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    OBSERVED DATA

    Shell: Nominal size 6

    Schedule no = 40

    Tubes:Number of tubes = 19

    OD = 0.5 inch

    BWG = 16

    Length = 96 inch

    Pump: Centrifugal pump, 1.5kW; 240V; 50Hz; 2900rpm; Hmax=38m; Qmax=250l/h

    Weight of the empty bucket W1= 1.5 kg

    Table 01: Observed data for Study of shell and tube heat exchanger

    No

    of

    Obs

    Steam

    Pressure

    (psig)

    Flow

    meter

    reading

    (L)

    Water

    Temperature

    (C)

    Weight of

    condensat

    e

    +

    bucket

    (kg)

    TimeManometer

    Reading

    Inlet

    (T1)

    Outlet

    (T2)

    Water

    (sec)

    Condensate

    (min)

    Left

    (inch)

    Right

    (inch)

    1

    2.5

    10 24.5 32 2.45 11.1 2 33 36

    2 10 24.5 31 2.7 8.79 2 32 36.7

    3 10 24.5 30.5 3 6.91 2 30.6 37.5

    4 10 24.5 29.5 3.2 5.54 2 27.5 38.8

    5

    5

    10 27 34.5 3.1 10.09 2 32.6 36.4

    6 10 27 33.5 3.65 8.6 2 31.5 37

    7 10 27 32.5 3.75 7 2 30.1 37.5

    8 10 27 31 3.9 5.72 2 27.4 38.8

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    CALCULATED DATA

    Table 02: Calculated data for Mean, Saturation, Film and Wall temperature and Heat of

    condensation and manometer reading in meter

    No

    of

    Obs

    Saturation

    Temperature,

    Ts (C)

    Mean

    Temperature,

    Tm(C)

    Film

    Temperature,

    Tf(C)

    Wall

    Temperature,

    Tw(C)

    Heat of

    Condensation

    hfg(kJ/kg)

    Manometer

    Reading

    Left

    (m)Right

    (m)

    1 104.44 28.25 75.86875 66.345 2244.6 0.8382 0.9144

    2 104.44 27.75 75.68125 66.095 2244.6 0.8128 0.93218

    3 104.44 27.5 75.5875 65.97 2244.6 0.77724 0.9525

    4 104.44 27 75.4 65.72 2244.6 0.6985 0.98552

    5 108.39 30.75 79.275 69.57 2234 0.82804 0.92456

    6 108.39 30.25 79.0875 69.32 2234 0.8001 0.9398

    7 108.39 29.75 78.9 69.07 2234 0.76454 0.9525

    8 108.39 29 78.61875 68.695 2234 0.69596 0.98552

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    Table 03: Calculated data for properties of water at mean temperature and properties of

    condensate at film temperature

    No

    of

    Obs

    Properties of water at mean temperatureProperties of condensate at film

    temperature

    Density

    (kg/m3)

    Viscosity

    (kg/m.s)

    Cp

    (kJ/kg.C)

    Thermal

    conductivity

    (W/m.C)

    Density

    (kg/m3)

    Viscosity

    (kg/m.s)

    Thermal

    conductivity

    (W/m.C)

    1 995.96 0.00083865 4.18056775 0.6165596 974.27875 0.00037466 0.6684263

    2 996.12 0.00084655 4.18063425 0.6157496 974.39125 0.00037559 0.6682913

    3 996.2 0.0008505 4.1806675 0.6153446 974.4475 0.00037606 0.6682238

    4 996.36 0.0008584 4.180734 0.6145346 974.56 0.000377 0.6680888

    5 995.16 0.00079915 4.18023525 0.6206096 972.235 0.00035763 0.6708788

    6 995.32 0.00080705 4.18030175 0.6197996 972.3475 0.00035856 0.6707438

    7 995.48 0.00081495 4.18036825 0.6189896 972.46 0.0003595 0.6706088

    8 995.72 0.0008268 4.180468 0.6177746 972.62875 0.00036091 0.6704063

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    Table 04: Calculated data for water and condensate flow rate, Heat rate of water and steam

    and mean heat rate

    No of

    Obs

    Water

    Flow

    Rate, mw

    (kg/s)

    Condens

    ate Flow

    rate, mc

    (kg/s)

    Heat

    absorbed

    by water

    Qw(kW)

    Heat

    released by

    steam, Qc

    (kW)

    Heat loss

    (kW)

    Percent

    heat loss

    Mean Heat

    Flow, Qm

    (kW)

    1 0.89726 0.00791 28.1329612 17.76975 -10.363 -58.31 22.9513556

    2 1.13324 0.01 30.7948658 22.446 -8.3488 -37.19 26.6204329

    3 1.44167 0.0125 36.1630764 28.0575 -8.1055 -28.88 32.1102882

    4 1.79848 0.01416 37.5949109 31.7985 -5.7964 -18.22 34.6967055

    5 0.98628 0.0133 30.9217263 29.7866667 -1.1350 -3.81 30.3541965

    6 1.15734 0.01791 31.4474379 40.0258333 8.57839 21.43 35.7366356

    7 1.42211 0.01875 32.6972877 41.8875 9.19021 21.94 37.2923939

    8 1.7407 0.02 29.1089203 44.68 15.57 34.85 36.8944601

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    Table 05: Calculated data for tube and shell side heat transfer co-efficient

    No

    of

    Obs

    Tube side

    Reynolds'

    No

    Tube Side

    prandtl no.

    Viscosity

    of water at

    wall

    temperature

    (kg/m.s)

    Tube side

    Nusselt NojH value

    Tube side

    heat

    transfer

    coefficient,

    hi

    (W/m2.C)

    Shell side

    heat transfer

    coefficient,

    ho

    (W/m2.C)

    1 7623.25572 5.68644644 0.00042666 67.57398 34.4410319 4433.21835 4730.50156

    2 9538.33328 5.74765444 0.00042821 81.1978593 41.2042258 5320.02015 4719.37987

    3 12078.0409 5.77831951 0.00042899 98.2895119 49.7692343 6435.61613 4713.85036

    4 14928.6017 5.83977219 0.00043054 116.949833 58.9629319 7647.34185 4702.85325

    5 8793.78339 5.38282843 0.00040667 74.3788083 38.6104066 4911.70488 4765.7861

    6 10218.0062 5.44323121 0.00040822 84.252684 43.5368188 5556.47796 4754.58813

    7 12433.8567 5.50379377 0.00040977 99.0236978 50.9387695 6522.09397 4743.47295

    8 15001.7891 5.59493858 0.00041209 115.845814 59.194071 7615.08844 4726.953

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    Table 06: Calculated data for experimental and theoretical overall heat transfer coefficient

    No of Obs

    Mass velocity

    of water

    (kg/m2.s)

    LMTD (C)

    Outside

    surface area

    of 19 tubes

    (m2)

    OverallExperimental

    heat transfer

    coefficient,

    UoE

    (W/m2.C)

    OverallTheoretical

    heat transfer

    coefficient,

    UoT

    (W/m2.C)

    1 680.277018 76.1284364 1.84847321 163.0978635 1937.165799

    2 859.190895 76.6440681 1.84847321 187.8985402 2146.361712

    3 1093.03828 76.9009928 1.84847321 225.891088 2368.989501

    4 1363.55732 77.41309 1.84847321 242.4714874 2568.412839

    5 747.771014 77.5795876 1.84847321 211.6694175 2062.035309

    6 877.467745 78.0949212 1.84847321 247.5584263 2204.945136

    7 1078.2051 78.6079342 1.84847321 256.6496755 2392.27619

    8 1319.79988 79.3732024 1.84847321 251.4630026 2570.629003

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    Table 07: Calculated data for tube side experimental and theoretical pressure drop

    No

    of

    Obs

    Experimental Pressure

    Drop from

    manometer

    reading,

    (Pa)

    Friction

    factor

    (sq ft/sq

    inch)

    Specific

    gravity,

    s

    t(/w)^0.14

    Pressure

    drop through

    tubes Pt

    (Pa)

    Pressure

    drop due to

    velocity

    head (Pa)

    TotalTheoretical

    Pressure

    drop PT

    (Pa)

    1 10161.8141 0.0003 0.99596 1.09923283 2362.721233 937.945183 3300.66642

    2 15920.1754 0.00027 0.99612 1.100118 3388.780082 1495.46379 4884.24387

    3 23372.1724 0.00025 0.9962 1.10055656 5075.783231 2419.70643 7495.48967

    4 38276.1663 0.00023 0.99636 1.10142577 7260.296222 3763.82565 11024.1219

    5 12871.6312 0.00028 0.99516 1.09919479 2666.729295 1136.0307 3802.75999

    6 18629.9925 0.00026 0.99532 1.10012354 3406.298481 1563.52805 4969.82653

    7 25065.808 0.00024 0.99548 1.10104053 4742.740664 2359.59079 7102.33145

    8 38614.8935 0.00023 0.99572 1.10239447 6800.188707 3532.93806 10333.1268

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    GRAPHS

    1) jH factor vs Reynolds No

    a) for 2.5 psig steam pressure:

    Figure 02: jH Factor vs Reynolds' No for 2.5 psig Steam Pressure

    y = 0.8001x +log0.00395

    10

    100

    1000 10000 100000

    jH

    Factor

    Reynolds' No

    jH Factor vs Reynolds' No for 2.5 psig Steam Pressure

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    b) for 5 psig steam pressure

    Figure 03: jH Factor vs Reynolds' No for 5 psig Steam Pressure

    y = 0.8001x +log0.00395

    10

    100

    1000 10000 100000

    jHF

    actor

    Reynolds' No

    jH Factor vs Reynolds' No for 5 psig Steam Pressure

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    2) Pressure drop vs velocity of water\

    a) For 2.5 psig steam pressure

    Figure 04: Pressure Drop vs Velocity of Water for 2.5 psig Steam Pressure

    0

    5000

    10000

    15000

    20000

    25000

    30000

    35000

    40000

    0.6 0.7 0.8 0.9 1 1.1 1.2 1.3 1.4

    PressureDrop(Pa)

    Velocity of Water (m/sec)

    Pressure Drop vs Velocity of Water for 2.5 psig Steam

    Pressure

    Experimental

    Theoretical

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    b) For 5 psig steam pressure:

    Figure 05: Pressure Drop vs Velocity of Water for 5 psig Steam Pressure

    0

    5000

    10000

    15000

    20000

    25000

    30000

    35000

    40000

    0.7 0.8 0.9 1 1.1 1.2 1.3 1.4

    PressureDrop(Pa)

    Velocity of Water (m/sec)

    Pressure Drop vs Velocity of Water for 5 psig Steam

    Pressure

    Experimental

    Theoretical

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    SAMPLE CALCULATION

    For observation no. 2 (2.5 psig steam pressure):

    Water inlet temperature, T1 = 24.5oC

    Water outlet temperature, T2 = 31o

    C

    Water mean temperature, Tm =2

    TT21

    =

    2

    315.24 = 27.75oC

    Properties of water at mean temperature (27.75oC),

    Density, = 996.12 kg/m3

    Viscosity, = 0.00084655 kg/m.sec

    Thermal conductivity, k = 0.6157496 W/m.oC

    Specific Heat, Cp = 4.18063425 kJ/kg. C

    [From J. P. Holman, Heat Transfer, McGraw - Hill, 10th Ed, 1997, Page-605, Table A-5]

    Saturation temperature at 2.5 psig steam pressure, Ts= 104.44oC

    Heat of Condensation at 2.5 psig steam pressure, hfg = 2244.6 kJ/kg

    [From J M Smith, H C Van Ness, M M Abbott, Chemical Engineering Thermodynamics,

    McGraw - Hill, 7th Ed, 2001, Page-715, Table F1]

    Weight of bucket and condensate = 2.7 kg

    Weight of empty bucket = 1.5 kg

    Weight of condensate = (2.7-1.5) kg

    = 1.2 kg

    Time of condensate taken = 2 minutes

    Mass flow rate of condensate, mc=sec602

    kg1.2

    = 0.01 kg/sec

    Heat released by condensation, Qc= mchfg

    = (0.012244.6) kW

    = 22.446 kW

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    Volume of water taken = 10L

    Time of water taken = 8.79 sec

    Mass flow rate of water, mw =

    =sec79.8

    /12.9961010 333 mkgm

    = 1.133242321 kg/sec

    Heat absorbed by water, Qw = mwCp(T2-T1)

    = 1.1332423214.18063425(31-24.5)

    = 30.79486579 kW

    Heat loss = (QcQw)

    = (22.446 - 30.79486579) kW

    = -8.3489 kW

    Percent heat loss = %100)(

    C

    WC

    Q

    QQ

    = -37.195 %

    Average heat transfer, Qavg =

    2

    QQ cw

    =2

    446.22930.7948657

    = 26.6204 kW

    Logarithmic Mean Temperature Difference,

    LMTD =

    2s

    1s

    2s1s

    TT

    TTln

    )T(T)T(T

    =

    3144.104

    5.2444.104ln

    )3144.104()5.2444.104(

    = 76.6441 C

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    For nominal size 6 & schedule 40 steel tube,

    Inside diameter (ID) of the tube, Di= 0.37 inch = 0.009398 m

    Outside diameter (OD) of tube, Do= 0.5 inch

    [From Donald Q. Kern, Process Heat Transfer, McGraw - Hill, International Ed, 1997,

    Page-843, Table 10]

    Outsied area of 19 tube = nDoL

    = 190.596 inch2

    = 2865.14 inch2

    = 1.84847 m2

    Experimental overall heat transfer co-efficient,

    UOE =LMTDA

    Q

    0

    avg

    =76.64411.84847

    100026.6204

    = 187.8985 W/m2. C

    Flow area of tube, Ai =

    =1

    1076.019inch2

    = 2.0444 inch2

    = 0.001318965 m2

    Velocity of water =

    =996.1250.00131896

    11.13324232

    = 0.86254 m/sec

    Mass velocity of water, =

    =50.00131896

    11.13324232= 859.191 kg/m2sec

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    Reynolds number, Re =

    vDwi

    =0.00084655

    12.99686254.00.009398

    = 9538.333

    Wall temperature Tw =2

    )]TT(0.5[Ts 21

    = 66.095 oC

    Prandtl Number, Pr = 5.74765

    Viscosity of water at wall temperature = 0.000428211 kg/m.sec

    [From J. P. Holman, Heat Transfer, McGraw - Hill, 10th Ed, 1997, Page-605, Table A-5]

    Using Seider-Tate equation,

    Nu=0.027 Re0.8 Pr1/3(/w)0.14

    = 0.027(9538.333)0.8 (5.74765)1/3(0.00084655/0.000428211) 0.14

    = 81.1978

    jH factor calculation,

    jH = Nu .Pr-1/3.

    14.0

    w

    = 41.2042

    Tube side heat transfer coefficient

    hi = Nu iD

    k

    = 81.19780.009398

    0.6157496

    = 5320.0201 W/m2. C

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    Film temperature, Tf = Ts0.75(Ts-Tw)

    = 75.68125 oC

    Properties of condensate at film temperature (75.68125oC),

    Density, f = 60.859 kg/m3

    Viscosity, f = 0.907023 kg/m.sec

    Thermal conductivity, kf= 0.386105 W/m.C

    [From J. P. Holman, Heat Transfer, McGraw - Hill, 10th Ed, 1997, Page-605, Table A-5]

    Density of steam, v 0

    Saturation temperature, Tg=Ts = 104.44 C

    Using Nusselt equation, steam side heat transfer co-efficient,

    ho = 0.725

    25.0

    wgf

    3ffgvff

    )Tnd(T

    kgh)(

    = 0.725

    25.0

    wgof

    3ffg

    2f

    )T(TD

    kgh

    = 4719.3798 W/m2. C

    Theoretical overall heat transfer co-efficient,

    UOT =

    -1

    ii

    o

    0 hD

    D

    h

    1

    = 2146.362 W/m2. C

    Pressure Drop Calculation:

    For Reynolds no = 9538.333

    The value of friction factor, f = 0.00027 sq ft/sq inch

    [From Donald Q. Kern, Process Heat Transfer, McGraw - Hill, International Ed, 1997,

    Page-836, Figure 26]

    Mass velocity of water Gt= 633513.753 lb/hr.ft2

    Length of the tube, L = 8 ft

    No of tube passes, n = 1

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    Inner diameter of tube, D = 0.03083333 ft

    Specific gravity, s = 0.99612

    Pressure drop through tube,

    Pt= 0.14w

    10

    2

    )/(sD105.22

    nLGtf

    = 0.491500997 psi

    = 3388.780082 Pa

    Velocity of water, v = 2.82985 ft/s

    Acceleration of gravity, g = 32.174 ft/s2

    Velocity head,'2

    2

    g

    v= 0.1244489 ft

    Pressure drop due to velocity head, Pr=

    s

    n4

    '2

    2

    g

    v

    144

    5.62

    = 0.21689868 psi

    = 1495.464 Pa

    Total pressure drop, PT= Pt+ Pr

    = 4884.24387 Pa

    Difference in manometer height, h = (0.93218- 0.8128) m Hg

    = 0.11848 m Hg

    Density of mercury, Hg = 13594 kg/m3

    Experimental pressure drop = hHgg

    = 0.11848 13594 9.81

    = 15920.175 Pa

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    RESULTS AND DISCUSSIONS

    Range of Overall Heat transfer co-efficient:

    Experimental Values -------- 163.1 to 256.54 W/m2

    . C

    Theoretical Values -------- 1937.2 to 2570.6 W/m2. C.

    Range of Pressure drop:

    Experimental Values -------- 10161.8 to 38614.9 Pa

    Theoretical Values -------- 3300.7 to 11024.12 Pa

    Some of the heat loss found in this experiment were a negative value. But that was not

    expected. The condensate was collected through a steam trap, in which the flow was not

    continuous. As a result condensate flow rate was not steady for this experiment, hence

    negative heat loss encountered in the experiment. The steam pressure was considered

    constant during the experiment but it was not constant. Heat lost during the experiment due to

    convection and conduction was not also considered.

    Two types of graphs were drawn in the experiment. From the 1sttype of graph, jH factor vs

    reynolds no the slope was found 0.8001 both for 2.5 and 5 psig steam pressure, which provesthe validity of Sieder-Tate equation.

    From the 2ndtype of graph, pressure drop vs velocity of water the experimental pressure drop

    was found somewhat greater than the theoretical pressure drop both for 2.5 and 5 psig steam

    pressure. The theoretical values found in this experiment were not absolutely theoretical.

    These values are found based on some parameters that are determined experimentally in one

    way or another. Hence, they cannot be said to be purely theoretical. However, these

    theoretical values can be of great importance when reasonable approximation and comparison

    are required in real life consequence. One of the important things in shell and tube exchanger

    operation is the pressure limitation that must be abided both in shell and tube sides. Beyond

    this pressure limits the system can become unstable and materials of construction is affected

    mainly due to corrosion and erosion.

    Excess fouling might encounter in tube side which decrease the overall heat transfer co-

    efficient.

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    After two consecutive reading we have to pause our experiment meanwhile heat exchanger

    lost its current status & become cool .Thereby temperature exchange not happen linearly

    which is great obstacle to perform this experiment.