Residence Time Distribution Analysis of a Taylor Couette Contactor by Computational Fluid Final

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  • CHEMCON-2013, Mumbai, 27-30 Dec 2013,

    1

    Residence Time Distribution Analysis of a Taylor

    Couette Contactor by Computational Fluid

    Dynamics using OpenFoam

    Abhishek Singh, M. Balamurugan, Shekhar Kumar*, U. Kamachi Mudali, R. Natarajan

    Corresponding author. Email: [email protected]

    1Reprocessing Group, IGCAR Kalpakkam, 603102 India.

    2E-mail addresses: [email protected]

    Abstract: Taylor Couette flow is the phenomenon of fluid flow between the annular gap of two coaxial cylinders, one or both

    rotating along their common axis, which results into the formation of Taylor vortices above a critical Taylor number. When a

    small amount of axial flow is introduced to the Taylor couette flow, it tries to carry Taylor vortices along its direction which

    results into radial mixing due to the toroidal motion of fluid elements. This type of flow can be considered as similar to the

    ideal plug flow reactor according to earlier studies. Authors have experimentally characterized the non-ideal flow in a Taylor-

    couette extractor column by pulse response analysis. In this paper, details of experimental work and unique computational fluid

    dynamics results related to the above mentioned work are discussed.

    Keywords: Taylor couette phenomenon, residence time distribution, solvent extraction, computational fluid dynamics

    1. Introduction:

    Taylor Couette Contactor (TCC) is a single compact unit

    which operates on the action of centrifugal force. The

    design of the TCC is based on Taylor-Couette principle

    where the inner cylinder rotates and the outer cylinder

    remains stationary. In the annular region between these

    two co-axial cylinders fluid is filled which forms taylor

    vortices when the inner cylinder is rotated above the

    critical taylor number.

    2 Taylor-Couette flow and flow instability:

    Taylor Couette flow is the phenomenon of fluid flow

    between the annular gap of two coaxial cylinders, one or

    both rotating along their common axis, which results into

    the formation of Taylor vortices above a critical Taylor

    number. At relatively low inner cylinder speeds, the flow

    in the annular region is dominated by the viscous forces and a tangential flow is obtained. As we increase the inner

    cylinder speed the centrifugal forces begin to dominate the

    viscous forces resulting into centrifugal instabilities this

    phenomenon is known as taylor couette flow. Earlier Couette [1] and Mallock [2] had carried out several

    experiments on this centrifugal instability phenomenon

    and they noted instabilities at certain rotational speeds.

    Later on Taylor used the linear theory of instability to give

    a solution for these centrifugal instabilities. He gave a

    dimensionless number known as the Taylor number (Ta)

    which is the ratio of the centrifugal force and viscous

    force and can be expressed mathematically as :

    (1)

    Later on Chandrashekhar [3] found the critical taylor

    number (Tacr) which depicted the transition from the

    Couette flow (CF) to Taylor vortex flow (TVF). He also

    showed that with the introduction of the axial flow in the

    annular region along with the taylor-couette flow there is a

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    delay in the onset of centrifugal instabilities which can be

    represented by the Eqn.(2) where the critical taylor

    number is the function of the axial reynold number shown

    in Eqn.(3)

    (2)

    (3)

    3. Experimental

    3.1 Equipment

    The experimental setup consisted of a Taylor couette

    contactor and one feed pump along with the product and

    feed tanks. The mixing section consists of a vertical co-

    axial cylindrical annulus with inner rotating cylinder (OD

    22 mm) and an outer fixed cylinder (ID 25 mm), the

    annular gap width thus being 1.5 mm. The total height of

    the working annular space i.e. the mixing section is 250

    mm yielding an aspect ratio (L/d) of 83.34 and a working

    volume of 27.69 cm3. The top and bottom settling sections

    are made up of glass of 200 mm length each with a combination of a frustum(50 mm height , and inner

    diameters of 88mm and 22mm respectively) and a

    cylinder (height 150 mm and inner diameter 88 mm).Each

    settling zone has two openings which are 90 mm apart and

    diametrically opposite. The inner rotating cylinder is made up of stainless steel and is pivoted at its base and the

    arrangement is made to reduce vibrations and any introduction of eccentricity is completely prohibited. The

    test fluid is pumped inside the top opening of the

    equipment a precision metering pumps (ISMATEC MFP

    Process drives (ISM-909) + FMI Q series Pumpheads).

    The continuous phase from the feed tank was fed to the

    top inlet through soft-tubes. The settler was provided with

    an overflow tube and a drain tube for continuous operation

    of the Taylor coquette equipment. The continuous phase

    outlet was connected to a laboratory pH meter (Metrohm

    model 827 pH meter) for the continuous monitoring of the

    pH. The view of the experimental setup in operation is

    shown in Fig.1.

    3.2 Experimental procedure

    Demineralised water was used as a testing fluid and a

    standard 4 N nitric acid as the tracer respectively. Initially

    the bottom settling zone was filled with CCl4 so that there

    was no introduction of the testing fluid in that part. Then

    the mixing zone was filled with the testing fluid at a

    constant flow rate till a steady state was achieved. It was

    checked that the pH measured at the outlet should match the pH of the testing fluid. Then the first series of

    experiments were conducted for 0 rpm inner cylinder

    rotation rate and the axial flow rate was varied from 10 and 20 ml/min respectively. Once the flow became stable and the value in the pH meter becomes steady, 2ml of 4N

    HNO3 pulse was injected from the inlet and a stop watch

    was started. The readings in the pH meter were noted down

    at an interval of 30 sec. The experiment was stopped when

    the pH meter reading becomes steady again and reaches

    approximately the initial pH of the testing fluid. Keeping

    all the parameters same a set of experiments was conducted

    for 100, 200, 400, 600, 800 rpm and the pH readings were

    noted down for the 10 and 20 ml/min inlet flow rates

    respectively. The resultant data was converted to

    concentration scale and then the numerical analysis for

    RTD was performed.

    1. Water tank 4. Regulator 7. pH meter 10. Tracer injector

    2. Peristaltic

    pump

    5. Electric

    motor

    8.Constant

    head

    11. Bottom

    section filled

    with CCl4

    3. Pump

    Controller

    6. TCC 9. Outlet tank

    Figure 1 : Schematic of the setup for the residence time distribution analysis of

    the Taylor Couette Contactor

    3.3 Data analysis

    Inorder to characterize flow, it is necessary to know the

    residence-time distribution, earliness of mixing, and state

    of aggregation of the fluid [1]. If the latter two factors can

    be ignored, the mean residence time can be determined as follows:-

    (Mean residence time of the Cpulse):

    (4)

    (Variance of the curve):

  • CHEMCON-2013, Mumbai, 27-30 Dec 2013,

    3

    (5)

    (To find the Ecurve):

    (6)

    Total number of tanks in series can be calculated by the

    following relation:

    (7)

    4. Computational fluid dynamics methodology

    Numerical simulations for the above Residence time

    distribution analysis has been done using the OpenFoam

    (version 2.0.1) at various rotational speeds and flow rates.

    4.1 (a) Model Formulation

    For the CFD analysis a 3D geometry has been prepared

    using the blockMesh functionality in the OpenFoam

    (version 2.0.1) .In the present case simpleFoam solver was

    used. The following continuity and momentum equations

    were solved using the above solver:

    Continuity equation:

    (8)

    Momentum equation:

    (9)

    The velocity ui can be written as a sum of mean velocity

    and fluctuating velocity:

    (10)

    Putting the above combination of mean and averaged

    velocity in Eqs. (7) and (8) and Reynolds averaging we

    get:

    (11)

    This can be written as the following continuity equation

    (12)

    (13)

    This can be further written as the following momentum

    equation

    (14)

    Standard k- Model

    In the present work, the standard k- model has been

    adopted to carry out the steady three dimensional CFD

    simulations in the annular and bottom region of the TCC (

    Taylor couette contactor) The conservation equation for

    the turbulent kinetic energy (k) and dissipation () can be

    expressed as (Launder and Spalding (1974)) ,

    k equation

    (19)

    equation

    (20)

    The turbulent eddy viscosity, t can be computed from the

    following correlation,

    (21)

    For the k- model

    (22)

    In the above Eqns. (14) and (15), C1, C2, C are turbulent

    model constant, k, are the turbulent Prantl number.

    The standard values selected for turbulent parameters such

    as C, C1, C2, k, are 0.09, 1.44, 1.92, 1.0 and 1.3

    respectively.

    4.1 (b) Model formulation for species transport

    After the flow in the present geometry was converged the

    simulation of passive tracer was done. A pulse of the

    tracer was given at the inlet with unit mass fraction. After

  • CHEMCON-2013, Mumbai, 27-30 Dec 2013,

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    two iterations the mass fraction of the tracer was again set

    to zero. The following transport equations were solved for

    the above case:

    (23)

    In Eqn. (18), Tk is the local mass fraction of the tracer and

    Deff is the effective diffusion coefficient:

    (24)

    Where Dt is the eddy diffusion coefficient and Dm is the

    molecular diffusion coefficient. Dt and Dm can be

    estimated by the equations given below:

    (25)

    (26)

    4.2 Numerical Framework

    The geometry of the annular and the bottom region of the

    Taylor Couette Contactor (TCC) is shown in Figure 3.

    The model geometry is meshed using unstructured

    tetrahedral grids. The minimum and maximum grid

    volume sizes are 1.405174e-002 and 4.950891e-002 cubic

    meter respectively. The unstructured grid is chosen for

    discretization .

    4.3 Boundary Conditions

    The computational domain is confined to the annular

    mixing section and the conical bottom region till the

    outlet. Velocity inlet condition is specified for the fluid

    inlet. Inner cylinder is described as the rotating wall. No

    slip boundary condition was imposed for all the walls.

    Pressure outlet condition was provided at the fluid outlet.

    The ambient pressure has been considered to be

    atmospheric pressure.

    4.4 Solution Strategies

    We have used simpleFoam solver for the present problem.

    In this problem we encounter swirl flow in the mixing

    section and the bottom region. Hence PISO ((Pressure

    Implicit with Splitting of Operators) scheme was used for

    pressure velocity coupling and solving momentum

    equation by segregated implicit method. The discretization

    of the momentum equation was done by Gauss upwind

    scheme. The preconditioned conjugate gradient solver

    (PCG) and preconditioned bi-conjugate gradient solver

    (PBiCG) were used for pressure and velocity respectively.

    After the flow gets fully developed in the given geometry

    a pulse of tracer was injected. scalarTransportFoam solver

    was used to calculate the concentration of the tracer at the

    outlet keeping the simulation in unsteady state. During the

    unsteady state simulation only the scalar concentration

    changed with time.

    5. Results and Discussion

    The flow is carried from the upper mixing annular section

    to the bottom section from where it goes to the outlet. In

    this study we aim to investigate the flow behavior in the

    annular zone as well as the bottom section. The residence

    time distribution analysis of the mixing as well as the

    bottom section has also been performed. All the

    simulations are carried out using the OPENFOAM vs 2.0.1 and ParaView vs 3.10.1. The results are shown in the

    table(1) and table(2) below:

    5 Validation of CFD Model

    The model has been validated by comparing the residence

    time distributions and the exit age distribution curves. It is

    observed that our CFD predictions agree fairly well with

    the experimental data generated during the residence time

    6 Conclusion

    (1) An experimental residence time distribution technique

    has been developed which is capable of analyzing pulse

    Sr

    no

    RPM Mean

    residence time

    Variance Total number of

    tanks in series

    Exp

    (min)

    CFD

    (min)

    Exp

    (min2)

    CFD

    (min2) Exp CFD

    1 0 25.7 29.20 192.9 280.2 3.44 3.05

    2 100 36.8 36.33 403.9 399.1 3.35 3.31

    3 200 30.3 29.60 359.2 357.8 2.57 2.45

    4 400 32.5 31.96 377.4 389.7 2.80 2.62

    5 600 32.5 32.22 388.0 411.2 2.71 2.52

    6 800 29.6 30.53 327.3 430.6 2.68 2.16

    Table 1 : Experimental results at 10 ml per min inlet flow rate

    Sr

    no

    RPM Mean residence

    time

    Variance Total number of

    tanks in series

    Exp

    (min)

    CFD

    (min)

    Exp

    (min2)

    CFD

    (min2)

    Exp CFD

    1 0 13.4 14.29 61.62 111.8 2.93 1.83

    2 100 16.0 16.98 72.95 113.7 3.53 2.54

    3 200 13.0 13.96 63.01 108.0 2.71 1.80

    4 400 15.7 16.40 83.62 129.7 2.95 2.1

    5 600 14.1 16.88 58.41 154.5 3.44 3.43

    6 800 13.3 14.37 63.66 115.4 2.77 1.90

    Table 2 : Experimental results at 20 ml per min inlet flow rate

  • CHEMCON-2013, Mumbai, 27-30 Dec 2013,

    5

    response in an apparatus such as Taylor Couette Contactor

    (TCC). RTD for the annular as well as the bottom section

    of TCC has been studied experimentally as well as

    computationally.

    (2) The CFD results show more dispersion as compared to

    the experimental results. Hence it could be assumed that

    bypassing and dead zones are present in the studied

    region.

    (3) The results obtained experimentally as well as

    computationally are in agreement with each other.

    7. Nomenclature

    CA = Exit concentration to an impulse input

    L = Length of the Couette flow device (cm)

    N = Total number of tanks in series

    = Axial Reynolds number,

    di = Inner cylinders outer diameter (cm) do = Outer cylinders inner diameter (cm)

    = Mean residence time (cm)

    Ta = Taylor number

    Tac = Critical Taylor number

    Greek symbols

    = Kinematic viscosity (m2/s) t = Turbulent kinematic viscosity (m

    2/s)

    = Radius ratio, do/di = Dynamic viscosity = Density i = Inner cylinder rotational speed v = Viscous energy dissipation rate t = Turbulent energy dissipation rate , = Turbulent parameters = Reynold stress Subscripts

    i, j, k = Indices in co-ordinate direction

    r = Radial direction

    z = Axial direction

    = Azimuthal direction

    8 Literature cited

    [1] M. Couette, Etudes sur le frottement des liquides,

    Annales de Chimie et de Physique 6, vol. 21, pp. 433

    510, 1890.

    [2] A. Mallock, Experiments on uid viscosity,

    Philosophical Transactions of the Royal Society A, vol.

    187, pp. 4156, 1896.

    [3] S. Chandrasekhar, The stability of spiral ow between

    rotating cylinders, Proceedings of the Royal Society A,

    vol. 265, no. 1321, pp. 188197, 1962.

    [4] G. I. Taylor, Stability of a viscous liquid contained

    between two rotating cylinders, Philosophical

    Transactions of the Royal Society A, vol. 223, no. 605

    615, pp. 289343, 1923.

    [5] K. E. Wardle, Open-source CFD simulations of liquid

    liquid ow in the annular centrifugal contactor,

    Separation Science and Technology, vol. 46, no. 15, pp.

    24092417, 2011

    [6] G. Baier and M. D. Graham, Two-uid Taylor-Couette

    ow : experiments and linear theory for immiscible

    liquids between corotating cylinders, Physics of Fluids,

    vol. 10, no. 12, pp. 30453055, 1998.

    [7] G. Baier, Liquid-liquid extraction based on a new ow

    pattern: two-uid Taylor-Couette ow [Ph.D. thesis],

    University of Wisconsin-Madison, Madison, Wis, USA,

    2000.

    [8] S. S. Deshmukh, M. J. Sathe, and J. B. Joshi, Residence

    time distribution and ow patterns in the single-phase

    annular region of annular centrifugal extractor,

    Industrial & Engineering Chemistry Research, vol. 48,

    no. 1, pp. 3746, 2009.