CONNECT FOR THERMODYNAMICS: AN ENGINEERI
CONNECT FOR THERMODYNAMICS: AN ENGINEERI
9th Edition
ISBN: 9781260048636
Author: CENGEL
Publisher: MCG
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Chapter 15.7, Problem 82P
To determine

The estimated temperature of the combustion products.

Expert Solution & Answer
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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

CONNECT FOR THERMODYNAMICS: AN ENGINEERI

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