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

Newton’s second law of motion leads to the conclusion that forces can result from or cause<br />

changes in a flowing <strong>fluid</strong>’s velocity magnitude and/or direction. Moment of force 1torque2 can result<br />

from or cause changes in a flowing <strong>fluid</strong>’s moment of velocity. These forces and torques can<br />

be associated with work and power transfer.<br />

The first law of thermodynamics is a statement of conservation of energy. The second law<br />

of thermodynamics identifies the loss of energy associated with every actual process. The mechanical<br />

energy equation based on these two laws can be used to analyze a large variety of steady,<br />

incompressible flows in terms of changes in pressure, elevation, speed, and of shaft work and loss.<br />

Good judgment is required in defining the finite region in space, the control volume, used<br />

in solving a problem. What exactly to leave out of and what to leave in the control volume are important<br />

considerations. The formulas resulting from applying the fundamental laws to the contents<br />

of the control volume are easy to interpret physically and are not difficult to derive and use.<br />

Because a finite region of space, a control volume, contains many <strong>fluid</strong> particles and even<br />

more molecules that make up each particle, the <strong>fluid</strong> properties and characteristics are often average<br />

values. In Chapter 6 an analysis of <strong>fluid</strong> flow based on what is happening to the contents of<br />

an infinitesimally small region of space or control volume through which numerous molecules<br />

simultaneously flow (what we might call a point in space) is considered.<br />

5.1 Conservation of Mass—The Continuity Equation<br />

The amount of<br />

mass in a system is<br />

constant.<br />

5.1.1 Derivation of the Continuity Equation<br />

A system is defined as a collection of unchanging contents, so the conservation of mass principle<br />

for a system is simply stated as<br />

or<br />

time rate of change of the system mass 0<br />

DM sys<br />

where the system mass, M sys , is more generally expressed as<br />

Dt<br />

0<br />

(5.1)<br />

M sys sys<br />

r dV<br />

(5.2)<br />

and the integration is over the volume of the system. In words, Eq. 5.2 states that the system mass<br />

is equal to the sum of all the density-volume element products for the contents of the system.<br />

For a system and a fixed, nondeforming control volume that are coincident at an instant of<br />

time, as illustrated in Fig. 5.1, the Reynolds transport theorem 1Eq. 4.192 with B mass and b 1<br />

allows us to state that<br />

D<br />

Dt sys<br />

r dV 0 0t cv<br />

r dV cs<br />

rV nˆ dA<br />

(5.3)<br />

System<br />

Control Volume<br />

(a) (b) (c)<br />

F I G U R E 5.1 System and control volume at three different<br />

instances of time. (a) System and control volume at time t Dt.<br />

(b) System and<br />

control volume at time t, coincident condition. (c) System and control volume at<br />

time t Dt.

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