/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 8 An air-standard Otto cycle has a... [FREE SOLUTION] | 91Ó°ÊÓ

91Ó°ÊÓ

An air-standard Otto cycle has a compression ratio of \(7.5\). At the beginning of compression, \(p_{1}=85 \mathrm{kPa}\) and \(T_{1}=32^{\circ} \mathrm{C}\). The mass of air is \(2 \mathrm{~g}\), and the maximum temperature in the cycle is \(960 \mathrm{~K}\). Determine (a) the heat rejection, in \(\mathrm{kJ}\). (b) the net work, in \(\mathrm{kJ}\). (c) the thermal efficiency. (d) the mean effective pressure, in \(\mathrm{kPa}\).

Short Answer

Expert verified
Heat rejection: 0.114 kJNet work: 0.167 kJThermal efficiency: 59.5%MEP: 91.45 kPa

Step by step solution

01

- Convert Initial Temperature to Kelvin

Convert the initial temperature from Celsius to Kelvin: \[T_1 = 32^{\text{°C}} + 273.15 = 305.15 \text{K}\]
02

- Determine State 1 Properties

Given: \[ p_1 = 85 \text{kPa} \] \[ T_1 = 305.15 \text{K} \] Convert the mass from grams to kilograms: \[ m = 2 \text{g} = 0.002 \text{kg} \]
03

- Calculate Volume at State 1

Using the ideal gas law, calculate the volume at state 1: \[ V_1 = \frac{mRT_1}{p_1} \] Where: - \( R = 0.287 \text{kJ/(kg·K)} \) (specific gas constant for air) Substituting the values: \[ V_1 = \frac{0.002 \times 0.287 \times 305.15}{85} = 0.00206 \text{m}^3 \]
04

- Calculate Temperature at State 2

Using the isentropic relation for compression process: \[ \frac{T_2}{T_1} = \left(\frac{V_1}{V_2}\right)^{k-1} \] Given the compression ratio: \( r = 7.5 \) Therefore: \[ \frac{T_2}{305.15} = 7.5^{0.4} \] \[ T_2 = 764.7 \text{K} \]
05

- Determine State 2 Pressure

Using the ideal gas law: \[ p_2 = \frac{p_1 \times T_2}{T_1} \] Substituting the values: \[ p_2 = \frac{85 \times 764.7}{305.15} = 213.17 \text{kPa} \]
06

- Determine State 3 Pressure and Volume

The process from state 2 to 3 is constant volume heat addition: Given the maximum temperature: \( T_3 = 960 \text{K} \) Using the ideal gas law: \[ p_3 = \frac{p_2 \times T_3}{T_2} \] Substituting the values: \[ p_3 = \frac{213.17 \times 960}{764.7} = 270.5 \text{kPa} \]
07

- Calculate Temperature at State 4

Using the isentropic relation for expansion process: \[ \frac{T_4}{T_3} = \left(\frac{V_3}{V_4}\right)^{k-1} \] Given the compression ratio: \( r = 7.5 \) Therefore: \[ \frac{T_4}{960} = \frac{1}{7.5^{0.4}} \] Substituting the values: \[ T_4 = 385.15 \text{K} \]
08

- Determine State 4 Pressure

Using the ideal gas law: \[ p_4 = \frac{p_3 \times T_4}{T_3} \] Substituting the values: \[ p_4 = \frac{270.5 \times 385.15}{960} = 108.5 \text{kPa} \]
09

- Calculate Heat Rejection

Using the ideal gas formula for constant volume heat rejection: \[ q_{out} = m \times c_v \times (T_4 - T_1) \] Where: - \( c_v = 0.717 \text{kJ/(kg·K)} \) Substituting the values: \[ q_{out} = 0.002 \times 0.717 \times (385.15 - 305.15) \] \[ q_{out} = 0.114 \text{kJ} \]
10

- Calculate Net Work Output

The net work output is the difference between the heat added and the heat rejected: \[ W_{net} = q_{in} - q_{out} \] Given: \[ q_{in} = m \times c_v \times (T_3 - T_2) \] Substituting the values: \[ q_{in} = 0.002 \times 0.717 \times (960 - 764.7) = 0.281 \text{kJ} \] \[ W_{net} = 0.281 - 0.114 = 0.167 \text{kJ} \]
11

- Calculate Thermal Efficiency

The thermal efficiency is given by the formula: \[ \eta = 1 - \frac{q_{out}}{q_{in}} \] Substituting the values: \[ \eta = 1 - \frac{0.114}{0.281} = 0.595 \text{ or } 59.5\% \]
12

- Calculate Mean Effective Pressure (MEP)

The mean effective pressure is given by: \[ MEP = \frac{W_{net}}{V_{1} - V_{2}} \] Using the volumes calculated previously: \[ V_1 = 0.00206 \text{m}^3, V_2 = \frac{V_1}{r} = \frac{0.00206}{7.5} = 0.000275 \text{m}^3 \] Substituting the values: \[ MEP = \frac{0.167}{0.00206 - 0.000275} = 91.45 \text{kPa} \]

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 91Ó°ÊÓ!

Key Concepts

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

Compression Ratio
The compression ratio in an Otto cycle is a crucial parameter defined as the ratio of the maximum to the minimum volume in the cylinder. Mathematically, it is expressed as: \[ r = \frac{V_1}{V_2} \] Here, \( V_1 \) is the initial volume before compression and \( V_2 \) is the volume after compression. In this particular problem, the compression ratio is given as 7.5. The higher the compression ratio, the more the air-fuel mixture is compressed, leading to higher efficiency and power output. However, it can also result in higher engine temperatures and potential knocking issues. Understanding the role of compression ratio helps in analyzing engine performance and optimizing fuel efficiency.
Isentropic Process
An isentropic process is a thermodynamic process in which entropy remains constant. In the context of the Otto cycle, both the compression and expansion processes are ideally assumed to be isentropic. For an isentropic compression, the relationship between temperature and volume is given by: \[ \frac{T_2}{T_1} = \left( \frac{V_1}{V_2} \right)^{k-1} \] Here, \(T_1\) and \(T_2\) are the initial and final temperatures, and \(k\) (or \(\gamma\)) is the specific heat ratio, typically 1.4 for air. Similarly, for isentropic expansion, the relation is: \[ \frac{T_4}{T_3} = \left( \frac{V_3}{V_4} \right)^{k-1} \] Where \(T_3\) and \(T_4\) are the temperatures before and after expansion. These relationships are essential for calculating state properties in cycles and are derived from the principles of thermodynamics.
Thermal Efficiency
Thermal efficiency of an Otto cycle is a measure of how well the cycle converts heat into work. It is defined as the ratio of the net work output to the heat input. For the Otto cycle, thermal efficiency can be expressed as: \[ \eta = 1 - \frac{q_{out}}{q_{in}} \] In the given problem, heat rejection \(q_{out}\) and heat addition \(q_{in}\) are computed using the specific heat at constant volume: \[ q_{out} = m \times c_v \times (T_4 - T_1) \] \[ q_{in} = m \times c_v \times (T_3 - T_2) \] With efficiencies calculated as: \[ \eta = 1 - \frac{0.114}{0.281} = 0.595 \] Meaning approximately 59.5 percent of the input energy is converted to useful work. Higher thermal efficiency indicates a more effective engine in converting fuel energy into mechanical work.
Mean Effective Pressure
Mean effective pressure (MEP) is a representative measure of the engine's power output. It is defined as the average pressure which, if acted upon the pistons, would produce the same work as the cycle. MEP is calculated by the formula: \[ MEP = \frac{W_{net}}{V_1 - V_2} \] In this problem, \(W_{net}\) is the net work output and \(V_1\) and \(V_2\) are the initial and final volumes during compression. With computed values: \[ V_1 = 0.00206 \text{ m}^3 \] \[ V_2 = \frac{V_1}{r} = \frac{0.00206}{7.5} = 0.000275 \text{ m}^3 \] \[ MEP = \frac{0.167}{0.00206 - 0.000275} = 91.45 \text{ kPa} \] The MEP provides an insight into the efficiency and performance of an engine, helping compare different engines regardless of their size.

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

Air at \(p_{\mathrm{o}}=1.5\) bar, \(T_{\mathrm{o}}=300 \mathrm{~K}\) expands isentropically through a converging nozzle and discharges to the atmosphere at 1 bar. The exit plane area is \(0.0015 \mathrm{~m}^{2}\). (a) Determine the mass flow rate, in \(\mathrm{kg} / \mathrm{s}\). (b) If the supply region pressure, \(p_{\mathrm{o}}\), were increased to \(2.1\) bar, what would be the mass flow rate, in \(\mathrm{kg} / \mathrm{s}\) ?

Consider an air-standard Otto cycle in which compression ratio is 10 . At the beginning of compression, \(T_{1}=298 \mathrm{~K}\) and \(p_{1}=1\) bar. During the cycle there is a heat addition of \(1300 \mathrm{~kJ}\) per \(\mathrm{kg}\) of flowing air. Determine (a) the net work in \(\mathrm{kJ}\) per \(\mathrm{kg}\) of air. (b) the thermal efficiency of the cycle. (c) the mean effective pressure, in bar. (d) the maximum temperature attained during the cycle, in \(\mathrm{K}\).

If the inlet state and the exit pressure are specified for a two-stage turbine with reheat between the stages and operating at steady state, show that the maximum total work output is obtained when the pressure ratio is the same across each stage. Use a cold air-standard analysis assuming that each compression process is isentropic, there is no pressure drop through the reheater, and the temperature at the inlet to each turbine stage is the same. Kinetic and potential energy effects can be ignored.

In an air-standard Brayton cycle, air from the atmosphere at 1 bar, \(300 \mathrm{~K}\) is compressed to 6 bar, and the maximum cycle temperature is limited to \(1050 \mathrm{~K}\). Take specific heat for air \(\left(c_{p}\right)\) to be \(1.005 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\) and \(k=1.4\). If the heat supply is \(95 \mathrm{MW}\), determine (a) the thermal efficiency of the cycle. (b) the back work ratio. (c) the power output in MW.

Carbon dioxide is contained in a large tank, initially at \(700 \mathrm{kPa}, 450 \mathrm{~K}\). The gas discharges through a converging nozzle to the surroundings, which are at \(101.3 \mathrm{kPa}\) and the pressure in the tank drops. Estimate the pressure in the tank, in \(\mathrm{kPa}\), when the flow first ceases to be choked.

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.