Entrance and Fully Developed Regions |
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Recall that Reynolds number (Re = ρVD/μ)
can be used to classify if a flow is
laminar or turbulent. The type of flow not only depends
on its velocity (V), but also its density (ρ), viscosity (μ)
and length scale (diameter D). For pipe flow, the flow is laminar
when Re < 2,100, and it is turbulent when Re > 4,000. The flow
is referred to as transition flow when Reynolds number is in between
2,100 and 4,000.
When a fluid enters a pipe, viscous effects due to the pipe wall will
develop. The region where viscous effects are important is referred to as the
boundary layer. The velocity profile, as shown
in the figure, will also vary due to the growth of this boundary layer. When
the velocity profile reaches a constant (i.e., velocity profile no longer
changes along the pipe), the flow is said to be fully developed. The length required for the flow to reach fully developed conditions is called
the entrance length (Le), and it can be determined from the following empirical relations:
For laminar flow: Le/D = 0.06Re
For turbulent flow: Le/D = 4.4(Re)1/6 |
Parabolic Velocity Profile |
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Fully developed laminar pipe flow is generally known as Hagan-Poiseuille
flow. The velocity profile of a fully developed
laminar horizontal circular pipe flow can be derived from the
Navier-Stokes equations and is given by
The derivation process is similar to that of obtaining the velocity distributions for
flow between parallel plates, hence the derivation details
are omitted here for brevity. The assumptions used in the derivation are as follows:
(a)
The fluid is incompressible (Dρ/Dt = 0).
(b) The flow is steady ().
(c) The flow is in the z-direction only
(vr =
vθ =
0).
(d) The flow is axisymmetric ().
The obtained velocity
profile is parabolic, and it closely resembles the velocity profile obtained for
flow between parallel plates.
The volumetric flow rate (Q) can then be determined by integrating the
velocity profile over the cross-sectional area to yield:
where Δp is the pressure drop across a pipe
length of L and radius R. The above equation is known
as Hagan-Poiseuille's law. |
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From another discussion, it is known that Bernoulli's equation can be applied along a streamline to analyze steady,
incompressible and inviscid
flow. Most flows in real practice, however, are viscous, and hence losses
due to viscous dissipation (friction) are unavoidable. To analyze
flow in a viscous pipe, Bernoulli's equation can be modified and applied
to two sections of the pipe flow:
where p is the static pressure, V is the average velocity, z is the
elevation, and hL accounts
for the head loss due to friction between section (1) and (2). |
Moody Chart
Table: Typical Values of
Surface Roughness
Pipe (New) |
Surface
Roughness, ε |
ft (10-3) |
mm |
Riveted Steel |
3 - 30 |
0.9-9.0 |
Concrete |
1 - 10 |
0.3-3.0 |
Wood Stave |
0.6 - 3 |
0.18-0.9 |
Cast Iron |
0.85 |
0.26 |
Galvanized Iron |
0.5 |
0.15 |
Commercial Steel
or Wrought Iron |
0.15 |
0.046 |
Drawn Tubing |
0.005 |
0.0015 |
PVC/Plastic
(smooth) |
0.005-
0.023 |
0.0015-
0.007 |
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Based on dimensional analysis, the head loss over the length of the pipe is given by
where f is an empirical friction factor. The above expression is also called the Darcy-Weisbach equation. The friction factor is a function of the Reynolds number (Re) and relative roughness of the pipe (ε/D) as shown in the Moody chart to the left. Typical values of the surface roughness of pipe (ε) are summarized in the table.
The Moody Chart actually has three main regions or sections. The first region is for laminar flow for when Re is approximately less than 2100. Then the friction factor is a a direct function of the Re, or
For laminar flow: f = 64/Re
The region between laminar and completely turbulent. This is when the chart is required. First determine the relative roughness number, ε/D, and then determine Re. Using these two numbers and the Moody Chart, estimate the friction factor, f.
In general, the friction factor is a function of Re and ε/D for turbulent flow. However, when Re is very high (completely turbulent flow), the friction factor becomes independent of Re, and it depends on the relative roughness only. This is the third region and as an alternative to determining the friction factor for turbulent flow from the Moody chart, it can be calculated using the correlation provided by Colebrook**,
For turbulent flow:
Note that iteration is needed to obtain f since the above equation is
not expressed explicitly in f.
[**Reference: Colebrook, C. F., "Turbulent
Flow in Pipes with Particular Reference to the Transition between the
Smooth and Rough Pipe Laws," Journal of the Institute of Civil
Engineering London, Vol. 11, pp. 133-156, 1939.] |