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230 Chapter 5 ■ Finite Control Volume Analysis<br />

where<br />

is the heat transfer rate per mass flowrate, or heat transfer per unit mass. Note that Eq. 5.73 involves<br />

energy per unit mass and is applicable to one-dimensional flow of a single stream of <strong>fluid</strong><br />

between two sections or flow along a streamline between two sections.<br />

If the steady, incompressible flow we are considering also involves negligible viscous effects<br />

1frictionless flow2, then the Bernoulli equation, Eq. 3.7, can be used to describe what happens between<br />

two sections in the flow as<br />

p out rV 2 out<br />

2<br />

q net<br />

in<br />

Q# net in<br />

m #<br />

gz out p in rV 2 in<br />

2 gz in<br />

(5.74)<br />

where g rg is the specific weight of the <strong>fluid</strong>. To get Eq. 5.74 in terms of energy per unit mass, so<br />

that it can be compared directly with Eq. 5.73, we divide Eq. 5.74 by density, r, and obtain<br />

Minimizing loss is<br />

the central goal of<br />

<strong>fluid</strong> mechanical<br />

design.<br />

p out<br />

r V 2 out<br />

2 gz out p in<br />

r V 2 in<br />

2 gz in<br />

A comparison of Eqs. 5.73 and 5.75 prompts us to conclude that<br />

(5.75)<br />

ǔ out ǔ in q net 0<br />

(5.76)<br />

in<br />

when the steady incompressible flow is frictionless. For steady incompressible flow with friction,<br />

we learn from experience (second law of thermodynamics) that<br />

ǔ out ǔ in q net 7 0<br />

in<br />

In Eqs. 5.73 and 5.75, we can consider the combination of variables<br />

p<br />

r V 2<br />

2 gz<br />

(5.77)<br />

as equal to useful or available energy. Thus, from inspection of Eqs. 5.73 and 5.75, we can conclude<br />

that ǔ out ǔ in q net in represents the loss of useful or available energy that occurs in an incompressible<br />

<strong>fluid</strong> flow because of friction. In equation form we have<br />

ǔ out ǔ in q net<br />

in<br />

loss<br />

For a frictionless flow, Eqs. 5.73 and 5.75 tell us that loss equals zero.<br />

It is often convenient to express Eq. 5.73 in terms of loss as<br />

(5.78)<br />

p out<br />

r V 2 out<br />

2 gz out p in<br />

r V 2 in<br />

2 gz in loss<br />

An example of the application of Eq. 5.79 follows.<br />

(5.79)<br />

E XAMPLE 5.23<br />

Energy—Effect of Loss of Available Energy<br />

GIVEN As shown in Fig. E5.23a, air flows from a room<br />

through two different vent configurations: a cylindrical hole in<br />

the wall having a diameter of 120 mm and the same diameter<br />

cylindrical hole in the wall but with a well-rounded entrance.<br />

The room pressure is held constant at 1.0 kPa above atmospheric<br />

pressure. Both vents exhaust into the atmosphere. As discussed<br />

in Section 8.4.2, the loss in available energy associated<br />

with flow through the cylindrical vent from the room to the vent<br />

exit is 0.5V 2 2/2 where V 2 is the uniformly distributed exit velocity<br />

of air. The loss in available energy associated with flow<br />

through the rounded entrance vent from the room to the vent exit<br />

is 0.05V 2 2/2, where V 2 is the uniformly distributed exit velocity<br />

of air.<br />

FIND Compare the volume flowrates associated with the two<br />

different vent configurations.

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