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An air-standard cycle with variable specific heats is executed in a closed system and is composed of the following four processes: \(1-2 \quad v=\) constant heat addition from 14.7 psia and \(80^{\circ} \mathrm{F}\) in the amount of \(300 \mathrm{Btu} / \mathrm{lbm}\) 2-3 \(P=\) constant heat addition to \(3200 \mathrm{R}\) \(3-4 \quad\) Isentropic expansion to 14.7 psia 4-1 \(P=\) constant heat rejection to initial state (a) Show the cycle on \(P\) -V and \(T\) -s diagrams. (b) Calculate the total heat input per unit mass. (c) Determine the thermal efficiency.

Short Answer

Expert verified
Q: Explain the given air-standard cycle including its processes. The given air-standard cycle consists of four processes: 1. Constant volume heat addition from the initial state (14.7 psia and \(80^{\circ} \mathrm{F}\)) with an energy input of 300 Btu/lbm. 2. Constant pressure heat addition up to a temperature of 3200 R. 3. Isentropic expansion (back to the initial pressure of 14.7 psia). 4. Constant pressure heat rejection returning to the initial state.

Step by step solution

01

Understand the Given Air-Standard Cycle

Analyze the given cycle, consisting of four processes: 1. Process 1-2: Constant volume heat addition from the initial state (14.7 psia and \(80^{\circ} \mathrm{F}\)) with an energy input of 300 Btu/lbm. 2. Process 2-3: Constant pressure heat addition up to a temperature of 3200 R. 3. Process 3-4: Isentropic expansion (back to the initial pressure of 14.7 psia). 4. Process 4-1: Constant pressure heat rejection returning to the initial state.
02

Sketch the P-V and T-s Diagrams for the Given Cycle

Draw the P-V and T-s diagrams for the given air-standard cycle, labeling the states (1, 2, 3, and 4) and the processes (1-2, 2-3, 3-4, and 4-1). The P-V diagram will show a constant volume process (1-2), followed by a constant pressure process (2-3), then an isentropic expansion (3-4), and finally a constant pressure process returning to the initial state (4-1). The T-s diagram will show an increase in temperature without a change in entropy (1-2), followed by a constant pressure heat addition (2-3), then an isentropic expansion (3-4), and finally a constant pressure heat rejection returning to the initial state (4-1).
03

Calculate the Initial State and Properties

Calculate the enthalpy and specific volume at the initial state (1). The temperature at state 1, \(T_1=80^{\circ} \mathrm{F}+460=540\,\mathrm{R}\). Assuming air to be an ideal gas, we can use the ideal gas law to calculate the specific volume \(v_1\): \(P_1v_1 = R T_1\), where \(R=287\,\mathrm{J}/\mathrm{(kg\cdot K)}\) for air, \(R=\frac{1545\,\mathrm{ft\cdot lb_f}}{\mathrm{(lb_m\cdot R)}}\), and \(1\,\mathrm{psia}=6895\,\mathrm{Pa}\). Lastly, use the enthalpy-temperature relationship to get the enthalpy and specific volume at state 1.
04

Calculate the Properties at State 2

Determine the enthalpy at state 2 using the given heat input of 300 Btu/lbm (1 Btu/lbm = 2.326 kJ/kg): \(h_2=h_1+300\,\mathrm{Btu/lbm}\). Since the process is constant volume, \(v_2=v_1\). Then, use the enthalpy and specific volume to calculate the temperature and pressure at state 2.
05

Calculate the Properties at State 3

Using the given temperature at state 3, \(T_3=3200\,\mathrm{R}\), and the constant pressure process, \(P_3=P_2\), calculate the specific volume \(v_3\) using the ideal gas law. Then, determine the enthalpy at state 3 using the enthalpy-temperature relationship.
06

Calculate the Properties at State 4

Because process 3-4 is isentropic, the entropy at state 4 is equal to the entropy at state 3, \(s_4=s_3\). Using the pressure at state 4, \(P_4=P_1=14.7\,\mathrm{psia}\), the entropy, and the ideal gas assumption, calculate the temperature, enthalpy, and specific volume at state 4.
07

Determine Total Heat Input per Unit Mass

Calculate the total heat input \(Q_{in}\) per unit mass using the enthalpy changes in processes 1-2 and 2-3: \(Q_{in}= (h_2-h_1) + (h_3-h_2)\).
08

Determine Work Output per Unit Mass

Calculate the work output \(W_{out}\) per unit mass using the enthalpy change in processes 3-4: \(W_{out} = (h_3-h_4)\).
09

Calculate the Thermal Efficiency

Determine the thermal efficiency (\(\eta\)) of the cycle using the calculated heat input and work output values: \(\eta = \frac{W_{out}}{Q_{in}}\). Having followed the steps, we have shown the cycle on P-V and T-s diagrams, calculated the total heat input per unit mass, and determined the thermal efficiency.

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Most popular questions from this chapter

When we double the compression ratio of an ideal Otto cycle, what happens to the maximum gas temperature and pressure when the state of the air at the beginning of the compression and the amount of heat addition remain the same? Use constant specific heats at room temperature.

The single-stage compression process of an ideal Brayton cycle without regeneration is replaced by a multistage compression process with intercooling between the same pressure limits. As a result of this modification, (a) Does the compressor work increase, decrease, or remain the same? (b) Does the back work ratio increase, decrease, or remain the same? \((c) \quad\) Does the thermal efficiency increase, decrease, or remain the same?

Consider a simple ideal Brayton cycle operating between the temperature limits of 300 and 1500 K. Using constant specific heats at room temperature, determine the pressure ratio for which the compressor and the turbine exit temperatures of air are equal.

Helium is used as the working fluid in a Brayton cycle with regeneration. The pressure ratio of the cycle is 8 the compressor inlet temperature is \(300 \mathrm{K},\) and the turbine inlet temperature is \(1800 \mathrm{K}\). The effectiveness of the regenerator is 75 percent. Determine the thermal efficiency and the required mass flow rate of helium for a net power output of \(60 \mathrm{MW},\) assuming both the compressor and the turbine have an isentropic efficiency of \((a) 100\) percent and \((b) 80\) percent.

Somebody claims that at very high pressure ratios, the use of regeneration actually decreases the thermal efficiency of a gas-turbine engine. Is there any truth in this claim? Explain.

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