debonding cannot be modeled.
The main objective of this research is to utilize the distinct element method in analyzing
wellbore instability so as to avoid or greatly minimize failure in wellbores. In this paper,
the cement-formation bond and cement-casing bond are thoroughly discussed as well as
their effect and contribution to well integrity. The ITASCA Particle flow code software is
used. It is validated and then used to analyze horizontal well using parameters from the
Barnett Shale.
Texas Tech University, Stacey J. Amamoo, May 2012
vii
LIST OF TABLES
1 Conditions For Mohr’s Failure ........................................................................................ 6
2 Data used in Validation .................................................................................................. 41
3 Data used in Horizontal well example ........................................................................... 46
Texas Tech University, Stacey J. Amamoo, May 2012
viii
LIST OF FIGURES
1 Graph Showing the Variation of Effective Stresses as a Function of Azimuth
(Zoback 2008) ..................................................................................................................... 4
2 An Illustration of Controllable and Uncontrollable Factors and Their Effects on the
Formation and Wellbore (PASIC 2007) ............................................................................. 5
3 Diagram Showing Mohr-Coulomb Failure Criterion (Soliman and Boonen 1999) ....... 6
4 Diagram Showing Casing Cement and the Formation ................................................... 9
5 Typical Triaxial Testing Cell ........................................................................................ 12
6 The Uniaxial or Brazilian Test ...................................................................................... 13
7 Setup for the Unconfined Compressive Test ................................................................ 14
8 Direct Shear Test.......................................................................................................... 14
9 Shear Displacement Curve ............................................................................................ 14
10 Cracks in Cement Sheath as Demonstrated by Ravi et al. (2002) .............................. 16
11 Plastic Deformation in Cement Sheath as Demonstrated By Ravi et al. (2002) ......... 16
12 Debonding in Cement- Formation Interface as Demonstrated by Ravi et al. (2002) . 17
13 Debonding In Cement-Casing Interface as Demonstrated by Ravi et al. (2002)........ 17
14 Numerical Methods Used in Geomechanics ............................................................... 18
15 Illustration of the Finite Element Method ................................................................... 19
16 Representation of Lagrangian FDM Where Domain is Divided into Nodes and
Zones ................................................................................................................................. 21
17 Particles during Motion (Courtesy Jing and Stephansson 2007) ................................ 25
19 Calculation Cycle of PFC ........................................................................................... 29
20 PFC Plot of Balls in Contact (Smooth Joint) .............................................................. 34
21 Determination of Microproperties of Materials .......................................................... 37
22 Part I of the Testing Procedure ................................................................................... 38
23 Part II of the Testing Procedure .................................................................................. 39
24 Part III of the Testing Procedure ................................................................................. 40
25 Sample Setup for Biaxial Test .................................................................................... 42
26 Sample after Failure Showing Deformation and Breaks in Parallel Bond ................. 43
Texas Tech University, Stacey J. Amamoo, May 2012
ix
27 Deviatorial Stress Versus Axial Strain Graph Showing The Initial Yield of the
Sample (PFC) .................................................................................................................... 44
28 Deviatorial Stress versus Axial Strain Graph Showing the Initial Yield of the
Sample as Indicated By Stiles (2006) ............................................................................... 45
29 Elastic Load/Unload Test to Determine Properties of Formation Setup .................... 47
30 Elastic Load/Unload Test to Determine Properties of CEMENT Setup..................... 48
31 Elastic Load/Unload Test to Determine Properties of CASING Setup ...................... 49
32 Cement Casing Formation Setup ................................................................................ 50
33 Diagram Showing Slight Deformation of the Casing ................................................. 52
34 Diagram Showing Plastic Deformation Of Cement.................................................... 53
35 Diagram Showing Debonding Deformation Of Cement ............................................ 54
36 Diagram Showing Microcrack Formation At 10mpa ................................................. 55
37 Graph Showing Microcrack Development At 10mpa ................................................ 56
38 Diagram Showing Microcrack Formation At 100mpa ............................................... 57
39 Graph Showing Microcrack Development At 100mpa .............................................. 58
40 PFC Derived Shear Stress versus Effective Normal Strain (10mpa Overburden)...... 59
41 PFC Derived Deviatoric Stress versus Axial Strain @ 10mpa Overburden ............... 60
42 PFC Derived Normal, Tangential and Hoop Stresses at 10mpa Overburden ............. 61
43 Spreadsheet Analysis of Deviatoric Stress versus Axial Strain @ 10mpa
Overburden ....................................................................................................................... 62
44 Spreadsheet Analysis of Deviatoric Stress versus Axial Strain @ 10mpa
Overburden ....................................................................................................................... 63
45 Spreadsheet Analysis Normal, Tangential and Hoop Stresses @ 10mpa
Overburden (Loading) ...................................................................................................... 64
46 Spreadsheet Analysis Normal, Tangential and Hoop Stresses @ 10mpa
Overburden (Unloading) ................................................................................................... 65
Texas Tech University, Stacey J. Amamoo, May 2012
x
NOMENCLATURE
A= Cross sectional area
D= outer diameter of casing
E= Young’s modulus
E100%= amplitude for100%bond
Ec,= Young’s modulus of confining formation
Ecement = Young’s modulus of cement
Efree =Free pipe amplitude
Emeas =Measured amplitude
Er= Young’s modulus of reservoir
Esteel= Young’s modulus of steel
F = Force
G= weight of casing
H= height of cement column
I = normal or shear
K = Stiffness
L = length of casing
µ = coefficient of friction
Pp= pore pressure
Q= Heat flux
R = major radius
r = minor radius
Texas Tech University, Stacey J. Amamoo, May 2012
xi
SHMAX = Maximum horizontal stress
Shmin = minimum horizontal stress
Sv = vertical principal stress or overburden stress
vc= Poisson’s ratio of confining formation
vcement= Poisson’s ratio of cement
vsteel = Poisson’s ratio of steel
Vmat = Volume of material within the region of interest
vr= Poisson’s ratio of reservoir
Vroi = Volume of region of interest
Vvoid = Volume of empty space
xp = position of a point p
x� ��= translational velocity
x� ��= velocity at a point p
x��= center of rotation
x��∅ = locationofabody�scentroid
x��� = locationofabody�scontact τ =Bond Strength
τn = shear stress which is acting on the bond interface
σn = adhesive strength
ϕ = internal friction angle
µ = coefficient of friction
Texas Tech University, Stacey J. Amamoo, May 2012
xii
υ = Poisson’s ratio
δ = increment
��� = averagestressinparticlep
σ����" = averagestressinclumps ω =rotational velocity
%&& = radial stress
%''= hoop or tangential stress
%((= vertical stress
Texas Tech University, Stacey J. Amamoo, May 2012
1
CHAPTER 1
INTRODUCTION
1.1 BACKGROUND
During the completion stage of the life of a wellbore, the wellbore is cased and cemented
in order to maintain its integrity. Wellbore integrity has been an issue in the drilling
industry since time immemorial and has cost the industry financially, socially and
environmentally. The objective of this work is to develop a better understanding of the
performance of the casing-cement-formation under high pressure using. Well integrity is
defined by the Norwegian Petroleum Industry (NORSOK) D-010 as “Application of
technical, operational and organizational solutions to reduce risk of uncontrolled release
of formation fluids throughout the life cycle of a well”. The study and analysis of
wellbore integrity is important because loss of well integrity results in loss of well control
and this may further lead to the damage of equipment, loss of reserves, reputational
damage, and cost of remediation and most importantly loss of human life. One of the
major contributory factors to the integrity of a well is the cement bond. The bond of
cement in a well consists of the bond between the cement and the formation and the bond
between the cement and the casing. Various tests, both experimental and numerical have
been performed to analyze the wellbore integrity. These tests have been successful to an
extent in that they have given some basis for cement as well as casing design. However,
cement formation bond mechanism understanding has been relegated to qualitative
observations involving formation permeability, the role of mud cake and mud
displacement practices (Wojtanowicz, 2008).
Wellbore integrity is first controlled by the wellbore stability during drilling. Here,
stability is often by the mud weight and consistent management of pressure. After
cementing, upward fluid migration through cement channels has also been cause for most
blowouts. When fluid seeps around the casing it may erode the borehole-casing annulus,
which may eventually lead to the formation of a crater. The cement sheath is constantly
Texas Tech University, Stacey J. Amamoo, May 2012
2
checked after cementing and cement bond logs are used to evaluate the integrity of the
bonds. Despite all these checks, unforeseen events such as seepage of contaminated fluids
into the formation and blowouts may cause the wellbore to lose its integrity. The
accurate, proper design and planning of cement jobs are primary requirements for
preventing the upward migration of gas around the casing. As a result, a great deal of
effort has been exerted by the petroleum industry to reduce the channel formation
tendency in the cemented annulus during cementing.
The main causes of wellbore instability may be grouped under chemical and mechanical
factors. Mechanical causes of instability include failure around the borehole as a result of
high stresses, insufficient rock strength and inadequate drilling practices. Chemical
causes of instability are as a result of interaction between the formation and/or formation
fluid and fluid pumped into the wellbore. However, the well bore instability is usually
due to a combination of these factors. When there is a concentration of stresses around a
wellbore, it may result in compressive or tensile failures. Zoback (2007) referred to these
failures as stress induced breakouts (compressive) and drilling induced (tensile) wall
fractures. Effective stresses around a wellbore may be described as follows:
%&& = 12 �+,-./ + +1-23 − 2561 − 7898: + 12 �+,-./ − +1-23× 61 − 47898 + 37>9> : cos 2? +5@7898
(1)
%AA = 12 �+,-./ + +1-23 − 2561 + 7898: − 12 �+,-./ − +1-23× 61 + 37>9> : cos 2? +5@7898 − %∆C
(2)
D&A = 12 �+,-./ − +1-23 × 61 + 4298 − 37>9> : sin2? (3)
Texas Tech University, Stacey J. Amamoo, May 2012
3
%EE = +F − 2G�+,-./ + +1-23 67898: cos 2? (4)
Where υ is Poisson’s ratio and θ is the angle measured from the azimuth of SHmax.
When the formation is in its original state it is often characterized by three states of
stress:
- Overburden or vertical stress in the z axis
- Horizontal stress in the x axis
- Horizontal stress in the y axis
The overburden stress is as a result of the overlying formation and the horizontal stresses
are mostly due to tectonic stresses. However, when a wellbore is drilled, the original state
of stress is greatly disturbed as a solid element (cylindrical in shape) is removed from the
mother formation. This eliminates the state of equilibrium which we normally attempt to
restore by replacing the void with a drilling fluid. When drilling on balance, the
hydrostatic pressure exerted by the drilling fluid is not enough to maintain the
equilibrium of the formation itself and the formation reacts by counteracting the stresses
exerted by the drilling fluid causing the formation to deform. It is only when this occurs
that equilibrium is restored (Gray et al., 2007). When the wellbore is cased and cemented,
the hydrostatic pressure exerted by the cement slurry usually not equal to that of the mud
and as a result the deformation cycle repeats itself to achieve stability. The same is true
about the hardening and shrinking process of the set cement (Gray et al, 2007).
The integrity of the wellbore may be compromised if the bond between the casing and the
cement as well as the casing and the formation are inadequately designed. Often the three
components of the system are designed separately using individual stress components. In
such a case the following may occur (Teodoriu et al, 2010):
- Cracks in the cement which will allow for gas and fluid migration
- Plastic deformation in cement or
Texas Tech University, Stacey J. Amamoo, May 2012
4
- Debonding of the component’s interfaces
The first two will cause radial fluid migration and latter vertical fluid migration. The
above anomalies may be due to tensile failure caused by shrinkage as a result of the
dehydration of the cement. It may also be due to compressive shear failure as a result of
high abnormalities in principal stresses. The above may also jeopardize wellbore
stability. The formation surrounding the wellbore is subject to the effective hoop stress,
radial stress and the effective stress parallel to the axis of the wellbore. If the strength of
the formation is less than these stresses, the formation is set to fail. This is analogous to
the maximum stress criterion. However, as differential pressure, ∆P increases there is a
decrease in the effective hoop stress and this can result in what Zoback (2007) referred to
as drilling induced tensile failures.
Figure 1: Graph Showing the Variation of Effective Stresses as a Function of Azimuth (Zoback 2008)
1.2 WELLBORE FAILURE
Wellbore failure may be as a result of controllable or uncontrollable factors. However,
both of these factors contribute to numerous disturbances in a wellbore region and
affecting productivity and the formation as a whole. Figure 2 is an illustration of
Texas Tech University, Stacey J. Amamoo, May 2012
5
controllable and uncontrollable factors and their effects on the formation and wellbore
behavior. There are several criteria for defining failure. In geomechanics the most widely
utilized and most applicable is the Mohr-Coulomb failure criterion.
Figure 2: An Illustration Of Controllable And Uncontrollable Factors And Their Effects On The
Formation And Wellbore (PASIC 2007)
1.3 MOHR-COULOMB FAILURE CRITERION
There are several different criteria of rock failure. However, the Mohr-Coulomb Failure
Criterion is the commonest and most applicable in the field of geomechanics. According
to the maximum normal stress criterion, when the maximum normal principal stress
reaches the uniaxial compressional strength or uniaxial tensile strength failure occurs.
Texas Tech University, Stacey J. Amamoo, May 2012
6
The Mohr-coulomb criterion is based on the Mohr’s circle and coulomb’s maximum
normal stress criterion. According to the Mohr-Coulomb criterion, when the Mohr’s
circle at a point in a body is no longer enveloped by the Mohr’s circle for uniaxial tensile
strength and uniaxial compressional strength, failure will occur.
Figure 3: Diagram Showing Mohr-Coulomb Failure Criterion (SOLIMAN AND BOONEN 1999)
TABLE 1: CONDITIONS FOR MOHR’S FAILURE
Case Stress Maximum allowable value to avoid failure
1 Both in compression σ 1> 0 , σ 2> 0
2 Both in tension σ 1< 0 , σ 2< 0
3 σ 1 in compression, σ 2 in tension σ1σt +σ2σc < 1
4 σ 2 in compression, σ 1 in tension σ1−σc +σ2σt < 1
Texas Tech University, Stacey J. Amamoo, May 2012
7
CHAPTER 2
LITERATURE REVIEW
2.1 EVALUATION OF EXISTING NUMERICAL, ANALYTICAL AND EXPERIMENTAL
CEMENT-CASING-FORMATION SYSTEMS
The integrity of the wellbore has been investigated over the years through various
experimental as well as numerical means. The experimental methods usually consist of
triaxial tests and other stress and strain tests. These experimental methods have been used
in the past by Carter and Evans (1964), Scott and Brace (1966), Evans and Harriman
(1972) Goodwin and Crook (1992), Stiles (2006) and many more. In these experiments
most of the attention was given to the cement sheath, its mechanical and elastic properties
and its role in maintaining wellbore integrity. Goodwin and Crook (1992) investigated
the effect of temperature and pressure on the mechanical and elastic properties of various
cements and concluded that cements with high elastic moduli were more likely to be
damaged. Early numerical analyses of wellbore integrity considering the cement-
formation and cement-casing bonds have been used by Goodwin and Zinkham (1962).
Other researchers like Gray et al (2007), Fleckenstein et al (2000), Ravi et al (2002),
Medhi et al (2006), Teodoriu et al (2010) and many others have also numerically
analyzed the integrity of the wellbore. However all of these analyses have been done
using the finite element method or other continuity methods. In 1962, Goodwin and
Zinkham used mathematical methods to analyze tensile and compressive stresses in an
unconfined cement sheath as well as compressive stresses in a confined cement sheath.
According to their computations, they were able to estimate the fracture initiation
pressure, effect of pipe size on cement stress and initial relationship between cement,
rock and casing. Medhi (2006) also used the finite element method in analyzing the
cement-formation and cement-casing bonds, how high temperature and high pressure
affect these as well as forecast the time of failure. He concluded that alternating high
temperature and high pressure effects can cause unexpected behavior in the cement
sheath, which will eventually lead to failure in the casing-cement bond.
Texas Tech University, Stacey J. Amamoo, May 2012
8
According to Goodwin and Zinkham, laboratory tests to analyze wellbore integrity may
not be too applicable and as such a small field evaluation incorporated into mathematical
analysis may be the best option for the analysis of well integrity. The finite element
method, which is also vastly used in the modeling of well integrity, ignores the
discontinuity behavior of fractures and interfacial interaction between the cement and the
formation as well as the cement and the casing. The discrete element method is hardly
ever used due to its computational complexities (Jing and Stephansson 2002).
2.2 CEMENT BONDING
The major functions of cement are to prevent fluid migration or interaction with the
formations and to support the casing (Lake 2007). The integrity of a well is dependent
upon the casing-cement contact and its capability to seal the annulus throughout the life
of the well. It is therefore imperative to understand the performance of the casing cement
bond under well conditions that can lead to best practices and a model to predict well life.
Two types of bonds are necessary when considering the bond between cement and
casing. These are shear bond and hydraulic bond. Shear bond is necessary for the
mechanical support of casing in a hole, whereas, hydraulic bond is needed to prevent the
seepage of fluids in and out of the formation (Carter and Evans, 1964).
Shear bond: According to Coulomb’s theory, shear failure can occur if the following
condition is satisfied:
τK = c + μσK
(5)
or τK = c + tanφ ∗σK
(6)
Where
τK = the shear stress which is acting on the bond interface
c = the adhesive strength
Texas Tech University, Stacey J. Amamoo, May 2012
9
φ = the internal friction angle between the cement sheath μ = the coefficient of friction
The stress relationship, showing the force required to produce shear failure along a bond
plane, is determined by measuring the force required to initiate pipe movement in the
cement sheath in the laboratory (Carter and Evans, 1964)
shearforcebond = forcecementcasingcontactsurfacearea (7)
During cement slurry design, therefore, the shear bond force should be an important
factor to be taking into consideration as this greatly affects the integrity of the well.
Figure 4: Diagram Showing Casing Cement and the Formation
Hydraulic Bond: This is defined by Carter and Evans (1964) as the bond that prevents the
migration of fluid into the cemented part and is determined by applying the pressure at
the pipe-cement interface until leakage occurs. In this experiment, special core holders
are built to determine the hydraulic bond of a specimen. The hydraulic pressure, when the
leakage appears at either end of the specimen, is defined as the bond failure pressure in
psi. The hydraulic bond prevents the longitudinal movement of fluid along the casing and
between cement and adjacent geological horizons. Hydraulic bond at the cement-
formation interface is influenced to a great extent by rock type and the presence or
absence of filter cake. Hydraulic bond is usually much better in Permeable formations
Cement
Casing Formation
Texas Tech University, Stacey J. Amamoo, May 2012
10
because cement slurry develops a higher compressive strength as it loses water to the
formation (Scott and Brace, 1966).
2.3 FACTORS AFFECTING CASING-CEMENT BOND AND CASING-ROCK BOND
2.3.1 Wettability of contact specimen
Fluids only adhere to solids when the solid material is wet by that particular fluid
medium. It is very important to check whether and to what extent the cement slurry
wets the solids which are supposed to be cemented when investigating the causes of
bond between cement slurries, pipes and formation. This is because the more surface
wetted with the cement material, the higher the resultant shear bond strength value.
However, very few studies have been performed to investigate the wetting behavior of
fluids. The contact angle set up by the fluid drop characterizes the wetting ability of the
fluid. The wettability is good when the fluid shows a flattened drop (Scott and Brace,
1966).
2.3.2 Roughness of contact faces
During wetting, the bond of cement slurry to the contact surface is caused by the
intermolecular adhesive forces. The intimacy of the contact determines the strength of the
adhesive force. It is assumed that the cement slurry must penetrate the pores of the
contact surface therefore the roughness of the medium affects the bond between casing or
formation and the slurry. Experiments have shown that bond strength increases with
increasing roughness of the contact surface (Scott and Brace, 1966).
2.3.3 Degree of hydration of the cement
Degree of hydration may be defined as the ratio of cement that has completely reacted
with water as compared to the total amount of cement in the sample. This is usually
computed by measuring the slurry’s chemical shrinkage within twenty-four hours of
hydration. This is based on measuring the volume of water imbibed into a cement slurry
sample of known mass during hydration. Chemical shrinkage will be at a maximum when
Texas Tech University, Stacey J. Amamoo, May 2012
11
the cement is hydrated completely and the products cease undergoing transformation.
Powers and Brownyard (1946).
2.3.4 Bond of cement under well conditions
Under well conditions the casing needs to be adequately supported. Bond strength needed
to support the casing is given by (Scott and Brace (1966)
τ = L ∗ GπDH (8)
Where
τ =Bond Strength
L = length of casing
G= weight of casing
H= height of cement column
D= outer diameter of casing, in the consistent system of units
The above mentioned factors are important when designing the a cased hole completion
and should be taken into consideration in order to prevent the wellbore from failing.
2.4 EXPERIMENTAL TESTS CARRIED OUT ON CEMENT
2.4.1 Triaxial Compression test
This is a test performed to determining Poisson’s ratio and young’s modulus. In 2006,
Stiles used it to determine effective compressive strength. In a triaxial compression test, a
constant confinement pressure is applied around the sample, usually, a cylindrical core
and the axial stress is steadily increased until failure is reached.
Texas Tech University, Stacey J. Amamoo, May 2012
12
Figure 5: Typical Triaxial Testing Cell
2.4.2 Brazilian Compression Testing Method/ Splitting Tensile Stress Testing
Brazilian Compression Test is done to determine the indirect tensile strength. Specimen
is disk shaped with double compressive forces acting across the diameter. The load is
applied until failure occurs. The load induces tensile stress thereby making tensile failure
occur instead of compression. The indirect tensile strength can then be computed by the
equation:
%U = 2VWXY (9)
Where
%U= Brazilian tensile strength, psi
F= maximum applied load, lbf
L= Length of the specimen, in
Texas Tech University, Stacey J. Amamoo, May 2012
13
D= diameter of the specimen, in
According to Heinold et al. (2003) the Brazilian compression tests gives a relatively
higher value as compared to the direct tensile testing method depending on the size and
aspect ratio however, Jaeger and Cook, 1976 believe they give very similar results. The
Brazilian compression tests are used more often because it is believed to be more
practicable and closely mimics the failure mode in most brittle materials.
2.4.3 Unconfined Compressive Test
In this experiment, only the axial stress is taken into consideration. The lateral stress is
set to zero. Therefore the singular axial stress measured here is known as the unconfined
compressive stress. The unconfined compressive test is important because it is able to
provide the least strength estimate of the material under testing. This can also be used to
calibrate the Young’s and Poisson’s ratios using the basic Hooke’s law. The state of
stress at the center of the sample can be represented by:
%Z = %%8 = %[ = 0 (10)
Figure 6: The Uniaxial or Brazilian Test
F
D
L
Texas Tech University, Stacey J. Amamoo, May 2012
14
Figure 7: Setup for the Unconfined Compressive Test
2.4.4 Direct shear Strength
This provides the shear strength properties along a plane of weakness
Figure 8: Direct Shear Test
Texas Tech University, Stacey J. Amamoo, May 2012
15
Figure 9: Generalized Shear Stress and Shear Displacement Curve
Figure 8 Shows the Setup for the Direct Shear Test and Figure 9 Shows the Generalized Shear Stress
and Shear Displacement Curve Courtesy ASTME
2.5 SCOPE AND OBJECTIVES
The aim of this thesis is to model and analyze a cased horizontal well using the distinct
element method. Using this method, the discontinuity of the casing cement and formation
bonded together as well as a portion of their continuous behavior will be taken into
consideration. The overburden stress will also be considered. Micro-crack initiation,
plastic deformation, debonding and ultimately failure will be analyzed.
In order to achieve these, the ITASCA Particle Flow Code software which allows one to
model and analyze discontinuity in granular media will be used. Data will be obtained
from a Barnett Shale horizontal well field example by Vermylen (2011). Using PFC, the
steel casing, shale formation and cement will be modeled separately and then put together
to determine the stresses at the interfaces. Graphs and other trend line plots will then be
used analyze the stresses, strains, deformation and failure.
Texas Tech University, Stacey J. Amamoo, May 2012
16
Figure 10: Cracks in Cement Sheath As Demonstrated By Ravi et al. (2002)
Figure 11: Plastic Deformation in Cement Sheath as Demonstrated By Ravi et al (2002)
Texas Tech University, Stacey J. Amamoo, May 2012
17
Figure 12: Debonding In Cement- Formation Interface As Demonstrated By Ravi Et Al (2002)
Figure 13: Debonding In Cement- Casing Interface As Demonstrated By Ravi Et Al (2002)
Texas Tech University, Stacey J. Amamoo, May 2012
18
CHAPTER 3
NUMERICAL MODELING OF CEMENT-CASING-FORMATION SYSTEM
Numerical methods used in geomechanics can be grouped under continuous methods and
discontinuous methods. The continuous or continuity methods are finite element method,
finite difference method and boundary element method. The discrete element method
falls under the discontinuous method.
Figure 14: Numerical Methods Used in Geomechanics
3.1 FINITE ELEMENT METHOD
This is one of the oldest numerical methods used in modeling continua. Many schools of
thought believe that it was in use long before the advent of computers. Using FEM,
partial differentials can be solved by separating the problem into numerous components
each with a shape peculiar to the component. Simple trial functions are then used to
approximate the solution. Due to these approximations it is always better to have a
greater number of components for better accuracy. FEM is widely used for engineering
stress analyses that do not require fragmentation of the material. According to Bobet
Texas Tech University, Stacey J. Amamoo, May 2012
19
(2010) the finite element method relies on the displacement principle that implies that the
total external virtual work done by a deformable body, as a result of its virtual
displacement (however small) applied to the body, must be equal to the total internal
work associated with the virtual displacement field for a body to be in equilibrium. As a
result of its relative ease of computations, finite element method is used in geomechanics
than any other form of numerical analysis.
Figure 15: Illustration of the Finite Element Method
According to Jaeger and Cook (1979) the advantages of Finite Element Method include
- Computations are relatively easy
- The size and mode of selecting elements are random such that irregular
boundaries can be fitted easily, usually, a greater portion of nodal points can be
selected in regions of higher stress concentration.
- Different surfaces and forces can be easily utilized as the boundaries are not a
fixed shape.
- Homogeneity and isotropicity is not a requirement as each element has its own
stiffness matrix.
3 2
1 4
3
2
1
4
Texas Tech University, Stacey J. Amamoo, May 2012
20
- Different rheological models may be utilized as it is not restricted to elastic
models only
- Friction and dilatants joints are allowed at joint surfaces
- The final output can be processed in the computer in any desired fashion.
Some disadvantages of the finite element method are
- for a specific problem, a specific solution is obtained thus making it impossible to
generalize the system’s behavior as a whole
- it is important to have a good and reliable FEM software in order to analyze a
system using FEM
- A large input and output data are required
- Approximation becomes a problem as computers can allow only a finite number
of significant figures
- Using grid systems does not model some geometrical figures accurately
- Effects like buckling cannot be accurately modeled
3.2 FINITE DIFFERENCE METHOD
This is also a very common method used in solving numerical problems especially partial
differential equations. Here, Taylor’s expansion is used to approximate the differential
equation. FDM usually requires the use of uniform grids which makes it very difficult to
solve complex problems requiring the use of non-uniform system of grids. (Ertekin et al)
The basic operators used in the approximation of the derivative of the finite difference
method are:
- Forward difference
- Central difference
- Backward difference
Texas Tech University, Stacey J. Amamoo, May 2012
21
Forward Difference
∆]�^2 = ]�^2_Z − ]�^2 (11)
Central Difference
`]�^2 = ]a^2_Z 8⁄ c − ]�^2dZ 8⁄ (12)
or `]�^2 = ]�^2_Z − ]�^2dZ (13)
Backward difference
∇]�^2 = ]�^2 − ]�^2dZ (14)
The finite difference method is normally used in simulation of hydrocarbon reservoirs
usually for fluid flow but sometimes (rarely) used in geomechanics.
Figure 16: Representation of Lagrangian FDM Where Domain Is Divided Into Nodes and Zones
Texas Tech University, Stacey J. Amamoo, May 2012
22
The main advantages of finite difference method are:
- Approximation methods make computations easier than the other numerical
methods
Disadvantages include:
- Uniform grid system makes it hard to solve problems involving non uniform grids
- Approximations make the source of error greater than the other numerical
methods
3.3 BOUNDARY ELEMENT METHOD
The boundary element method is used when the other continuity methods such as finite
element and finite difference have failed particularly in areas regarding better accuracy
such as stress concentration and infinite domains. The BEM requires that discretization is
done only at the boundaries instead of the whole domain.
Advantages of the boundary element method are:
- It requires less time to solve a problem
- It requires less data relative to the other numerical methods
- It requires less money since one only needs to discretize at the boundaries and
hence less data
- They are good for problems which involve rapidly changing stress
- Systems of equations are smaller and less cumbersome since discretization is at
the boundaries only
Disadvantages include
- The BEM is not applicable to non-linear flow equations
- Matrices used in BEM are unsymmetrical and fully populated making them
harder to solve than the other numerical methods.
Texas Tech University, Stacey J. Amamoo, May 2012
23
3.4 DISTINCT ELEMENT METHOD
This is a method introduced by Cundall and Strack 1979 to model granular media. In
recent times it has been used to model rock mass that usually contains faults and cracks a
well as granular media cemented together.DEM uses a form of finite difference scheme
that helps to study groups of individual particles. By monitoring the interaction between
the elements, the behavior of the material as a whole can be determined. When using
DEM, stresses and displacement in a space or volume containing a huge number of
particles such as sand grains or grains in cement can be modeled. In distinct element
modeling, the material is represented as an assembly of independent particles which are
able to interact with each other. A boundary of each element can be represented through
the model explicitly reproducing the discrete nature of the discontinuities.
The DEM can also be used to model several materials that do not have a particulate
nature. This may be achieved by the assumption that the whole material may be
approximated into discrete particles which are cemented together or bonded together by
cohesive forces. DEM also allows the incorporation of heat/ temperature effects as well
as fluid pressure (Jing and Stephansson 2008).
The distinct element method was mainly created for mechanical deformation of
assembled elements and these are governed by the equations of motion of rigid or
deformable bodies. To simulate deformation, Cauchy’s equations are sometimes used,
Fourier’s law is also used for heat transfer and Navier-Stokes for fluid flow though micro
apertures.
Cauchy’s equation of motion for deformation: Although many may argue that
deformation of a body is generally a continuum process, it may be considered otherwise
on a microscopic scale. It is however true that translation leading to deformation is
indeed considered as continuum but this is only on a macroscopic scale. Discretization of
a continuum as described in Jing and Stephansson’s Fundamentals of Discrete Element
Methods for Rock Engineering(2007) may be described as an ‘’approximation of a
Texas Tech University, Stacey J. Amamoo, May 2012
24
continuous system with infinite degrees of freedom by a discrete system of elements with
finite degrees of freedom’’.
Cauchy’s equation of motion can be derived from Newton’s second law – a body will
continue to move in a uniform state or, if at rest, remain at in that state unless acted upon
by an external unbalanced force. This unbalanced force will accelerate the body leading
to a change in direction, speed or both. Cauchy built equation based on this fact and came
up with the equation:
fYg2Yh = i%2ji j +k2
(15)
Where,
ρ = Density
t = Time
σ = Stress
b = Body force
(In the consistent system of units)
Texas Tech University, Stacey J. Amamoo, May 2012
25
Figure 17: Particles during Motion (Courtesy Jing and Stephansson 2007)
Fourier’s law: To determine the temperature distribution in wellbore, we can safely use
Fourier’s law and the heat equation. The basic Fourier’s law states that “heat flux across a
unit cross sectional area A, is proportional to the temperature gradient”
l∞n ioi j
(16)
l = −p ioi j (17)
Cylindrical coordinates may be used to describe Fourier’s law in a wellbore
l =−p�ioi9 q + ioir s + ioit u (18)
As well as heat flow
Texas Tech University, Stacey J. Amamoo, May 2012
26
p v19 ii9 w9 ioi9x + 198 iir w9 ioirx + iit wioitxy + z = f{@ ioih (19)
Where,
Q = Heat Flux
A = Cross Sectional area
T = Temperature
κ = Constant of Proportionality
cp = Specific Heat Capacity
ρ = Density
(In consistent system of units)
Texas Tech University, Stacey J. Amamoo, May 2012
27
Figure 18: Cylindrical Coordinates for Fourier’s Heat Law
3.5 USING PFC
The particle flow code, like any distinct element method models discontinuum in any
area of research where several discrete particles which exhibit huge strain and/or
fracturing is needed. It helps to analyze as well as test the mechanical properties of these
particles. The particle flow code is good in such a way that it is not limited to specific
problems or applications. Variations in simulations include simulating flow of a
substance – rapid or otherwise, as well as the brittleness of a rigid structure which takes
into consideration micro and macro fractures alike.
Assumptions made by the PFC model include
- the elements/ particles are regarded as rigid
- the contacts occur over an unusually small area
- the soft contact method is utilized at the contacts thereby allowing the
rigid particles to overlap one another at these points
- the overlaps are relatively small as compared to the actual particle sizes
Texas Tech University, Stacey J. Amamoo, May 2012
28
- The force displacement law relates the magnitude of overlap to the contact
force. The force displacement law is basically defined as
V2 = |2`2 (20)
Where,
F = Force
K = Stiffness
δ = increment
i = normal or shear
- Bonds may exist as contacts between particles
- All particles are spherical
As mentioned earlier, the PFC model, like any distinct element model allows continuum
to be adequately modeled by approximating the solid body into a compacted legion of
several particles. This allows the stress and strain to be measured accurately by defining
the average of the elemental volume.
3.5.1 The calculation cycle
The PFC utilizes a calculation cycle that involve the continuous cycle of the law of
motion and the force displacement law applied to each contact. The position of the walls
is also updated all the time. Contacts may be ball to ball, wall to wall or ball to wall
depending on the scenario.
Texas Tech University, Stacey J. Amamoo, May 2012
29
Figure 19: Calculation Cycle of PFC
3.5.2 Boundary and initial condition
Boundary and initial conditions may be set for both balls and walls. For walls,
translational velocities, rotational velocities as well as centre of rotation may be specified
but the applied force cannot. However, in the balls the translational, rotational velocities
and the applied force can be specified. The equation for finding the velocity of a point p
is calculated by
�2} = �2~ +�2j��j~a^�}−^�~c (21)
Where
xp = position of a point p
�2~= translational velocity
ωw=rotational velocity
Texas Tech University, Stacey J. Amamoo, May 2012
30
�2}= velocity at a point p
^�~= center of rotation
3.5.3 Contact Models
Selecting a contact bond is one of the most important steps in using ITASCA PFC 3d.
There are two main types of contact models of which other models have been derived.
The main contact bonds are:
- Linear
- Hertz
Each model is characterized by specific component behaviors namely stiffness, slip and
bonding behaviors.
Stiffness describes relative displacements and contact forces in the shear and normal
directions using the following equations for normal stiffness (secant) and shear stiffness
(tangent)
V23 =|3�3�2
(22)
∆V23 =−u��2� (23)
Slip, as its name suggests, describes the sliding nature of two contacting bodies. The
condition of slip is verified by calculating the maximum allowable shear contact force
defined by the equation:
V-./� = �|V23| (24)
If |V2�| > V-./� (25)
Then slip occurs and the magnitude of
Texas Tech University, Stacey J. Amamoo, May 2012
31
|V2�| = V-./�
(26)
And V2� ← V2� 6V-./��V2�� : (27)
Where,
Kn = normal stiffness
Fs = shear force
ks = shear stiffness
Un = normal displacement
Us = shear displacement
Fsmax = Maximum allowable shear force
3.5.4 Bonding Behaviors
Contact bond: These are characterized by the following,
- Constant normal and shear stress acting at the contact point
- Allow tensile forces to develop at contact that is, when Un < 0 there is no overlap
- If |Fcn| ≥n bond, the bond breaks and both the normal and shear bonds are set to
zero
- If |Fcs| ≥ s_bond, the bond breaks but contact forces are not changed, provided the
FS is not greater than the friction limit and provided the shear force is compressive V3 > 0 → o���q�� �3 > 0 → �g�9���
- Precludes the possibility of a slip
Texas Tech University, Stacey J. Amamoo, May 2012
32
Parallel bond: This is characterized by the following:
- Provides finite sized piece of a cementatious material deposited between two balls
that are treated as spheres
- Does not preclude the possibility of a slip
If
%-./ ≥%�
(28)
Or D-./ ≥D� (29)
Then the bond breaks
Where,
σmax = maximum normal stress
τmax = maximum shear stress
σc = normal stress at the contact
τc = shear stress at the contact
3.5.5 The Logic of Measurement in PFC
The following quantities are defined with respect to a specified measured volume in PFC:
porosity, coordination number, sliding fraction, stress rate and strain rate.
Porosity: The porosity φ is defined as the ratio of the empty volume in the specified
region of measurement to the whole volume of the measurement region. It may be
mathematically represented as:
Texas Tech University, Stacey J. Amamoo, May 2012
33
∅ =�F�2��&�2 = �&�2 − �-.U�&�2 = 1 − �-.U�&�2 (30)
Where,
Vvoid = Volume of empty space
Vroi = Volume of region of interest
Vmat = Volume of material within the region of interest
Sliding Fraction: This is defined as the ratio of contacts within the region of measurement
that are slipping to the whole region of measurement. Also the magnitude of the shear
contact force should be in the neighborhood of 0.1% (one tenth of a percent) of the
maximum allowable shear force, Fsmax
Stress: Since stress is a continuum quantity, PFC uses averaging steps in order to
compute stress in a discrete medium on a microscale. The following mathematical steps
are used in the computation of stress
The average stress acting throughout the measuring volume%�2j can be given by:
%�2j = 1��%2j��� (31)
And since stresses are only present in spherical particles and clumps when considering a
granular material, the sum over Np particles and Nl clumps can replace the integral,
thereby giving:
%�2j = 1���%�2j�@����� +�%�2j�����
���
(32)
Where,
Texas Tech University, Stacey J. Amamoo, May 2012
34
%�2j�@ = averagestressinparticlep
%�2j�� = averagestressinclumps The average stresses in each body can be computed by:
%�2j�∅ = 1��∅ � ^2�� − ^2�∅¡Vj��,∅�£�∅
(33)
Where,
^2�∅ = Location of a body’s centroid ^2�� = Location of a body’s contact Vj��,∅= Force at a body’s centroid
Figure 20: PFC Plot Of Balls In Contact (Smooth Joint)
Texas Tech University, Stacey J. Amamoo, May 2012
35
The volume associated with each body is represented by
� = ∑ ��@�� + ∑ �����1 − r (34)
Where φ is the porosity of the region of interest
The three equations can be combined to give the average stress:
%�2j = 6 1 − �∑ ��@�� ∑ ����� :��%�2j�@����� +�%�2j�����
���
(35)
%�2j = 6 1 − �∑ ��@�� ∑ ����� :¥�� ^2�� − ^2�@¡Vj��,@�£�∅��+�� ^2�� − ^2��¡Vj��,��£�∅�� y
(36)
Where,
Nl = number of clumps
Np = number of particles
Vc = velocity at contact
nc = number of active contacts
Coordination number: This can be defined as the number of active contacts in a body and
it is calculated by the equation:
¦3 = ∑ ���@�� + ∑ ������§@ + §� (37)
Texas Tech University, Stacey J. Amamoo, May 2012
36
CHAPTER 4
METHODOLOGY
In order to use the field properties of the materials, PFC needs to convert the
macroproperties into microproperties usable by PFC. Microproperties used in the
simulation are summarized in table 2 and table 3. Parallel bonds were assumed for steel
and cement whereas contact bonds were assumed for formation. Figure 21 to 24 shows
the step by step procedure for simulation in PFC 2D. The three materials: cement,
formation and casing were simulated separately to determine the correct microproperties
to be used. They were then combined and a biaxial compression test performed. Stress
and strain graphs as well as microcrack formation in the system were analyzed.
Texas Tech University, Stacey J. Amamoo, May 2012
37
4.1 DETERMINATION OF MICROPROPERTIES
Figure 21: Determination of Microproperties of Materials
Texas Tech University, Stacey J. Amamoo, May 2012
38
4.2 ALGORITHM FOR COMPRESSION TESTING WITH PFC
Figure 22: Part I of the Testing Procedure
Creation and Packing of ‘Granular’
Particles
Define Platens
- Use
Extended
Walls
Define Groups
ie alter steel,
rock cement
properties
Define Assembly
- Porosity
- Volume
- # of Balls
Define
lateral wall
stiffness
Set
Parameters,
Assemble,
Create walls,
Plot
Texas Tech University, Stacey J. Amamoo, May 2012
39
Figure 23: Part II of the Testing Procedure
Texas Tech University, Stacey J. Amamoo, May 2012
40
Figure 24: Part III of the Testing Procedure
4.3 VALIDATION
In validation of the software, a paper by D. Stiles (2006) – ‘The Effects of Ultrahigh
Temperature on the Mechanical Properties of cement’ is used. The effect of extremely
high temperature on the mechanical properties of cement was investigated over a two
year period using experimental analysis. The sample selected for validation is low-
density thixotropic cement with a density of 14.5ppg and consisted of 92% class A, 8%
gypsum together with 40% silica flour by weight of blend.
Texas Tech University, Stacey J. Amamoo, May 2012
41
From these experiments, he noted that the effective compressive strength (i.e. the
pressure at which confining the rock will cause it to fail) increased with time. He also
deduced that the Young’s modulus increased and stabilized. The conventional cement
system exhibited plastic behavior at room temperature but became brittle after continuous
exposure to high temperature. To convert the Stile’s laboratory macroproperties to PFC
readable properties, the microproperties of the cement are derived by the author and a
biaxial test is performed numerically on the sample. Figure 26 of the validation shows of
the sample and breaks in the parallel bond and deformation of the cylindrical sample.
Using PFC, initial yield occurred at 5.4 MPa (783 psi) was achieved which corresponds
to the initial yield estimated by Stiles as shown in Figure 28.
TABLE 2: DATA USED IN VALIDATION
Parameter Value
Young’s Modulus 7GPa
Poisson’s Ratio 0.06
Pb_kn 1.2e35
Pb_ks 1e2
Pb_nstrength 1.2e35
Pb_sstrength 1e2
Texas Tech University, Stacey J. Amamoo, May 2012
42
Figure 25: Sample Setup for Biaxial Test
PFC2D 4.00
Casing-cement- formation
Job Title: ’Validation’
Step 1750 19:17:32 Sun Apr 08 2012
View Size: X: -1.466e+001 <=> 2.666e+001 Y: -1.380e+001 <=> 2.580e+001
Groupsample_rock
Wall
Texas Tech University, Stacey J. Amamoo, May 2012
43
Figure 26: Sample after Failure Showing Deformation and Breaks in Parallel Bond
PFC2D 4.00
Casing-cement- formation
Job Title: ’Validation’
Step 34950 04:59:34 Tue Apr 10 2012
View Size: X: -2.463e+000 <=> 1.446e+001 Y: -2.110e+000 <=> 1.411e+001
Groupsample_rock
Wall
PBond Locations
Texas Tech University, Stacey J. Amamoo, May 2012
44
Figure
27: Deviatorial Stress versus Axial Strain Graph Showing The Initial Yield Of The Sample (PFC)
PFC2D 4.00
Casing-cement- formation
Job Title: ’Validation’
Step 34950 04:55:56 Tue Apr 10 2012
History
0.2 0.4 0.6 0.8 1.0
Axial Strain x10^-1
0.2
0.4
0.6
0.8
1.0
1.2
1.4
1.6
1.8
2.0Axial Stress Difference x10^7
2 devi (FISH Symbol) Linestyle 7.614e+003 <-> 2.004e+007
Vs. 3 deax (FISH Symbol) 7.177e-006 <-> 1.046e-001
Initial yield at
5.4MPa ~ 783psi
Texas Tech University, Stacey J. Amamoo, May 2012
45
Figure 28: Deviatorial Stress versus Axial Strain Graph Showing the Initial Yield of the Sample As Indicated By Stiles (2006)
Texas Tech University, Stacey J. Amamoo, May 2012
46
4.4 ANALYSIS OF HIGH PRESSURE ON WELL INTEGRITY – A HORIZONTAL WELL EXAMPLE
TABLE 3: DATA USED IN HORIZONTAL WELL EXAMPLE
Parameter Unit
Hole Size 7.875 inches
Casing OD 6.625 Inches
Casing ID 5.675 inches
Cement OD 7.875 Inches
Cement ID 6.625 inches
Reservoir pressure 9000 psi
Total Vertical Depth 5700 feet
Length of Lateral 3000 feet
Poisson’s ratio of shale formation 0.23
Young’s Modulus of shale formation 40 GPa
Texas Tech University, Stacey J. Amamoo, May 2012
47
Figure 29: Elastic Load/Unload Test To Determine Properties Of Formation Setup
Texas Tech University, Stacey J. Amamoo, May 2012
48
Figure 30: Elastic Load/Unload Test To Determine Properties Of CEMENT Setup
PFC2D 4.00
Casing-cement- formation
Job Title: ’Elastic
Step 1750 00:40:31 Thu Apr 05 2012
View Size: X: -7.330e+000 <=> 1.333e+001 Y: -6.900e+000 <=> 1.290e+001
Ball
Wall
Texas Tech University, Stacey J. Amamoo, May 2012
49
Figure 31: Elastic Load/Unload Test To Determine Properties Of CASING Setup
PFC2D 4.00
Casing-cement- formation
Job Title: ’Elastic
Step 1750 00:39:20 Thu Apr 05 2012
View Size: X: -7.330e+000 <=> 1.333e+001 Y: -6.900e+000 <=> 1.290e+001
Ball
Wall
Texas Tech University, Stacey J. Amamoo, May 2012
50
Figure 32: CEMENT CASING FORMATION SETUP
Set Up
Texas Tech University, Stacey J. Amamoo, May 2012
51
CHAPTER 5
RESULTS AND ANALYSIS
Loss of integrity of the casing may be demonstrated by the slight deformation of the casing as
shown in figure 33. In analyzing the integrity of the cement, the plastic deformation and
debonding are represented in figures 34 and 35 respectively.
In using this method, the progression of microcrack formation in the cement and formation
bonded together can be determined up to the point of failure. Figure 36 and Figure 38 show
microcrack formation at 10MPa and 100MPa respectively. More cracks are observed in the
vertical direction as a result of increasing overburden stress and deformation. Formation of
microcracks occurred faster when 100MPa was applied than in 10MPa. The direction of
microcracks can also be ascertained using this method and this may be helpful in the creation of
microfractures for the use of stimulation.
The analysis of normal, tangential and radial stresses in the loading and unloading phases of the
biaxial test reveal high hoop stress which is an indication of rock yield (figure 45). According to
Ravi et al (2002) an increase in radial compressive stress (figure 46) may cause compressive
shear failure and this may also be a result of huge differences in principal stresses.
Texas Tech University, Stacey J. Amamoo, May 2012
52
Figure 33: Diagram Showing Slight Deformation of the Casing
PFC2D 4.00
Casing-cement- formation
Job Title: Biaxial Test on Rock-Cement-Formation
Step 44950 20:33:18 Thu Apr 19 2012
View Size: X: -3.611e+000 <=> 9.611e+000 Y: -3.336e+000 <=> 9.336e+000
GroupNonecement_rockcasing_rock
Wall
Texas Tech University, Stacey J. Amamoo, May 2012
53
Figure 34: Diagram Showing Plastic Deformation Of Cement
PFC2D 4.00
Casing-cement- formation
Job Title: Biaxial Test on Rock-Cement-Formation
Step 46750 20:22:50 Thu Apr 19 2012
View Size: X: -3.611e+000 <=> 9.611e+000 Y: -3.336e+000 <=> 9.336e+000
GroupNonecement_rockcasing_rock
Wall
Texas Tech University, Stacey J. Amamoo, May 2012
54
Figure 35: Diagram Showing Debonding Deformation Of Cement
Texas Tech University, Stacey J. Amamoo, May 2012
55
Figure 36: Diagram Showing Microcrack Formation at 10mpa
PFC2D 4.00
Casing-cement- formation
Job Title: Biaxial Test on Rock-Cement-Formation
Step 39750 04:59:12 Fri Apr 20 2012
View Size: X: -2.289e+000 <=> 8.289e+000 Y: -2.069e+000 <=> 8.069e+000
GroupNonecement_rockcasing_rock
FISH function crk_item
Texas Tech University, Stacey J. Amamoo, May 2012
56
Figure 37: GRAPH Showing Microcrack DEVELOPMENT At 10mpa
PFC2D 4.00
Casing-cement- formation
Job Title: Biaxial Test on Rock-Cement-Formation
Step 39750 06:38:35 Fri Apr 20 2012
History
1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0
Deviatoric Stress x10^7
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
1.1
# CB failures in shear x10^2
51 crk_num_csf (FISH Symbol) Linestyle 0.000e+000 <-> 1.140e+002
Vs. 2 devi (FISH Symbol) 8.988e+003 <-> 9.342e+007
Texas Tech University, Stacey J. Amamoo, May 2012
57
Figure 38: Diagram Showing Microcrack Formation At 100mpa
PFC2D 4.00
Casing-cement- formation
Job Title: Biaxial Test on Rock-Cement-Formation
Step 39450 07:00:38 Fri Apr 20 2012
View Size: X: -1.231e+000 <=> 7.231e+000 Y: -1.055e+000 <=> 7.055e+000
GroupNonecement_rockcasing_rock
FISH function crk_item
Texas Tech University, Stacey J. Amamoo, May 2012
58
Figure 39: Graph Showing Microcrack DEVELOPMENT At 100mpa
PFC2D 4.00
Casing-cement- formation
Job Title: failure test 100MPa
Step 39450 07:08:01 Fri Apr 20 2012
History
0.2 0.4 0.6 0.8 1.0 1.2 1.4
Deviatoric Stress x10^8
0.0
0.2
0.4
0.6
0.8
1.0
1.2
1.4
1.6
1.8
2.0
2.2
2.4
2.6
2.8
# CB shear failure x10^2
51 crk_num_csf (FISH Symbol) Linestyle 0.000e+000 <-> 2.950e+002
Vs. 2 devi (FISH Symbol) 1.601e+005 <-> 1.497e+008
Texas Tech University, Stacey J. Amamoo, May 2012
59
Figure 40: PFC Derived Shear Stress versus Effective Normal Strain (10mpa Overburden)
PFC2D 4.00
Casing-cement- formation
Job Title: Failure Test
Step 72750 15:05:27 Sat Apr 07 2012
History
1.5 2.0 2.5 3.0 3.5 4.0 4.5 5.0 5.5
Normal Stress x10^6
0.2
0.4
0.6
0.8
1.0
1.2
1.4
1.6
1.8
2.0
Shear Stress x10^6
10 sstress (FISH Symbol) Linestyle 1.221e+003 <-> 2.171e+006
Vs. 5 nstress (FISH Symbol) 1.001e+006 <-> 5.627e+006
Texas Tech University, Stacey J. Amamoo, May 2012
60
Figure 41: PFC Derived Deviatoric Stress versus Axial Strain @ 10mpa Overburden
PFC2D 4.00
Casing-cement- formation
Job Title: Failure Test
Step 62350 22:36:58 Sat Apr 07 2012
History
0.5 1.0 1.5 2.0 2.5
Axial Strain x10^-1
0.5
1.0
1.5
2.0
2.5
3.0
3.5
4.0
4.5
deviatoric stress x10^6
2 devi (FISH Symbol) Linestyle 4.225e+003 <-> 4.589e+006
Vs. 3 deax (FISH Symbol) 9.311e-006 <-> 2.855e-001
Texas Tech University, Stacey J. Amamoo, May 2012
61
Figure 42: PFC Derived Normal, Tangential and Hoop Stresses at 10mpa Overburden
PFC2D 4.00
Casing-cement- formation
Job Title: Failure Test
Step 62350 22:55:41 Sat Apr 07 2012
History
2.10 2.12 2.14 2.16 2.18 2.20 2.22 2.24 2.26
Distance x10^1
-9.0
-8.0
-7.0
-6.0
-5.0
-4.0
-3.0
-2.0
-1.0
0.0
1.0
2.0
3.0
4.0
Stresses x10^6
5 nstress (FISH Symbol) Linestyle -5.884e+006 <-> -1.004e+006 6 hstress (FISH Symbol) Linestyle -9.178e+006 <-> -8.450e+003 7 rstress (FISH Symbol) Linestyle 4.225e+003 <-> 4.589e+006
Vs. 8 distx (FISH Symbol) 2.095e+001 <-> 2.266e+001
Texas Tech University, Stacey J. Amamoo, May 2012
62
Figure 43: Spreadsheet Analysis of Deviatoric Stress versus Axial Strain @ 10mpa Overburden
0.00E+00
5.00E+05
1.00E+06
1.50E+06
2.00E+06
2.50E+06
0.00E+00 1.00E+06 2.00E+06 3.00E+06 4.00E+06 5.00E+06 6.00E+06
Sh
ea
r S
tre
ss
Effective Normal Stress
shear vs normal
stress
Texas Tech University, Stacey J. Amamoo, May 2012
63
Figure 44: Spreadsheet Analysis of Deviatoric Stress versus Axial Strain @ 10mpa Overburden
0
500000
1000000
1500000
2000000
2500000
3000000
3500000
4000000
4500000
5000000
0 0.05 0.1 0.15 0.2 0.25 0.3
De
via
tori
c S
tre
ss
Axial Strain
devi vs deaxOnset of failure
Texas Tech University, Stacey J. Amamoo, May 2012
64
Figure 45: Spreadsheet Analysis Normal, Tangential and Hoop Stresses @ 10mpa Overburden (Loading)
0
1
2
3
4
5
6
7
8
9
10
0.00E+00 1.00E+02 2.00E+02 3.00E+02 4.00E+02 5.00E+02 6.00E+02 7.00E+02 8.00E+02
stre
sse
s i
n M
pa
distance/ radius in metres
Stresses vs Distance (Loading)
hstress
rstress
nstress
Poly. (hstress)
Poly. (rstress)
Poly. (nstress)
High hoop stresses
may be an indication
of rock yield
Texas Tech University, Stacey J. Amamoo, May 2012
65
Figure 46: Spreadsheet Analysis Normal, Tangential and Hoop Stresses @ 10mpa Overburden (Unloading)
-10000000
-8000000
-6000000
-4000000
-2000000
0
2000000
4000000
6000000
0.00E+00 1.00E+02 2.00E+02 3.00E+02 4.00E+02 5.00E+02 6.00E+02 7.00E+02 8.00E+02
Str
ess
es
in P
a
Distance
Sresses versus Distance(Unloading)
Texas Tech University, Stacey J. Amamoo, May 2012
66
CHAPTER 6
CONCLUSIONS
- When the mud weight is higher than the tangential/ hoop stresses, fractures (axial)
may develop and using the DEM, we can adequately determine when this will
occur.
- Failure can also be determined from the plot of shear stress against effective
normal stress using the most suitable failure criteria – in this case the Mohr-
Coulomb failure criterion may be used to analyze it.
- The plot of deviatoric stress versus axial strain gives a fair estimate of when the
material reaches the plastic region (i.e. loses its elasticity) figure 44.
- Although there were some computational restraints such as unusually long time
for running simulation and complexities of the mathematics, it can be seen that
PFC was able to model stability/instability in a horizontal well.
- Debonding was clearly seen after the load/unload biaxial tests which would have
been very difficult with continuity modeling method. Although Gray et al
discussed debonding in his 2007 paper, a visual representation of the phenomenon
was not achieved possibly due to discretization constraints in the use of finite
element method
- Further processing and trend line analysis of the points generated from the PFC
histories resulted in a much better understanding of the downhole conditions
- The distinct element method is a computationally and mathematically intensive
analytical tool. However as technology improves by the day, the accuracy of
analyzing wellbore stability and integrity and other matters pertaining to the
geomechanics of petroleum engineering will be greatly improved.
- Modeling the steel region (casing) which is not a particulate or granular substance
was particularly challenging but due inverse modeling a good estimate was used.
- From this work, it can be inferred that the best way to model a scenario which
takes into consideration the casing- cement- formation bond would be to use a
Texas Tech University, Stacey J. Amamoo, May 2012
67
numerical and analytical methods which combines both continuity and
discontinuity methods. If this proves feasible the following may be achieved:
• Adequate modeling of discontinuity such as cracks, fractures and
debonding of the interfaces.
• Adequate modeling of continuity such as deformation and representation
of continuous media like steel.
• Excellent representation and accurate modeling of temperature and fluid
flow effects.
Texas Tech University, Stacey J. Amamoo, May 2012
68
REFERENCES
1. Al-Ajmi, Adel. 2006. Wellbore Stability Analysis Based on a New True-Triaxial
Failure Criterion. PhD Dissertation. KTH Royal Institute of Technology.
2. Al-Ajmi, Adel and Robert Zimmerman. 2006. A New 3D Stability Model for the
Design of Non-Vertical Wellbores. American Rock Mechanics Association
3. Austin, S., Robins, P., Pan, Y. 1999. Shear Bond Testing of Concrete Repairs.
Cement and Concrete Research, Volume 29, Issue 7, Pages 1067-1076.
4. Bobet, A. 2010. Numerical Methods in Geomechanics. School of Civil
Engineering, Purdue University, West Lafayette, the Arabian Journal for Science
and Engineering, Volume 35 Number 1B
5. Carter, L. G. and Evans, G. W. 1963. A Study of Cement- pipe Bonding,
presented at SPE Regional Meeting, Santa Barbara, California.
6. Cundall, P. A., and J. Marti. 1979. Some New Developments in Discrete
Numerical Methods for Dynamic Modelling of Jointed Rock Masses. In
Proceedings of the Rapid Excavation and Tunnelling Conference (Atlanta, June
1979), Vol. 2, pp. 1466-1477. Baltimore: Port City Press.
7. Cundall, P. A., and O.D.L. Strack. 1979. A Discrete Numerical Model for
Granular Assemblies. Géotechnique, 29, 47-65 (1979).23.
8. Cundall, P. A., and O.D.L. Strack. 1979. The Development of Constitutive Laws
for Soil Using the Distinct Element Method. In Numerical Methods in
Geomechanics, Vol. 1, pp. 289-317. Rotterdam: Balkema.
9. Ertekin, T., Abou-Kassem, J. H. and King, G. R. 2001. Basic Applied Reservoir
Simulation. Textbook Series. SPE, Richardson.
10. Goodwin K.J., Crook R.J. 1990. Cement Sheath Stress Failure. SPE 20453, Paper
Presented at the SPE Annual Technical Conference and Exhibition, New Orleans.
11. Gray, K.E., E. Podnos and E. Becker. 2007. Finite element studies of near-
wellbore region during cementing operations: Part I. In SPE (106998-MS), 31
March - 3 April, Oklahoma City, Oklahoma, U.S.A.
Texas Tech University, Stacey J. Amamoo, May 2012
69
12. Heinold, T., R.L. Dillenbeck, M.J. Rogers and B.J.S. Company, 2003. Analysis of
tensile strength test methodologies for evaluating oil and gas well cement
systems. Proceedings of the Annual Technical Conference and Exhibition, Oct. 5-
8, Denver, Colorado, pp: 1-13.
13. Heinold, T.et al. 2003. Analysis of Tensile Strength Test Methodologies For
Evaluating Oil and Gas Well Cement Systems paper SPE 84565 presented at the
2003 SPE Annual Technical Conference and Exhibition
14. ITASCA PFC 2D/3D manual
15. Jaeger J.C. and Cook N.G.W., 1976. Fundamentals of Rock Mechanics.
Chapman and Hall, London, 2nd Ed., 585 Pp., Copyright © 1977 Published By
Elsevier B.V.
16. Jing, L. and Stephansson, O. 2007. Fundamentals of Discrete Element Methods
for Rock Engineering: Theory and Applications. Volume 85, Pages 1-545
17. Jones, P.R., and Berdine, D. 1940. Factors Influencing Bond Between Cement
and Formation. API Drilling and Production Practice, Union Oil Companies of
California, Wilmington, California (March),
18. K. Ravi, Halliburton, M. Bosma, Shell International E & P, and O. Gastebled,
TNO Building and Construction Research. 2002. Improve the Economics of Oil
and Gas Wells by Reducing the Risk of Cement Failure. Paper presented at the
2002 IADC/SPE Drilling Conference, Dallas, Texas, 26-28 February.
19. Khandkam, R. K. 2007. Leakage Behind Casing Drilling Specialization Thesis
Work, NTNU, 2007
20. Jing L., Hudson, J.A. 2002. Numerical methods in rock mechanics. International
Journal of Rock Mechanics and Mining Sciences, Volume 39, Issue 4, June 2002,
Pages 409-427
21. Ladva, H.K.J. ;. Braster, B; Jones, T.G.J. ; Goldsmith, G. ; Scott, D. ; The
Cement-to Formation Interface in Zonal Isolation (2004) IADC/SPE 88016,
Kuala Lamour, Malaysia, Sep. 13-15
22. Lake, Larry. 2007. Drilling Engineering. Petroleum Engineering Handbook Vol.2
Society of Petroleum Engineers Society of Petroleum Engineers, 770 pages
Texas Tech University, Stacey J. Amamoo, May 2012
70
23. Ma, Yong et al. 2007. How to Evaluate the Effect of Mud Cake on Cement Bond
Quality of Second Interface SPE/IADC 108240
24. Mohiuddin, M.A., Khan, K., Abdulraheem, A., Al-Majed, A., Awal, M.R. 2007.
Analysis of wellbore instability in vertical, directional, and horizontal wells using
field data, Journal of Petroleum Science and Engineering, Volume 55, Issues 1–2,
January 2007, Pages 83-92, ISSN 0920-4105, 10.1016/j.petrol.2006.04.021.
25. NORSOK Standard D-010 Well integrity in drilling and well operations Rev. 3,
August 2004
26. Orszulik, Stefan T. 2008. Environmental Technology in the Oil Industry (Ed.) 2nd
ed., 2008, XII, 408
27. Pašić, B., Gaurina-Međimurec, N., Matanović, D. 2007. Wellbore Instability:
Causes And Consequences University of Zagreb, Faculty of Mining, Geology and
Petroleum Engineering, Pierottijeva 6, 10000 Zagreb, Croatia, Rud.-geol.-naft.
zb., Vol. 19.
28. Powers, T. C. and Brownyard T. L. 1946. Studies of the Physical Properties of
Hardened Portland Cement Paste. Journal of the A.C.I., 18 (1946), page 101/131.
29. Saint-Marc, Jérémie and Garnier, André Total, and Bois, Axel-Pierre CurisTec:
Initial State of Stress: The Key to Achieving Long-Term Cement-Sheath
Integrity. 2008 SPE 116651 ATCE, Denver, USA
30. Scott, J. B. and Brace, R. L.: Coated Casings - A Technique for Improved Cement
Bonding, Drilling and Prod. Prac., API (1966) 43-47.
31. Shahri, A.M., 2005. Detecting and modeling cement failure in high pressure/high
temperature wells, using finite element method. M.Sc. Thesis, A and M
University, Texas, USA.
32. Soliman, M. and Boonen, P. 2000. Rock mechanics and stimulation aspects of
horizontal wells, Journal of Petroleum Science and Engineering. Volume 25,
Issues 3–4, March 2000, Pages 187-204,
33. Stiles, D. 2006. Effects of Long-Term Exposure to Ultrahigh Temperature on the
Mechanical Parameters of Cement. 98896-MS IADC/SPE Drilling Conference,
21-23 February 2006, Miami, Florida, USA
Texas Tech University, Stacey J. Amamoo, May 2012
71
34. Teodoriu, C., Ugwu, I., Schubert, J. 2010. Estimation of Casing-Cement-
Formation Interaction using a New Analytical Model. (SPE-131335) SPE
EUROPEC 2010, 14-17 June 2010, Barcelona, Spain
35. Vermylen, John P. 2011. Geomechanical Studies Of The Barnett Shale, Texas,
Usa Phd Dissertation Stanford University May 2011
36. Zoback, Mark .D. Reservoir Geomechanics Cambridge University Press, New
York, NY, USA (2007) 449 p
Texas Tech University, Stacey J. Amamoo, May 2012
72
APPENDIX A
DATA SET FOR FAILURE TEST 100MPA
Step Confining
Stress Deviatoric
Stress Axial Strain Volumetric
Strain Distance
x Distance y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
2.65E+03 -1.00E+08 1.99E+06 1.73E-04 3.25E-03 8.53E+00 8.61E+00 -1.00E+08 -3.98E+06 1.99E+06 -9.95E+05
2.85E+03 -1.00E+08 2.14E+06 7.84E-04 3.43E-03 8.53E+00 8.61E+00 -1.00E+08 -4.27E+06 2.14E+06 -1.07E+06
3.05E+03 -1.00E+08 2.32E+06 1.79E-03 2.60E-03 8.53E+00 8.61E+00 -1.00E+08 -4.64E+06 2.32E+06 -1.16E+06
3.25E+03 -1.00E+08 2.64E+06 3.18E-03 1.36E-03 8.52E+00 8.61E+00 -1.00E+08 -5.28E+06 2.64E+06 -1.32E+06
3.45E+03 -1.00E+08 3.01E+06 4.97E-03 -2.85E-04 8.52E+00 8.61E+00 -1.00E+08 -6.03E+06 3.01E+06 -1.51E+06
3.65E+03 -1.00E+08 3.49E+06 7.15E-03 -2.27E-03 8.51E+00 8.61E+00 -1.00E+08 -6.99E+06 3.49E+06 -1.75E+06
3.85E+03 -1.00E+08 4.06E+06 9.72E-03 -4.63E-03 8.50E+00 8.61E+00 -1.00E+08 -8.11E+06 4.06E+06 -2.03E+06
4.05E+03 -1.00E+08 4.72E+06 1.27E-02 -7.34E-03 8.49E+00 8.61E+00 -1.00E+08 -9.43E+06 4.72E+06 -2.36E+06
4.25E+03 -1.00E+08 5.45E+06 1.60E-02 -1.04E-02 8.48E+00 8.62E+00 -1.00E+08 -1.09E+07 5.45E+06 -2.73E+06
4.45E+03 -1.00E+08 6.29E+06 1.98E-02 -1.39E-02 8.47E+00 8.62E+00 -1.00E+08 -1.26E+07 6.29E+06 -3.14E+06
4.65E+03 -1.00E+08 7.15E+06 2.37E-02 -1.74E-02 8.46E+00 8.62E+00 -1.00E+08 -1.43E+07 7.15E+06 -3.58E+06
4.85E+03 -1.00E+08 8.03E+06 2.76E-02 -2.10E-02 8.45E+00 8.62E+00 -1.00E+08 -1.61E+07 8.03E+06 -4.02E+06
5.05E+03 -1.00E+08 8.92E+06 3.16E-02 -2.46E-02 8.44E+00 8.62E+00 -1.00E+08 -1.78E+07 8.92E+06 -4.46E+06
5.25E+03 -1.00E+08 9.81E+06 3.55E-02 -2.82E-02 8.43E+00 8.62E+00 -1.00E+08 -1.96E+07 9.81E+06 -4.90E+06
5.45E+03 -1.00E+08 1.07E+07 3.94E-02 -3.17E-02 8.41E+00 8.62E+00 -1.00E+08 -2.14E+07 1.07E+07 -5.35E+06
5.65E+03 -1.00E+08 1.16E+07 4.33E-02 -3.53E-02 8.40E+00 8.63E+00 -1.00E+08 -2.32E+07 1.16E+07 -5.80E+06
Texas Tech University, Stacey J. Amamoo, May 2012
73
Step Confining
Stress Deviatoric
Stress Axial Strain Volumetric
Strain Distance
x Distance y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
5.85E+03 -1.00E+08 1.25E+07 4.73E-02 -3.89E-02 8.39E+00 8.63E+00 -1.00E+08 -2.50E+07 1.25E+07 -6.25E+06
6.05E+03 -1.00E+08 1.34E+07 5.12E-02 -4.25E-02 8.38E+00 8.63E+00 -1.00E+08 -2.68E+07 1.34E+07 -6.70E+06
7.05E+03 -1.00E+08 1.80E+07 7.08E-02 -6.04E-02 8.32E+00 8.64E+00 -1.00E+08 -3.60E+07 1.80E+07 -9.00E+06
7.25E+03 -1.00E+08 1.89E+07 7.48E-02 -6.40E-02 8.31E+00 8.64E+00 -1.00E+08 -3.79E+07 1.89E+07 -9.47E+06
7.45E+03 -1.00E+08 1.99E+07 7.87E-02 -6.75E-02 8.30E+00 8.64E+00 -1.00E+08 -3.97E+07 1.99E+07 -9.94E+06
7.65E+03 -1.00E+08 2.08E+07 8.26E-02 -7.11E-02 8.28E+00 8.64E+00 -1.00E+08 -4.16E+07 2.08E+07 -1.04E+07
8.05E+03 -1.00E+08 2.27E+07 9.05E-02 -7.83E-02 8.26E+00 8.64E+00 -1.00E+08 -4.54E+07 2.27E+07 -1.14E+07
8.25E+03 -1.00E+08 2.37E+07 9.44E-02 -8.18E-02 8.25E+00 8.65E+00 -1.00E+08 -4.73E+07 2.37E+07 -1.18E+07
8.45E+03 -1.00E+08 2.46E+07 9.83E-02 -8.54E-02 8.24E+00 8.65E+00 -1.00E+08 -4.92E+07 2.46E+07 -1.23E+07
8.65E+03 -1.00E+08 2.56E+07 1.02E-01 -8.90E-02 8.22E+00 8.65E+00 -1.00E+08 -5.12E+07 2.56E+07 -1.28E+07
8.85E+03 -1.00E+08 2.66E+07 1.06E-01 -9.26E-02 8.21E+00 8.65E+00 -1.00E+08 -5.31E+07 2.66E+07 -1.33E+07
9.25E+03 -1.00E+08 2.85E+07 1.14E-01 -9.97E-02 8.19E+00 8.65E+00 -1.00E+08 -5.70E+07 2.85E+07 -1.42E+07
9.45E+03 -1.00E+08 2.95E+07 1.18E-01 -1.03E-01 8.18E+00 8.66E+00 -1.00E+08 -5.90E+07 2.95E+07 -1.47E+07
9.65E+03 -1.00E+08 3.05E+07 1.22E-01 -1.07E-01 8.17E+00 8.66E+00 -1.00E+08 -6.09E+07 3.05E+07 -1.52E+07
9.85E+03 -1.00E+08 3.15E+07 1.26E-01 -1.10E-01 8.15E+00 8.66E+00 -1.00E+08 -6.29E+07 3.15E+07 -1.57E+07
1.01E+04 -1.00E+08 3.24E+07 1.30E-01 -1.14E-01 8.14E+00 8.66E+00 -1.00E+08 -6.49E+07 3.24E+07 -1.62E+07
1.03E+04 -1.00E+08 3.34E+07 1.34E-01 -1.18E-01 8.13E+00 8.66E+00 -1.00E+08 -6.69E+07 3.34E+07 -1.67E+07
1.05E+04 -1.00E+08 3.44E+07 1.38E-01 -1.21E-01 8.12E+00 8.66E+00 -1.00E+08 -6.89E+07 3.44E+07 -1.72E+07
1.07E+04 -1.00E+08 3.54E+07 1.42E-01 -1.25E-01 8.11E+00 8.67E+00 -1.00E+08 -7.09E+07 3.54E+07 -1.77E+07
1.09E+04 -1.00E+08 3.65E+07 1.46E-01 -1.28E-01 8.10E+00 8.67E+00 -1.00E+08 -7.29E+07 3.65E+07 -1.82E+07
1.11E+04 -1.00E+08 3.75E+07 1.49E-01 -1.32E-01 8.08E+00 8.67E+00 -1.00E+08 -7.50E+07 3.75E+07 -1.87E+07
1.13E+04 -1.00E+08 3.85E+07 1.53E-01 -1.35E-01 8.07E+00 8.67E+00 -1.00E+08 -7.70E+07 3.85E+07 -1.92E+07
1.15E+04 -1.00E+08 3.95E+07 1.57E-01 -1.39E-01 8.06E+00 8.67E+00 -1.00E+08 -7.90E+07 3.95E+07 -1.98E+07
1.17E+04 -1.00E+08 4.06E+07 1.61E-01 -1.43E-01 8.05E+00 8.67E+00 -1.00E+08 -8.11E+07 4.06E+07 -2.03E+07
1.19E+04 -1.00E+08 4.16E+07 1.65E-01 -1.46E-01 8.04E+00 8.68E+00 -1.00E+08 -8.32E+07 4.16E+07 -2.08E+07
Texas Tech University, Stacey J. Amamoo, May 2012
74
Step Confining
Stress Deviatoric
Stress Axial Strain Volumetric
Strain Distance
x Distance y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
1.21E+04 -1.00E+08 4.26E+07 1.69E-01 -1.50E-01 8.02E+00 8.68E+00 -1.00E+08 -8.52E+07 4.26E+07 -2.13E+07
1.23E+04 -1.00E+08 4.37E+07 1.73E-01 -1.53E-01 8.01E+00 8.68E+00 -1.00E+08 -8.73E+07 4.37E+07 -2.18E+07
1.25E+04 -1.00E+08 4.47E+07 1.77E-01 -1.57E-01 8.00E+00 8.68E+00 -1.00E+08 -8.94E+07 4.47E+07 -2.24E+07
1.27E+04 -1.00E+08 4.58E+07 1.81E-01 -1.60E-01 7.99E+00 8.68E+00 -1.00E+08 -9.15E+07 4.58E+07 -2.29E+07
1.29E+04 -1.00E+08 4.68E+07 1.85E-01 -1.64E-01 7.98E+00 8.68E+00 -1.00E+08 -9.36E+07 4.68E+07 -2.34E+07
1.31E+04 -1.00E+08 4.79E+07 1.89E-01 -1.68E-01 7.97E+00 8.69E+00 -1.00E+08 -9.57E+07 4.79E+07 -2.39E+07
1.33E+04 -1.00E+08 4.89E+07 1.93E-01 -1.71E-01 7.95E+00 8.69E+00 -1.00E+08 -9.79E+07 4.89E+07 -2.45E+07
1.35E+04 -1.00E+08 5.00E+07 1.97E-01 -1.75E-01 7.94E+00 8.69E+00 -1.00E+08 -1.00E+08 5.00E+07 -2.50E+07
1.37E+04 -1.00E+08 5.11E+07 2.01E-01 -1.78E-01 7.93E+00 8.69E+00 -1.00E+08 -1.02E+08 5.11E+07 -2.55E+07
1.39E+04 -1.00E+08 5.22E+07 2.05E-01 -1.82E-01 7.92E+00 8.69E+00 -1.00E+08 -1.04E+08 5.22E+07 -2.61E+07
1.41E+04 -1.00E+08 5.32E+07 2.09E-01 -1.85E-01 7.91E+00 8.69E+00 -1.00E+08 -1.06E+08 5.32E+07 -2.66E+07
1.43E+04 -1.00E+08 5.43E+07 2.12E-01 -1.89E-01 7.89E+00 8.70E+00 -1.00E+08 -1.09E+08 5.43E+07 -2.72E+07
1.45E+04 -1.00E+08 5.54E+07 2.16E-01 -1.92E-01 7.88E+00 8.70E+00 -1.00E+08 -1.11E+08 5.54E+07 -2.77E+07
1.47E+04 -1.00E+08 5.65E+07 2.20E-01 -1.96E-01 7.87E+00 8.70E+00 -1.00E+08 -1.13E+08 5.65E+07 -2.83E+07
1.49E+04 -1.00E+08 5.76E+07 2.24E-01 -2.00E-01 7.86E+00 8.70E+00 -1.00E+08 -1.15E+08 5.76E+07 -2.88E+07
1.51E+04 -1.00E+08 5.87E+07 2.28E-01 -2.03E-01 7.85E+00 8.70E+00 -1.00E+08 -1.17E+08 5.87E+07 -2.94E+07
1.53E+04 -1.00E+08 5.98E+07 2.32E-01 -2.07E-01 7.84E+00 8.70E+00 -1.00E+08 -1.20E+08 5.98E+07 -2.99E+07
1.55E+04 -1.00E+08 6.09E+07 2.36E-01 -2.10E-01 7.82E+00 8.71E+00 -1.00E+08 -1.22E+08 6.09E+07 -3.05E+07
1.57E+04 -1.00E+08 6.21E+07 2.40E-01 -2.14E-01 7.81E+00 8.71E+00 -1.00E+08 -1.24E+08 6.21E+07 -3.10E+07
1.59E+04 -1.00E+08 6.32E+07 2.44E-01 -2.17E-01 7.80E+00 8.71E+00 -1.00E+08 -1.26E+08 6.32E+07 -3.16E+07
1.61E+04 -1.00E+08 6.43E+07 2.48E-01 -2.21E-01 7.79E+00 8.71E+00 -1.00E+08 -1.29E+08 6.43E+07 -3.21E+07
1.63E+04 -1.00E+08 6.54E+07 2.52E-01 -2.24E-01 7.78E+00 8.71E+00 -1.00E+08 -1.31E+08 6.54E+07 -3.27E+07
1.65E+04 -1.00E+08 6.66E+07 2.56E-01 -2.28E-01 7.76E+00 8.71E+00 -1.00E+08 -1.33E+08 6.66E+07 -3.33E+07
1.67E+04 -1.00E+08 6.65E+07 2.56E-01 -2.28E-01 7.76E+00 8.72E+00 -1.00E+08 -1.33E+08 6.65E+07 -3.33E+07
1.69E+04 -1.00E+08 6.63E+07 2.55E-01 -2.27E-01 7.77E+00 8.72E+00 -1.00E+08 -1.33E+08 6.63E+07 -3.32E+07
1.71E+04 -1.00E+08 6.61E+07 2.54E-01 -2.26E-01 7.77E+00 8.71E+00 -1.00E+08 -1.32E+08 6.61E+07 -3.30E+07
Texas Tech University, Stacey J. Amamoo, May 2012
75
Step Confining
Stress Deviatoric
Stress Axial Strain Volumetric
Strain Distance
x Distance y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
1.75E+04 -1.00E+08 6.51E+07 2.51E-01 -2.23E-01 7.78E+00 8.71E+00 -1.00E+08 -1.30E+08 6.51E+07 -3.26E+07
1.77E+04 -1.00E+08 6.45E+07 2.49E-01 -2.21E-01 7.79E+00 8.71E+00 -1.00E+08 -1.29E+08 6.45E+07 -3.23E+07
1.79E+04 -1.00E+08 6.38E+07 2.46E-01 -2.19E-01 7.79E+00 8.71E+00 -1.00E+08 -1.28E+08 6.38E+07 -3.19E+07
1.81E+04 -1.00E+08 6.29E+07 2.43E-01 -2.16E-01 7.80E+00 8.71E+00 -1.00E+08 -1.26E+08 6.29E+07 -3.15E+07
1.83E+04 -1.00E+08 6.19E+07 2.40E-01 -2.13E-01 7.81E+00 8.71E+00 -1.00E+08 -1.24E+08 6.19E+07 -3.10E+07
1.85E+04 -1.00E+08 6.09E+07 2.36E-01 -2.10E-01 7.82E+00 8.71E+00 -1.00E+08 -1.22E+08 6.09E+07 -3.04E+07
1.87E+04 -1.00E+08 5.98E+07 2.32E-01 -2.06E-01 7.84E+00 8.71E+00 -1.00E+08 -1.20E+08 5.98E+07 -2.99E+07
1.89E+04 -1.00E+08 5.87E+07 2.28E-01 -2.03E-01 7.85E+00 8.70E+00 -1.00E+08 -1.17E+08 5.87E+07 -2.93E+07
1.91E+04 -1.00E+08 5.76E+07 2.24E-01 -1.99E-01 7.86E+00 8.70E+00 -1.00E+08 -1.15E+08 5.76E+07 -2.88E+07
1.93E+04 -1.00E+08 5.65E+07 2.20E-01 -1.96E-01 7.87E+00 8.70E+00 -1.00E+08 -1.13E+08 5.65E+07 -2.82E+07
1.95E+04 -1.00E+08 5.54E+07 2.16E-01 -1.92E-01 7.88E+00 8.70E+00 -1.00E+08 -1.11E+08 5.54E+07 -2.77E+07
1.97E+04 -1.00E+08 5.43E+07 2.12E-01 -1.88E-01 7.89E+00 8.70E+00 -1.00E+08 -1.09E+08 5.43E+07 -2.71E+07
1.99E+04 -1.00E+08 5.32E+07 2.08E-01 -1.85E-01 7.91E+00 8.70E+00 -1.00E+08 -1.06E+08 5.32E+07 -2.66E+07
2.01E+04 -1.00E+08 5.21E+07 2.04E-01 -1.81E-01 7.92E+00 8.69E+00 -1.00E+08 -1.04E+08 5.21E+07 -2.61E+07
2.03E+04 -1.00E+08 5.10E+07 2.00E-01 -1.78E-01 7.93E+00 8.69E+00 -1.00E+08 -1.02E+08 5.10E+07 -2.55E+07
2.05E+04 -1.00E+08 4.99E+07 1.97E-01 -1.74E-01 7.94E+00 8.69E+00 -1.00E+08 -9.99E+07 4.99E+07 -2.50E+07
2.07E+04 -1.00E+08 4.89E+07 1.93E-01 -1.71E-01 7.95E+00 8.69E+00 -1.00E+08 -9.78E+07 4.89E+07 -2.44E+07
2.09E+04 -1.00E+08 4.78E+07 1.89E-01 -1.67E-01 7.97E+00 8.69E+00 -1.00E+08 -9.56E+07 4.78E+07 -2.39E+07
2.11E+04 -1.00E+08 4.73E+07 1.87E-01 -1.65E-01 7.97E+00 8.69E+00 -1.00E+08 -9.46E+07 4.73E+07 -2.37E+07
2.13E+04 -1.00E+08 4.74E+07 1.87E-01 -1.66E-01 7.97E+00 8.69E+00 -1.00E+08 -9.48E+07 4.74E+07 -2.37E+07
2.15E+04 -1.00E+08 4.76E+07 1.88E-01 -1.67E-01 7.97E+00 8.69E+00 -1.00E+08 -9.53E+07 4.76E+07 -2.38E+07
2.17E+04 -1.00E+08 4.79E+07 1.89E-01 -1.68E-01 7.96E+00 8.69E+00 -1.00E+08 -9.59E+07 4.79E+07 -2.40E+07
2.19E+04 -1.00E+08 4.84E+07 1.91E-01 -1.69E-01 7.96E+00 8.69E+00 -1.00E+08 -9.67E+07 4.84E+07 -2.42E+07
2.21E+04 -1.00E+08 4.89E+07 1.93E-01 -1.71E-01 7.95E+00 8.69E+00 -1.00E+08 -9.78E+07 4.89E+07 -2.45E+07
2.23E+04 -1.00E+08 4.96E+07 1.95E-01 -1.73E-01 7.95E+00 8.69E+00 -1.00E+08 -9.91E+07 4.96E+07 -2.48E+07
2.25E+04 -1.00E+08 5.03E+07 1.98E-01 -1.76E-01 7.94E+00 8.69E+00 -1.00E+08 -1.01E+08 5.03E+07 -2.52E+07
Texas Tech University, Stacey J. Amamoo, May 2012
76
Step Confining
Stress Deviatoric
Stress Axial Strain Volumetric
Strain Distance
x Distance y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
2.27E+04 -1.00E+08 5.12E+07 2.01E-01 -1.79E-01 7.93E+00 8.69E+00 -1.00E+08 -1.02E+08 5.12E+07 -2.56E+07
2.29E+04 -1.00E+08 5.22E+07 2.05E-01 -1.82E-01 7.92E+00 8.69E+00 -1.00E+08 -1.04E+08 5.22E+07 -2.61E+07
2.31E+04 -1.00E+08 5.32E+07 2.09E-01 -1.85E-01 7.91E+00 8.69E+00 -1.00E+08 -1.06E+08 5.32E+07 -2.66E+07
2.33E+04 -1.00E+08 5.43E+07 2.13E-01 -1.89E-01 7.89E+00 8.70E+00 -1.00E+08 -1.09E+08 5.43E+07 -2.72E+07
2.35E+04 -1.00E+08 5.54E+07 2.16E-01 -1.92E-01 7.88E+00 8.70E+00 -1.00E+08 -1.11E+08 5.54E+07 -2.77E+07
2.37E+04 -1.00E+08 5.65E+07 2.20E-01 -1.96E-01 7.87E+00 8.70E+00 -1.00E+08 -1.13E+08 5.65E+07 -2.82E+07
2.39E+04 -1.00E+08 5.76E+07 2.24E-01 -2.00E-01 7.86E+00 8.70E+00 -1.00E+08 -1.15E+08 5.76E+07 -2.88E+07
2.41E+04 -1.00E+08 5.87E+07 2.28E-01 -2.03E-01 7.85E+00 8.70E+00 -1.00E+08 -1.17E+08 5.87E+07 -2.93E+07
2.43E+04 -1.00E+08 5.98E+07 2.32E-01 -2.07E-01 7.84E+00 8.70E+00 -1.00E+08 -1.20E+08 5.98E+07 -2.99E+07
2.45E+04 -1.00E+08 6.09E+07 2.36E-01 -2.10E-01 7.82E+00 8.71E+00 -1.00E+08 -1.22E+08 6.09E+07 -3.05E+07
2.47E+04 -1.00E+08 6.20E+07 2.40E-01 -2.14E-01 7.81E+00 8.71E+00 -1.00E+08 -1.24E+08 6.20E+07 -3.10E+07
2.49E+04 -1.00E+08 6.32E+07 2.44E-01 -2.17E-01 7.80E+00 8.71E+00 -1.00E+08 -1.26E+08 6.32E+07 -3.16E+07
2.51E+04 -1.00E+08 6.43E+07 2.48E-01 -2.21E-01 7.79E+00 8.71E+00 -1.00E+08 -1.29E+08 6.43E+07 -3.21E+07
2.53E+04 -1.00E+08 6.54E+07 2.52E-01 -2.24E-01 7.78E+00 8.71E+00 -1.00E+08 -1.31E+08 6.54E+07 -3.27E+07
2.55E+04 -1.00E+08 6.66E+07 2.56E-01 -2.28E-01 7.76E+00 8.71E+00 -1.00E+08 -1.33E+08 6.66E+07 -3.33E+07
2.57E+04 -1.00E+08 6.77E+07 2.60E-01 -2.32E-01 7.75E+00 8.72E+00 -1.00E+08 -1.35E+08 6.77E+07 -3.39E+07
2.59E+04 -1.00E+08 6.89E+07 2.64E-01 -2.35E-01 7.74E+00 8.72E+00 -1.00E+08 -1.38E+08 6.89E+07 -3.44E+07
2.61E+04 -1.00E+08 7.00E+07 2.68E-01 -2.39E-01 7.73E+00 8.72E+00 -1.00E+08 -1.40E+08 7.00E+07 -3.50E+07
2.63E+04 -1.00E+08 7.12E+07 2.72E-01 -2.42E-01 7.72E+00 8.72E+00 -1.00E+08 -1.42E+08 7.12E+07 -3.56E+07
2.65E+04 -1.00E+08 7.23E+07 2.76E-01 -2.46E-01 7.70E+00 8.72E+00 -1.00E+08 -1.45E+08 7.23E+07 -3.62E+07
2.67E+04 -1.00E+08 7.35E+07 2.80E-01 -2.49E-01 7.69E+00 8.73E+00 -1.00E+08 -1.47E+08 7.35E+07 -3.68E+07
2.69E+04 -1.00E+08 7.47E+07 2.84E-01 -2.53E-01 7.68E+00 8.73E+00 -1.00E+08 -1.49E+08 7.47E+07 -3.73E+07
2.71E+04 -1.00E+08 7.59E+07 2.87E-01 -2.56E-01 7.67E+00 8.73E+00 -1.00E+08 -1.52E+08 7.59E+07 -3.79E+07
2.73E+04 -1.00E+08 7.71E+07 2.91E-01 -2.60E-01 7.66E+00 8.73E+00 -1.00E+08 -1.54E+08 7.71E+07 -3.85E+07
2.75E+04 -1.00E+08 7.83E+07 2.95E-01 -2.64E-01 7.65E+00 8.73E+00 -1.00E+08 -1.57E+08 7.83E+07 -3.91E+07
2.77E+04 -1.00E+08 7.95E+07 2.99E-01 -2.67E-01 7.63E+00 8.73E+00 -1.00E+08 -1.59E+08 7.95E+07 -3.97E+07
Texas Tech University, Stacey J. Amamoo, May 2012
77
Step Confining
Stress Deviatoric
Stress Axial Strain Volumetric
Strain Distance
x Distance y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
2.79E+04 -1.00E+08 8.07E+07 3.03E-01 -2.71E-01 7.62E+00 8.74E+00 -1.00E+08 -1.61E+08 8.07E+07 -4.03E+07
2.81E+04 -1.00E+08 8.19E+07 3.07E-01 -2.74E-01 7.61E+00 8.74E+00 -1.00E+08 -1.64E+08 8.19E+07 -4.09E+07
2.83E+04 -1.00E+08 8.31E+07 3.11E-01 -2.78E-01 7.60E+00 8.74E+00 -1.00E+08 -1.66E+08 8.31E+07 -4.15E+07
2.85E+04 -1.00E+08 8.43E+07 3.15E-01 -2.81E-01 7.59E+00 8.74E+00 -1.00E+08 -1.69E+08 8.43E+07 -4.21E+07
2.87E+04 -1.00E+08 8.55E+07 3.19E-01 -2.85E-01 7.57E+00 8.74E+00 -1.00E+08 -1.71E+08 8.55E+07 -4.28E+07
2.89E+04 -1.00E+08 8.67E+07 3.23E-01 -2.88E-01 7.56E+00 8.75E+00 -1.00E+08 -1.74E+08 8.67E+07 -4.34E+07
2.91E+04 -1.00E+08 8.80E+07 3.27E-01 -2.92E-01 7.55E+00 8.75E+00 -1.00E+08 -1.76E+08 8.80E+07 -4.40E+07
2.93E+04 -1.00E+08 8.92E+07 3.31E-01 -2.95E-01 7.54E+00 8.75E+00 -1.00E+08 -1.78E+08 8.92E+07 -4.46E+07
2.95E+04 -1.00E+08 9.05E+07 3.35E-01 -2.99E-01 7.53E+00 8.75E+00 -1.00E+08 -1.81E+08 9.05E+07 -4.52E+07
2.97E+04 -1.00E+08 9.17E+07 3.39E-01 -3.02E-01 7.52E+00 8.75E+00 -1.00E+08 -1.83E+08 9.17E+07 -4.59E+07
2.99E+04 -1.00E+08 9.30E+07 3.43E-01 -3.06E-01 7.50E+00 8.76E+00 -1.00E+08 -1.86E+08 9.30E+07 -4.65E+07
3.01E+04 -1.00E+08 9.43E+07 3.47E-01 -3.10E-01 7.49E+00 8.76E+00 -1.00E+08 -1.89E+08 9.43E+07 -4.71E+07
3.03E+04 -1.00E+08 9.55E+07 3.51E-01 -3.13E-01 7.48E+00 8.76E+00 -1.00E+08 -1.91E+08 9.55E+07 -4.78E+07
3.05E+04 -1.00E+08 9.68E+07 3.55E-01 -3.17E-01 7.47E+00 8.76E+00 -1.00E+08 -1.94E+08 9.68E+07 -4.84E+07
3.07E+04 -1.00E+08 9.81E+07 3.59E-01 -3.20E-01 7.46E+00 8.76E+00 -1.00E+08 -1.96E+08 9.81E+07 -4.91E+07
3.11E+04 -1.00E+08 1.01E+08 3.67E-01 -3.27E-01 7.43E+00 8.77E+00 -1.00E+08 -2.01E+08 1.01E+08 -5.04E+07
3.13E+04 -1.00E+08 1.02E+08 3.71E-01 -3.31E-01 7.42E+00 8.77E+00 -1.00E+08 -2.04E+08 1.02E+08 -5.10E+07
3.15E+04 -1.00E+08 1.03E+08 3.75E-01 -3.34E-01 7.41E+00 8.77E+00 -1.00E+08 -2.07E+08 1.03E+08 -5.17E+07
3.17E+04 -1.00E+08 1.05E+08 3.78E-01 -3.38E-01 7.40E+00 8.77E+00 -1.00E+08 -2.09E+08 1.05E+08 -5.23E+07
3.19E+04 -1.00E+08 1.06E+08 3.82E-01 -3.41E-01 7.38E+00 8.78E+00 -1.00E+08 -2.12E+08 1.06E+08 -5.30E+07
3.21E+04 -1.00E+08 1.07E+08 3.86E-01 -3.45E-01 7.37E+00 8.78E+00 -1.00E+08 -2.15E+08 1.07E+08 -5.36E+07
3.23E+04 -1.00E+08 1.09E+08 3.90E-01 -3.48E-01 7.36E+00 8.78E+00 -1.00E+08 -2.17E+08 1.09E+08 -5.43E+07
3.25E+04 -1.00E+08 1.10E+08 3.94E-01 -3.52E-01 7.35E+00 8.78E+00 -1.00E+08 -2.20E+08 1.10E+08 -5.50E+07
3.27E+04 -1.00E+08 1.11E+08 3.98E-01 -3.55E-01 7.34E+00 8.78E+00 -1.00E+08 -2.23E+08 1.11E+08 -5.56E+07
3.29E+04 -1.00E+08 1.13E+08 4.02E-01 -3.59E-01 7.33E+00 8.79E+00 -1.00E+08 -2.25E+08 1.13E+08 -5.63E+07
3.31E+04 -1.00E+08 1.14E+08 4.06E-01 -3.62E-01 7.31E+00 8.79E+00 -1.00E+08 -2.28E+08 1.14E+08 -5.70E+07
Texas Tech University, Stacey J. Amamoo, May 2012
78
Step Confining
Stress Deviatoric
Stress Axial Strain Volumetric
Strain Distance
x Distance y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
3.33E+04 -1.00E+08 1.15E+08 4.10E-01 -3.66E-01 7.30E+00 8.79E+00 -1.00E+08 -2.31E+08 1.15E+08 -5.77E+07
3.35E+04 -1.00E+08 1.17E+08 4.14E-01 -3.69E-01 7.29E+00 8.79E+00 -1.00E+08 -2.33E+08 1.17E+08 -5.84E+07
3.37E+04 -1.00E+08 1.18E+08 4.18E-01 -3.73E-01 7.28E+00 8.79E+00 -1.00E+08 -2.36E+08 1.18E+08 -5.91E+07
3.39E+04 -1.00E+08 1.19E+08 4.22E-01 -3.76E-01 7.27E+00 8.80E+00 -1.00E+08 -2.39E+08 1.19E+08 -5.97E+07
3.41E+04 -1.00E+08 1.21E+08 4.26E-01 -3.80E-01 7.25E+00 8.80E+00 -1.00E+08 -2.41E+08 1.21E+08 -6.04E+07
3.43E+04 -1.00E+08 1.22E+08 4.30E-01 -3.83E-01 7.24E+00 8.80E+00 -1.00E+08 -2.44E+08 1.22E+08 -6.11E+07
3.45E+04 -1.00E+08 1.24E+08 4.34E-01 -3.87E-01 7.23E+00 8.80E+00 -1.00E+08 -2.47E+08 1.24E+08 -6.18E+07
3.47E+04 -1.00E+08 1.25E+08 4.38E-01 -3.90E-01 7.22E+00 8.81E+00 -1.00E+08 -2.50E+08 1.25E+08 -6.24E+07
3.49E+04 -1.00E+08 1.26E+08 4.42E-01 -3.94E-01 7.21E+00 8.81E+00 -1.00E+08 -2.53E+08 1.26E+08 -6.31E+07
3.51E+04 -1.00E+08 1.28E+08 4.46E-01 -3.97E-01 7.19E+00 8.81E+00 -1.00E+08 -2.55E+08 1.28E+08 -6.38E+07
3.57E+04 -1.00E+08 1.32E+08 4.58E-01 -4.07E-01 7.16E+00 8.82E+00 -1.00E+08 -2.64E+08 1.32E+08 -6.59E+07
3.59E+04 -1.00E+08 1.33E+08 4.62E-01 -4.11E-01 7.15E+00 8.82E+00 -1.00E+08 -2.66E+08 1.33E+08 -6.66E+07
3.61E+04 -1.00E+08 1.35E+08 4.66E-01 -4.14E-01 7.13E+00 8.82E+00 -1.00E+08 -2.69E+08 1.35E+08 -6.73E+07
3.63E+04 -1.00E+08 1.36E+08 4.70E-01 -4.18E-01 7.12E+00 8.82E+00 -1.00E+08 -2.72E+08 1.36E+08 -6.80E+07
3.65E+04 -1.00E+08 1.37E+08 4.74E-01 -4.21E-01 7.11E+00 8.83E+00 -1.00E+08 -2.75E+08 1.37E+08 -6.87E+07
3.67E+04 -1.00E+08 1.39E+08 4.78E-01 -4.24E-01 7.10E+00 8.83E+00 -1.00E+08 -2.78E+08 1.39E+08 -6.94E+07
3.69E+04 -1.00E+08 1.40E+08 4.82E-01 -4.28E-01 7.09E+00 8.83E+00 -1.00E+08 -2.81E+08 1.40E+08 -7.01E+07
3.71E+04 -1.00E+08 1.42E+08 4.85E-01 -4.31E-01 7.08E+00 8.83E+00 -1.00E+08 -2.83E+08 1.42E+08 -7.08E+07
3.73E+04 -1.00E+08 1.43E+08 4.89E-01 -4.35E-01 7.06E+00 8.84E+00 -1.00E+08 -2.86E+08 1.43E+08 -7.15E+07
3.75E+04 -1.00E+08 1.44E+08 4.93E-01 -4.38E-01 7.05E+00 8.84E+00 -1.00E+08 -2.89E+08 1.44E+08 -7.22E+07
3.77E+04 -1.00E+08 1.46E+08 4.97E-01 -4.42E-01 7.04E+00 8.84E+00 -1.00E+08 -2.91E+08 1.46E+08 -7.29E+07
3.79E+04 -1.00E+08 1.47E+08 5.01E-01 -4.45E-01 7.03E+00 8.84E+00 -1.00E+08 -2.94E+08 1.47E+08 -7.35E+07
3.81E+04 -1.00E+08 1.49E+08 5.05E-01 -4.48E-01 7.02E+00 8.85E+00 -1.00E+08 -2.97E+08 1.49E+08 -7.43E+07
3.83E+04 -1.00E+08 1.50E+08 5.09E-01 -4.52E-01 7.00E+00 8.85E+00 -1.00E+08 -3.00E+08 1.50E+08 -7.50E+07
3.87E+04 -1.00E+08 1.52E+08 5.17E-01 -4.58E-01 6.98E+00 8.86E+00 -1.00E+08 -3.05E+08 1.52E+08 -7.62E+07
3.89E+04 -1.00E+08 1.54E+08 5.21E-01 -4.62E-01 6.97E+00 8.86E+00 -1.00E+08 -3.08E+08 1.54E+08 -7.69E+07
Texas Tech University, Stacey J. Amamoo, May 2012
79
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
2.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
6.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
6.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
6.45E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
6.65E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
6.85E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
7.05E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
7.25E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
7.45E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
80
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
7.65E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
7.85E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
8.05E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
8.25E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
8.45E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
8.65E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
8.85E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
9.05E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
9.25E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
9.45E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
9.65E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
9.85E+03 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.01E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.03E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.05E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.07E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.09E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.11E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.13E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.15E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.17E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.19E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.21E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.23E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.25E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.27E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
81
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
1.29E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.31E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
1.33E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
1.35E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
1.37E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
1.39E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
1.41E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
1.43E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
1.45E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
1.47E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
1.49E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
1.51E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
1.53E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
1.55E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
1.57E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
1.59E+04 4.00E+00 0.00E+00 4.00E+00 0.00E+00 0.00E+00
1.61E+04 4.00E+00 0.00E+00 4.00E+00 0.00E+00 0.00E+00
1.63E+04 7.00E+00 0.00E+00 7.00E+00 0.00E+00 0.00E+00
1.65E+04 7.00E+00 0.00E+00 7.00E+00 0.00E+00 0.00E+00
1.67E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.69E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.71E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.73E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.75E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.77E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.79E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
82
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
1.81E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.83E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.85E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.87E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.89E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.91E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.93E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.95E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.97E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
1.99E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.01E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.03E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.05E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.07E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.09E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.11E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.13E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.15E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.17E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.19E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.21E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.23E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.25E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.27E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.29E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.31E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
83
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
2.33E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.35E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.37E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.39E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.41E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.43E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.45E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.47E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.49E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.51E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.53E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.55E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
2.57E+04 9.00E+00 0.00E+00 9.00E+00 0.00E+00 0.00E+00
2.59E+04 1.00E+01 0.00E+00 1.00E+01 0.00E+00 0.00E+00
2.61E+04 1.00E+01 0.00E+00 1.00E+01 0.00E+00 0.00E+00
2.63E+04 1.00E+01 0.00E+00 1.00E+01 0.00E+00 0.00E+00
2.65E+04 1.00E+01 0.00E+00 1.00E+01 0.00E+00 0.00E+00
2.67E+04 1.10E+01 0.00E+00 1.10E+01 0.00E+00 0.00E+00
2.69E+04 1.30E+01 0.00E+00 1.30E+01 0.00E+00 0.00E+00
2.71E+04 1.30E+01 0.00E+00 1.30E+01 0.00E+00 0.00E+00
2.73E+04 1.50E+01 0.00E+00 1.50E+01 0.00E+00 0.00E+00
2.75E+04 1.70E+01 0.00E+00 1.70E+01 0.00E+00 0.00E+00
2.77E+04 1.70E+01 0.00E+00 1.70E+01 0.00E+00 0.00E+00
2.79E+04 1.70E+01 0.00E+00 1.70E+01 0.00E+00 0.00E+00
2.81E+04 1.90E+01 0.00E+00 1.90E+01 0.00E+00 0.00E+00
2.83E+04 1.90E+01 0.00E+00 1.90E+01 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
84
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
2.85E+04 1.90E+01 0.00E+00 1.90E+01 0.00E+00 0.00E+00
2.87E+04 2.10E+01 0.00E+00 2.10E+01 0.00E+00 0.00E+00
2.89E+04 2.10E+01 0.00E+00 2.10E+01 0.00E+00 0.00E+00
2.91E+04 2.30E+01 0.00E+00 2.30E+01 0.00E+00 0.00E+00
2.93E+04 2.60E+01 0.00E+00 2.60E+01 0.00E+00 0.00E+00
2.95E+04 2.60E+01 0.00E+00 2.60E+01 0.00E+00 0.00E+00
2.97E+04 2.70E+01 0.00E+00 2.70E+01 0.00E+00 0.00E+00
2.99E+04 2.80E+01 0.00E+00 2.80E+01 0.00E+00 0.00E+00
3.01E+04 2.90E+01 0.00E+00 2.90E+01 0.00E+00 0.00E+00
3.03E+04 3.10E+01 0.00E+00 3.10E+01 0.00E+00 0.00E+00
3.05E+04 3.30E+01 0.00E+00 3.30E+01 0.00E+00 0.00E+00
3.07E+04 3.30E+01 0.00E+00 3.30E+01 0.00E+00 0.00E+00
3.09E+04 3.40E+01 0.00E+00 3.40E+01 0.00E+00 0.00E+00
3.11E+04 3.50E+01 0.00E+00 3.50E+01 0.00E+00 0.00E+00
3.13E+04 3.60E+01 0.00E+00 3.60E+01 0.00E+00 0.00E+00
3.15E+04 3.60E+01 0.00E+00 3.60E+01 0.00E+00 0.00E+00
3.17E+04 3.90E+01 0.00E+00 3.90E+01 0.00E+00 0.00E+00
3.19E+04 4.20E+01 0.00E+00 4.20E+01 0.00E+00 0.00E+00
3.21E+04 4.50E+01 0.00E+00 4.50E+01 0.00E+00 0.00E+00
3.23E+04 5.00E+01 0.00E+00 5.00E+01 0.00E+00 0.00E+00
3.25E+04 5.40E+01 0.00E+00 5.40E+01 0.00E+00 0.00E+00
3.27E+04 5.60E+01 0.00E+00 5.60E+01 0.00E+00 0.00E+00
3.29E+04 5.90E+01 0.00E+00 5.90E+01 0.00E+00 0.00E+00
3.31E+04 6.50E+01 0.00E+00 6.50E+01 0.00E+00 0.00E+00
3.33E+04 6.80E+01 0.00E+00 6.80E+01 0.00E+00 0.00E+00
3.35E+04 7.20E+01 0.00E+00 7.20E+01 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
85
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
3.37E+04 7.80E+01 0.00E+00 7.80E+01 0.00E+00 0.00E+00
3.39E+04 8.40E+01 0.00E+00 8.40E+01 0.00E+00 0.00E+00
3.41E+04 8.70E+01 0.00E+00 8.70E+01 0.00E+00 0.00E+00
3.43E+04 8.90E+01 0.00E+00 8.90E+01 0.00E+00 0.00E+00
3.45E+04 1.01E+02 0.00E+00 1.01E+02 0.00E+00 0.00E+00
3.47E+04 1.12E+02 0.00E+00 1.12E+02 0.00E+00 0.00E+00
3.51E+04 1.27E+02 0.00E+00 1.27E+02 0.00E+00 0.00E+00
3.53E+04 1.34E+02 0.00E+00 1.34E+02 0.00E+00 0.00E+00
3.57E+04 1.44E+02 0.00E+00 1.44E+02 0.00E+00 0.00E+00
3.59E+04 1.53E+02 0.00E+00 1.53E+02 0.00E+00 0.00E+00
3.61E+04 1.63E+02 0.00E+00 1.63E+02 0.00E+00 0.00E+00
3.65E+04 1.77E+02 0.00E+00 1.77E+02 0.00E+00 0.00E+00
3.67E+04 1.87E+02 0.00E+00 1.87E+02 0.00E+00 0.00E+00
3.69E+04 1.95E+02 0.00E+00 1.95E+02 0.00E+00 0.00E+00
3.71E+04 2.06E+02 0.00E+00 2.06E+02 0.00E+00 0.00E+00
3.73E+04 2.13E+02 0.00E+00 2.13E+02 0.00E+00 0.00E+00
3.75E+04 2.25E+02 0.00E+00 2.25E+02 0.00E+00 0.00E+00
3.77E+04 2.33E+02 0.00E+00 2.33E+02 0.00E+00 0.00E+00
3.79E+04 2.41E+02 0.00E+00 2.41E+02 0.00E+00 0.00E+00
3.81E+04 2.53E+02 0.00E+00 2.53E+02 0.00E+00 0.00E+00
3.83E+04 2.60E+02 0.00E+00 2.60E+02 0.00E+00 0.00E+00
3.85E+04 2.70E+02 0.00E+00 2.70E+02 0.00E+00 0.00E+00
3.87E+04 2.75E+02 0.00E+00 2.75E+02 0.00E+00 0.00E+00
3.89E+04 2.83E+02 0.00E+00 2.83E+02 0.00E+00 0.00E+00
CNF = Contact bond normal failure CSF = Contact bond shear failure
PNF = Parallel bond normal failure PSF = Parallel bond shear failure
Texas Tech University, Stacey J. Amamoo, May 2012
86
APPENDIX B
DATA SET FOR FAILURE TEST 10 MPA
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
3.65E+03 -1.00E+07 9.33E+04 2.11E-04 -4.26E-05 1.07E+01 1.08E+01 -1.00E+07 -1.87E+05 9.33E+04 -4.66E+04
3.85E+03 -1.00E+07 1.36E+05 8.11E-04 -4.88E-04 1.07E+01 1.08E+01 -1.00E+07 -2.71E+05 1.36E+05 -6.78E+04
4.25E+03 -1.00E+07 3.06E+05 3.17E-03 -2.69E-03 1.07E+01 1.08E+01 -1.00E+07 -6.13E+05 3.06E+05 -1.53E+05
4.45E+03 -1.00E+07 4.40E+05 4.92E-03 -4.35E-03 1.07E+01 1.08E+01 -1.00E+07 -8.80E+05 4.40E+05 -2.20E+05
4.85E+03 -1.00E+07 7.85E+05 9.59E-03 -8.75E-03 1.07E+01 1.08E+01 -1.00E+07 -1.57E+06 7.85E+05 -3.93E+05
5.05E+03 -1.00E+07 9.97E+05 1.25E-02 -1.15E-02 1.07E+01 1.08E+01 -1.00E+07 -1.99E+06 9.97E+05 -4.99E+05
5.25E+03 -1.00E+07 1.25E+06 1.58E-02 -1.46E-02 1.07E+01 1.09E+01 -1.00E+07 -2.50E+06 1.25E+06 -6.24E+05
5.45E+03 -1.00E+07 1.53E+06 1.95E-02 -1.81E-02 1.07E+01 1.09E+01 -1.00E+07 -3.05E+06 1.53E+06 -7.64E+05
5.65E+03 -1.00E+07 1.81E+06 2.33E-02 -2.17E-02 1.07E+01 1.09E+01 -1.00E+07 -3.62E+06 1.81E+06 -9.05E+05
5.85E+03 -1.00E+07 2.11E+06 2.72E-02 -2.53E-02 1.07E+01 1.09E+01 -1.00E+07 -4.23E+06 2.11E+06 -1.06E+06
6.05E+03 -1.00E+07 2.42E+06 3.11E-02 -2.89E-02 1.06E+01 1.09E+01 -1.00E+07 -4.83E+06 2.42E+06 -1.21E+06
6.25E+03 -1.00E+07 2.72E+06 3.49E-02 -3.25E-02 1.06E+01 1.09E+01 -1.00E+07 -5.43E+06 2.72E+06 -1.36E+06
6.65E+03 -1.00E+07 3.33E+06 4.26E-02 -3.97E-02 1.06E+01 1.09E+01 -1.00E+07 -6.66E+06 3.33E+06 -1.67E+06
6.85E+03 -1.00E+07 3.64E+06 4.65E-02 -4.33E-02 1.06E+01 1.09E+01 -1.00E+07 -7.28E+06 3.64E+06 -1.82E+06
7.05E+03 -1.00E+07 3.95E+06 5.03E-02 -4.69E-02 1.06E+01 1.09E+01 -1.00E+07 -7.91E+06 3.95E+06 -1.98E+06
7.25E+03 -1.00E+07 4.27E+06 5.42E-02 -5.05E-02 1.06E+01 1.09E+01 -1.00E+07 -8.54E+06 4.27E+06 -2.13E+06
7.45E+03 -1.00E+07 4.58E+06 5.81E-02 -5.41E-02 1.06E+01 1.09E+01 -1.00E+07 -9.17E+06 4.58E+06 -2.29E+06
7.65E+03 -1.00E+07 4.90E+06 6.19E-02 -5.77E-02 1.06E+01 1.09E+01 -1.00E+07 -9.80E+06 4.90E+06 -2.45E+06
8.05E+03 -1.00E+07 5.54E+06 6.96E-02 -6.49E-02 1.05E+01 1.09E+01 -1.00E+07 -1.11E+07 5.54E+06 -2.77E+06
8.25E+03 -1.00E+07 5.86E+06 7.35E-02 -6.85E-02 1.05E+01 1.09E+01 -1.00E+07 -1.17E+07 5.86E+06 -2.93E+06
Texas Tech University, Stacey J. Amamoo, May 2012
87
8.25E+03 -1.00E+07 5.86E+06 7.35E-02 -6.85E-02 1.05E+01 1.09E+01 -1.00E+07 -1.17E+07 5.86E+06 -2.93E+06
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
8.45E+03 -1.00E+07 6.18E+06 7.73E-02 -7.21E-02 1.05E+01 1.09E+01 -1.00E+07 -1.24E+07 6.18E+06 -3.09E+06
8.65E+03 -1.00E+07 6.51E+06 8.12E-02 -7.58E-02 1.05E+01 1.09E+01 -1.00E+07 -1.30E+07 6.51E+06 -3.26E+06
8.85E+03 -1.00E+07 6.84E+06 8.51E-02 -7.94E-02 1.05E+01 1.09E+01 -1.00E+07 -1.37E+07 6.84E+06 -3.42E+06
9.05E+03 -1.00E+07 7.17E+06 8.89E-02 -8.30E-02 1.05E+01 1.09E+01 -1.00E+07 -1.43E+07 7.17E+06 -3.58E+06
9.25E+03 -1.00E+07 7.50E+06 9.28E-02 -8.66E-02 1.05E+01 1.09E+01 -1.00E+07 -1.50E+07 7.50E+06 -3.75E+06
9.45E+03 -1.00E+07 7.84E+06 9.66E-02 -9.02E-02 1.05E+01 1.09E+01 -1.00E+07 -1.57E+07 7.84E+06 -3.92E+06
9.65E+03 -1.00E+07 8.17E+06 1.01E-01 -9.38E-02 1.04E+01 1.09E+01 -1.00E+07 -1.63E+07 8.17E+06 -4.09E+06
9.85E+03 -1.00E+07 8.51E+06 1.04E-01 -9.74E-02 1.04E+01 1.09E+01 -1.00E+07 -1.70E+07 8.51E+06 -4.25E+06
1.01E+04 -1.00E+07 8.85E+06 1.08E-01 -1.01E-01 1.04E+01 1.09E+01 -1.00E+07 -1.77E+07 8.85E+06 -4.42E+06
1.03E+04 -1.00E+07 9.19E+06 1.12E-01 -1.05E-01 1.04E+01 1.09E+01 -1.00E+07 -1.84E+07 9.19E+06 -4.60E+06
1.05E+04 -1.00E+07 9.53E+06 1.16E-01 -1.08E-01 1.04E+01 1.09E+01 -1.00E+07 -1.91E+07 9.53E+06 -4.76E+06
1.07E+04 -1.00E+07 9.88E+06 1.20E-01 -1.12E-01 1.04E+01 1.09E+01 -1.00E+07 -1.98E+07 9.88E+06 -4.94E+06
1.09E+04 -1.00E+07 1.02E+07 1.24E-01 -1.15E-01 1.04E+01 1.09E+01 -1.00E+07 -2.04E+07 1.02E+07 -5.11E+06
1.11E+04 -1.00E+07 1.06E+07 1.28E-01 -1.19E-01 1.04E+01 1.09E+01 -1.00E+07 -2.11E+07 1.06E+07 -5.28E+06
1.13E+04 -1.00E+07 1.09E+07 1.31E-01 -1.23E-01 1.03E+01 1.09E+01 -1.00E+07 -2.18E+07 1.09E+07 -5.46E+06
1.15E+04 -1.00E+07 1.13E+07 1.35E-01 -1.26E-01 1.03E+01 1.09E+01 -1.00E+07 -2.25E+07 1.13E+07 -5.63E+06
1.17E+04 -1.00E+07 1.16E+07 1.39E-01 -1.30E-01 1.03E+01 1.09E+01 -1.00E+07 -2.32E+07 1.16E+07 -5.81E+06
1.19E+04 -1.00E+07 1.20E+07 1.43E-01 -1.33E-01 1.03E+01 1.09E+01 -1.00E+07 -2.39E+07 1.20E+07 -5.99E+06
1.21E+04 -1.00E+07 1.23E+07 1.47E-01 -1.37E-01 1.03E+01 1.09E+01 -1.00E+07 -2.46E+07 1.23E+07 -6.16E+06
1.23E+04 -1.00E+07 1.27E+07 1.51E-01 -1.41E-01 1.03E+01 1.09E+01 -1.00E+07 -2.54E+07 1.27E+07 -6.34E+06
1.25E+04 -1.00E+07 1.30E+07 1.55E-01 -1.44E-01 1.03E+01 1.09E+01 -1.00E+07 -2.61E+07 1.30E+07 -6.52E+06
1.27E+04 -1.00E+07 1.34E+07 1.58E-01 -1.48E-01 1.03E+01 1.09E+01 -1.00E+07 -2.68E+07 1.34E+07 -6.70E+06
1.29E+04 -1.00E+07 1.38E+07 1.62E-01 -1.51E-01 1.03E+01 1.09E+01 -1.00E+07 -2.75E+07 1.38E+07 -6.88E+06
1.31E+04 -1.00E+07 1.41E+07 1.66E-01 -1.55E-01 1.02E+01 1.09E+01 -1.00E+07 -2.83E+07 1.41E+07 -7.06E+06
1.33E+04 -1.00E+07 1.45E+07 1.70E-01 -1.59E-01 1.02E+01 1.09E+01 -1.00E+07 -2.90E+07 1.45E+07 -7.25E+06
Texas Tech University, Stacey J. Amamoo, May 2012
88
1.35E+04 -1.00E+07 1.49E+07 1.74E-01 -1.62E-01 1.02E+01 1.09E+01 -1.00E+07 -2.97E+07 1.49E+07 -7.43E+06
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
1.37E+04 -1.00E+07 1.52E+07 1.78E-01 -1.66E-01 1.02E+01 1.09E+01 -1.00E+07 -3.05E+07 1.52E+07 -7.62E+06
1.39E+04 -1.00E+07 1.56E+07 1.82E-01 -1.69E-01 1.02E+01 1.09E+01 -1.00E+07 -3.12E+07 1.56E+07 -7.80E+06
1.41E+04 -1.00E+07 1.60E+07 1.85E-01 -1.73E-01 1.02E+01 1.09E+01 -1.00E+07 -3.19E+07 1.60E+07 -7.99E+06
1.43E+04 -1.00E+07 1.64E+07 1.89E-01 -1.77E-01 1.02E+01 1.09E+01 -1.00E+07 -3.27E+07 1.64E+07 -8.18E+06
1.45E+04 -1.00E+07 1.67E+07 1.93E-01 -1.80E-01 1.02E+01 1.09E+01 -1.00E+07 -3.35E+07 1.67E+07 -8.36E+06
1.47E+04 -1.00E+07 1.71E+07 1.97E-01 -1.84E-01 1.01E+01 1.09E+01 -1.00E+07 -3.42E+07 1.71E+07 -8.55E+06
1.49E+04 -1.00E+07 1.75E+07 2.01E-01 -1.87E-01 1.01E+01 1.09E+01 -1.00E+07 -3.50E+07 1.75E+07 -8.74E+06
1.51E+04 -1.00E+07 1.79E+07 2.05E-01 -1.91E-01 1.01E+01 1.09E+01 -1.00E+07 -3.57E+07 1.79E+07 -8.93E+06
1.53E+04 -1.00E+07 1.82E+07 2.09E-01 -1.95E-01 1.01E+01 1.09E+01 -1.00E+07 -3.65E+07 1.82E+07 -9.12E+06
1.55E+04 -1.00E+07 1.86E+07 2.13E-01 -1.98E-01 1.01E+01 1.09E+01 -1.00E+07 -3.73E+07 1.86E+07 -9.31E+06
1.57E+04 -1.00E+07 1.90E+07 2.16E-01 -2.02E-01 1.01E+01 1.09E+01 -1.00E+07 -3.80E+07 1.90E+07 -9.51E+06
1.59E+04 -1.00E+07 1.94E+07 2.20E-01 -2.05E-01 1.01E+01 1.09E+01 -1.00E+07 -3.88E+07 1.94E+07 -9.70E+06
1.61E+04 -1.00E+07 1.98E+07 2.24E-01 -2.09E-01 1.01E+01 1.09E+01 -1.00E+07 -3.96E+07 1.98E+07 -9.90E+06
1.63E+04 -1.00E+07 2.02E+07 2.28E-01 -2.13E-01 1.01E+01 1.09E+01 -1.00E+07 -4.04E+07 2.02E+07 -1.01E+07
1.65E+04 -1.00E+07 2.06E+07 2.32E-01 -2.16E-01 1.00E+01 1.09E+01 -1.00E+07 -4.12E+07 2.06E+07 -1.03E+07
1.67E+04 -1.00E+07 2.10E+07 2.36E-01 -2.20E-01 1.00E+01 1.09E+01 -1.00E+07 -4.19E+07 2.10E+07 -1.05E+07
1.69E+04 -1.00E+07 2.14E+07 2.40E-01 -2.24E-01 1.00E+01 1.09E+01 -1.00E+07 -4.28E+07 2.14E+07 -1.07E+07
1.71E+04 -1.00E+07 2.18E+07 2.43E-01 -2.27E-01 1.00E+01 1.09E+01 -1.00E+07 -4.36E+07 2.18E+07 -1.09E+07
1.73E+04 -1.00E+07 2.22E+07 2.47E-01 -2.31E-01 1.00E+01 1.09E+01 -1.00E+07 -4.44E+07 2.22E+07 -1.11E+07
1.75E+04 -1.00E+07 2.26E+07 2.51E-01 -2.34E-01 9.99E+00 1.09E+01 -1.00E+07 -4.52E+07 2.26E+07 -1.13E+07
1.77E+04 -1.00E+07 2.25E+07 2.51E-01 -2.34E-01 9.99E+00 1.09E+01 -1.00E+07 -4.51E+07 2.25E+07 -1.13E+07
1.79E+04 -1.00E+07 2.25E+07 2.50E-01 -2.33E-01 9.99E+00 1.09E+01 -1.00E+07 -4.50E+07 2.25E+07 -1.13E+07
1.81E+04 -1.00E+07 2.24E+07 2.49E-01 -2.32E-01 9.99E+00 1.09E+01 -1.00E+07 -4.48E+07 2.24E+07 -1.12E+07
1.83E+04 -9.99E+06 2.23E+07 2.48E-01 -2.31E-01 1.00E+01 1.09E+01 -9.99E+06 -4.45E+07 2.23E+07 -1.11E+07
1.85E+04 -9.99E+06 2.21E+07 2.46E-01 -2.29E-01 1.00E+01 1.09E+01 -9.99E+06 -4.41E+07 2.21E+07 -1.10E+07
Texas Tech University, Stacey J. Amamoo, May 2012
89
1.87E+04 -9.99E+06 2.18E+07 2.44E-01 -2.27E-01 1.00E+01 1.09E+01 -9.99E+06 -4.37E+07 2.18E+07 -1.09E+07
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
1.89E+04 -9.99E+06 2.16E+07 2.42E-01 -2.25E-01 1.00E+01 1.09E+01 -9.99E+06 -4.31E+07 2.16E+07 -1.08E+07
1.91E+04 -9.98E+06 2.13E+07 2.39E-01 -2.22E-01 1.00E+01 1.09E+01 -9.98E+06 -4.25E+07 2.13E+07 -1.06E+07
1.93E+04 -9.98E+06 2.09E+07 2.35E-01 -2.19E-01 1.00E+01 1.09E+01 -9.98E+06 -4.18E+07 2.09E+07 -1.05E+07
1.95E+04 -9.98E+06 2.05E+07 2.32E-01 -2.16E-01 1.00E+01 1.09E+01 -9.98E+06 -4.10E+07 2.05E+07 -1.03E+07
1.97E+04 -9.98E+06 2.01E+07 2.28E-01 -2.12E-01 1.01E+01 1.09E+01 -9.98E+06 -4.03E+07 2.01E+07 -1.01E+07
1.99E+04 -9.98E+06 1.97E+07 2.24E-01 -2.08E-01 1.01E+01 1.09E+01 -9.98E+06 -3.95E+07 1.97E+07 -9.86E+06
2.01E+04 -9.98E+06 1.93E+07 2.20E-01 -2.05E-01 1.01E+01 1.09E+01 -9.98E+06 -3.87E+07 1.93E+07 -9.67E+06
2.03E+04 -9.98E+06 1.89E+07 2.16E-01 -2.01E-01 1.01E+01 1.09E+01 -9.98E+06 -3.79E+07 1.89E+07 -9.47E+06
2.05E+04 -9.98E+06 1.85E+07 2.12E-01 -1.97E-01 1.01E+01 1.09E+01 -9.98E+06 -3.71E+07 1.85E+07 -9.27E+06
2.07E+04 -9.98E+06 1.82E+07 2.08E-01 -1.94E-01 1.01E+01 1.09E+01 -9.98E+06 -3.63E+07 1.82E+07 -9.08E+06
2.09E+04 -9.98E+06 1.78E+07 2.05E-01 -1.90E-01 1.01E+01 1.09E+01 -9.98E+06 -3.55E+07 1.78E+07 -8.89E+06
2.11E+04 -9.98E+06 1.74E+07 2.01E-01 -1.87E-01 1.01E+01 1.09E+01 -9.98E+06 -3.48E+07 1.74E+07 -8.69E+06
2.13E+04 -9.98E+06 1.70E+07 1.97E-01 -1.83E-01 1.01E+01 1.09E+01 -9.98E+06 -3.40E+07 1.70E+07 -8.50E+06
2.15E+04 -9.98E+06 1.66E+07 1.93E-01 -1.79E-01 1.02E+01 1.09E+01 -9.98E+06 -3.32E+07 1.66E+07 -8.31E+06
2.17E+04 -9.98E+06 1.62E+07 1.89E-01 -1.76E-01 1.02E+01 1.09E+01 -9.98E+06 -3.25E+07 1.62E+07 -8.12E+06
2.19E+04 -9.98E+06 1.59E+07 1.85E-01 -1.72E-01 1.02E+01 1.09E+01 -9.98E+06 -3.17E+07 1.59E+07 -7.93E+06
2.21E+04 -9.99E+06 1.57E+07 1.83E-01 -1.70E-01 1.02E+01 1.09E+01 -9.99E+06 -3.13E+07 1.57E+07 -7.84E+06
2.23E+04 -9.99E+06 1.57E+07 1.84E-01 -1.71E-01 1.02E+01 1.09E+01 -9.99E+06 -3.14E+07 1.57E+07 -7.86E+06
2.25E+04 -1.00E+07 1.58E+07 1.85E-01 -1.72E-01 1.02E+01 1.09E+01 -1.00E+07 -3.16E+07 1.58E+07 -7.89E+06
2.27E+04 -1.00E+07 1.59E+07 1.86E-01 -1.73E-01 1.02E+01 1.09E+01 -1.00E+07 -3.18E+07 1.59E+07 -7.95E+06
2.29E+04 -1.00E+07 1.60E+07 1.87E-01 -1.74E-01 1.02E+01 1.09E+01 -1.00E+07 -3.21E+07 1.60E+07 -8.02E+06
2.31E+04 -1.00E+07 1.62E+07 1.89E-01 -1.76E-01 1.02E+01 1.09E+01 -1.00E+07 -3.25E+07 1.62E+07 -8.12E+06
2.33E+04 -1.00E+07 1.65E+07 1.92E-01 -1.78E-01 1.02E+01 1.09E+01 -1.00E+07 -3.29E+07 1.65E+07 -8.24E+06
2.35E+04 -1.00E+07 1.67E+07 1.94E-01 -1.81E-01 1.02E+01 1.09E+01 -1.00E+07 -3.35E+07 1.67E+07 -8.37E+06
2.37E+04 -1.00E+07 1.71E+07 1.97E-01 -1.84E-01 1.01E+01 1.09E+01 -1.00E+07 -3.41E+07 1.71E+07 -8.53E+06
Texas Tech University, Stacey J. Amamoo, May 2012
90
2.39E+04 -1.00E+07 1.74E+07 2.01E-01 -1.87E-01 1.01E+01 1.09E+01 -1.00E+07 -3.48E+07 1.74E+07 -8.70E+06
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
2.41E+04 -1.00E+07 1.78E+07 2.05E-01 -1.91E-01 1.01E+01 1.09E+01 -1.00E+07 -3.56E+07 1.78E+07 -8.89E+06
2.43E+04 -1.00E+07 1.82E+07 2.09E-01 -1.94E-01 1.01E+01 1.09E+01 -1.00E+07 -3.63E+07 1.82E+07 -9.08E+06
2.45E+04 -1.00E+07 1.86E+07 2.13E-01 -1.98E-01 1.01E+01 1.09E+01 -1.00E+07 -3.71E+07 1.86E+07 -9.28E+06
2.47E+04 -1.00E+07 1.89E+07 2.16E-01 -2.02E-01 1.01E+01 1.09E+01 -1.00E+07 -3.79E+07 1.89E+07 -9.47E+06
2.49E+04 -1.00E+07 1.93E+07 2.20E-01 -2.05E-01 1.01E+01 1.09E+01 -1.00E+07 -3.87E+07 1.93E+07 -9.67E+06
2.51E+04 -1.00E+07 1.97E+07 2.24E-01 -2.09E-01 1.01E+01 1.09E+01 -1.00E+07 -3.95E+07 1.97E+07 -9.87E+06
2.53E+04 -1.00E+07 2.01E+07 2.28E-01 -2.13E-01 1.01E+01 1.09E+01 -1.00E+07 -4.03E+07 2.01E+07 -1.01E+07
2.55E+04 -1.00E+07 2.05E+07 2.32E-01 -2.16E-01 1.00E+01 1.09E+01 -1.00E+07 -4.11E+07 2.05E+07 -1.03E+07
2.57E+04 -1.00E+07 2.09E+07 2.36E-01 -2.20E-01 1.00E+01 1.09E+01 -1.00E+07 -4.19E+07 2.09E+07 -1.05E+07
2.59E+04 -1.00E+07 2.14E+07 2.40E-01 -2.23E-01 1.00E+01 1.09E+01 -1.00E+07 -4.27E+07 2.14E+07 -1.07E+07
2.61E+04 -1.00E+07 2.18E+07 2.43E-01 -2.27E-01 1.00E+01 1.09E+01 -1.00E+07 -4.35E+07 2.18E+07 -1.09E+07
2.63E+04 -1.00E+07 2.22E+07 2.47E-01 -2.31E-01 1.00E+01 1.09E+01 -1.00E+07 -4.43E+07 2.22E+07 -1.11E+07
2.65E+04 -1.00E+07 2.26E+07 2.51E-01 -2.34E-01 9.99E+00 1.09E+01 -1.00E+07 -4.52E+07 2.26E+07 -1.13E+07
2.67E+04 -1.00E+07 2.30E+07 2.55E-01 -2.38E-01 9.97E+00 1.09E+01 -1.00E+07 -4.60E+07 2.30E+07 -1.15E+07
2.69E+04 -1.00E+07 2.34E+07 2.59E-01 -2.42E-01 9.96E+00 1.09E+01 -1.00E+07 -4.68E+07 2.34E+07 -1.17E+07
2.71E+04 -1.00E+07 2.38E+07 2.63E-01 -2.45E-01 9.95E+00 1.09E+01 -1.00E+07 -4.76E+07 2.38E+07 -1.19E+07
2.73E+04 -1.00E+07 2.42E+07 2.67E-01 -2.49E-01 9.94E+00 1.10E+01 -1.00E+07 -4.84E+07 2.42E+07 -1.21E+07
2.75E+04 -1.00E+07 2.46E+07 2.71E-01 -2.52E-01 9.93E+00 1.10E+01 -1.00E+07 -4.92E+07 2.46E+07 -1.23E+07
2.77E+04 -1.00E+07 2.50E+07 2.74E-01 -2.56E-01 9.92E+00 1.10E+01 -1.00E+07 -5.01E+07 2.50E+07 -1.25E+07
2.79E+04 -1.00E+07 2.54E+07 2.78E-01 -2.60E-01 9.91E+00 1.10E+01 -1.00E+07 -5.09E+07 2.54E+07 -1.27E+07
2.81E+04 -1.00E+07 2.59E+07 2.82E-01 -2.63E-01 9.89E+00 1.10E+01 -1.00E+07 -5.17E+07 2.59E+07 -1.29E+07
2.83E+04 -1.00E+07 2.63E+07 2.86E-01 -2.67E-01 9.88E+00 1.10E+01 -1.00E+07 -5.25E+07 2.63E+07 -1.31E+07
2.85E+04 -1.00E+07 2.67E+07 2.90E-01 -2.70E-01 9.87E+00 1.10E+01 -1.00E+07 -5.34E+07 2.67E+07 -1.33E+07
2.87E+04 -1.00E+07 2.71E+07 2.94E-01 -2.74E-01 9.86E+00 1.10E+01 -1.00E+07 -5.42E+07 2.71E+07 -1.36E+07
2.89E+04 -1.00E+07 2.75E+07 2.98E-01 -2.78E-01 9.85E+00 1.10E+01 -1.00E+07 -5.51E+07 2.75E+07 -1.38E+07
Texas Tech University, Stacey J. Amamoo, May 2012
91
2.91E+04 -1.00E+07 2.80E+07 3.02E-01 -2.81E-01 9.84E+00 1.10E+01 -1.00E+07 -5.59E+07 2.80E+07 -1.40E+07
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
2.93E+04 -1.00E+07 2.84E+07 3.05E-01 -2.85E-01 9.82E+00 1.10E+01 -1.00E+07 -5.68E+07 2.84E+07 -1.42E+07
2.95E+04 -1.00E+07 2.88E+07 3.09E-01 -2.88E-01 9.81E+00 1.10E+01 -1.00E+07 -5.76E+07 2.88E+07 -1.44E+07
2.97E+04 -1.00E+07 2.92E+07 3.13E-01 -2.92E-01 9.80E+00 1.10E+01 -1.00E+07 -5.85E+07 2.92E+07 -1.46E+07
2.99E+04 -1.00E+07 2.97E+07 3.17E-01 -2.96E-01 9.79E+00 1.10E+01 -1.00E+07 -5.93E+07 2.97E+07 -1.48E+07
3.01E+04 -1.00E+07 3.01E+07 3.21E-01 -2.99E-01 9.78E+00 1.10E+01 -1.00E+07 -6.02E+07 3.01E+07 -1.51E+07
3.03E+04 -1.00E+07 3.05E+07 3.25E-01 -3.03E-01 9.77E+00 1.10E+01 -1.00E+07 -6.11E+07 3.05E+07 -1.53E+07
3.05E+04 -1.00E+07 3.10E+07 3.29E-01 -3.06E-01 9.75E+00 1.10E+01 -1.00E+07 -6.20E+07 3.10E+07 -1.55E+07
3.07E+04 -1.00E+07 3.14E+07 3.32E-01 -3.10E-01 9.74E+00 1.10E+01 -1.00E+07 -6.28E+07 3.14E+07 -1.57E+07
3.09E+04 -1.00E+07 3.19E+07 3.36E-01 -3.14E-01 9.73E+00 1.10E+01 -1.00E+07 -6.37E+07 3.19E+07 -1.59E+07
3.11E+04 -1.00E+07 3.23E+07 3.40E-01 -3.17E-01 9.72E+00 1.10E+01 -1.00E+07 -6.46E+07 3.23E+07 -1.62E+07
3.13E+04 -1.00E+07 3.28E+07 3.44E-01 -3.21E-01 9.71E+00 1.10E+01 -1.00E+07 -6.55E+07 3.28E+07 -1.64E+07
3.15E+04 -1.00E+07 3.32E+07 3.48E-01 -3.24E-01 9.70E+00 1.10E+01 -1.00E+07 -6.64E+07 3.32E+07 -1.66E+07
3.17E+04 -1.00E+07 3.37E+07 3.52E-01 -3.28E-01 9.68E+00 1.10E+01 -1.00E+07 -6.73E+07 3.37E+07 -1.68E+07
3.19E+04 -1.00E+07 3.41E+07 3.56E-01 -3.32E-01 9.67E+00 1.10E+01 -1.00E+07 -6.82E+07 3.41E+07 -1.71E+07
3.21E+04 -1.00E+07 3.46E+07 3.60E-01 -3.35E-01 9.66E+00 1.10E+01 -1.00E+07 -6.91E+07 3.46E+07 -1.73E+07
3.23E+04 -1.00E+07 3.50E+07 3.63E-01 -3.39E-01 9.65E+00 1.10E+01 -1.00E+07 -7.00E+07 3.50E+07 -1.75E+07
3.25E+04 -1.00E+07 3.55E+07 3.67E-01 -3.42E-01 9.64E+00 1.10E+01 -1.00E+07 -7.09E+07 3.55E+07 -1.77E+07
3.27E+04 -1.00E+07 3.60E+07 3.71E-01 -3.46E-01 9.63E+00 1.10E+01 -1.00E+07 -7.19E+07 3.60E+07 -1.80E+07
3.29E+04 -1.00E+07 3.64E+07 3.75E-01 -3.49E-01 9.61E+00 1.10E+01 -1.00E+07 -7.27E+07 3.64E+07 -1.82E+07
3.31E+04 -1.00E+07 3.68E+07 3.79E-01 -3.53E-01 9.60E+00 1.10E+01 -1.00E+07 -7.37E+07 3.68E+07 -1.84E+07
3.33E+04 -1.00E+07 3.72E+07 3.83E-01 -3.56E-01 9.59E+00 1.10E+01 -1.00E+07 -7.45E+07 3.72E+07 -1.86E+07
3.35E+04 -1.00E+07 3.77E+07 3.87E-01 -3.60E-01 9.58E+00 1.10E+01 -1.00E+07 -7.54E+07 3.77E+07 -1.89E+07
3.37E+04 -1.00E+07 3.82E+07 3.91E-01 -3.63E-01 9.57E+00 1.10E+01 -1.00E+07 -7.64E+07 3.82E+07 -1.91E+07
3.39E+04 -1.00E+07 3.86E+07 3.94E-01 -3.67E-01 9.56E+00 1.10E+01 -1.00E+07 -7.72E+07 3.86E+07 -1.93E+07
3.41E+04 -1.00E+07 3.91E+07 3.98E-01 -3.71E-01 9.54E+00 1.10E+01 -1.00E+07 -7.81E+07 3.91E+07 -1.95E+07
Texas Tech University, Stacey J. Amamoo, May 2012
92
3.43E+04 -1.00E+07 3.96E+07 4.02E-01 -3.74E-01 9.53E+00 1.10E+01 -1.00E+07 -7.91E+07 3.96E+07 -1.98E+07
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear
Stress
3.45E+04 -1.00E+07 4.01E+07 4.06E-01 -3.78E-01 9.52E+00 1.10E+01 -1.00E+07 -8.01E+07 4.01E+07 -2.00E+07
3.47E+04 -1.00E+07 4.05E+07 4.10E-01 -3.81E-01 9.51E+00 1.10E+01 -1.00E+07 -8.09E+07 4.05E+07 -2.02E+07
3.49E+04 -1.00E+07 4.08E+07 4.14E-01 -3.85E-01 9.50E+00 1.10E+01 -1.00E+07 -8.16E+07 4.08E+07 -2.04E+07
3.51E+04 -1.00E+07 4.13E+07 4.18E-01 -3.88E-01 9.49E+00 1.10E+01 -1.00E+07 -8.25E+07 4.13E+07 -2.06E+07
3.53E+04 -1.00E+07 4.18E+07 4.22E-01 -3.92E-01 9.48E+00 1.10E+01 -1.00E+07 -8.35E+07 4.18E+07 -2.09E+07
3.57E+04 -1.00E+07 4.26E+07 4.29E-01 -3.99E-01 9.45E+00 1.10E+01 -1.00E+07 -8.53E+07 4.26E+07 -2.13E+07
3.59E+04 -1.00E+07 4.30E+07 4.33E-01 -4.02E-01 9.44E+00 1.10E+01 -1.00E+07 -8.61E+07 4.30E+07 -2.15E+07
3.61E+04 -1.00E+07 4.35E+07 4.37E-01 -4.06E-01 9.43E+00 1.10E+01 -1.00E+07 -8.69E+07 4.35E+07 -2.17E+07
3.63E+04 -1.00E+07 4.39E+07 4.41E-01 -4.09E-01 9.42E+00 1.10E+01 -1.00E+07 -8.79E+07 4.39E+07 -2.20E+07
3.65E+04 -1.00E+07 4.44E+07 4.45E-01 -4.13E-01 9.41E+00 1.10E+01 -1.00E+07 -8.89E+07 4.44E+07 -2.22E+07
3.67E+04 -1.00E+07 4.49E+07 4.49E-01 -4.16E-01 9.39E+00 1.10E+01 -1.00E+07 -8.98E+07 4.49E+07 -2.24E+07
3.69E+04 -1.00E+07 4.54E+07 4.53E-01 -4.20E-01 9.38E+00 1.10E+01 -1.00E+07 -9.08E+07 4.54E+07 -2.27E+07
3.71E+04 -1.00E+07 4.59E+07 4.56E-01 -4.23E-01 9.37E+00 1.10E+01 -1.00E+07 -9.17E+07 4.59E+07 -2.29E+07
3.73E+04 -1.00E+07 4.64E+07 4.60E-01 -4.27E-01 9.36E+00 1.10E+01 -1.00E+07 -9.27E+07 4.64E+07 -2.32E+07
3.77E+04 -1.00E+07 4.74E+07 4.68E-01 -4.34E-01 9.34E+00 1.10E+01 -1.00E+07 -9.48E+07 4.74E+07 -2.37E+07
3.79E+04 -1.00E+07 4.79E+07 4.72E-01 -4.38E-01 9.32E+00 1.10E+01 -1.00E+07 -9.58E+07 4.79E+07 -2.39E+07
3.81E+04 -1.00E+07 4.84E+07 4.76E-01 -4.41E-01 9.31E+00 1.11E+01 -1.00E+07 -9.68E+07 4.84E+07 -2.42E+07
3.83E+04 -1.00E+07 4.87E+07 4.80E-01 -4.45E-01 9.30E+00 1.11E+01 -1.00E+07 -9.75E+07 4.87E+07 -2.44E+07
3.85E+04 -1.01E+07 4.90E+07 4.84E-01 -4.48E-01 9.29E+00 1.11E+01 -1.01E+07 -9.81E+07 4.90E+07 -2.45E+07
3.87E+04 -1.01E+07 4.95E+07 4.87E-01 -4.51E-01 9.28E+00 1.11E+01 -1.01E+07 -9.90E+07 4.95E+07 -2.48E+07
3.89E+04 -1.00E+07 5.00E+07 4.91E-01 -4.55E-01 9.27E+00 1.11E+01 -1.00E+07 -1.00E+08 5.00E+07 -2.50E+07
3.91E+04 -1.00E+07 5.06E+07 4.95E-01 -4.58E-01 9.25E+00 1.11E+01 -1.00E+07 -1.01E+08 5.06E+07 -2.53E+07
3.93E+04 -1.00E+07 5.10E+07 4.99E-01 -4.62E-01 9.24E+00 1.11E+01 -1.00E+07 -1.02E+08 5.10E+07 -2.55E+07
3.95E+04 -1.00E+07 5.11E+07 5.03E-01 -4.66E-01 9.23E+00 1.11E+01 -1.00E+07 -1.02E+08 5.11E+07 -2.56E+07
3.97E+04 -1.01E+07 5.16E+07 5.07E-01 -4.69E-01 9.22E+00 1.11E+01 -1.01E+07 -1.03E+08 5.16E+07 -2.58E+07
Texas Tech University, Stacey J. Amamoo, May 2012
93
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
3.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
4.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
5.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
6.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
6.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
6.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
6.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
6.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
8.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
8.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
94
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
8.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
8.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
8.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.01E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.03E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.05E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.07E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.09E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.11E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.13E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.15E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.17E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.19E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.21E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.23E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.25E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.27E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.29E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.31E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.33E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.35E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
95
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
1.37E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.39E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.41E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.43E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.45E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.47E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.49E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.51E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.53E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.55E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.57E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.59E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.61E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.63E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.65E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.67E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.69E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.71E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.73E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.75E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.77E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.79E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.81E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.83E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.85E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.87E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
96
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
1.89E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.91E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.93E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.95E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.97E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.99E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.01E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.03E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.05E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.07E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.09E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.11E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.13E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.15E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.17E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.19E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.21E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.23E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.25E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.27E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.29E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.31E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.33E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.35E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.37E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.39E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
97
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
2.41E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.43E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.45E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.47E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.49E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.51E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.53E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.55E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.57E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.59E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.61E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.63E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.65E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.67E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.69E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.71E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.73E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.75E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.77E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.79E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.81E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.83E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.85E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.87E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.89E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.91E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
98
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
2.93E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.95E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.97E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.01E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.03E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.05E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.07E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.13E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.15E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.17E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.19E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.21E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.23E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.25E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.27E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
3.29E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
3.31E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
3.33E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
3.35E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.37E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.39E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.41E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.43E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.45E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
3.47E+04 5.00E+00 0.00E+00 5.00E+00 0.00E+00 0.00E+00
3.49E+04 5.00E+00 0.00E+00 5.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
99
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
3.51E+04 5.00E+00 0.00E+00 5.00E+00 0.00E+00 0.00E+00
3.53E+04 7.00E+00 0.00E+00 7.00E+00 0.00E+00 0.00E+00
3.55E+04 8.00E+00 0.00E+00 8.00E+00 0.00E+00 0.00E+00
3.57E+04 1.00E+01 0.00E+00 1.00E+01 0.00E+00 0.00E+00
3.59E+04 1.10E+01 0.00E+00 1.10E+01 0.00E+00 0.00E+00
3.61E+04 1.10E+01 0.00E+00 1.10E+01 0.00E+00 0.00E+00
3.63E+04 1.20E+01 0.00E+00 1.20E+01 0.00E+00 0.00E+00
3.65E+04 1.20E+01 0.00E+00 1.20E+01 0.00E+00 0.00E+00
3.67E+04 1.20E+01 0.00E+00 1.20E+01 0.00E+00 0.00E+00
3.69E+04 1.30E+01 0.00E+00 1.30E+01 0.00E+00 0.00E+00
3.71E+04 1.30E+01 0.00E+00 1.30E+01 0.00E+00 0.00E+00
3.73E+04 1.30E+01 0.00E+00 1.30E+01 0.00E+00 0.00E+00
3.75E+04 1.30E+01 0.00E+00 1.30E+01 0.00E+00 0.00E+00
3.77E+04 1.40E+01 0.00E+00 1.40E+01 0.00E+00 0.00E+00
3.79E+04 1.40E+01 0.00E+00 1.40E+01 0.00E+00 0.00E+00
3.81E+04 1.60E+01 0.00E+00 1.60E+01 0.00E+00 0.00E+00
3.83E+04 2.00E+01 0.00E+00 2.00E+01 0.00E+00 0.00E+00
3.85E+04 2.00E+01 0.00E+00 2.00E+01 0.00E+00 0.00E+00
3.87E+04 2.10E+01 0.00E+00 2.10E+01 0.00E+00 0.00E+00
3.89E+04 2.10E+01 0.00E+00 2.10E+01 0.00E+00 0.00E+00
3.91E+04 2.40E+01 0.00E+00 2.40E+01 0.00E+00 0.00E+00
3.93E+04 2.50E+01 0.00E+00 2.50E+01 0.00E+00 0.00E+00
3.95E+04 2.80E+01 0.00E+00 2.80E+01 0.00E+00 0.00E+00
3.97E+04 2.80E+01 0.00E+00 2.80E+01 0.00E+00 0.00E+00
3.99E+04 3.20E+01 0.00E+00 3.20E+01 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
100
APPENDIX C
DATA SET FOR FAILURE TEST 1MPA
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear Stress
6.65E+03 -9.97E+05 2.36E+04 2.15E-04 -2.41E-04 1.11E+01 1.14E+01 -9.97E+05 -4.72E+04 2.36E+04 -1.18E+04
6.85E+03 -1.00E+06 4.63E+04 8.15E-04 -8.51E-04 1.11E+01 1.14E+01 -1.00E+06 -9.26E+04 4.63E+04 -2.31E+04
7.05E+03 -1.01E+06 8.01E+04 1.80E-03 -1.80E-03 1.11E+01 1.14E+01 -1.01E+06 -1.60E+05 8.01E+04 -4.01E+04
7.25E+03 -1.01E+06 1.45E+05 3.17E-03 -3.09E-03 1.11E+01 1.14E+01 -1.01E+06 -2.91E+05 1.45E+05 -7.27E+04
7.65E+03 -1.02E+06 3.00E+05 7.07E-03 -6.65E-03 1.11E+01 1.14E+01 -1.02E+06 -5.99E+05 3.00E+05 -1.50E+05
7.85E+03 -1.03E+06 4.21E+05 9.59E-03 -8.92E-03 1.11E+01 1.14E+01 -1.03E+06 -8.42E+05 4.21E+05 -2.11E+05
8.05E+03 -1.03E+06 5.49E+05 1.25E-02 -1.16E-02 1.11E+01 1.14E+01 -1.03E+06 -1.10E+06 5.49E+05 -2.75E+05
8.25E+03 -1.04E+06 6.84E+05 1.58E-02 -1.45E-02 1.11E+01 1.14E+01 -1.04E+06 -1.37E+06 6.84E+05 -3.42E+05
8.65E+03 -1.05E+06 1.01E+06 2.33E-02 -2.11E-02 1.11E+01 1.14E+01 -1.05E+06 -2.02E+06 1.01E+06 -5.04E+05
8.85E+03 -1.05E+06 1.19E+06 2.72E-02 -2.45E-02 1.11E+01 1.14E+01 -1.05E+06 -2.38E+06 1.19E+06 -5.94E+05
9.05E+03 -1.05E+06 1.37E+06 3.10E-02 -2.79E-02 1.10E+01 1.14E+01 -1.05E+06 -2.74E+06 1.37E+06 -6.86E+05
9.25E+03 -1.05E+06 1.54E+06 3.49E-02 -3.12E-02 1.10E+01 1.14E+01 -1.05E+06 -3.08E+06 1.54E+06 -7.70E+05
9.45E+03 -1.05E+06 1.72E+06 3.87E-02 -3.46E-02 1.10E+01 1.14E+01 -1.05E+06 -3.44E+06 1.72E+06 -8.60E+05
9.65E+03 -1.05E+06 1.91E+06 4.26E-02 -3.79E-02 1.10E+01 1.14E+01 -1.05E+06 -3.82E+06 1.91E+06 -9.54E+05
9.85E+03 -1.05E+06 2.10E+06 4.64E-02 -4.13E-02 1.10E+01 1.14E+01 -1.05E+06 -4.21E+06 2.10E+06 -1.05E+06
1.03E+04 -1.05E+06 2.48E+06 5.42E-02 -4.80E-02 1.10E+01 1.14E+01 -1.05E+06 -4.97E+06 2.48E+06 -1.24E+06
1.05E+04 -1.05E+06 2.68E+06 5.80E-02 -5.14E-02 1.10E+01 1.14E+01 -1.05E+06 -5.37E+06 2.68E+06 -1.34E+06
1.07E+04 -1.05E+06 2.88E+06 6.19E-02 -5.48E-02 1.10E+01 1.14E+01 -1.05E+06 -5.75E+06 2.88E+06 -1.44E+06
1.09E+04 -1.05E+06 3.07E+06 6.57E-02 -5.81E-02 1.09E+01 1.14E+01 -1.05E+06 -6.15E+06 3.07E+06 -1.54E+06
1.11E+04 -1.05E+06 3.27E+06 6.96E-02 -6.15E-02 1.09E+01 1.14E+01 -1.05E+06 -6.54E+06 3.27E+06 -1.63E+06
1.11E+04 -1.05E+06 3.27E+06 6.96E-02 -6.15E-02 1.09E+01 1.14E+01 -1.05E+06 -6.54E+06 3.27E+06 -1.63E+06
Texas Tech University, Stacey J. Amamoo, May 2012
101
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear Stress
1.15E+04 -1.05E+06 3.67E+06 7.73E-02 -6.82E-02 1.09E+01 1.14E+01 -1.05E+06 -7.34E+06 3.67E+06 -1.83E+06
1.17E+04 -1.05E+06 3.87E+06 8.11E-02 -7.15E-02 1.09E+01 1.14E+01 -1.05E+06 -7.75E+06 3.87E+06 -1.94E+06
1.19E+04 -1.05E+06 4.08E+06 8.50E-02 -7.49E-02 1.09E+01 1.14E+01 -1.05E+06 -8.15E+06 4.08E+06 -2.04E+06
1.21E+04 -1.05E+06 4.29E+06 8.88E-02 -7.83E-02 1.09E+01 1.14E+01 -1.05E+06 -8.59E+06 4.29E+06 -2.15E+06
1.23E+04 -1.05E+06 4.50E+06 9.27E-02 -8.16E-02 1.09E+01 1.14E+01 -1.05E+06 -9.00E+06 4.50E+06 -2.25E+06
1.27E+04 -1.05E+06 4.92E+06 1.00E-01 -8.84E-02 1.08E+01 1.14E+01 -1.05E+06 -9.84E+06 4.92E+06 -2.46E+06
1.29E+04 -1.05E+06 5.13E+06 1.04E-01 -9.17E-02 1.08E+01 1.14E+01 -1.05E+06 -1.03E+07 5.13E+06 -2.56E+06
1.31E+04 -1.05E+06 5.35E+06 1.08E-01 -9.51E-02 1.08E+01 1.14E+01 -1.05E+06 -1.07E+07 5.35E+06 -2.67E+06
1.33E+04 -1.05E+06 5.57E+06 1.12E-01 -9.85E-02 1.08E+01 1.14E+01 -1.05E+06 -1.11E+07 5.57E+06 -2.78E+06
1.35E+04 -1.05E+06 5.79E+06 1.16E-01 -1.02E-01 1.08E+01 1.15E+01 -1.05E+06 -1.16E+07 5.79E+06 -2.89E+06
1.37E+04 -1.05E+06 6.01E+06 1.20E-01 -1.05E-01 1.08E+01 1.15E+01 -1.05E+06 -1.20E+07 6.01E+06 -3.01E+06
1.39E+04 -1.05E+06 6.24E+06 1.24E-01 -1.09E-01 1.08E+01 1.15E+01 -1.05E+06 -1.25E+07 6.24E+06 -3.12E+06
1.41E+04 -1.05E+06 6.47E+06 1.27E-01 -1.12E-01 1.08E+01 1.15E+01 -1.05E+06 -1.29E+07 6.47E+06 -3.23E+06
1.45E+04 -1.05E+06 6.93E+06 1.35E-01 -1.19E-01 1.07E+01 1.15E+01 -1.05E+06 -1.39E+07 6.93E+06 -3.47E+06
1.47E+04 -1.05E+06 7.17E+06 1.39E-01 -1.22E-01 1.07E+01 1.15E+01 -1.05E+06 -1.43E+07 7.17E+06 -3.59E+06
1.49E+04 -1.05E+06 7.41E+06 1.43E-01 -1.26E-01 1.07E+01 1.15E+01 -1.05E+06 -1.48E+07 7.41E+06 -3.70E+06
1.51E+04 -1.05E+06 7.65E+06 1.47E-01 -1.29E-01 1.07E+01 1.15E+01 -1.05E+06 -1.53E+07 7.65E+06 -3.82E+06
1.53E+04 -1.05E+06 7.88E+06 1.51E-01 -1.32E-01 1.07E+01 1.15E+01 -1.05E+06 -1.58E+07 7.88E+06 -3.94E+06
1.55E+04 -1.05E+06 8.13E+06 1.54E-01 -1.36E-01 1.07E+01 1.15E+01 -1.05E+06 -1.63E+07 8.13E+06 -4.06E+06
1.57E+04 -1.05E+06 8.37E+06 1.58E-01 -1.39E-01 1.07E+01 1.15E+01 -1.05E+06 -1.67E+07 8.37E+06 -4.19E+06
1.59E+04 -1.05E+06 8.62E+06 1.62E-01 -1.43E-01 1.06E+01 1.15E+01 -1.05E+06 -1.72E+07 8.62E+06 -4.31E+06
1.61E+04 -1.05E+06 8.88E+06 1.66E-01 -1.46E-01 1.06E+01 1.15E+01 -1.05E+06 -1.78E+07 8.88E+06 -4.44E+06
1.63E+04 -1.04E+06 9.13E+06 1.70E-01 -1.49E-01 1.06E+01 1.15E+01 -1.04E+06 -1.83E+07 9.13E+06 -4.57E+06
1.65E+04 -1.05E+06 9.39E+06 1.74E-01 -1.53E-01 1.06E+01 1.15E+01 -1.05E+06 -1.88E+07 9.39E+06 -4.69E+06
1.67E+04 -1.04E+06 9.65E+06 1.78E-01 -1.56E-01 1.06E+01 1.15E+01 -1.04E+06 -1.93E+07 9.65E+06 -4.82E+06
1.69E+04 -1.04E+06 9.91E+06 1.81E-01 -1.60E-01 1.06E+01 1.15E+01 -1.04E+06 -1.98E+07 9.91E+06 -4.95E+06
Texas Tech University, Stacey J. Amamoo, May 2012
102
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear Stress
1.71E+04 -1.05E+06 1.02E+07 1.85E-01 -1.63E-01 1.06E+01 1.15E+01 -1.05E+06 -2.03E+07 1.02E+07 -5.09E+06
1.73E+04 -1.05E+06 1.04E+07 1.89E-01 -1.66E-01 1.06E+01 1.15E+01 -1.05E+06 -2.09E+07 1.04E+07 -5.22E+06
1.75E+04 -1.04E+06 1.07E+07 1.93E-01 -1.70E-01 1.06E+01 1.15E+01 -1.04E+06 -2.14E+07 1.07E+07 -5.35E+06
1.77E+04 -1.05E+06 1.10E+07 1.97E-01 -1.73E-01 1.05E+01 1.15E+01 -1.05E+06 -2.19E+07 1.10E+07 -5.48E+06
1.79E+04 -1.04E+06 1.12E+07 2.01E-01 -1.77E-01 1.05E+01 1.15E+01 -1.04E+06 -2.25E+07 1.12E+07 -5.62E+06
1.81E+04 -1.05E+06 1.15E+07 2.05E-01 -1.80E-01 1.05E+01 1.15E+01 -1.05E+06 -2.30E+07 1.15E+07 -5.75E+06
1.83E+04 -1.05E+06 1.18E+07 2.08E-01 -1.83E-01 1.05E+01 1.15E+01 -1.05E+06 -2.36E+07 1.18E+07 -5.89E+06
1.85E+04 -1.04E+06 1.21E+07 2.12E-01 -1.87E-01 1.05E+01 1.15E+01 -1.04E+06 -2.41E+07 1.21E+07 -6.03E+06
1.87E+04 -1.05E+06 1.23E+07 2.16E-01 -1.90E-01 1.05E+01 1.15E+01 -1.05E+06 -2.47E+07 1.23E+07 -6.17E+06
1.89E+04 -1.04E+06 1.26E+07 2.20E-01 -1.94E-01 1.05E+01 1.15E+01 -1.04E+06 -2.52E+07 1.26E+07 -6.30E+06
1.95E+04 -1.04E+06 1.34E+07 2.32E-01 -2.04E-01 1.04E+01 1.15E+01 -1.04E+06 -2.69E+07 1.34E+07 -6.72E+06
1.97E+04 -1.05E+06 1.37E+07 2.36E-01 -2.07E-01 1.04E+01 1.15E+01 -1.05E+06 -2.74E+07 1.37E+07 -6.86E+06
1.99E+04 -1.05E+06 1.40E+07 2.39E-01 -2.11E-01 1.04E+01 1.15E+01 -1.05E+06 -2.80E+07 1.40E+07 -7.00E+06
2.01E+04 -1.05E+06 1.43E+07 2.43E-01 -2.14E-01 1.04E+01 1.15E+01 -1.05E+06 -2.86E+07 1.43E+07 -7.14E+06
2.03E+04 -1.05E+06 1.46E+07 2.47E-01 -2.18E-01 1.04E+01 1.16E+01 -1.05E+06 -2.91E+07 1.46E+07 -7.28E+06
2.05E+04 -1.05E+06 1.49E+07 2.51E-01 -2.21E-01 1.04E+01 1.16E+01 -1.05E+06 -2.97E+07 1.49E+07 -7.43E+06
2.07E+04 -1.02E+06 1.48E+07 2.51E-01 -2.21E-01 1.04E+01 1.16E+01 -1.02E+06 -2.96E+07 1.48E+07 -7.41E+06
2.09E+04 -1.02E+06 1.48E+07 2.50E-01 -2.20E-01 1.04E+01 1.16E+01 -1.02E+06 -2.96E+07 1.48E+07 -7.39E+06
2.11E+04 -1.00E+06 1.47E+07 2.49E-01 -2.19E-01 1.04E+01 1.16E+01 -1.00E+06 -2.94E+07 1.47E+07 -7.36E+06
2.13E+04 -9.95E+05 1.46E+07 2.48E-01 -2.17E-01 1.04E+01 1.16E+01 -9.95E+05 -2.92E+07 1.46E+07 -7.30E+06
2.15E+04 -9.88E+05 1.45E+07 2.46E-01 -2.16E-01 1.04E+01 1.16E+01 -9.88E+05 -2.89E+07 1.45E+07 -7.24E+06
2.17E+04 -9.83E+05 1.43E+07 2.44E-01 -2.14E-01 1.04E+01 1.16E+01 -9.83E+05 -2.86E+07 1.43E+07 -7.15E+06
2.19E+04 -9.79E+05 1.41E+07 2.41E-01 -2.11E-01 1.04E+01 1.16E+01 -9.79E+05 -2.82E+07 1.41E+07 -7.06E+06
2.21E+04 -9.77E+05 1.39E+07 2.38E-01 -2.09E-01 1.04E+01 1.16E+01 -9.77E+05 -2.78E+07 1.39E+07 -6.94E+06
2.23E+04 -9.74E+05 1.36E+07 2.35E-01 -2.06E-01 1.04E+01 1.16E+01 -9.74E+05 -2.72E+07 1.36E+07 -6.81E+06
2.25E+04 -9.66E+05 1.33E+07 2.31E-01 -2.02E-01 1.04E+01 1.15E+01 -9.66E+05 -2.67E+07 1.33E+07 -6.67E+06
Texas Tech University, Stacey J. Amamoo, May 2012
103
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear Stress
2.27E+04 -9.62E+05 1.31E+07 2.28E-01 -1.99E-01 1.05E+01 1.15E+01 -9.62E+05 -2.61E+07 1.31E+07 -6.53E+06
2.29E+04 -9.61E+05 1.28E+07 2.24E-01 -1.95E-01 1.05E+01 1.15E+01 -9.61E+05 -2.55E+07 1.28E+07 -6.38E+06
2.31E+04 -9.61E+05 1.25E+07 2.20E-01 -1.92E-01 1.05E+01 1.15E+01 -9.61E+05 -2.50E+07 1.25E+07 -6.24E+06
2.33E+04 -9.61E+05 1.22E+07 2.16E-01 -1.88E-01 1.05E+01 1.15E+01 -9.61E+05 -2.44E+07 1.22E+07 -6.09E+06
2.35E+04 -9.62E+05 1.19E+07 2.12E-01 -1.85E-01 1.05E+01 1.15E+01 -9.62E+05 -2.38E+07 1.19E+07 -5.95E+06
2.37E+04 -9.62E+05 1.16E+07 2.08E-01 -1.81E-01 1.05E+01 1.15E+01 -9.62E+05 -2.32E+07 1.16E+07 -5.81E+06
2.39E+04 -9.59E+05 1.13E+07 2.04E-01 -1.78E-01 1.05E+01 1.15E+01 -9.59E+05 -2.27E+07 1.13E+07 -5.67E+06
2.41E+04 -9.60E+05 1.11E+07 2.01E-01 -1.74E-01 1.05E+01 1.15E+01 -9.60E+05 -2.21E+07 1.11E+07 -5.53E+06
2.43E+04 -9.61E+05 1.08E+07 1.97E-01 -1.71E-01 1.05E+01 1.15E+01 -9.61E+05 -2.16E+07 1.08E+07 -5.39E+06
2.45E+04 -9.59E+05 1.05E+07 1.93E-01 -1.67E-01 1.06E+01 1.15E+01 -9.59E+05 -2.10E+07 1.05E+07 -5.25E+06
2.47E+04 -9.60E+05 1.02E+07 1.89E-01 -1.64E-01 1.06E+01 1.15E+01 -9.60E+05 -2.05E+07 1.02E+07 -5.12E+06
2.49E+04 -9.57E+05 9.97E+06 1.85E-01 -1.61E-01 1.06E+01 1.15E+01 -9.57E+05 -1.99E+07 9.97E+06 -4.99E+06
2.51E+04 -9.83E+05 9.84E+06 1.83E-01 -1.59E-01 1.06E+01 1.15E+01 -9.83E+05 -1.97E+07 9.84E+06 -4.92E+06
2.53E+04 -9.83E+05 9.88E+06 1.84E-01 -1.60E-01 1.06E+01 1.15E+01 -9.83E+05 -1.98E+07 9.88E+06 -4.94E+06
2.55E+04 -9.98E+05 9.92E+06 1.84E-01 -1.60E-01 1.06E+01 1.15E+01 -9.98E+05 -1.98E+07 9.92E+06 -4.96E+06
2.57E+04 -1.00E+06 1.00E+07 1.86E-01 -1.62E-01 1.06E+01 1.15E+01 -1.00E+06 -2.00E+07 1.00E+07 -5.00E+06
2.59E+04 -1.01E+06 1.01E+07 1.87E-01 -1.63E-01 1.06E+01 1.15E+01 -1.01E+06 -2.02E+07 1.01E+07 -5.06E+06
2.61E+04 -1.01E+06 1.03E+07 1.89E-01 -1.65E-01 1.06E+01 1.15E+01 -1.01E+06 -2.05E+07 1.03E+07 -5.13E+06
2.63E+04 -1.02E+06 1.04E+07 1.91E-01 -1.67E-01 1.06E+01 1.15E+01 -1.02E+06 -2.08E+07 1.04E+07 -5.21E+06
2.65E+04 -1.02E+06 1.06E+07 1.94E-01 -1.70E-01 1.06E+01 1.15E+01 -1.02E+06 -2.12E+07 1.06E+07 -5.31E+06
2.67E+04 -1.03E+06 1.08E+07 1.97E-01 -1.72E-01 1.05E+01 1.15E+01 -1.03E+06 -2.17E+07 1.08E+07 -5.42E+06
2.69E+04 -1.03E+06 1.11E+07 2.01E-01 -1.76E-01 1.05E+01 1.15E+01 -1.03E+06 -2.22E+07 1.11E+07 -5.55E+06
2.71E+04 -1.03E+06 1.14E+07 2.05E-01 -1.79E-01 1.05E+01 1.15E+01 -1.03E+06 -2.27E+07 1.14E+07 -5.68E+06
2.73E+04 -1.04E+06 1.17E+07 2.08E-01 -1.83E-01 1.05E+01 1.15E+01 -1.04E+06 -2.33E+07 1.17E+07 -5.83E+06
2.75E+04 -1.04E+06 1.19E+07 2.12E-01 -1.86E-01 1.05E+01 1.15E+01 -1.04E+06 -2.39E+07 1.19E+07 -5.97E+06
2.77E+04 -1.04E+06 1.22E+07 2.16E-01 -1.90E-01 1.05E+01 1.15E+01 -1.04E+06 -2.44E+07 1.22E+07 -6.11E+06
Texas Tech University, Stacey J. Amamoo, May 2012
104
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear Stress
2.79E+04 -1.04E+06 1.25E+07 2.20E-01 -1.93E-01 1.05E+01 1.15E+01 -1.04E+06 -2.50E+07 1.25E+07 -6.26E+06
2.81E+04 -1.04E+06 1.28E+07 2.24E-01 -1.97E-01 1.05E+01 1.15E+01 -1.04E+06 -2.56E+07 1.28E+07 -6.40E+06
2.83E+04 -1.04E+06 1.31E+07 2.28E-01 -2.00E-01 1.05E+01 1.15E+01 -1.04E+06 -2.62E+07 1.31E+07 -6.54E+06
2.85E+04 -1.04E+06 1.34E+07 2.32E-01 -2.04E-01 1.04E+01 1.15E+01 -1.04E+06 -2.68E+07 1.34E+07 -6.69E+06
2.87E+04 -1.04E+06 1.37E+07 2.36E-01 -2.07E-01 1.04E+01 1.15E+01 -1.04E+06 -2.73E+07 1.37E+07 -6.84E+06
2.89E+04 -1.04E+06 1.40E+07 2.39E-01 -2.11E-01 1.04E+01 1.15E+01 -1.04E+06 -2.79E+07 1.40E+07 -6.98E+06
2.91E+04 -1.04E+06 1.42E+07 2.43E-01 -2.14E-01 1.04E+01 1.15E+01 -1.04E+06 -2.85E+07 1.42E+07 -7.12E+06
2.93E+04 -1.04E+06 1.45E+07 2.47E-01 -2.17E-01 1.04E+01 1.16E+01 -1.04E+06 -2.91E+07 1.45E+07 -7.27E+06
2.95E+04 -1.04E+06 1.48E+07 2.51E-01 -2.21E-01 1.04E+01 1.16E+01 -1.04E+06 -2.97E+07 1.48E+07 -7.42E+06
2.97E+04 -1.04E+06 1.51E+07 2.55E-01 -2.24E-01 1.04E+01 1.16E+01 -1.04E+06 -3.03E+07 1.51E+07 -7.57E+06
2.99E+04 -1.05E+06 1.54E+07 2.59E-01 -2.28E-01 1.04E+01 1.16E+01 -1.05E+06 -3.08E+07 1.54E+07 -7.71E+06
3.01E+04 -1.05E+06 1.57E+07 2.63E-01 -2.31E-01 1.03E+01 1.16E+01 -1.05E+06 -3.14E+07 1.57E+07 -7.85E+06
3.03E+04 -1.05E+06 1.60E+07 2.66E-01 -2.35E-01 1.03E+01 1.16E+01 -1.05E+06 -3.20E+07 1.60E+07 -7.99E+06
3.05E+04 -1.05E+06 1.63E+07 2.70E-01 -2.38E-01 1.03E+01 1.16E+01 -1.05E+06 -3.26E+07 1.63E+07 -8.14E+06
3.07E+04 -1.05E+06 1.66E+07 2.74E-01 -2.41E-01 1.03E+01 1.16E+01 -1.05E+06 -3.31E+07 1.66E+07 -8.29E+06
3.09E+04 -1.05E+06 1.69E+07 2.78E-01 -2.45E-01 1.03E+01 1.16E+01 -1.05E+06 -3.37E+07 1.69E+07 -8.43E+06
3.11E+04 -1.05E+06 1.72E+07 2.82E-01 -2.48E-01 1.03E+01 1.16E+01 -1.05E+06 -3.43E+07 1.72E+07 -8.58E+06
3.13E+04 -1.05E+06 1.75E+07 2.86E-01 -2.52E-01 1.03E+01 1.16E+01 -1.05E+06 -3.49E+07 1.75E+07 -8.73E+06
3.19E+04 -1.04E+06 1.84E+07 2.97E-01 -2.62E-01 1.02E+01 1.16E+01 -1.04E+06 -3.67E+07 1.84E+07 -9.18E+06
3.21E+04 -1.04E+06 1.87E+07 3.01E-01 -2.65E-01 1.02E+01 1.16E+01 -1.04E+06 -3.74E+07 1.87E+07 -9.34E+06
3.23E+04 -1.05E+06 1.90E+07 3.05E-01 -2.69E-01 1.02E+01 1.16E+01 -1.05E+06 -3.79E+07 1.90E+07 -9.48E+06
3.25E+04 -1.05E+06 1.93E+07 3.09E-01 -2.72E-01 1.02E+01 1.16E+01 -1.05E+06 -3.86E+07 1.93E+07 -9.64E+06
3.27E+04 -1.05E+06 1.96E+07 3.13E-01 -2.75E-01 1.02E+01 1.16E+01 -1.05E+06 -3.92E+07 1.96E+07 -9.79E+06
3.29E+04 -1.05E+06 1.99E+07 3.17E-01 -2.79E-01 1.02E+01 1.16E+01 -1.05E+06 -3.98E+07 1.99E+07 -9.94E+06
3.31E+04 -1.05E+06 2.02E+07 3.21E-01 -2.82E-01 1.02E+01 1.16E+01 -1.05E+06 -4.04E+07 2.02E+07 -1.01E+07
3.33E+04 -1.06E+06 2.05E+07 3.25E-01 -2.85E-01 1.02E+01 1.16E+01 -1.06E+06 -4.10E+07 2.05E+07 -1.03E+07
Texas Tech University, Stacey J. Amamoo, May 2012
105
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear Stress
3.35E+04 -1.05E+06 2.08E+07 3.28E-01 -2.89E-01 1.02E+01 1.16E+01 -1.05E+06 -4.16E+07 2.08E+07 -1.04E+07
3.37E+04 -1.05E+06 2.11E+07 3.32E-01 -2.92E-01 1.01E+01 1.16E+01 -1.05E+06 -4.22E+07 2.11E+07 -1.06E+07
3.39E+04 -1.06E+06 2.14E+07 3.36E-01 -2.95E-01 1.01E+01 1.16E+01 -1.06E+06 -4.29E+07 2.14E+07 -1.07E+07
3.41E+04 -1.05E+06 2.18E+07 3.40E-01 -2.99E-01 1.01E+01 1.16E+01 -1.05E+06 -4.35E+07 2.18E+07 -1.09E+07
3.43E+04 -1.05E+06 2.21E+07 3.44E-01 -3.02E-01 1.01E+01 1.16E+01 -1.05E+06 -4.41E+07 2.21E+07 -1.10E+07
3.45E+04 -1.05E+06 2.24E+07 3.48E-01 -3.05E-01 1.01E+01 1.16E+01 -1.05E+06 -4.48E+07 2.24E+07 -1.12E+07
3.47E+04 -1.05E+06 2.27E+07 3.52E-01 -3.09E-01 1.01E+01 1.16E+01 -1.05E+06 -4.54E+07 2.27E+07 -1.14E+07
3.49E+04 -1.05E+06 2.30E+07 3.56E-01 -3.12E-01 1.01E+01 1.16E+01 -1.05E+06 -4.61E+07 2.30E+07 -1.15E+07
3.51E+04 -1.05E+06 2.34E+07 3.59E-01 -3.16E-01 1.01E+01 1.16E+01 -1.05E+06 -4.67E+07 2.34E+07 -1.17E+07
3.53E+04 -1.05E+06 2.37E+07 3.63E-01 -3.19E-01 1.00E+01 1.16E+01 -1.05E+06 -4.73E+07 2.37E+07 -1.18E+07
3.55E+04 -1.06E+06 2.40E+07 3.67E-01 -3.22E-01 1.00E+01 1.17E+01 -1.06E+06 -4.80E+07 2.40E+07 -1.20E+07
3.57E+04 -1.06E+06 2.43E+07 3.71E-01 -3.26E-01 1.00E+01 1.17E+01 -1.06E+06 -4.86E+07 2.43E+07 -1.22E+07
3.59E+04 -1.06E+06 2.47E+07 3.75E-01 -3.29E-01 1.00E+01 1.17E+01 -1.06E+06 -4.93E+07 2.47E+07 -1.23E+07
3.61E+04 -1.06E+06 2.49E+07 3.79E-01 -3.32E-01 1.00E+01 1.17E+01 -1.06E+06 -4.99E+07 2.49E+07 -1.25E+07
3.63E+04 -1.06E+06 2.53E+07 3.83E-01 -3.36E-01 9.99E+00 1.17E+01 -1.06E+06 -5.05E+07 2.53E+07 -1.26E+07
3.65E+04 -1.06E+06 2.56E+07 3.87E-01 -3.39E-01 9.98E+00 1.17E+01 -1.06E+06 -5.12E+07 2.56E+07 -1.28E+07
3.67E+04 -1.06E+06 2.59E+07 3.90E-01 -3.42E-01 9.96E+00 1.17E+01 -1.06E+06 -5.18E+07 2.59E+07 -1.30E+07
3.69E+04 -1.06E+06 2.62E+07 3.94E-01 -3.45E-01 9.95E+00 1.17E+01 -1.06E+06 -5.24E+07 2.62E+07 -1.31E+07
3.71E+04 -1.05E+06 2.65E+07 3.98E-01 -3.49E-01 9.94E+00 1.17E+01 -1.05E+06 -5.31E+07 2.65E+07 -1.33E+07
3.73E+04 -1.06E+06 2.69E+07 4.02E-01 -3.52E-01 9.93E+00 1.17E+01 -1.06E+06 -5.37E+07 2.69E+07 -1.34E+07
3.75E+04 -1.06E+06 2.72E+07 4.06E-01 -3.56E-01 9.92E+00 1.17E+01 -1.06E+06 -5.44E+07 2.72E+07 -1.36E+07
3.77E+04 -1.06E+06 2.75E+07 4.10E-01 -3.59E-01 9.91E+00 1.17E+01 -1.06E+06 -5.51E+07 2.75E+07 -1.38E+07
3.79E+04 -1.06E+06 2.79E+07 4.14E-01 -3.62E-01 9.89E+00 1.17E+01 -1.06E+06 -5.57E+07 2.79E+07 -1.39E+07
3.81E+04 -1.06E+06 2.82E+07 4.18E-01 -3.66E-01 9.88E+00 1.17E+01 -1.06E+06 -5.64E+07 2.82E+07 -1.41E+07
3.83E+04 -1.06E+06 2.86E+07 4.21E-01 -3.69E-01 9.87E+00 1.17E+01 -1.06E+06 -5.71E+07 2.86E+07 -1.43E+07
3.85E+04 -1.06E+06 2.89E+07 4.25E-01 -3.72E-01 9.86E+00 1.17E+01 -1.06E+06 -5.78E+07 2.89E+07 -1.44E+07
Texas Tech University, Stacey J. Amamoo, May 2012
106
Step Confining
Stress Deviatoric
Stress Axial
Strain Volumetric
Strain Distance
x Distance
y Normal
Stress Hoop
Stress Radial
Stress Shear Stress
3.87E+04 -1.06E+06 2.92E+07 4.29E-01 -3.75E-01 9.85E+00 1.17E+01 -1.06E+06 -5.85E+07 2.92E+07 -1.46E+07
3.89E+04 -1.06E+06 2.96E+07 4.33E-01 -3.79E-01 9.84E+00 1.17E+01 -1.06E+06 -5.92E+07 2.96E+07 -1.48E+07
3.91E+04 -1.06E+06 2.99E+07 4.37E-01 -3.82E-01 9.82E+00 1.17E+01 -1.06E+06 -5.99E+07 2.99E+07 -1.50E+07
3.93E+04 -1.07E+06 3.03E+07 4.41E-01 -3.85E-01 9.81E+00 1.17E+01 -1.07E+06 -6.06E+07 3.03E+07 -1.51E+07
3.95E+04 -1.07E+06 3.06E+07 4.45E-01 -3.88E-01 9.80E+00 1.17E+01 -1.07E+06 -6.12E+07 3.06E+07 -1.53E+07
3.97E+04 -1.07E+06 3.10E+07 4.49E-01 -3.92E-01 9.79E+00 1.17E+01 -1.07E+06 -6.19E+07 3.10E+07 -1.55E+07
3.99E+04 -1.07E+06 3.13E+07 4.53E-01 -3.95E-01 9.78E+00 1.17E+01 -1.07E+06 -6.26E+07 3.13E+07 -1.56E+07
4.01E+04 -1.07E+06 3.16E+07 4.56E-01 -3.98E-01 9.77E+00 1.17E+01 -1.07E+06 -6.33E+07 3.16E+07 -1.58E+07
4.03E+04 -1.07E+06 3.20E+07 4.60E-01 -4.01E-01 9.75E+00 1.17E+01 -1.07E+06 -6.39E+07 3.20E+07 -1.60E+07
4.05E+04 -1.07E+06 3.24E+07 4.64E-01 -4.05E-01 9.74E+00 1.17E+01 -1.07E+06 -6.48E+07 3.24E+07 -1.62E+07
4.07E+04 -1.08E+06 3.27E+07 4.68E-01 -4.08E-01 9.73E+00 1.18E+01 -1.08E+06 -6.53E+07 3.27E+07 -1.63E+07
4.09E+04 -1.09E+06 3.30E+07 4.72E-01 -4.11E-01 9.72E+00 1.18E+01 -1.09E+06 -6.60E+07 3.30E+07 -1.65E+07
4.11E+04 -1.08E+06 3.34E+07 4.76E-01 -4.14E-01 9.71E+00 1.18E+01 -1.08E+06 -6.68E+07 3.34E+07 -1.67E+07
4.13E+04 -1.13E+06 3.37E+07 4.80E-01 -4.17E-01 9.70E+00 1.18E+01 -1.13E+06 -6.74E+07 3.37E+07 -1.68E+07
4.15E+04 -1.11E+06 3.40E+07 4.84E-01 -4.19E-01 9.68E+00 1.18E+01 -1.11E+06 -6.80E+07 3.40E+07 -1.70E+07
4.17E+04 -1.08E+06 3.44E+07 4.88E-01 -4.22E-01 9.67E+00 1.18E+01 -1.08E+06 -6.88E+07 3.44E+07 -1.72E+07
4.19E+04 -1.09E+06 3.47E+07 4.91E-01 -4.25E-01 9.66E+00 1.18E+01 -1.09E+06 -6.94E+07 3.47E+07 -1.74E+07
4.21E+04 -1.08E+06 3.50E+07 4.95E-01 -4.28E-01 9.65E+00 1.18E+01 -1.08E+06 -7.00E+07 3.50E+07 -1.75E+07
4.23E+04 -1.07E+06 3.54E+07 4.99E-01 -4.32E-01 9.64E+00 1.18E+01 -1.07E+06 -7.08E+07 3.54E+07 -1.77E+07
4.25E+04 -1.08E+06 3.57E+07 5.03E-01 -4.35E-01 9.63E+00 1.18E+01 -1.08E+06 -7.14E+07 3.57E+07 -1.79E+07
4.27E+04 -1.10E+06 3.60E+07 5.07E-01 -4.38E-01 9.61E+00 1.18E+01 -1.10E+06 -7.20E+07 3.60E+07 -1.80E+07
4.29E+04 -1.11E+06 3.61E+07 5.11E-01 -4.41E-01 9.60E+00 1.18E+01 -1.11E+06 -7.22E+07 3.61E+07 -1.80E+07
Texas Tech University, Stacey J. Amamoo, May 2012
107
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
6.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
6.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
7.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
8.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
8.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
8.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
8.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
8.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.05E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.25E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.45E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.65E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
9.85E+03 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.01E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.03E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.05E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.07E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.09E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.11E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.13E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.15E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
108
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
1.17E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.19E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.21E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.23E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.25E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.27E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.29E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.31E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.33E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.35E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.37E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.39E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.41E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.43E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.45E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.47E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.49E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.51E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.53E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.55E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.57E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.59E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.61E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.63E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.65E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.67E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
109
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
1.69E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.71E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.73E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.75E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.77E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.79E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.81E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.83E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.85E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.87E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.89E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.91E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.93E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.95E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.97E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
1.99E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.01E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.03E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.05E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.07E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.09E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.11E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.13E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.15E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.17E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.19E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
110
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
2.21E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.23E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.25E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.27E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.29E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.31E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.33E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.35E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.37E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.39E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.41E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.43E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.45E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.47E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.49E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.51E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.53E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.55E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.57E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.59E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.61E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.63E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.65E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.67E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.69E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.71E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
111
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
2.73E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.75E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.77E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.79E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.81E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.83E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.85E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.87E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.89E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.91E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.93E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.95E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.97E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
2.99E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.01E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.03E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.05E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.07E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.09E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.11E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.13E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.15E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.17E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.19E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.21E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.23E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
112
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
3.25E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.27E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.29E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.31E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.33E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.35E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.37E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.39E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.41E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.43E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.45E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.47E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.49E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.51E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.53E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.55E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.57E+04 0.00E+00 0.00E+00 0.00E+00 0.00E+00 0.00E+00
3.59E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
3.61E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
3.63E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
3.65E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
3.67E+04 1.00E+00 0.00E+00 1.00E+00 0.00E+00 0.00E+00
3.69E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.71E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.73E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.75E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
Texas Tech University, Stacey J. Amamoo, May 2012
113
Step # Microcracks # Microcracks(CNF) # Microcracks(CSF) # Microcracks(PNF) # Microcracks(PSF)
3.79E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.81E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.83E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.85E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.87E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.89E+04 2.00E+00 0.00E+00 2.00E+00 0.00E+00 0.00E+00
3.91E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
3.93E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
3.95E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
3.99E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
4.01E+04 3.00E+00 0.00E+00 3.00E+00 0.00E+00 0.00E+00
4.03E+04 4.00E+00 0.00E+00 4.00E+00 0.00E+00 0.00E+00
4.05E+04 4.00E+00 0.00E+00 4.00E+00 0.00E+00 0.00E+00
4.07E+04 4.00E+00 0.00E+00 4.00E+00 0.00E+00 0.00E+00
4.09E+04 4.00E+00 0.00E+00 4.00E+00 0.00E+00 0.00E+00
4.11E+04 5.00E+00 0.00E+00 5.00E+00 0.00E+00 0.00E+00
4.13E+04 5.00E+00 0.00E+00 5.00E+00 0.00E+00 0.00E+00
4.15E+04 5.00E+00 0.00E+00 5.00E+00 0.00E+00 0.00E+00
4.17E+04 6.00E+00 0.00E+00 6.00E+00 0.00E+00 0.00E+00
4.19E+04 6.00E+00 0.00E+00 6.00E+00 0.00E+00 0.00E+00
4.21E+04 7.00E+00 0.00E+00 7.00E+00 0.00E+00 0.00E+00
4.23E+04 7.00E+00 0.00E+00 7.00E+00 0.00E+00 0.00E+00
4.25E+04 9.00E+00 1.00E+00 8.00E+00 0.00E+00 0.00E+00
4.27E+04 1.00E+01 2.00E+00 8.00E+00 0.00E+00 0.00E+00
4.29E+04 1.20E+01 4.00E+00 8.00E+00 0.00E+00 0.00E+00