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Research article

A new α-robust nonlinear numerical algorithm for the time fractional nonlinear KdV equation

  • Received: 07 October 2023 Revised: 08 December 2023 Accepted: 12 January 2024 Published: 25 January 2024
  • 65M60; 26A33

  • In this work, we consider an α-robust high-order numerical method for the time fractional nonlinear Korteweg-de Vries (KdV) equation. The time fractional derivatives are discretized by the L1 formula based on the graded meshes. For the spatial derivative, the nonlinear operator is defined to approximate the uux, and two coupling equations are obtained by processing the uxxx with the order reduction method. Finally, the nonlinear difference schemes with order (2α) in time and order 2 precision in space are obtained. This means that we can get a higher precision solution and improve the computational efficiency. The existence and uniqueness of numerical solutions for the proposed nonlinear difference scheme are proved theoretically. It is worth noting the unconditional stability and α-robust stability are also derived. Moreover, the optimal convergence result in the L2 norms is attained. Finally, two numerical examples are given, which is consistent with the theoretical analysis.

    Citation: Caojie Li, Haixiang Zhang, Xuehua Yang. A new α-robust nonlinear numerical algorithm for the time fractional nonlinear KdV equation[J]. Communications in Analysis and Mechanics, 2024, 16(1): 147-168. doi: 10.3934/cam.2024007

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  • In this work, we consider an α-robust high-order numerical method for the time fractional nonlinear Korteweg-de Vries (KdV) equation. The time fractional derivatives are discretized by the L1 formula based on the graded meshes. For the spatial derivative, the nonlinear operator is defined to approximate the uux, and two coupling equations are obtained by processing the uxxx with the order reduction method. Finally, the nonlinear difference schemes with order (2α) in time and order 2 precision in space are obtained. This means that we can get a higher precision solution and improve the computational efficiency. The existence and uniqueness of numerical solutions for the proposed nonlinear difference scheme are proved theoretically. It is worth noting the unconditional stability and α-robust stability are also derived. Moreover, the optimal convergence result in the L2 norms is attained. Finally, two numerical examples are given, which is consistent with the theoretical analysis.



    Korteweg-de Vries equation is a classic representative of the nonlinear dispersion equation. Since it satisfies a lot of conservation laws in solids and liquids, it is widely used in the field of gas and plasma [1]. Dutch mathematicians Diederik Korteweg and Gustav de Vries [2] first discovered the KdV equation for unidirectional motion in 1895 while studying the small and medium amplitude long wave motion of diving waves; thus, the equation is named after the above two scholars. Since then, researchers gradually found that many physical phenomena are closely related to the KdV equation such as magnetic current wave and ionic sound wave in plasma, and pressure wave in liquid-gas mixture [3,4].

    In recent years, time fractional derivative has received extensive attention because of its heredity and memory [5,6,7,8,9,10,11], which can simulate a large number of physical phenomena involving anomalous diffusion and non-local behaviors. There are a series of numerical works on fractional linear or nonlinear differential equations [12,13,14,15,16,17,18,19,20]. In fact, fractional derivative was first developed by pure mathematicians in the middle of the 19th century. Some 100 years later, engineers and physicists have found applications for these concepts in their areas[21]. The emergence of the concept of fractional derivatives further strengthens the connection between disciplines. The presence of the fractional derivative introduces memory effects and non-local interactions, leading to the emergence of new wave phenomena and intriguing solutions[22,23,24,25]. Correspondingly, integer-order derivatives limit the ability of equations to capture the complexity of real-world phenomena, and many phenomena involving non-local or non-local behavior cannot be accurately described using traditional integer-order derivatives. To solve these problems, one can introduce the concept of fractional derivative and apply it to the KdV equation [26] to obtain the following nonlinear fractional KdV equation

    C0Dαtu(x,t)+γu(x,t)ux(x,t)+uxxx(x,t)=f(x,t),(x,t)Ωx×Ωt, (1.1)
    u(x,0)=ϕ(x),xΩx, (1.2)
    u(0,t)=0,u(L,t)=0,ux(L,t)=0,tΩt, (1.3)

    where Ωx=(0,L),Ωt=(0,T], the source term f(x,t) and initial condition ϕ(x) are known smooth functions. Here, the Caputo fractional derivative is used[27,28], which is define as follows

    C0Dαtu(x,t)=1Γ(1α)t0(ts)αu(x,s)sds,α(0,1).

    This definition takes into account the memory effect of the system, that is, the response of the system is affected by past time periods. By introducing fractional derivatives, the nonlinear fractional derivative KdV equation can describe long-term interactions, memory effects, and non-local phenomena.

    Over the past few decades, there has been an increasing amount of theoretical and numerical work on the nonlinear KdV equation. However, due to the nonlinearity and complexity of the KdV equation, it is very difficult or impossible to find the analytical solution. Therefore, a lot of scholars have devoted to obtain numerical solutions of various KdV equations. An et al.[29] proposed a fully discrete discontinuous Galerkin (DG) method combining the well-known L1 discretization in time and DG method in space to approximate the time fractional KdV equation. Cen et al.[30] studied a spatial first-order numerical method for integer order KdV equation with initial singularity, and a second order scheme is also presented, but no corresponding theoretical proof is given. Chen et al.[31] studied a numerical solution of the linearized fractional order KdV equation with the initial singular on graded meshes. Shen et al. [32] proposed a method for the fractional KdV equation, which on graded meshes got the fact that the convergence order of the numerical scheme was O(h+Nmin{2α,rα}). There are other KdV-types studies[33,34,35,36,37,38]. According to the existing research results, there is no space second-order difference scheme with complete theory and there is much room for progress in the study of the fractional order KdV equation. Therefore, in paper we construct a spatial second-order fully discrete difference scheme with complete theory analysis. Because of the improvement of the convergence rate, it can greatly improve the operation efficiency, which is very beneficial to large-scale calculations [39].

    In this paper, we consider an α-robust high-order numerical method for the time fractional nonlinear KdV equation, and the major results are as follows

    ● We use the reduction method of to handle uxxx and introduce the nonlinear operator ψ to approximate uux, and then a spatial second-order nonlinear difference scheme is obtained.

    ● We prove the existence, uniqueness, stability, and convergence of the proposed second-order nonlinear difference scheme, and then improved the unconditional stability to α-robust stability.

    ● The results of numerical examples are consistent with the theory, and it is verified that the proposed nonlinear difference scheme converges with order 2 in space and order (2α) in time on graded meshes.

    The rest of this article is arranged as follows. In Section 2, we provide some relevant symbols and lemmas needed for theoretical proof and constructing the nonlinear difference scheme. In Section 3, we present the theoretical result, where the existence, uniqueness, unconditional stability, α-robust stability, and convergence are proved in turn. In Section 4, two experiments are given to verify the reliability of the theoretical proof. At the end of the article, we have made a summary in Section 5.

    In this paper, C stands for some constants that can take on different values at different places, and the c with the subscript represents a specific constant.

    In the section, we provide some relevant symbols and lemmas needed in constructing the nonlinear difference scheme and theoretical analysis.

    Given the positive integers M and N, denote h:=LM be the spatial step, xj:=jh(0jM). Divide the interval [0,T] into N non-uniform compartments and set

    tn=(nτ)r, n=0,1,...,N, τ=T1/rN,

    where r (r1) is called the grading exponent, τn=tntn1 (n=1,2,,N) are time-steps. Define the grid functions as follows

    Uni:=u(xi,tn), fni:=f(xi,tn),0iM,0nN. (2.1)

    Denote

    Uh:={u|u=(u0,u1,...,uM)}

    and

    Uh:={u|uUh,u0=uM=0}

    be two set of grid functions.

    Next, we introduce some important notations, for uUh, let

    δxui+12=1h(ui+1ui), δ2xui=1h2(ui12ui+ui+1),  Δxui=12h(ui+1ui1).

    Assume u,vUh, we introduce inner product and norm as follows

    (u,v)=h(12u0v0+M1i=1uivi+12uMvM), u=(u,u), u=max0iM|ui|.

    In addition, we define the nonlinear operator ψ [40] as follows

    ψ(u,v)i=13[uiΔxvi+Δx(uv)i],1iM1.

    Now, we introduce several lemmas help to develop the theoretical analysis.

    Lemma 2.1. [41] Let vUh and u˚Uh, then one gets

    (ψ(v,u),u)=0. (2.2)

    Lemma 2.2. [42] For any grid function u,v˚Uh, then

    uLu,(u,δ2xv)=(δxu,δxv). (2.3)

    Next, we begin to construct a nonlinear difference method for Eq.(1.1)-(1.3). Let v=ux, then Eq.(1.1)–(1.3) can be written as

    C0Dαtu(x,t)+γu(x,t)ux(x,t)+vxx(x,t)=f(x,t), 0<x<L, 0<tT, (2.4a)
    v=ux,0<x<L, 0<tT, (2.4b)
    u(x,0)=ϕ(x), 0<x<L, (2.4c)
    u(0,t)=0, u(L,t)=0, v(L,t)=0, 0tT. (2.4d)

    Now, considering Eq.(2.4a) at the points (xi,tn) and Eq.(2.4b) at the points (xi+12,tn), one has

    C0Dαtu(xi,tn)+γu(xi,tn)ux(xi,tn)+vxx(xi,tn)=f(xi,tn), 1im1,0nN, (2.5)
    v(xi+12,tk)=ux(xi+12,tk),0im1,0nN. (2.6)

    Next, we discretize the equation (2.5). First, we approximate the Caputo fractional derivative C0Dαtu(xi,tn) by employing the L1 formula on the graded meshes

    DαNu(xi,tn)=an,1Γ(2α)u(xi,tn)1Γ(2α)n1s=1(an,san,s+1)u(xi,tns)an,nΓ(2α)u(xi,t0), (2.7)

    where

    an,s=((tntns)1α(tntns+1)1α)/τns+1, 1sn. (2.8)

    Denote (R1)ni=C0Dαtu(xi,tn)DαNu(xi,tn), from [44], then we can get the error as follows

    |(R1)ni|Cnmin{rα,2α}. (2.9)

    Second, using Taylor expansion and the definition of the operator ψ, one gets

    u(xi,tn)ux(xi,tn)=13{[u(xi1,tn)+u(xi,tn)+u(xi+1,tn)]+O(h2)}[Δxu(xi,tn)+O(h2)]=13(Uni1+Uni+Uni+1)ΔxUni+O(h2)=13[UniΔxUni+(Uni+1+Uni1)ΔxUni]+O(h2)=ψ(Un,Un)i+(R2)ni. (2.10)

    Using second-order central difference, one arrives at

    vxx(xi,tn)=δ2xVni+O(h2)=δ2xVni+(R3)ni. (2.11)

    Combining Eq.(2.7)-(2.11), we can easily obtain the nonlinear difference scheme of (2.4) as follows

    DαNUni+γψ(Un,Un)i+δ2xVni=fni+Pni, 1iM1, 1nN, (2.12a)
    Vni+12=δxUni+12+Qni+12, 0iM1, 1nN, (2.12b)
    U0i=ϕ(xi), 0iM, (2.12c)
    Un0=UnM=0, VnM=0, 0nN, (2.12d)

    where the |Pni|=|(R1)ni+(R2)ni+(R3)ni|C(h2+nmin{rα,2α}).

    Then, eliminating Pni and Qni+12 in the expression and substituting numerical solution uni and vni for its exact solution Uni and Vni, respectively, we can obtain the nonlinear difference scheme of Eq.(1.1)–(1.3) as follows

    DαNuni+γψ(un,un)i+δ2xvni=fni, 1iM1, 1nN, (2.13a)
    vni+12=δxuni+12, 0iM1, (2.13b)
    u0i=ϕ(xi), 0iM, (2.13c)
    un0=unM=0, vnM=0, 0nN. (2.13d)

    We refer to the following Browder theorem which help us to prove the existence of the solution of the difference scheme.

    Theorem 3.1. (Browder theorem)[43] Let (H,(,)) be a finite dimensional inner product space, is the derived norm operator, and Π:HH be continuous. Assume that

     α>0, zH, z=α, Re(Π(z),z)0.

    Then there exists satisfying |z|α such that Π(z)=0.

    Theorem 3.2. The nonlinear difference scheme (2.13) has at least a solution.

    Proof. Denote

    uk=(uk0,uk1,,ukM),vk=(vk0,vk1,,vkM).

    It is easy to get u0 from (2.13c), we can get v0 by computing (2.13b) and (2.13d).

    Suppose {u0,u1,,un1} and {v0,v1,,vn1} exist, then we now consider {un,vn} for nonlinear difference scheme (2.13), one has

    DαNuni+γψ(un,un)i+δ2xvni=fni, 1iM1, (3.1)
    vni+12=δxuni+12, 0iM1, (3.2)
    u0i=ϕ(xi), 0iM, (3.3)

    and

    un0=unM=0,vnM=0, 0nN. (3.4)

    Define Π(u):˚Uh˚Uh:

    Π(ui)={DαNui+γψ(u,u)i+δ2xvifni, 1iM1,0,i=0, M. (3.5)

    We notice that Π(u) is a continuous operator in ˚Uh. Thereupon, taking an inner product with u, leads to

    (Π(u),u)=an,1Γ(2α)u21Γ(2α)n1s=1(an,san,s+1)(uns,un)an,nΓ(2α)(u0,u)+(δ2xvn,u)(fn,u)an,1Γ(2α)u21Γ(2α)n1s=1(an,san,s+1)uunsan,nΓ(2α)uu0+12(v0)2ufnuΓ(2α)[an,1uan,nu0n1s=1(an,san,s+1)unsfn].

    Then, let u=1an,1(an,nu0+n1s=1(an,san,s+1)uns+fn), we can figure out (Π(u),u)0 such that Π(un)=0.

    Therefore, the nonlinear difference scheme (2.13) exists a solution {un,vn} at least.

    Denote:

    c2=max(x,t)[0,L]×[0,T]{|u(x,t)|,|ux(x,t)|,|uxx(x,t)|}.

    Theorem 3.3. The solution of the difference scheme (2.13) is unique.

    Proof. It is easy to get that u0 and v0 are unique, respectively. Now, suppose that

    {u0,u1,,un1} and {v1,v2,,vn1} are unique.

    For k=n, assuming that both {un,vn} and {ˆun,ˆvn} are the solutions of (2.13), respectively, that is to say they satisfy:

    {DαNuni+γψ(un,un)i+δ2xvni=fni, 1iM1,vni+12=δxuni+12, 0iM1,un0=unM=0, vnM=0, (3.6)

    and

    {DαNˆuni+γψ(ˆun,ˆun)i+δ2xˆvni=fni, 1iM1,ˆvni+12=δxˆuni+12, 0iM1,ˆun0=ˆunM=0, ˆvnM=0. (3.7)

    Let

    ρni=uniˆuni, ηni=vniˆvni.

    Subtracting (3.6) from (3.7), due to u0,u1,,un1 and v0,v1,,vn1 are unique, we get

    an,1Γ(2α)ρni+γ[ψ(un,un)iψ(ˆun,ˆun)i]+δ2xηni=0, 1iM1, (3.8)
    ηni+12=δxρni+12, 0iM1, (3.9)
    ρn0=ρnM=0,ηnM=0. (3.10)

    Further, taking inner product for (3.8) with ρn, one leads to

    an,1Γ(2α)ρn2+(γ[ψ(un,un)ψ(ˆun,ˆun)],ρn)+(δ2xηn,ρn)=0. (3.11)

    For the second term on the left side of the equation, by Lemma 2.2, leads to

    (γ[ψ(un,un)ψ(ˆun,ˆun)],ρn)=(γ[ψ(un,un)ψ(unρn,unρn)],ρn)=γ(ψ(ρn,un),ρn). (3.12)

    Combining the previous definitions of both inner products and operators ψ(,), we can derive

    (ψ(ρn,un),ρn)=h3M1i=1[ρniΔxuni+Δx(ρnun)i]ρni=h3M1i=1(ρni)2Δxunih6M1i=1uni+1unihρniρni+1c22ρn2. (3.13)

    In addition, using Eq.(3.9) and (3.10), for the third term on the left side, we derive

    (δ2xηn,ρn)=(δxηn,δxρn)=hm1i=0(δxηni+12)ηni+12=12[(ηnM)2(ηn0)2]=12(ηn0)20. (3.14)

    Substituting (3.12)-(3.14) into (3.11), then we have

    an,1Γ(2α)ρn2c2|γ|2ρn2. (3.15)

    When an,1Γ(2α)>c2|γ|2, that is ταn<2Γ(2α)|γ|c3. We can get ρn=0. That is to say it holds that u=ˆu,v=ˆv. By mathematical induction, the solution of difference scheme (2.13) is unique.

    Theorem 3.4. (L2-stability) Assume that {uni| 1iM1,1nN} is the solution of the difference scheme (2.13), then the solution is unconditionally stable.

    Proof. First, we take the inner product on both sides of the Eq.(2.13a) with un, one obtains

    (DαNun,un)+γ(ψ(un,un),un)+(δ2xvn,un)=(fn,un), 1nN. (3.16)

    Using Lemma 2.2, one has

    γ(ψ(un,un),un)=0. (3.17)

    Second, by (2.13b) and (2.13d), one has

    (δ2xvn,un)=(δxvn,δxun)=hm1i=0(δxvni+12)vni+12=12[(vnM)2(vn0)2]=12(vn0)20. (3.18)

    Thus, we get the following inequality

    (DαNun,un)(fn,un). (3.19)

    Using the Cauchy-Schwarz inequality and noticing an,san,s+1, we arrive at

    an,1Γ(2α)unfn+1Γ(2α)(an,nu0+n1s=1(an,san,s+1)uns), (3.20)

    the above formula can be rearranged as

    unταn(Γ(2α)fn+an,nu0+n1s=1(an,san,s+1)uns). (3.21)

    Next, we define

    λn,n=1, λn,m=nms=1ταns(an,san,s+1)λns,m. (3.22)

    Then, from [Lemma 4.1 and Lemma 4.2 of [44]], one has

    un≤≤u0+Γ(2α)ταnns=1λn,sfs. (3.23)

    According to [Lemma 4.3, [44]], we select the parameter βrα, and note that Γ(1+α)=αΓ(α), leads to

    ταnns=1sβλn,sTαNβ1α. (3.24)

    Then, we get

    Γ(2α)ταnns=1sβλn,sΓ(2α)1αTαNβ=Γ(1α)TαNβ. (3.25)

    The above equation can also be written

    Γ(2α)ταnns=1λn,sΓ(1α)Tα(nN)β, sn. (3.26)

    Further, we can have

    Γ(2α)ταnns=1λn,sfsTαΓ(1α)(nN)βmax1snfs. (3.27)

    In the end, combined Eq.(3.23) and Eq.(3.27), we get

    unu0+TαΓ(1α)(nN)βmax1snfs. (3.28)

    Remark 3.5. In this theorem, we have completed the stability proof of solution. However, when α1, we note that it leads to Γ(1α), and the values on the right-hand side of the inequality are no longer binding. In order to avoid this shortcoming, we next to improved the result in Theorem 3.7.

    Lemma 3.6. [45] For any finite time tN=T>0 and a given nonnegative sequence (λl)N1l=0, assume that there exists a constant λ, independent of time-steps, such that λN1l=0λl. Suppose that the grid function {vn|n0} satisfies

    DαNvnnl=1λnlvl+ξn+ηn,n1, (3.29)

    where {ξn,ηn|1nN} are nonnegative sequences. If the time-step satisfies τk1τk and the maximum time-step τNα12Γ(2α)λ, one holds that

    vk2Eα(2λαk)(v0+max1ikil=1P(i)ilξl+ω1+α(tk)max1ikηi),1kN, (3.30)

    where Eα(x)=k=0xk/Γ(1+kα) is the Mittag-Leffler function, ωβ(t)=tβ1Γ(β), and the discrete convolution kernel P(n)nk is defined as follows

    P(n)nk=1ak,1{Γ(2α),k=n,ni=k+1(ai,ikai,ik+1)P(n)ni,1kn1.

    Theorem 3.7. (α-robust L2-stability) Assume that {uni|1iM1,1nN} is the solution of the scheme (2.13), then one has

    un2C(u0+tαnΓ(1+α)max1knfk).

    Proof. First, taking inner product to un for the Eq.(2.13a), we can get

    (DαNun,un)=an,1Γ(2α)un2an,nΓ(2α)(u0,un)1Γ(2α)n1s=1(an,san,s+1)(uns,un)an,1Γ(2α)un212an,nΓ(2α)u0212an,nΓ(2α)un212Γ(2α)n1s=1(an,san,s+1)uns212Γ(2α)n1s=1(an,san,s+1)un212DαNun2.

    According to Lemma 2.2 and equation (3.18), we have

    γ(ψ(un,un),un)=0

    and

    (δ2xvn,un)=12(vn0)20.

    Therefore, employing Cauchy-Schwartz inequality and Young inequality, we arrive at

    12DαNun2(fn,un)fnun12fn2+12un2. (3.31)

    Further, due to the Lemma 3.6, one leads to

    un22Eα(2tαn)(u02+ω1+α(tn)max1knfk2)C(u02+ω1+α(tn)max1knfk2). (3.32)

    Finally, we can get the result of stability

    un2C(u0+ω1+α(tn)max1knfk)2, (3.33)

    which is equivalent to

    unC(u0+tαnΓ(1+α)max1knfk). (3.34)

    The above theorem solves the shortcoming when α1.

    In this subsection, we will prove the convergence of the nonlinear difference scheme (2.13). First, we introduce the following lemma to help us complete the proof.

    Lemma 3.8. [46] For any fixed t[0,T], if u(x,)C6([0,L]), for 0kN, denote

    Ski=1h(Qki+12Qki12),1iM1,
    RkM1=0,Rkj=M1i=j+1(1)ij1Ski,j=M2,M3,.

    Then there exists a constant c3, one has

    |Ski|c3h2, 1iM1, 0kN,
    |Rkj|c3h2, 0jM2, 0kN,

    and

    |δxRkj+12|c3h2, 0jM2.

    Theorem 3.9. Assume {Uki,Vki| 0iM, 0kN} and {uki,vki| 0iM, 0kN} be the solution of (2.12) and the difference scheme (2.13), respectively. Then there exists a constant such that

    Nn=1τnenC(τ2α+h2).

    Proof. Denote

    eki=Ukiuki, gki=Vkivki, 0iM, 0kN

    and

    c4=c21+c23+2c1c3L+c23L.

    Subtracting (2.12) from (2.13), one can get the system of error equation

    DαNeni+γ[ψ(Un,Un)iψ(un,un)i]+δ2xgni=Pni, 1iM1, 1nN, (3.35)
    gni+12=δxe2i+12+Qni+12, 0iM1, 1nN, (3.36)
    e0i=0, 0iN, (3.37)
    en0=enM=0,gnM=0, 0nN. (3.38)

    Taking inner product of (3.35) with en, leads to

    (DαNen,en)+(δ2xgn,en)=(Pn,en)γ(ψ(Un,Un)ψ(un,un),en). (3.39)

    For the first term, by the definition and Cauchy-Schwartz inequality, we have

    (DαNen,en)=hM1i=1[an,1eniΓ(2α)an,ne0iΓ(2α)1Γ(2α)n1s=1(an,san,s+1)ensi]eni=an,1en2Γ(2α)an,n(e0,en)Γ(2α)1Γ(2α)n1s=1(an,san,s+1)(ens,en)an,1Γ(2α)en212an,nΓ(2α)e0212an,nΓ(2α)en2n1s=1(an,san,s+1)2Γ(2α)ens2n1s=1(an,san,s+1)2Γ(2α)en212DαNen2. (3.40)

    According to equation (3.13), for the second term on right of equation, one has

    γ(ψ(Un,Un)ψ(un,un),en)c2|γ|2en2. (3.41)

    For the second term on the left hand

    (δ2xgn,en)=(δxgn,δxen)=hM1i=0(δxgni+12)(gni+12Qni+12)=hM1i=0(δxgni+12)gni+12hM1i=0(δxgni+12)Qni+12=12M1i=0[(gni+1)2(gni)2]M1i=0(gni+1gni)Qni+12=12(gn0)2+hM1i=1gniSni+gn0Qn12. (3.42)

    Rewrite gni as follows

    gni=(gni+gni1)(gni1+gni2)++(1)i1(gn1+gn0)+(1)ign0=2i1j=0(1)ij1gni+12+(1)ign0. (3.43)

    By the definitions of Rni and δxRni+12, we arrive at

    hM1i=1gniSni=hM1i=1[2i1j=0(1)ij1gni+12+(1)ign0]Sni=2hM2j=0gni+12M1i=j+1(1)ij1Sni+hm1i=1(1)ign0Sni=2hM2j=0gni+12Rnj+gn0[hM1i=1(1)iSni]=2hM2j=0(δxenj+12+Qnj+12)Rnj+gn0(Rn0)=2hM2j=0Qnj+12Rnj2hM1j=1enj(δxRnj12)gn0Rn0. (3.44)

    Substituting the above results and applying Lemma 3.8, leads to

    (δ2xgn,en)=12(gn0)2+gn0Qn12gn0Rn0+2hM2j=0Qnj+12Rnj2hM1j=1enj(δxRj12)12(gn0)2+[14(gn0)2+(Qn12)2]+[14(gn0)2+(Rn0)2]+2hM2j=0|Qnj+12||Rk+12j|+en2+hM1j=1(δxRnj12)2en2+(c21+c23+2c1c3L+c23L)h4. (3.45)

    Combining with (3.39)-(3.45), we get

    12DαNen2(c2|γ|2+1)en2+(c21+c23+2c1c3L+c23L)h4+(Pn,en)(c2|γ|2+1+12)en2+c4h4+12Pn2. (3.46)

    Further, there exists a constant c5 such that

    DαNen2(|γ|c2+3)en2+(c5nmin{rα,2α}+c5h2)2. (3.47)

    Using the Lemma 3.6, then we have

    |en22Eα(2λαn)ω1+α(tn)(c5nmin{rα,2α}+c5h2)2. (3.48)

    Taking the square root of both sides, for simplicity, the above equation can be written as

    enC(nmin{rα,2α}+h2). (3.49)

    Multiplying both sides of this inequality by τn, and then summing up for n from 1 to N, arrives at

    Nn=1τnenCNn=1τn(h2+nmin{rα,2α})Ch2T01dt+Cτmin{rα,2α}Nn=1τntmin{α,2αr}nC(h2+τmin{rα,2α}).

    We select r=2αα, then we can get the optimal grids, which leads to the difference scheme can achieve (2α) precision in the time direction.

    Nn=1τnenC(τ2α+h2).

    In this section, we will present two numerical experiments to verify the reliability of the previous theoretical results. From the theoretical proofs of the nonlinear difference scheme established in this paper, it can be found that the scheme has only one solution, so we choose the fixed point iteration method to calculate the numerical solution. For details, see reference [47]HY__HY, Algorithm 1]. Another way, for the variable v introduced in the nonlinear difference scheme, it is not necessary to participate in the calculation, and the difference scheme can be separated to obtain a difference system with only variable u. We select T=L=γ=1 and employ the scheme (2.13) to solve the following examples. In order to achieve the optimal convergence rate in time, we select r=2αα.

    In our examples we consider the exact solution has no known and define L-errors and convergence rate, respectively.

    E(M,N)=max1kN{max1iM1|uhkiuki|},
    ratet=log2E(M,N)E(M,2N),ratex=log2E(M,N)E(2M,N),

    where the u is reference solution that can approximately replace the exact solution in time or space with high-precision.

    Example 1. In this example, we consider the initial value condition is u0(x)=0 and the source term is

    f(x,t)=t1αsin(2πx)/Γ(2α)+2πt2sin(2πx)cos(2πx)8π3tsin(2πx).

    In Example 1, we can compute numerical solutions for different nodes at different time and space steps as in Table 1. To verify the spatial convergence rate, we first fix N=512. Table 2 lists the convergence rates for different α. We can observe that the spatial convergence rate is order 2, and it is clear that the calculated result satisfies the theoretical expectation well. On the other hand, when we verify the temporal convergence rate, we fix M=512. Table 3 lists the change of the numerical solution of Example 1 with N for different α, where Ratet is the convergence rate in the time direction. However, we notice that both α and N values are small, the convergence rate is slow, failing to meet the theoretical expectation of (2α). Thus, we increase the number of nodes, and the convergence rate gradually approaches the theoretical value. Therefore, the time convergence diagram drawn in Figure 3, the space convergence diagram drawn in Figure 4, where the numerical curve are parallel to the theoretical expected curve. This shows the superiority of graded meshes.

    Table 1.  Take N=4, T=1, the numerical solution of each node under different space steps in example 1.
    x M = 8 M = 16 M = 32 M = 64 M = 128
    1/4 6.087 5.798 5.729 5.712 5.707
    5/8 3.774 3.597 3.555 3.545 3.542
    7/8 5.043 4.850 4.801 4.789 4.786

     | Show Table
    DownLoad: CSV
    Table 2.  L errors and convergence rates in spatial direction for Example 1.
    M α=0.1 α=0.2 α=0.35 α=0.5 α=0.8 α=0.95
    E(M, N) ratex E(M, N) ratex E(M, N) ratex E(M, N) ratex E(M, N) ratex E(M, N) ratex
    8 2.905e-01 2.899e-01 2.893e-01 2.889e-01 2.891e-01 2.900e-01
    16 6.950e-02 2.064 6.937e-02 2.063 6.922e-02 2.063 6.914e-02 2.063 6.921e-02 2.063 6.921e-02 2.063
    32 1.740e-02 1.998 1.736e-02 1.998 1.732e-02 1.999 1.729e-02 1.999 1.731e-02 2.000 1.731e-02 2.000
    64 4.340e-03 2.003 4.331e-03 2.003 4.322e-03 2.003 4.316e-03 2.003 4.320e-03 2.002 4.320e-03 2.002

     | Show Table
    DownLoad: CSV
    Table 3.  Example 1: L errors and convergence rates in temporal direction.
    N α=0.1 α=0.2 α=0.35 α=0.5 α=0.8 α=0.95
    E(M, N) ratet E(M, N) ratet E(M, N) ratet E(M, N) ratet E(M, N) ratet E(M, N) ratet
    32 1.815e-04 2.171e-04 2.222e-04 2.386e-04 8.521e-04 2.905e-03
    64 1.007e-04 0.850 9.110e-05 1.253 8.730e-05 1.348 9.579e-05 1.318 4.015e-04 1.086 1.515e-03 0.939
    128 4.099e-05 1.297 3.313e-05 1.456 3.177e-05 1.459 3.658e-05 1.389 1.814e-04 1.146 7.639e-04 0.988
    256 1.437e-05 1.512 1.118e-05 1.567 1.107e-05 1.521 1.359e-05 1.429 8.044e-05 1.174 3.764e-04 1.021
    512 4.659e-06 1.625 3.613e-06 1.630 3.758e-06 1.559 4.961e-06 1.453 3.534e-05 1.187 1.837e-04 1.035
    1024 1.444e-06 1.690 1.137e-06 1.668 1.254e-06 1.584 1.794e-06 1.468 1.546e-05 1.193 8.915e-05 1.043
    2048 4.358e-07 1.729 3.503e-07 1.699 4.126e-07 1.604 6.447e-07 1.476 6.746e-06 1.196 4.316e-05 1.047
    4096 1.293e-07 1.753 1.069e-07 1.712 1.352e-07 1.610 2.284e-07 1.497 2.940e-06 1.198 2.087e-05 1.048

     | Show Table
    DownLoad: CSV

    Example 2. For the second example, we consider the initial condition is u0(x)=0, and the source term is

    f(x,t)=4x(1x)Γ(3α)t2α+4x(1x)(12x)t4.

    In Example 2, fixed N=512, Table 2 lists the changes of the maximum error values E(M,N) of different α with M. From the table, we see that the spatial convergence rate is order 2. Then, to verify the time convergence rate, fixed M=512, Table 5 lists the variation of the maximum error E(M,N) with N for different α. Similar to Example 1, when α is larger, the time convergence rate is (2α), which is consistent with the theory. When α is small, due to the effect of the singularity of this equation, the time convergence rate is lower than the theoretical value, so we increase the time node quantity N, and with the increase of N, the time convergence rate gradually returns to (2α).

    Table 4.  Example 2 L errors and convergence rates in spatial direction.
    M α=0.1 α=0.2 α=0.35 α=0.5 α=0.8 α=0.95
    E(M, N) ratex E(M, N) ratex E(M, N) ratex E(M, N) ratex E(M, N) ratex E(M, N) ratex
    8 6.702e-04 6.908e-04 7.225e-04 7.552e-04 8.276e-04 8.849e-04
    16 1.679e-04 1.997 1.731e-04 1.997 1.824e-04 1.986 1.922e-04 1.975 2.136e-04 1.954 2.261e-04 1.969
    32 4.227e-05 1.990 4.369e-05 1.986 4.588e-05 1.991 4.814e-05 1.999 5.344e-05 1.999 5.657e-05 1.999
    64 1.057e-05 2.000 1.093e-05 2.000 1.147e-05 2.000 1.205e-05 1.999 1.336e-05 2.000 1.415e-05 1.999

     | Show Table
    DownLoad: CSV
    Table 5.  Example 2 L errors and convergence rates in temporal direction.
    N α=0.1 α=0.2 α=0.35 α=0.5 α=0.8 α=0.95
    E(M, N) ratet E(M, N) ratet E(M, N) ratet E(M, N) ratet E(M, N) ratet E(M, N) ratet
    32 6.899e-05 7.384e-05 6.704e-05 6.197e-05 5.372e-04 9.439e-05
    64 3.545e-05 0.961 3.020e-05 1.290 2.605e-05 1.364 2.472e-05 1.326 2.452e-05 1.131 4.742e-05 0.993
    128 1.420e-05 1.320 1.094e-05 1.456 9.458e-06 1.462 9.430e-06 1.390 1.096e-05 1.162 2.336e-05 1.021
    256 4.981e-06 1.512 3.695e-06 1.566 3.295e-06 1.521 3.503e-06 1.429 4.842e-06 1.179 1.140e-05 1.036
    512 1.620e-06 1.620 1.195e-06 1.628 1.119e-06 1.559 1.279e-06 1.453 2.125e-06 1.188 5.531e-06 1.043
    1024 5.034e-07 1.686 3.762e-07 1.668 3.733e-07 1.584 4.624e-07 1.468 9.273e-07 1.196 2.678e-06 1.046
    2048 1.520e-07 1.728 1.161e-07 1.696 1.231e-07 1.601 1.659e-07 1.479 4.071e-07 1.188 1.296e-06 1.047
    4096 4.495e-08 1.758 3.536e-08 1.716 4.023e-08 1.613 5.907e-08 1.490 1.773e-07 1.199 6.286e-07 1.045

     | Show Table
    DownLoad: CSV

    The solution of the KdV equation describes the propagation and evolution behavior of waves in the system under the influence of nonlinear, non-local and memory effects. The dynamic evolution graph enables us to understand the spatial and temporal characteristics of the solution, the physical meaning of the evolutionary behavior, and the propagation and interaction of the wave. Figures 12 and Figures 56 are the dynamic evolution graph of the solutions of Example 1 and Example 2 respectively. Because the temporal convergence rate is (2α), the numerical solution obtained by taking different α at the same time will change with the change of α. Figures 1 and Figure 2 draw the numerical solution surface obtained by different α of Example 1, Figure 5 and Figure 6 draw the numerical solution surface obtained by different α of Example 2, from which we can see only the slight difference. To highlight the difference, we draw Figure 7, the curve of the value obtained by different α at the same time T=1 for the example 2.

    Figure 1.  The graph of the numerical solution with α=0.2.
    Figure 2.  The graph of the numerical solution with α=0.8.
    Figure 3.  Temporal convergence.
    Figure 4.  Spatial convergence.
    Figure 5.  The graph of the numerical solution with α=0.2.
    Figure 6.  The graph of the numerical solution with α=0.8.
    Figure 7.  T=1, the graph with different α.
    Figure 8.  Temporal convergence.
    Figure 9.  Spatial convergence.

    In this paper, a nonlinear difference scheme has been established for solving time fractional nonlinear KdV equations. The precision of τ2α is achieved in time and h2 in space. In theoretical analysis, the mathematical induction is applied in the proof of the existence and uniqueness, and the Browder theorem plays an important role for the existence analysis of nonlinear difference scheme solutions. In addition, the unconditional stability proof of the nonlinear difference scheme and the α-robust stability proof are given. Finally, the proof of convergence in the L2 norm is derived. The above several theoretical results are verified by two numerical examples. It is worth noting that two kinds of stability analysis are carried out and that the first stability result will explode when α1, so we introduce the discrete Gronwall inequality to improve the analysis. The relevant theoretical proofs in this paper are complementary to the fractional order nonlinear KdV equation.

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

    We thank the anonymous referees for their valuable comments and suggestions which helped us to improve the manuscript a lot.

    The work was supported by National Natural Science Foundation of China Mathematics Tianyuan Foundation (12226337, 12226340, 12126321, 12126307), Scientific Research Fund of Hunan Provincial Education Department (21B0550, 22C0323, 23C0193), Hunan Provincial Natural Science Foundation of China (2022JJ50083, 2023JJ50164).

    The authors declare that there no conflicts of interest.



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