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LaTeX Math Block
anchordivW1
alignmentleft
\partial_t \bigg [  \phi \ \rho_W  \bigg ]  + \nabla \bigg (     \rho_w \ \mathbf{u}_w     \bigg )      =  q_{mW}(\mathbf{r}) 
LaTeX Math Block
anchordivO1
alignmentleft
\partial_t \bigg [  \phi \ \rho_O \bigg ]  + \nabla \bigg (   {\tilde m}_{Oo} \ \rho_o \ \mathbf{u}_o 

+  {\tilde m}_{Og} \ \rho_{g} \  \mathbf{u}_g    \bigg )       =  q_{mO}(\mathbf{r})
LaTeX Math Block
anchordivG1
alignmentleft
\partial_t \bigg [  \phi \ \rho_G  \bigg ]  +  \nabla  \bigg (  {\tilde m}_{Go} \ \rho_{o} \ \mathbf{u}_o

+    {\tilde m}_{Gg} \ \rho_g \ \mathbf{u}_g  \bigg )     =  q_{mG}(\mathbf{r}) 
Column
width20%
LaTeX Math Block
anchorDarcyW1
alignmentleft
\mathbf{u}_w = - k_a \ \frac{k_{rw}(s_w, s_g)}{\mu_w} \ ( \nabla P_w - \rho_w  \mathbf{g} )
LaTeX Math Block
anchorDarcyO1
alignmentleft
\mathbf{u}_o = - k_a \ \frac{k_{ro}(s_w, s_g)}{\mu_o} \ ( \nabla P_o - \rho_o   \mathbf{g} )
LaTeX Math Block
anchorDarcyG1
alignmentleft
\mathbf{u}_g = - k_a \ \frac{k_{rg}(s_w, s_g)}{\mu_g} \ ( \nabla P_g - \rho_g  \mathbf{g} )
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width20%
LaTeX Math Block
anchorCapilarOW1
alignmentleft
P_o - P_w = P_{cow}(s_w)
LaTeX Math Block
anchorCapilarOG1
alignmentleft
P_o - P_g = P_{cog}(s_g)
LaTeX Math Block
anchorswsosg1
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s_w + s_o + s_g = 1
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width30%



Подставляя значения плотностей и массовых долей компонент  Substituting the values of mass densities and mass shares of fluid components (см. "Модель Летучей Нефти") и разделив каждое уравнение на плотность соотвествующей компоненты в стандартных условиях, получаем наиболее популярную форму записи уравнений движения Летучей НефтиVolatile Oil Model") and dividing each equation by density of corresponding component in standard conditions one gets the most popular form of Volatile Oil flow equations:

Section
Column
width25%
LaTeX Math Block
anchordivW
alignmentleft
\partial_t \bigg [  \phi \ \bigg (  \frac{s_w}{B_w}  \bigg ) \bigg ]  +  \nabla \bigg (     \frac{1}{B_w} \ \mathbf{u}_w  \bigg )      = 
q_W (\mathbf{r})
LaTeX Math Block
anchordivO
alignmentleft
\partial_t \bigg [  \phi \ \bigg (  \frac{s_o}{B_o} + \frac{R_v \ s_g}

{B_g}  \bigg ) \bigg ]  +  \nabla \bigg (     \frac{1}{B_o} \ \mathbf{u}_o 

+    \frac{R_v}{B_g} \   \mathbf{u}_g   \bigg )       = q_O(\mathbf{r})
LaTeX Math Block
anchordivG
alignmentleft
\partial_t \bigg [  \phi \ \bigg (  \frac{s_g}{B_g} + \frac{R_s \ s_o}

{B_o}  \bigg ) \bigg ]  +  \nabla  \bigg (     \frac{1}{B_g} \ \mathbf{u}_g

+    \frac{R_s}{B_o} \ \mathbf{u}_o  \bigg )     = q_G (\mathbf{r})
Column
width20%
LaTeX Math Block
anchorDarcyW
alignmentleft
\mathbf{u}_w = - k_a \ \frac{k_{rw}(s_w, s_g)}{\mu_w} \ ( \nabla  P_w - \rho_w \  \mathbf{g} )
LaTeX Math Block
anchorDarcyO
alignmentleft
\mathbf{u}_o = - k_a \ \frac{k_{ro}(s_w, s_g)}{\mu_o} \ ( \nabla P_o - \rho_o \ \mathbf{g} )
LaTeX Math Block
anchorDarcyG
alignmentleft
\mathbf{u}_g = - k_a \ \frac{k_{rg}(s_w, s_g)}{\mu_g} \ ( \nabla P_g - \rho_g \ \mathbf{g} )
Column
width20%
LaTeX Math Block
anchorCapilarOW
alignmentleft
P_o - P_w = P_{cow}(s_w)
LaTeX Math Block
anchorCapilarOG
alignmentleft
P_o - P_g = P_{cog}(s_g)
LaTeX Math Block
anchorswsosg
alignmentleft
s_w + s_o + s_g = 1
Column
width30%



Equations В уравнениях 

LaTeX Math Block Reference
anchordivW
 – 
LaTeX Math Block Reference
anchordivG
 правые части равны нулю во всем объеме пласта за исключением контакта скважин с пластом, который описывается моделью скважины (см. ниже).

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 suggest no sources of flow in the right side except the contacts between wells and reservroir which is specified by well models as boundary conditions (see below).


Initial Conditions

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Начальное условие по температуре задается распределением температурного поля:

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