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Modern Engineering Thermodynamics

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6.4 Flow Stream Specific Kinetic and Potential Energies 173<br />

Integrating Eq. (6.12) over time gives the open system modified energy balance (MEB) as<br />

1Q 2 − 1 W 2 +<br />

The open system modified energy balance (MEB)<br />

Z 2<br />

1<br />

_m½h in − h out + ðV 2 in − V2 out Þ/ð2g cÞ + ðZ in − Z out Þðg/g c ÞŠ dt = 0 (6.13)<br />

However, the vast majority of open system problems are set up on a rate basis, so the modified energy rate<br />

balance is the equation most often used in open system analysis.<br />

When the conditions of steady state (steady flow), single inlet, or single outlet do not exist in any particular problem,<br />

we must return to the more general energy rate balance of Eq. (6.4) as a starting point for the analysis.<br />

This is illustrated with the unsteady state examples presented later in this chapter.<br />

6.4 FLOW STREAM SPECIFIC KINETIC AND POTENTIAL ENERGIES<br />

Before we can begin analyzing thermodynamic problems, we must establish a criterion for when the specific<br />

kinetic and potential energy flow stream terms of Eqs. (6.4) and (6.12) are important and when they are not.<br />

To get some feeling for the importance of these terms, we look at how their magnitude varies over a wide range<br />

of velocities and heights. First, consider the specific kinetic energy term V 2 /2g c : If we work in the <strong>Engineering</strong><br />

English units system, then V is normally in feet per second, and g c = 32:174 lbm.ft/ðlbf .s 2 Þ: Hence,<br />

V 2<br />

2g c<br />

=<br />

½VŠ 2 ft 2 /s 2<br />

<br />

2 × 32:174 lbm = ½VŠ2<br />

.ft 64:348<br />

lbf .s 2<br />

ft.lbf<br />

lbm<br />

where the symbol [V] stands for the numerical value of V in units of ft/s. The remaining term in the flow stream<br />

energy transport equation to which the specific kinetic and potential energy terms are to be added is the specific<br />

enthalpy h. In the <strong>Engineering</strong> English units system, the specific enthalpy has units of Btu/lbm. If we convert the<br />

specific kinetic energy into these units, we get<br />

V 2<br />

2g c<br />

=<br />

<br />

½VŠ 2<br />

64:348<br />

ft.lbf<br />

lbm<br />

<br />

In the SI units system, g c = 1.0 and is dimensionless, so<br />

where 1 m 2 /s 2 = 1 J/kg = 10 −3 kJ/kg.<br />

l Btu<br />

778:16 ft.lbf<br />

V 2<br />

= ½VŠ2 m 2 /s 2<br />

= ½VŠ2<br />

2g c 2ð1Þ 2<br />

J<br />

kg = ½VŠ2<br />

2000<br />

<br />

= ½VŠ2<br />

50,070<br />

Table 6.1 gives values of the specific kinetic energy for various velocities using these equations. Since the specific<br />

enthalpy values for most substances fall roughly between 100 and 1000 Btu/lbm, Table 6.1 shows that the specific<br />

kinetic energy is very small when compared to these h values for velocities less than about 250 ft/s (76 m/s),<br />

or V 2 /2g c is less than about 1:0 Btu/lbm ð2:3 kJ/kgÞ. Consequently, it is common to neglect the effect of a flow<br />

stream’s specific kinetic energy when the flow stream velocityislessthanabout250ft/s(76m/s).Thisisa<br />

relatively high velocity (~170 mi/h or 270 km/h), and most engineering applications do not have such rapid<br />

flow streams.<br />

kJ<br />

kg<br />

Btu<br />

lbm<br />

Table 6.1 The Effect of Velocity on Kinetic Energy<br />

Velocity, V<br />

Kinetic Energy, V 2 /2g c<br />

ft/s m/s Btu/lbm kJ/kg<br />

0 0 0 0<br />

1 0.3 2 × 10 −5 4.7 × 10 −5<br />

10. 3.0 2.0 × 10 −3 4.7 × 10 −3<br />

100. 30.5 2.0 × 10 −1 4.70 × 10 −1<br />

1000. 305 20.0 470.

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