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    Analysis of solid state phase transformationkinetics: models and recipes

    F. Liu1,2, F. Sommer2, C. Bos2 and E. J. Mittemeijer*2

    The progress of solid-state phase transformations can generally be subdivided into three

    overlapping mechanisms: nucleation, growth and impingement. These can be modelled

    separately if hard impingement prevails. On that basis, an overview has been given of recent

    numerical and analytical methods for determination of the kinetic parameters of a transformation.

    The treatment focuses on both isothermally and isochronally conducted transformations. To

    extend the range of transformations that can be described analytically, a number of more or less

    empirical submodels, which are compatible with experimental results, has been included in the

    discussion. It has been shown that powerful, flexible, analytical models are possible, once the

    concept of time or temperature dependent growth exponent and effective activation energy, in

    agreement with the existing experimental observations, has been adopted. An explicit (numerical)

    procedure to deduce the operating kinetic processes from experimental transformation-rate data,

    on the basis of different nucleation, growth and hard impingement mechanisms, has been

    demonstrated. Without recourse to any specific kinetic model, simple recipes have been given for

    the determination of the growth exponent and the effective activation energy from the

    experimental transformation-rate data.

    Keywords: Phase transformation, Kinetics, Nucleation, Growth, Impingement, Isothermal, Isochronal, Numerical and analytical kinetic analyses

    IntroductionSolid-state phase transformations are important means

    for the adjustment of the microstructure and thus the

    tuning of the properties of materials. To exploit this tool

    to full extent, much effort is spent on the modelling of

    phase transformations, e.g. Refs. 113. The required

    models should not be in particular of atomistic nature,

    but pertain to larger, mesoscopic and even macroscopic

    scales. However, atomistic simulations can be very

    useful for the interpretation of the values obtained for

    the kinetic parameters.1416

    In the classical treatment,6 the JohnsonMehl

    Avrami (JMA) approach15 plays a central role in

    studies of transformations where nucleation and growthmechanisms operate. Very many experimental results ofphase transformation kinetics have been fitted with a

    JMA model. The original JMA equation can only be

    validated under certain conditions, in particular for

    nucleation (see the following section).15 Under these

    conditions, the growth exponent n and the effective

    activation energy Q should be constant during the

    course of the transformation. The JMA equation can

    also be applied to transformations that do not satisfy

    these conditions, but then n and Q are generally notconstant.6 When, in practice, n and Q are found not tobe constant, a traditional explanation is the suggestionof corresponding changes in the nucleation and

    growth mechanisms during the course of the transfor-mation.1722 As shown in Ref. 6 and as will be shown

    more explicitly in the present work, this is notnecessarily the only explanation (i.e. even with constantnucleation and growth mechanisms during the entire

    transformation, Q and n do not have to be constant).

    A general modular, transformation model is possiblethat recognises the three mechanisms, nucleation,growth and impingement of the growing new phase

    particles, as entities that can be modelled separately ifhard impingement is adopted.23,24 In a treatment dealing

    with the analysis of phase transformation kinetics, bothisothermally and non-isothermally (in particular iso-chronally, i.e. constant heating/cooling rate) conducted

    transformations have to be considered. It will be shownhere that also for isochronally conducted transforma-tions, explicit equations for the effective activation

    energy and the growth exponent can be given.

    Two routes of this modular approach23,24 have been

    shown to be feasible. First, a numerical description of

    the transformation can be given. Fitting on that basis toexperimental data in principle leads to determination ofphysically meaningful parameters that are characteristic

    for the process. This numerical method has not beenapplied often.25,26 Normally, special recipes arefollowed for the determination of kinetic parameters,

    1State Key Laboratory of Solidification Processing, NorthwesternPolytechnical University, Xian 710072, China2

    Max Planck Institute for Metals Research, Heisenbergstrasse 3, D70569Stuttgart, Germany

    *Corresponding author, email [email protected]

    2007 Institute of Materials, Minerals and Mining and ASM InternationalPublished by Maney for the Institute and ASM InternationalDOI 10.1179/174328007X160308 International Materials Reviews 2007 VOL 52 NO 4 19 3

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    as the (effective) activation energy, on the basis of ananalytical description of the transformation kinetics,subject to assumptions. Furthermore, if both a numer-ical and an analytical description are available, one

    favours the analytical description of the transformation,as the use of analytical expressions has an advantageover numerical calculations because the influence of,for example, the different nucleation, growth and

    impingement models can be more easily identified andinvestigated. Hence, second, against this background,considerable effort has been made recently to arrive at

    accurate, flexible analytical descriptions of phase trans-formation kinetics.2729 The analytical descriptions giveexplicit expressions for the (possible) change in Q and nas the transformation progresses.

    The present paper has been devised to review theserecent developments and to provide a practical guide fortransformation kinetics analysis. Both approaches, thenumerical (the section on The numerical approach) andthe analytical (the section on The analytical approach),will be presented and discussed. An emphasis lies onthe analytical approach and therefore, in particular

    those nucleation and growth modules that are suitablefor analytical analysis will be discussed (the sectionson Modes of nucleation and Modes of growth).Guidelines for a fit procedure to determine the modelparameters are given (the section Determination ofmodel parameters) and examples of applications toexperimental data are included (the section onApplications of kinetic model fitting to real transforma-tions). Furthermore, avoiding full fitting procedures asin the numerical and analytical approaches, recipes willbe given for the determination of the kinetic parameters,without recourse to a specific kinetic model (the sectionon Recipes to determine the effective activation energyand the growth exponent).

    The number of different phase transformations thathas been described with JMA-like models is very large.The present review is restricted to transformations wherethe nucleation and growth mechanisms remain constant

    during the course of the transformation and whichcomply with hard impingement.

    Modes of nucleationIn the following, an overview is given of a number ofdifferent nucleation modes that have been presented inthe literature. Their differences are illustrated by Fig. 1,for the case of isothermal annealing. The nucleationmodes dealt with here and as presented in the literaturegenerally pertain to large undercooling or overheating ofthe transformation system. At this stage of the develop-ment, the equations presented below for the nucleationrate apply to a virtual, infinite volume of untransformedmaterial where the nuclei are not affected by the growthof other nuclei (see the discussion on extended volumebelow).

    Upon a phase transformation, interfaces developbetween the old and the new phases, and (possibly)misfit strain is introduced in the system. Whereas theproduction of the new phase releases chemical Gibbsenergy, the creation of the interfaces and the introduc-tion of misfit strain cost Gibbs energy. According to the

    classical nucleation theory,6,30

    a critical particle size ofthe new phase can be defined such that if the particle isof subcritical size, it costs energy to increase the size of

    the particle, whereas if the particle (nucleus) is ofsupercritical size, energy is released if the particle grows

    further. The formation of particles of supercritical sizefrom particles of subcritical size is called nucleation.

    The nucleation rate is determined by the number ofparticles of critical size and the rate of the jumping of

    atoms through the interface between the parent phaseand the particles of critical size. The frequency ofjumping through the interface is given by an Arrheniusterm. The number of particles of critical size depends onthe critical free energy of nucleus formation DG*, whichaccording to the above description, depends on thedecrease of the chemical Gibbs free energy per unitvolume, the interface energy per unit area and the misfitstrain energy per unit volume. The classical theory ofnucleation gives the nucleation rate per unit volume:N(T(t)), i.e. the rate of formation of particles ofsupercritical size (i.e. nuclei), as6,30

    :N(T(t))~Cv exp {

    DG(T(t))zQN

    RT(t) (1)

    where R is the gas constant, T the temperature, C thenumber density of suitable nucleation sites, v thecharacteristic frequency factor and QN the activationenergy for the jumping of atoms through the interface*.

    Continuous nucleationIf the undercooling or the overheating is very large, DG*can be considered to be very small as compared to RT.

    a pre-existing nuclei (site saturation): N*; b continuous

    nucleation: N0, a51; c continuous nucleation: N0, a51?5; d

    mixed nucleation: N*, N0, a51; e mixed nucleation: N*, N0,

    a51?5; f Avrami nucleation: N9, l05861018 s21 m23; g

    Avrami nucleation: N9, l05661019 s21 m23; h Avraminucleation: N9, l053610

    20 s21 m23

    1 Evolution of the number of nuclei per unit volume with

    time at constant temperature (T5600 K) for different

    nucleation modes with N*5N95261021 m23, N05

    1040 s2a m23

    *Equation (1) is also often written including the Zeldovic non-equilibriumfactor (e.g. Ref. 31) and the characteristic frequency factor is often writtenas kT/h, with kas Boltzmanns constant and has Plancks constant. Here,

    in accordance with Ref. 6, the Zeldovic factor is left out and a constantcharacteristic frequency is used (see also footnote on page 197), allowingthe development of analytical expressions for the (extended) fractiontransformed material (seesection on this subject below).

    Liu et al. Solid state phase transformation kinetics

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    The nucleation rate per unit volume is then only deter-

    mined by the atomic mobility for transport through the

    interface, which for isothermally and non-isothermally

    conducted transformations, gives23,24,27

    :N(T(t))~N0 exp {

    QN

    RT t

    (2)

    where Cv has been combined into N0, the

    temperature-independent nucleation rate. QN, the acti-vation energy for the jumping of atoms through

    the interface between the particle of critical size and

    the matrix, is defined for the remainder of this text as the

    temperature-independent activation energy for nuclea-

    tion. This type of nucleation is called continuous

    nucleation characterised by a constant nucleation rate

    at constant temperature; the number of nuclei equals 0

    at t50. This type of nucleation often operates in the

    crystallisation of amorphous alloys.32

    It should be noted that for smaller undercooling or

    overheating, DG* is not very small as compared to RT.

    In this case, the full nucleation equation (equation (1))

    must be used. Note that DG* in equation (1) depends on

    temperature. An analytical treatment on the basis of

    equation (1) is only possible for isothermal transforma-

    tions (cf. the section on Extended volume and extended

    transformed fraction); an isochronal process could be

    subdivided in isothermal steps to perform an analytical

    treatment per step.

    The nucleation index a

    With the use of equation (2), the nucleation rate is

    constant at constant temperature during the entire

    course of the transformation. To allow for dependence

    of the nucleation rate on the degree of transformation, it

    was proposed to introduce the empirical nucleation

    index a.33,34 The number of particles (for isothermaltransformation) in that case can be expressed as

    N(t)5n9ta, with n9 as a constant (a50 for zero nucleation

    rate, a51 for constant nucleation rate, a.1 for

    nucleation rate accelerating with progress of transfor-

    mation). Values for a in the range of 0,a,1 imply a

    nucleation rate decelerating with ongoing transforma-

    tion. Such a case can better be described with the

    Avrami nucleation mechanism (see below) and there-

    fore, the range 0,a,1 is not considered further.

    Anticipating the analysis of non-isothermal

    (isochronal) kinetics, the nucleation index should be

    introduced such that both time and temperature

    dependences of the nucleation density can be considered.Accordingly, the relationship between N and t for

    continuous nucleation in isothermal transformation

    becomes

    N(T,t)~N0ta exp {

    QN

    RT

    (3)

    and it follows (cf. equation (2))

    :N(T,t)~aN0t

    a{1 exp {QN

    RT

    (4)

    For isochronal transformation, the number of nuclei

    per unit volume of untransformed material can be

    expressed as an integration of the continuousnucleation rate from T0 to T(t), i.e. as a function of

    T(t) (Ref. 35)

    N~

    T t T0

    N0 exp {QN

    RT t0

    !d

    T t0

    W

    %RN0

    QNWT t 2exp {

    QN

    RT t

    (5)

    where W is the constant heating rate dT(t)/dt. The

    temperature integral has been approximated asdescribed in Ref. 7, T(t).T0 and QN=RTww1, implyingthat equation (5) holds for the case of isochronal heating

    (see Appendix).

    Now, adopting the philosophy as described above in

    equation (3) for the case of isothermal annealing, it

    appears appropriate for isochronal annealing to incor-

    porate the nucleation index a as follows

    N T t ~RN0T t

    QN

    T t

    W

    aexp {

    QN

    RT t

    (6)

    and the corresponding nucleation rate is given by

    :N T t %N0

    T(t)

    W

    a{1exp {

    QN

    RT t

    (7)

    For application of the transformation model incorpor-

    ating the nucleation index, see the section on Appli-

    cations of kinetic model fitting to real transformations.

    It should be noted here that all equations involving

    the nucleation index a only provide an empirical

    description of the nucleation rate. When available,

    models with a stronger theoretical justification should

    be used. For a.1, the constant N0 can no longer be

    interpreted as a temperature independent nucleation

    rate; the unit of N0 should be given as s2a m23.

    Saturation by pre-existing nucleiIn the section on Continuous nucleation, it was

    assumed that the number of nuclei at the beginning of

    the transformation is zero. Here, the case is considered

    where there already is a number of pre-existing nuclei

    (supercritical particles of the new phase) at t50 and the

    further nucleation rate is zero. This implies for the

    nucleation rate23,27

    :N(T)~Nd t{0 (8)

    for isothermal transformation and

    :N T t ~Nd

    T t {T0W (9)

    for isochronal transformation, where N* is the number

    of (pre-existing) nuclei per unit volume, d(t20) and

    d{[T(t)2T0]/W} denote Dirac functions and W is the

    constant heating/cooling rate with T05T (t50) and

    T(t)5T0zWt with W5dT(t)/dt.

    A typical situation where the nucleation rate can

    be described by equation (8) or equation (9) is the

    case of saturation caused by preferential

    nucleation at grain boundaries, edges or corners as

    discussed by Cahn.6,36 Depending predominantly on

    the degree of supercooling (or superheating),

    saturation of the (grain boundary) nucleation sites

    can occur very early in the transformation leadingto a zero nucleation rate for the remainder of the

    transformation.

    Liu et al. Solid state phase transformation kinetics

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    The activation energy for supercritical particle formation QS

    Upon rapid cooling/quenching of a phase stable at

    elevated temperature, this phase can become metastable

    at lower temperatures, e.g. an amorphous alloy or a

    supersaturated crystalline solid solution may occur,

    which strives for crystallisation or decomposition

    respectively. Depending on the precise thermal history

    of such metastable phases, more or less particles of a

    new, stable phase may have been frozen in. If a heattreatment is applied subsequently to such a metastable

    phase with frozen-in particles of the new, stable phase,

    then those particles larger than the critical size (which

    are called the nuclei of the new, stable phase24) can

    grow, implying occurrence of initial pre-existing nuclei

    with no formation of further nuclei (cf. equations (8)

    and (9)). The critical size depends on temperature. Then,

    given a certain size distribution for the frozen-in

    particles of the new, stable phase, it is evident that the

    number of nuclei (i.e. supercritical particles) acting in

    the pre-existing nuclei nucleation mechanism is tem-

    perature dependent. Hence, an activation energy QScan be introduced that controls the number of frozen-in

    nuclei acting in the pre-existing nuclei mechanism upon

    progressing transformation.

    As a first approximation, the critical size of the frozen-in

    new phase particles can be assumed to depend on

    temperature as A/DT, with DT as the undercooling.30

    Hence, the critical size increases with decreasing under-

    cooling, i.e. with increasing annealing temperature.

    Assuming that the size distribution of the frozen-in particles

    of the new, stable phase exhibits an exponential tail towards

    larger particle size, the temperature dependence of the

    number of supercritical particles operating in the pre-

    existing nuclei nucleation mode may be given as exp(QS/

    RT). (Note that the number of active sites decreases with

    increasing annealing temperature: thus QS is not anactivation energy in the usual sense, which would have

    required a minus sign in the argument of the exponent.)

    On this basis, an analytical treatment can be given but only

    for the case of isothermal annealing, as explained in

    Ref. 35.

    For isothermal transformations conducted at different

    annealing temperatures, different values for the number of

    the supercritical particles thus occur for each annealing

    temperature T. Equation (8) can then be rewritten as35

    :N(T)~NS exp

    QS

    RT

    d t{0 (10)

    with NS* as a constant.

    Avrami nucleationAccording to this nucleation mechanism, the particles of

    supercritical size (nuclei) are formed from the particles

    of subcritical size of number Nsub (:

    N~{:

    Nsub), such that

    the total number of particles, of sub- and supercritical

    size N9 is constant.24 The change of the number of

    particles of supercritical size is thus equal to the product

    of the number of particles of subcritical size Nsub and

    the rate l, at which an individual subcritical particle

    becomes supercritical

    :N~{

    :Nsub~lNsub (11)

    It is supposed that l obeys Arrhenius-type temperature

    dependence

    l~l0 exp {QN

    RT

    (12)

    with l0 as a temperature-independent rate. Uponintegration of equation (11), after separation of vari-

    ables, using equation (12) and the boundary condition

    that the number of subcritical particles equals N9 at t50,

    it is obtained for the rate of formation of supercritical

    particles at t

    :N T(t) ~{

    :Nsub~lN

    0 exp {

    t0

    ldt

    0@

    1A (13)

    By variation of l0, the mode of nucleation can be

    varied from only pre-existing nuclei (l0 infinitely

    large) to continuous nucleation (l0 infinitely small).This behaviour is shown for isothermal annealing in

    Fig. 1.

    For isothermal annealing, l is constant and equa-tion (13) becomes23

    :N T,t ~Nl exp {lt (14)

    For isochronal annealing, with T(t).T0 and QN/RT&1(usually QN/RT>25), equation (13) can be rewritten

    using the approximation for the temperature integral as

    given in Appendix7,27

    :N T(t) %Nl exp {

    Rl

    QNWT t 2

    (15)

    Mixture of nucleation mechanismsIn practice, mixed types of nucleation may occur. The

    specific name mixed nucleation represents a combination

    of the pre-existing nuclei and continuous nucleation

    modes: the nucleation rate is equal to some weightedsum of the nucleation rates according to continuousnucleation (equations (2), (4) and (7)) and pre-existing

    nuclei (equations (8) and (9)). Hence, for isothermal

    transformation27

    :N(T,t)~Nd t{0 zN0 exp {

    QN

    RT

    (16)

    which after introduction of the nucleation index a (cf.equation (4)), becomes

    :N(T,t)~Nd t{0 zaN0t

    a{1 exp {QN

    RT

    (17)

    and for isochronal transformation

    27

    :N T t ~Nd

    T t {T0W

    zN0 exp {

    QN

    RT t

    (18)

    which after introduction of the nucleation index a (cf.

    equation (7)), becomes

    :N T t ~Nd

    T t {T0W

    z

    N0 exp {QN

    RT(t)

    T t

    W

    a{1" #(19)

    where N* and N0 represent the relative contributions of

    the two modes of nucleation.Unambiguous preference for this type of mixed

    nucleation has been observed for the crystallisation of

    Liu et al. Solid state phase transformation kinetics

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    different amorphous alloys, indicating a contribution ofquenched in nuclei and of subsequent nucleation uponannealing.25,28,29,37

    According to equations (1315), Avrami nucleation

    approaches the continuous nucleation mode and thepre-existing nuclei mode, at the start and at the endof the transformation respectively (see Fig. 1).Therefore, a combination of pre-existing nuclei and

    Avrami nucleation also offers a description of inter-mediate cases of nucleation. Hence, for isothermaltransformation28

    :N(T,t)~Nd t{0 zN0l exp {lt (20)

    and for isochronal transformation

    :N T t ~Nd

    T t {T0W

    z

    N0l exp {Rl

    QNWT(t)2

    (21)

    where N* and N9 represent the relative contributionsof the two modes of transformation. For example,

    the isothermal crystallisation of amorphous MgNialloys was shown to exhibit nucleation according toequation (20).28

    A combination of continuous nucleation with

    Avrami nucleation is physically less meaningful toconsider: according to both nucleation modes, thenumber of nuclei continuously increases with progres-sing transformation.

    Modes of growthTwo (extreme) growth models are considered: one forvolume diffusion controlled growth and one for inter-face-controlled growth. Volume diffusion controlled

    growth can occur for phase transformations where long-range compositional changes take place. The case ofinterface-controlled growth can occur if the growth isdetermined by atomic processes in the immediatevicinity of the interface, as the massive austenite (c)Rferrite (a) transformation in substitutional binary Fe-based alloys3840 and also in some cases of crystallisationreactions of amorphous alloys.28,29

    The diffusion-controlled and interface-controlledgrowth modes can be given in a compact form. At timet, the volume Yof a particle nucleated at time t is givenby24

    Y t,t ~gtt

    n dt0@ 1A

    d=m

    (22)

    with g as a particle-geometry factor (m3 m2d) and n asthe growth velocity, m as the growth mode parameter(interface-controlled growth: m51; volume diffusioncontrolled growth: m52; particle thickening obeys aparabolic growth law) and das the dimensionality of thegrowth.

    For the case of interface-controlled growth (then

    equation (22) is applied with m51), the textbookequation for the interface velocity v is given by6

    v(T(t))~v0 exp {

    DGa

    RT(t)

    1{ exp

    DG

    RT(t)

    (23)

    where n0 is the pre-exponential factor for growth, DGa is

    the activation energy for the transfer of atoms through

    the parent phase/new phase interface and DG is theenergy difference between the new phase and the parentphase.

    For large undercooling or overheating, DGj j is largecompared to RT and equation (23) becomes

    v(T(t))~v0 exp {QG

    RT(t) (24)with QG (5DG

    a) as the activation energy for growth andn0 as the temperature-independent interface velocity.For interpretation ofDGa, see Ref. 41.

    For small undercooling or overheating, the drivingforce DGj j is small as compared to RTand equation (23)reduces to

    v(T(t))~M({DG)

    ~M0 exp {QG

    RT(t)

    ({DG(T(t))) (25)

    where QG5DGa and M is the temperature dependent

    interface mobility*. Note that DG in equation (25)

    depends on temperature. For isothermal transforma-tions, Y can still be calculated analytically according toequation (22), after substitution of equation (25) ifDGisconstant for the integration. For isochronally conductedmeasurements, Y can only be calculated by numericalintegration. This has led to limited application ofequation (25), as compared to equation (24).

    In general, growth can exhibit a mixed-mode char-acter: the transformation can start with interface-controlled growth and then a transition to diffusion-controlled growth can occur, as obtained from modelconsideration, e.g. for the isothermal austenite (c)Rferrite (a) transformation in FeC alloys.42 The transi-tion from interface-controlled growth to diffusioncontrolled growth has been observed during nano-crystallisation of amorphous Al-based alloys.32

    The activation energy introduced for nucleation in thesection on Continuous nucleation QN (cf. equation (2))has been conceived as an activation energy for thetransfer from the matrix (cf. an atom) through the inter-face between the particle of critical size and the matrix;thereby the particle considered becomes a nucleus. Inthe current section, the activation energy introducedfor interface controlled growth QG (5DG

    a) (cf. equa-tion (23)) has been conceived as an activation energy fortransfer from the matrix (of an atom) through theinterface between the growing particle (much larger than

    a nucleus) and the matrix. Both activation energiesdepend on elementary atomic jumps. Yet, they can haveconsiderably different values. This may be due toconsiderably different structures for the interface withthe matrix for the minute embryos (particles smallerthan and just equal to critical size) and for the muchlarger (up to orders of magnitude) growing particles.

    *Equation (24) contains v0 as the temperature-independent interfacevelocity. This means that v0 includes a temperature independentfrequency factor. In the derivation of equation (25) from equation (23) apre-exponential factor M05v0/RT appears. To arrive at a temperatureindependent factor M0 (equation (25)) the atomic vibration frequency isusually assumed to be proportional to kT/h(with kas Boltzmanns constant

    andh

    as Plancks constant). Because the influence of the temperaturedependence of the frequency factor is small in comparison to theexponential term the error that is made by adopting either v0 astemperature independent or M0 as temperature independent is small.

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    For example, in initial stages, coherent interfaces mayoccur, whereas a growing particle may exhibit anincoherent interface. Then in the initial stage of growth,the activation energy may change due to the occurring

    changes in the interface structure. Activation energiesfor interface mobilities can be determined by groups ofatomic jumps leading to effective activation energiesconsiderably larger than the activation energy for a

    single atomic jump.41 Such processes may have sig-nificantly different net effects for minute embryos andlarge growing particles, in view of the different interface

    structures.For the case of diffusion-controlled growth (then

    equation (22) is applied with m52), n in equation (22)can generally be substituted by n according to equa-tion (24), where QG has to be replaced by the activationenergy for diffusion QD and n0 has to be replaced bythe pre-exponential factor for diffusion D0, i.e.n5D(T(t))5D0 exp(2QD/RT).

    Unambiguous results for the activation energies ofboth the nucleation and growth mechanisms for thesame solid-solid state transformation are rare. The

    methodology presented in the present review allowsthe separate determination of QN and QG in one kineticanalysis. First results with this approach demonstratethat QN can be larger than QG (Ref. 28) and that QN canbe smaller than QG or QD but exhibiting the same orderof magnitude.29 Clearly, much more experimental dataare necessary to arrive, possibly with the aid ofdedicated computer simulations,4345 at detailed inter-pretation of values determined for QN and QG or QD.

    Extended volume and extendedtransformed fractionThe number of supercritical nuclei formed in a unit

    volume, at time t during a time lapse dt, is given by:N(T(t))dt, with

    :N(T(t)) according to equations (121).

    The volume of each of these nuclei grows from t until taccording to equation (22) where it is supposed thatevery particle grows into an infinitely large parent phase,in the absence of other growing particles. In thishypothetical case, the volume of all particles at time t,called the extended volume Ve, is given by

    Ve~

    t0

    V:

    N t Y t,t dt (26)

    with V as the sample volume, which is supposed to be

    constant throughout the transformation. To evaluateequation (26) for non-isothermal transformation, it isnecessary to apply explicit time dependences for the

    temperature Toccurring in the expressions for:

    N and Y.The extended transformed fraction xe is defined as

    xe:Ve

    V~

    t0

    :N t Y t,t dt (27)

    To arrive at explicit expressions for xe and as discussedin the section on Modes of growth, in the following,equation (24) will be applied for the growth functionboth for interface- and diffusion-controlled growth. For

    the cases of only pre-existing nuclei and continuousnucleation, it now follows straightforwardly fromequation (27); first, for isothermal transformations

    (equations (2) and (8))

    xe~Kn0 t

    n exp {nQ

    RT

    ~bn (28)

    with b~K0t exp{(Q=RT) and second, for isochronaltransformations (equations (7) and (9))

    xe~Kn

    0t

    0

    exp {Q

    RT t dt24 35

    n

    ~bn (29)

    with

    b%RT2

    WK0 exp {

    Q

    RT

    and for a.1 (continuous nucleation) with b>

    T2K0 exp({Q=RT). For both isothermal and isochro-nal transformations, n is the constant growth exponentand Q is the constant effective activation energy (see

    Table 3 for Kn0 , n and Q).

    For all the other (mixed) nucleation modes considered(equations (13) and (1621)), the extended volume can

    be shown to be given always by the addition of twoparts27,28 that can be conceived as due to pre-existingnuclei and to continuous-like nucleation (a>1) respec-

    tively. Then, by extensive calculation, the followingexplicit analytical expressions for the extended trans-formed fraction can be obtained27

    for isothermal transformation

    xe~K0 t n t

    tn t exp {n t Q t

    RT

    (30)

    for isochronal transformation

    xe~K0 T n T RT

    2

    W

    n T

    exp {n T Q T

    RT (31)

    for a51

    xe~K0 T n T

    T2 n T

    exp {n T Q T

    RT

    (31a)

    for a.1, which can be generally written as

    xe~Kn0 a

    nexp {

    nQ

    RT

    (32)

    where a is identified with either the annealing time t for

    isothermal transformation or with RT2/W (a51) and T2

    (a.1) for isochronal transformation.

    In general, the kinetic parameters n, Q and K0 are

    functions of time t (isothermal transformation) ortemperature T (isochronal transformation) and dependon model parameters as N*, N0 and a (mixed nucleation

    incorporating a.1) or N9 and l0 (Avrami nucleation),QN, QS (pre-existing nuclei incorporating QS) and QG(see the section on Isochronal crystallisation of amor-

    phous Zr50Al10Ni40). Explicit expressions for n, Q andKn0 , in terms of the general nucleation and growthmechanisms, for both isothermal and isochronal anneal-

    ing (heating), have been listed in Tables 13.

    Finally, it is noted that within the theoretical frame-work of this section, equation (30) holds exactly,whereas equation (31) is subject to the approximation

    made for the temperature integral in nucleation andgrowth functions and thus pertains to the case ofisochronal heating.

    Liu et al. Solid state phase transformation kinetics

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    Table1

    Expressions

    forthe

    (time

    and

    temp

    erature

    dependencies

    ofthe)growthe

    xponentn,the

    overallactivation

    energ

    y

    Q

    and

    the

    rate

    constantK0,to

    be

    inserted

    into

    equation(32)

    forisothermalannealingandisochr

    onalannealingrespectively*

    Isothermal

    Isochronal

    Mixednucleation

    27

    n

    n~

    d mz

    1

    1z(r2=r1){

    1

    n~

    d mz

    1

    1z(r

    2=r1){

    1

    Q

    d mQGz

    n{

    d m

    QN

    !0n

    d mQGz

    n{

    d m

    QN

    !0n

    Kn 0

    gv

    d=m

    0

    (d=m)z11

    =1z(r

    2=r1)

    1

    N

    1z

    r2 r1

    !1=1zr2=r1

    N0

    1z

    r2 r1{1

    "

    #

    (

    )1=1z(r

    2=r1)

    1

    gv

    d=m

    0

    (d=m)z11

    =1z(r

    2=r

    1)

    1

    N

    Qd=m

    G

    1z

    r2 r1

    "

    #1=1zr

    2=r1

    CcN

    0

    1z

    r2 r1{1

    "

    #

    (

    )1=1z(r

    2=r1)

    1

    r2/r1

    N0texp

    {QN=RT

    (d=m)z1N

    CcQ

    d=m

    G

    N0exp

    {QN=RT

    (d=m)z1N

    RT

    2

    W

    Avrami

    nucleation

    27

    n

    d mz

    1

    1z(r

    2=r1)

    d mz

    1

    1z(r

    2=r1)

    Q

    d mQGz

    n{

    d m

    QN

    !0n

    d mQGz

    n{

    d m

    QN

    !0n

    Kn 0

    gN

    0f(lT)v

    d=m

    0

    (d=m)z1

    l1=1zr2=r1

    0

    (lt)

    1=1z(r2=r1)

    1

    gv

    d=m

    0

    N0f(lRT

    2=QNW)

    (d=m)z1

    l1=1

    zr2=r1

    0

    l

    RT

    2

    W

    1=1z(r

    2=r1)

    1

    Cc

    r2/r1

    lt

    (d=m)z1

    CcQ

    d=m

    G

    (d=m)z1

    RT

    2

    W

    l

    Avrami

    nucleationpluspre-existingnuclei

    n

    d mz

    1

    1z(r

    2=r1)

    d mz

    1

    1z(r

    2=r1)

    Q

    d mQGz

    n{

    d m

    QN

    !0n

    d mQGz

    n{

    d m

    QN

    !0n

    Kn 0

    gv

    d=m

    0

    (d=m)z11

    =1z(r

    2=r1)

    Nz

    N0ltf(lt)

    2(d

    =m)z1

    1z

    r2 r1{

    1

    lt

    (d=m)z1

    !1=1z(r

    2=r1)

    1|

    N0l

    0

    f(lt)

    2

    1z

    r2 r1

    lt

    (d=m)z1

    {1

    !1=1z(r

    2=r

    1)

    2 6664

    3 7775

    gv

    d=m

    0

    d=m

    z1

    1=1z

    r2=r1

    1

    Qd=

    m

    G

    Nz

    N0Q

    d=m

    G

    Ccl

    RT

    2

    =W

    fl

    RT

    2

    =QNW

    2

    d=m

    z1

    |

    1z

    1

    d=m

    z1

    CcQ

    d=m

    G

    RT

    2

    W

    l

    r2 r1

    {1

    !

    8>>>< >>>:

    9>>>= >>>;1=

    1z

    r2=r1

    {1

    |

    N0l

    0Ccfl(RT

    2=QNW)

    2

    1

    z

    r2 r1

    1

    (d=m)z1

    CcQ

    d=m

    G

    RT

    2

    W

    l

    {1

    "

    #1=1z(r

    2=r1)

    r2/r1

    N

    N0z

    lt

    2

    (d=m)z1

    flt

    !01 2f(lt)

    N

    N0z

    CcQ

    d=m

    G

    l

    2

    (d=m)z1

    RT

    2

    W

    f

    l

    RT

    2

    QNW

    "

    #,1 2

    f

    l

    RT

    2

    QNW

    *ForCc

    ,f(lt)andf(lRT2

    /QNW),seeRef.27.Thes

    evaluesarevalidfortheanalyticalmode

    lbasedonmixednucleation(a51)andA

    vraminucleationpluspre-existingnuclei,

    aspresentedinthepresent

    paper.

    n0

    andQG

    havetobesubstitutedbyD0a

    ndQD

    inthecaseofvolumediffusion-controlledgrowth.

    Liu et al. Solid state phase transformation kinetics

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    Table2

    Expressions

    forthe

    (time

    and

    temp

    erature

    dependencies

    ofthe)growthe

    xponentn,the

    overallactivation

    energ

    y

    Q

    and

    the

    rate

    constantK0

    ,to

    be

    inserted

    into

    equation(32)

    forisothermalannealingandisochr

    onalannealingrespectively*

    Mixed

    nucleation

    Isothermal

    Isochronal

    n

    d mz

    a

    1z

    r2=r1

    {1

    d mz(

    1za

    2

    )

    1

    1z

    r2=r1

    {1

    Q

    d mQGz

    n{(d=m

    )

    a

    QN

    !=n

    d mQGz

    n{(d=m)

    (1za)=2

    QN

    !=n

    Kn 0

    Interfacecontrolled

    (m51)

    Kn 0

    gv

    d 0=

    Pd i~

    1

    iazi

    {1=1z(r2=r1){

    1

    "

    #N

    1z

    r2 r1

    !1=1zr2=r1

    N0

    1z

    r2 r1{1

    "

    #1=1z(r2=r1){

    1

    8< :

    9= ;

    gv

    d=m

    0

    (d=mz1)1

    =1z(r2=r1){

    1

    N

    RQGW

    d=m

    1z

    r2 r1

    "

    #1=1zr2=r1

    CcN

    0

    Rd=mz1

    Wd=mza

    1z

    r2 r1{1

    "

    #

    (

    )1=1zr2=r1){

    1

    r2/r1

    Interfacecontrolled

    (m51)

    r2/r1

    Pd i~

    1

    iazi

    h

    iN0taex

    p({QN=RT)

    N

    CcQ

    d=m

    G

    N0exp

    {QN=RT

    (d=mz1)N

    RT

    1za

    Wa

    Kn 0

    Volumediffusionco

    ntrolled(m52)

    gv

    d=2

    0

    =

    Pa i~

    1

    i

    (d=2)zi

    {1=1z(r2=r1){

    1

    "

    #N

    1z

    r2 r1

    !1=1zr2=r1

    N0

    1z

    r2 r1{1

    "

    #1=1z(r2=r1){

    1

    8< :

    9= ;

    r2/r1

    Volumediffusionco

    ntrolled(m52)

    Pa i~

    1

    i

    (d=2)zi

    h

    iN0t

    aexp({QN=RT)

    N

    *ForCc

    ,seeRef.27.Thesevaluesarevalidforth

    eanalyticalmodelbasedonmixednuclea

    tionincorporatingthenucleationindexa,aspresentedinthepresentpaper.Equationspresentedforisothermal

    transformationsandvolumediffusioncontrolledgrowthareonlyvalidforintegervaluesof

    a.n0

    andQG

    havetobesubstitutedbyD

    0

    andQD

    inthecaseofvolumediffusion

    controlledgrowth.

    Liu et al. Solid state phase transformation kinetics

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    Because the interpretation of values determined for

    the activation energy of a phase transformation often

    led and leads to confusion in the literature,4650 the

    following remarks are made.

    For all combinations of nucleation (a51) and growth

    modes, with Arrhenius temperature dependences, as

    considered in the present review, the effective, overall

    activation energy of the transformation can be given as

    (cf. Tables 13)

    Q~(d=m)QGz n{d=m QN

    n(33)

    As noted above, Q (through n) is time and temperature

    dependent, whereas the activation energies for nuclea-

    tion and growth QN and QG are constants. Therefore, an

    observation of change of Q with time or temperature,

    i.e. during the course of a transformation, needs not be

    considered as an experimental artefact or as a con-

    sequence of change of transformation mechanism.

    Modes of impingementA relationship between the actually transformed volume

    Vt and the extended transformed volume Ve or betweenthe real transformed fraction f5Vt/V and the extendedtransformed fraction xe5V

    e/V is required. The expres-

    sions for the extended transformed volume/fraction donot account for the overlap of growing particles (hardimpingement). Furthermore, in diffusion-controlled

    transformations, as can pertain to nano-crystallisationof amorphous alloys32,51,52 and the gammaalpha trans-formation in (carbon containing) alloyed steels,53,54 theoverlap of diffusion fields surrounding the growingparticles has to be considered (soft impingement). Somespecific analytical and numerical approaches to accountfor the diffusion fields surrounding the product-phaseparticles have been proposed,5154 which however, areunsuited for general applications. Within the context ofthe general modular transformation model,23,24 modelsfor (hard) impingement are discussed below.

    Randomly dispersed nuclei

    Suppose that the nuclei are dispersed randomlythroughout the total volume. If the time is increasedby dt, the extended and the actual transformed volumeswill increase by dVe and dVt respectively. From thechange of the extended volume dVe, only a part willcontribute to the change of the actually transformedvolume dVt, namely a part as large as the untransformedvolume fraction.15 Hence

    dVt~V{Vt

    VdVe;

    df

    dxe~1{f (34)

    and thus

    f~1{ exp {xe (35)

    Anisotropic growthIn the case of anisotropically growing particles, the timeinterval that particles, after their randomly dispersednucleation, can grow before blocking by other particlesoccurs is, on average, smaller than for isotropicgrowth.13,15,16 This blocking effect due to anisotropicgrowth leads to hard impingement that results in strong

    Table 3 Expressions for the (time and temperature dependencies of the) growth exponent n, the overall activationenergy Q and the rate constant K0, to be inserted into equation (32) for isothermtal annealing and isochronalannealing respectively*

    Isothermtal (a51) Isothermtal ( a.1) Isochronal ( a51) Isochronal ( a.1)

    Continuous nucleationn d=mz1 d/mza d=mz1 d=mz 1za =2Q (d=m)QGzQN

    n

    (d=m)QGzaQNn

    (d=m)QGzQNn

    dm

    QGzn{d=m1za =2 QN

    nK0

    n

    gN0nd=m0

    n

    gN0nd=m0

    n

    gN0nd=m0 Cc

    n

    gnd=m0

    d=mz1CcN0

    Rd=mz1

    Wd=mza

    Isothermal (QS50) Isothermal (QS.0) Isochronal (QS50) Isochronal (QS.0)Pre-existing nuclein d/m d /m d/m Q QG (d=m)QG{QS

    n

    QG

    K0n

    gNnd=m0 gN

    nd=m0 gN

    nd=m0

    *For Cc, seeRef. 27. These values are valid for the analytical model based on continuous nucleation incorporating the nucleation indexor pre-existing nuclei incorporating QS, as presented in the present paper. n0 and QG have to be substituted by D0 and QD in the caseof volume diffusion controlled growth.

    2 The transformed fraction f as a function of the

    extended fraction xe for the case of impingement by

    anisotropically growing particles corresponding to j>1

    and for the case by impingement of non-random nuclei

    distributions corresponding to e>1

    Liu et al. Solid state phase transformation kinetics

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    deviations from classical JMA kinetics.16 Considering

    this blocking effect, one phenomenological approach*

    accounting for impingement in this case has been

    proposed13,16 by extending equation (34) to

    df

    dxe~(1{f)j (36)

    where j>1. Impingement due to equation (36) is more

    severe, i.e. the difference between f and xe is larger thandue to equation (34), and increases with j (see Fig. 2).

    For j.1, integrating equation (36) gives

    f~1{ 1z j{1 xe {1=(j{1)

    (37)

    For j51, equation (36) reduces to equation (34) (see

    Fig. 2).

    Non-random nuclei distributionsA more regular dispersion of the growing particles, as

    compared to the randomly dispersed case, would lead to

    a smaller influence of the impingement correction, i.e.

    the difference between xe and f is smaller. If the initial

    material is polycrystalline, the corners of the grains ofthe parent phase can act as preferred nucleation sites.

    This implies that the dispersion of the growing particles

    cannot be considered as truly random and thus, the

    impingement correction as indicated by equation (34)

    does not hold exactly. The dispersion of the growing

    particles will also be not exactly periodic, corresponding

    to an inexactly homogeneous parent crystallite size and

    shape, and hence the impingement correction for ideally

    periodically dispersed growing particles is also incor-

    rect.38 A general approach to impingement for non-

    randomly distributed nuclei can be proposed

    df

    dxe~1{fe (38)

    with e>1. The impingement according to equation (38)

    with e.1 is less distinct than the one according to

    equation (34), because the difference between f and xe is

    smaller, and decreases with increasing e (see Fig. 2).

    Departing from equation (38), it follows that an

    analytical expression for f cannot be obtained for all

    values of e. However, a simple recursive procedure is

    possible. Provided the differences between the consecu-

    tive f values, fiz1 and fi, and the corresponding xevalues, xe(fiz1) and xe(fi), are sufficiently small, equa-

    tion (38) can be written in difference form and it follows

    fiz1~ 1{fe

    i

    xe fiz1 {xe fi zfi (39)Given the initial condition f150 and xe(f1)50, xe(f2) is

    calculated for t2 (isothermal annealing) or T2 (isochronal

    annealing) and f2 follows from equation (39), etc.

    For special values of e, analytical expressions result.

    Obviously for e51, equation (35) results. For e52, it

    follows

    f~ tanh xe (40)

    This approach was first used to describe the kinetics of

    the massive austenite (c)Rferrite (a) transformation in

    iron and iron-based alloys.3840

    The transformed fractionThe general recipe for deriving an explicit analytical

    formulation or numerically calculating values for the

    degree of transformation in terms of the modular

    transformation model is as follows (see Fig. 3). The

    extended volume is calculated according to equa-

    tion (26) using the appropriate nucleation mode (see

    above) and the appropriate growth mode (see above).

    The expression for the extended volume (see the section

    above) is then substituted into the appropriate impinge-

    ment correction (see the previous section) to give the

    degree of transformation. Note that values of a, e and j

    different from unity imply that a phenomenological

    description of nucleation and/or impingement in the

    fraction transformed is given.

    The numerical approachThe cornerstone of the numerical calculation is the

    evaluation of the extended fraction xe (equation (27))

    that implies the execution of a nested, double integration

    (see equations (22) and (27)). Even with modern

    computers, the full numerical evaluation of equa-tion (27) is not trivial. In a typical fit of the model to

    experimental data, equation (27) must be calculated very

    many times. Not only must equation (27) be evaluated

    for many different times/temperatures (typically y100

    points per xe-curve (or f-curve)), but also for a number

    of different temperatures/heating rates. Thus, a fit to

    experimental data may require very many function

    iterations before the optimal set of parameters is found.

    To directly use equation (27) in a fit of the model to

    experimental data, the numerical evaluation of the

    double integral represented by equation (27) must be

    done as efficiently as possible. Two different approaches

    can be followed to solve equation (27) in a numericalway fast enough for application in a fit procedure that

    can be applied in practice:

    *Equation (36) is one of several phenomenological approaches possible.

    16

    For isothermal transformations with continuous nucleation an analyticaltheory is available,16,55 which, however, cannot be expressed as a relationbetween f and xe.

    3 Schematic diagram of the modular transformation

    model: the specific models for nucleation, growth and

    impingement have to be substituted into the expres-

    sion for the extended transformation fraction xe to cal-

    culate the real transformed fraction f (see the sections

    on Modes of nucleation, Modes of growth and

    Modes of impingement)

    Liu et al. Solid state phase transformation kinetics

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    (i) because the integrands are smooth functions ofthe variables, high order algorithms as describedin Ref. 56 can calculate the integrals with arelatively small number of function evaluations,

    or an even more sophisticated algorithm asdescribed in Ref. 57 can be applied

    (ii) a different approach involves development of analgorithm optimised for the specific problem. The

    inner integral of equation (27) concerns theevaluation of Y. As follows from equation (22),Y is obtained by integrating the growth velocity

    from time (of nucleation) t to time t. Forequation (27), this integral has to be evaluatedfor all times within the considered range of t.However, once Yhas been calculated for t50, allwork has in fact already been done for the othertimes t and by storing the result for t50, Y doesnot have to be calculated for the other values oftanymore. The same principle can be used for theouter integral of equation (27): once it has beenevaluated for the end time of t, most of thecalculation work for the intermediate times has in

    fact already been performed and by storing theresults for t5tend, xe can be calculated with aminimal amount of work for all other values of t.

    The analytical approachThe recipe described above can also be adopted for thederivation of analytical formulations of the degree oftransformation f. The analytical procedures depart from

    equations (30) and (31) for xe (with parameters fromTables 13). Analytical descriptions of f provide moredirect insight into functional dependences and are oftenused in practice. This explains the large, also recent,interest in analytical descriptions of transformationkinetics712,2729 and their application (see, out of an

    enormous body of such literature, a few very recentexamples2022,28,29,35,37).

    In contrast with the original JMA equation,15 whichis still at present often but in many cases inappropriatelyused,17,18,2022 the present overview provides a summaryof possible, flexible analytical approaches. It may be saidthat the variety of single and combined nucleation andimpingement models considered offers the possibility todescribe real phase transformations in many cases.

    The main limitation in the application of theconsidered nucleation and growth modes to arrive atanalytical expressions for f is that the undercooling or

    overheating of the transforming system is relativelylarge, in order that Arrhenius temperature dependencesfor the nucleation and growth rates are assured (cf. thediscussions in the sections on Modes of nucleation and

    Modes of growth). For small undercooling or over-heating, the nucleation and growth modes cannot bedescribed using an Arrhenius temperature dependencewith a constant activation energy (cf. for continuous

    nucleation, equation (1) and for growth, equation (25)).Another limitation of the analytical expressions for f

    is caused by the use of the temperature integral for

    isochronal transformations (see Appendix). As noted inthe section on Extended volume and extended trans-formed fraction, this means that equation (31) is only avalid approximation for isochronal heating. The accu-racy of this approximation is determined by themagnitude of RT/Q (where Q can be either QG orQN), i.e. the first neglected term of the series expansion(see Appendix). Especially, for high values ofn, the errormade by this approximation can be significant eventhough RT/Q is small. To assess the total error made bythe approximation, a comparison with a direct numer-

    ical calculation can be made (as described above in thesection on The numerical approach). Such a compar-ison shows that typically, the activation energies QN andQG are relatively insensitive to the error made by theapproximation but, for example, pre-exponential factorsof the nucleation rate, as N* and N0, can showconsiderable deviations from their true values.

    Numerical v. analytical approachThe analytical formulations for xe as given by equa-tions (30) and (31) have some important advantagesover a direct numerical solution. The analytical solu-tions can show which parameters can be determinedindependently from a fit of the model to experimental

    results (see also the section on Determination of modelparameters). The analytical equations are also easierand much faster to evaluate. The last point becomesimportant for a fit of the model to experimental results(see above).

    On the other hand, the numerical evaluation of xe(equation (27)) allows to consider cases not amenable toanalytical treatment in general, as the case of smallundercooling or overheating for interface-controlledgrowth (i.e. v obeys equation (25)) and the case ofisochronal cooling for which the analytical approxima-tion given by equations (29) and (31) does not hold.

    Table 4 Values of the model parameters used for the numerical calculations of isothermally and isochronallyconducted phase transformations for the case of only pre-existing nuclei, continuous nucleation (incorporatingnucleation index a) and mixed nucleation as nucleation mode, in combination with interface controlled growthas growth mode*

    Parameters d/m N*, m23 N0, m23 s2a QN, kJ mol

    21 QG, kJ mol21 n0, m s

    21 a

    Isothermal 3 0 161028 200 300 161010 13 561016 161028 200 300 161010 13 161018 161028 200 300 161010 13 161019 161028 200 300 161010 13 161019 0 200 300 161010 13 161019 161028 200 300 161010 2

    Isochronal 3 0 161028 200 300 161010 13 161020 0 200 300 161010 1

    3 16

    10

    18

    16

    10

    28

    200 300 16

    10

    10

    13 161018 161028 200 300 161010 1.5

    *cf. the section on Effect of model parameters and impingement and Figs. 4ad and 5ad.

    Liu et al. Solid state phase transformation kinetics

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    Numerical evaluation also allows use of the full

    nucleation rate equation (equation (1)). Thereby, the

    range of different transformation mechanisms that can

    be described with the modular transformation model is

    increased considerably.

    Effect of model parameters andimpingementTo illustrate the role of various kinetic model para-

    meters, the dependences of the growth exponent n, the

    effective, overall activation energy Q and the degree of

    transformation f on transformation time/temperatureand the development of the transformation rate df/dt on

    the degree of transformation have been illustrated for

    the cases of isothermal and isochronal transformations

    in Figs. 4ad and 5ad respectively. Here, mixed

    nucleation (a>1), interface-controlled growth and var-

    ious modes of impingement have been considered. Thevalues for the model parameters have been gathered in

    Table 4.

    Growth exponent and effective activationenergyFor both isothermal and isochronal transformations, ifN*50, continuous nucleation prevails and the values ofn (54) and Q (5(QNz3QG)/4) are constant throughoutthe transformation (see the horizontal bold dotted linesin Fig. 4a and b, and the open circles in Fig. 5a and b)and if N050, the only nuclei are the pre-existing nucleiand the values ofn (53) and Q (5QG) are also constantthroughout the transformation (see the horizontal boldfull lines in Fig. 4a and b, and the open triangles inFig. 5a and b). Upon increasing N*, the contribution ofthe pre-existing nuclei becomes of increasing importanceand thus, the value of n decreases and the value of Qincreases (see Figs. 4a, b 5a and b). n and Q change as afunction of transformation time (Fig. 4a and b) ortemperature (Fig. 5a and b): n changes from 3 to 4 andQ changes from QG to (QNz3QG)/4. Incorporation of

    the nucleation index (a.1) leads to values of n and Qbeyond these ranges (see the dash-dot lines in Fig. 4aand b, and the solid lines in Fig. 5a and b).

    4 a the growth exponent n and b the effective activation energy Q at T5800 K: solid line only pre-existing nuclei,

    N*51610

    19

    m23

    , N050 s21

    m23

    , dashed line pure continuous nucleation, N*50 m

    23

    , N05161028

    s21

    m23

    , $ mixednucleation (a51), N*5561016 s21 m23, N051610

    28 s21 m23, & mixed nucleation (a51), N*5161018 s21 m23,

    N05161028 s21 m23, . mixed nucleation (a51), N*5161019 s21 m23, N051610

    28 s21 m23, dotted line mixed

    nucleation (a52), N*5161019 s22 m23, N05161028 s21 m23; c the transformed fraction f at T5800 K, for different

    nucleation and impingement modes: random nucleation, anisotropic growth (j52) and non-random nucleation (e52),

    as functions of time t, with N*5161018 m23 and N05161028 s2a m23; d the transformation rate df/dt, for mixed

    nucleation with N*5161018 m23 and N05161028 s2a m23, at T5780 and 800 K, as a function of f

    Liu et al. Solid state phase transformation kinetics

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    Transformed fraction and transformation rateThe effect of impingement on the transformationbehaviour is illustrated for both isothermal and iso-chronal annealing in Figs. 4c, d, 5c and d respectively.Clearly, for any nucleation mode considered, the time

    (isothermal transformation) or temperature (isochronal

    transformation) to attain the same fraction transformedis reduced with changing the mode of impingement from

    equation (38) to (34) and then to equation (36).

    For any kind of nucleation and growth modesconsidered, the height of the df/dt (df/dT51/W df/dt)peak maximum occurs at the same f value applying thesame impingement model and irrespective of the appliedannealing temperature or applied heating rate, moves to

    larger f values with changing the mode of impingementfrom equation (34) to (36) (j52) and then to equa-tion (38) (e52) (Figs. 4d and 5d).

    If impingement according to random nucleation (seeequation (34)) is taken as a reference, impingement in

    the case of anisotropic growth (equations (36) and (37))retards the transformation (i.e. the height of the df/dtmaximum decreases) while the df/dt maximum moves to

    smaller values of f with increasing j (Figs. 4d and 5d),

    whereas impingement according to non-random nuclea-tion (equations (38) and (39)) accelerates the transfor-

    mation (i.e. the height of the df/dt maximum increases)

    while the df/dt maximum can appear at larger f values

    with increasing e.

    Determination of model parametersAccording to the modular model,23,24 for extreme

    conditions such as pure continuous nucleation (a>1)

    or where growth occurs only at pre-existing nuclei,equations (30) and (31) reduce to equations (28) and

    (29): an analytical solution characterised by the follow-

    ing set of model parameters: n0 (or D0), QN and QG (or

    QD) together with either N* or N0 and a, with constant

    values for n, Q and K0 (see Table 3). For these extreme

    conditions, n, Q and K0 can be chosen as the fittingparameters.

    For all mixed nucleation modes considered in thisoverview, n, Q and K0 are time or temperature dependent.

    Accordingly, the parameters to be fitted aren0 (or D0), QN

    5 a the growth exponent n and b the effective activation energy Q as a function of temperature T at different heating

    rates as indicated: # pure continuous nucleation, N05161028 s21 m23, N*50 m23, e only pre-existing nuclei,

    N050 s21 m23, N*5161020 m23, dashed line mixed nucleation (a51), N05161028 s21 m23, N05161018 m23, solidline mixed nucleation (a51?5), N051610

    28 s21?5 m23, N*5161018 m23; c the transformed fraction f as a function of

    temperature T for various impingement modes and for different nucleation modes, at W51 K s21: N*5161018 m23,

    N05161028 s2a m23; d the transformation rate df/dT as a function of f for various impingement modes and for mixed

    nucleation at heating rates as indicated: N*5161018 m23, N05161028 s2a m23

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    and QG (or QD) together with either N*, N0 and possibly

    a (mixed nucleation with possibly a>1), or N9 and l0(Avrami nucleation), or N*, N9 and l0 (Avrami nuclea-

    tion plus pre-existing nuclei) (see the sections on Modes

    of nucleation and Modes of growth).

    As follows from the equations gathered in Tables 13,

    n0 (or D0) is not an independent parameter. In the case of

    mixed nucleation (with a>1), it is multiplied with N0 and

    N*

    , in the case of Avrami nucleation withl0 or in the caseof Avrami nucleation plus pre-existing nuclei with l0, N*

    and N9. This means that a change in n0 can be fully

    compensated by a change in the other parameters.

    Parameter determinationThe discussion above implies that individual values for

    n0, N0 and N* (mixed nucleation with a>1), or n0 and l0(Avrami nucleation), or n0, l0, N* and N9 (Avrami

    nucleation plus pre-existing nuclei), cannot be deter-

    mined independently by fitting to experimental kinetic

    data. Hence for a fit to kinetic data, one of these

    parameters must be given an estimated, fixed value. In

    the recipe given below, a fixed value for n0 will be used.

    It must be realised that the value assigned to n0 directlyinfluences the absolute value of the other parameters.

    For example, in the case of mixed nucleation (with a51),

    ifn0 is taken as 106 m s21, but in reality is (found to be)

    1010 m s21, then the values obtained for N0 and N* by

    the fit procedure will be much too high (yet, because

    both N0 and N* deviate with the same factor, the ratio

    N0/N* is found correctly).

    On this basis, the following procedure for determina-

    tion of the model parameters by fitting to the experi-

    mental data is appropriate:

    (i) choose values for a and for n0 (or D0). Physically

    reasonable initial values for these parameters can

    be chosen, for example within the range of valuesgiven in Tables 4 and 5

    (ii) fit the model to the experimental data which leads

    to optimal values for QN and QG, and for N0 and

    N* (mixed nucleation with a>1), or l0 (Avrami

    nucleation), or l0, N* and N9 (Avrami nucleation

    plus pre-existing nuclei).

    If the optimal value for a is unknown, this procedure

    should be repeated for different values of a.

    With extra experimental information, it is possible toarrive at absolute values for the fit parameters. Thenucleation rate as described in the section on Modes ofnucleation is the nucleation rate for a hypothetical

    infinite volume. The real nucleation rate is given by:

    NR(t)~:

    N(t)(1{f) (41)

    i.e. the real nucleation rate decreases (with respect to:

    N(t) as given in the section on Modes of nucleation)as the transformation progresses. Integrating equa-tion (41) with respect to time gives the real number ofnew particles (per unit volume) formed during thetransformation5

    NR~

    t0

    :N(t)(1{f(t))dt (42)

    Equation (42) can be evaluated numerically. To thisend, experimental or calculated (as the model has

    already been fitted) f values can be used. Fittingequation (42) to the experimentally determined numberof product grains will give absolute values for N0 and N*(mixed nucleation with a>1), or l

    0(Avrami nucleation),

    or l0, N* and N9 (Avrami nucleation plus pre-existingnuclei), as their ratios (as N0/N* in the case of mixednucleation) are already known (see above).

    Sensitivity to experimental errorsFor a correct interpretation of the values obtained forthe parameters of a fit of the modular model toexperimental data, it is important to know how different

    experimental errors affect the fit results. Experimentalerrors are made in temperature and in transformedfraction measurements. These errors can be simulatedseparately and combined departing from ideal, calcu-

    lated f-curves.

    To investigate the effect of an error in the tem-perature measurement, four isothermal f-curves weregenerated with QN5200 kJ mol

    21, QG5300 kJ mol21,

    N051028 m23 s21, N*51018 m23, n0510

    10 m s21 and

    d/m53 (mixed nucleation, a51; see also Table 4 and

    Fig. 4) for T5790, 800, 810 and 820 K. If a systematicerror of 2 K is made in the temperature, then a fit of themodel gives values for QN and QG within 1% of theoriginal, true QN and QG values with which the f-curves

    Table 5 Kinetic parameters as determined by fitting the analytical phase transformation model to the isochronalcrystallisation of amorphous Pd40Cu30P20Ni10 after different pre-annealings for 600 s at different temperaturesTpre (Ref. 25)

    Analytical model based on Tpre, K N*, m23 l0, s

    21 N0, s21 m23 N9, m23

    QN,kJ mol21

    QG,kJ mol21 n

    Q,kJ mol21 Error, %

    Mixed nucleation and volumediffusion controlled growth

    620 1.161019 4.261041 256 330 2.5 301 17622 1.361020 3.561041 255 325 14623 2.361020 4.161041 254 321 12625 6.161020 5.561041 255 315 11626 7.461020 7.461040 255 315 10628 2.261021 2.261041 250 315 12629 8.161021 2.161040 253 320 1.5 320 11

    Avrami nucleation and volumediffusion controlled growth

    620 4.661017 1.261024 252 313 2.5 299 17622 1.061018 8.161023 247 310 13623 9.861018 9.861023 259 309 14625 8.261019 1.361024 254 320 14626 5.061019 1.161022 249 319 15

    628 8.4610

    20

    2.0610

    24

    256 315 15629 1.061021 1.061022 253 318 1.5 318 14

    Analytical models based on interface-controlled growth and mixed nucleation or Avrami nucleation .100

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    were generated. The values found for N* and N0 alsoonly deviate minimally from their original values.However, if a statistical error of 1 K is imposed

    (some temperatures are too high, others too low), then adirect fit ofQN, QG, N* and N0 is rather sensitive to theinitial values chosen for the fit parameters; different

    initial values lead to rather different results for theparameters determined by fitting (QN and QG candeviate up to 30% of the original, true values) althoughthe goodness of fit is nearly equal (for the different sets

    of final values for the parameters).

    The influence of an error in the measurement of f hasbeen assessed for the same data set as above. An error infis simulated by shifting an entire curve 1% down or up.No matter whether all curves are shifted in the samedirection (systematic error) or whether some curves areshifted up and others down (statistical error), the fitresults are similar: QG, N0 and N* are close to theiroriginal, true values, but QN can deviate up to 35% fromits original value.

    In the section on Recipes to determine the effectiveactivation energy and the growth exponent, recipes for

    the direct determination of the effective activation energyQ and the growth exponent n from experimental data arepresented. Once both Q and n are known as a function off, QG and QN can be determined by fitting equation (33)to the (Q, n) data set. The values found for QG and QN bythis two-step procedure (applied to simulated data witherrors in T and/or f as described above) are closer (seebelow) to the original, true values, then as determinedby a direct fit (as above) of the model, here with thefour parameters QN, QG, N* and N0. Therefore, it isrecommended to first determine QG and QN (via Q and n)by the recipes described in the section on Recipes to

    determine the effective activation energy and the growthexponent. Values for parameters as N* and N0 can thenbe found by fitting the model to the experimental

    transformation curves with fixed QG and QN (firstdetermined by the two-step procedure). Applying thistwo-step fit procedure to the simulated data containingstatistical errors in both Tand f, QG and QN were found

    to be within 15% of their original values ( N* and N0 candeviate up to a factor of 104 of their original, true values).

    Applications of kinetic model fitting toreal transformations

    Crystallisation of bulk amorphousPd40Ni10P20Cu30The kinetics of the crystallisation of amorphousPd40Ni10P20Cu30 was investigated on the basis of dif-ferential scanning calorimetry (DSC) measurements as

    presented in Ref. 25. Isothermal pre-annealing in thesupercooled liquid temperature range has significantinfluence on the kinetics of the transformation (see Fig. 6).

    The kinetic parameters were determined by fitting theanalytical modular phase transformation model to,simultaneously, all DSC runs recorded isochronallyemploying five different heating rates.

    Of all nucleation, growth and impingement modesconsidered, it was found that mixed nucleation (a51) orAvrami nucleation, volume diffusion controlled growth

    and impingement for randomly dispersed nuclei providethe best description of the isochronal crystallisationbehaviour of amorphous Pd40Cu30P20Ni10 (see Fig. 6).

    A gradual change of nucleation mode can be realisedby increase of the pre-annealing performed before the

    kinetic analysis. As indicated by the observed increase of

    N*

    upon pre-annealing (mixed nucleation with a51; cf.equation (18)) and by the increase of l0 upon pre-annealing (Avrami nucleation; cf. equation (15)), it

    6 Rate of enthalpy change divided by the heating rate,

    dDH/Wdt5dDH/dT, due to isochronal crystallisation of

    amorphous Pd40Cu30P20Ni10, at the heating rates indi-

    cated, as measured (symbols), and as fitted (lines), by

    adopting mixed nucleation and volume diffusion con-

    trolled growth, after pre-annealing for 600 s at 623, 626

    and 629 K

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    follows that the character of the nucleation mode

    changes from largely continuous nucleation to only

    pre-existing nuclei for increasing pre-annealing. Also,

    depending on the degree of pre-annealing performed, the

    obtained value of n varies between d/m (3/2) pertaining

    to only pre-existing nuclei and d/mz1 (5/2) pertaining to

    continuous nucleation (see Tables 3 and 5).

    In particular for the cases of intermediate pre-

    annealing, n and Q are not constant during thetransformation (see Fig. 7). Values for QN and QD are

    a direct result of the fitting of the kinetic model. They

    can also be determined from the dependence of Q on n

    by fitting of equation (33); this makes sense if Q and n

    have been determined without full fitting of a kinetic

    model (see the section on Recipes to determine the

    effective activation energy and the growth exponent).

    The values for QN and QD determined here by full fitting

    of the kinetic model (see Table 5) indeed do not depend

    on the degree of pre-annealing, as it should be.

    Isochronal crystallisation of amorphous

    Zr50Al10Ni40The crystallisation kinetics of the amorphousZr50Al10Ni40 alloy was measured by means of

    isochronally conducted DSC scans. For details about

    the experiments performed, see Ref. 37. The measured

    heat release due to crystallisation is proportional to df/

    dT, i.e.

    dDH

    dT~DHt

    df

    dT

    with DHt as the total enthalpy of crystallisation. DHt(df/

    dT) has been calculated on the basis of equations (31)

    and (35) and has been fitted to the experimental DSCdata (dDH/dT).

    Of all nucleation, growth and impingement modes

    considered, it was found that the isochronal crystal-

    lisation of Zr50Al10Ni40 can best be described by mixed

    nucleation with a nucleation index a54?6, interface-

    controlled growth and impingement according to ran-

    dom nucleation (see Fig. 8a). The importance of

    incorporating the nucleation index (a.1) in the

    model is illustrated by Fig. 8: evidently, the results

    obtained by fitting using an imposed value of a51

    (Fig. 8b) give a bad fit to the experimental data. A value

    of the nucleation index distinctly larger than one

    indicates that the nucleation rate is substantiallyincreased during the transformation. This is reflected

    in the occurrence of a relatively high transformation-rate

    7 a the growth exponent n and b the overall effective

    activation energy Q as a function of temperature for

    isochronal annealing, at the heating rates indicated,

    for the crystallisation of amorphous Pd40Cu30P20Ni10after pre-annealing for 600 s at 626 K

    8 Rate of enthalpy change, dDH/W dt5dDH/dT, due to

    isochronal crystallisation of amorphous Zr50Al10Ni40, at

    the heating rates indicated, as measured (symbols)and as fitted (lines), by adopting mixed nucleation as

    nucleation mode and interface-controlled growth as

    growth mode

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    maximum, which in no way can be described by classicalnucleation modes.

    Recipes to determine the effectiveactivation energy and the growthexponentWithout recourse to any specific kinetic model, it ispossible to determine values for an important kineticparameter as the overall activation energy Q fromexperimental data of the degree of transformation independence on time and temperature.7,35 Thereby, a

    strong practical need is satisfied. Determination of thegrowth exponent n requires adoption of an impingementmodel.

    In this section, simple recipes are given for determina-

    tion of the time and/or temperature dependent growthexponent n and effective activation energy Q. Sub-sequently, the constant QN and QG values can be

    determined from the dependence of Q on n usingequation (33).23,35

    Effective activation energy Q(f)(i) Isothermal transformationWithout recourse to any kinetic model, values for theactivation energy can be obtained from the lengths oftime tf needed at different isothermal annealing tem-

    peratures, to attain a certain fixed value of f. Withrespect to that given f value, the values obtained byplotting ln tf versus 1/T are usually approximated by a

    straight line, from the slope of which a value for Q(f) isobtained.7 However, this procedure is only strictly validif the effective activation energy Q is constant during thetransformation.

    In general, Q is a function of both transformationtime and temperature (cf. Tables 1 and 2). For iso-

    thermal annealing, the ratio r2/r1 can be expressed asc9ta exp(2aQN/RT) (with c9 as a constant; cf. Tables 1and 2). From equations (35), (37) and (40), i.e. irres-pective of specific nucleation, growth and impingementmodes, it then follows

    d ln tf

    d 1=T ~

    dm

    QGz1

    1z r2=r1 {1 QN

    dmz a

    1z r2=r1 {1

    R~

    Q f TR

    with

    Q f T~dm

    QGz1a

    n f T{dm

    QN

    n f T(43)

    Plotting of ln tf versus 1/T will not yield a truly straightline. Thus, the value ofQ(f) depends on the temperaturewhere the slope of the plot of ln tfversus 1/Tis taken. Todetermine the slope in practice, several annealingtemperatures are required. The slope of the straightlines drawn through the data points of two of thesetemperatures can then be considered as an approxima-tion for Q(f) corresponding to a temperature betweenthese two annealing temperatures. Only for the limitingcases, r2/r1R0 or r2/r1R, the ln tf versus 1/T curvebecomes a truly straight line and Q then equals QG or[(d/m)QGzQN]/n, corresponding to n5d/m and n5d/mza respectively. The dependence of Q on f at the

    temperature (range) considered can be determined byrepeating the above procedure for a chosen number of fvalues.

    (ii) Isochronal transformation

    Without recourse to any kinetic model, values for the

    activation energy can be obtained upon isochronalannealing from the temperature Tf needed to attain a

    certain fixed value off, as measured for different heating

    rates. With respect to that given f value, the data points

    in a plot of ln(Tf2/W) versus 1/Tf are usually approxi-

    mated by a straight line, from the slope of which a value

    for Q(f) is obtained.7

    However, this procedure is strictlyvalid only if the effective activation energy Q is constant

    during the transformation.

    In general, Q is a function of both transformationtime and temperature (cf. Tables 1 and 2). From equa-

    tions (35), (37) and (40), i.e. irrespective of specific

    nucleation, growth and impingement models, it then

    follows

    d l n (T2f=W)

    d(1=Tf)R~{

    dm

    QGz1

    1z r2=r1 {1 QN

    dmz 1za

    21

    1z r2=r1 {1

    ~{Q f W

    with

    Q f W~

    dm QGz 21za n f W{ dm

    QN

    n f W

    (44)

    Plotting of ln(Tf2/W) versus 1/Tf will not yield a truly

    straight line. Thus, the value of Q(f) depends on the

    heating rate where the slope of the plot of ln(Tf2/W)

    versus 1/Tf is taken. To determine the slope in practice,several heating rates are required. The slope of the

    straight line drawn through the data points of two of

    these heating rates can be considered as an approxima-

    tion for Q(f) corresponding to a heating rate between

    these two heating rates. Only for the limiting cases,

    r2/r1R0 or r2/r1R, the ln(Tf2/W) versus 1/Tf curve

    becomes a truly straight line and Q then equals QG or

    (d=m)QGzQN=n, corresponding to n5d/m and n5d/mz(1za)/2 respectively. The dependence of Q on f at

    different heating rates can be determined by repeating

    the above procedure for a chosen number of f values.

    For the case of a constant effective activation energy,

    an equation like equation (44) was proposed originally

    by Kissinger58 for a special case of reaction kinetics,

    although instead of Tf, the temperature where the

    transformation-rate maximum occurs was used. This

    so-called Kissinger equation has been and is often used,

    usually without justification. Mittemeijer7 was the first

    to derive the general validity of the analysis provided

    that the temperature of maximal transformation rate is

    replaced by the temperature of the same degree oftransformation Tf.

    Growth exponent n(f)(i) Isothermal transformation

    Probably, the most popular method to determine n from

    isothermal annealing data is based on the slope of the

    straight line that should occur upon plotting

    ln[2ln(12f)] as a function of lnt and thus6

    d ln{ ln(1{f)

    d ln t~n (45)

    This result holds strictly only for classical JMA

    kinetics,15

    implying a constant value of n. In general,n is not constant (see the section on Effect of model

    parameters and impingement).

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    In general, n is a function of both transformation time

    and temperature (cf. Tables 1 and 2). The ratio r2/r1 can

    be rewritten for isothermal transformation as c0ta (with

    c0 as a constant; cf. Tables 1 and 2). From equa-

    tions (35), (37) and (40), it then follows for the

    corresponding modes of impingement

    d ln { ln 1{f

    d ln t~

    d

    mz

    a

    1z r2=r1 {1~n t T~n(f)T (46)

    d ln1{f 1{j{1

    j{1

    d ln t~

    d

    mz

    a

    1z r2=r1 {1~n t T~n(f)T (47)

    d ln H f

    d ln t~

    d

    mz

    a

    1z r2=r1 {1~n t T~n(f)T (48)

    with a51 for the Avrami nucleation and

    Avrami nucleation plus pre-existing nuclei and a>1

    for mixed nucleation. H(f) denotes the numerical

    relationship between xe and f, expressed as

    xe fiz1 ~ 1{fe

    i {1 fiz1{fi zxe fi according toequation (39). For e52, an analytical form of equa-tion (48) results

    d ln arctanh f

    d ln t~

    d

    mz

    a

    1z r2=r1 {1~n t T~n(f)T(49)

    The curves obtained by plotting ln[2ln(12f)] or

    ln{[(12f)12j21]/(j21)} or ln[H(f)] or ln arctanh(f),

    versus lnt, do not yield truly straight lines (r2/r15f(t)).

    The slope at time t provides the value of n(t) at time t.

    Only for the limiting cases, r2/r1R0 or r2/r1R, the

    above curves become straight lines with their slopes

    equal to d/m or d/mza respectively. Once the depen-

    dence of n on t is known, the dependence of n on f can

    be determined straightforwardly for each isothermalannealing experiment as the relationship between t and f

    has been determined experimentally for each annealing

    temperature.

    (ii) Isochronal transformation

    A value for the growth exponent can be obtained from the

    transformed fraction fT attained at a certain fixed value of

    T, as measured for different heating rates. With respect to

    that given T value, the values obtained by plotting

    ln[2ln(12fT)] versus ln W can be represented by a straight

    line if the growth exponent n is constant during trans-

    formation. The slope of this straight line then equals n

    d ln{ ln 1{fT

    d lnW~n (50)

    This result holds strictly only for the extreme conditions

    as indicated below equation (45).

    In general, n is a function of both transformation time

    and temperature (cf. Tables 1 and 2). For all the

    nucleation and growth modes considered in the present

    review, the value of the growth exponent n can be deter-

    mined in correspondence with the prevailing impinge-

    ment mechanisms (equations (35), (37) and (40)) according

    to equations (35), (37) and (40) respectively

    d ln{ ln 1{fT

    d lnW~

    d

    mz

    1za

    2

    1

    1z r2=r1 {1

    ~n(T)W~n(f)W (51)

    d ln1{fT

    j{1{1

    j{1

    d lnW~

    d

    mz

    1za

    2

    1

    1z r2=r1 {1

    ~n(T)W~n(f)W (52)

    d ln H fT

    d lnW~

    d

    mz

    1za

    2

    1

    1z r2=r1 {1

    ~n(T)W~n(f)W (53)

    For e52, an analytical form of equation (53) results

    d ln arctanh f Td lnW

    ~d

    mz

    1za

    2

    1

    1z r2=r1 {1

    ~n(T)W~n(f)W (54)

    with a51 for the Avrami nucleation and Avraminucleation plus pre-existing nuclei and a>1 for

    mixed nucleation. Plotting of ln[2ln(12fT)], orln{[(12fT)

    12j21]/(j21)}, or ln[H(fT)] or ln arctanh(fT)

    versus ln W does not yield a truly straight line (r2/r15f(W)). The value ofn(T)W depends on the heating rate

    where the slopes of the above plots are taken. Severalheating rates are required to determine the slope in

    practice. The slope of the straight line drawn throughthe data points of two of these heating rates can beconsidered as an approximation for n(T)W correspondingto a heating rate between these two heating rates. Only

    for the limiting cases, r2/r1R0 or r2/r1R, the abovecurves become truly straight lines with their slopes equalto d/m or d/mz(1za)/2 respectively.

    The dependence of n on T at a given heating rate(range) can be determined by repeating the aboveprocedure for a chosen number of T values. Once the

    dependence of n on T is known, the dependence of n on

    f, for the heating rate considered, can be determinedstraightforwardly as the relationship between T and fhas been determined experimentally for each heating

    rate.

    The recipes given here have been applied in analysingthe crystallisation of amorphous alloys.35,37 Once thevalues for n and Q have been determined as a function off, the constant values for QN and QG can be obtainedby fitting of equation (33) to the deduced (Q, n) datapoints.25

    ConclusionsBy adopting a modular approach, nucleation, growthand impingement modes can be straightforwardlyincorporated in a quantitative description of phase

    transformation kinetics. An efficient numerical analysisis possible by utilising the properties of the nesteddouble integral to be evaluated for determination of theextended transformed volume fraction (the section The

    numerical approach).

    The approach presented also provides a flexible,

    analytical description of phase transformation kineticsduring both isothermal and isochronal anneals, i.e. alsofor cases where extreme kinetic conditions (continuousnucleation or growth only at pre-existing nuclei) cannot

    be assumed. In particular, mixed nucleation, a mixture

    of pre-existing nuclei and continuous nucleation(incorporating the nucleation index a), Avraminucleation, Avrami nucleation plus pre-existing nuclei,

    Liu et al. Solid state phase transformation kinetics

    21 0 International Materials Reviews 2007 VOL 52 NO 4

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    interface-controlled growth and volume-diffusion con-

    trolled growth and impingement for random and non-random nucleation and for anisotropic growth have

    been dealt with.

    No matter which of the nucleation and growth modes

    govern the transformation, the extended volume fraction

    of transformation xe can be given as (equations 30 and

    31)

    xe~K0 t n t

    tn t exp { n t Q t RT

    for