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Air enters a compressor operating at steady state at \(1.05\) bar, \(300 \mathrm{~K}\), with a volumetric flow rate of \(12 \mathrm{~m}^{3} / \mathrm{min}\) and exits at 12 bar, \(400 \mathrm{~K}\). Heat transfer occurs at a rate of \(2 \mathrm{~kW}\) from the compressor to its surroundings. Assuming the ideal gas model for air and neglecting kinetic and potential energy effects, determine the power input, in \(\mathrm{kW}\).

Short Answer

Expert verified
The power input is 26.52 kW.

Step by step solution

01

- Identify given information

Note down the given data: - Inlet pressure, \( P_1 = 1.05 \text{ bar} \) - Inlet temperature, \( T_1 = 300 \text{ K} \) - Inlet volumetric flow rate, \( \dot{V} = 12 \text{ m}^3/\text{min} \) - Exit pressure, \( P_2 = 12 \text{ bar} \) - Exit temperature, \( T_2 = 400 \text{ K} \) - Heat transfer rate, \( Q = -2 \text{ kW} \) (negative because heat is lost)
02

- Convert volumetric flow rate to mass flow rate

Using the ideal gas equation: \( PV = nRT \) and the relation \( \dot{m} = \rho \dot{V} \), convert the volumetric flow rate to mass flow rate.First, calculate the air density at inlet conditions: \[ \rho_1 = \frac{P_1}{RT_1} \]Where \( R = 287 \text{ J/kg} \cdot K \) is the specific gas constant for air.Thus, \rho_1 = \frac{1.05 \times 10^5}{287 \times 300} = 1.22 \text{ kg/m}^3 \[ \dot{m} = \rho_1 \dot{V} = 1.22 \times 12/60 = 0.244 \text{ kg/s} \]
03

- Apply the first law of thermodynamics for control volumes

The first law of thermodynamics for a steady-state control volume is given by: \[ \dot{Q} - \dot{W} = \dot{m}(h_2 - h_1) \]Rearranging for the work term: \[ \dot{W} = \dot{Q} - \dot{m}(h_2 - h_1) \]
04

- Determine enthalpy of air at inlet and outlet conditions

For an ideal gas, the enthalpy is given by: \[ h = c_p T \]Where \( c_p = 1005 \text{ J/kg} \cdot K \) for air at constant pressure. Thus, \[ h_1 = c_p T_1 = 1005 \times 300 = 301500 \text{ J/kg} \]\[ h_2 = c_p T_2 = 1005 \times 400 = 402000 \text{ J/kg} \]
05

- Calculate the work input

Using the enthalpy values obtained: \[ \dot{W} = -2 \times 10^3 - 0.244 (402000 - 301500) \]\[ \dot{W} = -2000 - 0.244 \times 100500 \]\[ \dot{W} = -2000 - 24522 = -26522 \text{ W} \]Converting to kilowatts: \[ \dot{W} = -26.52 \text{ kW} \]

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

steady-state process
In a steady-state process, the properties of the system, such as pressure, temperature, and energy content, do not change over time. This means that the mass, energy, and properties entering the system equal the mass, energy, and properties leaving the system. In our exercise, the air entering the compressor and the air exiting are assumed to be in steady-state, meaning the flow rates and thermodynamic properties are constant over time. This simplifies the analysis because we do not need to account for any transient behaviors or time-dependent changes.
ideal gas model
The ideal gas model simplifies the analysis of gases by assuming the gas molecules do not interact with each other and occupy no volume. This model is often accurate for gases at low pressure and high temperature. For our problem, we assume air behaves as an ideal gas. We use the ideal gas law, defined as \( PV = nRT \), to relate pressure (\( P \)), volume (\( V \)), and temperature (\( T \)) of the gas, where \( R \) is the specific gas constant. This assumption allows us to easily calculate the air density and subsequently the mass flow rate, which are crucial for further calculations related to energy and work.
first law of thermodynamics
The first law of thermodynamics is a form of the law of conservation of energy, which states that energy cannot be created or destroyed, only transferred or changed from one form to another. For a control volume, like the compressor in our problem, the first law is expressed as: \[ \dot{Q} - \dot{W} = \dot{m}(h_2 - h_1) \] Here, \( \dot{Q} \) is the rate of heat transfer, \( \dot{W} \) is the rate of work done, \( \dot{m} \) is the mass flow rate, and \( h_2 \) and \( h_1 \) are the specific enthalpies at the exit and entrance, respectively. In our problem, we're tasked with finding the power input (\( \dot{W} \)) to the compressor. By rearranging the equation and using the known values of heat transfer, mass flow rate, and enthalpy, we determine the required work input.
enthalpy
Enthalpy (\( h \)) is a measure of the total energy of a thermodynamic system, including internal energy and the energy required to make space for the system. For ideal gases, enthalpy is a function of temperature alone and can be calculated using: \[ h = c_p T \] Where \( c_p \) is the specific heat at constant pressure and \( T \) is the temperature. In the given exercise, we calculate the enthalpies at both the inlet and outlet of the compressor using the specific heat \( c_p = 1005 \) J/kg·K and the temperatures \( T_1 \) and \( T_2 \). These values are then used in conjunction with the first law of thermodynamics to determine the power input required for the compressor to operate.

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Most popular questions from this chapter

Air modeled as an ideal gas enters a combustion chamber at \(20 \mathrm{lbf} / \mathrm{in}^{2}\) and \(70^{\circ} \mathrm{F}\) through a rectangular duct, \(5 \mathrm{ft}\) by \(4 \mathrm{ft}\). If the mass flow rate of the air is \(830,000 \mathrm{lb} / \mathrm{h}\), determine the velocity, in \(\mathrm{ft} / \mathrm{s}\).

Steam enters a turbine operating at steady state with a mass flow of \(10 \mathrm{~kg} / \mathrm{min}\), a specific enthalpy of \(3100 \mathrm{~kJ} / \mathrm{kg}\), and a velocity of \(30 \mathrm{~m} / \mathrm{s}\). At the exit, the specific enthalpy is \(2300 \mathrm{~kJ} / \mathrm{kg}\) and the velocity is \(45 \mathrm{~m} / \mathrm{s}\). The elevation of the inlet is \(3 \mathrm{~m}\) higher than at the exit. Heat transfer from the turbine to its surroundings occurs at a rate of \(1.1 \mathrm{~kJ}\) per \(\mathrm{kg}\) of steam flowing. Let \(g=9.81 \mathrm{~m} / \mathrm{s}^{2}\). Determine the power developed by the turbine, in \(\mathrm{kW}\).

Refrigerant \(134 \mathrm{a}\) enters a well-insulated nozzle at \(200 \mathrm{lbf} / \mathrm{in} .{ }^{2}, 220^{\circ} \mathrm{F}\), with a velocity of \(120 \mathrm{ft} / \mathrm{s}\) and exits at 20 lbf/in. \({ }^{2}\) with a velocity of \(1500 \mathrm{ft} / \mathrm{s}\). For steady-state operation, and neglecting potential energy effects, determine the exit temperature, in \({ }^{\circ} \mathrm{F}\).

Refrigerant 134 a enters a water-jacketed compressor operating at steady state at \(-10^{\circ} \mathrm{C}, 1.4\) bar, with a mass flow rate of \(4.2 \mathrm{~kg} / \mathrm{s}\), and exits at \(50^{\circ} \mathrm{C}, 12\) bar. The compressor power required is \(150 \mathrm{~kW}\). Neglecting kinetic and potential energy effects, determine the rate of heat transfer to the cooling water circulating through the water jacket.

A rigid tank whose volume is \(0.5 \mathrm{~m}^{3}\), initially containing ammonia at \(20^{\circ} \mathrm{C}, 1.5\) bar, is connected by a valve to a large supply line carrying ammonia at 12 bar, \(60^{\circ} \mathrm{C}\). The valve is opened only as long as required to fill the tank with additional ammonia, bringing the total mass of ammonia in the tank to \(143.36 \mathrm{~kg}\). Finally, the tank holds a two-phase liquid-vapor mixture at \(20^{\circ} \mathrm{C}\). Determine the heat transfer between the tank contents and the surroundings, in \(\mathrm{kJ}\), ignoring kinetic and potential energy effects.

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