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    UCL 2009/G017 Steady-state heat transfer II 1

    Steady-state heat transfer II

    Dr Farlan Veraitch

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    UCL 2009/G017 Steady-state heat transfer II 2

    Heat transfer between fluids - Recap

    Consider heat transfer through the wall of a fermenter or througha pipe in a heat exchanger.

    Hot and cold fluids flow on either side of thewall

    Heat transfer across the wall is byconduction

    Heat transfer between the fluid and the wallis by convection

    Each layer represents a resistance to heattransfer

    Rate of heat transfer:

    But how to we calculate h?

    Hot

    fluid

    Th

    Tc

    Cold

    fluid

    T1T2

    Liquid

    films

    wall

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    UCL 2009/G017 Steady-state heat transfer II 3

    Estimation of heat transfer coefficients

    Well now review empirical correlations to calculate individual heattransfer coefficients h

    What factors need to be considered in the correlation to calculate h?Hot

    fluid

    Th

    Tc

    Cold

    fluid

    T1

    T2

    Liquid

    films

    wall

    How do we correlate all these variables?

    Why does this help? Simplifies problem as the number of groups < the number of variables a = f (b, c)

    operating conditions: velocity u (pipe), stirrer speed N (vessel)

    fluid properties: viscosity thermal conductivity specific heat capacity density

    system geometry Characteristic length eg. diameter

    h = f (u or N, , k,, Cp, d)

    Dimensionless analysis to relate the most importantvariables together in the form ofdimensionless numbers

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    UCL 2009/G017 Steady-state heat transfer II 4

    Estimation of heat transfer coefficients

    Values ofh for flow in pipes or stirred vessels are usually evaluatedusing empirical correlations expressed in terms ofdimensionless

    numbers

    Dimensionless numbers that are used to calculate h are:Nusselt no. FlowReynolds no. ImpellerReynolds no. Prandtl no.

    where

    h individual heat transfer coefficient (W.m-2.K-1)

    kfluid thermal conductivity of hot/cold fluid (W.m-1.K-1)

    d Pipe or tank diameter (m)

    Liquid density (kg.m-3)u Liquid velocity (m.s-1)

    dp Pipe diameter (m) Liquid viscosity (N.s.m-2)N Impeller rotational speed (s-1)

    di Impeller diameter (m)

    Cp Specific heat capacity (J. kg-1.K-1)

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    UCL 2009/G017 Steady-state heat transfer II 5

    Estimation of heat transfer coefficients Significance of each dimensionless group:

    Nusselt no. conductive resistance : convective resistance

    FlowReynolds no. inertial forces : viscous forces

    Ref< .LAMINAR FLOW

    Ref> ....TURBULENT FLOW

    ImpellerReynolds no. inertial forces : viscous forces

    Rei < .. LAMINAR FLOW

    Rei > .TURBULENT FLOW

    Prandtl no. momentum transfer : heat transfer

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    UCL 2009/G017 Steady-state heat transfer II 6

    Estimation of heat transfer coefficients

    In most industrial applications, heat transfer occurs betweenturbulent fluids in pipes or in stirred vessels - forced convection in

    these systems is more important than natural convection

    For forced convection in pipes or stirred vessels, the general formof heat transfer correlations is:

    Nu = c * Rea * Prb

    The values of a, b and c depend on the heat-transfer equipmentand the flow regime We will look at correlations for:

    turbulent flow in pipes turbulent flow in stirred tanks

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    UCL 2009/G017 Steady-state heat transfer II 7

    Turbulent flow in pipes

    A widely accepted correlation for forced convection in pipes:Nu = 0.023 Ref

    0.8

    Pr0.4

    This equation is valid for:

    liquids with viscosity close to water

    104 Ref 1.2 x 105

    0.7 Pr 120L / d 60

    When using these correlations to calculate h, it is important toalways check that Re and Prlie within the valid ranges!

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    UCL 2009/G017 Steady-state heat transfer II 8

    Turbulent flow in pipes

    For very viscous liquids, there may be a marked difference betweenthe viscosity of fluid in bulk flow and the viscosity of fluid adjacent to

    the wall

    A modified form of the equation includes a viscosity correction term:

    where b is the viscosity of bulk fluid

    w is the viscosity of fluid adjacent to the wall

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    UCL 2009/G017 Steady-state heat transfer II 9

    Turbulent flow in pipes - Eg

    A single-pass shell-and-tube heat exchanger is used to heat adilute salt solution for a large-scale protein chromatography

    column. 25.5m3h-1 solution passes through 42 parallel tubes inside

    the heat exchanger; the internal diameter is 1.5cm and the tube

    length is 4m. The viscosity of the bulk salt solution is 10-3 kg m-1 s-1,

    the density is 1010 kg m-3, the average heat capacity is 4 kJ kg-1 K-1

    and the thermal conductivity is 0.64 W m-1 K-1.

    a) Calculate the tube-side heat transfer coefficient (for the insideliquid film) and the resistance

    b) Keeping all other variables constant, what is the expected %

    change in h and Rif:

    viscosity increases by 10%? velocity is doubled?Hint - spend some time working out the fluid velocity in the tubes

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    UCL 2009/G017 Steady-state heat transfer II 10

    RECAP: Single-pass shell-and-tube heat exchanger

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    UCL 2009/G017 Steady-state heat transfer II 11

    Turbulent flow in pipes - Eg

    Solution

    List known parametersN = 42

    Qv = 25.5 m-3h-1 = ...

    Di = 0.015 m

    L = 4 m = 10-3 kgm-1s-1 = 1010 kgm-3Cp = 4000 Jkg

    -1K-1

    kfluid = 0.64 Wm-1K-1

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    UCL 2009/G017 Steady-state heat transfer II 12

    Turbulent flow in pipes - Eg

    Solution

    What equation will you use to find h?Nu = 0.023 Re0.8 Pr0.4

    What parameter values need to be calculated?

    What order will you calculate parameters?hi d = 0.023 p u d

    0.8 Cp0.4kfluid kfluid

    ? ?

    u

    Re

    Pr

    Nu

    hR

    u = Q/A

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    UCL 2009/G017 Steady-state heat transfer II 13

    Turbulent flow in pipes - Eg

    Solution

    Qv

    u = Qv/A

    A = d2 x number of tubes

    4

    = (0.015)2 x 42

    4

    A = 0.0074m2

    u = Qv = 25.5/3600A 0.0074

    u = 0.95ms-1

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    UCL 2009/G017 Steady-state heat transfer II 14

    Turbulent flow in pipes - Eg

    Ref= ud= 1010 x 0.95 x 0.015

    10-3

    Ref= 1.44 x 104

    Pr = Cpkfluid

    = 4000x(1x10-3)

    0.64

    Pr = 6.25

    L/d = 4 = 267

    0.015

    As 104 < Re < 1.25x105

    0.7 < Pr < 120

    L/d > 60

    Eqn is VALID

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    UCL 2009/G017 Steady-state heat transfer II 15

    Turbulent flow in pipes - Eg

    Nu = 0.023 Re0.8 Pr0.4

    = 0.023(1.44 x 104)0.8(6.25)0.4

    Nu = 101.6

    Nu = hid

    kfluid

    hi = 101.6 x 0.64

    0.015

    hi = 4335 Wm-2K-1

    R = 1 = 0.00023 m2KW-1

    hi

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    UCL 2009/G017 Steady-state heat transfer II 16

    What happens if viscosity increases by 10%?

    x 1.1hd = 0.023 ud 0.8 Cp 0.4k kh 1 0.80.4

    -0.8.0.4h -0.4 [and therefore R 0.4]hnew = new -0.4hold oldhnew = (1.1)

    -0.4 = 0.96

    hold

    4% in hi

    Check Re + Pr still valid

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    UCL 2009/G017 Steady-state heat transfer II 17

    Rnew = new 0.4Rold old

    = (1.1)0.4

    = 1.04

    4% in R as expected

    R 1/h 0.4

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    UCL 2009/G017 Steady-state heat transfer II 18

    What happens if velocity doubles?h u0.8

    hnew = unew0.8

    hold uold

    = 20.8

    = 1.74

    74% in h when u doubles

    Rnew = 0.57

    Rold

    R u-0.8 2-0.843% in R when u x 2

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    UCL 2009/G017 Steady-state heat transfer II 19

    Turbulent flow in stirred tanks

    Jacketed vessels

    Inside film heat transfer coefficient hi Two correlations for heat transfer in jacketed vessel equipped with 6-turbine flat

    blade stirrer:

    1) Nu = 0.81 Rei0.68Pr0.33

    This equation is valid for:

    105 Rei 7 x 105

    liquids with physical properties close to water

    Ref. Akse, H., et al Chem. Eng. Sci., 22, 135, 1967

    2) Nu = 0.76 Rei0.67 Pr 0.33

    This equation is valid for:

    4 x 103 Rei 2.8 x 105

    1.9 Pr 1 x 105

    Ref. Strek, F., et al Int. Chem. Eng., 7, 693, 1967

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    UCL 2009/G017 Steady-state heat transfer II 20

    Turbulent flow in stirred tanks

    Helical cooling coils

    Inside film heat transfer coefficient hi The value ofhican be found using the correlations for turbulent flow in pipes.

    (eg. Nu = 0.023 Ref0.8Pr0.4)

    These correlations have been obtained for straight tubes; with a coil somewhatgreater transfer is obtained for the same physical conditions:

    hi(coil) = hi(straight pipe) ( 1 + 3.5 d/dc)

    where d is the inside diameter of the tube and dc is the

    diameter of the helix.

    Outside film heat transfer coefficient ho The value ofho depends on the degree of agitation and the fluid properties.

    Ref. Chilton, T. H., et al Ind. Eng. Chem., 36, 510-516, 1944

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    UCL 2009/G017 Steady-state heat transfer II 21

    Logarithmic and arithmetic mean temp differences

    Thi

    Tho

    Tci

    Tco

    Use Ta when one fluid is maintained at a constant temperature

    E.g. In a fermenter

    T1 = Tci - Tferm

    T2 = Tco - Tferm

    LM is used if temperature varies in both fluids in eithercounter-currentorco-currentflow

    T1 = Thi - Tci

    T2 = Tho - Tco

    Thi

    Tho

    Tci

    Tco

    T1 = Thi - Tco

    T2 = Tho - Tci

    co-current counter-current

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    UCL 2009/G017 Steady-state heat transfer II 22

    RECAP: Single-pass shell-and-tube heat exchanger

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    UCL 2009/G017 Steady-state heat transfer II 23

    Turbulent flow in stirred tanks Case studyHeat transfer coefficient for stirred vessel and cooling coil length

    A fermenter used for antibiotic production must be kept at 27C. After considering theoxygen demand of the organism and the heat dissipation from the stirrer, themaximum heat-transfer rate required is estimated at 550 kW.

    Cooling water is available at 10C and the exit temperature of the cooling water is

    calculated as 25C. It is proposed to install a helical cooling coil inside the fermenter;

    the outer diameter of the coil pipe is 8 cm, the pipe thickness is 5 mm and the

    thermal conductivity of the steel is 60 W m-1 C-1. The heat transfer coefficient for the

    cooling water is 14,000 W m-2 C-1. The internal fouling factor of the coil is 8500 W

    m-2 C-1; the fermenter side of the coil is kept relatively clean.

    The fermenter has diameter 5m and is mixed using a turbine impeller 1.8 m indiameter operated at 60 rpm. The fermentation broth has the following properties: b

    = 5 x 10-3 Pa s; = 1000 kg m-3; Cp = 4.2 kJ kg-1 C-1; k = 0.7 W m-1 C-1.

    Neglecting viscosity changes at the wall of the coil, Calculate the heat transfer coefficient for the broth Calculate the length of cooling coil required. Comment on your answer.

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    UCL 2009/G017 Steady-state heat transfer II 24

    Turbulent flow in stirred tanks Case study

    List parametersLet broth be hot fluid denoted as h

    Let broth be cold fluid denoted as c

    Broth Cold water Coil

    Th = 27C Tci = 10C qmax = 550,000w

    = 5 x 10-3 PaS Tco = 25C do = 0.08m

    = 1000kg/m3 x = 0.005m

    Cp = 4200J/kgC Ksteel = 60 W/mC

    kh = 0.7W/mC hc = 14,000W/m2C

    1/hfh = 0 hfc = 8500W/m2C

    Fermenter: dv = 5m, di = 1.8m, N = 60rpm = 1s-1

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    UCL 2009/G017 Steady-state heat transfer II 25

    CW

    hc

    hfc

    hh

    BROTH

    x or roln(ro/ri)

    k k

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    UCL 2009/G017 Steady-state heat transfer II 26

    Turbulent flow in stirred tanks Case study

    Calculate the heat transfer coefficient for the broth1) Calculate hh?

    Nu = 0.87 Rei0.62Pr0.33

    Re Ndi2 1000 x 60/60 x 1.82 6.48x105 5x10-3Pr Cp 4.2x103 x 5x10-3 30

    Kh 0.7

    Nu = 0.87(6.48x105)0.62 (30)0.33

    = 1.07x104

    hh = Nu,kh 1.07x104 x 0.7 1501W/m2C

    dv 5

    ===

    = = =

    ==

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    UCL 2009/G017 Steady-state heat transfer II 27

    Turbulent flow in stirred tanks Case study

    Calculate the length of cooling coil required. What equation will you use to find L?

    What parameter values need to be calculated?

    What order will you calculate parameters?

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    UCL 2009/G017 Steady-state heat transfer II 28

    Calculate L

    q = Uo Ao TaCalculate Ta

    UoAo

    L

    Ta T1 + T2 (27-10)+(27-25)2 2

    Ta = 9.5C

    = =

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    UCL 2009/G017 Steady-state heat transfer II 29

    1 1 + 1 + x + 1 + 1U hh hfh k hfc hc

    1 + 0 + 5x10-3 + 1 + 1

    1501 60 8500 14,000

    6.67x10-4 + 8.33x10-5 + 1.17x10-4 + 7.14x10-5

    small small

    = 9.386 x 10-4

    U = 1065W/m2C

    or U = 1113W/m2C if use

    roln(ro/ri)

    k0

    =

    =

    =

    roln(ro/ri)

    k

    Wall resistance +

    cw resistance - minor

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    UCL 2009/G017 Steady-state heat transfer II 30

    q = Uo Ao TaAo= q

    Uo Ta= 550000

    1065 x 9.5

    Ao = 54.36m2

    AO = do L

    L = 54.36 X 0.08

    L = 216m