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Modern Engineering Thermodynamics

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6.10 Open System Unsteady State Processes 193<br />

Air at 20.0°C<br />

and 1.40 MPa Air T Final = ?<br />

FIGURE 6.16<br />

Example 6.8.<br />

The unknown is the final temperature in the tank immediately after filling. The material is air.<br />

The final temperature in the scuba tank immediately after it has been filled is given by Eq. (6.36) as<br />

T final<br />

= kT in<br />

filling<br />

In this problem, T in = 20.0°C and Table C.13b gives k = 1.40 for air. Then, Eq. (6.36) gives<br />

T final<br />

= kT in = 1:40ð20:0 + 273:15Þ = 410 K = 137°C<br />

filling<br />

Therefore, bottled gas tanks can get quite hot during their filling process and should be cooled to minimize any rupture<br />

potential.<br />

Exercises<br />

20. If the scuba tank in Example 6.8 were filled with air at 70.0°F and 2000. psia, determine the final temperature,<br />

neglecting any air initially in the tank and assuming the tank is insulated during the filling process.<br />

Answer: T final = 742 R = 282°F.<br />

21. How do you account for the fact that the final temperature given by Eq. (6.36) is independent of the ideal gas<br />

pressure? Answer: Since the internal energy of an ideal gas is independent of pressure (see Chapter 3) and the<br />

property that defines the final state after the filling is complete is u 2 , the final pressure cannot affect the final<br />

temperature when an ideal gas is used in the filling operation.<br />

22. If the scuba tank in Example 6.8 is filled very quickly, it appears to be insulated whether it is actually insulated or not<br />

(why?) and the air inside gets quite hot. However, the tank is a heavy walled steel vessel with a large capacity to absorb<br />

the heat produced in filling the tank. If the tank itself has a mass of 10.0 kg, a specific heat of 0.503 kJ/kg · K, and<br />

initially is at 20.0°C, and it contains 0.500 kg of air with (c v ) air = 0.718 kJ/kg · K that is initially at 137°C, determine the<br />

final equilibrium temperature of the tank-air combined system. Answer: T combined = 27.8°C.<br />

The tank-emptying process is illustrated in Figure 6.17. Again we<br />

neglect flow stream specific kinetic and potential energies and<br />

require that the tank remain stationaryandhavenoworktransport<br />

of energy.<br />

Valve<br />

When the valve is opened, the initially pressurized rigid tank<br />

empties into the environment. The generalized energy rate balance<br />

for this process reduces to<br />

_Q − 0 + 0 − _m out ðh out + 0 + 0Þ = ðdU/dt + 0 + 0<br />

Þ tank<br />

or<br />

FIGURE 6.17<br />

Emptying a rigid vessel.<br />

Rigid tank (vessel)<br />

System boundary<br />

_Q − _m out h out = ½dðmuÞ/dtŠ tank<br />

Again, multiplying through by dt and integrating gives<br />

1Q 2 −<br />

Z 2<br />

1<br />

h out dm out = ðm 2 u 2 − m 1 u 1 Þ tank<br />

(6.37)<br />

where state 1 is the filled state and state 2 is the empty state (the<br />

reverse of the filling process). Unlike the filling process described<br />

earlier, the emptying process has no constant flow stream specific

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