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  • 7/30/2019 Heat Chap13 054

    1/17

    Chap 15Heat Exchangers

    13-54 Glycerin is heated by ethylene glycol in a thin-walled double-pipe parallel-flow heat exchanger. Therate of heat transfer, the outlet temperature of the glycerin, and the mass flow rate of the ethylene glycolare to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant. 6 The thermal resistance of the inner tube is negligible since

    the tube is thin-walled and highly conductive.Properties The specific heats of glycerin and ethyleneglycol are given to be 2.4 and 2.5 kJ/kg.C,respectively.

    Analysis (a) The temperature differences at thetwo ends are

    T T T

    T T T T T

    h in c in

    h out c out h out h out

    1

    2

    60 20

    15

    = =

    = =

    , ,

    , , , ,(

    C C = 40 C

    C) = 15 C

    and

    T

    T T

    T Tlm =

    =

    = 1 2

    1 2

    40 15

    40 15255

    ln( / ) ln( / ). C

    Then the rate of heat transfer becomes

    kW19.58==== W584,19C)5.25)(mC)(3.2.W/m240( 22lms TUAQ

    (b) The outlet temperature of the glycerin is determined from

    C47.2=

    +=+==C)kJ/kg.kg/s)(2.43.0(

    kW584.19C20)]([ glycerin

    pinoutinoutp

    Cm

    QTTTTCmQ

    (c) Then the mass flow rate of ethylene glycol becomes

    kg/s3.56=

    =

    =

    =

    C]60C15)+C)[(47.2kJ/kg.(2.5

    kJ/s584.19

    )(

    )]([

    glycolethylene

    glycolethylene

    outinp

    outinp

    TTC

    Qm

    TTCmQ

    13-37

    Glycerin20C0.3 kg/s

    Hot ethylene

    60C3 kg/s

  • 7/30/2019 Heat Chap13 054

    2/17

    Chap 15Heat Exchangers

    13-55 Air is preheated by hot exhaust gases in a cross-flow heat exchanger. The rate of heat transfer andthe outlet temperature of the air are to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant.

    Properties The specific heats of air and combustion gases are given to be 1005 and 1100 J/kg.C,respectively.

    Analysis The rate of heat transfer is

    kW103=

    C)95CC)(180kJ/kg.kg/s)(1.11.1(

    )]([ gas.

    =

    = outinp TTCmQ

    The mass flow rate of air is

    ( ..m

    PV

    RT= =

    =(95 kPa)(0.8 m / s)

    kPa. m / kg. K) K kg / s

    3

    30 287 293

    0904

    Then the outlet temperature of the air becomes

    C133=

    +=+=

    =

    C)J/kg.kg/s)(1005904.0(

    W10103C20

    )(

    3

    ,,

    ,,

    pincoutc

    incoutcp

    Cm

    QTT

    TTCmQ

    13-38

    Air95 kPa20C

    0.8 m3/s

    Exhaust gases

    1.1 kg/s95C

  • 7/30/2019 Heat Chap13 054

    3/17

    Chap 15Heat Exchangers

    13-56 Water is heated by hot oil in a 2-shell passes and 12-tube passes heat exchanger. The heat transfersurface area on the tube side is to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant.

    Properties The specific heats of water and oil are given to be 4.18 and 2.3 kJ/kg.C, respectively.

    Analysis The rate of heat transfer in this heat exchanger is

    [ ( )] ( .Q mC T T p out in= = water kg / s)(4.18 kJ / kg. C)(70 C C) = 940.5 kW4 5 20

    The outlet temperature of the hot water is determined from

    C129C)kJ/kg.kg/s)(2.310(

    kW5.940C170)]([ oil =

    ===

    pinoutoutinp

    Cm

    QTTTTCmQ

    The logarithmic mean temperature difference for counter-flow arrangement and the correction factor F are

    C109=C20C129

    C100=C70C170

    ,,2

    ,,1

    ==

    ==

    incouth

    outcinh

    TTT

    TTT

    C105)109/100ln(

    109100

    )/ln( 21

    21, =

    =

    =

    TT

    TTT CFlm

    0.1

    2.1170129

    7020

    27.017020

    170129

    12

    21

    11

    12

    =

    =

    =

    =

    =

    =

    =

    F

    tt

    TTR

    tT

    ttP

    Then the heat transfer surface area on the tube side becomes

    2

    m15=

    =

    ==

    C)105(C)(1.0).kW/m6.0(

    kW5.940

    2,

    ,CFlm

    sCFlms TUF

    Q

    ATFUAQ

    13-39

    Oil170C10 kg/s

    Water20C

    4.5 kg/s

    70C

    (12 tube passes)

  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    13-57 Water is heated by hot oil in a 2-shell passes and 12-tube passes heat exchanger. The heat transfersurface area on the tube side is to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant.

    Properties The specific heats of water and oil are given to be 4.18 and 2.3 kJ/kg.C, respectively.

    Analysis The rate of heat transfer in this heat exchanger is

    [ ( )] (Q mC T T p out in= = water kg / s)(4.18 kJ / kg. C)(70 C C) = 418 kW2 20

    The outlet temperature of the oil is determined from

    C8.151C)kJ/kg.kg/s)(2.310(

    kW418C170)]([ oil =

    ===

    pinoutoutinp

    Cm

    QTTTTCmQ

    The logarithmic mean temperature difference for counter-flow arrangement and the correction factor F are

    T T T

    T T T

    h in c out

    h out c in

    1

    2

    170 70

    1518 20

    = =

    = =

    , ,

    , , .

    C C = 100 C

    C C = 131.8 C

    T

    T T

    T Tlm CF,

    ln( / )

    .

    ln( / . ).=

    =

    = 1 2

    1 2

    100 1318

    100 1318115 2 C

    }

    0.1

    7.21708.151

    7020

    12.017020

    1708.151

    12

    21

    11

    12

    =

    =

    =

    =

    =

    =

    =

    F

    tt

    TTR

    tT

    ttP

    Then the heat transfer surface area on the tube side becomes

    2m6.05=

    =

    ==C)2.115(C)(1.0).kW/m6.0(

    kW418

    2,, CFlmiiCFlmii TFU

    QATFAUQ

    13-40

    Oil

    170C10 kg/s

    Water20C2 kg/s

    70C

    (12 tube passes)

  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    13-58 Ethyl alcohol is heated by water in a 2-shell passes and 8-tube passes heat exchanger. The heattransfer surface area of the heat exchanger is to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant.

    Properties The specific heats of water and ethyl alcohol are given to be 4.19 and 2.67 kJ/kg.C,respectively.

    Analysis The rate of heat transfer in this heat exchanger is

    kW252.3=C)25CC)(70kJ/kg.kg/s)(2.671.2()]([ alcoholethyl == inoutp TTCmQ

    The logarithmic mean temperature difference for counter-flow arrangement and the correction factor F are

    T T T

    T T T

    h in c out

    h out c in

    1

    2

    95 70

    45 25

    = =

    = =

    , ,

    , ,

    C C = 25 C

    C C = 20 C

    T

    T T

    T Tlm CF,

    ln( / ) ln( / ).=

    =

    = 1 2

    1 2

    25 20

    25 2022 4 C

    77.0

    9.09545

    7025

    7.09525

    9545

    12

    21

    11

    12

    =

    =

    =

    =

    =

    =

    =

    F

    tt

    TTR

    tT

    ttP

    Then the heat transfer surface area on the tube side becomes

    2m15.4=

    =

    ==C)4.22(C)(0.77).kW/m950.0(

    kW3.2522

    ,

    ,

    CFlmi

    iCFlmiiTFU

    QATFAUQ

    13-41

    Water90C

    EthylAlcohol

    25C2.1 kg/s

    70C

    (8 tube passes)

    45C

  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    13-59 Water is heated by ethylene glycol in a 2-shell passes and 12-tube passes heat exchanger. The rateof heat transfer and the heat transfer surface area on the tube side are to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant.

    Properties The specific heats of water and ethylene glycol are given to be 4.18 and 2.68 kJ/kg.C,respectively.

    Analysis The rate of heat transfer in this heat exchanger is :

    kW160.5=C)22CC)(70kJ/kg.kg/s)(4.188.0()]([ water == inoutp TTCmQ

    The logarithmic mean temperature difference for counter-flow arrangement and the correction factor F are

    T T T

    T T T

    h in c out

    h out c in

    1

    2

    110 70

    60 22

    = =

    = =

    , ,

    , ,

    C C = 40 C

    C C = 38 C

    T

    T T

    T Tlm CF,

    ln( / ) ln( / )=

    =

    = 1 2

    1 2

    40 38

    40 3839 C

    94.0

    96.011060

    7022

    57.011022

    11060

    12

    21

    11

    12

    =

    =

    =

    =

    =

    =

    =

    F

    tt

    TTR

    tT

    ttP

    Then the heat transfer surface area on the tube side becomes

    2m15.6=

    =

    ==C)39(C)(0.94).kW/m28.0(

    kW5.1602

    ,

    ,

    CFlmi

    iCFlmiiTFU

    QATFAUQ

    13-42

    Ethylene110C

    Water22C

    0.8 kg/s

    70C

    (12 tube passes)

    60C

  • 7/30/2019 Heat Chap13 054

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  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    0.25 0.65 1.05 1.45 1.85 2.25

    50

    10 0

    15 0

    20 0

    25 0

    30 0

    35 0

    40 0

    45 0

    5

    10

    15

    20

    25

    30

    35

    40

    45

    mw[kg/s]

    Q

    [kW]

    A

    m2

    heat

    area

    13-44

  • 7/30/2019 Heat Chap13 054

    9/17

    Chap 15Heat Exchangers

    13-61E Steam is condensed by cooling water in a condenser. The rate of heat transfer, the rate ofcondensation of steam, and the mass flow rate of cold water are to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant. 6 The thermal resistance of the inner tube is negligible sincethe tube is thin-walled and highly conductive.

    Properties We take specific heat of water are given to be1.0 Btu/lbm.F. The heat of condensation of steam at 90Fis 1043 Btu/lbm.

    Analysis (a) The log mean temperature difference isdetermined from

    T T T

    T T T

    h in c out

    h out c in

    1

    2

    90 73

    90 60

    = =

    = =

    , ,

    , ,

    F F = 17 F

    F F = 30 F

    T

    T T

    T Tlm CF,

    ln( / ) ln( / ).=

    =

    = 1 2

    1 2

    17 30

    17 3022 9 F

    The heat transfer surface area is

    2ft7.392ft)ft)(548/3(5088 === DLnAs

    and

    Btu/h105.396 6=== F)9.22)(ftF)(392.7.Btu/h.ft600( 22lms TUAQ

    (b) The rate of condensation of the steam is

    lbm/s1.44=lbm/h5173=

    ===Btu/lbm1043

    Btu/h10396.5)(

    6

    fgsteamsteamfg

    h

    QmhmQ

    (c) Then the mass flow rate of cold water becomes

    lbm/s115lbm/h104.15 5 ==

    =

    =

    =

    F]60FF)(73Btu/lbm.(1.0

    Btu/h10396.5

    )(

    )]([

    6

    watercold

    watercold

    inoutp

    inoutp

    TTC

    Qm

    TTCmQ

    13-45

    Steam90F20 lbm/s

    60F

    Water

    73F

    90F

  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    13-62"!PROBLEM 13-62E"

    "GIVEN"N_pass=8N_tube=50"T_steam=90 [F], parameter to be varied"h_fg_steam=1043 "[Btu/lbm]"

    T_w_in=60 "[F]"T_w_out=73 "[F]"C_p_w=1.0 "[Btu/lbm-F]"D=3/4*1/12 "[ft]"L=5 "[ft]"U=600 "[Btu/h-ft^2-F]"

    "ANALYSIS""(a)"DELTAT_1=T_steam-T_w_outDELTAT_2=T_steam-T_w_inDELTAT_lm=(DELTAT_1-DELTAT_2)/ln(DELTAT_1/DELTAT_2)A=N_pass*N_tube*pi*D*L

    Q_dot=U*A*DELTAT_lm*Convert(Btu/h, Btu/s)"(b)"Q_dot=m_dot_steam*h_fg_steam"(c)"Q_dot=m_dot_w*C_p_w*(T_w_out-T_w_in)

    Tsteam [F] Q [Btu/s] msteam[lbm/s] mw [lbm/s]

    80 810.5 0.7771 62.34

    82 951.9 0.9127 73.23

    84 1091 1.046 83.89

    86 1228 1.177 94.42

    88 1363 1.307 104.990 1498 1.436 115.2

    92 1632 1.565 125.694 1766 1.693 135.8

    96 1899 1.821 146.1

    98 2032 1.948 156.3

    100 2165 2.076 166.5

    102 2297 2.203 176.7

    104 2430 2.329 186.9

    106 2562 2.456 197.1

    108 2694 2.583 207.2110 2826 2.709 217.4

    112 2958 2.836 227.5

    114 3089 2.962 237.6

    116 3221 3.088 247.8

    118 3353 3.214 257.9

    120 3484 3.341 268

    13-46

  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    80 85 90 95 100 105 110 115 120

    50 0

    1000

    1500

    2000

    2500

    3000

    3500

    0. 5

    1

    1. 5

    2

    2. 5

    3

    3. 5

    Tsteam

    [F]

    Q

    [Btu/s]

    msteam

    [lbm/s]

    heat

    msteam

    80 85 90 95 100 105 110 115 12050

    95

    14 0

    18 5

    23 0

    27 5

    Tsteam[F ]

    mw

    [lbm/s]

    13-47

  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    13-63 Glycerin is heated by hot water in a 1-shell pass and 13-tube passes heat exchanger. The mass flowrate of glycerin and the overall heat transfer coefficient of the heat exchanger are to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant.

    Properties The specific heats of water and glycerin are given to be 4.18 and 2.48 kJ/kg.C, respectively.

    Analysis The rate of heat transfer in this heat exchanger is

    [ ( )] (5Q mC T T p in out= = water kg / s)(4.18 kJ / kg. C)(100 C C) = 940.5 kW55

    The mass flow rate of the glycerin is determined from

    kg/s9.5=

    =

    =

    =

    C]15CC)[(55kJ/kg.(2.48

    kJ/s5.940

    )(

    )]([

    glycerin

    glycerin

    inoutp

    inoutp

    TTC

    Qm

    TTCmQ

    The logarithmic mean temperature difference for counter-flow arrangement and the correction factor F are

    T T T

    T T T

    h in c out

    h out c in

    1

    2

    100 55

    55 15= = = =

    , ,

    , ,

    C C = 45 C

    C C = 40 C

    T

    T T

    T Tlm CF,

    ln( / ) ln( / ).=

    =

    = 1 2

    1 2

    45 40

    45 4042 5 C

    77.0

    89.010055

    5515

    53.010015

    10055

    12

    21

    11

    12

    =

    =

    =

    =

    =

    =

    =

    F

    tt

    TTR

    tT

    ttP

    The heat transfer surface area is

    2m0.94=m)m)(2015.0(10 == DLnAs

    Then the overall heat transfer coefficient of the heat exchanger is determined to be

    C.kW/m30.6 2 =

    =

    ==C)5.42)(77.0)(m94.0(

    kW5.9402

    ,,

    CFlmsCFlms

    TFA

    QUTFUAQ

    13-48

    Glycerin15C

    100C

    Hot Water5 kg/s

    55C

    55C

  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    13-64 Isobutane is condensed by cooling air in the condenser of a power plant. The mass flow rate of airand the overall heat transfer coefficient are to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant.

    Properties The heat of vaporization of isobutane at 75C is given to be hfg = 255.7 kJ/kg and specific heatof air is given to be Cp = 1005 J/kg.C.

    Analysis First, the rate of heat transfer is determined from

    kW39.690)kJ/kg7.255)(kg/s7.2()( isobutane === fghmQ

    The mass flow rate of air is determined from

    kg/s98.14=

    C)21CC)(28kJ/kg.(1.005

    kJ/s39.690

    )(

    )]([

    inoutair

    airinout

    =

    =

    =

    TTC

    Qm

    TTCmQ

    p

    p

    The temperature differences between the isobutane andthe air at the two ends of the condenser are

    C47=C28C75

    C54=C21C75

    inc,outh,2

    outc,inh,1

    ==

    ==

    TTT

    TTT

    and

    C4.50)47/54ln(

    4754

    )/ln( 21

    21lm =

    =

    =

    TT

    TTT

    Then the overall heat transfer coefficient is determined from

    C.W/m571 2 == =C)4.50)(m(24W390,690 2lm UUTUAQ s

    13-49

    Isobutane

    75C2.7 kg/s

    Air21C

    Air28C

  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    13-65 Water is evaporated by hot exhaust gases in an evaporator. The rate of heat transfer, the exittemperature of the exhaust gases, and the rate of evaporation of water are to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant.

    Properties The heat of vaporization of water at 200C is given to be hfg = 1941 kJ/kg and specific heat ofexhaust gases is given to be Cp = 1051 J/kg.C.

    Analysis The temperature differences between the waterand the exhaust gases at the two ends of the evaporator are

    C)200(

    C350=C200C550

    outh,inc,outh,2

    outc,inh,1

    ==

    ==

    TTTT

    TTT

    and

    [ ])200/(350ln)200(350

    )/ln( outh,

    outh,

    21

    21lm

    =

    =

    T

    T

    TT

    TTT

    Then the rate of heat transfer can be expressed as

    [ ])200/(350ln)200(350

    )m5.0)(C.kW/m780.1(outh,

    outh,22lm

    ==

    T

    TTUAQ s

    (Eq. 1)

    The rate of heat transfer can also be expressed as in the following forms

    )CC)(550kJ/kg.51kg/s)(1.025.0()]([ outh,gasesexhaustouth,inh, TTTCmQ p ==

    (Eq. 2)

    )kJ/kg1941()( waterwater mhmQ fg == (Eq. 3)

    We have three equations with three unknowns. Using an equation solver such as EES, the unknowns aredetermined to be

    Q

    T

    m

    =

    =

    =

    88.85 kW

    211.8 C

    0.0458 kg/ s

    h,out

    water

    13-50

    Water200C

    550F

    Exhaustgases

    Th,out

    200C

  • 7/30/2019 Heat Chap13 054

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    Chap 15Heat Exchangers

    13-66 "!PROBLEM 13-66"

    "GIVEN""T_exhaust_in=550 [C], parameter to be varied"C_p_exhaust=1.051 "[kJ/kg-C]"m_dot_exhaust=0.25 "[kg/s]"

    T_w=200 "[C]"

    h_fg_w=1941 "[kJ/kg]"A=0.5 "[m^2]"U=1.780 "[kW/m^2-C]"

    "ANALYSIS"DELTAT_1=T_exhaust_in-T_wDELTAT_2=T_exhaust_out-T_wDELTAT_lm=(DELTAT_1-DELTAT_2)/ln(DELTAT_1/DELTAT_2)Q_dot=U*A*DELTAT_lmQ_dot=m_dot_exhaust*C_p_exhaust*(T_exhaust_in-T_exhaust_out)Q_dot=m_dot_w*h_fg_w

    Texhaust,in [C] Q [kW] Texhaust,out [C] mw [kg/s]

    300 25.39 203.4 0.01308

    320 30.46 204.1 0.0157

    340 35.54 204.7 0.01831

    360 40.62 205.4 0.02093

    380 45.7 206.1 0.02354

    400 50.77 206.8 0.02616420 55.85 207.4 0.02877

    440 60.93 208.1 0.03139

    460 66.01 208.8 0.03401

    480 71.08 209.5 0.03662

    500 76.16 210.1 0.03924

    520 81.24 210.8 0.04185540 86.32 211.5 0.04447

    560 91.39 212.2 0.04709580 96.47 212.8 0.0497

    600 101.5 213.5 0.05232

    13-51

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    Chap 15Heat Exchangers

    300 350 400 450 500 550 600

    20

    30

    40

    50

    60

    70

    80

    90

    10 0

    11 0

    20 2

    20 4

    20 6

    20 8

    21 0

    21 2

    21 4

    Texhaust,in

    [C ]

    Q

    [kW]

    T

    C

    heat

    temperature

    300 350 400 450 500 550 600

    0.01

    0.015

    0.02

    0.025

    0.03

    0.035

    0.04

    0.045

    0.05

    0.055

    Texhaust,in

    [C]

    mw

    [kg/s]

    13-52

  • 7/30/2019 Heat Chap13 054

    17/17

    Chap 15Heat Exchangers

    13-67 The waste dyeing water is to be used to preheat fresh water. The outlet temperatures of each fluidand the mass flow rate are to be determined.

    Assumptions1 Steady operating conditions exist. 2 The heat exchanger is well-insulated so that heat lossto the surroundings is negligible and thus heat transfer from the hot fluid is equal to the heat transfer tothe cold fluid. 3 Changes in the kinetic and potential energies of fluid streams are negligible. 4 There isno fouling. 5 Fluid properties are constant.

    Properties The specific heats of waste dyeing water and the fresh water are given to be Cp = 4295 J/kg.Cand Cp = 4180 J/kg.C, respectively.

    Analysis The temperature differences between the dyeing waterand the fresh water at the two ends of the heat exchanger are

    15

    75

    outh,inc,outh,2

    outc,outc,inh,1

    ==

    ==

    TTTT

    TTTT

    and

    [ ])15/()75(ln)15()75(

    )/ln( outh,outc,

    outh,outc,

    21

    21lm

    =

    =

    TT

    TT

    TT

    TTT

    Then the rate of heat transfer can be expressed as

    [ ])15/()75(ln)15()75(

    )m65.1)(C.kW/m625.0(kW35outh,outc,

    outh,outc,22

    lm

    =

    =

    TT

    TT

    TUAQ s

    (Eq. 1)

    The rate of heat transfer can also be expressed as

    )CC)(75kJ/kg.(4.295kW35)]([ outh,waterdyeingouth,inh, TmTTCmQ p ==

    (Eq. 2)

    C)15C)(kJ/kg.(4.18kW35)]([ outc,waterdyeingouth,inh, == TmTTCmQ p

    (Eq. 3)

    We have three equations with three unknowns. Using an equation solver such as EES, the unknowns are

    determined to be

    T

    T

    m

    c,out

    h,out

    =

    =

    =

    41.4 C

    49.3 C

    0.317 kg/ s

    13-53

    Freshwater15C

    Dyeingwater

    75C

    Tc,out

    Th,out