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Modern Engineering Thermodynamics

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Problems 197<br />

we have<br />

_m R / _m D = ðk − 1Þ/ ½kT ð 1 /T T Þ− 1Š<br />

In part b, we are given that T T = 70.0°F = 530. R and T 1 = 200.°F = 660. R.<br />

Table C.13a gives us the specific heat ratio for nitrogen as k = 1.40. Therefore, our resultant equation gives<br />

_m R / _m D = ð1:40 − 1Þ/1:40 ½ ð660:/530:<br />

Þ− 1Š = 0:538<br />

Thus, 53.8% of the discharge mass must be recycled to keep the tank temperature constant.<br />

To find the rate of recycle heat transfer required in part b, we must analyze the heater and compressor as a separate system<br />

(Figure 6.21).<br />

m R<br />

m R<br />

2<br />

1<br />

Heater<br />

Compressor<br />

W C = −3.00 hp<br />

System<br />

boundary<br />

Q H = ?<br />

FIGURE 6.21<br />

Example 6.10, heater and compressor as a separate system.<br />

In general, _m R is not constant in time in this system. We assume that a feedback control system exists that automatically<br />

scales down _W C and _Q H as _m R goes to zero and the tank empties. We also assume that the internal, kinetic, and potential<br />

energies of the entire system are constant in time, so that we have a steady state, steady flow, single-inlet, single-outlet system.<br />

Under these conditions, the modified energy rate balance becomes<br />

_Q H − _W C + _m R ðh 1 − h 2 Þ = 0<br />

where we again neglect any changes in flow stream specific kinetic and potential energies. Using the ideal gas relationship<br />

for specific enthalpy gives<br />

Table 13a gives c p = 0.248 Btu/(lbm · R) for nitrogen. Then,<br />

_Q H = _m R c p ðT 2 − T 1 Þ+ _W C<br />

_Q H = ð0:500 lbm/sÞ½0:248 Btu/ðlbm.RÞŠð660: − 530: RÞ<br />

+ ð−3:00 hpÞ½550 ft.lbf/ ðs.hpÞŠ½1 Btu/ ð778:16 ft.lbfÞŠ<br />

= 14:0 Btu/s<br />

SUMMARY<br />

In this chapter, we investigate a series of open system examples and carry out a first law analysis of them using<br />

the energy balance or the energy rate balance. The primary purpose of this is to illustrate the material presented<br />

in Chapter 4. Several new equations are introduced in this chapter. Some of the more important equations are<br />

these.<br />

1. The one-dimensional mass flow equation:<br />

<br />

dm<br />

= ð _mÞ<br />

dt<br />

flow stream<br />

= ðρAVÞ flow stream<br />

(6.1)<br />

flow stream

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