Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

Air enters a compressor operating at steady state with a volumetric flow rate of \(8 \mathrm{~m}^{3} / \mathrm{min}\) at \(23^{\circ} \mathrm{C}, 0.12 \mathrm{MPa}\). The air is compressed isothermally without internal irreversibilities, exiting at \(1.5 \mathrm{MPa}\). Kinetic and potential energy effects can be ignored. Evaluate the work required and the heat transfer, each in \(\mathrm{kW}\).

Short Answer

Expert verified
The work required is approximately \(-0.391 \mathrm{kW}\) and the heat transfer is \( -0.391 \mathrm{kW} \) as well.

Step by step solution

01

Identify the Process and Given Data

This is an isothermal compression process. Given data are: \( \dot{V_{in}} = 8 \mathrm{~m^3 / min} \), since 1 \( \mathrm{min} = 60 \mathrm{s} \), it translates to \( \dot{V_{in}} = \frac{8 \mathrm{~m^3}}{60 \mathrm{s}} = \frac{2}{15} \mathrm{~m^3 / s} \) Initial temperature \( T_1 = 23^{\circ} \mathrm{C} = 296 \text{ K} \) Initial pressure \( P_1 = 0.12 \mathrm{~MPa} \) Final pressure \( P_2 = 1.5 \mathrm{~MPa} \)
02

Apply the Ideal Gas Law to Determine Initial Mass Flow Rate

Using the ideal gas law, \( PV = nRT \), where, \( n = \frac{m}{M} \), therefore, \( V = \frac{mRT}{P} \)Rearranged, we have, \( m = \frac{PV}{RT} \) Since \( V_{in} = \dot{V_{in}} \times t \), the mass flow rate is: \( \dot{m} = \frac{P_1 \dot{V_{in}}}{R T_1} \), where, \( R = 287 \mathrm{J/(kg \cdot K)} \) Substitute the values to get mass flow rate, \( \dot{m} \): \( P_1 = 0.12 \mathrm{MPa} = 120 \mathrm{kPa} = 120000 \mathrm{Pa} \), \( \dot{V_{in}} = \frac{2}{15} \mathrm{m^3/s} \), \( T_1 = 296 \mathrm{K} \)\( \dot{m} = \frac{120000 \times \frac{2}{15}}{287 \times 296} \approx 0.00288 \mathrm{~kg/s} \)
03

Calculate Work Required for Isothermal Compression

For isothermal processes, work required is given by: \[ W = -nRT \ln \left(\frac{P_2}{P_1} \right) \] since \( n = \frac{m}{M} \) \[ W = - \dot{m} R T_1 \ln \left(\frac{P_2}{P_1} \right) \] Substitute values: \( \dot{m} = 0.00288 \mathrm{~kg/s} \), \( R = 287 \mathrm{J/(kg\cdot K)} \), \( T_1 = 296 \mathrm{K} \) \( P_1 = 0.12 \mathrm{MPa} \), \( P_2 = 1.5 \mathrm{MPa} \) \[ W = -0.00288 \times 287 \times 296 \ln \left(\frac{1.5}{0.12} \right) \approx -2.88 \times 287 \times 296 \times 1.610 \approx -390.6 \mathrm{W} \] Convert to \( \mathrm{kW} \): \[ W \approx -0.391 \mathrm{kW} \]
04

Calculate Heat Transfer for Isothermal Process

Using the first law of thermodynamics for an isothermal process: \[ \Delta U = Q - W = 0 \] (because internal energy change for isothermal process is zero). Therefore, \( Q = W \).Substitute the value of work calculated, thus: \[ Q \approx -0.391 \mathrm{kW} \]

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

Key Concepts

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

steady state operation
In a steady-state operation, the properties of the system do not change with time. This means that the mass flow rate, pressure, and temperature at any given point remain constant over time.
In the context of the problem, the compressor is operating in a steady state. This implies that the air entering and leaving the compressor does so continuously without any accumulation inside the system. Steady states simplify analysis because we can assume that any changes in properties are due to the flow rather than time-dependent fluctuations.
ideal gas law
The Ideal Gas Law is a fundamental relation between pressure (P), volume (V), temperature (T), and the number of moles (n) of a gas. It is expressed as: \( PV = nRT \)Here, \(R\) is the universal gas constant. For air, we often use \( R = 287 \mathrm{J/(kg \bullet K)} \).
In this exercise, the Ideal Gas Law helps determine the mass flow rate. By knowing the volumetric flow rate, pressure, and temperature of the air entering the compressor, we can rearrange the Ideal Gas Law to: \( m = \frac{PV}{RT} \)This formula allows us to calculate the mass \(m\) of the air entering per unit time.
mass flow rate calculation
Mass flow rate is the mass of a substance passing through a cross-section per unit of time. It is denoted as \( \dot{m} \). For the given problem, to calculate \( \dot{m} \):1. Convert volumetric flow rate to compatible units: \( \dot{V}_{in} = \frac{8 \ m^3}{60s} = \frac{2}{15} \mathrm{m^3/s} \)2. Use the Ideal Gas Law to find the mass of air, and then the mass flow rate: \( \dot{m} = \frac{P_1 \bullet \dot{V}_{in}}{R \bullet T_1} \)Substitute the known values:\( P_1 = 120 \mathrm{kPa} = 120000 \mathrm{Pa} \)\( T_1= 296 K \)\( R = 287 \mathrm{J/(kg \bullet K)} \)\( \dot{m} = \frac{120000 \bullet \frac{2}{15}}{287 \bullet 296} \approx 0.00288 \ kg/s \)This tells us how much air mass enters the compressor each second.
work required for compression
In an isothermal compression process, the temperature remains constant. The work required (W) for compressing an ideal gas is given by:\[ W = - \dot{m} R T \text{ln} \left(\frac{P_2}{P_1}\right) \]Given that temperature is constant, use: \( T = T_1 \).
Now substitute the known values:\( \dot{m} = 0.00288 \ kg/s, \, R = 287 \mathrm{J/(kg \bullet K)}, \, T_1 = 296 K, \, P_1 = 0.12 MPa, \, and \, P_2 = 1.5 MPa \).\[ W = -0.00288 \bullet 287 \bullet 296 \bullet \text{ln} \left(\frac{1.5}{0.12}\right) \]\[ W \approx -390.6 \mathrm{W} \text{ or } -0.391 \mathrm{kW} \]This negative sign indicates work is done on the gas (input).
heat transfer calculation
To find the heat transfer (Q) during an isothermal process, we use the first law of thermodynamics: \( \Delta U = Q - W \)Since the internal energy change \( \Delta U \) is zero for an isothermal process (temperature is constant), the equation simplifies to:\( Q = W \)From the previous section, the work done on the gas \( W \) is -0.391 kW.
Therefore, the heat transferred also equals -0.391 kW but with a direction opposite to the work input (indicating heat is released to the surroundings).

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Methane gas \(\left(\mathrm{CH}_{4}\right)\) enters a compressor at \(298 \mathrm{~K}, 1\) bar and exits at 2 bar and temperature \(T\). Employing the ideal gas model, determine \(T\), in \(\mathrm{K}\), if there is no change in specific entropy from inlet to exit.

A patent application describes a device for chilling water. At steady state, the device receives energy by heat transfer at a location on its surface where the temperature is \(540^{\circ} \mathrm{F}\) and discharges energy by heat transfer to the surroundings at another location on its surface where the temperature is \(100^{\circ} \mathrm{F}\). A warm liquid water stream enters at \(100^{\circ} \mathrm{F}, 1 \mathrm{~atm}\) and a cool stream exits at temperature \(T\) and \(1 \mathrm{~atm}\). The device requires no power input to operate, there are no significant effects of kinetic and potential energy, and the water can be modeled as incompressible. Plot the minimum theoretical heat addition required, in Btu per \(\mathrm{lb}\) of cool water exiting the device, versus \(T\) ranging from 60 to \(100^{\circ} \mathrm{F}\).

Methane \(\left(\mathrm{CH}_{4}\right)\) undergoes an isentropic expansion from an initial state where the temperature is \(1000 \mathrm{~K}\) and the pressure is 5 bar to a final state where the temperature is \(T\) and the pressure is \(p\). Using the ideal gas model together with \(\bar{c}_{\mathrm{p}}(T)\) from Table A-21, determine (a) \(p\) when \(T=500 \mathrm{~K}\) (b) \(T\) when \(p=1\) bar. (c) Check the results of parts (a) and (b) using \(I T\).

Steam at \(0.7 \mathrm{MPa}, 355^{\circ} \mathrm{C}\) enters an open feedwater heater operating at steady state. A separate stream of liquid water enters at \(0.7 \mathrm{MPa}, 35^{\circ} \mathrm{C}\). A single mixed stream exits as saturated liquid at pressure \(p\). Heat transfer with the surroundings and kinetic and potential energy effects can be ignored. (a) If \(p=0.7 \mathrm{MPa}\), determine the ratio of the mass flow rates of the incoming streams and the rate at which entropy is produced within the feedwater heater, in \(\mathrm{kJ} / \mathrm{K}\) per \(\mathrm{kg}\) of liquid exiting. (b) Plot the quantities of part (a), each versus pressure \(p\) ranging from \(0.6\) to \(0.7 \mathrm{MPa}\).

At steady state, a device receives a stream of saturated water vapor at \(210^{\circ} \mathrm{C}\) and discharges a condensate stream at \(20^{\circ} \mathrm{C}, 0.1 \mathrm{MPa}\) while delivering energy by heat transfer at \(300^{\circ} \mathrm{C}\). The only other energy transfer involves heat transfer at \(20^{\circ} \mathrm{C}\) to the surroundings. Kinetic and potential energy changes are negligible. What is the maximum theoretical amount of energy, in \(\mathrm{kJ}\) per \(\mathrm{kg}\) of steam entering, that could be delivered at \(300^{\circ} \mathrm{C} ?\)

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free