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Basics of Fluid Mechanics, 2014a

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548 CHAPTER 13. MULTI–PHASE FLOW<br />

13.7.1 Pressure Loss Components<br />

In a tube flowing upward in incline angle θ, the pressure loss is affected by friction loss,<br />

acceleration, and body force(gravitation). These losses are non-linear and depend on<br />

each other. For example, the gravitation pressure loss reduce the pressure and thus the<br />

density must change and hence, acceleration must occur. However, for small distances<br />

(dx) and some situations, this dependency can be neglected. In that case, from equation<br />

(13.25), the total pressure loss can be written as<br />

friction acceleration gravity<br />

{ }} { { }} { { }} {<br />

dP<br />

dx = dP<br />

dP<br />

dx ∣ +<br />

dP<br />

f<br />

dx ∣ +<br />

a<br />

dx ∣ (13.27)<br />

g<br />

Every part <strong>of</strong> the total pressure loss will be discussed in the following section.<br />

13.7.1.1 Friction Pressure Loss<br />

The frictional pressure loss for a conduit can be calculated as<br />

− dP<br />

dx ∣ = S<br />

f<br />

A τ w (13.28)<br />

Where S is the perimeter <strong>of</strong> the fluid. For calculating the frictional pressure loss in the<br />

pipe is<br />

− dP<br />

dx ∣ = 4 τ w<br />

(13.29)<br />

f<br />

D<br />

The wall shear stress can be estimated by<br />

τ w = f ρ 2<br />

m U m<br />

(13.30)<br />

2<br />

The friction factor is measured for a single phase flow where the average velocity is<br />

directly related to the wall shear stress. There is not available experimental data for<br />

the relationship <strong>of</strong> the averaged velocity <strong>of</strong> the two (or more) phases and wall shear<br />

stress. In fact, this friction factor was not measured for the “averaged” viscosity <strong>of</strong> the<br />

two phase flow. Yet, since there isn’t anything better, the experimental data that was<br />

developed and measured for single flow is used.<br />

The friction factor is obtained by using the correlation<br />

( ) −n ρm U m D<br />

f = C<br />

(13.31)<br />

μ m<br />

Where C and n are constants which depend on the flow regimes (turbulent or laminar<br />

flow). For laminar flow C =16and n =1. For turbulent flow C =0.079 and n =0.25.

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