Thermodynamics: An Engineering Approach ( 9th International Edition ) ISBN:9781260092684
Thermodynamics: An Engineering Approach ( 9th International Edition ) ISBN:9781260092684
9th Edition
ISBN: 9781260048667
Author: Yunus A. Cengel Dr.; Michael A. Boles
Publisher: McGraw-Hill Education
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Chapter 12.6, Problem 97RP

a)

To determine

The entropy changes and the work input of the compressor per unit mass by treating the propane as an ideal gas variable specific heats.

a)

Expert Solution
Check Mark

Answer to Problem 97RP

The work input of the compressor per unit mass by treating the propane as an ideal gas is 1121kJ/kg.

The change in entropy per unit mass by treating the propane as an ideal gas is 1.5873kJ/kgK.

Explanation of Solution

Refer the table A-2 (c), “Ideal gas specific heats of various common gases”.

The general empirical correlation is c¯P=a+bT+cT2+dT3.

Write the formula for enthalpy change in molar basis at ideal gas state (h¯2h¯1)ideal.

(h¯2h¯1)ideal=T1T2cPdT=T1T2(a+bT+cT2+dT3)dT=[aT+b2T2+c3T3+d4T4]T1T2=a(T2T1)+b2(T22T12)+c3(T23T13)+d4(T24T14) (I)

Here, specific heat capacity at constant pressure is cP, initial temperature is T1, final temperature is T2, the empirical constants are a, b, c, and d.

Write the formula for work input to the compressor (win).

win=(h¯2h¯1)idealM (II)

Here, molar mass of propane is M.

Write the formula for entropy change in molar basis at ideal gas state (s¯2s¯1)ideal.

(s¯2s¯1)ideal=T1T2cPTdTRuln(P2P1)==T1T2(aT+b+cT+dT2)dTRuln(P2P1)=[aln(T)+bT+c2T2+d3T3]T1T2Ruln(P2P1)=aln(T2T1)+b(T2T1)+c2(T22T12)+d3(T23T13)Ruln(P2P1) (III)

Here, universal gas constant is Ru, initial pressure is P2, and final pressure is P2.

Write the formula for entropy change in mass basis (s2s1)ideal.

(s2s1)ideal=(s¯2s¯1)idealM . (IV)

Refer table A-1, “Molar mass, gas constant and critical properties table”.

The molar mass (M) propane is 44.097kg/kmol.

Refer the table A-2 (c), “Ideal gas specific heats of various common gases”.

Obtain the empirical constants as follows.

a=4.04b=30.48×102c=15.72×105d=31.74×109

The universal gas constant (Ru) is 8.314kJ/kmolK.

Conclusion:

Convert the temperature T1,T2 from degree Celsius to Kelvin.

T1=100°C+273=373K

T2=500°C+273=773K

Substitute 4.04 for a, 773K for T2, 373K for T1, 30.48×102 for b, 15.72×105 for c, and 31.74×109 for d in Equation (I).

(h¯2h¯1)ideal={4.04(773K373K)+30.48×1022[(773K)2(373K)2]+15.72×1053[(773K)3(373K)3]+31.74×1094[(773K)4(373K)4]}=1616+69860.1621524.727+2679.5227=49398.9557kJ/kmol49440kJ/kmol

Substitute 49440kJ/kmol for (h¯2h¯1)ideal and 44.097kg/kmol for M in Equation (II)

win=49440kJ/kmol44.097kg/kmol=1121.1647kJ/kg1121kJ/kg

Thus, the work input of the compressor per unit mass by treating the propane as an ideal gas variable specific heats is 1121kJ/kg.

Substitute 4.04 for a, 773K for T2, 373K for T1, 30.48×102 for b, 15.72×105 for c, 31.74×109 for d, 4000kPa for P2, 500kPa for P1, and 8.314kJ/kmolK for Ru in

Equation (III).

(s¯2s¯1)ideal={(4.04)ln(773K373K)+30.48×102[(773K)(373K)]+15.72×1052[(773K)2(373K)2]+31.74×1093[(773K)3(373K)3](8.314kJ/kmolK)ln(4000kPa500kPa)}=2.9439+121.9236.0302+4.337717.2885=69.9951kJ/kmolK

Substitute 69.9951kJ/kmolK for (s¯2s¯1)ideal and 44.097kg/kmol for M in Equation (IV).

(s2s1)ideal=69.9951kJ/kmolK44.097kg/kmol=1.5873kJ/kgK

Thu, the change in entropy per unit mass by treating the propane as an ideal gas variable specific heats is 1.5873kJ/kgK.

b)

To determine

The entropy changes and the work input of the compressor per unit mass by using departure charts.

b)

Expert Solution
Check Mark

Answer to Problem 97RP

The work input of the compressor per unit mass by using enthalpy departure chart is 664.2kJ/kg.

The change in entropy per unit mass by using entropy departure chart is 0.8278kJ/kgK.

Explanation of Solution

Calculate the reduced temperature (TR1) at initial state.

TR1=T1Tcr (V)

Here, critical temperature is Tcr and initial temperature is T1.

Calculate the reduced pressure (PR1) at initial state.

PR1=P1Pcr (VI)

Here, critical pressure is Pcr and initial pressure is P1.

Calculate the reduced temperature (TR2) at final state.

TR2=T2Tcr (VII)

Here, critical temperature is Tcr and final temperature is T2.

Calculate the reduced pressure (PR2) at final state.

PR2=P2Pcr (VIII)

Here, critical pressure is Pcr and final pressure is P2.

Write the formula for change in enthalpy and change in entropy at ideal state.

(h2h1)ideal=cp(T2T1) (IX)

(s2s1)ideal=cplnT2T1RlnP2P1 (X)

Write the formula for change in enthalpy (h2h1) using generalized enthalpy departure chart relation.

h2h1=(h2h1)idealRTcr(Zh2Zh1) (XI)

Here, change in enthalpy of ideal gas is (h2h1)ideal, gas constant of propane is R, the enthalpy departure factor is Zh, and the subscripts 1 and 2 indicates initial and final states.

Write the formula for change in entropy (s2s1) using generalized entropy departure chart relation.

(s2s1)=(s2s1)idealRTcr(Zs2Zs1) (XII)

Here, change in entropy of ideal gas is (s2s1)ideal, and the entropy departure factor is Zs.

Refer Table A-1, “Molar mass, gas constant, and critical-point properties”.

The critical temperature and critical pressure of the propane is as follows.

Tcr=370KPcr=4.26MPa

Refer Table A-2 (a), “Ideal-gas specific heats of various common gases”.

The gas constant (R) of propane is 0.1885kJ/kgK.

The specific heat at constant pressure (cp) of propane is 1.6794kJ/kgK.

Conclusion:

Substitute 373K for T1 and 370K for Tcr in Equation (V).

TR1=373K370K=1.008

Substitute 500kPa for P1 and 4.26MPa for Pcr in Equation (VI).

PR1=500kPa4.26MPa=0.5MPa4.26MPa=0.117

Refer Figure A-29, “Generalized enthalpy departure chart”.

The enthalpy departure factor (Zh1) corresponding the reduced pressure (PR1) and reduced temperature (TR1) is 0.124.

Refer Figure A-30, “Generalized entropy departure chart”.

The entropy departure factor (Zs1) corresponding the reduced pressure (PR1) and reduced temperature (TR1) is 0.0837.

Substitute 773K for T2 and 370K for Tcr in Equation (VII).

TR2=773K370K=2.089

Substitute 4000kPa for P2 and 4.26MPa for Pcr in Equation (VIII).

PR2=4000kPa4.26MPa=4MPa4.26MPa=0.939

Refer Figure A-29, “Generalized enthalpy departure chart”.

The enthalpy departure factor (Zh2) corresponding the reduced pressure (PR2) and reduced temperature (TR2) is 0.233.

Refer Figure A-30, “Generalized entropy departure chart”.

The entropy departure factor (Zs2) corresponding the reduced pressure (PR2) and reduced temperature (TR2) is 0.105.

Substitute 1.6794kJ/kgK for cp, 773K for T2, and 373K for T1 in Equation (IX).

(h2h1)ideal=1.6794kJ/kgK(773K373K)=671.76kJ/kg671.8kJ/kg

Substitute 671.8kJ/kg for (h2h1)ideal, 0.233 for Zh2, 0.124 for Zh1, 0.1885kJ/kgK for R, and 370K for Tcr in Equation (XI).

h2h1=671.8kJ/kg(0.1885kJ/kgK)(370K)(0.2330.124)=671.8kJ/kg7.6022kJ/kg=664.19779664.2kJ/kg

Here, the work input of the compressor is equal to the enthalpy difference.

win=h2h1=664.2kJ/kg

Thus, the work input of the compressor per unit mass by using enthalpy departure chart is 664.2kJ/kg.

Substitute 1.6794kJ/kgK for cp, 773K for T2, 373K for T1, 0.1885kJ/kgK for R, 4000kPa for P2, and 500kPa for P1 in Equation (X).

(s2s1)ideal=((1.6794kJ/kgK)ln(773K373K)(0.1885kJ/kgK)ln(4000kPa500kPa))=1.2238kJ/kgK0.3919kJ/kgK=0.8318kJ/kgK

Substitute 0.8318kJ/kgK for (s2s1)ideal, 0.105 for Zs2, 0.0837 for Zs1 and 0.1885kJ/kgK for R in Equation (XII).

s2s1=0.8318kJ/kgK(0.1885kJ/kgK)(0.1050.0837)=0.8318kJ/kgK0.004015kJ/kgK=0.82778kJ/kgK0.8278kJ/kgK

Thus, the change in entropy per unit mass by using entropy departure chart is 0.8278kJ/kgK.

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Chapter 12 Solutions

Thermodynamics: An Engineering Approach ( 9th International Edition ) ISBN:9781260092684

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