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Refrigerant-134a at \(1 \mathrm{MPa}\) and \(100^{\circ} \mathrm{C}\) is throttled to a pressure of 0.8 MPa. Determine the reversible work and exergy destroyed during this throttling process. Assume the surroundings to be at \(30^{\circ} \mathrm{C}\)

Short Answer

Expert verified
Answer: The reversible work during the throttling process is 0. The exergy destroyed during the throttling process can be calculated using the equation \(Ex_{destroyed} = T_{0} \cdot (S_2 - S_1)\), where the values of \(S_1\), \(S_2\), and \(T_{0}\) are determined using the given conditions and thermodynamic tables.

Step by step solution

01

Determine initial conditions

As given in the problem statement, the initial pressure \(P_1\) is \(1\) MPa and the initial temperature \(T_1\) is \(100^{\circ} \mathrm{C}\) (\((100+273.15)\) K). Using the temperature and pressure data, we can find the necessary thermodynamic properties of Refrigerant-134a.
02

Determine final conditions

The problem statement specifies that the Refrigerant-134a is throttled to a final pressure of \(0.8\) MPa. In a throttling process, there is no heat transfer or work done, thus we can conclude that enthalpy remains constant, \(h_1 = h_2\). With this, we can use a thermodynamic table for Refrigerant-134a to find its final temperature \(T_2\) and other properties based on these conditions.
03

Determine reversible work

Since the throttling process is an isenthalpic process (constant enthalpy), the reversible work \(W_{rev}\) can be calculated using the following equation derived from the first law of thermodynamics: \(W_{rev} = h_2 - h_1 + q\) Since \(h_1 = h_2\) and \(q=0\) in a throttling process, \(W_{rev} = 0\)
04

Determine exergy destroyed

To calculate the exergy destroyed during the throttling process, we can use the following equation derived from the second law of thermodynamics: \(Ex_{destroyed} = T_{0} \cdot \Delta S_{gen}\) Here, \(T_{0}\) is the surrounding temperature, which is given as \(30^{\circ} \mathrm{C}\) (\((30+273.15)\) K) and \(\Delta S_{gen}\) is the entropy generated during the process. Since the throttling process is irreversible, entropy is generated, and we can calculate \(\Delta S_{gen}\) using the following equation: \(\Delta S_{gen} = S_2 - S_1\) We can find the values of \(S_1\) and \(S_2\) using the thermodynamic tables for Refrigerant-134a at the given initial and final conditions. Now we can calculate the exergy destroyed as: \(Ex_{destroyed} = T_{0} \cdot (S_2 - S_1)\)
05

Conclusion

In conclusion, the reversible work done during the throttling process is \(0\). The exergy destroyed during the throttling process can be calculated using the equation \(Ex_{destroyed} = T_{0} \cdot (S_2 - S_1)\), where the values of \(S_1\), \(S_2\), and \(T_{0}\) are determined using the given conditions and thermodynamic tables.

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Most popular questions from this chapter

Consider a well-insulated horizontal rigid cylinder that is divided into two compartments by a piston that is free to move but does not allow either gas to leak into the other side. Initially, one side of the piston contains \(1 \mathrm{m}^{3}\) of \(\mathrm{N}_{2}\) gas at \(500 \mathrm{kPa}\) and \(80^{\circ} \mathrm{C}\) while the other side contains \(1 \mathrm{m}^{3}\) of \(\mathrm{He}\) gas at \(500 \mathrm{kPa}\) and \(25^{\circ} \mathrm{C}\). Now thermal equilibrium is established in the cylinder as a result of heat transfer through the piston. Using constant specific heats at room temperature, determine \((a)\) the final equilibrium temperature in the cylinder and ( \(b\) ) the wasted work potential during this process. What would your answer be if the piston were not free to move? Take \(T_{0}=25^{\circ} \mathrm{C}\)

A \(0.1-m^{3}\) rigid tank contains saturated refrigerant\(134 \mathrm{a}\) at \(800 \mathrm{kPa}\). Initially, 30 percent of the volume is occupied by liquid and the rest by vapor. A valve at the bottom of the tank is opened, and liquid is withdrawn from the tank. Heat is transferred to the refrigerant from a source at \(60^{\circ} \mathrm{C}\) so that the pressure inside the tank remains constant. The valve is closed when no liquid is left in the tank and vapor starts to come out. Assuming the surroundings to be at \(25^{\circ} \mathrm{C}\) determine \((a)\) the final mass in the tank and \((b)\) the reversible work associated with this process.

Steam enters an adiabatic turbine at \(6 \mathrm{MPa}, 600^{\circ} \mathrm{C}\) and \(80 \mathrm{m} / \mathrm{s}\) and leaves at \(50 \mathrm{kPa}, 100^{\circ} \mathrm{C},\) and \(140 \mathrm{m} / \mathrm{s}\). If the power output of the turbine is \(5 \mathrm{MW}\), determine \((a)\) the reversible power output and ( \(b\) ) the second-law efficiency of the turbine. Assume the surroundings to be at \(25^{\circ} \mathrm{C}\).

Refrigerant-22 absorbs heat from a cooled space at \(50^{\circ} \mathrm{F}\) as it flows through an evaporator of a refrigeration system. \(R-22\) enters the evaporator at \(10^{\circ} \mathrm{F}\) at a rate of \(0.08 \mathrm{lbm} / \mathrm{s}\) with a quality of 0.3 and leaves as a saturated vapor at the same pressure. Determine \((a)\) the rate of cooling provided, in \(\mathrm{Btu} / \mathrm{h},(b)\) the rate of exergy destruction in the evaporator, and \((c)\) the second-law efficiency of the evaporator. Take \(T_{0}\) \(=77^{\circ} \mathrm{F} .\) The properties of \(\mathrm{R}-22\) at the inlet and exit of the evaporator are: \(h_{1}=107.5 \mathrm{Btu} / \mathrm{lbm}, s_{1}=0.2851 \mathrm{Btu} / \mathrm{lbm} \cdot \mathrm{R}\) \(h_{2}=172.1 \mathrm{Btu} / \mathrm{lbm}, s_{2}=0.4225 \mathrm{Btu} / \mathrm{lbm} \cdot \mathrm{R}\)

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