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The multiphase wellbore flow in hydrodynamic and thermodynamic equilibrium is defined by the following set of 1D equations: 

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LaTeX Math Inline
bodym

indicates a mixture of fluid phases

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body\alpha = \{w,o,g \}

water, oil, gas phase indicator

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bodyl

measure length along wellbore trajectory

Image Modified

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bodyu_\alpha(l)

in-situ velocity of

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body\alpha
-phase fluid flow

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body\rho_\alpha(l)

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body\alpha
-phase fluid density

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body\rho_m(l)
 

cross-sectional average fluid density

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body \theta(l)

wellbore trajectory inclination to horizon

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bodyd(l)

cross-sectional average pipe flow diameter

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bodyA(l)

in-situ cross-sectional area

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bodyA(l) = 0.25 \, \pi \, d^2(l)

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bodyf(l)

Darci flow friction coefficient

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body\nu_\alpha

kinematic viscosity of

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body\alpha
-phase

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bodyT_\alpha(l)

temperature of

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body\alpha
-phase fluid flowing from reservoir into a wellbore


Equations 

mathblock-
LaTeX Math Block Reference
anchorMatBal
 – 
mathblock-ref
anchorMatBal
 – 
LaTeX Math Block Reference
anchordivT
 define a closed set of 3 scalar equations on 3 unknowns: pressure 
LaTeX Math Inline
bodyp(l)
, temperature 
LaTeX Math Inline
bodyT(l)
 and  fluid velocity 
LaTeX Math Inline
bodyu(l)
 .

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This usually takes effect in the wellbore during the first minutes or hours after changing the well flow regime (as a consequence of choke/pump operation). 


The multiphase fluid density 

LaTeX Math Inline
body\rho_m
 is defined by exact formula:

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anchor1
alignmentleft
\rho_m = sum_\alpha \rho_\alpha s_\alpha

where 

LaTeX Math Inline
bodys_\alpha
 – fractional volumes of
LaTeX Math Inline
body\alpha
-phase which are naturally constraint by:

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body\sum_\alpha s_\alpha = s_w + s_o + s_g = 1
.

The 

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bodys_\alpha
 can be also expressed as fraction of the total flowing cross-sectional area 
LaTeX Math Inline
bodyA
 occupied by 
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body\alpha
-phase:

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anchor1
alignmentleft
s_\alpha = \frac{A_\alpha}{A}


The term 

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body(\rho \,c_p)_m
 defines mass-specific heat capacity of the multiphase mixture and defined by exact formula:

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anchorrho_cp
alignmentleft
(\rho \,c_p)_m = \sum_\alpha \rho_\alpha c_\alpha s_\alpha


The in-situ velocities 

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bodyu_\alpha
 are usually expressed via the macroscopic flow velocity 
LaTeX Math Inline
bodyu_m
 using the 


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titleDerivation


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anchordivT
alignmentleft
(\rho \,c_{pt})_p \frac{\partial T}{\partial t} 
 
-  \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ \eta_{s \alpha} \ \frac{\partial P_\alpha}{\partial t}  
 
+  \sum_{a = \{w,o,g \}} \rho_\alpha \ c_{p \alpha} \ u_\alpha \frac{\partial T}{\partial l}
 \  =   \   \frac{\delta E_H}{ \delta V \delta t}


Equation 

LaTeX Math Block Reference
anchordivT
  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 

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body\frac{\delta E_H}{ \delta V \delta t}
 defines the speed of change of  heat energy 
LaTeX Math Inline
bodyE_H
 volumetric density due to the inflow from formation into the wellbore.




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