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Definition



Mathematical model of multiphase wellbore flow predicts the temperature, pressure and flow speed distribution along the wellbore trajectory with account for:

  • tubing head pressure which is set by gathering system or injection pump

  • wellbore design

  • pump characterisits

  • fluid friction with tubing /casing walls

  • interfacial phase slippage

  • heat exchange between wellbore fluid and surrounding rocks


Flow Model




(1) (\rho \,c_{pt})_p \frac{\partial T}{\partial t}   - \ \phi \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ \eta_{s \alpha} \ \frac{\partial P_\alpha}{\partial t}   + \bigg( \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ \epsilon_\alpha \ \mathbf{u}_\alpha \bigg) \nabla P   + \bigg( \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ \mathbf{u}_\alpha \bigg) \ \nabla T   - \nabla (\lambda_t \nabla T) = \frac{\delta E_H}{ \delta V \delta t}

The disambiguation fo the properties in the above equation is brought in The list of dynamic flow properties and model parameters.


Equations 

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 – 
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 define the continuity of the fluid components flow or equivalently represent the mass conservation of each mass component  \{ m_W, \ m_O, \ m_G \} during its transportation in space. 

Equations 

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 – 
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 define the motion dynamics of each phase, represented as linear correlation between phase flow speed   \bar u_\alpha and partial pressure gradient of this phase  \bar \nabla P_\alpha .


Equation  (1)  defines the heat flow continuity or equivalently represents heat conservation due to heat conduction and convection with account for adiabatic and Joule–Thomson throttling effect.

The term  \frac{\delta E_H}{ \delta V \delta t}  defines the speed of change of  heat energy  E_H volumetric density due to the inflow from formation into the wellbore.


The term  \bigg( \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ \mathbf{u}_\alpha \bigg) \ \bar \nabla T  represents heat convection defined by the wellbore mass flow. 

The term  \bigg( \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ \epsilon_\alpha \ \mathbf{u}_\alpha \bigg) \bar \nabla P represents the heating/cooling effect of the multiphase flow through the porous media. This effect is the most significant with light oils and gases.


The term  \ \phi \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ \eta_{s \alpha} \ \frac{\partial P_\alpha}{\partial t} represents the heating/cooling effect of the fast adiabatic pressure change. This usually takes effect in and around the wellbore during the first minutes or hours after changing the well flow regime (as a consequence of choke/pump operation). This effect is absent in stationary flow and negligible during the quasi-stationary flow and usually not modeled in conventional monthly-based flow simulations. 


The set 


Stationary Flow Model



Stationary wellbore flow is defined as the flow with constant pressure and temperature:   \frac{\partial T}{\partial t} = 0 and  \frac{\partial P}{\partial t} = 0 .

This happens during the long-term (usually hours & days & weeks) production/injection or long-term (usually hours & days & weeks)  shut-in.


The temperature dynamic equation  (1) is going to be:

(2) \bigg( \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ \mathbf{u}_\alpha \bigg) \ \nabla T   = \frac{\delta E_H}{ \delta V \delta t}

and its discrete computational scheme will be:

(3) \bigg( \sum_{a = \{w,o,g \}} \rho_\alpha^{k-1} \ c_{p \alpha}^{k-1} \ q_\alpha^{k-1} \bigg) T^{k-1} - \bigg( \sum_{a = \{w,o,g \}} \rho_\alpha^k \ c_{p \alpha}^k \ q_\alpha^k \bigg) T^k = \sum_{a = \{w,o,g \}} \rho_\alpha^k \ c_{p \alpha}^k \ (q_\alpha^{k-1} - q_\alpha^k) \, (T_r^k + \epsilon_\alpha^k \delta p^k )

where  \delta p^k = p_e^k - p_{wf}^k is drawdown,  p_e^k – formation pressure in  k-th grid layer,  p_{wf}^k – bottom-hole pressure across  k-th grid layer, T_r^k – remote reservoir temperature of   k-th grid layer.

The l-axis is pointing downward along hole with  (k-1)-th grid layer sitting above the k-th grid layer.

If the flowrate is not vanishing during the stationary lift ( \sum_{a = \{w,o,g \}} |q_\alpha^{k-1}| > 0) then   T^{k-1} can be calculated iteratively from previous values of the wellbore temperature  T^k as:

(4) T^{k-1} = \frac{\bigg( \sum_{a = \{w,o,g \}} \rho_\alpha^k \ c_{p \alpha}^k \ q_\alpha^k \bigg) T^k + \sum_{a = \{w,o,g \}} \rho_\alpha^k \ c_{p \alpha}^k \ (q_\alpha^{k-1} - q_\alpha^k) \, (T_r^k + \epsilon_\alpha^k \delta p^k )}{\bigg( \sum_{a = \{w,o,g \}} \rho_\alpha^{k-1} \ c_{p \alpha}^{k-1} \ q_\alpha^{k-1} \bigg) }




The wellbore fluid velocity  u_\alpha can be expressed thorugh the volumetric flow profile  q_\alpha and tubing/casing cross-section area  \pi r_f^2 as:

(5) u_\alpha = \frac{q_\alpha}{\pi r_f^2}

so that 

(6) \bigg( \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ \mathbf{u}_\alpha \bigg) \ \nabla T = \frac{\delta E_H}{ \delta V \delta t}



References



Beggs, H. D. and Brill, J. P.: "A Study of Two-Phase Flow in Inclined Pipes," J. Pet. Tech., May (1973), 607-617




The list of dynamic flow properties and model parameters



(t,x,y,z)

time and space corrdinates ,

z -axis is orientated towards the Earth centre,

(x,y) define transversal plane to the z -axis

\mathbf{r} = (x, \ y, \ z)

position vector at which the flow equations are set

q_{mW} = \frac{d m_W}{dt}

speed of water-component mass change in wellbore draining points

q_{mO} = \frac{d m_O}{dt}

speed of oil-component mass change in wellbore draining points

q_{mG} = \frac{d m_G}{dt}

speed of gas-component mass change in wellbore draining points

q_W = \frac{1}{\rho_W^{\LARGE \circ}} \frac{d m_W}{dt} = \frac{d V_{Ww}^{\LARGE \circ}}{dt} = \frac{1}{B_w} q_w

volumetric water-component flow rate in wellbore draining points recalculated to standard surface conditions

q_O = \frac{1}{\rho_O^{\LARGE \circ}} \frac{d m_O}{dt} = \frac{d V_{Oo}^{\LARGE \circ}}{dt} + \frac{d V_{Og}^{\LARGE \circ}}{dt} = \frac{1}{B_o} q_o + \frac{R_v}{B_g} q_g

volumetric oil-component flow rate in wellbore draining points recalculated to standard surface conditions

q_G = \frac{1}{\rho_G^{\LARGE \circ}} \frac{d m_G}{dt} = \frac{d V_{Gg}^{\LARGE \circ}}{dt} + \frac{d V_{Go}^{\LARGE \circ}}{dt} = \frac{1}{B_g} q_g + \frac{R_s}{B_o} q_o

volumetric gas-component flow rate in wellbore draining points recalculated to standard surface conditions

q_w = \frac{d V_w}{dt}

volumetric water-phase flow rate in wellbore draining points

q_o = \frac{d V_o}{dt}

volumetric oil-phase flow rate in wellbore draining points

q_g = \frac{d V_g}{dt}

volumetric gas-phase flow rate in wellbore draining points

q^S_W =\frac{dV_{Ww}^S}{dt}

total well volumetric water-component flow rate

q^S_O = \frac{d (V_{Oo}^S + V_{Og}^S )}{dt}

total well volumetric oil-component flow rate

q^S_G = \frac{d (V_{Gg}^S + V_{Go}^S )}{dt}

total well volumetric gas-component flow rate

q^S_L = q^S_W + q^S_O

total well volumetric liquid-component flow rate

P_w = P_w (t, \vec r)

water-phase pressure pressure distribution and dynamics

P_o = P_o (t, \vec r)

oil-phase pressure pressure distribution and dynamics

P_g = P_g (t, \vec r)

gas-phase pressure pressure distribution and dynamics

\vec u_w = \vec u_w (t, \vec r)

water-phase flow speed distribution and dynamics

\vec u_o = \vec u_o (t, \vec r)

oil-phase flow speed distribution and dynamics

\vec u_g = \vec u_g (t, \vec r)

gas-phase flow speed distribution and dynamics

P_{cow} = P_{cow} (s_w)

capillary pressure at the oil-water phase contact as function of water saturation


P_{cog} = P_{cog} (s_ g)

capillary pressure at the oil-gas phase contact as function of gas saturation

k_{rw} = k_{rw}(s_w, \ s_g)

relative formation permeability to water flow as function of water and gas saturation

k_{ro} = k_{ro}(s_w, \ s_g)

relative formation permeability to oil flow as function of water and gas saturation

k_{rg} = k_{rg}(s_w, \ s_g)

relative formation permeability to gas flow as function of water and gas saturation

\phi = \phi(P)

porosity as function of formation pressure

k_a = k_a(P)

absolute formation permeability to air

\vec g = (0, \ 0, \ g)

gravitational acceleration vector

g = 9.81 \ m/s^2

gravitational acceleration constant

\rho_\alpha(P,T)

mass density of \alpha-phase fluid

\mu_\alpha(P,T)

viscosity of \alpha-phase fluid

\lambda_t(P,T,s_w, s_o, s_g)

effective thermal conductivity of the rocks with account for multiphase fluid saturation

\lambda_r(P,T)

rock matrix thermal conductivity

\lambda_\alpha(P,T)

thermal conductivity of \alpha-phase fluid

\rho_r(P,T)

rock matrix mass density

\eta_{s \alpha}(P,T)

differential adiabatic coefficient of \alpha-phase fluid

c_{pr}(P,T)

specific isobaric heat capacity of the rock matrix

c_{p\alpha}(P,T)

specific isobaric heat capacity of \alpha-phase fluid

\epsilon_\alpha (P, T)

differential Joule–Thomson coefficient of \alpha-phase fluid

дифференциальный коэффициент Джоуля-Томсона фазы  \alpha

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