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



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q(l) = \frac{\rho_s \cdot q_0}{\rho}



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u(l) = \frac{\rho_s \cdot q_s}{\rho \cdot A}



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p(l=0) = p_s



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q(l=0) = q_s



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\rho(T_s, p_s) = \rho_s


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LaTeX Math Block
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-\frac{1}{c} \frac{d}{dl} \left( \frac{1}{\rho} \right) + \frac{\rho_s^2 q_s^2}{2A^2} \frac{d}{dl} \left( \frac{1}{\rho^2} \right) + \frac{\rho_s^2 q_s^2}{2A^2} \frac{f}{d} \left( \frac{1}{\rho^2} \right) - g \frac{dz}{dl} = 0

See derivation at 

derivation here
LaTeX Math Block Reference
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pageDerivation of Pressure Profile in Stationary Quasi-Isothermal Homogenous Pipe Flow @model
.

It does not give much benefit in computations comparing to 

LaTeX Math Block Reference
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 but it makes an easy path to some proxy models (like Slightly Compressible Fluid and  Ideal Gas). 


Approximations

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Incompressible pipe flow 

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body\rho(T, p) = \rho_s
with constant viscosity 
LaTeX Math Inline
body\mu(T, p) = \mu_s

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