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    1

    The Arithmetic Average Case

    of Asian Options:Reducing the PDE to theBlack-Scholes Equation

    Solomon M. Antoniou

    SKEMSYS

    S cientific Knowledge Engineering

    and Management Systems

    37 oliatsou Street, Corinthos 20100, [email protected]

    Abstract

    We consider the path-dependent contingent claims where the underlying assetfollows an arithmetic average process. Considering the no-arbitrage PDE of these

    claims, we first determine the underlying Lie Point Symmetries. After

    determination of the invariants, we transform the PDE to the Black-Scholes (BS)

    equation. We then transform the BS equation into the heat equation and we

    provide some general solutions to that equation. This procedure appears for the

    first time in the finance literature.

    Keywords: Path-Dependent Options, Asian Options, Arithmetic Average Path-

    Dependent Contingent Claims, Lie Symmetries, Exact Solutions.

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    1. Introduction

    A path-dependent option is an option whose payoff depends on the past history of

    the underlying asset. In other words these options have payoffs that do not depend

    on the assets value at expiry. Two very common examples of path-dependent

    options areAsian options and lookback options.

    The terminal payoff of an Asian option depends on the type of averaging of the

    underlying asset price over the whole period of the options lifetime. According to

    the way of taking average, we distinguish two classes of Asian options: arithmetic

    andgeometric options.

    A lookback option is another type of path-dependent option, whose payoff

    depends on the maximum or minimum of the asset price during the lifetime of the

    option.

    The valuation of path-dependent (Asian) European options is a difficult problem

    in mathematical finance. There are only some simple cases where the price of

    path-dependent contingent claims can be obtained in closed-form (refs. [1]-[8]).

    If the underlying asset price follows a lognormal stochastic process, then its

    geometric average has a lognormal probability density and in this case there is a

    closed-form solution (ref. [5]). This is not however the case by considering

    arithmetic average. In this case there is no closed-form solution. However in both

    cases there are some numerical procedures available (ref. [8]).

    It is the purpose of this article to provide a closed-form general solution for the

    arithmetic path-dependent options.

    The paper is organized as follows: In Section 2 we consider the general problem of

    pricing the path-dependent contingent claims. In Section 3 we consider the Lie

    Point Symmetries of the Partial Differential Equation (equation (3.1)) for the path-

    dependent arithmetic average options. Full details of the calculation are provided

    in Appendix A. In Section 4, considering two invariants of the PDE, we convert

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    the equation into the Black-Scholes equation. In section 5, we transform the BS

    equation to the heat equation. We then find the general solution of our PDE

    (Theorem 3). In section 6 we provide some solutions to the heat equation.

    Because of the complexity of the calculations, we have included a great deal ofcalculation details, supplemented by many Appendices.

    2. Path-Dependent Contingent Claims

    Suppose that an option pays off at expiration time T an amount that is a function

    of the path taken by the asset between time zero and T. This path-dependent

    quantity can be represented by an integral of some function of the asset over the

    time period 0 :

    =T

    0

    d),S(f)( (2.1)

    where )t,S(f is a suitable function. Therefore, for every t, t0 , we have

    =t

    0

    d),S(f)t( (2.2)

    or, in differential form,

    dt)t,S(fdA = (2.3)

    We have thus introduced a new state variable A, which will later appear in our

    PDE.

    We are now going to derive the PDE of pricing of the path-dependent option. To

    value the contract, we consider the function )t,A,S(V and set up a portfolio

    containing one of the path-dependent options and a number of the underlying

    asset:

    S)t,A,S(V = (2.4)

    The change in the value of this portfolio is given by, according to Its formula, by

    dSS

    VdA

    A

    Vdt

    S

    VS

    2

    1

    t

    Vd

    2

    222

    +

    +

    +

    = (2.5)

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    Choosing

    S

    V

    = (2.6)

    to hedge the risk and using (2.3), we find that

    dtA

    V)t,S(f

    S

    VS

    2

    1

    t

    Vd

    2

    222

    +

    +

    = (2.7)

    This change is risk-free and thus earns the risk-free rate of interest r,

    dtrd = (2.8)

    leading to the pricing equation

    0VrSVSr

    AV)t,S(f

    SVS

    21

    tV 2

    2

    22 =+++(2.9)

    combining (2.7), (2.8) and (2.4), where in (2.4) has been substituted by (2.6)

    for the value of .

    The previous PDE is solved by imposing the condition

    )A,S()T,A,S(V = (2.10)

    where T is the expiration time.

    If A is considered to be an arithmetic average state variable,

    =t

    0

    d)(S (2.11)

    then PDE (2.9) becomes

    0VrS

    VSr

    A

    VS

    S

    VS

    2

    1

    t

    V

    2

    222 =

    +

    +

    +

    (2.12)

    If A is considered to be a geometric average state variable,

    =t

    0

    d)(Sln (2.13)

    then PDE (2.9) becomes

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    0VrS

    VSr

    A

    V)S(ln

    S

    VS

    2

    1

    t

    V

    2

    222 =

    +

    +

    +

    (2.14)

    We list below the payoff types we have to consider along with PDEs (2.12) and

    (2.14).

    For average strike call, we have the payoff )A,S(

    )0,AS(max (2.15)

    For average strike put, we have the payoff

    )0,SA(max (2.16)

    For average rate call, we have the payoff

    )0,EA(max

    (2.17)

    For average rate put, we have the payoff

    )0,AE(max (2.18)

    where E is the strike price.

    This is an introduction to the path-dependent options. Details can be found in

    Wilmotts 3-volume set on Quantitative Finance (ref. [3]).

    3. Lie Symmetries of the Partial Differential Equation

    The technique of Lie Symmetries was introduced by S. Lie [11]-[12] and is best

    described in refs [13]-[28]. This technique was for the first time used in partial

    differential equations of Finance by Ibragimov and Gazizov [29]. The same

    technique was also used by the author in solving the Bensoussan-Crouhy-Galai

    equation [30] and the HJB equation for a portfolio selection problem [31]. There is

    however a growing lists of papers in applying this method to Finance. For a non

    complete set of references, see [29]-[40].

    We consider the PDE (2.12)

    0VrA

    VS

    S

    VSr

    S

    VS

    2

    1

    t

    V

    2

    222 =

    +

    +

    +

    (3.1)

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    We shall determine the Lie Point Symmetries of the previous equation.

    We follow closely Olver (ref. [15]).

    Let )V,t,A,S( )2( be defined by

    VrA

    VS

    S

    VSr

    S

    VS

    2

    1

    t

    V)V,t,A,S(

    2

    222)2(

    +

    +

    +

    = (3.2)

    We introduce the vector field X (the generator of the symmetries) by

    +

    +

    =A

    )V,t,A,S(S

    )V,t,A,S(X 21

    V)V,t,A,S(

    t)V,t,A,S(3

    +

    + (3.3)

    We calculate in Appendix A the coefficients 321 ,, and and we find that

    the Lie algebra of the infinitesimal transformations of the original equation (3.1)

    is spanned by the five vectors

    tX1

    = (3.4)

    A

    X2

    = (3.5)

    AA

    SSX3

    +

    = (3.6)

    VV)ArS(

    2

    AA

    SAS2X

    2

    24

    +

    +

    = (3.7)

    V

    VX5

    = (3.8)

    and the infinite dimensional sub-algebra

    V)t,A,S(X

    = (3.9)

    where )t,A,S( is an arbitrary solution of the original PDE (3.1).

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    4. Reduction of the equation to the BS equation

    We shall now try to transform the pricing differential equation into another by

    reducing the number of independent variables. We shall retain the time variable

    and try to find a combination of the other two variables S and A. The best

    candidate for this job is the generator 4X given by (3.7).

    We state and prove the following Theorem:

    Theorem 1. Any solution of the partial differential equation

    0VrA

    VS

    S

    VSr

    S

    VS

    2

    1

    t

    V

    2

    222 =

    +

    +

    +

    can be expressed into the form

    =

    A

    Sbexp)t,x(uA)t,A,S(V n (4.1)

    where the function )t,x(u satisfies the Black-Scholes equation

    0uruxrux2

    1u xxx

    22t =++ (4.2)

    with2A

    Sx = , brn = and

    2

    2b = .

    Proof. Considering the generator 4X , we can determine two invariants of the

    PDE. For this purpose we have to solve the following system

    V)ArS(

    dV

    2

    A

    dA

    AS2

    dS 2

    2 == (4.3)

    The differential equation2

    A

    dA

    AS2

    dS= is equivalent to

    A

    dA2

    S

    dS= , which can be

    integrated to give 12C

    A

    S= from which we can obtain our first invariant x:

    2A

    Sx = (4.4)

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    The second differential equation

    V)ArS(

    dV

    2

    A

    dA 2

    2 =

    can be written as (since 2AxS = )

    V

    dVdA

    A

    ArAxb

    2

    2

    =

    ,

    or

    V

    dVdA

    A

    rxb =

    where 22b = . By integration of this equation we find

    VlnC)AlnrAx(b 2 =+

    from which there follows that Axbbr eACV= , where C is a constant.

    Therefore another invariant of the PDE is the function )t,x(u , related to )t,A,S(V

    by

    = AS

    bexp)t,x(uA)t,A,S(Vn

    (4.5)

    with2

    r2brn == .

    Upon substitution of )t,A,S(V given by (4.5) into equation (3.1), we find that the

    function )t,x(u satisfies the BS equation

    0uruxrux

    2

    1u xxx

    22t =++ (4.6)

    The proof is in Appendix B.

    5. Transformation of the BS equation to the heat equation.

    Under the substitution

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    is transformed into the equation

    yy2

    2

    1 = (5.11)

    Introducing further a new independent variable by

    2

    y = (5.12)

    equation (5.11) is transformed to the heat equation

    ww = (5.13)

    where

    )y,(),(ww == (5.14)

    We thus arrive at the following

    Theorem 2. The solution to the BS equation (4.6) is given by

    ),(we)t,x(ur= (5.15)

    where

    )x(ln

    2y

    2 +== (5.16)

    t

    =(5.17)

    and ),(w satisfies the heat equation ww = .

    Using Theorems 1 and 2, we get the following

    Theorem 3. The differential equation (3.1) has the general solution

    = r

    A

    Sbexp),(wA)t,A,S(V

    m (5.18)

    where the function ),(w satisfies the heat equation ww = .

    The variables and are defined by (5.16) and (5.17) respectively, while

    brm = ,2

    2b = , is given by (5.3) and x by (4.4).Therefore equation (5.18)

    can be written in full notation as

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    = r

    A

    S

    2exp),(w

    A

    1)t,A,S(V

    2

    r22

    where

    +

    =

    2

    1r

    A

    Sln

    2

    2

    2

    What we need now is some solutions to the heat equation, which are not singular

    at 0 = ( Tt = ). We come to this point next.

    6. General solutions of the heat equation

    The Lie algebra of the infinitesimal symmetries of the heat equation ww = is

    produced by the six vector fields

    X1

    =

    2

    X4

    +

    =

    X2

    = w

    w

    2X5

    =

    w

    wX3

    = w

    w)2(

    4

    4X22

    6

    +

    +

    =

    and the infinite dimensional sub-algebra

    w ),(X =

    where ),( is an arbitrary solution of the heat equation (refs. [15], [37]).

    6.1. The solution that is invariant with respect to the generator

    w2

    2

    362 w)a2()14(4XaXX +++=++

    (a is a constant) is given by ([15], [37])

    +

    +

    +

    +=

    14

    2,

    2

    aWK

    14

    2,

    2

    aWK

    14

    1),(w

    22

    214 2

    +

    + )2arctan(

    2

    a

    14

    exp

    2

    2

    (6.1)

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    where )z,a(W is the parabolic cylindrical function of imaginary argument

    (Appendix D).

    Note. The solution given by Olver [15] (Example 3.17, p.208) contains some

    misprints. We have repeated the calculations [28] and we have found the solutiongiven by (6.1).

    6.2. The solution that is invariant with respect to the generator

    w52 w2XX +=

    is given by ([15], [37])

    ++++=3

    2exp})(BiK)(AiK{),(w

    32

    22

    1 (6.2)

    where )x(Ai and )x(Bi are the Airy functions (Appendix E).

    Both solutions (6.1) and (6.2) we have considered, are not singular for 0 =

    ( Tt = ). This is because we want to take into account the payoff conditions (2.15)-

    (2.18) valid for Tt = ( 0 = ).

    Appendix A. Lie Symmetry Analysis of the pricing PDE.

    We consider the PDE (3.1) :

    0VrA

    VS

    S

    VSr

    S

    VS

    2

    1

    t

    V

    2

    222 =

    +

    +

    +

    (A.1)

    We shall determine the Lie Point Symmetries of the previous equation.

    We follow closely Olver (ref. [15]).

    Let )V,t,A,S()2(

    be defined by

    VrA

    VS

    S

    VSr

    S

    VS

    2

    1

    t

    V)V,t,A,S(

    2

    222)2( +

    +

    +

    = (A.2)

    We introduce the vector field X (the generator of the symmetries)

    by

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    +

    +

    +

    =t

    )V,t,A,S(A

    )V,t,A,S(S

    )V,t,A,S(X 321

    V)V,t,A,S(

    + (A.3)

    The second prolongation is defined in our case by the equation

    SS

    SS

    t

    t

    A

    A

    S

    S)2(

    V

    V

    V

    VXXpr

    +

    +

    +

    += (A.4)

    The Lie point symmetries of the equation are determined by

    0)]V,t,A,S([Xpr)2()2( = as long as 0)V,t,A,S( )2( = .

    We implement next the equation 0)]V,t,A,S([Xpr)2()2( = .We have

    0)]V,t,A,S([Xpr)2()2( =

    0VrVSVSrVS2

    1VXpr ASSS

    22t

    )2( =

    +++

    ++++ )r(]VVrVS[ ASSS2

    1

    0S2

    1)S()Sr(

    SS22tAS =++++ (A.5)

    We have the following expressions for the coefficients S , A ,t

    and SS

    += tS32SV1SS1VS

    S VVV)(

    ASV2tSV3AS2 VVVVV

    += tA32AV2AA2VA

    A VVV)(

    tAV3SAV1SA1 VVVVV

    += St12tV3tt3Vt

    t VVV)(

    tSV1tAV2At2 VVVVV

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    ++= 2SSV1VVtSS3SSS1SVSSSS

    V)2(VV)2(

    + SSS1Vt2SVV3

    3SVV1tSSV3

    V)2(VVVVV2

    StSV3SSAV2SSSV1SAS2

    VV2VVVV3V2

    SStV3SASV2StS3SASV2 VVVV2V2VV2

    ASS2A2SVV2 VVV

    Using the previous expressions for S , A ,t and SS we get from

    the equation (A.5) that

    +++ r]VVrVS[ ASSS2

    1

    ++ AS2tS32SV1SS1VS VVVV)({Sr

    + }VVVV ASV2tSV3

    ++ SA1tA32AV2AA2VA VVVV)({S

    + }VVVV tAV3SAV1

    ++ At2St12tV3tt3Vt VVVV)(

    + tSV1tAV2 VVVV

    +++ 2SSV1VVtSS3SSS1SVSS22 V)2(VV)2({S

    2

    1

    + SSS1Vt2SVV3

    3SVV1tSSV3

    V)2(VVVVV2

    StSV3SSAV2SSSV1SAS2 VV2VVVV3V2

    SStV3SASV2StS3SASV2 VVVV2V2VV2

    0}VVV ASS2A2SVV2 = (A.6)

    We have now to take into account condition 0)V,t,A,S()2( = .

    For this purpose we substitute tu by

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    VrVSVSrVS2

    1ASSS

    22 +

    into (A.6). We thus derive the equation

    +++ r]VVrVS[ ASSS2

    1

    +++ }VVVVV)({Sr ASV2AS22SV1SS1VS

    +

    ++ VrVSVSrVS

    2

    1}V{Sr ASSS

    22SV3S3

    +++ }VVVVV)({S SAV1SA12AV2AA2VA

    +

    ++ VrVSVSrVS

    2

    1}V{S ASSS

    22AV3A3

    +++ VrVSVSrVS

    2

    1)( ASSS

    22t3Vt

    +

    + At2St1

    2

    ASSS22

    V3 VVVrVSVSrVS2

    1

    +

    ++ VrVSVSrVS

    2

    1}VV{ ASSS

    22SV1AV2

    ++++ }V)2(V)2({S21 2SSV1VVSSS1SVSS22

    + }VV2{S2

    1 2SVV3SSV3SS3

    22

    +

    + VrVSVSrVS

    2

    1ASSS

    22

    ++ SAS2SSS1V3SVV1

    22V2V)2(V{S

    2

    1

    StSV3SSAV2SSSV1 VV2VVVV3

    + }VV2V2VV2 SASV2StS3SASV2

    +

    ++ VrVSVSrVS

    2

    1}V{S

    2

    1ASSS

    22SSV3

    22

    0}VVV{S2

    1ASS2A

    2SVV2

    22 =+ (A.7)

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    Equate all the coefficients of the partial derivatives of the function V to zero. We

    are then going to obtain a system of partial differential equations of the unknown

    coefficients 321 ,, and of the vector field (A.3). Before that, and just for the

    economy of the calculations, we observe that we can get some simple expressions,

    by first looking at the coefficients of the mixed partial derivatives.

    In fact the coefficient of the derivative SAV is )2(S2

    1S2

    22 and that of

    SAS VV is )2(S2

    1V2

    22 which means that 0 S2 = and 0 V2 = .

    Therefore the coefficient 2 does not depend either on S or V:

    )t,A( 22 = (A.8)

    The coefficient of the derivative StS VV is )2(S2

    1V3

    22 and that of StV is

    )2(S2

    1S3

    22 which means that 0 V3 = and 0 S3 = . Therefore the

    coefficient 3 does not depend neither on V nor on S:

    )t,A( 33 = (A.9)

    Because of (A.8) and (A.9), equation (A.7) becomes

    +++ r]VVrVS[ ASSS2

    1

    +++ }VV)({Sr 2SV1SS1VS

    +++ }VVVV)({S SAV1SA1AA2VA

    +

    ++ VrVSVSrVS

    2

    1)(S ASSS

    22A3

    +++ VrVSVSrVS

    2

    1)( ASSS

    22t3Vt

    +

    ++ VrVSVSrVS

    2

    1)V(VV ASSS

    22SV1At2St1

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    ++++ }V)2(V)2({S2

    1 2SSV1VVSSS1SVSS

    22

    0}VV3V)2(V{S2

    1SSSV1SSS1V

    3SVV1

    22 =++ (A.10)

    The coefficient of SSSVV is the sum of the terms

    22V1 S

    2

    1)( and )3(S

    2

    1V1

    22

    and therefore 0 V1 = , which means that

    )t,A,S( 11 = (A.11)

    Therefore (A.10) becomes

    +++ r]VVrVS[ ASSS2

    1

    +++++ }VV)({S}V)({Sr SA1AA2VASS1VS

    +

    ++ VrVSVSrVS

    2

    1)(S ASSS

    22A3

    +++ VrVSVSrVS

    2

    1)( ASSS

    22t3Vt

    ++++ }VV)2({S2

    1VV 2

    SVVSSS1SVSS

    22

    At2St1

    0V)2(S2

    1SSS1V

    22 =+ (A.12)

    From (A.12) we get the following coefficients, which have to be zero:

    Coefficient of 2SV :

    0S2

    1VV

    22 = (A.13)

    Coefficient of AV :

    0)(SS t212t332 =++ (A.14)

    Coefficient of SSV :

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    0S2

    1)2(S

    2

    1S A3

    32S1t3

    221

    2 =++ (A.15)

    Coefficient of SV :

    +++ A32A1S1t31 SrS)(Srr

    0)2(S2

    1t1SS1SV

    22 =+ (A.16)

    Zero-th order coefficient

    ++++ t3AS VSrSSrr

    0S2

    1V)(r SS

    22t3V =++ (A.17)

    We have now to solve the system of PDEs (A.13)-(A.17).

    From (A.13) we get 0VV = and therefore is a linear function with respect to

    V:

    )t,A,S(V)t,A,S( += (A.18)

    From (A.15) we get

    A3t31S1 S2

    1

    2

    1

    S

    1 += (A.19)

    which is a linear differential equation with unknown function 1 .

    The solution of the previous differential equation is

    )t,(SS2

    1)SlnS(

    2

    1 A3

    2t31 ++= (A.20)

    where )t,( is a function to be determined.

    From (A.14), using the expression (A.20) for the function 1 , we derive the

    equation

    ++ )SlnS(2

    1S

    2

    3t3

    23

    0S)]t,([ t22t3 =++ (A.21)

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    Since the previous equation should hold for every S, each one of the coefficients

    has to be zero. Therefore we obtain the following four equations:

    0 3 = (A.22)

    0 t3 = (A.23)0)t,( 2t3 =+ (A.24)

    0 t2 = (A.25)

    From the equations (A.22) and (A.23) and taking into account (A.9),we get that 3

    is a constant:

    13 a = (A.26)

    From equation (A.25) there follows that 2 is independent of the time t and so

    )A(f2 = (A.27)

    Therefore equation (A.24) gives us

    )A(f)t,( = (A.28)

    The function 1 becomes, as follows from (A.20),

    )(fS1 = (A.29)

    From the above equation we get the following expressions to be used later on.

    )(f S1 = (A.30a)

    0 SS1 = (A.30b)

    )A(fS A1 = (A.30c)

    0 t1 = (A.30d)

    Equation (A.16), using the expressions (A.18)-(A.20), takes the form

    0S)A(fS)A(fSr)A(fSr S222

    =+Solving the previous equation with respect to S , we find

    )A(f S2 = (A.31)

    and therefore

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    )t,A(S)A(f2 += (A.32)

    where )t,A( is a function to be determined.

    We also find from (A.31) that

    0S SS2 = (A.33)

    an expression we shall need later on.

    From (A.32) we also get

    )t,A( tt2 = (A.34)

    and

    )t,A(S)A(f AA2 += (A.35)

    From (A.17), using (A.18) we obtain the equation

    ++++++ )V(S)V(Sr)V(r ASS

    0)V(S2

    1V)(r)V( SSSS

    22t3tt =+++++ (A.36)

    Equating the coefficients of V to zero, we get from the previous equation the

    following two equations:

    +++ AS SSrr

    0S2

    1)(r SS

    22t3t =+++ (A.37)

    and

    0S2

    1SSrr SS

    22tS =++++ (A.38)

    Equation (A.38) expresses the fact that the function introduced in (A.14) is a

    solution of the original PDE.Equation (A.37) can be expressed as

    +++ )}t,A(S)A(f{

    1S)A(f

    1Sr A22

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    0)t,A(

    1t2

    =+ (A.39)

    The previous equation can be written in equivalent form

    0S)A(fS)}A(fr)t,A({)t,A(2

    At =+++ (A.40)

    Since the previous equation should hold for any value of S, we get the following

    equations:

    0)A(f = (A.41)

    0)A(fr)t,A(A =+ (A.42)

    0)t,A( t = (A.43)

    From (A.41) we conclude that )A(f is a second degreepolynomial with respect to A:

    2

    432 AaAaa)A(f ++= (A.44)

    From (A.43), we obtain that )t,A( does not depend on t. Therefore

    )A(g)t,A( = (A.45)

    and so equation (A.42) becomes, because of (A.45) and (A.44)

    0a2r)A(g4=+

    from which we determine the function )A(g :

    54 aAar2)A(g += (A.46)

    Therefore

    54 aAar2)t,A( += (A.47)

    Le us collect now everything together.

    We find from (A.29) and (A.44) that

    )Aa2a(S 431 += (A.48)

    From (A.27) and (A.44) we find that

    2

    4322 AaAaa ++= (A.49)

    We also have from (A.26)

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    Using the transformation (4.5), we can express the various partial derivatives of

    the function )t,A,S(V in terms of the partial derivatives of the function )t,x(u .

    We find that

    =

    ASbexpAuV ntt

    +=

    A

    Sbexp)AubAu(V 1n2nxS

    ++=

    A

    Sbexp)AubAub2Au(V 2n23nx

    4nxxSS

    +=

    A

    Sbexp)ASubAunASu2(V 2n1n3nxA

    Substituting the above expressions into the original equation (3.1), we obtain

    ++++ )AubAub2Au(S2

    1uA 2n23nx

    4nxx

    22t

    n

    +++ )AubAu(Sr 1n2nx

    ++ )ASubAunASu2(S 2n1n3nx

    0Aur n =

    The previous equation can be put into the form

    ++ xx4n22

    tn u)AS(

    2

    1uA

    +

    ++ x

    3n22n3n22 u)AS(2)AS(r)AS(b22

    1

    +++

    )AS(n)AS(br)AS(b2

    1 1n1n2n222

    ] 0uAr)AS(b n2n2 = (B.1)We now have to simplify the expressions appearing within the brackets of the

    previous equation. We have

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    C1. Lie Symmetry Analysis of the equationAfter performing a Lie symmetry analysis, we have found that the above equation

    has the six symmetry generators (six vector fields)

    tX1

    = (C.1)

    uutc

    a4

    bx

    a4

    b

    tt

    xx

    2

    1X

    2

    2

    22

    +

    +

    = (C.2)

    +

    +

    = 2xa8

    1t2x

    a4

    b

    tt

    xtxX 2

    22

    23

    uut

    2

    1tc

    a4

    b 22

    2

    (C.3)

    xX4

    = (C.4)

    uut

    a2

    bx

    a2

    1

    xtX

    225

    +

    = (C.5)

    uuX6

    = (C.6)

    and the infinite dimensional sub-algebra

    u)t,x(X

    = (C.7)

    where )t,x( is an arbitrary solution of the original equation (ref. [37])

    C.2. Transformation of the equation to the heat equation

    We shall consider a linear combination of generators such as to convert the BS

    equation to the heat equation. For this reason, we consider

    uu

    x

    1

    t

    1X

    +

    +

    = (C.8)

    where and are constants to be determined.

    In order to determine the invariants corresponding to the symmetry (C.8), we

    consider the system

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    u

    du

    1

    dx

    1

    dt == (C.9)

    From the equation1

    dx

    1

    dt = we get by integration xCt 1 =+

    or 1Ctx += and hence one invariant of the equation is

    txy = (C.10)

    From the equationu

    du

    1

    dt = we get by integration )uCln(t 2=

    or uCe 2t = and hence another invariant is

    teu= (C.11)

    Therefore

    teu = (C.12)

    Using (C.12) and (C.10) we find that

    tytt e)(u +=

    tyx eu =

    tyyxx eu =

    Therefore the equation ucubuau xxx2

    t ++= transforms to the equation

    (divided by the factort

    e )

    cba yyy2

    yt ++=+

    from which we get

    )c()b(a yyy2t +++= (C.13)

    We determine now and such as to become zero the coefficients

    of y and :

    0b =+

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    0c =

    Therefore we should have b = and c= , and hence the two

    invariants will be

    tbxy += and ue tc = Therefore we arrive at the following

    Lemma

    The substitution

    )btyx,t(ue tc ==

    converts the equation ucubuau xxx2

    t ++= to the heat equation

    yy2

    t a =

    Appendix D. Webers Differential Equation

    Abramowitz and Stegun ([41], 19.17) define as standard solutions of Webers

    equation

    yx4

    1ay 2

    =

    the functions )x,a(W where

    )yG2yG(2

    )a(cosh)x,a(W 2311

    4/1 =with

    += ai

    2

    1

    4

    1G1

    += ai

    2

    1

    4

    3G3

    and 1y , 2y are defined by

    +

    +

    ++=

    !6

    xa

    2

    7a

    !4

    x

    2

    1a

    !2

    xa1y

    63

    42

    2

    1

    +

    ++

    ++

    !8

    xa

    4

    211a25a

    !8

    x

    4

    15a11a

    835

    824

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    and

    +

    +

    ++=

    !7

    xa

    2

    13a

    !5

    x

    2

    3a

    !3

    xaxy

    73

    52

    3

    2

    +

    ++

    ++

    !11

    xa

    4

    531a35a

    !9

    x

    4

    63a17a

    1135924

    respectively.

    In the previous expressions, the non-zero coefficients na of!n

    xn

    are connected by

    2nn2n a)1n(n4

    1

    aaa + =

    It is also worth noting that )x,a(W can be expressed in terms of the Confluent

    Hypergeometric functions ([41], 19.25)

    = 2

    3

    14/3 x4

    1,a

    2

    1,

    4

    3H

    G

    G2)x,a(W

    21

    3 x

    4

    1,a

    2

    1,

    4

    1Hx

    G

    G2

    where

    =++= )xi2;2m2;ni1m(Fe)x,n,m(H 11xi

    )xi2;2m2;ni1m(Me xi ++=

    Note. Webers equation can be obtained by separation of variables for the Laplace

    equation in parabolic cylindrical coordinates (ref [42], Chapter 10).

    Appendix E. The Airy equation

    The differential equation ofAiry

    0wzw =

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    has as solutions the linearly independent solutions

    )z(Ai and )z(Bi

    (Abramowitz and Stegun [41], 10.4).

    These functions are defined by

    )z(gc)z(fc)z(Ai 21 =

    )]z(gc)z(fc[3)z(Bi 21 +=

    where

    !)k3(

    z

    3

    13z

    !9

    741z

    !6

    41z

    !3

    11)z(f

    k3

    k0k

    k963

    =

    =+

    +

    ++=

    and

    !)1k3(

    z

    3

    23z

    !10

    852z

    !7

    52z

    !4

    2z)z(g

    1k3

    k0k

    k1074

    +

    =+

    +

    ++=

    +

    =

    respectively.

    The constants 1c and 2c are given by

    )3/2(3

    1

    3

    )0(Bi)0(Aic

    3/21===

    and

    )3/1(3

    1

    3

    )0(iB)0(iAc

    3/12=

    ==

    They also can be expressed in terms ofBessels functions of fractional order:

    )(K3

    z

    1)z(Ai 3/1= ([41], 10.4.14)

    )}(I)(I{3z)z(Bi 3/13/1 += ([41], 10.4.18)

    where zz3

    2 =

    References.

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