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 Volumetric Flowrate in inclined pipe

LaTeX Math Inline
body\cos \theta \neq 0


LaTeX Math Block
anchorq_0G
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q_0^2 = \frac{2 d A^2 G}{f} \cdot \left[ 

1 + \frac{ (\rho/\rho_0)^2 -1}{1- (\rho_0/\rho)^{\frac{2}{n-1}} \cdot 
\exp \left( \frac{fL/d}{ n-1}  \right)}
\right]
LaTeX Math Block
anchorn
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n = \frac{f \, L^*}{2 \, d}
LaTeX Math Block
anchorL*
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L^* = \frac{1}{G \, c^* \, \rho^*}






Volumetric Flowrate in horizontal pipe

LaTeX Math Inline
body\cos \theta = 0


LaTeX Math Block
anchorq0_G0
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q_0^2 = \frac{A^2}{c^* \rho^*} \cdot \frac{1 - (\rho/\rho_0)^2}{2 \ln (\rho_0/\rho) + fL/d}





where

LaTeX Math Inlinebody--uriencoded--\displaystyle


LaTeX Math Block
anchorn
alignmentleft
n = \frac{f \, L^*}{2 \, d}



LaTeX Math Block
anchorL*
alignmentleft
L^* = \frac{1}{G \, c^* \, \rho^*}



LaTeX Math Block
anchorrho_rho0
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\rho_0/\rho = \
frac%7B1
frac{1+
c%5e
c^* p_
0%7D%7B1+c%5e* p%7D
0}{1+c^* p}


with the following asymptotes:

Low compressible fluids:

LaTeX Math Inline
body--uriencoded--c%5e* p \ll 1, \, \, c%5e* p_0 \ll 1

High compressible fluids:

LaTeX Math Inline
body--uriencoded--c%5e* p \gg 1, \, \, c%5e* p_0 \gg 1

LaTeX Math Inline
body--uriencoded--\displaystyle \rho_0/\rho = c%5e* \cdot (p_0-p)

 

LaTeX Math Inline
body\displaystyle \rho_0/\rho = p_0/p


Approximations

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LaTeX Math Inline
bodyn \geq 1
 (most practical cases)


LaTeX Math Block
anchorq0_G
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q_0^2 = \frac{A^2}{c^* \rho^*} \cdot \frac{1 - (\rho/\rho_0)^2 \cdot \exp \left(  -L/ L^* \right)}{2 \ln (\rho_0/\rho) + fL/d \cdot (1- \exp \left(  - L/ L^* \right))/(L/L^*)}







LaTeX Math Block
anchorq0_G
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\dot m^2 = \frac{A^2}{c^* \rho^*} \cdot \frac{\rho_0^2 - \rho^2 \cdot \exp \left(  -L/ L^* \right)}{2 \ln (\rho_0/\rho) + fL/d \cdot (1- \exp \left(  - L/ L^* \right))/(L/L^*)}







LaTeX Math Block
anchorstatic
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\rho = \rho_0 \, \exp (c^* \rho^* \, G \, L) \cdot \sqrt{ 1 - \frac{f}{2d} \cdot \frac{j_m^2}{G \, \rho_0^2} \cdot ( 1 - \exp(-2 \, c^* \rho^* \, G \, L))}



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anchorstatic
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p(L) = \frac{1}{c^*} \cdot \left[ 
-1 + (1+c^* p_0) \cdot \exp (c^* \rho^* \, G \, L) \cdot \sqrt{  1 - \frac{f}{2d}  \cdot \frac{j_m^2}{G \rho_0^2} \cdot \big(1 - \exp (-2 \, c^* \rho^* \, G \, L) \big) }
\right]


Pressure Profile in GC-proxy static fluid column @model

LaTeX Math Inline
body\dot m = 0, \, q_0 = 0
 (no flow)


LaTeX Math Block
anchorstatic
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\rho = \rho_0 \, \exp (L/L^*)



LaTeX Math Block
anchorstatic
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p(L) = \frac{-1 + (1+c^* \, p_0) \cdot \exp(L/L^*)}{c^*}   


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