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Motivation

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In



Inputs & Outputs

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InputsOutputs

LaTeX Math Inline
bodyq_t

total sandface rate

LaTeX Math Inline
bodyp(t,x)

reservoir pressure

LaTeX Math Inline
bodyp_i

initial formation pressure

LaTeX Math Inline
bodyp_{wf}(t)

bottom-hole pressure

LaTeX Math Inline
bodyd

reservoir width



LaTeX Math Inline
body\sigma

transmissibility

LaTeX Math Inline
body\chi

diffusivity


Expand
titleDetailing


LaTeX Math Inline
body\sigma = \frac{k \, h}{\mu}

transmissibility

LaTeX Math Inline
body\chi = \frac{k}{\mu} \, \frac{1}{\phi \, c_t}

diffusivity

LaTeX Math Inline
bodyk

absolute permeability

LaTeX Math Inline
body\phi

porosity

LaTeX Math Inline
body\mu

fluid viscosity

LaTeX Math Inline
bodyc_t = c_r + c

total compressibility

LaTeX Math Inline
bodyc_r

pore compressibility

LaTeX Math Inline
bodyc

fluid compressibility




Physical Model

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Constant rate production

LaTeX Math Inline
bodyq_t = \rm const

Linear fluid flow

LaTeX Math Inline
bodyp(t, x)

Slightly compressible fluid flow

LaTeX Math Inline
bodyc_t(, p) = c_r +c = \rm const

Homogeneous reservoir

LaTeX Math Inline
bodyM(x, p)=M =\rm const

LaTeX Math Inline
body\phi(x, p)=\phi =\rm const

LaTeX Math Inline
bodyh(x)=h =\rm const

Infinite boundary

LaTeX Math Inline
bodyx \rightarrow \infty


Mathematical Model

Consider 

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LaTeX Math Inline
bodyh

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bodyd

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LaTeX Math Inline
bodyx

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LaTeX Math Inline
bodyx=0

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LaTeX Math Inline
bodyp_i

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LaTeX Math Inline
bodyt = 0

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LaTeX Math Inline
bodyq_t

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Диффузия давления описывается решением уравнения однофазного линейного течения в бесконечном однородном пласте


LaTeX Math Block
anchor52112
alignmentleft
\frac{\partial p}{\partial t}  = \chi \, \frac{d^2 p}{dx^2}

с начальным условием 



LaTeX Math Block
anchor88AEG
alignmentleft
p(t = 0, x) = p_i

и граничными условиями



LaTeX Math Block
anchor3MUX9
alignmentleft
p(t, x \rightarrow \infty ) = p_i



LaTeX Math Block
anchorEM415
alignmentleft
\frac{\partial p(t, x )}{\partial x} \bigg|_{x \rightarrow 0} = \frac{q_t}{\sigma \, d

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}

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LaTeX Math Inline
body\chi = \frac{k}{\mu} \, \frac{1}{\phi \, c_t}

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LaTeX Math Inline
bodyk

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LaTeX Math Inline
body\phi

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LaTeX Math Inline
bodyc_t = c_r + c

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LaTeX Math Inline
bodyc_r

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bodyc

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LaTeX Math Inline
body\mu

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LaTeX Math Block
anchorLB89P
alignmentleft
p(t,x) = p_i - \frac{q_t}{\sigma \, d} \bigg[ \sqrt{\frac{4 \chi t}{\pi}} \exp \bigg( -\frac{x^2}{4 \chi t} \bigg) - x \, \bigg[ 1- {\rm erf} \bigg(\frac{x}{\sqrt{4 \, \chi \, t}} \bigg) \bigg]  \bigg]

В стволе  скважины (

LaTeX Math Inline
bodyx=0
) динамика давления будет описываться следующей формулой:



LaTeX Math Block
anchorG38IV
alignmentleft
p_{wf}(t) = p_i - \frac{q_t}{\sigma \, d} \,  \sqrt{\frac{4 \chi t}{\pi}} 




Scope of Applicability

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Pressure Testing






Fig. 2. PTA Diagnostic plot for


Drawdown

Отсюда следует что динамическая депрессия на пласт растет пропорционально квадратному корню из времени

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