Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
9th Edition
ISBN: 9781259822674
Author: Yunus A. Cengel Dr., Michael A. Boles
Publisher: McGraw-Hill Education
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Chapter 13.3, Problem 68P
To determine

The thermal efficiency of the cycle.

Expert Solution & Answer
Check Mark

Answer to Problem 68P

The thermal efficiency of the cycle is 0.468_.

Explanation of Solution

Refer to Table A-1E, Obtain the molar masses of N2,O2,H2O,andCO2 as below:

MN2=28.0lbm/lbmolMO2=32.0lbm/lbmolMH2O=18.0lbm/lbmolMCO2=44.0lbm/lbmol

Refer to Table A-2Ea, obtain the constant-pressure specific heats of the gases at room temperature.

cp,N2=0.248Btu/lbmRcp,O2=0.219Btu/lbmRcp,H2O=0.445Btu/lbmRcp,CO2=0.203Btu/lbmR

Write the mass of N2.

mN2=NN2MN2 (I)

Here, the mole number of N2 is NN2.

Write the mass of O2.

mO2=NO2MO2 (II)

Here, the mole number of O2 is NO2.

Write the mass of H2O.

mH2O=NH2OMH2O (III)

Here, the mole number of H2O is NH2O.

Write the mass of CO2.

mCO2=NCO2MCO2 (IV)

Here, the mole number of CO2 is NCO2.

Write the equation to calculate the total mass of the mixture.

mm=mN2+mO2+mH2O+mCO2 (V)

Calculate the mass fraction of N2.

mfN2=mN2mm (VI)

Calculate the mass fraction of O2.

mfO2=mO2mm (VII)

Calculate the mass fraction of H2O.

mfH2O=mH2Omm (VIII)

Calculate the mass fraction of CO2.

mfCO2=mCO2mm (IX)

Calculate the molar mass of the gas mixture.

Mm=mmNm (X)

Write the equation to calculate the constant-pressure specific heat of the mixture.

cp=mfN2cp,N2+mfO2cp,O2+mfH2Ocp,H2O+mfCO2cp,CO2 (XI)

Here, mass fraction of O2,N2,CO2,andH2O are mfO2, mfN2, mfCO2, and mfH2O, respectively and constant pressure specific heat of O2,N2,CO2,andH2O are cp,O2, cp,N2, cp,CO2, and cp,H2O respectively.

Calculate the gas constant of the mixture.

R=RuMm (XII)

Here, the universal gas constant is Ru.

Calculate the constant volume specific heat.

cv=cpR (XIII)

Calculate the specific heat ratio.

k=cpcv (XIV)

Refer to Table A-2Ea, obtain the air properties at room temperature.

cp,air=0.240Btu/lbmRcv,air=0.171Btu/lbmRkair=1.4

Calculate the constant pressure and constant velocity specific heat on an average.

cp,avg=cp+cp,air2 (XV)

cv,avg=cv+cv,air2 (XVI)

Calculate the average specific heat ratio.

kavg=k+kair2 (XVII)

Calculate the final temperature during the compression process.

T2=T1rkair1 (XVIII)

Here, the compression ratio is r.

Express the heat addition process.

qin=cv,avg(T3T2) (XIX)

Here, specific heat at constant volume on an average is cv,avg.

Write the equation to calculate the temperature during the expansion process.

T4=T3(1r)k1 (XX)

Express the heat rejection process.

qout=cv,avg(T4T1) (XXI)

Calculate the thermal efficiency of the cycle.

ηth=1qoutqin (XXII)

Conclusion:

Consider 100 lbmol of this mixture.

NN2=25lbmolNO2=7lbmolNH2O=28lbmolNCO2=40lbmol

Substitute 25 lbmol for NN2, 28 lbm/lbmol for MN2, 7 lbmol for NO2, 32 lbm/lbmol for MO2, 28 lbmol for NH2O, 18 lbm/lbmol for MH2O, 40 lbmol for NCO2, and 44 lbm/lbmol for MCO2 in Equations (I) to (IV).

mN2=700lbmmO2=224lbmmH2O=504lbmmCO2=1760lbm

Substitute 224 lbm for mO2, 700 lbm for mN2, 1760 lbm for mCO2, and 504 lbm for mH2O in Equation (V).

mm=700lbm+224lbm+504lbm+1760lbm=3188lbm

Substitute 224 lbm for mO2, 700 lbm for mN2, 1760 lbm for mCO2, and 504 lbm for mH2O, and 3188 lbm for mm in Equations (VI) to (IX).

mfN2=0.2196mfO2=0.07026mfH2O=0.1581mfCO2=0.5521

Substitute 3188 lbm for mm and 100lbmol for Nm in Equation (X).

Mm=3188lbm100lbmol=31.88lbm/lbmol

Substitute 0.07026 for mfO2, 0.2196 for mfN2, 0.5521 for mfCO2, 0.1581 for mfH2O, 0.219Btu/lbmR for cp,O2, 0.248Btu/lbmR for cp,N2, 0.203Btu/lbmR for cp,CO2, and 0.445Btu/lbmR for cp,H2O in Equation (XI).

cp=[(0.2196)(0.248kJ/kgK)+(0.07026)(0.219kJ/kgK)+(0.1581)(0.445kJ/kgK)+(0.5521)(0.203kJ/kgK)]=0.2523Btu/lbmR

Substitute 1.9858Btu/lbmolR for Ru and 31.88 lbm/lbmol for Mm in Equation (XII).

R=1.9858Btu/lbmolR31.88lbm/lbmol=0.06229Btu/lbmR

Substitute 0.06229Btu/lbmR for R and 0.2523Btu/lbmR for cp in Equation (XIII).

cv=0.2523Btu/lbmR0.06229Btu/lbmR=0.1900Btu/lbmR

Substitute 0.2523Btu/lbmR for cp and 0.1900Btu/lbmR for cv in Equation (XIV).

k=0.2523Btu/lbmR0.1900Btu/lbmR=1.328

Substitute 0.2523Btu/lbmR for cp, 0.2523Btu/lbmR for cp,air, 0.1900Btu/lbmR for cv, 0.171Btu/lbmR for cv,air in Equations (XV) and (XVI).

cp,avg=0.2462Btu/lbmRcv,avg=0.1805Btu/lbmR

Substitute 1.328 for k and 1.4 for kair in Equation (XVII).

kavg=1.328+1.42=1.364

Substitute 1.4 for kair, 7 for r, and 515 R for T1 in Equation (XVIII).

T2=(515R)(7)1.411.4=1122R

Substitute 0.1805Btu/lbmR for cv,avg, 1122 R for T2, and 2060 R for T3 in Equation (XIX).

qin=0.1805Btu/lbmR(2060R1122R)=169.3Btu/lbm

Substitute 1.328 for k, 7 for r, and 2060 R for T3 in Equation (XX).

T4=(2060R)(17)1.32811.328=1014R

Substitute 0.1805Btu/lbmR for cv,avg, 1014 R for T4, and 515 R for T1 in Equation (XXI).

qout=0.1805Btu/lbmR(1014R515R)=90.1Btu/lbm

Substitute 90.1Btu/lbm for qout and 169.3Btu/lbm for qin in Equation (XXII).

ηth=190.1Btu/lbm169.3Btu/lbm=0.468

Thus, the thermal efficiency of the cycle is 0.468_.

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Chapter 13 Solutions

Thermodynamics: An Engineering Approach

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