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    The thesis of Pichit Vardcharragosad was reviewed and approved* by the following:

    Luis F. AyalaAssociate Professor of Petroleum and Natural Gas EngineeringThesis Advisor

    R. Larry GraysonProfessor of Energy and Mineral EngineeringGraduate Program Officer of Energy and Mineral Engineering

    Li LiAssistant Professor of Energy and Mineral Engineering

    Yaw D. YeboahProfessor of Energy and Mineral EngineeringHead of the Department of Energy and Mineral Engineering

    *Signatures are on file in the Graduate School

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    iv

    condensate tank model for the case volatile oil reservoirs are addressed. Further recommended

    studies on negative value of decline exponent variable and expanding current capability of the

    proposed model are also presented.

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    v

    TABLE OF CONTENTS

    List of Figures .......................................................................................................................... viiList of Tables ........................................................................................................................... ixNomenclature ........................................................................................................................... xAcknowledgements .................................................................................................................. xvChapter 1 Introduction ............................................................................................................. 1Chapter 2 Background ............................................................................................................. 3

    2.1 Gas Condensate Hydrocarbon Fluid .......................................................................... 32.2 Modified Black-Oil Model ......................................................................................... 52.3 Zero-Dimensional Reservoir Model .......................................................................... 72.4 Field Performance Prediction ..................................................................................... 82.5 Visual Basic for Applications (VBA) ........................................................................ 12

    Chapter 3 Problem Statement .................................................................................................. 13Chapter 4 Model Description ................................................................................................... 15

    4.1 Phase Behavior Model (PBM) ................................................................................... 164.1.1 Compressibility Factor .................................................................................... 174.1.2 Vapor-Liquid Equilibrium ............................................................................... 214.1.3 Fluid Property Prediction ................................................................................ 274.1.4 Phase Stability Analysis .................................................................................. 37

    4.2 Standard PVT Properties ............................................................................................ 424.2.1 Definitions, Mathematic Relationships, and Characteristics ........................... 434.2.2 Obtaining Standard PVT Properties from Laboratory PVT Reports ............... 514.2.3 Obtaining Standard PVT Properties from a Phase Behavior Model ............... 60

    4.3 Zero-Dimensional Reservoir Model .......................................................................... 704.3.1 Generalized Material Balance Equation .......................................................... 714.3.2 Material Balance Equation for a Gas Condensate Fluid ................................. 754.3.3 Phase Saturation Calculations ......................................................................... 804.3.4 Volumetric OGIP/OOIP Calculations ............................................................. 82

    4.4 Flow Rates and Flowing Pressures Calculation ......................................................... 844.4.1 Inflow Performance Relationship (IPR) .......................................................... 854.4.2 Tubing Performance Relationships ................................................................. 914.4.3 Nodal Analysis ................................................................................................ 96

    4.5 Field Performance Prediction ..................................................................................... 994.5.1 Performance during Plateau Period ................................................................. 1004.5.2 Performance during Decline Period ................................................................ 1034.5.3 Annual Production Calculation ....................................................................... 106

    4.6 Economic Analysis and Field Optimization............................................................... 1094.6.1 Simplified Economic Model ........................................................................... 1104.6.2 Field Optimization ........................................................................................... 116

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    vii

    LIST OF FIGURES

    Figure 2-1: Phase Diagram of Typical Gas Condensate Reservoir .......................................... 3Figure 2-2: Distributions of Pseudo Components among Phases in Modified Black-Oil

    Model ............................................................................................................................... 5Figure 2-3: Graphical Representation of Zero-Dimensional Reservoir Model ........................ 7Figure 2-4: Typical Field Performance of Gas Condensate Gas and Oil Flow Rates vs.

    Time ................................................................................................................................. 9Figure 2-5: Typical Field Performance of Gas CondensateReservoir Pressure,

    Bottomhole Flowing Pressure and Wellhead Pressure vs. Time ..................................... 10Figure 2-6: Typical Field Performance of Gas Condensate Cumulative Gas and Oil

    Production vs. Time ......................................................................................................... 11Figure 4-1: Graphical Representation of Standard PVT Properties ......................................... 44Figure 4-2: Typical Characteristic of Gas Formation Volume Factor () and Volatilized

    Oil-Gas Ratio () for Gas Condensate .......................................................................... 48Figure 4-3: Typical Characteristic of Oil Formation Volume Factor () and Solution

    Gas-Oil Ratio () for Gas Condensate ........................................................................... 48Figure 4-4: Graphical Representation of CVD Data used in Walsh-Towler Algorithm .......... 53Figure 4-5: Graphical Representation of Nodal Analysis ........................................................ 96

    Figure 4-6: Graphical Representation of Field Optimization .................................................. 116Figure 5-1: Simulated Gas Formation Volume Factor and Volatilized Oil-Gas Ratio of

    Gas Condensate ................................................................................................................ 118Figure 5-2: Simulated Oil Formation Volume Factor and Solution Gas-Oil Ratio of Gas

    Condensate ....................................................................................................................... 119Figure 5-3: Simulated Specific Gravity of Reservoir Gas ....................................................... 120Figure 5-4: Volumes of Surface Gas Pseudo Component in Reservoir Gas Reservoir Oil,

    and Cumulative Gas Production ....................................................................................... 121Figure 5-5: Volumes of Stock-Tank Oil Pseudo Component in Reservoir Gas, Reservoir

    Oil, and Cumulative Oil Production................................................................................. 122Figure 5-6: Densities of Surface Gas and Stock-Tank Oil Pseudo Components at First

    Stage Separator, Second Stage Separator and Stock Tank Condition .............................. 124

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    Figure 5-7: Volumes of Stock-Tank Oil Pseudo Component in Reservoir Gas, ReservoirOil, and Cumulative Oil Production in term of Gas-Equivalent ...................................... 125

    Figure 5-8: Total Volumes of Stock-Tank Oil Pseudo Component and Surface Gas

    Pseudo Component in term of Gas-Equivalent ................................................................ 126Figure 5-9: Simulated Production Results of Gas Condensate using Simplified Gas

    Condensate Tank Model .................................................................................................. 130Figure 5-10: Phase Envelope and Reservoir Depletion Paths at Two Different Reservoir

    Temperatures .................................................................................................................... 133Figure 5-11: Simulated Gas Formation Volume Factor and Volatilized Oil-Gas Ratio of

    Volatile Oil using Gas Condensate PVT Model .............................................................. 134Figure 5-12: Simulated Oil Formation Volume Factor and Solution Gas-Oil Ratio of

    Volatile Oil using Gas Condensate PVT Model .............................................................. 134Figure 5-13: Simulated Production Results of Volatile Oil using Simplified Gas

    Condensate Tank Model .................................................................................................. 135Figure 5-14: Mole Fraction Behavior of Vapor Phase Molar Fraction ( ) for Gas

    Condensates and Volatile Oils ......................................................................................... 136Figure 5-15: Cumulative Gas and Oil Production vs. Time..................................................... 138Figure 5-16: Total Gas and Oil Flow Rates vs. Time .............................................................. 139Figure 5-17: Reservoir Pressure, Bottomhole Flowing Pressure, and Wellhead Pressure

    vs. Time ............................................................................................................................ 140Figure 5-18: Gas Saturation and Specific Gravity of Reservoir Gas vs. Time ........................ 142Figure 5-19: Total Gas Flow Rate () vs. Cumulative Gas Production during Decline

    Period .................................................................................................. 143Figure 5-20: Decline Rate () vs. Cumulative Gas Production during Decline Period

    () ........................................................................................................... 145Figure 5-21: Annual Expenditure, Annual Total Revenue, and Cumulative Discounted

    Net Cash Flow vs. Production Time ................................................................................ 147Figure 5-22: Net Present Value vs. Interest Rate ..................................................................... 148Figure 5-23: Field Optimization Results .................................................................................. 149

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    ix

    LIST OF TABLES

    Table 4-1: Volume-Translation Coefficients for Pure Components (Whitson and Brule,2000) ................................................................................................................................ 31

    Table A-1: Pressures and Temperatures for Standard PVT Properties CalculationSubroutine ........................................................................................................................ 163

    Table A-2: Physical Properties of Pure Components ............................................................... 163Table A-3: Binary Interaction Coefficients of Pure Components ............................................ 164Table A-4: Volume Translation Coefficient of Pure Components .......................................... 164Table A-5: Reservoir Input Data .............................................................................................. 165Table A-6: Relative Permeability Input Data .......................................................................... 165Table A-7: Standard PVT Properties ....................................................................................... 166Table A-7: Standard PVT Properties (Cont.) ........................................................................... 167Table A-8: Tubing Input Data .................................................................................................. 168Table A-9: Economic Input Data ............................................................................................. 168Table A-9: Economic Input Data (Cont.)................................................................................. 169Table A-10: Field Performance Prediction Input ..................................................................... 169Table A-11: Field Performance Optimization Input ................................................................ 169

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    x

    NOMENCLATURE

    Normal Symbol Definition

    Reservoir drainage area Hyperbolic decline exponent Co-volume parameter of i-th component Formation volume factor Gas formation volume factor Oil formation volume factor Two-phase gas formation volume factor Two-phase oil formation volume factor Overall molar faction of i-th component Formation (rock) compressibility

    Deitz shape factor

    Non-Darcy coefficient / Tubing Diameter Decline rate Expansivity of formation (rock) Expansivity of reservoir gas Expansivity of reservoir oil Expansivity of reservoir water Efficiency factor of tubing Fannings friction factor Fugacity of i-th component in vapor phase Fugacity of i-th component in liquid phase

    Moodys friction factor

    Molar fraction of vapor phase

    Molar fraction of liquid phase at reservoir condition Molar fraction of liquid phase Molar fraction of liquid phase at first-stage separator Molar fraction of liquid phase at first-stage separator produced fromreservoir gas Molar fraction of liquid phase at first-stage separator produced fromreservoir oil Molar fraction of liquid phase at second-stage separator Molar fraction of liquid phase at second-stage separator produced fromreservoir gas

    Molar fraction of liquid phase at second-stage separator produced fromreservoir oil Molar fraction of liquid phase at stock-tank condition Molar fraction of liquid phase at stock-tank condition produced fromreservoir gas Molar fraction of liquid phase at stock-tank condition produced fromreservoir oil Fugacity of i-th component in original fluid

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    Fugacity of i-th component in liquid-like phase Fugacity of i-th component in vapor-like phase

    Amount of surface gas pseudo component / Gas in place

    Amount of gas-equivalent pseudo component Amount of surface gas pseudo component in reservoir gas phase Amount of surface gas pseudo component in reservoir oil phase Amount of cumulative gas injection Amount of cumulative gas production Cumulative gas production at year Cumulative gas production at abandonment condition Cumulative gas production at end of plateau Cumulative gas recovery Incremental of cumulative gas production

    Annual gas production at year

    Incremental of gas recovery

    Reservoir thickness Elevation of upstream node Elevation of downstream node Difference in elevation of downstream and upstream node Absolute permeability of reservoir Effective permeability of reservoir gas Relative permeability of reservoir gas Relative permeability of reservoir oil Volatility ratio of i-th component Tubing length

    Temperature dependency coefficient of i-th component

    Molecular weight of vapor phase Molecular weight of gas at reservoir condition Molecular weight of i-th component Molecular weight of oil at reservoir condition Molecular weight of oil at stock-tank condition Molecular weight of oil at stock-tank condition produced from reservoirgas Molecular weight of oil at stock-tank condition produced from reservoiroil Molecular weight of liquid phase

    Molecular weight of remaining fluid inside PVT cell

    Number of component in multi-component hydrocarbon

    Mole fraction of excess gas removed from PVT cell Mole fraction of remaining gas inside PVT cell Mole fraction of remaining gas inside PVT cell plus excess gas Mole fraction of remaining oil inside PVT cell Mole fraction of remaining fluid inside PVT cell Amount of stock-tank oil pseudo component / Oil in place Amount of stock-tank oil pseudo component in reservoir gas phase Amount of stock-tank oil pseudo component in reservoir oil phase

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    Amount of cumulative oil production Cumulative oil production at year

    Cumulative oil production at abandonment condition

    Cumulative oil recovery

    Reynolds number Incremental of cumulative oil production Annual oil production at year Incremental of oil recovery Original gas in place Original oil in place Pressure Upstream pressure Downstream pressure Average pressure between upstream and downstream

    Critical pressure of i-th component

    Drawdown pressure inside the reservoir

    Pseudocritical pressure Reservoir pressure Reservoir pressure at abandonment condition Reservoir pressure at end of plateau Reduced pressure of i-th component Pressure at standard condition Bottomhole flowing pressure Bottomhole flowing pressure at end of plateau Wellhead pressure Minimum allowable wellhead pressure

    Pressure drop from initial reservoir pressure

    Total gas flow rate of the field Total gas flow rate of the field at abandonment condition Total gas flow rate of the field during plateau period Total oil flow rate of the field Total oil flow rate of the field at abandonment condition Gas flow rate per well Gas flow rate per well during plateau period Annual average gas flow rate of the field Annual average oil flow rate of the field

    Reservoir radius

    Wellbore radius Universal gas constant Gas-oil equivalent factor Fugacity ratio of i-th component Solution gas-oil ratio Solution gas-oil ratio at bubble point pressure Volatilized oil-gas ratio Volatilized oil-gas ratio at dew point pressure Target recovery factor at end of plateau

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    Fugacity ratio of i-th component in liquid-like phase Fugacity ratio of i-th component in vapor-like phase

    Total skin factor

    Volume-translate coefficient of i-th component

    Mechanical skin factor Average reservoir gas saturation Minimum gas saturation Sum of the mole number of liquid-like phase Average reservoir oil saturation Sum of the mole number of vapor-like phase Average reservoir water saturation Connate water saturation Specific gravity of gas Production time Production time at abandonment condition Production time at end of plateau Temperature Temperature of upstream node Temperature of downstream node Pipe section average temperature Critical temperature of fluid Critical temperature of i-th component Pseudocritical temperature of Reduced temperature of i-th component Temperature at standard condition Fluid velocity

    Retrograde liquid volume fraction

    Amount of excess gas at reservoir condition Amount of remaining gas phase at reservoir condition Amount of remaining gas phase plus excess gas at reservoir condition Amount of remaining oil phase at reservoir condition Pore volume of reservoir Original volume of PVT cell Molar volume of phase a calculated from EOS Critical molar volume of i-th component Molar volume of vapor phase Molar volume of vapor phase calculated from EOS

    Molar volume of liquid phase

    Molar volume of liquid phase calculated from EOS Pseudocritical molar volume Amount of water pseudo component in reservoir water Amount of water influx Amount of cumulative water injection Amount of cumulative water production Molar fraction of surface gas pseudo component in reservoir oil Molar fraction of i-th component in liquid phase Molar fraction of stock-tank oil pseudo component in reservoir oil

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    Molar fraction of surface gas pseudo component in reservoir gas Molar fraction of i-th component in vapor phase Molar fraction of stock-tank oil pseudo component in reservoir gas

    Molar fraction of i-th component in liquid-like phase

    Molar fraction of i-th component in vapor-like phase Molar number of i-th component in liquid-like phase Molar number of i-th component in vapor-like phase Compressibility factor of fluid Two-phase compressibility factor Compressibility factor of phase a Average compressibility factorGreek Symbol Definition

    Coefficient to adjust relative permeability of reservoir gas

    Turbulence parameter

    Specific gravity of gas Binary interaction coefficient between i-th and j-th component Tubing roughness Fluid viscosity Viscosity of vapor phase / Viscosity of reservoir gas Viscosity of i-th component at low pressure Viscosity of liquid phase Viscosity of liquid phase at low pressure Viscosity of reservoir oil Fluid density

    Density of vapor phase

    Density of gas phase at reservoir condition Density of liquid phase Density of oil phase at reservoir condition Density of oil phase at stock-tank condition Density of oil phase at stock-tank condition produced from reservoir gas Density of oil phase at stock-tank condition produced from reservoir oil Pseudo reduced density of liquid phase Density of remaining fluid inside PVT cell Molar density of reservoir gas Molar density of surface gas pseudo component

    Molar density of reservoir oil

    Molar density of stock-tank oil pseudo component Annual production time Average reservoir porosity Fugacity coefficient of i-th component in vapor phase Fugacity coefficient of i-th component Fugacity coefficient of i-th component in liquid phase Pitzers acentric factor of i-th component

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    xv

    ACKNOWLEDGEMENTS

    First and foremost I would like to thanks my advisor, Dr. Luis Ayala, for his continuous

    guidance, support and friendship throughout my graduate study. Without his encouragement and

    invaluable advice, this research would not have been completed. Additional thanks are extended

    to Dr. Larry Grayson, and Dr. Li Li for their interest and time in serving as my thesis committee.

    I would like to express my sincere appreciation to Dr. Turgay Ertekin and Dr. Russel

    Johns, and Dr. Zuleima Karpyn for the fundamental knowledge they have taught. I am also very

    grateful for educational environment that the faculty and staff of the Department of Energy and

    Mineral Engineering have created. I highly thank my sponsor, PTT Exploration and Production

    Company, for every support they have given.

    Many friends and colleagues have been very supportive. I would like to express my

    gratitude to Pipat Likanapaisal, Nithiwat Siripatrachai and Kanin Bodipat who always are good

    friends throughout my student life at Pennsylvania State University. I also thank all of my

    colleagues for making me have meaningful time and experience.

    Finally, but most deeply, I am forever in dept to my family, my father Phiraphong

    Vardcharragosad, my mother Pikun Tanarungreung, my sister Pungjai Keandoungchun, and

    sisters family, for their support, encouragement, and most importantly their tolerance.

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    Chapter 1Introduction

    Natural gas is a natural occurring gas which consisting of methane primarily. It plays a

    significant role in global economic as one of the main sources of energy. In 2009, world natural

    gas reserves equaled 6.29 Trillion Standard Cubic Feet (TCF) while world production reached

    106 BCF for the year (EIA, 2011). Conventional reservoirs consist of five different fluid types:

    dry gas, wet gas, retrograde gas, volatile oil, and black oils (McCain, 1990). They are

    distinguished from each other based on the present of fluid phases inside the reservoir and at

    surface production facilities.

    Field development and investment decisions in petroleum and natural gas require an

    integration of expertise from various areas including geology, reservoir, drilling, completion,

    process, and economic. Location and size of reservoirs, production rates and time, total

    recoverable volumes, number of wells and platforms, drilling and completion techniques,

    processing facilities scheme, cost and revenue, etc. are examples of information required for

    adequate field development decisions. Field performance indicators consist of information

    regarding flow rates, pressures, and production time is very important for field development. If

    field performance indicators are satisfactorily predicted, the hydrocarbon field could be

    developed using the best possible exploitation strategy while optimizing its economic

    performance. If not, the field might end up with too many wells, processing facilities that are too

    large, or wrong equipment sizing which can jeopardize profits or even lead to significant losses of

    investors capital.

    In modern age, computer simulation is used to simulate various types of mathematical

    models which can couple geological, fluid property, reservoir, production network, processing

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    facilities, and economic information. Field performance could be predicted by integrating these

    models together. However, the required type of mathematical model needs to be carefully

    selected to be able to perform the calculation most effectively. For reservoir characterization, for

    example, the modeler might utilize either afully dimensional numerical model- which can aptly

    capture all reservoir heterogeneities and geometry by discretizing it into many small grids -, or a

    zero-dimensional model - which assumes average reservoir and fluid properties across the

    domain. For fluid behavior characterization, the modeler might select either a fully compositional

    modelbased on the use of an equation of state and detailed fluid composition data, or a black-oil

    model - which uses the pseudo-component concept and relies on PVT laboratory results.

    Selection of those models generally depends on availability of input data, time constraint, and

    required accuracy of simulation results. In this study, a zero dimensional model coupled with a

    black-oil PVT fluid description is implemented for the study of field development optimization

    strategies in retrograde natural gas reservoirs.

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    Chapter 2Background

    2.1 Gas Condensate Hydrocarbon Fluid

    A gas condensate, retrograde gas condensate, or retrograde gas, is one of the five

    reservoir fluid types (McCain, 1990). The typical phase envelope of gas condensate reservoirs is

    shown in Figure 2-1. Gas condensates contain more intermediate and heavy hydrocarbon

    components more than dry gases or wet gases. As shown in Figure 2-1, their reservoir

    temperature is located in between the fluids critical temperature and their cricondentherm. The

    reservoir depletion path of a gas condensate fluid typically crosses the dew point line and a liquid

    phase appears at reservoir pressures lower than that of the dew point. The presence of liquid

    phase in the reservoir significantly increases the system complexity, even if this liquid phase does

    not flow and is very unlikely to be produced under normal production conditions.

    Figure 2-1: Phase Diagram of Typical Gas Condensate Reservoir

    Re

    servoirPressure

    Reservoir Temperature

    Reservoir

    Depletion

    Path

    Surface

    Depletion

    Path

    Critical Point

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    The general characteristics of gas condensate reservoir fluid can be summarized as

    follows (Walsh and Lake, 2003):

    Initial Fluid Molecular Weight: 2340 lb/lbmol Stock-Tank Oil Color: Clear to Orange Stock Tank Oil Gravity: 4560 API C7-plus Mole Fraction: 0.010.12 Typical Reservoir Temperature: 150300 F Typical Reservoir Pressure: 15009000 psia Volatilized Oil-Gas Ratio: 50300 STB/MMSCF Primary Recovery of Original Gas In Place: 70%85% Primary Recovery of Original Oil In Place: 30% - 60%

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    2.2 Modified Black-Oil Model

    A black-oil fluid model is a fluid characterization formulation which represents multi-

    component hydrocarbon mixture in terms of two hydrocarbon pseudo components, namely the

    surface gas and stock-tank oil pseudo components. In a traditional black-oil model, the

    solubility of the surface gas pseudo component in the reservoir oil fluid phase is taken into

    account while the solubility of stock-tank oil pseudo component in reservoir gas phase is

    neglected. The modified black-oil model which also called two-phase two-pseudo component

    model does not neglect the stock tank oil solubility in the gaseous reservoir phase, thus

    including both solubility variables into the formulation. Figure 2-2 shows the distribution of

    surface gas and stock-tank oil pseudo components among reservoir gas and reservoir oil phases.

    Figure 2-2: Distributions of Pseudo Components among Phasesin Modified Black-Oil Model

    The assumptions behind the modified black-oil PVT model can be summarized as

    follows (Walsh and Lake, 2003 and Whitson and Brule, 2000):

    There are two pseudo components which are surface gas and stock-tank oil. There are two fluid phases which are reservoir gas (vapor) and reservoir oil

    (liquid) phases.

    Surface GasStock-Tank

    Oil

    Surface Gas Stock-Tank Oil

    Reservoir Gas

    Phase

    Reservoir Oil

    Phase

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    Surface gas pseudo component is reservoir fluid which remains in gas phase atstandard condition.

    Stock-tank oil pseudo component is reservoir fluid which remains in oil phase atstandard condition.

    The reservoir gas phase, which is reservoir fluid remains in vapor phase atreservoir condition, consists of surface gas and stock-tank oil pseudo

    components.

    The reservoir oil phase, which is reservoir fluid remains in liquid phase atreservoir condition, consists of surface gas and stock-tank oil pseudo

    components.

    Properties of surface gas and stock-tank oil pseudo components remain the samethroughout the reservoir depletion.

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    2.3 Zero-Dimensional Reservoir Model

    The Material Balance Equation (MBE) is a specialized type of mass balance equation that

    combines mass balance equations of all pseudo components present in the reservoir into single

    equation. The MBE is also called zero-dimensional reservoir modelor tank model because it

    assumes that a reservoir behaves like a homogeneous tank with average rock and fluid properties

    across the domain. Pressure, temperature, and compositional gradients are thus neglected. MBEs

    can be derived from integrating diffusivity equations over space and time.

    Figure 2-3: Graphical Representation of Zero-Dimensional Reservoir Model

    (Source: http://www.joe.co.jp/english/menu2-5.html)

    The following assumptions are implemented in traditional in zero-dimensional reservoir

    models:

    Reservoir is isothermal Reservoir is under thermodynamic equilibrium condition There are no chemical and biological reaction in reservoir Capillary pressures of reservoir fluids are negligible Gravitational gradients in reservoir are negligible Pressure gradients in reservoir are negligible

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    Figure 2-5: Typical Field Performance of Gas CondensateReservoir Pressure, Bottomhole Flowing Pressure

    and Wellhead Pressure vs. Time

    Figure 2-5 demonstrates that, during field development calculations, reservoir pressure

    () decreases as production time increases because more oil and gas are being removed from thereservoir. Wellhead pressure () is also continuously decreased in time in order to maintain thegas flow rate () per well during the build-up and plateau periods. After that, once wellheadpressure () reaches the minimum allowable wellhead pressure at surface conditions, theplateau gas flow rate () cannot be maintained any longer and the decline period starts.Bottomhole flowing pressure (

    ) changes along with changes in reservoir pressure (

    ) and

    wellhead pressure () in order to provide the required pressure drop within the reservoir andproduction tubing.

    Pressure

    Production Time

    pr

    pwf

    pwh

    Build-up Plateau Decline

    Minimum Allowable Wellhead Pressure

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    2.5 Visual Basic for Applications (VBA)

    Visual Basic for Applications (VBA) is a programming language from Microsoft. The

    program is built into most MS-Office applications i.e. MS-Word, MS-Excel, MS-Access. Users

    can use VBA to create calculation subroutine and control user interface features such as menus,

    toolbars, worksheets, charts, etc (Walkenbach, 2007). VBA can only run within the host

    application, and not as a standalone application. VBA is functionally rich, and flexible. Because it

    is built into MS-Office applications, VBA subroutines will be able to execute so long as those

    applications are available on computer machines. MS-Excel with built in VBA is a very favorable

    platform for developing simulations. The main reasons are that most of engineers are familiar

    with MS-Excel application and MS-Excel itself is user-friendly software with many useful built-

    in features. Excels worksheets could be used as table to store input data. Simulation results could

    be easily stored in the tabular form and displayed on various types of built-in chart.

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    black oil PVT formulation for fluid properties calculation. These models are relatively simple, but

    fast, reliable, and robust. Results show that the proposed model is able to predict field

    performance while faithfully capturing the most salient characteristics of gas condensate

    reservoirs. In addition, optimization on targeted variables can be accomplished without difficulty.

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    Chapter 4Model Description

    The proposed field performance predictor has been developed using Microsoft Excel with built-in

    Visual Basic for Applications (VBA) subroutines. Workflow begins with the simulation of

    standard black-oil PVT properties, which could be done either based on standard PVT laboratory

    results (such as the Constant Volume Expansion or CVD) or via a phase behavior model based on

    cubic equations of state. Next, field performance data is calculated by integrating a zero-

    dimensional reservoir model, standard PVT fluid properties, well performance models for flow

    rates and pressure calculation, and production constraints. Based on this, an economic analysis

    can be performed based on simplified economic model. Finally, optimization on target variables

    can be carried out by evaluating field performance and net present value repeatedly for different

    and plausible production scenarios. The proposed simulation tool has been designed to simulate a

    single gas condensate reservoir based on the continuous drilling of identical wells placed at

    different locations of the reservoir area. Wellhead pressure is used to control gas flow rate.

    Reservoir pressure is used as the abandonment criteria. Optimization variables are target recovery

    factor at end of plateau and total number of wells. Those variables could be re-selected by simple

    modification in the VBA code. However, optimization variables can be made independent for a

    real field operation.

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    4.1 Phase Behavior Model (PBM)

    A phase behavior calculation (or a flash calculation) is used to predict the phase behavior

    of a reservoir fluid at an equilibrium condition. A standard phase behavior model consists of four

    main calculation modules; namely, compressibility factor calculations, vapor-liquid equilibrium

    calculations, fluid properties predictions, and phase stability analysis, which must be fully

    integrated to perform the flash calculation. The calculation starts with the determination of

    number of co-existent phases or phase stability analysis. If fluid is found in a single phase (stable)

    condition, fluid properties are calculated based on the available information on overall fluid

    composition. If fluid is found in a two-phase (unstable) condition, composition and molar fraction

    of each phase are determined using vapor-liquid equilibrium calculations. Then properties of each

    co-existent phase are calculated based on fluid composition of that phase (Ayala, 2009b).

    Input data consists of pressure, temperature, overall composition, physical properties,

    binary interaction coefficients, and volume translation coefficient of each pure component. Peng-

    Robinson Equation-of-State (PR EOS) is used to calculate Pressure-Volume-Temperature (PVT)

    relationship of the reservoir fluid (Peng and Robinson, 1976). Vapor-liquid equilibrium is

    assumed and an overall species material balance for a two-phase system is enforced. The output

    from a PBM subroutine consists of number of phases, molar fraction, composition, molecular

    weight, compressibility factor, density, adjusted density and viscosity of each fluid phase.

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    4.1.2 Vapor-Liquid Equilibrium

    Two main components are considered in order to predict properties of multi-component

    hydrocarbon in Vapor-Liquid Equilibrium (VLE) condition: material balance considerations and

    thermodynamic considerations. Iterative procedure is applied until the solution that satisfies both

    criteria can be determined.

    Mater ial Balance Considerations

    Rachford and Rice objective function, which is derived from enforcing an overall species

    mass balance in a two-phase multi-component system, is utilized to calculate molar fraction of

    each phase (Rachford and Rice, 1952):

    Equation 4-5

    where:

    = molar faction of i-th component = volatility ratio of i-th component =

    = molar fraction of i-th component in vapor phase

    = molar fraction of i-th component in liquid phase = molar fraction of vapor phase

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    After solving for from the objective function, molar fraction of liquid phase iscalculated from Equation 4-6, composition of vapor phase is calculated from Equation 4-7, and

    composition of liquid phase is calculated from Equation 4-8.

    Equation 4-6

    Equation 4-7

    Equation 4-8

    Thermodynamic Considerations

    According to the second law of thermodynamics, any system in equilibrium, such as a

    VLE condition, must have the maximum possible entropic state under the prevailing conditions.

    For such condition to be established, thermodynamics shows that net transfer of heat, momentum,

    and mass between both phases must be zero. Thus, temperature, pressure, and every species

    chemical potential in both phases must be equal to each other.

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    Chemical potential cannot be measured directly. However, equality of chemical potential

    can be represented by equality of fugacity between both phases. Fugacity is the pressure

    multiplier to correct non-ideality and to make ideal gas equation work for real gas during Gibbs

    energy calculations. In a VLE condition, fugacity of liquid phase must be equal to fugacity of

    vapor phase. Equation 4-9 is used to calculate fugacity for vapor phase while Equation 4-10 is

    used for liquid phase.

    Equation 4-9

    Equation 4-10

    where:

    = fugacity of i-th component in vapor phase

    = fugacity of i-th component in liquid phase = fugacity coefficient of i-th component in vapor phase = fugacity coefficient of i-th component in liquid phase= molar fraction of i-th component in vapor phase= molar fraction of i-th component in liquid phase = pressure {psia}

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    For the generalized formula of cubic EOSs discussed above, fugacity coefficients can be

    calculated using Equation 4-11 (Coats, 1985) below. Definitions of parameters are the same as

    definitions used in Equation 4-1. It should be noted that is equal to for calculating fugacitycoefficient of a liquid phase and is equal to for calculating fugacity coefficient of a vaporphase.

    Equation 4-11

    Volatility ratio () is equal to ratio between the gas composition and the liquidcomposition during an equilibrium condition. For a system with a VLE condition, is equalto

    . By substituting Equation 4-9 and Equation 4-10 into definition of volatility ratio, volatility

    ratio can be expressed in terms of fugacity coefficients as follows.

    Equation 4-12

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    The Successive Substi tut ion Method

    From material balance consideration, molar fraction of vapor phase and composition of

    each phase are functions of volatility ratios and overall composition. Volatility ratios themselves

    are also function of composition of each phase. Thus, an iterative procedure is needed in order to

    perform VLE prediction and honor the fugacity equality constraint. The following procedure is

    used to perform two-phase flash calculation (Whitson and Brule, 2000, p.52-55).

    First, initial guesses of volatility ratios are calculated using Equation 4-13 as proposed by

    Wilson (Wilson, 1968). Rachford and Rice objective function (Equation 4-5) is then solved using

    a standard Newton-Raphson iterative method. Then, the compositions of each phase are

    calculated using Equation 4-7 and Equation 4-8.

    Equation 4-13

    Next, the fugacity values of each component in both liquid and vapor phases are

    calculated using Equation 4-9 through Equation 4-11. Successive Substitution Method (SSM) is

    utilized to update volatility ratios (Equation 4-14) for a next iteration as shown below

    Equation 4-14

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    where:

    = volatility ratio of i-th component at iteration level n = fugacity of i-th component in liquid phase at iteration level n = fugacity of i-th component in vapor phase at iteration level n

    Once volatility ratios are updated, convergence criteria presented in Equation 4-15 must

    be checked. If the criteria are not satisfied, the procedure is repeated by solving Rachford and

    Rice objective function and recalculating phase compositions and resulting fugacities until

    convergence is attained.

    Equation 4-15

    The SSM algorithm is expected to have slow convergence rate near the critical point. To

    avoid this problem, accelerated SSM algorithm has been proposed. The algorithm proposed by

    Michelsen (Michelsen, 1982b) or the algorithm proposed by Merah et al(Merah et al, 1983) are

    examples of well-known ASSM algorithms.

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    4.1.3 Fluid Property Prediction

    Molecular Weight

    Molecular weight of vapor and liquid phases are weighted average of molecular weight

    of all pure components, as shown below

    Equation 4-16

    Equation 4-17

    where: = molecular weight of vapor phase {lb/lbmol} = molecular weight of liquid phase {lb/lbmol} = molecular weight of i-th component {lb/lbmol} = mole fraction of i-th component in vapor phase

    = mole fraction of i-th component in liquid phase

    = number of components in the multi-component hydrocarbon

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    Density

    Density of each phase is calculated from Equation 4-18 and Equation 4-19.

    Equation 4-18

    Equation 4-19

    where:

    = density of vapor phase {lbm/ft3} = density of liquid phase {lbm/ft3}

    = molecular weight of vapor phase {lbm/lbmol}

    = molecular weight of liquid phase {lbm/lbmol} = molar volume of vapor phase {ft3/lbmol} = molar volume of liquid phase {ft3/lbmol }

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    Molar volume of each phase is calculated from real gas law (Equation 4-20), then,

    adjusted by using volume-translation technique.

    Equation 4-20

    where

    = calculated molar volume of phase a from EOS {ft3/lbmol}= compressibility factor of phase a = universal gas constant {10.732 psi-ft3/R-lbmol} = temperature {R} = pressure {psia}

    As discussed by Whitson and Brule (p.51) and Danesh (p.141-143), calculated molar

    volume from real gas law can be adjusted by implementing volume-translation or volume-shift

    technique (Whitson and Brule, 2000 and Danesh, 1998). This technique improves volumetric

    calculation of liquid phase, which is the main problem of two-constant EOSs, without altering

    VLE prediction results. The volume translation technique, originally introduced by Martin and

    further developed by Penelous et aland Jhaveri and Youngren, can be summarized as follows

    (Martin, 1979, Penelus et al, 1982, and Jhaveri and Youngren, 1988):

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    31 Equation 4-23

    where:

    = component-dependent volume-shift parameter = co-volume parameter of i-th component= volume-translate coefficient of i-th component

    Table 4-1: Volume-Translation Coefficients for Pure Components (Whitson and Brule, 2000)

    Component PR EOS SRK EOS

    N2 -0.1927 -0.0079

    CO2 -0.0817 0.0833

    H2S -0.1288 0.0466

    C1 -0.1595 0.0234

    C2

    -0.1134 0.0605

    C3 -0.0863 0.0825

    i-C4 -0.0844 0.0830n-C4 -0.0675 0.0975

    i-C5 -0.0608 0.1022

    n-C5 -0.0390 0.1209

    n-C6 -0.0080 0.1467

    n-C7 0.0033 0.1554

    n-C8 0.0314 0.1794

    n-C9 0.0408 0.1868

    n-C10 0.0655 0.2080

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    Viscosity

    Viscosity of vapor phase is calculated from the correlation proposed by Lee et alin 1966

    (Equation 4-24 through Equation 4-27).

    Equation 4-24

    Equation 4-25

    Equation 4-26

    Equation 4-27

    where:

    = viscosity of vapor phase {cp} = density of vapor phase {lbm/ft

    3

    } = molecular weight of vapor phase {lbm/lbmol} = temperature {R}

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    Equation 4-30

    Equation 4-31

    where:

    = viscosity of liquid phase at low pressure {cp} = molar fraction of i-th component in liquid phase = viscosity of i-th component at low pressure {cp} = viscosity parameter of i-th component {cp -1} = reduce temperature of i-th component ( )

    = temperature {R}

    = critical temperature of i-th component {R} = critical pressure of i-th component {psia} = molecular weight of i-th component {lbm/lbmol} = number of componentsViscosity parameter of liquid phase is calculated from Equation 4-32 to Equation 4-35.

    Equation 4-32

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    Pseudo reduced density of the liquid phase is calculated from Equation 4-36 and

    Equation 4-37 shown below.

    Equation 4-36

    Equation 4-37

    where:

    = pseudo reduced density of liquid phase = density of liquid phase {lbm/ft3}

    = molecular weight of liquid phase {lbm/lbmol}

    = pseudocritical molar volume of liquid phase {ft3/lbmol} = critical molar volume of i-th component {ft3/lbmol} = molar fraction of i-th component in liquid phase = number of components

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    Step 6: Calculate the fugacity of vapor-like and liquid-like phases based on the calculated

    mole fraction from Step 5. Equation 4-9 , Equation 4-10 and Equation 4-11 are utilized.

    Step 7: Calculate the fugacity ratio corrections for successive substitution update of the values.

    Equation 4-44

    Equation 4-45

    where:

    = fugacity ratio calculation of i-th component in vapor-like phase = fugacity ratio calculation of i-th component in liquid-like phase = fugacity of i-th component in original fluid = fugacity of i-th component in vapor-like phase = fugacity of i-th component in liquid-like phase

    = Sum the mole numbers of vapor-like phase

    = Sum the mole numbers of liquid-like phase

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    Step 8: Check whether convergence criteria is achieved

    Equation 4-46

    Step 9: If convergence is not obtained, update values

    Equation 4-47Step10: Apply criterion to check whether a trivial solution has been obtained

    Equation 4-48

    Step 11: If a trivial solution is not indicated, go to Step 3 for the next iteration.

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    42

    4.2 Standard PVT Properties

    The standard PVT properties used to describe a two-phase, two-pseudo component fluid

    model (black oil model) relies on the definition and calculation of four basic properties,

    namely: gas formation volume factor (), oil formation volume factor (), volatilized oil-gasratio (), and solution gas-oil ratio (). These PVT properties are required inputs for a zero-dimensional reservoir model. In this study, these required PVT properties can be obtained from

    either a laboratory fluid analysis, typically a Constant Volume Depletion (CVD) test, or from a

    phase behavior model (PBM) calculation. If the PVT/CVD laboratory report is available, the

    resulting PVT properties are calculated using Walsh-Towler algorithm (Walsh and Lake, 2003).

    A template has been prepared using MS-Excel worksheet for this purpose. In the absence of a

    PVT lab report, a PBM calculation is implemented which combines Walsh-Tolwer method with

    the work of Thararoop in 2007 (Thararoop, 2007). This PBM subroutine does not only extend the

    flexibility of the main simulator significantly, but also provide very useful information about fluid

    properties which could help in thoroughly analyzing the depletion characteristics of the given gas

    condensate fluid.

    The specific gravity of reservoir gas is required for flow rate and flowing pressure

    calculations, as it will be discussed below. The specific gravity of a reservoir gas can be obtained

    from either the laboratory fluid analysis or from molecular weight calculations derived from

    PBM. If the lab analysis is available, compositions of the produced wellstreams reported in the

    experimental depletion study based on the Constant Volume Depletion (CVD) test are used to

    calculate molecular weight of reservoir gas. If the lab report is unavailable, the molecular weight

    of the reservoir gas is obtained directly from flash/PBM calculation results. Specific gravity of

    reservoir gas is equal to molecular weight of reservoir gas divided by molecular weight of air.

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    4.2.1 Definitions, Mathematic Relationships, and Characteristics

    A clear understanding of the definitions of standard PVT black oil properties that are

    used to characterize two-phase, two-pseudo component fluid models is crucial for their

    meaningful calculation and prediction. These definitions, mathematic relationships, and their

    most significant features have been summarized below (Walsh and Lake, 2003; Whitson and

    Brule, 2000).

    Definitions

    Figure 4-1shows the graphical representation of the definitions of the standard PVT

    properties used in the formulation of two-phase, two-pseudo component fluid model (or modified

    black-oil model). In this figure, the gas phase at reservoir condition () results from the mixingof certain amounts of surface gas () and stock-tank oil () pseudo components. The oilphase at reservoir condition (

    ) results from the mixing of certain amounts of surface gas (

    )

    and stock-tank oil () pseudo components. The produced gas phase at surface condition ()(not shown in the figure) would consists of the combination of surface gas pseudo component

    produced from gas phase at reservoir condition () and surface gas pseudo component liberatedfrom oil phase at reservoir condition (). By the same token, the produced oil phase at surfacecondition () (not shown in the figure) consists of stock-tank oil pseudo component producedfrom oil phase at reservoir condition (

    ) and stock-tank oil pseudo component condensed from

    gas phase at reservoir condition ().

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    component in oil phase at reservoir condition is thus defined as . Clearly, + = 1. Theirformulas are summarized in Equation 4-53 through Equation 4-56.

    Equation 4-53

    Equation 4-54

    Equation 4-55

    Equation 4-56

    Mathematic Relati onships

    If only one mole of reservoir fluid is considered, volumes at reservoir condition, and

    , can be represented by molar density at reservoir condition,

    and

    , respectively.

    Similarly, volumes at surface condition, , , , and , can be represented by molarfraction of pseudo component in reservoir fluid and molar density at surface condition, , , , and , respectively. If we substitute these definitions into equations for

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    Figure 4-2: Typical Characteristic of Gas Formation Volume Factor ()and Volatilized Oil-Gas Ratio () for Gas Condensate

    Figure 4-3: Typical Characteristic of Oil Formation Volume Factor ()and Solution Gas-Oil Ratio () for Gas Condensate

    Rv-VolatilizedOil-GasRatio

    Bg-GasFormationVolumeFactor

    Reservoir Pressure

    Dew Point Pressure

    Rv

    Bg

    Rs-SolutionGas-OilRatio

    Bo-OilFormationVolumeFactor

    Reservoir Pressure

    Dew Point Pressure

    Bo

    Rs

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    As shown in Figure 4-2, gas formation volume factors () are expected to increase withdecreasing reservoir pressure () because the denominator, , in Equation 4-57 approaches zero.Volatilized oil-gas ratio () will remain constant because all parameters in Equation 4-59 remainthe same. Constant values of, , and result from the constant composition of gas phase inthe reservoir. Once dew point conditions are reached, Figure 4-2 also shows that the volatilized

    oil-gas ratio () is expected to decrease with decreasing reservoir pressure, mainly because ofdecreasing and increasing values in Equation 4-59. Driven by the condensate drop out thatdevelops in the reservoir below dew point conditions, the reservoir gas will start to contain less

    heavy hydrocarbon molecules that can be produced as condensate at surface condition. As a

    result, the fraction of stock-tank oil () in the reservoir gas decreases while fraction of surfacegas () increases ( + = 1). As pressure depletion progresses, and if it gets low enough, thevolatilized oil-gas ratio () trend would be reversed.

    Figure 4-3 illustrates that at reservoir pressure above the dew point there is no liquid

    phase at reservoir condition and therefore no calculations of

    and

    can be directly performed

    from their definitions. Once dew point conditions are crossed, oil formation volume factor () isexpected to decrease with decreasing reservoir pressure mainly because of increasing and values in Equation 4-58. As pressure decreases, more surface gas pseudo component will be

    liberated from the oil phase. As a result, the molar fraction of stock-tank oil pseudo component in

    oil phase () becomes higher and the density of oil phase at reservoir condition () alsoincreases. Similarly, the solution gas-oil ration (

    ) will be expected to decrease with decreasing

    reservoir pressure because of the increased molar fraction of stock-tank oil pseudo component in

    oil phase () and decreasing molar fraction of surface gas pseudo component in oil phase () inEquation 4-60. Even though oil formation volume factors () and solution gas-oil ratios ()cannot be calculated directly because of the lack of an actual liquid phase at reservoir from their

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    definitions, Walsh and Lake suggest employing the following relationships for oil formation

    volume factor () and solution gas-oil ratio () as place-holder values above the dew point:

    Equation 4-61

    Equation 4-62

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    4.2.2 Obtaining Standard PVT Properties from Laboratory PVT Reports

    In a laboratory PVT test, a representative sample of the reservoir fluid is subjected to a

    series of depletion steps that try to closely mimic or reproduce the expected pressure depletion

    path followed by the fluid during reservoir production. Temperature of the test is maintained

    constant and equal to prevailing reservoir temperature. Resulting volumes of each phase (liquid

    and vapor) are recorded along with the pressure at which the record is made. Fluid composition

    and physical properties of the produced fluids are also analyzed. The typical standardized PVT

    tests conducted for gas condensate fluids are the Constant Composition Expansion (CCE) and

    Constant Volume Depletion (CVD) tests. Details of these PVT tests can be found in many

    petroleum engineering textbooks (McCain, 1990; Denesh, 1998; Whitson and Brule, 2000, Walsh

    and Lake, 2003); thus, they will be discussed very briefly in this manuscript.

    In a CCE test, the reservoir fluid sample is placed inside a PVT cell and is pressurized to

    a pressure equal to initial reservoir pressure, while maintaining a constant temperature inside the

    PVT cell equal to reservoir temperature. Pressure inside the cell is then decreased to a next lower

    pressure level by isothermal expansion. The new volume of each phase is recorded. This process

    continues until abandonment pressure conditions are reached. In the CCE testing process, no fluid

    is taken out the cell and therefore the overall composition of reservoir fluid inside the PVT cell

    remains constant while the volumes and densities of each the co-existing phases below dew point

    conditions do change with cell pressure.

    In a CVD test, a reservoir fluid sample will be placed inside the PVT cell and pressurized

    to the dew point pressure, while the temperature of the PVT cell is kept constant at reservoir

    temperature. Then, pressure of the cell will be lowered to the next pressure level by isothermal

    expansion. After that, a portion of gas phase inside the cell is produced (i.e., removed out of the

    cell) so that the cells volume is restored back to the original cell volume at dew point conditions.

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    The volume that the liquid phase occupies inside the PVT cell is recorded and the excess

    (produced) gas analyzed. Depletion study which provides the resulting cumulative production

    data at every pressure level is recorded and is used during the calculation of the standard PVT

    properties from laboratory PVT fluid test report.

    In this study, a calculation template is prepared in MS-Excel worksheet. The Walsh-

    Towler algorithm is implemented to convert the results from the CVD experiments into the

    standard table of PVT properties for a gas condensate fluid. Walsh-Towler algorithm is

    summarized below.

    Walsh-Towler Algori thm

    Walsh-Towler algorithm is one of the methods used to calculate standard PVT properties

    for gas condensate based on CVD testing results (Walsh and Towler, 1995; Walsh and Lake,

    2003). This algorithm is relatively simple because it based on enforcing material balance

    constraints around the PVT cell at every pressure level during the PVT lab test. The algorithm

    was originally proposed by Walsh and Towler in 1995 and was later modified by Walsh and Lake

    in 2003. By directly using data from a CVD report, this algorithm is implicitly assuming that

    actual field separator conditions of the surface production system is the same as those surface

    condition used during the CVD PVT test. It also assumes that only the gas phase at reservoir

    condition can be recovered and that any condensate drops out inside the reservoir will remain

    immobile during reservoir life.

    One of the constraints of using this method is the availability of cumulative production

    data at surface conditions because such data is not always performed or reported for every CVD

    experiment. If such cumulative production data at surface conditions is not available in the CVD

    report, it is customarily recommended to implement surface flash calculations using Standings

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    K-values to reproduce them (Walsh and Lake, 2003). The algorithm also requires a high accuracy

    and reliability of the CVD report in order to obtain a healthy and physically meaningful set of

    derived standard PVT properties. It can be demonstrated that small error in the data reported by a

    CVD test can result in PVT property values which are physically impossible (e.g., negative

    values). And even when the data reported by the CVD report is highly reliable, the Walsh and

    Towler algorithm can still lead to unphysical values for standard PVT properties. This limitation

    results from combining the two-phase two-pseudo component (black oil) model with material

    balance calculation around the PVT cell. This limitation will be discussed in detail in Chapter 5.

    Walsh-Towler algorithm consists of six sequential steps which must be fully completed at

    every given pressure level before moving to the next pressure. One pre-calculation is also needed

    before starting the algorithm. The variables and their nomenclature employed in the sequence of

    calculations are graphically illustrated in Figure 4-4.

    Figure 4-4: Graphical Representation of CVD Data used in Walsh-Towler Algorithm

    Vg,j

    Vo,j

    Reservoir Condition Surface Condition

    Gfg,j

    Nfg,j

    Gfo,j

    Nfo,j

    Reservoir Gas

    Reservoir Oil

    Surface Gas

    Stock-Tank Oil

    Vg,j

    Gfg,j

    Bg = ----------- Rv = -----------

    Nfg,j

    Gfg,j

    Bo = ----------- Rs = -----------

    Vo,j

    Nfo,j

    Gfo,j

    Nfo,j

    VT

    VEG,j

    PR PDew PR < PDew Gpj

    Npj

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    Pre-calculation: In this step, the total cumulative volumes of surface gas () and stock-tank oil () pseudo components produced from the reservoir fluid, and the resulting volume ofPVT cell () are calculated for the dew point condition. The volume of surface gas pseudocomponent () is calculated from the summation of cumulative gas recovery from 1 st stageseparator, 2nd stage separator, and stock tank for all available pressures - from dew point

    conditions to the last reported (abandonment) pressure. The volume of stock-tank oil pseudo

    components () is equal to cumulative oil recovery from stock tank for all available and reportedpressures (dew point to abandonment). These data are obtained from the calculated cumulative

    recovery reported in the depletion table.

    PVT cells volume is calculated from the definition of gas formation volume factor

    (Equation 4-63). The gas formation volume factor () is calculated from Equation 4-57.Compressibility factor of gas phase () can be obtained from the CVD report. Mole fraction ofsurface gas pseudo component in the reservoir gas () is equal to divided by the volume of gasequivalent at the dew point (

    ) which is usually taken as 1000 MSCF.

    Equation 4-63

    Volatilized oil-gas ratio at dew point () is calculated from Equation 4-64, while oilformation volume factor (

    ) and solution gas-oil ratio (

    ) are calculated from Equation 4-61

    and Equation 4-62, respectively.

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    Equation 4-64

    Step 1: Find and : Starting at the dew point, the volume of surface gas pseudocomponent released from the excess gas () at each pressure is calculated from the summationof cumulative gas recovery from 1st stage separator, 2nd stage separator, and stock tank. Volume

    of and stock-tank oil pseudo component released from the same excess gas () at each pressureis equal to cumulative oil recovery from stock tank. These data are obtained from the calculated

    cumulative recovery reported in the depletion table. Incremental of and from pressure levelj-1 to pressure level j are calculated from Equation 4-65 and Equation 4-66. Please note that

    pressure level j begins from zero at the dew point (j=0). , , , and are alsoequal to zero.

    Equation 4-65

    Equation 4-66

    Step 2: Find

    and

    : Total volume of surface gas (

    ) and stock-tank oil (

    ) pseudo

    components released from both reservoir gas and reservoir oil at pressure level j are calculated

    from Equation 4-67 and Equation 4-68. It should be noted that pressure level j begins from zero at

    the dew point (j=0), and and are equal to and , respectively.

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    56 Equation 4-67

    Equation 4-68

    Step 3: Find and : Volume of oil phase at reservoir condition at pressure level j() is calculated from Equation 4-69. Retrograde liquid volume fraction at pressure level j(), can be obtained from CVD report. Volume of gas phase after excess gas removal atreservoir condition at pressure level j () is calculated from Equation 4-70. Note that pressurelevel j begins at zero at dew point conditions (j=0)

    Equation 4-69

    Equation 4-70

    Step 4: Find , , and : Molar fraction of reservoir fluid which remains in thePVT cell at pressure level j (

    ) is calculated from Equation 4-71. For this calculation, two-

    phase compressibility factor () data can be obtained from the CVD report. Molar fraction ofexcess gas which is removed from PVT cell at pressure level j () is calculated from Equation4-72. Molar fraction of gas phase which remain in PVT cell at pressure level j () is calculatedfrom Equation 4-73. Compressibility factor of gas () is also obtained from the CVD report.

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    Please note that pressure level j begins from zero (j=0) at the dew point. and at dewpoint are equal to 1.0 while at dew point is equal to zero.

    Equation 4-71

    Equation 4-72

    Equation 4-73

    Step 5: Find and : Volume of surface gas pseudo component produced fromreservoir gas at pressure level j () is calculated from Equation 4-74. Volume of stock-tankpseudo component produced from reservoir gas at pressure level j () is calculated fromEquation 4-75. It is important to note that pressure level j begins from zero at the dew point (j=0).

    and

    at dew point pressure are equal to

    and

    , respectively.

    Equation 4-74

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    Equation 4-75

    Step 6: Find and : Volume of surface gas pseudo component produced fromreservoir oil at pressure level j () is calculated from Equation 4-76. Volume of stock-tank oilpseudo component produced from reservoir oil at pressure level j () is calculated fromEquation 4-77.

    Equation 4-76

    Equation 4-77

    After completing all six steps outline above for the given pressure level, Equation 4-49

    through Equation 4-52 are now directly used to calculate the standard PVT properties. All

    applicable unit conversion factors must be checked and adjusted properly. The calculation

    process is systematically repeated for all pressure levels until all reported data in the CVD report

    have been considered and abandonment conditions have been reached.

    Standard PVT properties at pressures higher than the dew point are calculated based on

    the properties at dew point pressure. Gas formation volume factor () is the product of gasformation volume factor at dew point pressure and relative volume obtained directly from CCE

    testing results. The relative volume is the ratio between total volume of hydrocarbon at reservoir

    conditions and the volume at saturated conditions. For under-saturated gas condensate system,

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    relative volume is equal to the ratio between at specified pressure and at dew point pressure.Volatized oil-gas ratio () is equal to volatilized oil gas ratio at dew point pressure. Oilformation volume factor () and solution gas-oil ratio () are calculated from Equation 4-61and Equation 4-62, respectively.

    Finally, it is very important to mention that, in Walsh-Towler algorithm, volumes of

    pseudo components produced from the reservoir oil (step 6) do not actually come from direct

    surface measurement. In a CVD test, the oil inside the cell is never produced (is assumed

    immobile) so surface data for produced oil is not available.. Instead, these values are indirectly

    calculated based on the enforcement of mass balance constraints around the PVT cell. Therefore,

    actual oil formation volume factor () and solution gas-oil ratio () calculated from actualsurface flashes of the reservoir fluid might be significantly different from the ones estimated

    using these indirectly calculated surface volumes. If the calculated and resulting from theapplication of this algorithm do not agree with the physically acceptable trends or values, the

    results should be disregarded and the laboratory results have to be adjusted.

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    direct calculation of saturation pressure at the prevailing reservoir temperature could be also

    alternatively employed (Whitson and Brule, 2000).

    The initial amount of mole of the reservoir fluid sample inside PVT cell () iscalculated from Equation 4-78. Standard condition is set to be 14.7 psia and 520 R. Volume ofinitial reservoir fluid in term of gas equivalent () is assumed to be 1.0 MMSCF which is usedas the basis for the calculation.

    Equation 4-78

    The associated volume of PVT cell () is calculated from Equation 4-79. Molecularweight () and density () are obtained by performing flash calculation on initial reservoirfluid composition at the dew point condition.

    Equation 4-79

    The molar fractions of surface gas (

    ) and stock-tank oil (

    ) pseudo components in

    reservoir fluid are calculated from Equation 4-80 and Equation 4-81. Molar fraction of liquid

    phase at first-stage separator () is obtained by performing flash calculation on initialreservoir fluid composition at first-stage separator condition. Molar fraction of liquid phase at

    second-stage separator () is obtained by performing flash calculation on liquid composition

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    from first-stage separator at second-stage separator condition. Molar fraction of liquid phase at

    stock-tank condition () is obtained by performing flash calculation on liquid compositionfrom second-stage separator at stock-tank condition.

    Equation 4-80

    Equation 4-81

    Total volume of surface gas () and stock-tank oil () pseudo components initiallypresent in the reservoir fluid are calculated from Equation 4-82 and Equation 4-83. Value of

    379.56 is molar volume of gases at standard condition which is constant. Molecular weight

    () and density () of oil at stock-tank condition are obtained from flash calculationresults at stock-tank condition. Please note that these values (G and N) are not being obtained by

    cumulative adding cumulative production values at every pressure level, as done in the original

    Walsh and Tower algorithm. Chapter 5 will present a discussion on this regard and justification.

    Equation 4-82

    Equation 4-83

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    Step 2: Find and : The volume that the gas phase occupies at reservoircondition before the removal of the excess gas at every pressure level j () is calculatedfrom Equation 4-87. The volume of reservoir oil phase present at pressure level j () iscalculated from Equation 4-88. Molecular weight and density of gas and oil phases at reservoir

    condition at pressure level j (, , , ) are obtained by performing flashcalculation on overall composition from pressure level j-1, at pressure level j. Note that pressure

    level j begins from zero at the dew point (j=0). is equal to and is equal to zero.

    Equation 4-87

    Equation 4-88

    Step 3: Find and : The volume of reservoir gas phase after excess gas removal atpressure level j () is calculated from Equation 4-89. Volume of excess gas at reservoircondition at pressure level j () is then calculated from Equation 4-90.

    Equation 4-89

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    separator at second-stage separator condition. The fraction of liquid phase at stock-tank condition

    recovered from reservoir gas at pressure level j ( ) is obtained by performing flashcalculation on liquid composition from second-stage separator at stock-tank condition.

    Equation 4-93

    Equation 4-94

    Step 6: Find and : Volume of surface gas () and stock-tank oil ()pseudo components in reservoir gas at pressure level j are calculated from Equation 4-95 and

    Equation 4-96. The value of 379.56 is molar volume of gases at standard condition which is a

    constant for ideal gases. Molecular weight (

    ) and density (

    ) of oil at stock-tank

    condition recovered from reservoir gas at pressure level j are obtained from flash calculation

    results at stock-tank condition in Step 5.

    Equation 4-95

    Equation 4-96

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    Step 7: Find and : The molar fractions of surface gas () and stock-tank oil() pseudo components in the reservoir oil at every pressure level j are calculated fromEquation 4-97 and Equation 4-98. The fraction of liquid phase at first-stage separator recoveredfrom reservoir oil at pressure level j ( ) is obtained by performing flash calculation oncomposition of reservoir oil at pressure level j, at first-stage separator condition. The fraction of

    liquid phase at second-stage separator recovered from reservoir oil at pressure level j ( ) isobtained by performing flash calculation on liquid composition from first-stage separator at

    second-stage separator condition. The fraction of liquid phase at stock-tank condition recovered

    from reservoir oil at pressure level j ( ) is obtained by performing flash calculation on liquidcomposition from second-stage separator at stock-tank condition.

    Equation 4-97

    Equation 4-98

    Step 8: Find and : The volume of surface gas () and stock-tank oil ()pseudo components in reservoir oil at pressure level j are calculated from Equation 4-99 and

    Equation 4-100. The value of 379.56 is molar volume of gas at standard condition which is

    constant. Molecular weight () and density ( ) of oil at stock-tank condition recoveredfrom reservoir oil at pressure level j are obtained from flash calculation results at stock-tank

    condition in Step 7.

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    Equation 4-99

    Equation 4-100

    Step 9: Find and : Remaining moles of reservoir fluid inside PVT cell at pressurelevel j ( ) is calculated from Equation 4-101. Overall composition of i-th component insiderPVT cell at pressure level j () after gas removal is updated by implementing Equation 4-102.Note that pressure level j begins from zero (j=0) at the dew point. is equal to . Liquidcomposition () and vapor composition () of i-th component at pressure level j are obtainedby performing flash calculation on overall composition from pressure level j-1, at pressure level j.

    Equation 4-101

    Equation 4-102

    After completing all nine steps outlined above at every given pressure level, Equation

    4-49 through Equation 4-52 will be used to directly calculate standard PVT properties. All unit

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    conversion factors must be checked and properly adjusted. This calculation process must be

    continuously repeated for the every pressure level until abandonment pressure is reached.

    Standard PVT properties at pressures higher than the dew point are calculated based on

    available properties at dew point pressure. Gas formation volume factor () is calculated fromgas formation volume factor at dew point pressure using Equation 4-103. The ratio between

    ( ) at dew point pressure and ( ) at specified pressures above the dew point is equivalent toratio between volume of reservoir gas () at specified pressures above the dew point and volumeof reservoir gas (

    ) at dew point pressure. Volatized oil-gas ratio (

    ) is equal to volatilized oil-

    gas ratio at dew point pressure (). Oil formation volume factor () and solution gas-oil ratio() are calculated from Equation 4-61 and Equation 4-62, respectively.

    Equation 4-103

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    4.3 Zero-Dimensional Reservoir Model

    The Material Balance Equation (MBE) (also known as zero-dimensional reservoir model

    or tank model) is a mass balance statement that combines mass balance equations of all pseudo

    components present in the reservoir fluid. The assumptions behind a tank model have been

    already addressed in Section 2.3. Walsh and Lake (2003) have presented a generalized form of

    material balance equation that could be used for the analysis of depletion performance for all five

    types from reservoir fluids, based on the work originally published by Walsh (1995). They also

    developed the MBE specialized for gas condensate fluids by simplifying the generalized MBE for

    the conditions particular to these kind of fluids. Section 4.3.1 discusses and presents the GMBE

    proposed by Walsh as implemented in this study.

    In zero-dimensional reservoir model, cumulative productions of pseudo components and

    saturations of reservoir fluids are calculated as functions of reservoir pressure, standard PVT

    properties, and initial reservoir condition. This model treats a reservoir as a homogeneous tank;

    thus only average reservoir pressure and average PVT properties are required as the model inputs.

    In this study, a VBA subroutine has been developed to simulate cumulative oil and gas

    productions as well as their saturations as a function of reservoir pressure, by implementing the

    MBE specialized for gas condensate fluids. Most of the time, the MBE is used to simulate the

    results explicitly as a function of time and depletion. However, if some target outputs are

    specified, such as cumulative recovery at end of plateau, an iterative procedure would need to be

    implemented in order to honor the additional constraint.

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    Equation 4-104

    where:

    = volume of surface gas pseudo component in reservoir gas at initialcondition {SCF}

    = volume of stock-tank oil pseudo component in reservoir oil at

    initial condition {STB}

    = volume of water component in reservoir water at initial condition{STB}

    = pore volume at initial condition {RB} = volume of water influx {RB}

    = cumulative gas production {SCF}

    = cumulative gas injection {SCF} = cumulative oil production {STB} = cumulative water production {STB} = cumulative water injection {SCF} = expansivity of reservoir gas {RB/SCF} = expansivity of reservoir oil {RB/STB} = expansivity of reservoir water {RB/STB} = expansivity of formation (rock) {Dimensionless} = gas formation volume factor {RB/SCF} = oil formation volume factor {RB/STB}

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    73 = water formation volume factor {RB/STB} = volatilized oil-gas ratio {STB/SCF} = solution gas-oil ratio {SCF/STB}

    Expansivity of reservoir fluid is defined as the total expansion of a unit mass of reservoir

    fluid between two reservoir pressures at the same reservoir temperature. Expansivities of

    reservoir gas, reservoir oil, and reservoir water are calculated from Equation 4-105, Equation

    4-106, and Equation 4-107, respectively. Expansivity of formation (rock) is defined in a different

    form from fluid expansivity and is calculated in terms of formation (rock) compressibility as

    indicated by Equation 4-108.

    Equation 4-105

    Equation 4-106

    Equation 4-107

    Equation 4-108

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    where:

    = two-phase gas formation volume factor {RB/SCF} = two-phase oil formation volume factor {RB/SCF} = formation (rock) compressibility {psi-1} = pressure drop from initial reservoir pressure {psi}

    The two-phase formation volume factor implemented above is defined as the ratio

    between total volume of reservoir fluid (gas and oil phases) and total volume of the pseudo

    component. Two-phase formation volume factor of gas () and oil () are calculated fromEquation 4-109 and Equation 4-110, respectively. If reservoir is a single phase gas reservoir, two-

    phase gas formation volume factor () will be equal to gas formation volume factor () whiletwo-phase oil formation will remain undefined. Similarly, if reservoir is single phase oil reservoir,

    two-phase oil formation volume factor () will be equal to oil formation volume factor ()while the two-phase gas formation volume factor will remain undefined.

    Equation 4-109

    Equation 4-110

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    4.3.2 Material Balance Equation for a Gas Condensate Fluid

    GMBE can be simplified significantly when condensate drop out, developed below dew

    point saturation conditions in the reservoir, is considered immobile. The immobile condensate

    assumption is a fairly reasonable one for gas condensates; however, it cannot be applied for other

    types of reservoir fluid (Walsh and Lake, 2003). The Simplified Gas Condensate Tank model,

    SGCT, is derived from Generalized Material Balance Equation with the following additional

    assumptions:

    Reservoir is under-saturated at initial reservoir pressure Expansivities of water and formation are negligible There is no water influx, water production, and water injection There is no gas injection Condensate drop out in the reservoir is immobile

    Gas Condensate Performance Below Dew Poin t

    At initial undersaturated conditions, the volume of surface gas pseudo component in

    reservoir gas at initial condition is equal to the Original Gas In Place (OGIP or G) while and the

    volume of stock-tank oil pseudo component in reservoir oil at initial condition is equal to zero.

    Equation 4-111 is the SGCT model after applying all these additional assumptions:

    Equation 4-111

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    This SGCT model can be further manipulated in order to obtain a more useful form by

    dividing it through by and substituting by . After that, finite differenceapproximation is applied, resulting in expressions for the calculation of incremental oil and gas

    production. As a result, Equation 4-112 through Equation 4-118 are a set of equations that can be

    used to calculate reservoir performance from SGCT model.

    Equation 4-112

    Equation 4-113

    Equation 4-114

    Equation 4-115

    Equation 4-116

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    Equation 4-121

    Equation 4-122

    Equation 4-123

    It should be noted that this set of equation (Equation 4-120 to Equation 4-123) only

    applies for pressures above dew point. The pressure level j begins from zero at initial reservoir

    and end at the last pressure above the dew point. , , , and are equal tozero at the initial reservoir pressure. The calculation has to be completed at one pressure level

    before moving to the next pressure level.

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    4.3.3 Phase Saturation Calculations

    One of the methods to derive a phase saturation equation is to combine the mass balance

    equation for the stock-tank oil pseudo-component with the saturation equation constraint in order

    to eliminate gas saturation parameter ( ) and then combine the resultingequation and volumetric OGIP calculation equation so that the pore volume variable is

    eliminated. The resulting saturation equation for the oil phase is shown in Equation 4-124.

    Equation 4-124

    where:

    = average reservoir oil saturation = average reservoir gas saturation = average reservoir water saturation = cumulative oil production {STB} = original oil in place {STB} = average reservoir porosity = gas formation volume factor {RB/SCF} = oil formation volume factor {RB/STB} = volatilized oil-gas ratio {STB/SCF} = subscript for initial co