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 15.7, Problem 82P
To determine

The estimated temperature of the combustion products.

Expert Solution & Answer
Check Mark

Answer to Problem 82P

The estimated temperature of the combustion products is 1956K.

Explanation of Solution

Express the total mass of the coal when the ash is substituted.

mtotal=100mash (I)

Here, mass of ash is mash.

Express the mass fraction of carbon.

mfC=mCmtotal (II)

Here, mass of carbon is mC.

Express the mass fraction of hydrogen.

mfH2=mH2mtotal (III)

Here, mass of hydrogen is mH2.

Express the mass fraction of oxygen.

mfO2=mO2mtotal (IV)

Here, mass of oxygen is mO2.

Express the mass fraction of nitrogen.

mfN2=mN2mtotal (V)

Here, mass of nitrogen is mN2.

Express the mass fraction of sulphur.

mfS=mSmtotal (VI)

Here, mass of sulphur is mS.

Express the number of moles of carbon.

NC=mfCMC (VII)

Here, molar mass of carbon is MC.

Express the number of moles of hydrogen.

NH2=mfH2MH2 (VIII)

Here, molar mass of hydrogen is MH2.

Express the number of moles of oxygen.

NO2=mfO2MO2 (IX)

Here, molar mass of oxygen is MO2.

Express the number of moles of nitrogen.

NN2=mfN2MN2 (X)

Here, molar mass of nitrogen is MN2.

Express the number of moles of sulphur.

NS=mfSMS (XI)

Here, molar mass of sulphur is MS.

Express the total number of moles.

Nm=NC+NH2+NO2+NN2+NS (XII)

Express the mole fraction of carbon.

yC=NCNm (XIII)

Express the mole fraction of hydrogen.

yH2=NH2Nm (XIV)

Express the mole fraction of oxygen.

yO2=NO2Nm (XV)

Express the mole fraction of nitrogen.

yN2=NN2Nm (XVI)

Express the mole fraction of sulphur.

yS=NSNm (XVII)

Apply energy balance under steady flow conditions on the combustion chamber.

NP(h¯fo+h¯h¯o)P=NR(h¯fo+h¯h¯o)RNP(h¯fo+h¯h¯o)P=NRh¯f,Ro (XVIII)

Here, number of moles of products is NP, number of moles of reactants is NR, enthalpy of formation is h¯f.

Conclusion:

Refer Table A-1, “molar mass, gas constant, and the critical point properties”, and write the molar masses.

MC=12kg/kmolMH2=2kg/kmolMO2=32kg/kmolMS=32kg/kmol

Mair=29kg/kmolMN2=28kg/kmol

Here, molar mass of air is Mair.

Substitute 8.62 for mash in Equation (I).

mtotal=1008.62=91.38kg

Substitute 79.61kg for mC and 91.38kg for mtotal in Equation (II).

mfC=79.61kg91.38kg=0.8712=87.12kg

Substitute 4.66kg for mH2 and 91.38kg for mtotal in Equation (III).

mfH2=4.66kg91.38kg=0.05100=5.10kg

Substitute 4.76kg for mO2 and 91.38kg for mtotal in Equation (IV).

mfO2=4.76kg91.38kg=0.05209=5.209kg

Substitute 1.83kg for mN2 and 91.38kg for mtotal in Equation (V).

mfN2=1.83kg91.38kg=0.02003=2.003kg

Substitute 0.52kg for mS and 91.38kg for mtotal in Equation (VI).

mfS=0.52kg91.38kg=0.00569=0.569kg

Substitute 87.12kg for mC and 12kg/kmol for MC in Equation (VII).

NC=87.12kg12kg/kmol=7.26kmol

Substitute 5.10kg for mH2 and 2kg/kmol for MH2 in Equation (VIII).

NH2=5.10kg2kg/kmol=2.55kmol

Substitute 5.209kg for mO2 and 32kg/kmol for MO2 in Equation (IX).

NO2=5.209kg32kg/kmol=0.1628kmol

Substitute 2.003kg for mN2 and 28kg/kmol for MN2 in Equation (X).

NN2=2.003kg28kg/kmol=0.07154kmol

Substitute 0.569kg for mS and 32kg/kmol for MS in Equation (XI).

NS=0.569kg32kg/kmol=0.01778kmol

Substitute 7.26kmol for NC, 2.55kmol for NH2, 0.1628kmol for NO2, 0.07154kmol for NN2 and 0.01778kmol for NS in Equation (XII).

Nm=7.26kmol+2.55kmol+0.1628kmol+0.07154kmol+0.01778kmol=10.06kmol

Substitute 7.26kmol for NC and 10.06kmol for Nm in Equation (XIII).

yC=7.26kmol10.06kmol=0.7125

Substitute 2.55kmol for NH2 and 10.06kmol for Nm in Equation (XIV).

yH2=2.55kmol10.06kmol=0.2535

Substitute 0.1628kmol for NO2 and 10.06kmol for Nm in Equation (XV).

yO2=0.1628kmol10.06kmol=0.01618

Substitute 0.07154kmol for NN2 and 10.06kmol for Nm in Equation (XVI).

yN2=0.07154kmol10.06kmol=0.00711

Substitute 0.01778kmol for NS and 10.06kmol for Nm in Equation (XVII).

yS=0.01778kmol10.06kmol=0.00177

Express the combustion equation.

[0.7215C+0.2535H2+0.01618O2+0.00711N2+0.00177S+1.5ath(O2+3.76N2)xCO2+yH2O+zSO2+kN2+0.5athO2] (XIX)

Perform the species balancing:

Carbon balance:

x=0.7215

Hydrogen balance:

y=0.2535

Sulphur balance:

z=0.00177

Oxygen balance:

0.01618+1.5ath=x+0.5y+z+0.5ath0.01618+1.5ath=0.7215+0.5(0.2535)+0.00177+0.5athath=0.7215+0.12675+0.001770.01618ath=0.8339

Nitrogen balance:

0.00711+1.5(3.76ath)=kk=0.00711+1.5(3.76×0.8339)k=4.710

Substitute 0.7215 for x, 0.2535 for y, 0.00177 for z, 0.8339 for ath and 4.710 for k in Equation (XIX).

[0.7215C+0.2535H2+0.01618O2+0.00711N2+0.00177S+1.5(0.8339)(O2+3.76N2)0.7215CO2+0.2535H2O+0.00177SO2+4.710N2+0.5(0.8339)O2][0.7215C+0.2535H2+0.01618O2+0.00711N2+0.00177S+1.2509(O2+3.76N2)0.7215CO2+0.2535H2O+0.00177SO2+4.710N2+0.4170O2] (XX)

Refer Equation (XX), and write the number of moles of products and reactants.

NC=0.7215kmolNH2=0.2535kmolNO2=0.01617kmol

NN2=0.00711kmolNS=0.00177kmol

Refer Appendix Table A-18, A-19, A-20 and A-23 and write the property table for products and reactants as in Table (1).

Substance

hfo¯

(kJ/kmol)

h¯298K

(kJ/kmol)

h¯400K

(kJ/kmol)

O20868211,171
N20866911,640
H2O(g)241,8209904 
CO2393,5209364 

Substitute the values form Table (I) into Equation (XVIII) to get,

[0.7215(393,520+h¯CO29364)+(0.2535)(241,820+h¯H2O9904)+(0.4170)(0+h¯O28682)+(4.71)(0+h¯N28669)=(1.2509)(0+11,7118682)+(4.703)(11,6408669)]0.7215h¯CO2+0.2535h¯H2O+0.4170h¯O2+4.71h¯N2=416,706kJ (XXI)

Perform trial and error method to balance the Equation (XXI).

Iteration I:

Take TP=2000K

[0.7215h¯CO2+0.2535h¯H2O+0.4170h¯O2+4.71h¯N2]=[(0.7125)(100,804)+(0.2535)(82,593)+(0.4170)(67,881)+(4.71)(64,810)]=427,229kJ(higherthan416,706kJ)

Iteration II:

Take Tprod=1980K

[0.7215h¯CO2+0.2535h¯H2O+0.4170h¯O2+4.71h¯N2]=[(0.7125)(99,606)+(0.2535)(81,573)+(0.4170)(67,127)+(4.71)(64,090)]=422,400kJ(higherthan416,706kJ)

Perform the interpolation method to obtain the adiabatic flame temperature of the product gases.

Write the formula of interpolation method of two variables.

y1=(x2x1)(y2y3)(x3x1)+y2 (XXII)

Here, the variables denote by x and y is enthalpy and estimated temperature respectively

Show the adiabatic flame temperature corresponding to enthalpy as in Table (1).

Enthalpy

h¯(kJ)

Estimated

temperature

TP(K)

416,706(x1)(y1=?)
422,400(x2)1980 (y2)
427,229(x3)2000(y3)

Substitute 416,706kJ for x1, 422,400kJ for x2, 427,229kJ for x3, 1980K for y2 and 2000K for y3 in Equation (XXII).

y1=(422,400kJ416,706kJ)(1980K2000K)(427,229kJ416,706kJ)+1980K=1956K

Thus, the estimated temperature of the combustion product gases is,

TP=1956K

Here, estimated temperature of the combustion product gases is TP.

Hence, the estimated temperature of the combustion products is 1956K.

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Chapter 15 Solutions

Thermodynamics: An Engineering Approach

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