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 7.13, Problem 180RP

Air enters the evaporator section of a window air conditioner at 100 kPa and 27°C with a volume flow rate of 6 m3/min. The refrigerant-134a at 120 kPa with a quality of 0.3 enters the evaporator at a rate of 2 kg/min and leaves as saturated vapor at the same pressure. Determine the exit temperature of the air and the rate of entropy generation for this process, assuming (a) the outer surfaces of the air conditioner are insulated and (b) heat is transferred to the evaporator of the air conditioner from the surrounding medium at 32°C at a rate of 30 kJ/min.

Chapter 7.13, Problem 180RP, Air enters the evaporator section of a window air conditioner at 100 kPa and 27C with a volume flow

FIGURE P7–180

a)

Expert Solution
Check Mark
To determine

The exit temperature of air and the entropy generated during the process.

Answer to Problem 180RP

The exit temperature of air is 15.9°C.

The entropy generated during the process is 0.00196kW/K.

Explanation of Solution

Write the expression to calculate the initial enthalpy of the refrigerant.

h1=hf+x1hfg (I)

Here, initial enthalpy is h1, saturated liquid enthalpy is hf, initial vapor quality is x1 and evaporated enthalpy is hfg.

Write the expression to calculate the initial entropy of the refrigerant.

s1=sf+x1sfg (II)

Here, initial entropy is s1, saturated liquid entropy is sf, initial vapor quality is x1 and evaporated entropy is sfg.

Write the expression to calculate the mass flow rate of air.

m˙air=P3V˙3RT3 (III)

Here, mass flow rate of air is m˙air, inlet pressure of air is P3, volumetric flow rate is V˙3, gas constant is R and inlet temperature of air is T3.

Write the expression for the mass balance of the system.

m˙inm˙out=Δm˙system (IV)

Here, mass flow rate into the control system is m˙in, mass flow rate exit from the control volume is m˙out and mass flow rate change in the system is Δm˙system.

Write the expression for the energy balance equation for closed system.

E˙inE˙out=ΔE˙system (V)

Here, rate of energy transfer into the control volume is E˙in, rate of energy transfer exit from the control volume is E˙out and rate of change in internal energy of system is ΔE˙system

Write the expression for the rate of entropy balance for the system.

S˙inS˙out+S˙gen=ΔS˙system (VI)

Here, rate of entropy in the system is S˙in, rate of entropy exit from the system is S˙out, rate of entropy generated is S˙gen and rate of change of entropy in the system is ΔS˙system.

Conclusion:

From Table A-12, “Saturated refrigerant-134a-Pressure table”, Obtain the following properties at saturated pressure of 120 kPa

Saturated liquid enthalpy, hf=22.47kJ/kg

Evaporated enthalpy, hfg=214.52kJ/kg

Saturated vapor enthalpy, h2=hg@120kPa=236.99kJ/kg

Saturated vapor entropy, s2=sg@120kPa=0.9479kJ/kgK

Saturated liquid entropy, sf=0.09269kJ/kgK

Evaporated entropy, sfg=0.85520kJ/kgK

Substitute 22.47kJ/kg for hf, 0.3 for x1 and 214.52kJ/kg for hfg in Equation (I).

h1=22.47kJ/kg+(0.3)(214.52kJ/kg)=86.83kJ/kg

Substitute 0.09269kJ/kgK for sf, 0.3 for x1 and 0.85520kJ/kgK for sfg in Equation (II).

s1=0.09269kJ/kgK+(0.3)(0.85520kJ/kgK)=0.3492kJ/kgK

Refrigerant –134a enters and leaves at the same pressure. Hence, P2=P1

From Table A-1E, “the molar mass, gas constant and critical–point properties table”, select the gas constant of air at room temperature as 0.287kJ/kgK.

Substitute 100 kPa for P3, 6m3/min for V˙3, 0.287kJ/kgK for R and 27 C for T3 in Equation (III).

m˙air==(100kPa)(6m3/min)(0.287kJ/kgK)27°C=(100kPa)(6m3/min)(0.287kJ/kgK)(1kPam31kJ)(27+273)K=6.968kg/min

Substitute m˙1 for m˙in, m˙2 for m˙out and 0 for Δm˙system in Equation (I).

m˙1m˙2=0m˙1=m˙2=m˙R

Here, mass flow rate of refrigerant is m˙R.

Substitute m˙3 for m˙in, m˙4 for m˙out and 0 for Δm˙system in Equation (IV).

m˙3m˙4=0m˙3=m˙4=m˙air

Here, mass flow rate of air is m˙air.

Substitute m˙1h1+m˙3h3 for E˙in, m˙2h2+m˙4h4 for E˙out and 0 for ΔE˙system in Equation (V).

m˙1h1+m˙3h3(m˙2h2+m˙4h4)=0m˙1h1+m˙3h3=m˙2h2+m˙4h4

m˙R(h2h1)=m˙air(h3h4)m˙R(h2h1)=m˙aircp(T3T4)T4=T3m˙R(h2h1)m˙aircp (VII)

From the Table A-2, “Ideal-gas specific heats of various common gases”, select the value of the specific heat at constant pressure value of air as 1.005kJ/kgK.

Substitute 27 C for T3, 2kg/min for m˙R, 236.99kJ/kg for h2, 86.83kJ/kg for h1, 6.968kg/min for m˙air and 1.005kJ/kgK for cp in Equation (VII).

T4=27°C(2kg/min)(236.99kJ/kg86.83kJ/kg)(6.968kg/min)(1.005kJ/kgK)=15.9°C

Hence, the exit temperature of air is 15.9°C.

For the steady flow system, change of entropy in the system is zero.

Substitute m˙1s1+m˙3s3 for S˙in, m˙2s2+m˙4s4 for S˙out, 0 for ΔS˙system in Equation (VI).

m˙1s1+m˙3s3(m˙2s2+m˙4s4)+S˙gen=0S˙gen=m˙R(s2s1)+m˙air(s4s3)=m˙R(s2s1)+m˙air(cpln(T4T3)Rln(P4P3)) (VIII)

Substitute 2kg/min for m˙R, 0.9479kJ/kgK for s2, 0.3492kJ/kgK for s1, 6.968kg/min for m˙air, 1.005kJ/kgK for cp, –15.9 C for T4, 27 C for T3, and P4 for P3 in Equation (VIII).

S˙gen={2kg/min(0.9479kJ/kgK0.3492kJ/kgK)+6.968kg/min(1.005kJ/kgKln(15.9°C27°C)Rln(P4P4))}

S˙gen={2kg/min(0.9479kJ/kgK0.3492kJ/kgK)+6.968kg/min(1.005kJ/kgKln((15.9+273)K(27+273)K)Rln(P4P4))}=1.1974(6.968)0.1551=0.1175kJ/minK(1min60sec)=0.00196kW/K

Hence, the entropy generated during the process is 0.00196kW/K.

b)

Expert Solution
Check Mark
To determine

The exit temperature of air and the entropy generated during the process.

Answer to Problem 180RP

The exit temperature of air is 11.6°C.

The entropy generated during the process is 0.00225kW/K.

Explanation of Solution

Write the expression for the energy balance equation for closed system.

E˙inE˙out=ΔE˙system (IX)

Here, rate of energy transfer into the control volume is E˙in, rate of energy transfer exit from the control volume is E˙out and rate of change in internal energy of system is ΔE˙system

Write the expression for the rate of entropy balance for the system.

S˙inS˙out+S˙gen=ΔS˙system (X)

Here, rate of entropy in the system is S˙in, rate of entropy exit from the system is S˙out, rate of entropy generated is S˙gen and rate of change of entropy in the system is ΔS˙system.

Conclusion:

Substitute m˙1h1+m˙3h3+Q˙in for E˙in, m˙2h2+m˙4h4 for E˙out and 0 for ΔE˙system in Equation (IX).

m˙1h1+m˙3h3+Q˙in(m˙2h2+m˙4h4)=0m˙1h1+m˙3h3+Q˙in=m˙2h2+m˙4h4Q˙in=m˙R(h2h1)+m˙aircp(T4T3)T4=T3+Q˙inm˙R(h2h1)m˙aircp (XI)

Here, rate of heat gain from the surrounding is Q˙in

Substitute 27 C for T3, 30kJ/min for Q˙in, 2kg/min for m˙R, 236.99kJ/kg for h2, 86.83kJ/kg for h1, 6.968kg/min for m˙air and 1.005kJ/kgK for cp in Equation (XI).

T4=27°C+30kJ/min(2kg/min)(236.99kJ/kg86.83kJ/kg)(6.968kg/min)(1.005kJ/kgK)=11.6°C

Hence, the exit temperature of air is 11.6°C.

For the steady flow system, change of entropy in the system is zero.

Substitute m˙1s1+m˙3s3+Q˙inTsurr for S˙in, m˙2s2+m˙4s4 for S˙out, 0 for ΔS˙system in Equation (I).

m˙1s1+m˙3s3+Q˙inTsurr(m˙2s2+m˙4s4)+S˙gen=0S˙gen=m˙R(s2s1)+m˙air(s4s3)Q˙inTsurrS˙gen=m˙R(s2s1)+m˙air(cpln(T4T3)Rln(P4P3))Q˙inTsurr (XII)

Substitute 2kg/min for m˙R, 0.9479kJ/kgK for s2, 0.3492kJ/kgK for s1, 6.968kg/min for m˙air, 1.005kJ/kgK for cp, –11.6 C for T4, 27 C for T3,P4 for P3, 30kJ/min for Q˙in, and 32 C for Tsurr in Equation (XII).

S˙gen={2kg/min(0.9479kJ/kgK0.3492kJ/kgK)+6.968kg/min(1.005kJ/kgKln(11.6°C27°C)Rln(P4P4))30kJ/min32°C}

S˙gen={2kg/min(0.9479kJ/kgK0.3492kJ/kgK)+6.968kg/min(1.005kJ/kgKln((11.6+273)K(27+273)K)Rln(P4P4))30kJ/min(32+273)K}=1.1974+(6.968)(0.1384)0.09836=0.1348kJ/minK(1min60sec)=0.00225kW/K

Hence, the entropy generated during the process is 0.00225kW/K.

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Chapter 7 Solutions

Thermodynamics: An Engineering Approach

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