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LaTeX Math Block
anchor9QRCZPP
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\bigg( 1 -  \frac{c(p) \, \rho_0^2 \, q_0^2}{A^2}   \bigg )  \frac{dp}{dl} = \rho(p) \, g \, \frac{dz}{dl}  - \frac{\rho_0^2 \, q_0^2 }{2 A^2 d} \frac{f({\rm Re}, \, \epsilon)}{\rho(p)}



LaTeX Math Block
anchor1
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u(l) = \frac{\rho_0 \cdot q_0}{\rho(p) \cdot A}



LaTeX Math Block
anchor1
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q(l) = \frac{\rho_0 \cdot q_0}{\rho(p)}


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Pressure profilePressure gradient profileFluid velocityFluid rate


LaTeX Math Block
anchorH8MPTPPconst
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p(l) = p_0 + \rho \, g \, z(l) - \frac{\rho_0 \, q_0^2 }{2 A^2 d} \, f_0 \, l



LaTeX Math Block
anchorIFPGP
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\frac{dp}{dl} = \rho \, g \cos \theta(l) - \frac{\rho_0 \, q_0^2 }{2 A^2 d} \, f_0 



LaTeX Math Block
anchor1
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u(l) = u_0 = \frac{q_0}{A} = \rm const



LaTeX Math Block
anchor1
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q(l) =q_0 = \rm const


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Expand
titleDerivation


Panel
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Incompressible fluid 

LaTeX Math Inline
body\rho(p) = \rho_0 = \rm const
 means that compressibility vanishes 
LaTeX Math Inline
bodyc(p) = 0
 and fluid velocity is going to be constant along the pipeline trajectory 
LaTeX Math Inline
body--uriencoded--u(l) = u_0 = \frac%7Bq_0%7D%7BA%7D = \rm const
.

For the constant viscosity 

LaTeX Math Inline
body\mu(T, p) = \mu_0 = \rm const
 along the pipeline trajectory the Reynolds number 
LaTeX Math Inline
body--uriencoded--\displaystyle %7B\rm Re%7D = \frac%7B4 \rho_0 q_0%7D%7B\pi d%7D \frac%7B1%7D%7B\mu_0%7D = \rm const
 and Darcy friction factor 
LaTeX Math Inline
body--uriencoded--f(%7B\rm Re%7D, \, \epsilon) = f_0 = \rm const
 are going to be constant along the pipeline trajectory.

Equation 

LaTeX Math Block Reference
anchorPP
 becomes:

LaTeX Math Block
anchorPP
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\frac{dp}{dl} = \rho_0 \, g \, \frac{dz}{dl}  - \frac{\rho_0 \, q_0^2 }{2 A^2 d} f_0

and can be explicitly integrated leading to 

LaTeX Math Block Reference
anchorPPconst
.



The first term in 

LaTeX Math Block Reference
anchorIFPGP
defines the hydrostatic column of static fluid while the last term defines the friction losses under fluid movement:

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