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The Allen-Cahn equation with a time Caputo-Hadamard derivative: Mathematical and Numerical Analysis

  • In this paper, we investigate the local discontinuous Galerkin (LDG) finite element method for the fractional Allen-Cahn equation with Caputo-Hadamard derivative in the time domain. First, the regularity of the solution is analyzed, and the results indicate that the solution of this equation generally possesses initial weak regularity in the time dimension. Due to this property, a logarithmic nonuniform L1 scheme is adopted to approximate the Caputo-Hadamard derivative, while the LDG method is used for spatial discretization. The stability and convergence of this fully discrete scheme are proven using a discrete fractional Gronwall inequality. Numerical examples demonstrate the effectiveness of this method.

    Citation: Zhen Wang, Luhan Sun. The Allen-Cahn equation with a time Caputo-Hadamard derivative: Mathematical and Numerical Analysis[J]. Communications in Analysis and Mechanics, 2023, 15(4): 611-637. doi: 10.3934/cam.2023031

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  • In this paper, we investigate the local discontinuous Galerkin (LDG) finite element method for the fractional Allen-Cahn equation with Caputo-Hadamard derivative in the time domain. First, the regularity of the solution is analyzed, and the results indicate that the solution of this equation generally possesses initial weak regularity in the time dimension. Due to this property, a logarithmic nonuniform L1 scheme is adopted to approximate the Caputo-Hadamard derivative, while the LDG method is used for spatial discretization. The stability and convergence of this fully discrete scheme are proven using a discrete fractional Gronwall inequality. Numerical examples demonstrate the effectiveness of this method.



    Fractional calculus has been increasingly gaining attention from researchers due to its widespread applications in fields such as physics, chemistry and biology [1,2,3,4,5]. The most commonly used approaches entail the use of the Riemann-Liouville integral/derivative, Caputo derivative, Riesz derivative and fractional Laplacian. However, there is another type of fractional calculus that was discovered in 1892 but largely overlooked, and it is Hadamard calculus [6]. It was only in recent years that people realized its ability to provide more accurate descriptions of complex processes, such as Lomnitz's logarithmic creep law for special materials [7] and ultra-low diffusion processes [8]. As a result, it has gradually come into the spotlight [9,10].

    The Allen-Cahn equation (AC equation) was originally proposed by Allen and Cahn in 1979 while studying the motion of phase boundaries in crystalline solids as a model for phase separation processes in binary alloys at a given temperature [11,12]. Over the years, it has become one of the most widely used phase field models for describing physical phenomena in materials science and fluid mechanics [13]. Early studies of the AC model primarily focused on the following integer-order partial differential equation:

    utε2Δu=F(u)=:f(u), (1.1)

    where ε>0 represents the interface width parameter and F(u)=14(1u2)2 denotes a double-well potential [14,15,16]. The particle motion in model (1.1) follows Brownian motion, meaning that the mean square displacement (MSD) satisfies (x(t))2t), and the forces are spatially local, i.e., long-range interactions between particles are not considered. However, due to the heterogeneity of the medium, non-local interaction forces unavoidably exist in phase field models, which cannot be described in integer-order models. Therefore, an increasing number of researchers have started to focus on studying fractional AC equations:

    CDα0,tuε2Δu=f(u),0<α<1, (1.2)

    where CDα0,t is the Caputo fractional derivative defined by

    CDα0,tu(x,t)=1Γ(1α)t0(ts)αu(x,s)sds.

    The fractional AC equation (1.2) describes subdiffusion phenomena in nature, characterized by the power-law growth of the MSD with time (i.e., (x(t))2tα).

    However, an equally important and significant fact is that there are also many ultra-low diffusion behaviors in nature. This is because diffusing particles have a heavy-tailed waiting time distribution, which is slower than any power-law decay. Their MSDs exhibit logarithmic growth over time, i.e., (x(t))2(logt)α. Describing these phenomena using Hadamard calculus would be more accurate. Therefore, we consider the following form of the Caputo-Hadamard-type time-fractional AC equation:

    {CHDαa,tu(x,t)ε2Δu(x,t)=f(u(x,t)),(x,t)Ω×(a,T],u(x,a)=ua(x),xΩ,u(x,t)=0,(x,t)Ω×[a,T], (1.3)

    where CHDαa,t(0<α<1) represents the Caputo-Hadamard fractional derivative defined in (2.6), and the domain ΩRd(d1) is a bounded and convex polygon.

    Although there have been many studies on the AC equation with a time Caputo derivative (see (1.2)), there seems to be no report on the time derivative in the Caputo-Hadamard sense. This paper will focus on the following two goals for this type of situation:

    ● Provide some theoretical results on the solution of problem (1.3), including the existence, uniqueness and regularity of the solution in certain spaces.

    ● Consider the numerical solution of problem (1.3), use the local discontinuous Galerkin (LDG) method for spatial approximation and discretize the time direction using a nonuniform difference formula to obtain the corresponding fully discrete scheme. The stability and convergence of this scheme are demonstrated through numerical examples.

    The organization of this article is as follows. In Section 2, we provide some symbols and definitions. By utilizing the modified Laplace transform and its inverse form, the mild solution of (1.3) is derived. Section 3 mainly focuses on some theoretical analysis of (1.3). In Section 4, we present a nonuniform L1/LDG scheme for (1.3) with generalized alternating numerical fluxes. The stability analysis and error estimation of this scheme are investigated. Numerical examples are presented in Section 5. A brief summary is provided in the final section.

    In this section, we review some common symbols and definitions and provide a representation for the solution of (1.3).

    For any measurable subset ω of Ω, let (,)ω be the L2 inner product on ω and ω denote the L2(ω) norm defined by v2ω=(v,v)ω. Here, we omit the subscript when ω=Ω. For each nonnegative integer r, Hr(ω) denotes the usual Sobolev space with its associated norm r.

    Suppose S is a real Banach space with norm S. C([a,T];S) represents the space consisting of all continuous functions v:[a,T]S, whose norm is defined as

    vC([a,T];S):=maxatTv(t)S. (2.1)

    To simplify the notation, in this paper we assume that ε=1 in (1.3). Set X=L2(Ω), D=H10(Ω)H2(Ω) and A=Δ, with a homogeneous Dirichlet boundary condition. Then the operator A satisfies the following resolvent estimate [17]:

    (zαIA)1XXC|z|α,zΣθ,θ(0,π), (2.2)

    where XX is the operator norm on the space X, I is the identity operator and Σθ:={zC{0}:|arg(z)|θ}. One can thus get from (2.2) that

    A(zαIA)1XXC,zΣθ,θ(0,π). (2.3)

    Definition 2.1 ([18]). The Hadamard fractional integral of a given function f(t) with order α>0 is defined as

    HDαa,xf(x)=1Γ(α)xa(logxlogt)α1f(t)dtt,x>a>0, (2.4)

    where Γ() is the usual Gamma function.

    Definition 2.2 ([18]). The Hadamard fractional derivative of a given function f(t) with order α(n1<α<nZ+) is defined as

    HDαa,xf(x)=δn[HD(nα)a,xf(x)]=1Γ(nα)δnxa(logxlogt)nα1f(t)dtt,x>a>0, (2.5)

    where δng(x)=(xd/dx)ng(x)=δ(δn1g(x)).

    Definition 2.3 ([8,19]). The Caputo-Hadamard fractional derivative of a given function f(t) with order α(n1<α<nZ+) is defined as

    CHDαa,xf(x)=HD(nα)a,x[δnf(x)]=1Γ(nα)xa(logxlogt)nα1δnf(t)dtt,x>a>0. (2.6)

    For more information on Definitions 2.1–2.3, one may refer to [20,21,22,23].

    Definition 2.4 ([21]). The modified Laplace transform of a given function f(t) with t[a,+)(a>0) is defined by

    ˜f(s)=Lm{f(t);s}=aes(logtloga)f(t)dtt,sC. (2.7)

    The inverse modified Laplace transform is given by

    f(t)=L1m{˜f(s);t}=12πic+icies(logtloga)˜f(s)ds,c>0,i2=1. (2.8)

    Definition 2.5 ([21]). For the given functions f(t) and g(t) defined on [a,+)(a>0), the convolution is defined by

    f(t)g(t)=(fg)(t)=taf(atw)g(w)dww.

    From the definition of operator δ, it is easy to see that

    δ(fg)(t)=f(a)g(t)+taf(ats)g(s)atsdss. (2.9)

    Let w=uua. Then, one can get from (1.3) that w satisfies the following equations:

    CHDαa,tw(x,t)Aw(x,t)=Aua+f(u(x,t)),withw(x,a)=0. (2.10)

    By virtue of the modified Laplace transform, one has

    zα˜w(z)A˜w(z)=z1Aua+˜f(u), (2.11)

    which further yields

    ˜w(z)=(zαA)1(z1Aua+˜f(u)). (2.12)

    According to the inverse modified Laplace transform and the convolution rule, one gets

    w(t)=F(t)Aua+taE(ats)f(u(s))dss, (2.13)

    where the operators E(t),F(t):XX are defined as

    E(t)=12πiΓθ,ϑez(logtloga)(zαA)1dz,F(t)=12πiΓθ,ϑez(logtloga)(zαA)1dzz. (2.14)

    For fixed ϑ>0 and θ(π2,π), Γθ,ϑ is given by

    Γθ,ϑ={sC:|s|=ϑ,|args|θ}{sC:s=ρe±iθ,ρϑ}, (2.15)

    in which Im s increases.

    As a consequence, the mild solution of (1.3) can be derived, that is,

    u(t)=ua+F(t)Aua+taE(ats)f(u(s))dss. (2.16)

    Here and hereafter u(t)=u(x,t) with xΩ.

    Now we study the properties of the operators F(t) and E(t).

    Lemma 2.1. The operators E(t) and F(t) defined in (2.14) satisfy the following properties:

    (ⅰ) For t[a,T], F(t):XD is continuous and AF(a)=0.

    (ⅱ) For t(a,T], it holds that

    (logtloga)αF(t)XX+(logtloga)1αδF(t)XX+AF(t)XXC.

    (ⅲ) For t(a,T], it holds that

    (logtloga)1αE(t)XX+(logtloga)2αδE(t)XX+(logtloga)AE(t)XXC.

    (ⅳ) For t(a,T], E(t):XD is continuous.

    Proof. (ⅰ) For t[a,T], Sakamoto and Yamamoto have shown in [24, Theorem 2.1] that AF(t)=F(t)A:XX is continuous. Thus, F(t):XD is continuous with respect to t[a,T]. Letting f(u)=0 in (2.16), and taking the limit as ta, one can deduce AF(a)=0.

    (ⅱ) Notice that A(zαA)1=I+zα(zαA)1, and choose ϑ=(logtloga)1 in the contour Γθ,ϑ; then, for any nonnegative integers k, one has

    AmδkF(t)XX=12πiΓθ,ϑez(logtloga)zk1Am(zαA)1dzXXCΓθ,ϑe(z)(logtloga)|z|k1+(m1)α|dz|C(logtloga)(m1)αk,m=0,1. (2.17)

    So we get (ⅱ).

    (ⅲ) Because E(t)=δF(t), (ⅲ) follows from (2.17).

    (ⅳ) Using the equivalent norm vDvX+AvX,vD, the conclusion in (iv) can be obtained.

    In order to provide a theoretical basis for the numerical analysis that follows, we will consider the existence, uniqueness and regularity of solutions to (1.3) in the present section.

    Theorem 3.1. Suppose f:RR is a Lipschitz continuous function, i.e.,

    |f(x)f(y)|L|xy|,x,yR. (3.1)

    Assume that uaH10(Ω)H2(Ω). Then, (1.3) has a unique solution u that satisfies

    uC([a,T];H10(Ω)H2(Ω)),CHDαa,tuC([a,T];L2(Ω)),δu(t)C(logtloga)α1,t(a,T], (3.2)

    where C is a positive constant.

    Proof. First, we prove the existence of a unique solution to (1.3). For any fixed λ>0, we denote by C([a,T];X)λ the weighted norm space of function vC([a,T];X), equipped with the norm

    ||v||X,λ:=maxt[a,T]eλ(logtloga)v(t)X. (3.3)

    Let M:C([a,T];X)λC([a,T];X)λ be a nonlinear map defined as

    Mv(t)=ua+F(t)Aua+taE(ats)f(v(s))dss. (3.4)

    Then, for any v1(t),v2(t)C([a,T];X)λ, by virtue of Lemma 2.1 and the Lipschitz continuity of f, we have

    Mv1(t)Mv2(t)X,λCeλ(logtloga)ta(logtlogτ)α1v1(τ)v2(τ)XdττCta(logtlogτ)α1eλ(logtlogτ)maxτ[a,T]eλ(logτloga)(v1(τ)v2(τ))X,λdττC(logTlogaλ)α/2v1(t)v2(t)X,λ. (3.5)

    Thus, by choosing a sufficiently large λ, the following inequality holds:

    Mv1(t)Mv2(t)X,λ12v1(t)v2(t)X,λ,

    which means that M is a contractive mapping on the space C([a,T];X)λ. Then, based on the contraction mapping principle and the equivalence of spaces C([a,T];X)λ and C([a,T];X), we obtain that (2.16) has a unique fixed point uC([a,T];X).

    We now prove that there exists a positive constant C such that

    u(t)u(s)C|logtlogs|α,s,t[a,T]. (3.6)

    When s=t, (3.6) obviously holds. We focus on proving the case of as<tT. The same can be obtained for the other case. According to (2.16), one has

    u(t)u(s)(logtlogs)α=F(t)F(s)(logtlogs)αAua+saE(w)f(u(atw))f(u(asw))(logtlogs)αdww+1(logtlogs)αtsE(w)f(u(atw))dww. (3.7)

    For the first term, we apply Lemma 2.1–(ⅱ) and the Minkowski inequality to get

    F(t)F(s)(logtlogs)α1(logtlogs)αtsδF(w)dwwC(logtloga)α(logsloga)α(logtlogs)αC. (3.8)

    For the second term, we can obtain from Lemma 2.1–(ⅱ) that

    1(logtlogs)αtsE(w)f(u(atw))dwwC(logtlogs)αts(logwloga)α1dwwC. (3.9)

    Similarly, the third term can be bounded as

    eλ(logtloga)saE(w)f(u(atw))f(u(asw))(logtlogs)αdwwsaeλ(logslogw)(logslogw)α1eλ(logwtsloga)u(wts)u(w)(log(wts)logw)αdww. (3.10)

    Denoting

    W=maxas<tT{eλ(logtloga)u(t)u(s)(logtlogs)α}

    and substituting (3.8)–(3.10) into (3.7) yield

    WC+saeλ(logslogw)(logslogw)α1WdwwC+C(logTlogaλ)α/2W.

    Hence, by choosing a sufficiently large λ, we can achieve the desired result.

    Applying the operator A to both sides of (2.16), and noting that

    AF(t)=taAE(ats)dss,

    we get

    Au(t)Aua=AF(t)Aua+taAE(ats)f(u(s))dss=AF(t)(Aua+f(u(t)))+taAE(ats)(f(u(s))f(u(t)))dss:=Φ1(t)+Φ2(t). (3.11)

    By directly applying Lemma 2.1–(ⅰ), we can obtain Φ1(t)C([a,T];X) and

    Φ1(t)CAua+f(u(t))C. (3.12)

    In view of Lemma 2.1–(ⅲ), one has

    Φ2(t)=taAE(ats)(f(u(s))f(u(t)))dssCtau(t)u(s)logtlogsdssC(logtloga)α,t(a,T], (3.13)

    which implies that Φ2(t) is continuous at t=a. Meanwhile, by using Lemma 2.1–(ⅳ), we know that Φ2(t) is continuous for t(a,T]. Therefore, Φ2(t)C([a,T];X). Combining the previous three estimates, we can see that

    uC([a,T];H10(Ω)H2(Ω))C.

    This, together with (1.3), also show that CHDαa,tuC([a,T];L2(Ω)).

    Finally, the term δu(t) has not been estimated yet. By differentiating (2.16) with respect to variable t, we obtain

    δu(t)=E(t)(Aua+f(ua))+taE(ats)f(u(s))u(s)ds. (3.14)

    Multiplying both sides of this equation by eλ(logtloga)(logtloga)1α, and by using Lemma 2.1, one gets

    eλ(logtloga)(logtloga)1αδu(t)=eλ(logtloga)(logtloga)1αE(t)(Aua+f(ua))+eλ(logtloga)(logtloga)1αta(logtloga)1α(logsloga)α1×E(ats)f(u(s))us(logsloga)1αdsCeλ(logtloga)Aua+f(ua)+C(T/λ)α/2maxs[a,T]eλ(logsloga)(logsloga)1αδu(s).

    By taking maximum of the left-hand side over t[a,T] and choosing a sufficiently large λ, we obtain

    maxt[a,T]{eλ(logtloga)(logtloga)1αδu(t)}C.

    All of this completes the proof.

    Lemma 3.1. Let Dv(t)=(logtloga)δv(t). Then, the following relation holds:

    D(vw)=vw+(Dv)w+v(Dw).

    Proof. Recalling Definition 2.4, the following relation holds:

    D(vw)(t)=(logtloga)v(a)w(t)+ta(Dv)(ats)w(s)dss+ta(logsloga)v(ats)w(s)atsdss=vw+(Dv)w+v(Dw).

    Lemma 3.2 (Gronwall inequality [25]). Suppose that f(t) and g(t) are nonnegative integrable functions on [a,b]. If there exists a nonnegative constant C1 such that

    f(t)g(t)+C1taf(s)(logtlogs)α1dss,t(a,b),α(0,1),

    then

    f(t)g(t)+C1tan=1(C1Γ(α))nΓ(nα)(logtlogs)nα1g(s)dss,t(a,b).

    In particular, if g(t) is non-decreasing, then

    f(t)g(t)Eα,1(C1Γ(α)(logtloga)α),t(a,b).

    Based on the above lemmas, we next show that the solution u(x,t) of (1.3) satisfies higher regularity.

    Theorem 3.2. Assume that f satisfies the condition in Theorem 3.1 and uaH10(Ω)H4(Ω). Then, for t(a,T], it holds that

    δlu(t)2C(logtloga)αlforl=1,2, (3.15)

    and

    CHDαa,tu2+Au(t)2C, (3.16)

    where C is a positive constant.

    Proof. Step 1. By applying the operator D on both sides of (2.16) and utilizing Lemma 3.1, one gets

    (logtloga)δu(t)=(logtloga)δF(t)Aua+taE(ats)(u(s)u3(s))dss+ta(logtlogs)δE(ats)(u(s)u3(s))dss+taE(ats)(logsloga)(δu(s)δ(u3(s)))dss. (3.17)

    Applying the Laplace operator A to both sides of (3.17) further implies the following

    (logtloga)A(Au(t))=(logtloga)δF(t)A2ua+taE(ats)(Au(s)A(u3(s)))dss+ta(logtlogs)δE(ats)(Au(s)A(u3(s)))dss+taE(ats)(logsloga)(A(δu(s))3A(u2(s)δu(s)))dss. (3.18)

    Recalling the Sobolev embedding formula uL(Ω)+uL4(Ω)Cu2, and by using the fact that uC([a,T];H10(Ω)H2(Ω)) from (3.2), one has

    AuAu3=Au6u|u|23u2AuC. (3.19)

    Likewise,

    A(u2(s)δu(s))C(u2Auδu(s)2+u22δu(s)22+u22δu(s)2+u22A(δu(s)))CA(δu(s)). (3.20)

    Combining (3.18)–(3.20) and Lemma 2.1, one gets

    (logtloga)A(δu(t))C(logtloga)αua4+ta(logtlogs)α1Au(s)Au3(s)dss+ta(logtlogs)α1Au(s)Au3(s)dss+ta(logsloga)(logtlogs)α1A(δu(s))3A(u2(s)δu(s))dssC(logtloga)α+Cta(logtlogs)α1(logsloga)×A(δu(s))dss. (3.21)

    By virtue of Lemma 3.2, we obtain

    A(δu(t))C(logtloga)α1, (3.22)

    which confirms the case of l=1 in (3.15).

    Step 2. In view of the definition of the Caputo-Hadamard fractional derivative in (2.6), we obtain

    A(CHDαa,tu)Cta(logtlogs)α(logsloga)α1dssC, (3.23)

    where the second inequality is derived by (3.22). As a result, we get from (1.3) and (3.19) that

    A2u=A(CHDαa,tu)A(uu3)A(CHDαa,tu)+A(uu3)C. (3.24)

    By virtue of (1.3), we know that CHDαa,tu|Ω=Au|Ω=0 for t[a,T]. Noting that Ω is a bounded convex polygonal domain, we can therefore prove that (3.16) holds according to (3.23) and (3.24).

    Step 3. Now, we demonstrate the case l=2 in (3.15). Apply operator δ on both sides of (3.17) to obtain that

    (logtloga)δ2u(t)+δu(t)=δF(t)Aua+(logtloga)δ2F(t)Aua+E(t)(uau3a)+taE(ats)(δu(s)3u2(s)δu(s))dss+(logtloga)δ(E(t)(uau3a))+ta(logtlogs)δE(ats)(δu(s)3u2(s)δu(s))dss+taE(ats){(δu(s)3u2(s)δu(s))+(logsloga)(δ2u(s)3(2u(s)(δu(s))2+u2(s)δ2u(s)))}dss. (3.25)

    Then, applying the Laplace operator A on both sides of (3.25) further leads to

    (logtloga)A(δ2u(t))+A(δu(t))=δF(t)A(Aua)+(logtloga)δ2F(t)A(Aua)+E(t)A(uau3a)+taE(ats)A(δu(s)3u2(s)δu(s))dss+(logtloga)δ(E(t)A(uau3a))+ta(logtlogs)δE(ats)A(δu(s)3u2(s)δu(s))dss+taE(ats){A(δu(s)3u2(s)δu(s))+(logsloga)A(δ2u(s)3(2u(s)(δu(s))2+u2(s)δ2u(s)))}dss. (3.26)

    From (3.20) and (3.22), one can deduce that

    A(δu(s)3u2(s)δu(s))Aδu(s)+3A(u2(s)δu(s))C(logsloga)α1. (3.27)

    Again use the embedding theorem uL(Ω)+uL4(Ω)Cu2 to show that

    A[u(s)(δu(s))2]CδuL(Ω)A(δu)uL(Ω)+(δu)2L4(Ω)uL(Ω)+δuL(Ω)(δu)L4(Ω)uL4(Ω)+δu2L(Ω)AuC(logsloga)2α2. (3.28)

    Similar to the proof of (3.20), one can get that

    A(u2(s)δ2u(s))CAδ2u(s). (3.29)

    Therefore, by the assumption uaH4(Ω), (3.26)–(3.29) and Lemma 2.1, one can derive that

    (logtloga)A(δ2u(t))A(δu(t))+δF(t)A(Aua)+(logtloga)δ2F(t)A(Aua)+E(t)A(uau3a)+taE(ats)A(δu(s)3u2(s)δu(s))dss+(logtloga)δ(E(t)A(uau3a))+ta(logtlogs)δE(ats)A(δu(s)3u2(s)δu(s))dss+taE(ats){A(δu(s)3u2(s)δu(s))+(logsloga)A(δ2u(s)3(2u(s)(δu(s))2+u2(s)δ2u(s)))}dssC(logtloga)α1+Cta(logtlogs)α1(logsloga)×A(δ2u(s))dss. (3.30)

    This, together with Lemma 3.2, leads to the desired result.

    As shown in Theorems 3.1 and 3.2, the solution u(x,t) of problem (1.3) may behave as weakly regular at the starting time t=a. Thus, we utilize the L1 scheme on nonuniform meshes (see [21] for more information about this scheme) to discretize the time Caputo-Hadamard derivative and by using the LDG method in space. Without loss of generality, suppose that the bounded domain Ω=(1,1)d in (1.3) and f(u) satisfies

    max|f(u)|C, (4.1)

    where C is a positive constant.

    In the next analysis, we will consider the cases d=1 and 2. The more general case d>2, which can also be obtained by changing the tensor product structure of the mesh, is omitted here.

    For r1, denote tn=a(T/a)(n/M)r, where n=0,1,,M, MN. We divide the interval [a,T] into a grading mesh in the logarithmic sense, that is, loga=logt0<logt1<<logtn1<logtn<<logtM=logT with

    logtn=loga+(logTloga)(n/M)r.

    Let τn=logtnlogtn1, n=1,,M be the time mesh sizes.

    The nonuniform L1 approximation in the logarithmic sense for the Caputo-Hadamard derivative [21] at t=tn is defined as

    CHDαa,tu(x,t)|t=tn=1Γ(2α)(bn,1u(x,tn)bn,nu(x,t0)n1i=1(bn,ibn,i+1)u(x,tni))+Υn:=Λαlogu(x,tn)+Υn,α(0,1),n=1,2,,M,

    where the discrete coefficients and the local truncation error are given, respectively, by

    bn,i=(logtntni)1α(logtntni+1)1αlogtni+1tni,i=1,2,,n (4.2)

    and

    Υn=1Γ(1α)n1i=0ti+1ti(logtnw)α(u(x,ti+1)u(x,ti)logti+1tiδu(x,w))dww. (4.3)

    Denote a(n)nk=bn,nk+1/Γ(2α), k=1,2,,n, and

    P(n)nk=1a(k)0{1,k=n,nj=k+1(a(j)jk1a(j)jk)P(n)nj,1kn1.

    Letting ωβ(t)=tβ1/Γ(β), we use (4.2) to obtain

    a(n)nk=ω2α(logtnlogtk1)ω2α(logtnlogtk)τk,k=1,2,,n.

    Similar to [26, Lemma 2.1–(ⅱ)], one can prove that

    nj=1P(n)njω1+mαα(logtnloga)ω1+mα(logtnloga),form=0,1. (4.4)

    In view of the integral mean-value theorem, one has

    a(n)nk+1<ω1α(logtnlogtk1)<a(n)nk. (4.5)

    For simplicity, we denote un=u(x,tn); then, the nonuniform L1 approximation scheme given in (4.2) can be rewritten as

    Λαlogun=ni=1a(n)ni(uiui1),n=1,2,,M. (4.6)

    Lemma 4.1. [21] Let the function u(x,t) satisfy that |δlu(,t)|C(1+(logtloga)αl) for l=0,1,2 and all t(a,T]. Then, it holds that

    |Υn|Cnmin{2α,rα},n=1,2,,M. (4.7)

    Lemma 4.2. Assume that u(,t)C2(a,T] and |δlu(,t)|C(1+(logtloga)αl) for l=0,1,2 and all t(a,T]. Then for n=1,2,,M, the following inequality holds:

    nj=1P(n)nj|Υn|C(α1(logTloga)αMrα+r21α4r1(logTloga)αMmin{2α,rα}).

    Proof. The proof of this lemma is analoguous to that of (3.12) in [26], so is omitted here.

    Lemma 4.3 (Discrete Gronwall inequality). Let (λl)M1l=0 be a nonnegative sequence and there exist a constant λ independent of time steps such that M1l=0λlλ. Assume that the sequences {ϕn}Mn=1 and {ψn}Mn=1 are nonnegative, and that the grid function {vn}Mn=1 satisfies

    Λαlog(vn)2nl=1λnl(vl)2+ϕnvn+(ψn)2,n=1,2,,M. (4.8)

    If the maximum time-step τM(2Γ(2α)λ)1/α, the following holds:

    vn2Eα,1(778λ(logtnloga)α)(v0+max1knkj=1P(k)kjϕj+Γ(1α)max1kn{(logtkloga)α/2ψk}),n=1,2,,M, (4.9)

    where Eα,1(z) is the well-known Mittag-Leffler function.

    Proof. Denote

    Enα=2Eα,1(778λ(logtnloga)α).

    If vnΨ:=Γ(1α)max1kn{(logtkloga)α/2ψk}, then (4.9) is directly obtained from Enα2. For the alternative case vn>Ψ, we have vn>Γ(1α){(logtnloga)α/2ψk}, and the inequality (4.8) can be rewritten as

    Λαlog(vn)2nl=1λnl(vl)2+ϕnvn+vnψnΓ(1α)(logtnloga)α. (4.10)

    Using [27, Lemma 3.6] with

    ξn+1=ϕn+ψnΓ(1α)(logtnloga)α,ηn=0,

    we get from (4.4) that

    vnv0+max1knkj=1P(k)kjϕj+max1knkj=1P(k)kjψjΓ(1α)(logtjloga)αEnα[v0+max1knkj=1P(k)kjϕj+Γ(1α)max1kn((logtkloga)α/2ψk)×max1knkj=1P(k)kjω1α(logtjloga)]. (4.11)

    The proof is completed.

    Remark 4.1. The conclusion in Lemma 4.3 provides the theoretical support for the numerical approach to the Caputo-Hadamard fractional differential equation. The results are almost identical to the usual nonuniform L1 formula (for Caputo fractional derivative, see [28, Theorem 2.3] for details).

    Let us denote by Ωh={K} a shape-regular subdivision of Ω, and set Ωh={K:KΩh}. Suppose that the "left" and "right" elements KL and KR share a face e, and φ is a function defined on KL and KR, but may be discontinuous on e. Then, we use φL and φR to denote the traces of e from the left and right direction, respectively. The finite element space associated with the mesh Ωh is of the form

    Vh={vhL2(Ω):vh|KQk(K),KΩh},Vh={vh=(v1h,,vdh)(L2(Ω))d:vih|KQk(K),i=1,,d,KΩh},

    where Qk(K) is a tensor product space defined over K with maximal k-th polynomial. When d = 1, Qk(K)=Pk(K).

    Case A (d=1): For an arbitrary element K:=Ij=(xj12,xj+12) with j=1,2,,N, we denote xj=(xj12+xj+12)/2, hj=xj+12xj12 and h=max1jNhj. Obviously, x12=1 and xN+12=1. Let Ωh be a quasi-uniform mesh, that is, there exists a fixed positive constant ρ independent of h such that ρhhjh for j=1,2,,N as h0.

    Let Ph:L2(Ω)Vh represent the standard L2 projection, defined as

    Kj(Phuu)vhdx=0,vhPk(Kj),j=1,,N. (4.12)

    The Gauss-Radau projections P±h:H1(Ω)Vh are given by [29]

    Ij(P+huu)vhdx=0,vhPk1(Ij),(P+hu)+j12=u(x+j12),j=1,,N, (4.13)

    and

    Ij(Phuu)vhdx=0,vhPk1(Ij),(Phu)j+12=u(xj+12),j=1,,N. (4.14)

    Case B (d=2): For an arbitrary rectangular element K:=Kij=Ii×Jj=(xi12xi+12)×(yj12,yj+12), we denote hxi=xi+12xi12 and hyj=yj+12yj12. Analogous to the one-dimensional case, hij=max{hxi,hyj} and h=maxKijΩhhij are well defined. We also list the projections that will be used [30].

    The projection Πh:H1(Ω)Vh for scalar functions is defined as

    Πh=Ph,xPh,y,

    where Ph,x and Ph,y represent the one-dimensional projection Ph given in (4.14) on a two-dimensional rectangular element Kij.

    Let Ph,x and Ph,y be the standard L2 projections in the x and y directions, respectively.

    The projection Π+h=P+h,xPh,y:[H1(Ω)]2Vh for vector-valued functions is defined as

    IiJj(Π+hvv)wdxdy,wQk(Kij),Jj(Π+hv(xi1/2,y)v(xi1/2,y))nw(x+i1/2,y)dy=0,wQk(Kij),Ii(Π+hv(x,yj1/2)v(x,yj1/2))nw(x,y+j1/2)dx=0,wQk(Kij), (4.15)

    where n denotes the outward unit normal vector.

    As shown in [31, Lemma 2.4], the projections mentioned above satisfy the following approximation properties:

    QhvvChk+1vk+1,v[Hk+1(Ω)]d, (4.16)

    where Qh=P±h, Πh, or Π+h. Moreover, the projection Πh also has the following superconvergence property (see [31, Lemma 3.7]):

    |(vΠhv,uh)(v^Πhv,uhn)Ωh|Chk+1vk+2uh,vHk+2(Ω),uhVh. (4.17)

    The "hat" term here is the numerical flux, which will be given later.

    Rewrite (1.3) into the following equivalent first-order system:

    CHDα0,tupf(u)=0, (4.18a)
    pu=0. (4.18b)

    Then the weak form of (4.16) at tn can be formulated as follows:

    (CHDαa,tun,v)K+(pn,v)K(pnn,v)K(f(un),v)K=0, (4.19a)
    (pn,w)K+(un,w)K(un,wn)K=0, (4.19b)

    in which v and w are test functions. The fully discrete nonuniform L1/LDG scheme is defined as follows: find (unh,pnh)Vh×Vh such that

    (Λαlogunh,vh)K+(pnh,vh)K(^pnhn,vh)K(f(unh),vh)K=0, (4.20a)
    (pnh,wh)K+(unh,wh)K(^unh,whn)K=0 (4.20b)

    hold for any (vh,wh)Vh×Vh. The alternating numerical fluxes are chosen, namely,

    ^unh=unh,L,^pnh=pnh,R, (4.21)

    or

    ^unh=unh,R,^pnh=pnh,L. (4.22)

    It is now time to present the stability and error estimate for the scheme (4.20) in the L2-norm.

    Theorem 4.1. (Stability) Assume that unh and pnh (n=1,2,,M) are the LDG solutions of (4.20) with numerical flux (4.21). Then, it holds that

    unh2Eα,1(774(logtnloga)α)u0h.

    Proof. Taking (vh,wh)=(unh,pnh) in (4.20), and by summing over all K, one has

    (Λαlogunh,unh)+(pnh,unh)(^pnhn,unh)Ωh+((unh)3unh,unh)=0, (4.23a)
    (pnh,pnh)+(unh,pnh)(^unh,pnhn)Ωh=0. (4.23b)

    Adding them together and using integration by parts, one gets

    (Λαlogunh,unh)+pnh2+(unh)22=unh2,

    which means that

    (Λαlogunh,unh)unh2. (4.24)

    Notice that

    (Λαlogunh,unh)=a(n)0(unh,unh)n1k=1(a(n)nk1a(n)nk)(ukh,unh)2a(n)n1(u0h,unh)a(n)0unh212n1k=1(a(n)nk1a(n)nk)unh212a(n)n1unh212n1k=1(a(n)nk1a(n)nk)ukh212a(n)n1u0h2=12Λαlogunh2. (4.25)

    This, together with (4.24), yields

    Λαlogunh22unh2. (4.26)

    Therefore, utilizing Lemma 4.3 with vn=unh and ϕn=ψn=0, one has

    unh2Eα,1(774(logtnloga)α)u0h,

    provided that the maximum time step τM(4Γ(2α))1/α. The proof is completed.

    Theorem 4.2. (Error estimate) Let u(x,tn) be the exact solution of problem (1.3), which satisfies that |δlu(,t)|C(1+(logtloga)αl) for l=0,1,2 and all t(a,T]. unh and pnh (n=1,2,,M) are the LDG solutions of (4.20), with numerical flux given by (4.21). Suppose that f(u) satisfies the condition (4.1). Then, there exists a positive constant C independent of M and h such that

    ununhC(Mmin{2α,rα}+hk+1).

    Proof. Let us first denote

    enu=ununh=unPun+Pununh=unPun+Penu, (4.27a)
    enp=pnpnh=pnΠpn+Πpnpnh=pnΠpn+Πenp. (4.27b)

    Here, the projectors are selected as

    (P,Π)=(Ph,P+h)for Case A, (P,Π)=(Πh,Π+h)for Case B. (4.28)

    Subtracting (4.20) from (4.19) and summing over all K yield the following error equations:

    (CHDαa,tunΛαlogunh,vh)+(pnpnh,vh)((pn^Pnh)n,vh)Ωh(f(un)f(unh),vh)=0, (4.29a)
    (pnpnh,wh)+(ununh,wh)((un^unh),whn)Ωh=0. (4.29b)

    Taking (vh,wh)=(Penu,Πenp) in (4.29), and by noticing the error decomposition (4.27), we obtain

    (ΛαlogPenu,Penu)+(Πenp,Πenp)(f(un)f(unh),Penu)=(Λαlog(unPun),Penu)(Υn,Penu)(pnΠpn,Penu)+((pn^Πpn)n,Penu)Ωh(pnΠpn,Πenp)(unPun,Πenp)+((un^Pun),Πenpn)Ωh(Πenp,Penu)+(^Πenpn,Penu)Ωh(Penu,Πenp)+(^Penu,Πenpn)Ωh, (4.30)

    where Υn=CHDαa,tunΛαlogun. By virtue of (4.21) and the projection properties (4.12)–(4.15), we have

    (ΛαlogPenu,Penu)+(Πenp,Πenp)(f(un)f(unh),Penu)=(Λαlog(unPun),Penu)(Υn,Penu)(pnΠpn,Πenp)(unPun,Πenp)+((un^Pun),Πenpn)Ωh. (4.31)

    Then, from the Cauchy-Schwarz inequality and superconvergence property given by (4.17) that

    (ΛαlogPenu,Penu)+(Πenp,Πenp)(f(un)f(unh),Penu)Λαlog(unPun)Penu+ΥnPenu+pnΠpnΠenp+Chk+1ΠenpChk+1(Penu+Πenp)+ΥnPenu. (4.32)

    On the other hand, for the nonlinear term in (4.32), we can obtain

    (f(unh)f(un),Penu)=(f(Pun)f(un),Penu)(f(Pun)f(unh),Penu)=(f(ξ)(Punun),Penu)(f(Pun)f(unh),Penu), (4.33)

    where ξ=θun+(1θ)Pun,θ[0,1]. Employing the Cauchy-Schwarz inequality and interpolation property (4.16), we have

    |(f(ξ)(Punun),Penu)|fL(Ω)|(Punun,Penu)|CPenu2+Ch2k+2. (4.34)

    Notice that f(u)f(v)=f(u)(uv)(uv)3+3u(uv)2. Hence, we derive from (4.1) that

    |(f(Pun)f(unh),Penu)|=|(f(Pun)(Pununh)(Pununh)3+3Pun(Pununh)2,Penu)|=|(f(Pun)Penu(Penu)3+3Pun(Penu)2,Penu)|=|((Penu)3,Penu)(f(Pun)Penu+3Pun(Penu)2,Penu)|CPenu2+(Penu)22. (4.35)

    Substituting (4.34)–(4.35) into (4.33) and applying (4.32), we have

    (ΛαlogPenu,Penu)+Πenp2+(Penu)22Chk+1(Penu+Πenp)+ΥnPenu+Chk+1Πenp+CPenu2+(Penu)22+Ch2k+2CPenu2+Πenp2+(Penu)22+Ch2k+2+ΥnPenu. (4.36)

    This, combined with (4.25), further results in

    ΛαlogPenu22CPenu2+2Ch2k+2+2ΥnPenu. (4.37)

    As a consequence, according to Lemma 4.3 with vn=Penu, ϕn=2Υn, ψn=2Chk+1, λ0=2C and λj=0 for j=1,2,,M1, as long as τM(4CΓ(2α))1/α, we will obtain

    Penu2Eα,1(774C(logtnloga)α)[2max1knkj=1P(k)kjΥj+2CΓ(1α)max1kn((logtkloga)α/2hk+1)]. (4.38)

    Then, Lemma 4.2 leads to

    PenuC(Mmin{2α,rα}+hk+1).

    By combining the above estimate with the triangle inequality, the desired result can be obtained.

    The main purpose of this section is to give a numerical example to demonstrate the validity of the proposed scheme (4.20).

    Example 5.1.

    {CHDαa,tu(x,y,t)Δu(x,y,t)=u(x,y,t)u3(x,y,t)+g(x,y,t),(x,y)Ω,t(1,2],u(x,y,1)=0,(x,y)Ω,u(x,y,t)=0,(x,y)Ω,t[1,2], (5.1)

    where Ω=(1,1)×(1,1) and the source term g(x,y,t) is chosen such that the exact solution of the problem is u(x,y,t)=((logt)α+(logt)2)(x+1)2(x1)2(y+1)2(y1)2.

    We apply the nonuniform L1/LDG scheme (4.20) to solve problem (5.1). Table 1 gives the L2-errors and convergence orders versus M for different values of α(α=0.4,0.6,0.8) and grading parameter r(r=1,2α2α,2αα) when taking t=2 and M=Nx=Ny, from which it is obvious that the convergence order in time is min{2α,rα}. To investigate the spatial convergence order, we utilize (4.20) to solve (5.1) by using both linear and quadratic finite element approximations, respectively. The L2 errors and convergence order are listed in Table 2. The results show that the spatial convergence orders for the L2-norm are close to (k+1).

    Table 1.  L2 errors uMuMh and convergence rates in temporal dimension (Example 5.1).
    α=0.4 α=0.6 α=0.8
    M L2 error order L2 error order L2 error order
    20 2.0882e-02 1.4460e-02 9.8692e-03
    40 1.8728e-02 0.1570 1.0975e-02 0.3979 3.8145e-03 1.3714
    r=1 60 1.7169e-02 0.2144 9.1246e-03 0.4554 2.9052e-03 0.6717
    80 1.6027e-02 0.2392 7.9451e-03 0.4811 2.3930e-03 0.6741
    100 1.5145e-02 0.2537 7.1118e-03 0.4966 2.0627e-03 0.6656
    120 1.4434e-02 0.2637 6.4837e-03 0.5072 1.8200e-03 0.6866
    Predicted 0.4000 0.6000 0.8000
    α=0.4 α=0.6 α=0.8
    M L2 error order L2 error order L2 error order
    20 1.4291e-02 1.1880e-02 8.9725e-03
    40 6.4511e-03 1.1475 8.2447e-03 0.5270 6.4527e-03 0.4756
    r=2α2α 60 4.8619e-03 0.6975 6.5163e-03 0.5802 5.5439e-03 0.3744
    80 3.9526e-03 0.7198 5.4768e-03 0.6041 4.9066e-03 0.4245
    100 3.3562e-03 0.7330 4.7710e-03 0.6183 4.4352e-03 0.4527
    120 2.9316e-03 0.7419 4.2549e-03 0.6280 4.0701e-03 0.4712
    Predicted 0.8000 0.7000 0.6000
    α=0.4 α=0.6 α=0.8
    M L2 error order L2 error order L2 error order
    20 3.1821e-02 1.7151e-02 1.2386e-02
    40 1.0143e-02 1.6494 5.3431e-03 1.6825 4.0576e-03 1.6100
    r=2αα 60 4.9364e-03 1.7762 2.5870e-03 1.7889 2.0479e-03 1.6864
    80 2.9189e-03 1.8265 1.5325e-03 1.8199 1.2614e-03 1.6846
    100 1.9301e-03 1.8536 1.0189e-03 1.8294 8.7017e-04 1.6639
    120 1.3725e-03 1.8699 7.2993e-04 1.8291 6.4570e-04 1.6364
    Predicted 1.6000 1.4000 1.2000

     | Show Table
    DownLoad: CSV
    Table 2.  L2 errors uMuMh and convergence rates in spatial dimension (Example 5.1).
    α=0.4 α=0.6 α=0.8
    Nx×Ny L2 error order L2 error order L2 error order
    20×20 8.7815e-03 8.3408e-03 7.9187e-03
    40×40 2.8128e-03 1.6424 2.6596e-03 1.6490 2.5293e-03 1.6466
    Q1 60×60 1.3688e-03 1.7764 1.2864e-03 1.7914 1.2308e-03 1.7763
    80×80 8.1730e-04 1.7925 7.6164e-04 1.8218 7.3552e-04 1.7897
    100×100 5.5120e-04 1.7653 5.0799e-04 1.8151 4.9663e-04 1.7600
    Predicted 2.0000 2.0000 2.0000
    α=0.4 α=0.6 α=0.8
    Nx×Ny L2 error order L2 error order L2 error order
    10×10 3.8914e-02 3.7122e-02 3.3095e-02
    Q2 20×20 5.2323e-03 2.8948 5.0468e-03 2.8788 4.5058e-03 2.8768
    30×30 1.5620e-03 2.9815 1.5274e-03 2.9478 1.3618e-03 2.9510
    40×40 6.4505e-04 3.0742 6.4657e-04 2.9762 5.7490e-04 2.9978
    Predicted 3.0000 3.0000 3.0000

     | Show Table
    DownLoad: CSV

    Comparisons between the numerical solution and the exact solution are depicted in Figures 13, and it can be seen that the numerical solution is in good agreement with the exact solution. The numerical solution surfaces for different times t(t=1.2,1.4,1.6,1.8) and α(α=0.1,0.5,0.9) are shown in Figures 47. We can observe that the diffusion behavior of uh increases with time, and the maximum peak always appears in the center of the region. But if α is smaller, the diffusion process changes more slowly.

    Figure 1.  Comparison between numerical solution (left) and exact solution (right) with α=0.25 and T=2 (Example 5.1).
    Figure 2.  Comparison between numerical solution (left) and exact solution (right) with α=0.50 and T=2 (Example 5.1).
    Figure 3.  Comparison between numerical solution (left) and exact solution (right) with α=0.75 and T=2 (Example 5.1).
    Figure 4.  The numerical solution surface at t=1.2 with M=Nx=Ny=40 (Example 5.1).
    Figure 5.  The numerical solution surface at t=1.4 with M=Nx=Ny=40 (Example 5.1).
    Figure 6.  The numerical solution surface at t=1.6 with M=Nx=Ny=40 (Example 5.1).
    Figure 7.  The numerical solution surface at t=1.8 with M=Nx=Ny=40 (Example 5.1).

    The article first investigates the existence, uniqueness and regularity of solutions to (1.3). Then, a nonuniform L1/LDG scheme is constructed, and its stability and convergence are proven. Finally, the theoretical analysis is validated through numerical examples. In future work, we will focus on showcasing the physical properties of this numerical scheme and explore the implications of different definitions of α-order fractional derivatives in the original problem. Additionally, we will examine which definition yields better results in terms of effectiveness.

    The work was supported by the National Natural Science Foundation of China (No. 12101266).

    The authors declare they have not used Artificial Intelligence (AI) tools in the creation of this article.

    The authors declare there is no conflict of interest.



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