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Motivation

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One of the key challenges in Pipe Flow Dynamics is to predict the along-hole temperature distribution during the stationary fluid transport.

In many practical cases the temperature distribution for the stationary fluid flow can be approximated by homogenous fluid flow model.

Pipeline Flow Temperature Model is addressing this problem with account of the varying pipeline trajectory, pipeline schematic and heat transfer with the matter around pipeline.


In many practical cases the along-hole 
temperature distribution during the stationary fluid flow can be approximated by homogenous fluid flow model.

Inputs & Outputs


Outputs

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LaTeX Math Inline
bodyT(t, l)

along-pipe temperature distribution and evolution in time


Inputs

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InputsOutputspipeline trajectory

LaTeX Math Inline
body--uriencoded--%7B\bf r%7D(l)

LaTeX Math Inline
body

{

--uriencoded--%7B\bf

r} = {\bf r}

r%7D(l) = \

{

%7B x(l), \, y(l), \, z(l) \

}along-pipe temperature

%7D

LaTeX Math Inline
body\rho(T

(t

,

lpipeline cross-section area 

p)

distribution and evolution in time

LaTeX Math Inline
bodyA(l)

fluid density

LaTeX Math Inline
body\

rho

mu(T, p)

and

LaTeX Math Inline
body

\mu(T, p)inflow temperature 

T_0(t)

intake temperature

LaTeX Math Inline
bodyT_

0

{e0}(

t

l)

, inflow pressure 
initial temperature of the medium around the pipeline

LaTeX Math Inline
bodyp_0

, inflow rate 
intake pressure

LaTeX Math Inline
body

q_0initial temperature   LaTeX Math InlinebodyT_g

c_p(l)

specific heat capacity of the medium around
the
pipeline
specific heat capacity

LaTeX Math Inline
body

c_p(l)thermal conductivity 

q_0

intake flowrate

LaTeX Math Inline
body\lambda_e(l)

  of
thermal conductivity of the medium around pipeline
heat transfer coefficient 

LaTeX Math Inline
bodyU(l)

 based

heat transfer coefficient  based on pipeline schematic




Assumptions

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Equations

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LaTeX Math Block
anchorWIFEB
alignmentleft
\rho \, c \, \frac{\partial T}{\partial t} = \frac{d}{dl} \, \bigg( \lambda \, \frac{dT}{dl} \bigg)  - \rho \, c \, v \, \frac{dT}{dl} + \frac{U}{r_w} \cdot \big( T_e(t, l, r_w) - T \big)



LaTeX Math Block
anchorD11O7
alignmentleft
\rho_e \, c_e \, \frac{\partial T_e}{\partial t} = \nabla ( \lambda_e \nabla T_e)



LaTeX Math Block
anchorUSVI3
alignmentleft
T(t=0, l) = T_{e0}(l)



LaTeX Math Block
anchorRVUHY
alignmentleft
T_e(t=0, l, r) = T_{e0}(l)



LaTeX Math Block
anchorPSFGA
alignmentleft
T(t, l=0) = T_0(t)



LaTeX Math Block
anchor6QNDD
alignmentleft
T_e(t, l, r \rightarrow \infty) = T_{e0}(l)



LaTeX Math Block
anchorU
alignmentleft
2 \pi \, \lambda_e \, r_w \, \frac{\partial T_e}{\partial r} \, \bigg|_{r=r_w} = 2 \pi \, r_f \, U \
,
cdot \
bigg
left( T_e \, \bigg|_{r=r_w} - T \
bigg
right)

(see Derivation of Stationary Isothermal Homogenous Pipe Flow Pressure Profile @model )

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Approximations

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See also

Show If
grouparax


Panel
bgColorpapayawhip
titleARAX

PipeFlow.xls

Температурный профиль однородного потока жидкости в трубе



References

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https://en.wikipedia.org/wiki/Darcy_friction_factor_formulae


https://neutrium.net/fluid_flow/pressure-loss-in-pipe/ 

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