Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
8th Edition
ISBN: 9780077624811
Author: CENGEL
Publisher: MCG
bartleby

Concept explainers

Question
Book Icon
Chapter 9.12, Problem 164RP

a)

To determine

The net power output of the cycle.

a)

Expert Solution
Check Mark

Answer to Problem 164RP

The net power output of the cycle is 6488kW.

Explanation of Solution

Draw the Pν for an ideal Otto cycle as shown in Figure (1).

Thermodynamics: An Engineering Approach, Chapter 9.12, Problem 164RP

Write the expression for compression ratio to calculate the clearance volume or one cylinder.

r=νc+νd/4νc (I)

Here, clearance volume is νc, displacement volume for four cylinders νd.

Write the expression to calculate the volume at state 1.

ν1=νc+νd4 (II)

Write the expression to calculate the mass of the air.

P1ν1=mRT1m=P1ν1RT1 (III)

Write temperature and specific volume relation for the isentropic compression process 1-2.

T2=T1(v1v2)k1 (IV)

Write the pressure, temperature, and specific volume relation for isentropic compression process 1-2.

P2v2T2=P1v1T1P2=(v1v2)T2T1×P1 (V)

Here, the temperature at state 1 is T1, the temperature at state 2 is T2, specific volume at state 1 is v1, specific volume at state 2 is v2, and the specific heat ratio is k.

Write the expression for heat addition process 2-3(Q23,in).

Q23,in=mcv(T3T2) (VI)

Here, temperature at state 3 is T3 and specific heat at constant volume is cv.

Write the temperature, pressure, and specific volume relation for the constant volume heat addition process 2-3.

P3v3T3=P2v2T2

For process 2-3, v2 and v3 are equal.

P3=T3T2P2 (VII)

Conclusion:

From Table A-1, “Ideal-gas specific heats of various common gases”, obtain the value of gas constant (R) of air as 0.287kPam3/kgK.

Substitute 11 for r and 1.8L for νd in Equation (I).

11=νc+1.8L4νc11=νc+1.8L(1m31000L)4νc11=νc+0.0018m34νcνc=ν2=0.000045m3

Substitute 0.000045m3 for νc and 1.8L for νd in Equation (II).

ν1=0.000045m3+1.8L4=0.000045m3+1.8L4(1m31000L)=0.000495m3

Substitute 90kPa for P1 , 0.000495m3 for ν1 , 0.287kPam3/kgK for R and 50°C for T1 in Equation (III).

m=90kPa×0.000495m30.287kPam3/kgK×50°C=90kPa×0.000495m30.287kPam3/kgK×(50+273)K=0.0004805kg

Substitute 50°C for, 11 for (v1v2), and 0.35 for k in Equation (IV).

T2=50°C(11)1.351=(50+273)K(11)1.351=747.6K

Substitute 11 for (v1v2), 90kPa for P1, 747.6K for T2, and 50°C for T1 to find P2 in Equation (V).

P2=(11)(747.6K50°C)(90kPa)=(11)(747.6K(50+273)K)(90kPa)=2292kPa

Substitute 0.5kJ for Q23,in, 0.0004805kg for m , 0.821kJ/kgK for cv, 747.6K for T2 in Equation(VI).

0.5kJ=(0.0004805kg)(0.821kJ/kgK)(T3747.6K)T3=2015K

Substitute 2015K for T3, 747.6K for T2, and 2292kPa for P2 in Equation (VIII).

P3=2015K747.6K(2292kPa)=6176kPa

b)

To determine

The net work per cycle per cylinder and the thermal efficiency of the cycle.

b)

Expert Solution
Check Mark

Answer to Problem 164RP

The net work per cycle per cylinder is 0.284kJ.

The thermal efficiency of the cycle is 56.8%.

Explanation of Solution

Write the temperature and specific volume relation for isentropic expansion process 3-4

T4=T3(v3v4)k1 (VIII)

Here, temperature at state 4 is T4, and specific volume at state 4 is v4.

Write the expression for heat rejection process 4-1, (qout).

Q41,out=mcv(T4T1) (IX)

Write the expression to calculate the net power output Wnet.

Wnet=Q23,inQ41,out (X)

Write the expression to calculate the thermal efficiency of the cycle (ηth).

ηth=WnetQin (XI)

Conclusion:

Substitute 1734K for T3 , 111 for (v3v4), and 1.35 for k in Equation (VIII).

T4=(1734K)(111)1.351=1734K×(111)0.35=870.4K

Substitute 0.0004805kg for m , 0.821kJ/kgK for cv, 870.5K for T4, 50°C for T1 in Equation(IX).

Q41,out=0.0004805kg×0.821kJ/kgK(870.5K50°C)=0.0004805kg×0.821kJ/kgK(870.5K(50+273)K)=0.216kJ

Substitute 0.5kJ for Q23,in and 0.216kJ for Q41,out in Equation (X).

Wnet=0.5kJ0.216kJ=0.284kJ

Thus, the net work per cycle per cylinder is 0.284kJ.

Substitute 0.284kJ for Wnet, and 0.5kJ for Qin in Equation(XI).

ηth=0.284kJ0.5kJ=0.568×100%=56.8%

Thus, the thermal efficiency of the cycle is 56.8%.

c)

To determine

The mean effective pressure of the cycle.

c)

Expert Solution
Check Mark

Answer to Problem 164RP

The mean effective pressure of the cycle is 631.1kPa.

Explanation of Solution

Write the expression to calculate the mean effective pressure for an ideal otto cycle (MEP).

MEP=Wnetv1v2 (XII)

Here, the compression ratio is r.

Conclusion:

Substitute, 0.284kJ for Wnet, 0.000045m3 for ν2, and 0.000495m3 for v1 in Equation (XII).

MEP=0.284kJ0.000495m30.000045m3=0.284kJ(1kPam3kJ)0.000495m30.000045m3=631.1kPa

Thus, the mean effective pressure of the cycle is 631.1kPa.

d)

To determine

The power output for an engine speed of 3000 rpm.

d)

Expert Solution
Check Mark

Answer to Problem 164RP

The power output for an engine speed of 3000 rpm is 28.4W.

Explanation of Solution

Write the expression to calculate the power produced by the engine (W˙net).

W˙net=(ncyl×Wnet)n˙nrev (XIII)

Here, speed of the engine is n˙, and number of revolutions per cycle in a four-stroke engine is nrev.

Here, the compression ratio is r.

Conclusion:

In one cycle there are two revolutions in four stroke engines.

Substitute 4cylinder for ncyl , 0.284kJ/cylinder-cycle for Wnet , 3000rev/min for n˙ and 2rev/cycle in Equation (XIII).

W˙net=(4cylinder×0.284kJ/cylinder-cycle)3000rev/min2rev/cycle=(4cylinder×0.284kJ/cylinder-cycle)3000rev/min(1min60s)2rev/cycle=28.4W

Thus, the power output for an engine speed of 3000 rpm is 28.4W.

Want to see more full solutions like this?

Subscribe now to access step-by-step solutions to millions of textbook problems written by subject matter experts!
Students have asked these similar questions
Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion. The pressure ratio across each stage of the compressor and turbine is 3. The air enters each stage of the compressor at 300 K and each stage of the turbine at 1200 K. Determine the back work ratio and the thermal efficiency of the cycle, assuming no regenerator is used.
A spark-ignition engine has a compression ratio of 10, an isentropic compression efficiency of 85 percent, and an isentropic expansion efficiency of 90 percent. At the beginning of the compression, the air in the cylinder is at 13 psia and 60°F. The maximum gas temperature is found to be 2300°F by measurement. Determine the heat supplied per unit mass, the thermal efficiency, and the mean effective pressure of this engine when modeled with the Otto cycle. Use constant specific heats at room temperature. The properties of air at room temperature are R = 0.3704 psia·ft3/lbm·R, cp = 0.240 Btu/lbm·R, cv = 0.171 Btu/lbm·R, and k = 1.4.   Question:  The heat supplied per unit mass is ___________.Btu/lbm. The thermal efficiency is_________________%. The mean effective pressure is________________.psia.
A four-cylinder, four-stroke, spark-ignition engine operates on the ideal Otto cycle with a compression ratio of 11 and a total displacement volume of 1.8 L. The air is at 90 kPa and 50°C at the beginning of the compression process. The heat input is 0.5 kJ per cycle per cylinder. Determine the power output for an engine speed of 3000 rpm. Use constant specific heats with cv = 0.821 kJ/kg·K, cp = 1.108 kJ/ kg·K, and k = 1.35.

Chapter 9 Solutions

Thermodynamics: An Engineering Approach

Ch. 9.12 - Prob. 11PCh. 9.12 - Can any ideal gas power cycle have a thermal...Ch. 9.12 - Prob. 13PCh. 9.12 - Prob. 14PCh. 9.12 - Prob. 15PCh. 9.12 - Prob. 16PCh. 9.12 - Prob. 17PCh. 9.12 - Prob. 18PCh. 9.12 - Prob. 19PCh. 9.12 - Repeat Prob. 919 using helium as the working...Ch. 9.12 - The thermal energy reservoirs of an ideal gas...Ch. 9.12 - Consider a Carnot cycle executed in a closed...Ch. 9.12 - Consider a Carnot cycle executed in a closed...Ch. 9.12 - What four processes make up the ideal Otto cycle?Ch. 9.12 - Are the processes that make up the Otto cycle...Ch. 9.12 - How do the efficiencies of the ideal Otto cycle...Ch. 9.12 - How does the thermal efficiency of an ideal Otto...Ch. 9.12 - Why are high compression ratios not used in...Ch. 9.12 - An ideal Otto cycle with a specified compression...Ch. 9.12 - Prob. 30PCh. 9.12 - Prob. 31PCh. 9.12 - Determine the mean effective pressure of an ideal...Ch. 9.12 - Reconsider Prob. 932E. Determine the rate of heat...Ch. 9.12 - An ideal Otto cycle has a compression ratio of 8....Ch. 9.12 - Prob. 36PCh. 9.12 - A spark-ignition engine has a compression ratio of...Ch. 9.12 - An ideal Otto cycle has a compression ratio of 7....Ch. 9.12 - Prob. 39PCh. 9.12 - An ideal Otto cycle with air as the working fluid...Ch. 9.12 - Repeat Prob. 940E using argon as the working...Ch. 9.12 - Someone has suggested that the air-standard Otto...Ch. 9.12 - Repeat Prob. 942 when isentropic processes are...Ch. 9.12 - Prob. 44PCh. 9.12 - Prob. 45PCh. 9.12 - Prob. 46PCh. 9.12 - Prob. 47PCh. 9.12 - Prob. 48PCh. 9.12 - Prob. 49PCh. 9.12 - Prob. 50PCh. 9.12 - Prob. 51PCh. 9.12 - Prob. 52PCh. 9.12 - Prob. 53PCh. 9.12 - Prob. 54PCh. 9.12 - Prob. 55PCh. 9.12 - Prob. 56PCh. 9.12 - Prob. 57PCh. 9.12 - Repeat Prob. 957, but replace the isentropic...Ch. 9.12 - Prob. 60PCh. 9.12 - Prob. 61PCh. 9.12 - The compression ratio of an ideal dual cycle is...Ch. 9.12 - Repeat Prob. 962 using constant specific heats at...Ch. 9.12 - Prob. 65PCh. 9.12 - Prob. 66PCh. 9.12 - Prob. 67PCh. 9.12 - An air-standard cycle, called the dual cycle, with...Ch. 9.12 - Prob. 69PCh. 9.12 - Prob. 70PCh. 9.12 - Consider the ideal Otto, Stirling, and Carnot...Ch. 9.12 - Consider the ideal Diesel, Ericsson, and Carnot...Ch. 9.12 - An ideal Ericsson engine using helium as the...Ch. 9.12 - An ideal Stirling engine using helium as the...Ch. 9.12 - Prob. 75PCh. 9.12 - Prob. 76PCh. 9.12 - Prob. 77PCh. 9.12 - Prob. 78PCh. 9.12 - Prob. 79PCh. 9.12 - For fixed maximum and minimum temperatures, what...Ch. 9.12 - What is the back work ratio? What are typical back...Ch. 9.12 - Why are the back work ratios relatively high in...Ch. 9.12 - How do the inefficiencies of the turbine and the...Ch. 9.12 - A simple ideal Brayton cycle with air as the...Ch. 9.12 - A stationary gas-turbine power plant operates on a...Ch. 9.12 - A gas-turbine power plant operates on the simple...Ch. 9.12 - Prob. 87PCh. 9.12 - Prob. 88PCh. 9.12 - Repeat Prob. 988 when the isentropic efficiency of...Ch. 9.12 - Repeat Prob. 988 when the isentropic efficiency of...Ch. 9.12 - Repeat Prob. 988 when the isentropic efficiencies...Ch. 9.12 - Air is used as the working fluid in a simple ideal...Ch. 9.12 - An aircraft engine operates on a simple ideal...Ch. 9.12 - Repeat Prob. 993 for a pressure ratio of 15.Ch. 9.12 - A gas-turbine power plant operates on the simple...Ch. 9.12 - A simple ideal Brayton cycle uses argon as the...Ch. 9.12 - A gas-turbine power plant operates on a modified...Ch. 9.12 - A gas-turbine power plant operating on the simple...Ch. 9.12 - Prob. 99PCh. 9.12 - Prob. 100PCh. 9.12 - Prob. 101PCh. 9.12 - Prob. 102PCh. 9.12 - Prob. 103PCh. 9.12 - Prob. 104PCh. 9.12 - A gas turbine for an automobile is designed with a...Ch. 9.12 - Rework Prob. 9105 when the compressor isentropic...Ch. 9.12 - A gas-turbine engine operates on the ideal Brayton...Ch. 9.12 - An ideal regenerator (T3 = T5) is added to a...Ch. 9.12 - Prob. 109PCh. 9.12 - Prob. 111PCh. 9.12 - A Brayton cycle with regeneration using air as the...Ch. 9.12 - Prob. 113PCh. 9.12 - Prob. 114PCh. 9.12 - Prob. 115PCh. 9.12 - Prob. 116PCh. 9.12 - Prob. 117PCh. 9.12 - Prob. 118PCh. 9.12 - Prob. 119PCh. 9.12 - Prob. 120PCh. 9.12 - A simple ideal Brayton cycle without regeneration...Ch. 9.12 - A simple ideal Brayton cycle is modified to...Ch. 9.12 - Consider a regenerative gas-turbine power plant...Ch. 9.12 - Repeat Prob. 9123 using argon as the working...Ch. 9.12 - Consider an ideal gas-turbine cycle with two...Ch. 9.12 - Repeat Prob. 9125, assuming an efficiency of 86...Ch. 9.12 - A gas turbine operates with a regenerator and two...Ch. 9.12 - Prob. 128PCh. 9.12 - Prob. 129PCh. 9.12 - Prob. 130PCh. 9.12 - Prob. 131PCh. 9.12 - Air at 7C enters a turbojet engine at a rate of 16...Ch. 9.12 - Prob. 133PCh. 9.12 - A turbojet is flying with a velocity of 900 ft/s...Ch. 9.12 - A pure jet engine propels an aircraft at 240 m/s...Ch. 9.12 - A turbojet aircraft is flying with a velocity of...Ch. 9.12 - Prob. 137PCh. 9.12 - Prob. 138PCh. 9.12 - Reconsider Prob. 9138E. How much change would...Ch. 9.12 - Consider an aircraft powered by a turbojet engine...Ch. 9.12 - An ideal Otto cycle has a compression ratio of 8....Ch. 9.12 - An air-standard Diesel cycle has a compression...Ch. 9.12 - Prob. 144PCh. 9.12 - Prob. 145PCh. 9.12 - Prob. 146PCh. 9.12 - Prob. 147PCh. 9.12 - A Brayton cycle with regeneration using air as the...Ch. 9.12 - Prob. 150PCh. 9.12 - A gas turbine operates with a regenerator and two...Ch. 9.12 - A gas-turbine power plant operates on the...Ch. 9.12 - Prob. 153PCh. 9.12 - An air-standard cycle with variable specific heats...Ch. 9.12 - Prob. 155RPCh. 9.12 - Prob. 156RPCh. 9.12 - Prob. 157RPCh. 9.12 - Prob. 158RPCh. 9.12 - Prob. 159RPCh. 9.12 - Prob. 160RPCh. 9.12 - Prob. 161RPCh. 9.12 - Consider an engine operating on the ideal Diesel...Ch. 9.12 - Repeat Prob. 9162 using argon as the working...Ch. 9.12 - Prob. 164RPCh. 9.12 - Prob. 165RPCh. 9.12 - Prob. 166RPCh. 9.12 - Prob. 167RPCh. 9.12 - Consider an ideal Stirling cycle using air as the...Ch. 9.12 - Prob. 169RPCh. 9.12 - Consider a simple ideal Brayton cycle with air as...Ch. 9.12 - Prob. 171RPCh. 9.12 - A Brayton cycle with a pressure ratio of 15...Ch. 9.12 - Helium is used as the working fluid in a Brayton...Ch. 9.12 - Consider an ideal gas-turbine cycle with one stage...Ch. 9.12 - Prob. 176RPCh. 9.12 - Prob. 177RPCh. 9.12 - Prob. 180RPCh. 9.12 - Prob. 181RPCh. 9.12 - Prob. 182RPCh. 9.12 - For specified limits for the maximum and minimum...Ch. 9.12 - A Carnot cycle operates between the temperature...Ch. 9.12 - Prob. 194FEPCh. 9.12 - Prob. 195FEPCh. 9.12 - Helium gas in an ideal Otto cycle is compressed...Ch. 9.12 - Prob. 197FEPCh. 9.12 - Prob. 198FEPCh. 9.12 - In an ideal Brayton cycle, air is compressed from...Ch. 9.12 - In an ideal Brayton cycle, air is compressed from...Ch. 9.12 - Consider an ideal Brayton cycle executed between...Ch. 9.12 - An ideal Brayton cycle has a net work output of...Ch. 9.12 - In an ideal Brayton cycle with regeneration, argon...Ch. 9.12 - In an ideal Brayton cycle with regeneration, air...Ch. 9.12 - Consider a gas turbine that has a pressure ratio...Ch. 9.12 - An ideal gas turbine cycle with many stages of...
Knowledge Booster
Background pattern image
Mechanical Engineering
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
SEE MORE QUESTIONS
Recommended textbooks for you
Text book image
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Text book image
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Text book image
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Text book image
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Text book image
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Text book image
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY