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    Chemical Kinetics

    1

    Global vs. Elementary Reactions

    Law of Mass Action

    Arrhenius Law

    Relation between forward and reverse reaction rates

    Steady State approximation

    from S.R Turns

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    Hydrocarbon Combustion (Turns p. 157)

    2

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    H2-O2 Combustion (Turns p. 117)

    3

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    4

    Reactor models

    Constant pressure reactor

    T = T(t)

    [Xi] = [Xi](t)

    V = V(t)

    Constant volume reactor

    T = T(t)

    [Xi] = [Xi](t)

    P = P(t)

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    5

    Reactor models (contd.)

    Well-stirred reactor

    T = constant[Xi] = constant

    P = constant

    Plug-flow reactor

    T = T(x)[Xi] = [Xi](x)

    P = P(x)

    V = V(x)

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    6

    Assumptions:

    No temperature gradients

    No composition gradientsi.e. T and [Xi] are functions of time

    Known:

    0

    0

    )0(

    )0(

    ii XtX

    TtT

    Constant Pressure Reactor

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    7

    Conservation of energy (First Law of Thermodynamics):

    dt

    dvP

    dt

    dhm

    dt

    dvmP

    dt

    dumWQ

    dt

    dh

    m

    Q

    Constant Pressure Reactor

    Expressing system chemical enthalpy in terms of chemical composition,

    m

    hN

    m

    Hh i

    ii

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    8

    i i

    ii

    ii

    dt

    hdN

    dt

    dNh

    mdt

    dh 1

    Assuming Ideal Gas behavior (h is a function of T only) :

    dt

    dT

    cdt

    dT

    T

    h

    dt

    hdip

    ii

    ,

    Constant Pressure Reactor (contd.)

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    9

    N

    j

    i

    M

    k u

    akkkikii

    kjk X

    TR

    ETA

    11

    '

    ,

    "

    ,

    ,'

    exp

    The rate of change ofNi : [ ]i

    i i i

    dNN V X Vdt

    Where,

    Substituting these expressions in the First Law,

    i

    pi

    i

    ii

    icX

    hVQ

    dt

    dT

    Constant Pressure Reactor (contd.)

    1

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    10

    Where,

    i

    ii MWX

    mV

    T

    T

    ipifi

    ref

    dTchh ,0,

    Constant Pressure Reactor (contd.)

    dt

    dV

    VXdt

    dV

    VNdt

    dN

    Vdt

    V

    Nd

    dt

    Xdiii

    i

    i

    i 1112

    The rate of change of[Xi] is given by :

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    11

    dt

    dT

    TX

    X

    dt

    Xd

    ii

    i

    i

    iii 1

    By using the ideal gas law :

    dt

    dT

    Tdt

    dN

    Ndt

    dV

    V i

    i

    i

    i

    111

    Constant Pressure Reactor (contd.)

    2

    i ui

    PV N R T Differentiating

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    Constant Pressure Reactor (contd.)

    Solution Methodology:

    System ofFirst order ODEs

    Integration routine capable of handling stiff equations

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    13

    Assumptions:

    No temperature gradients

    No composition gradients

    i.e. T and [Xi] are functions of time

    Known:

    0

    0

    )0(

    )0(

    ii XtX

    TtT

    Constant Volume Reactor

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    14

    Conservation of energy (First Law of Thermodynamics):

    dt

    dumWQ

    dt

    du

    m

    Q

    Constant Volume Reactor

    Expressing system chemical internal energy in terms of chemical

    composition,

    i

    upi

    i

    ii

    i

    iu

    RcX

    hTRVQ

    dt

    dT

    i

    1

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    Constant Volume Reactor (contd.)

    Also, the rate of change of pressure (using Ideal Gas Law):

    The rate of change of[Xi] is given by :

    ii

    dt

    Xd

    iiu

    iiu dt

    dT

    XRTRdt

    dP

    2

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    16

    Well-stirred reactor

    Conservation of species for the integral CV :

    Assumptions: Steady state operation

    Steady flow operation

    System isperfectly mixedand

    homogenous in compositionini

    ini

    h

    Y

    m

    ,

    ,

    outi

    outi

    h

    Y

    m

    ,

    ,

    outiinii

    cvi mmVmdt

    dm,,

    "',

    Rate of

    accumulation

    of mass i inCV

    Rate of

    generation of

    mass i in CV

    Mass

    flow ofi

    into CV

    Mass flow

    ofi out of

    CV

    Known: iniYVm ,,,

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    Well-stirred reactor (contd.)

    Since diffusional mass flow rate is negligible,

    0)( ,,"' outiinii YYmVm

    N

    j

    i

    M

    k u

    akkkikiii

    kjk XTR

    ETBMWm11

    '

    ,

    "

    ,

    ,'

    exp

    Where,

    ii Ymm Hence, conservation of mass :

    fori = 1,2,,N

    Since the reactor is homogeneous, the mass fraction at the outlet is

    equivalent to that inside the reactor

    TXfTXfVmouticvii

    ,,"'

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    Well-stirred reactor (contd.)

    Conservation of Species providesNequations withN+1 unknowns

    Additional equation from conservation of energy

    inout hhmQ

    N

    j

    jj

    ii

    i

    MWX

    MWX

    Y

    1

    Where, [Xi]and Y

    iare related as

    Conservation of energy for steady state,

    steady flow conditions:

    In terms of individual species :

    N

    i

    iniini

    N

    iiouti

    ThYThYmQ1

    ,

    1

    ,

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    Well-stirred reactor (contd.)

    T

    T

    ipifi

    ref

    dTchTh ,0,Where,

    Conservation of mass and conservation of energy are simultaneously

    solved forTand Yi,out

    Solution Methodology:

    Coupled non-linear algebraic equations, rather than system ofODEs

    Mass generation rate depends only on Yior[X]i

    Generalized Newtons methodused to solve the system

    "'im

    Mean residence time, tR

    mVtR /

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    Plug flow reactor

    Assumptions:

    Steady state and steady flow operation

    No mixing in the axial direction

    Uniform properties in direction perpendicular to flow

    Ideal frictionless flow

    Ideal gas behavior

    X

    x

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    Plug flow reactor (contd.)

    Conservation of mass :

    Known quantities :

    ", ( ), ( ) (nozzle or diffuser), ( )i

    m k T A x Q x

    0

    dx

    uAd

    Conservation of momentum: 0dx

    duu

    dx

    dP

    Conservation of energy:

    2

    "

    2 0m

    ud h

    Q Pdx m

    (Pm = perimeter)

    Conservation of species: "'

    ii m

    dx

    uYd

    fori = 1,2,,N

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    22

    Plug flow reactor (contd.)

    Ideal gas equation of state:

    1

    1

    N

    i i

    imix

    mix

    u

    MW

    YMW

    MW

    TR

    P

    Where,

    Hence,N+4 unknowns (Yis,, P, T, u)

    withN+4 equations

    Usable forms of equations

    0111

    dx

    dA

    Adx

    du

    udx

    d

    From conservation of mass

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    23

    Plug flow reactor (contd.)

    0 dx

    duudx

    dP

    0"

    m

    PQ

    dx

    duu

    dx

    dh

    dx

    dYh

    dx

    dTc

    dx

    dh iN

    i

    ip

    1

    From ideal gas calorific

    equation of state h=h(T, Yi)

    01111 dx

    dMWMWdx

    dTTdx

    ddxdP

    Pmix

    mix

    From conservation of momentum

    From conservation of energy

    From ideal gas law

    dx

    dY

    MW

    MW

    dx

    dMW iN

    i i

    mixmix

    1

    2 1 FromMWmix

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    Combustion system modeling

    Conceptual drawing of a Gas turbine combustor

    Fuel

    Air

    ProductsWSR1 WSR2 PFR