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 45P

(a)

To determine

The volume flow rate of the mixture using the ideal gas mixture.

The mass flow rate of the mixture using the ideal gas mixture.

(a)

Expert Solution
Check Mark

Answer to Problem 45P

The volume flow rate of the mixture using the ideal gas mixture is 0.05454ft3/s_.

The mass flow rate of the mixture using the ideal gas mixture is 0.408lbm/s_.

Explanation of Solution

Refer to Table A-1E, Obtain the molar masses of O2,N2,CO2,andCH4 as below:

MO2=32.0kg/kmolMN2=28.0kg/kmolMCO2=44.0kg/kmolMCH4=16.0kg/kmol

Consider 100 lbmol of the mixture. Since the volume fractions are equal to the mole fractions, calculate the mass of each component.

mO2=NO2MO2 (I)

mN2=NN2MN2 (II)

mCO2=NCO2MCO2 (III)

mCH4=NCH4MCH4 (IV)

Here, the mole numbers of O2,N2,CO2,andCH4 are NO2,NN2,NCO2,andNCH4 respectively.

Write the equation of total mass of the mixture.

mm=mCO2+mO2+mN2+mCH4 (V)

Here, the mass of O2,N2,CO2,andCH4 are mO2,mN2,mCO2,andmCH4 respectively.

Write the equation to calculate the apparent molecular weight of the mixture.

Mm=mmNm=mmNO2+NN2+NCO2+NCH4 (VI)

Write the equation to calculate the apparent gas constant of the mixture.

R=RuMm (VII)

Here, the universal gas constant is Ru.

Write the equation of specific volume of the mixture.

v=RTP (VIII)

Here, temperature of the mixture is T and atmospheric pressure is P.

Calculate the volume flow rate of the mixture.

V˙=AV=π4D2V (IX)

Here, cross-sectional area of the pipe is A.

Calculate the mass flow rate of the mixture.

m˙=V˙v (X)

Conclusion:

Apply spreadsheet and substitute the given values of mole numbers and molar masses of O2,N2,CO2,andCH4 in Equations (I) to (IV) as in Table (I).

S.NomassesMole number (N), lbmolMolar masses (M), lbm/lbmolM×N(lbm)
1mO23032960
2mN240281120
3mCO21044440
4mCH42016320

Substitute 960 lbm for mO2, 1120 lbm for mN2, 440 lbm for mCO2, and 320 lbm for mCH4 in Equation (V).

mm=960lbm+1120lbm+440lbm+320lbm=2840lbm

Substitute 2840 lbm for mm, 30 lbmol for NO2, 40 lbmol for NN2, 10 lbmol for NCO2, and 20 lbmol for NCH4 in Equation (VI).

Mm=2840lbm30lbmol+40lbmol+10lbmol+20lbmol=28.40lbm/lbmol

Substitute 10.73psiaft3/lbmolR for Ru and 28.40lbm/lbmol for Mm in Equation (VII).

R=10.73psiaft3/lbmolR28.40lbm/lbmol=0.3778psiaft3/lbmR

Substitute 0.3778psiaft3/lbmR for R, 75°F  for T, and 1500 psia for P in Equation (VIII).

v=(0.3778psiaft3/lbmR)70°F1500psia=(0.3778psiaft3/lbmR)(70+460.67)R1500psia=0.13365ft3/lbm

Substitute 10ft/s for V and 1 in for D in Equation (IX).

V˙=π4(1in)210ft/s=π4(1in×1ft12in)210ft/s=0.05454ft3/s

Thus, the volume flow rate of the mixture using the ideal gas mixture is 0.05454ft3/s_.

Substitute 0.05454ft3/s for V˙ and 0.13365ft3/lbm for v in Equation (X).

m˙=0.05454ft3/s0.13365ft3/lbm=0.408lbm/s

Thus, the mass flow rate of the mixture using the ideal gas mixture is 0.408lbm/s_.

(b)

To determine

The volume flow rate of the mixture using the compressibility factor based on Amagat’s law of additive volumes.

The mass flow rate of the mixture using the compressibility factor based on Amagat’s law of additive volumes.

(b)

Expert Solution
Check Mark

Answer to Problem 45P

The volume flow rate of the mixture using the compressibility factor based on Amagat’s law of additive volumes is 0.05454ft3/s_.

The mass flow rate of the mixture using the compressibility factor based on Amagat’s law of additive volumes is 0.4702lbm/s_.

Explanation of Solution

Write the equation of reduced temperatures and pressures of O2,N2,CO2,andCH4.

TR,O2=TmTcr,O2 (XI)

PR,O2=PmPcr,O2 (XII)

TR,N2=TmTcr,N2 (XIII)

PR,N2=PmPcr,N2 (XIV)

TR,CO2=TmTcr,CO2 (XV)

PR,CO2=PmPcr,CO2 (XVI)

TR,CH4=TmTcr,CH4 (XVII)

PR,CH4=PmPcr,CH4 (XVIII)

Here, the critical temperature of O2 is Tcr,O2, mixture temperature is Tm, mixture pressure is Pm, critical temperature of N2 is Tcr,N2, critical temperature of CO2 is Tcr,CO2, critical temperature of CH4 is Tcr,CH4, critical pressure of N2 is Pcr,N2, critical pressure of CO2 is Pcr,CO2, critical pressure of CH4 is Pcr,CH4,

Write the equation of compressibility factor of the mixture.

Zm=yiZi=yO2ZO2+yN2ZN2+yCO2ZCO2+yCH4ZCH4 (XIX)

Here, the mole fraction of O2,N2,CO2,andCH4 are yO2,yN2,yCO2,andyCH4 respectively.

Calculate the specific volume of the mixture.

v=ZmRTP (XX)

Calculate the mass flow rate of the mixture using the compressibility factor based on Amagat’s law of additive volumes.

m˙=V˙v (XXI)

Here, the volume flow rate of mixture using the compressibility factor based on Amagat’s law of additive volumes is V˙.

Conclusion:

Refer to Table A-1E, obtain the critical temperatures and pressures of O2,N2,CO2,andCH4.

Tcr,O2=278.6RPcr,O2=736psiaTcr,N2=227.1RPcr,N2=492psia

Tcr,CO2=547.5RPcr,CO2=1071psiaTcr,CH4=343.9RPcr,CH4=673psia

Substitute 530 R for Tm, 1500 psia for Pm and obtained values from Table A-1E in Equations (XI) to (XVIII).

TR,O2=1.902PR,O2=2.038TR,N2=2.334PR,N2=3.049

TR,CO2=0.968PR,CO2=1.401TR,CH4=1.541PR,CH4=2.229

Refer to Figure A-15, obtain the compressibility factor for O2,N2,CO2,andCH4 by reading the above values of reduced temperatures and reduced pressure.

ZO2=0.94ZN2=0.99ZCO2=0.21ZCH4=0.85

Substitute 0.30 for yO2, 0.94 for ZO2, 0.40 for yN2, 0.99 for ZN2, 0.10 for yCO2, 0.21 for ZCO2, 0.20 for yCH4, and 0.85 for ZCH4 in Equation (XIX).

Zm=(0.30)(0.94)+(0.40)(0.99)+(0.10)(0.21)+(0.20)(0.85)=0.869

Substitute 1500 psia for P, 0.869 for Zm, 0.3778psiaft3/lbmR for R, and 530 R for T in Equation (XX).

v=0.869(0.3778psiaft3/lbmR)530R1500psia=0.1160ft3/lbm

Refer to part (a), the value calculated for volume flow rate is 0.05454ft3/s_.

Substitute 0.05454ft3/s for V˙  and 0.1160ft3/lbm for v in Equation (XXI).

m˙=0.05454ft3/s0.1160ft3/lbm=0.4702lbm/s

Thus, the mass flow rate of the mixture using the compressibility factor based on Amagat’s law of additive volumes is 0.4702lbm/s_.

(c)

To determine

The volume flow rate of the mixture using Kay’s pseudocritical pressure and temperature.

The mass flow rate of the mixture using Kay’s pseudocritical pressure and temperature.

(c)

Expert Solution
Check Mark

Answer to Problem 45P

The volume flow rate of the mixture using Kay’s pseudocritical pressure and temperature is 0.05454ft3/s_.

The mass flow rate of the mixture using Kay’s pseudocritical pressure and temperature.

is 0.4467lbm/s_.

Explanation of Solution

Write the critical temperature of a gas mixture.

Tcr,m=yiTcr,i=yO2Tcr,O2+yN2Tcr,N2+yCO2Tcr,CO2+yCH4Tcr,CH4 (XXII)

Write the critical pressure of a gas mixture.

Pcr,m=yiPcr,i=yO2Pcr,O2+yN2Pcr,N2+yCO2Pcr,CO2+yCH4Pcr,CH4 (XXIII)

Write the equation of reduced temperature and pressure.

TR=TmTcr,m (XXIV)

PR=PmPcr,m (XXV)

Conclusion:

Substitute 0.30 for yO2, 278.6 R for Tcr,O2, 0.40 for yN2, 227.1 R for Tcr,N2, 0.10 for yCO2, 547.5 R for Tcr,CO2, 0.20 for yCH4, and 343.9 R for Tcr,CH4 in Equation (XXII).

Tcr,m=(0.30)(278.6R)+(0.40)(227.1R)+(0.10)(547.5R)+(0.20)(343.9R)=298.0R

Substitute 0.30 for yO2, 278.6 R for Pcr,O2, 0.40 for yN2, 227.1 R for Pcr,N2, 0.10 for yCO2, 547.5 R for Pcr,CO2, 0.20 for yCH4, and 343.9 R for Pcr,CH4 in Equation (XXIII).

Pcr,m=(0.30)(736psia)+(0.40)(492psia)+(0.10)(1071psia)+(0.20)(673psia)=659.3psia

Substitute 530 R for Tm, 1500 psia for Pm, 298.0 R for Tcr,m, and 659.3 psia for Pcr,m in Equations (XXIV) and (XXV).

TR=1.779PR=2.275

Refer to Figure A-15, obtain the compressibility factor for gas mixture by reading the values of TRandPR.

Zm=0.915

Substitute 1500 psia for P, 0.915 for Zm, 0.3778psiaft3/lbmR for R, and 530 R for T in Equation (XX).

v=0.915(0.3778psiaft3/lbmR)530R1500psia=0.1221ft3/lbm

Refer to part (a), the value calculated for volume flow rate is 0.05454ft3/s_.

Substitute 0.05454ft3/s for V˙  and 0.1221ft3/lbm for v in Equation (XXI).

m˙=0.05454ft3/s0.1221ft3/lbm=0.4467lbm/s

Thus, the mass flow rate of the mixture using the compressibility factor based on Amagat’s law of additive volumes is 0.4467lbm/s_.

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Chapter 13 Solutions

Thermodynamics: An Engineering Approach

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