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Reservoir Engineering 1 Course (2nd Ed.)
1. Reservoir CharacteristicsA. Reservoir Fluid Types According To Compressibility
B. Types of Flow Regimes
C. Types of Reservoir Geometries
D. Darcy’s Law Remarks
2. SS Regime for:A. Linear Flow and Tilted Reservoirs
B. Radial Flow of a. Incompressible and Slightly Compressible Fluids
b. Compressible Fluids
1. Multiple-Phase Flow
2. Pressure Disturbance in Reservoirs
3. USS Flow RegimeA. USS: Mathematical Formulation
4. Diffusivity EquationA. Solution of Diffusivity Equation
a. Ei- Function Solution
Horizontal Multiple-Phase Flow
When several fluid phases are flowing simultaneously in a horizontal porous system, the concept of the effective permeability to each phase and the associated physical properties must be used in Darcy’s equation
(The effective permeability can be expressed in terms of the relative and absolute permeability, ko=krok and etc.).
For a radial system, the generalized form of Darcy’s equation can be applied to each reservoir as follows:
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Multiple-Phase Flow Rate
Using the concept in Darcy’s equation and expressing the flow rate in standard conditions yield:Oil Phase
Water Phase
Gas Phase
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Flow Rate Ratios
In numerous petroleum-engineering calculations, it is convenient to express the flow rate of any phase as a ratio of other flowing phase.
Two important flow ratios are the “instantaneous” water-oil ratio (WOR) and “instantaneous” gas-oil ratio (GOR).
The generalized form of Darcy’s equation can be used to determine both flow ratios.
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Instantaneous Water-Oil Ratio
The water-oil ratio is defined as the ratio of the water flow rate to that of the oil.
Both rates are expressed in stock-tank barrels per day, WOR = water-oil ratio, STB/STB.
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Instantaneous Gas-Oil Ratio
The instantaneous GOR, as expressed in scf/STB, is defined as the total gas flow rate, i.e., free gas and solution gas, divided by the oil flow rate, or
GOR = “instantaneous” gas-oil ratio, scf/STB
Rs = gas solubility, scf/STB
Qg = free gas flow rate, scf/day
Qo = oil flow rate, STB/day
Bg = the gas formation volume factor, bbl/scf
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Pressure Disturbance for Shut-In Well
Figure shows a shut-in well that is centered in a homogeneous circular reservoir of radius re with a uniform pressure pi throughout the reservoir.
This initial reservoir condition represents the zero producing time.
If the well is allowed to flow at a constant flow rate of q, a pressure disturbance will be created at the sand face.
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Parameters Affecting Pressure DisturbanceThe pressure at the wellbore, i.e., pwf, will drop
instantaneously as the well is opened. The pressure disturbance will move away from the wellbore at a rate that is determined by:Permeability
Porosity
Fluid viscosity
Rock and fluid compressibilities
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Pressure Disturbance for Constant Rate ProductionFigure shows that at time t1, the pressure
disturbance has moved a distance r1 into the reservoir. Notice that the pressure disturbance radius is
continuously increasing with time.
This radius is commonly called radius of investigation and referred to as rinv.
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Infinite Acting Reservoir
It is also important to point out that as long as the radius of investigation has not reached the reservoir boundary, i.e., re, the reservoir will be acting as if it is infinite in size. During this time we say that the reservoir is infinite
acting because the outer drainage radius re can be mathematically infinite.
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Pressure Disturbance for Constant Bottom-Hole Flowing PressureA similar discussion to the above can be used to
describe a well that is producing at a constant bottom-hole flowing pressure.
Figure schematically illustrates the propagation of the radius of investigation with respect to time. At time t6, the pressure disturbance reaches the
boundary, i.e., rinv = re. This causes the pressure behavior to change.
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t6
Transient (USS) Flow
Based on the above discussion, the transient (unsteady-state) flow is defined as that time period during which the boundary has no effect on the pressure behavior in the reservoir and the reservoir will behave as its infinite in size. Section B shows that the
transient flow period occurs during the time interval 0 < t < tt for the constant flow rate scenario and
During the time period 0 < t < t4 during the constant pwf scenario as depicted by Section C.
Pressure disturbance as a function of timeFall 13 H. AlamiNia Reservoir Engineering 1 Course (2nd Ed.) 17
Steady-State vs. Unsteady-State Flow
Under the steady-state flowing condition, the same quantity of fluid enters the flow system as leaves it.
In unsteady-state flow condition, the flow rate into an element of volume of a porous media may not be the same as the flow rate out of that element. Accordingly, the fluid content of the porous medium
changes with time.
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Additional Variables in Unsteady-State FlowThe variables in unsteady-state flow additional to
those already used for steady-state flow, therefore, become:Time, t
Porosity, φ
Total compressibility, ct
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Mathematical Formulation of the Transient-FlowThe mathematical formulation of the transient-flow
equation is based on:Combining three independent equations and
(Continuity, Transport and Compressibility Equations)
A specifying set of boundary and initial conditions that constitute the unsteady-state equation.
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Basic Transient Flow Equation
a. Continuity EquationThe continuity equation is essentially a material balance
equation that accounts for every pound mass of fluid produced, injected, or remaining in the reservoir.
b. Transport EquationThe continuity equation is combined with the equation for
fluid motion (transport equation) to describe the fluid flow rate “in” and “out” of the reservoir. Basically, the transport equation is Darcy’s equation in its generalized differential form.
c. Compressibility EquationThe fluid compressibility equation (expressed in terms of
density or volume) is used in formulating the unsteady-state equation with the objective of describing the changes in the fluid volume as a function of pressure.
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Initial and Boundary Conditions
Initial and Boundary Conditions required to complete the formulation and the solution of the transient flow equation (diffusivity equation).The two boundary conditions are:
The formation produces at a constant rate into the wellbore.
There is no flow across the outer boundary and the reservoir behaves as if it were infinite in size, i.e., re = ∞.
The initial condition:The reservoir is at a uniform pressure when production begins,
i.e., time = 0.
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Continuity in Unsteady-State
The element has a width of dr and is located at a distance of r from the center of the well.
The porous element has a differential volume of dV.
According to the concept of the material-balance equation:
Mass entering volume element during interval Δt
- (minus)Mass leaving volume element
during interval Δt = (must be equal to)Rate of mass accumulation
during interval Δt
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Mass Entering and Leaving the Volume Element during Δt
Where ν = velocity of flowing fluid, ft/day
ρ = fluid density at (r + dr), lb/ft3
A = Area at (r + dr)
Δt = time interval, days
The area of element at the entering side is:
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Total Mass Accumulation during Δt
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Continuity Equation
Dividing the above equation by (2πrh) dr and simplifying, gives:
The Equation is called the continuity equation, and it provides the principle of conservation of mass in radial coordinates.
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Synergy of Transport Equation & Continuity EquationThe transport equation must be introduced into
the continuity equation to relate the fluid velocity to the pressure gradient within the control volume dV. Darcy’s Law is essentially the basic motion equation,
which states that the velocity is proportional to the pressure gradient (∂p/∂r).
Combining Equations results in:
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Right-Hand Side of the Equation
Expanding the right-hand side:
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General Partial Differential Equation
Finally, substituting the above relation into the Equation and the result into its previous Equation, gives:
The Equation is the general partial differential equation used to describe the flow of any fluid flowing in a radial direction in porous media.
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Transient Flow Equation Assumptions
In addition to the initial assumptions, Darcy’s equation has been added, which implies that the flow is laminar. Otherwise, the equation is not restricted to any type of
fluid and is equally valid for gases or liquids.
Compressible and slightly compressible fluids, however, must be treated separately in order to develop practical equations that can be used to describe the flow behavior of these two fluids.
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Gaining Diffusivity Equation
To simplify the general partial differential equation, assume that the permeability and viscosity are constant over pressure, time, and distance ranges. This leads to:
Expanding the above equation gives:
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Gaining Diffusivity Equation (Cont.)
Using the chain rule in the above relationship yields:
Dividing the above expression by the fluid density ρ gives
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Gaining Diffusivity Equation (Cont.)
Recalling that the compressibility of any fluid is related to its density by:
Define total compressibility, ct, as ct=c+cf, (the time t is expressed in days.)
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Diffusivity Equation
Diffusivity equation is one of the most important equations in petroleum engineering. The equation is particularly used in analysis well testing data
where the time t is commonly recorded in hours. The equation can be rewritten as:
Where k = permeability, mdr = radial position, ftp = pressure, psiact = total compressibility, psi−1t = time, hrsφ = porosity, fractionμ = viscosity, cp
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Total Compressibility in Diffusivity EquationWhen the reservoir contains more than one fluid,
total compressibility should be computed as ct = coSo + cwSw + cgSg + cf
Note that the introduction of ct into diffusivity equation does not make it applicable to multiphase flow; The use of ct, simply accounts for the compressibility of
any immobile fluids that may be in the reservoir with the fluid that is flowing.
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Diffusivity Constant
The term [0.000264 k/φμct] is called the diffusivity constant and is denoted by the symbol η, or:
The diffusivity equation can then be written in a more convenient form as:
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Diffusivity Equation Assumptions and LimitationsThe diffusivity equation is essentially designed to
determine the pressure as a function of time t and position r.
Summary of the assumptions and limitations used in diffusivity equation:1. Homogeneous and isotropic porous medium
2. Uniform thickness
3. Single phase flow
4. Laminar flow
5. Rock and fluid properties independent of pressure
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Flash Back: Laplace’s Equation for SS RegimeNotice that for a steady-state flow condition,
The pressure at any point in the reservoir is Constant and
Does not change with time, i.e., ∂p/∂t = 0,:
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Diffusivity Equation Solutions
Based on the boundary conditions imposed on diffusivity equation, there are two generalized solutions to the diffusivity equation:Constant-terminal-pressure solution
Constant-terminal-rate solution
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Constant-Terminal-Pressure Solution
The constant-terminal-pressure solution is designed to provide the cumulative flow at any particular time for a reservoir in which the pressure at one boundary of the reservoir is held constant. The pressure is known to be constant at some particular
radius and the solution is designed to provide the cumulative fluid movement across the specified radius (boundary).
This technique is frequently used in water influx calculations in gas and oil reservoirs.
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Application of Constant-Terminal-Rate SolutionThe constant-terminal-rate solution is an integral
part of most transient test analysis techniques, such as with drawdown and pressure buildup analyses. Most of these tests involve producing the well at a
constant flow rate and recording the flowing pressure as a function of time, i.e., p (rw, t).
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Constant-Terminal-Rate Solution
In the constant-rate solution to the radial diffusivity equation, the flow rate is considered to be constant at certain radius (usually wellbore radius) and
The pressure profile around that radius is determined as a function of time and position.
These are two commonly used forms of the constant-terminal-rate solution:The Ei-function solution
The dimensionless pressure pD solution
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The Ei-Function Solution Assumptions
Matthews and Russell (1967) proposed a solution to the diffusivity equation that is based on the following assumptions:Infinite acting reservoir, i.e., the reservoir is infinite in
size. (BC)
The well is producing at a constant flow rate. (BC)
The reservoir is at a uniform pressure, pi, when production begins. (IC)
The well, with a wellbore radius of rw, is centered in a cylindrical reservoir of radius re. (The Ei solution is commonly referred to as the line-source solution.)
No flow across the outer boundary, i.e., at re.
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Ei-Function Solution
Employing the above conditions, the authors presented their solution in the following form:
Where p (r, t) = pressure at radius r from the well after t hours
t = time, hrs
k = permeability, md
Qo = flow rate, STB/day
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Exponential Integral
The mathematical function, Ei, is called the exponential integral and is defined by:
For x > 10.9, the Ei (−x) can be considered zero for all practical reservoir engineering calculations.
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Values of the Ei-Function
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Exponential Integral Approximation
The exponential integral Ei can be approximated (with less than 0.25% error) by the following equation when its argument x is less than 0.01:Ei (−x) = ln (1.781x)
Where the argument x in this case is given by:
(t = time, hr, k = permeability, md)
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Behavior of the Pwf
When the parameter x in the Ei-function is less than 0.01, the log approximation can be used in the Ei-Function Solution to give:
For most of the transient flow calculations, engineers are primarily concerned with the behavior of the bottom-hole flowing pressure at the wellbore, i.e., r = rw
Where k = permeability, md, t = time, hr, ct = total compressibility, psi−1
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Pressure Profiles as a Function of Time
Most of the pressure loss occurs close to the wellbore; accordingly, near-wellbore conditions will exert the greatest influence on flow behavior.
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1. Ahmed, T. (2010). Reservoir engineering handbook (Gulf Professional Publishing). Chapter 6
1. Solutions of Diffusivity EquationA. pD Solution
B. Analytical Solution
2. USS(LT) Regime for Radial flow of SC Fluids: Finite-Radial Reservoir
3. Relation between pD and Ei
4. USS Regime for Radial Flow of C Fluids A. (Exact Method)
B. (P2 Approximation Method)
C. (P Approximation Method)
5. PSS regime Flow Constant