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Research article

A novel two-grid Crank-Nicolson mixed finite element method for nonlinear fourth-order sin-Gordon equation

  • Received: 18 September 2024 Revised: 28 October 2024 Accepted: 31 October 2024 Published: 05 November 2024
  • MSC : 65M15, 65N12, 65N35

  • A new nonlinear fourth-order sin-Gordon equation with actual physical background is first created. Then, by introducing an auxiliary function, the nonlinear fourth-order sin-Gordon equation is decomposed into the nonlinear system of equations of second-order derivatives of spatial variables. Subsequently, the time derivative is discretized by using the Crank-Nicolson (CN) scheme to construct a new time semi-discretized mixed CN (TSDMCN) scheme. Thereafter, the spatial variables in the TSDMCN scheme are discretized by using a two-grid mixed finite element (MFE) method to construct a new two-grid CN MFE (TGCNMFE) method with unconditional stability and second-order time precision, which consists of a system of nonlinear MFE equations defined on coarser grids and a system of linear MFE equations defined on finer grids with sufficiently high precision, and is very easy to solve. The existence, stability, and error estimates of the TSDMCN and TGCNMFE solutions are strictly proved theoretically, and the superiorities of the TGCNMFE method and the correctness of theoretical results are verified by two sets of numerical experiments.

    Citation: Yanjie Zhou, Xianxiang Leng, Yuejie Li, Qiuxiang Deng, Zhendong Luo. A novel two-grid Crank-Nicolson mixed finite element method for nonlinear fourth-order sin-Gordon equation[J]. AIMS Mathematics, 2024, 9(11): 31470-31494. doi: 10.3934/math.20241515

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  • A new nonlinear fourth-order sin-Gordon equation with actual physical background is first created. Then, by introducing an auxiliary function, the nonlinear fourth-order sin-Gordon equation is decomposed into the nonlinear system of equations of second-order derivatives of spatial variables. Subsequently, the time derivative is discretized by using the Crank-Nicolson (CN) scheme to construct a new time semi-discretized mixed CN (TSDMCN) scheme. Thereafter, the spatial variables in the TSDMCN scheme are discretized by using a two-grid mixed finite element (MFE) method to construct a new two-grid CN MFE (TGCNMFE) method with unconditional stability and second-order time precision, which consists of a system of nonlinear MFE equations defined on coarser grids and a system of linear MFE equations defined on finer grids with sufficiently high precision, and is very easy to solve. The existence, stability, and error estimates of the TSDMCN and TGCNMFE solutions are strictly proved theoretically, and the superiorities of the TGCNMFE method and the correctness of theoretical results are verified by two sets of numerical experiments.



    Let ΩRd (d=2,3) be a connected bounded domain with the boundary Ω. We propose a new nonlinear fourth-order sin-Gordon (NFOSG) equation, which is different from the standard sin-Gordon equation in [1,2] and is defined as follows:

    Problem 1. Find ϖ:[0,te]C4(ˉΩ), satisfying

    {ϖtt(x,t)Δϖ(x,t)+Δ2ϖ(x,t)+sin(ϖ(x,t))=0,(x,t)Ω×(0,te),ϖ(x,t)=Δϖ(x,t)=0,(x,t)Ω×(0,te),ϖ(x,0)=ϖ0(x),ϖt(x,0)=ϖ1(x),xΩ, (1.1)

    where te is a specified time upper bound,

    ϖtt(x,t)=2ϖ(x,t)/t2,x=(x1,x2,,xd),Δ=di=12/x2i

    is the Laplace operator, both ϖ0(x) and ϖ1(x) are sufficiently smooth known initial functions, and

    ϖt(x,t)=ϖ(x,t)/t.

    The NFOSG equation is obtained by adding a fourth-order term Δ2ϖ(x,t) to the standard sin-Gordon equation. It is well known (see, e.g., [3,4,5]) that the fourth-order term Δ2ϖ(x,t) can describe the deformation of an object under the action of an external force such as seismic waves and flying aircraft, while the nonlinear term sin(ω(x,t)) can describe the nonlinear behavior of a moving body/wave. Therefore, the NFOSG equation can not only describe the fluid mechanics of porous media [6,7,8], groundwater dynamics [9], seepage mechanics and groundwater hydraulics [10,11,12], etc., like the standard sin-Gordon equation, but also describe the nonlinear deformation behavior of moving bodies/waves, such as the movement of seismic waves or the movement of flying aircraft. Therefore, the NFOSG equation is an important mathematical physics model with a real application background and has a wider range of applications than the standard sin-Gordon equation.

    However, as a result of the NFOSG equation including a strong nonlinear term sin(ω(x,t)), it is very difficult to solve analytically. A numerical method is the most effective choice to solve the NFOSG equation. Fortunately, the numerical methods of the NFOSG equation play a pivotal role in simulation of the earthquake wave, the motion of flying aircraft, as well as the fluid mechanics of porous media, groundwater dynamics, seepage mechanics, groundwater hydraulics, and other phenomena. Therefore, it is very important to study the numerical methods of the NFOSG equation.

    A large number of numerical examples have showed that the two-grid finite element (FE) algorithm is one of the best numerical methods for solving nonlinear partial differential equations (PDEs), which consists of a nonlinear FE system of equations defined on coarser grids and a linear FE system of equations defined on finer grids with sufficiently high precision. Hence, it can simplify computation and enhance calculation efficiency. It was originally used to solve quasi-linear elliptic equations [13]. More recently, Shi's and Liu's teams have used it to solve some of the more complex nonlinear PDEs (see [14,15,16]).

    However, to our knowledge, at the moment, there has been no report on the Crank-Nicolson (CN) mixed FE (MFE) (CNMFE) format for the NFOSG equation reduced with two-grid FE technique. Therefore, the main task of this paper is to develop a new two-grid CNMFE (TGCNMFE) method for the NFOSG equation (i.e., Problem 1). The TGCNMFE method has at least three benefits. First, by introducing an auxiliary function φ=Δϖ, the NFOSG equation is split into two second-order equations, which can be easily solved by lower degree FEs such as linear or quadratic FEs. Second, the TGCNMFE method has unconditional stability and second-order time accuracy. Third, the TGCNMFE method also consists of a nonlinear MFE equation defined on coarser grids and a linear MFE equation defined on finer grids, which greatly simplifies the calculation and improves the calculation efficiency.

    Although some single-grid FE methods for the standard sin-Gordon equation with only second-order derivatives of spatial variables have been proposed in [10,11,12], they are completely different from the TGCNMFE method for the NFOSG equation with fourth-order derivatives of spatial variables. Both the TGCNMFE method and the NFOSG equation are far more complex than those in [10,11,12]. Therefore, both the establishment of the TGCNMFE method and the theoretical analysis of existence, stability, and errors of the TGCNMFE solutions herein are more difficult and require more skills than the single-grid FE methods in [10,11,12], but the NFOSG equation has a wider range of applications than the standard sin-Gordon equation, as mentioned above. Hence, it is very valuable to study the TGCNMFE method for solving the NFOSG equation.

    The rest of this paper consists of the following four sections. In Section 2, by introducing an auxiliary function φ=Δϖ, we split the NFOSG equation into two second-order equations, and by using the time CN scheme to discretize them, we design a new time semi-discretization mixed CN (TSDMCN) scheme and discuss the existence, stability, and error estimates of the TSDMCN solutions. In Section 3, by using the two-grid MFE method to discretize the TSDMCN scheme, we construct a new TGCNMFE method for the NFOSG equation and analyze the existence, stability, and errors of the TGCNMFE solutions. In Section 4, we use two sets of numerical experiments to confirm the correctness of the obtained theoretical results and show the superiorities of the TGCNMFE method. Finally, we give the main conclusions of this article and future study prospects in Section 5.

    The Sobolev spaces and norms used in this context are classical (see [5,17,18]). Let

    W=H10(Ω)andφ=Δϖ.

    Thus, by Green's formula, we can derive the following mixed variational format of Problem 1.

    Problem 2. For any t(0,te), find (ϖ,φ)W×W, meeting

    {(ϖtt,υ)+(φ,υ)+(φ,υ)=(f(ϖ),υ),υW,(ϖ,ϑ)=(φ,ϑ),ϑW,ϖ(x,0)=ϖ0(x),ϖt(x,0)=ϖ1(x),φ(x,0)=Δϖ0(x),xΩ, (2.1)

    where (,) denotes the L2 inner product, and

    f(ϖ)=sin(ϖ).

    Using the proof method of Theorem 3.3.1 in [5] or the proof method of the following Theorem 1, we can demonstrate the existence and stability of the generalized solutions for Problem 2.

    In order to establish the TGCNMFE method, we first set up a new TSDMCN scheme. Therefore, we assume that K>0 is an integer,

    Δt=te/K

    is the time step, and ϖk and φk are the approximations to ϖ(x,t) and φ(x,t) at

    tk=kΔt(0kK),

    respectively.

    Using an implicit scheme of time to discretize the first equation in Problem 2 yields

    1Δt2(ϖk+12ϖk+ϖk1,υ)+(φk+1,υ)+(φk+1,υ)=(f(ϖk+1),υ),υW. (2.2)

    Using an explicit scheme of time to discretize the first equation in Problem 2 yields

    1Δt2(ϖk+12ϖk+ϖk1,υ)+(φk1,υ)+(φk1,υ)=(f(ϖk1),υ),υW. (2.3)

    By adding formulas (2.2) and (2.3), we obtain the following brand-new TSDMCN format, which is different from the existing time semi-discrete formats, including that in [1].

    Problem 3. Find {ϖk,φk}W×W (1kK), meeting

    {1Δt2(ϖk+12ϖk+ϖk1,υ)+12((φk+1+φk1),υ)+12(φk+1+φk1,υ)=12(f(ϖk+1)+f(ϖk1),υ),υW,1kK1,(ϖk,ϑ)=(φk,ϑ),ϑW,0kK,ϖ0=ϖ0,ϖ1=ϖ0+Δtϖ1,φ0=Δϖ0,φ1=φ0ΔtΔϖ1,inΩ. (2.4)

    For Problem 3, we obtain the following results:

    Theorem 1. Problem 3 has a unique series of solutions

    {ϖk,φk}Kk=1W×W

    meeting the following boundness, i.e., stability:

    ϖk0+φk0c(ϖ01+ϖ11),1kK. (2.5)

    The c used in this context is a generical positive constant independent of Δt. And, when ϖ0(x) and ϖ1(x) are adequately smooth, the series of solutions {ϖk,φk}Kk=1 meets the error estimates

    (ϖ(tk)ϖk)0+(φ(tk)φk)0cΔt2,1kK, (2.6)

    where

    ϖ(tk)=ϖ(x,tk)andφ(tk)=φ(x,tk)(1kK).

    Proof. The demonstration of Theorem 1 consists of the following three parts.

    (1) The existence and uniqueness of series of solutions of Problem 3.

    Taking

    υ=ϖk+1ϖk1

    in the first subsystem of equations of (2.4), by the second subsystem of equations of (2.4), the Hölder and Cauchy inequalities, and the Lagrange differential mean formula (LDMF), we obtain

    ϖk+1ϖk20ϖkϖk120+Δt22(φk+120φk120)+Δt22(ϖk+120ϖk120)=Δt22(f(ϖk+1)+f(ϖk1),ϖk+1ϖk1)cΔt2(ϖk+1ϖk20+ϖkϖk120),1kK1. (2.7)

    By summing (2.7) from 1 to k (kK1) and using the third equation of (2.4), we obtain

    ϖk+1ϖk20+Δt22(φk+120+φk20)+Δt22(ϖk+120+ϖk20)ϖ1ϖ020+Δt22(φ120+φ020)+Δt22(ϖ120+ϖ020)+cΔt2kj=0ϖj+1ϖj20cΔt2(ϖ021+ϖ121)+cΔt2kj=0ϖj+1ϖj20,1kK1. (2.8)

    When Δt is adequately small satisfying cΔt21/4, by simplifying (2.8), we obtain

    ϖk+1ϖk20+Δt2φk+120+Δt2ϖk+120cΔt2(ϖ021+ϖ121)+cΔt2k1j=0ϖj+1ϖj20,1kK1. (2.9)

    By applying Gronwall's inequality (see [5, Lemme 3.1.9]) to (2.9), we obtain

    ϖk+1ϖk20+Δt2φk+120+Δt2ϖk+120cΔt2(ϖ021+ϖ121)exp(ckΔt2)cΔt2(ϖ021+ϖ121),1kK1. (2.10)

    Thereupon, we obtain

    φk0+ϖk0c(ϖ01+ϖ11),1kK. (2.11)

    Further, by the first and second subsystems of equations of (2.4), the Hölder and Cauchy inequalities, and LDMF, we obtain

    (ϖk+1ϖk)20(ϖkϖk1)20+Δt22(φk+120φk120)+Δt22(φk+120φk120)=(ϖk+12ϖk+ϖk1,φk+1φk1)+Δt22((φk+1+φk1),(φk+1φk1))+Δt22(φk+1+φk1,φk+1φk1)=Δt22(f(ϖk+1)+f(ϖk1),φk+1φk1)cΔt(ϖk+1ϖk20+ϖkϖk120)+cΔt3(φk+120+φk120),1kK1. (2.12)

    By summing (2.12) from 1 to k (kK1) and using the third equation of (2.4), we obtain

    (ϖk+1ϖk)20+Δt22(φk+120+φk20)+Δt22(φk+120+φk20)cΔtkj=0ϖj+1ϖk20+cΔt3kj=0φj+121+cΔt2(ϖ021+ϖ121),1kK1. (2.13)

    When Δt is adequately small satisfying cΔt21/4, by simplifying (2.13), we obtain

    (ϖk+1ϖk)20+Δt2φk+120+Δt2φk+120cΔtk1j=0ϖj+1ϖk20+cΔt3k1j=0φj+121+cΔt2(ϖ021+ϖ121),1kK1. (2.14)

    By applying Gronwall's inequality (see [5, Lemme 3.1.9]) to (2.14), we obtain

    (ϖk+1ϖk)20+Δt2φk+120+Δt2φk+120cΔt2(ϖ021+ϖ121)exp(ckΔt),1kK1. (2.15)

    Thereupon, we obtain

    φk+10+φk+10c(ϖ01+ϖ11),1kK1. (2.16)

    Thus, when

    ϖ0=ϖ1=0,

    by (2.11) and (2.16), we obtain

    φk=ϖk=0.

    This signifies that Problem 3 has at least one series of solutions {ϖk,φk}Nk=1.

    If Problem 3 has another series of solutions {˜ϖk,˜φk}Nk=1, it should satisfy the following system of equations:

    {1Δt(˜ϖk+12˜ϖk+˜ϖk1,υ)+12((˜φk+1+˜φk1),υ)+12(˜φk+1+˜φk1,υ)=12(f(˜ϖk+1)+f(˜ϖk1),υ),υW,1kK1,(˜ϖk,ϑ)=(˜φk,ϑ),ϑW,0kK,˜ϖ0=ϖ0,˜φ0=Δϖ0,˜ϖ1=ϖ1,˜φ1=φ0ΔtΔϖ1,inΩ. (2.17)

    Let

    Ek=ϖk˜ϖkandek=φk˜φk.

    Subtracting (2.17) from (2.4) yields

    {1Δt(Ek+12Ek+Ek1,υ)+12((ek+1+ek1),υ)+12(ek+1+ek1,υ)=12(f(ϖk+1)+f(ϖk1)f(˜ϖk+1)f(˜ϖk1),υ),υW,1kK1,(Ek,ϑ)=(ek,ϑ),ϑW,0kK,E0=E1=0,e0=e1=0,inΩ. (2.18)

    Taking

    υ=EkEk1

    in the first equation of (2.18), by the second equation of (2.18), the Hölder and Cauchy inequalities, and the LDMF, we obtain

    2(Ek+1Ek20EkEk120)+Δt2(ek+120ek120)+Δt2(Ek+120Ek120)=Δt2(f(ϖk+1)f(˜ϖk+1)+f(ϖk1)f(˜ϖk1),Ek+1Ek1)=Δt2(Ek+1f(ξk)+Ek1f(ξk1),Ek+1Ek1)cΔt2(Ek+1Ek20+EkEk120),1kK1, (2.19)

    where ξi lies between ϖi and ˜wi (i=k,k1).

    Summing (2.19) from 1 to k (kK1) and noting that

    E1=e1=E0=e0=0,

    we obtain

    2Ek+1Ek20+Δt2(ek+120+ek20)+Δt2(Ek+120+Ek20)cΔt2ki=0Ei+1Ei20,1kK1. (2.20)

    When Δt is adequately small, satisfying cΔt21, by simplifying (2.20), we obtain

    Ek+1Ek20+Δt2ek+120+Δt2Ek+120cΔt2k1i=0Ei+1Ei20,1kK1. (2.21)

    By applying Gronwall's inequality to (2.21), we obtain

    Ek+1Ek20+Δt2ek+120+Δt2Ek+1200,1kK1. (2.22)

    Thereupon, we obtain

    ˜ϖk=˜ϖkandφk=φk(1kK).

    Hence, Problem 3 has a unique series of solutions {ϖk,φk}Kk=1.

    (2) Discuss the boundness, i.e., stability of solutions {ϖk,φk}Kk=1 of Problem 3.

    When Problem 3 has a unique series of {ϖk,φk}Kk=1, by (2.11) and (2.16), we claim that it is bounded, i.e., stable, namely (2.5) holds.

    (3) Estimate the errors of solutions {ϖk,φk}Kk=1 of Problem 3.

    Via the Taylor expansion, we obtain

    v(tk+1)=v(tk)+Δtv(tk)+Δt22v(tk)+Δt36v(tk)+Δt424v(tk)+, (2.23)
    v(tk1)=v(tk)Δtv(tk)+Δt22v(tk)Δt36v(tk)+Δt424v(tk)+, (2.24)
    f(v(tk+1))=f(v(tk))+[v(tk+1)v(tk)]f(v(tk))+12(v(tk+1)v(tk))2f(v(tk))+, (2.25)
    f(v(tk1))=f(v(tk))+[v(tk1)v(tk)]f(v(tk))+12(v(tk1)v(tk))2f(v(tk))+. (2.26)

    Therefore, we obtain

    ϖ(tk)=ϖ(tk+1)2ϖ(tk)+ϖ(tk1)Δt2+Δt224ϖ(ηk),tk1ζktk+1, (2.27)
    φ(tk)=φ(tk+1)+φ(tk1)2Δt2φ(ςk),tk1ςktk+1, (2.28)
    f(ϖ(tk))=f(ϖ(tk+1))+f(ϖ(tk1))2Δt2R(x,t), (2.29)

    where R(x,t) is a bounded remainder function, which is obtained by (2.23)–(2.26).

    Thereupon, subtracting the first equation of (2.4) from the first equation of (2.1) after taking t=tk and setting

    ϱk=ϖ(x,tk)ϖkand˜ϱk=φ(x,tk)φk,

    we obtain the following system of error equations:

    1Δt2(ϱk+12ϱk+ϱk1,υ)+12((˜ϱk+1+˜ϱk1),υ)+12(˜ϱk+1+˜ϱk1,υ)=12(f(ϖ(tk+1))f(ϖk+1)+f(ϖ(tk1))f(ϖk1),υ)+Δt2(R(x,t),υ),υW,1kK1, (2.30)
    (ϱk,ϑ)=(˜ϱk,ϑ),ϑW,0kK, (2.31)
    ϱ0=ϱ1=˜ϱ0=˜ϱ1=0, (2.32)

    where ˜R(x,t) is also a bounded remainder function, which is determined by substituting (2.27)–(2.29) into (2.1).

    Taking

    υ=ϱk+1ϱk1

    in (2.30) and using Eq (2.31), the Hölder and Cauchy inequalities, Green's formula, and the LDMF, we obtain

    ϱk+1ϱk20ϱkϱk120+Δt22(˜ϱk+120˜ϱk120)+Δt22(ϱk+120ϱk120)=Δt22(f(ϖ(tk+1))f(ϖk+1)+f(ϖ(tk1))f(ϖk1),ϱk+1ϱk1)+Δt4(R(x,t),ϱk+1ϱk1)cΔt(ϱk+1ϱk20+ϱkϱk120)+cΔt7,1kK1. (2.33)

    Summing (2.33) from 1 to k (kK1), and noting that

    ϱ0=ϱ1=˜ϱ0=˜ϱ1=0,

    we get

    ϱk+1ϱk20+Δt22(˜ϱk+120+˜ϱk20)+Δt22(ϱk+120+ϱk20)cΔtki=0ϱi+1ϱi20+ckΔt7,1kK1. (2.34)

    Thus, when Δt is adequately small, satisfying cΔt1/4, by simplifying (2.34), we get

    ϱk+1ϱk20+Δt2˜ϱk+120+Δt2ϱk+120cΔtk1i=0ϱi+1ϱi20+cΔt6,1kK1. (2.35)

    By applying Gronwall's inequality to (2.35), we obtain

    ϱk+1ϱk20+Δt2˜ϱk+120+Δt2ϱk+120cΔt6exp(ckΔt)cΔt6,1kK1. (2.36)

    Thereupon, we obtain

    φ(tk)φk0+(ϖ(tk)ϖk)0cΔt2,1kK. (2.37)

    Further, by (2.30) and (2.31), the Hölder and Cauchy inequalities, and the LDMF, we obtain

    2((˜ρk+1˜ρk)20(˜ρk˜ρk1)20)+Δt2(˜ρk+120˜ρk120)+Δt2(˜ρk+120˜ρk120)=(ρk+12ρk+ρk1,˜ρk+1˜ρk1)+Δt2((˜ρk+1+˜ρk1),(˜ρk+1˜ρk1))+Δt2(˜ρk+1+˜ρk1,˜ρk+1˜ρk1)=Δt2(f(ϖ(tk+1))f(ϖk+1)+f(ϖ(tk1))f(ϖk1),˜ρk+1˜ρk1)+Δt4(R(x,t),˜ρk+1˜ρk1)cΔt((˜ρk+1˜ρk)20+(˜ρk˜ρk1)20)+Δt3(˜ρk+120+˜ρk120)+cΔt7,1kK1. (2.38)

    By summing (2.38) from 1 to k (kK1) and noting that

    ϱ0=ϱ1=˜ϱ0=˜ϱ1=0,

    we obtain

    2(˜ρk+1˜ρk)20+Δt2(˜ρk+120+˜ρk20)+Δt2(˜ρk+120+˜ρk20)cΔtkj=0(˜ρj+1˜ρj)20+cΔt3kj=0˜ρj+120+ckΔt7,1kK1. (2.39)

    Thus, when Δt is adequately small, satisfying cΔt1/2, by simplifying (2.39), we get

    (˜ρk+1˜ρk)20+Δt2˜ρk+120+Δt2˜ρk+120cΔtk1j=0(˜ρj+1˜ρj)20+cΔt3k1j=0˜ρj+120+cΔt6,1kK1. (2.40)

    By applying Gronwall's inequality to (2.40), we obtain

    (˜ρk+1˜ρk)20+Δt2˜ρk+120+Δt2˜ρk+120cΔt6exp(ckΔt)cΔt6,1kK1. (2.41)

    Thereupon, we obtain

    (φ(tk)φk)0+φ(tk)φk0cΔt4,1kK1. (2.42)

    Combining (2.37) with (2.42) yields (2.6). Theorem 1 is proved.

    Remark 1. Theorem 1 shows that the TSDMCN solutions are stable and their H1 norm error estimates can reach second-order accuracy, which is the optimal order error estimates.

    In order to construct the TGCNMFE format, it is necessary further to discretize the spatial variables in Problem 3 by using the two-grid MFE method. To this end, we assume that H is a coarse grid of quasi-uniform partition on ˉΩ, which is formed by two-dimensional triangles or quadrangles and three-dimensional tetrahedrons or hexahedrons, and H denotes the maximum diameter of all elements in H. Thus, the FE space defined on the coarse grids is expressed by

    WH={vHC(ˉΩ)W:vH|EPl(E),EH},

    where Pl(E) (l1) denotes the space of polynomials with degree l defined on the coarse grid element EH.

    Further, we assume that h is a fine grid of quasi-uniform partition on ˉΩ and h denotes the maximum diameter of all elements in h (hH). Likewise, the FE space defined on the fine grids h is denoted by

    Wh={vhC(ˉΩ)W:vh|ePl(e),eh}.

    Thereupon, a new TGCNMFE formulation can be created as follows.

    Problem 4. Step 1. Find

    (ϖkH,φkH)WH×WH(1kK)

    defined on the coarse grid H, satisfying the nonlinear system of equations:

    {(ϖk+1H2ϖkH+ϖk1H,υH)+Δt22((φk+1H+φk1H),υH)+Δt22(φk+1H+φk1H,υH)=Δt2(f(ϖk+1H)+f(ϖk1H),υH),υHWH,1kK1,(ϖkH,ϑH)=(φkH,ϑH),ϑHWH,0kK,ϖ0H=RHϖ0,ϖ1H=RHϖ1,φ0H=RHφ0,φ1H=RHφ1,inΩ. (3.1)

    Step 2. Find

    (ϖkh,φkh)Wh×Wh(1kK)

    defined on the fine grid h, satisfying the linear system of equations:

    {(ϖk+1h2ϖkh+ϖk1h,υh)+Δt2((φk+1h+φk1h),υh)+Δt2(φk+1h+φk1h,υh)=Δt2(f(ϖk+1H)+f(ϖk+1H)(ϖk+1hϖk+1H)+f(ϖk1h),υh),υhWh,1kK1,(ϖkh,ϑh)=(φkh,ϑh),ϑhWh,0kK,ϖ0h=Rhϖ0,ϖ1h=Rhϖ1,φ0h=Rhφ0,φ1h=Rhφ1,inΩ. (3.2)

    The above operators Rδ: WWδ (δ=H,h) denote the Ritz projection; i.e., for any φW, there exist two unique RδφWδ satisfying

    ((φRδφ),ϑδ)=0,ϑδWδ,δ=H,h, (3.3)

    and the following error estimates:

    |φRδφ|rCδl+1r,ifφWHl+1(Ω),δ=H,h,r=1,0,1. (3.4)

    For Problem 4, we obtain the following results:

    Theorem 2. Problem 4 has a unique set of solutions

    {(ϖkH,φkH)}Kk=1WH×WH

    defined on the coarse grid H and a unique set of solutions

    {(ϖkh,φkh)}Kk=1Wh×Wh

    defined on the fine grid h, respectively, meeting the following unconditional boundness, i.e., unconditional stability:

    ϖkH1+ϖkh1+φkH0+φkh0c(ϖ01+ϖ11),1kK. (3.5)

    The c that appears here and after is also a positive constant independent of H, h, and Δt. Further, when

    h=O(H1+1/l),

    they meet the following error estimates:

    ϖ(tk)ϖkH0+φ(tk)φkH0+H(ϖ(tk)ϖkH)0+H(φ(tk)φkH)0c(Δt2+Hl+1), (3.6)
    ϖ(tk)ϖkh0+φ(tk)φkh0+h(ϖ(tk)ϖkh)0+h(φ(tk)φkh)0c(Δt2+hl+1), (3.7)

    where 1kK.

    Proof. The demonstration of Theorem 2 consists of the following two parts:

    (1) Prove the existence and unconditional stability of TGCNMFE solutions.

    (ⅰ) Consider the existence and unconditional stability of the TGCNMFE solutions defined on the coarse grid H.

    Noting that the system of Eq (3.1) has the same form as the system of Eq (2.4), by using the same approach as proving Theorem 2, we can demonstrate that the nonlinear system of Eq (3.1) has a unique set of solutions

    {(ϖkH,φkH)}Kk=1WH×WH,

    satisfying

    ϖkH0+φkH0c(ϖ01+ϖ11),1kK. (3.8)

    (ⅱ) Consider the existence and unconditional stability of the TGCNMFE solutions defined on the fine grid h.

    Let

    A((ϖ,φ),(ϑ,υ))=(ϖ,υ)(φ,ϑ)+(ϖ,ϑ)+Δt22(φ,υ)Δt22(f(ϖk+1H)ϖ,υ)+Δt22(φ,υ),F(υ,ϑ)=(2ϖkhϖk1h,υ)Δt22(φk1h,υ)Δt22(φk1h,υ)+Δt22(f(ϖk+1H)f(ϖk+1H)ϖk+1H+f(ϖk1h),υ).

    The linear system of equations (3.2) can be rewritten into as follows:

    Find

    (ϖkh,φkh)Wh×Wh(1kK)

    satisfying the following linear system of equations:

    {A((ϖk+1h,φk+1h),(ϑh,υh))=F(ϑh,υh),(ϑh,υh)Wh×Wh,1kK1,ϖ0h=Rhϖ0(x),ϖ1h=Rhϖ1(x),φ0h=Rhφ0(x),φ1h=Rhφ1(x),xΩ. (3.9)

    By Poincaré's inequality, we claim that there is a constant θ0>0 such that

    ϑ0ϑ1θ0ϑ0(ϑW=H10(Ω))

    and

    |f(ϖk+1H)|=|cos(ϖk+1H)|1.

    Thereupon, when Δt is adequately small meeting

    Δt2θ0<4,

    there exists a constant

    α0=min{Δt2/2,1Δt2θ0/4}/θ20

    satisfying

    A((ϖ,φ),(ϖ,φ))=(ϖ,φ)(φ,ϖ)+(ϖ,ϖ)+Δt22(φ,φ)+Δt22(φ,φ)Δt22(cos(ϖkH)ϖ,φ)(1Δtθ04)ϖ20+Δt2φ20+Δt2φ20Δt4φ20α0(ϖ,φ)21,(ϖ,φ)Wh×Wh, (3.10)

    where

    (ϖ,φ)1=(ϖ21+φ21)1/2

    is the norm in W×W. Thus, A((ϖ,φ),(ϑ,υ)) is positive definite, and the bilinear functional A((ϖ,φ),(ϑ,υ)) and the linear functional F(υ,ϑ) are evidently bounded in Wh×Wh for given ϖk+1H, ϖkh, ϖk1h, and φk1h. Thereupon, by the Lax-Milgram theorem (see [5, Theorem 1.2.1]), we assert that the linear system of Eq (3.9), namely Step 2 for Problem 4, has a unique set of solutions

    {(ϖkh,φkh)}Kk=1Wh×Wh

    satisfying

    ϖkh0+φkh0c(ϖ01+ϖ11),1kK. (3.11)

    This signifies that the series of solutions

    {(ϖkh,φkh)}Kk=1Wh×Wh

    for Problem 4 defined on the fine grid h is unconditionally bounded, namely it is unconditionally stable. Combining (3.8) with (3.11) yields (3.5).

    (2) Estimate the errors of the TGCNMFE solutions of Problem 4.

    (a) Estimate the errors of the solutions {(ϖkH,φkH)}Kk=1 of Problem 4 defined on H.

    By subtracting (3.1) from (2.4), and taking

    υ=υHandϑ=ϑH,

    as well as setting

    EkH=ϖkϖkH,ρkH=ϖkRHϖk,ϱkH=RHϖkϖkH,˜EkH=φkφkH,˜ρkH=φkRHφk

    and

    ˜ϱkH=RHφkφkH,

    we obtain

    1Δt2(Ek+1H2EkH+Ek1H,υH)+12((˜Ek+1H+˜Ek1H),υH)+12(˜Ek+1H+˜Ek1H,υH)=12(f(ϖk+1)f(ϖk+1H)+f(ϖk1)f(ϖk1H),υH),υHWH,1kK1, (3.12)
    (EkH,ϑH)=(˜EkH,ϑH),ϑHWH,1kK, (3.13)
    E0H=ϖ0RHϖ0,E1H=ϖ1RHϖ1,˜E0H=φ0RHφ0,˜E1H=φ1RHφ1. (3.14)

    By (3.2)–(3.4), (3.12), (3.13), Taylor's formula, LDMF, and the Hölder and Cauchy inequalities, when

    h=O(H1+1/l),

    we obtain

    1Δt2((Ek+1HEkH)20(EkHEk1H)20)+12(˜Ek+1H20˜Ek1H20)+12(˜Ek+1H20˜Ek1H20)=1Δt2((ρk+1H2ρkH+ρk1H),(ρk+1Hρk1H))+1Δt2(˜Ek+1H2˜EkH+˜Ek1H,ϱk+1Hϱk1H)+12((˜ρk+1H+˜ρk1H),(˜ρk+1H˜ρk1H))+12((˜Ek+1H+˜Ek1H),(˜ϱk+1H˜ϱk1H))+12(˜Ek+1H+˜Ek1H,˜ρk+1H˜ρk1H)+12(˜Ek+1H+˜Ek1H,˜ϱk+1H˜ϱk1H)=1Δt2((ρk+1H2ρkH+ρk1H),(ρk+1Hρk1H))+12((˜ρk+1H+˜ρk1H),(˜ρk+1H˜ρk1H))+12(˜Ek+1H+˜Ek1H,˜ρk+1H˜ρk1H)+12(f(ϖk+1)f(ϖk+1H)+f(ϖk1)f(ϖk1H),˜ϱk+1H˜ϱk1H)1Δt((Ek+1HEkH)20+(EkHEk1H)20)+cΔtH2l+cΔt(˜Ek+1H20+˜Ek1H20),1kK1. (3.15)

    By summing (3.15) from 1 to k (kK1), and using (3.4) and (3.14), we obtain

    1Δt2(Ek+1HEkH)20+12(˜Ek+1H20+˜EkH20)+12(˜Ek+1H20+˜EkH20)cΔtki=0(Ei+1HEiH)20+cH2l+cΔtki=0˜Ei+1H20,1kK1. (3.16)

    Thus, when Δt is adequately small, satisfying cΔt1/4, by simplifying (3.16), we get

    1Δt2(Ek+1HEkH)20+˜Ek+1H20+˜Ek+1H0cΔtk1i=0(Ei+1HEiH)20+cH2l+cΔtk1i=0˜Ei+1H20,1kK1. (3.17)

    By applying Gronwall's inequality to (3.17), we obtain

    1Δt2(Ek+1HEkH)20+˜Ek+1H20+˜Ek+1H20cH2lexp(ckΔt),1kK1. (3.18)

    Thereupon, we obtain

    ˜EkH0+˜EkH0cHl,1kK. (3.19)

    By the Nitsche technique (see [5, Theorem 1.3.9]) and (3.19), we immediately obtain the following error estimates:

    φkφkH0+H(φkφkH)0cHl+1,1kK. (3.20)

    Further, by (3.2), (3.3), (3.12), (3.13), Taylor's formula, the LDMF, the Hölder and Cauchy inequalities, we obtain

    1Δt2(Ek+1HEkH20EkHEk1H20)+12(˜Ek+1H20˜Ek1H20)+12(Ek+1H20Ek1H20)=1Δt2(Ek+1H2EkH+Ek1H,ρk+1Hρk1H)+1Δt(Ek+1H2EkH+Ek1H,ϱk+1Hϱk1H)+12(˜Ek+1H+˜Ek1H,˜ρk+1H˜ρk1H)+12((ρkH+ρk1H),(ρk+1Hρk1H))+12(˜Ek+1H+˜Ek1H,˜ϱk+1H˜ϱk1H)+12((EkH+Ek1H),(ϱk+1Hϱk1H))=1Δt2(Ek+1H2EkH+Ek1H,ρk+1Hρk1H)+12((ρkH+ρk1H),(ρk+1Hρk1H))+12((ρkH+ρk1H),(ρk+1Hρk1H))+12(f(ϖk)f(ϖkH)+f(ϖk1)f(ϖk1H),ϱkHϱk1H)cΔt(Ek+1HEkH20+EkHEk1H20)+cΔtH2l+cΔt(˜Ek+1H20+˜Ek1H20),1kK1. (3.21)

    By summing (3.21) from 1 to k, and using (3.4) and (3.14), we obtain

    1Δt2Ek+1HEkH20+12(˜Ek+1H20+˜EkH20)+12(Ek+1H20+EkH20)cΔtki=0Ei+1HEiH20+cH2l+cΔtki=0˜Ei+1H20,1kK1. (3.22)

    Thus, when Δt is adequately small, satisfying cΔt1/4, by simplifying (3.22), we get

    1Δt2Ek+1HEkH20+˜Ek+1H20+Ek+1H20cΔtk1i=0Ei+1HEiH20+cH2l+cΔtk1i=0˜Ei+1H20,1kK1. (3.23)

    By applying Gronwall's inequality to (3.23), we obtain

    1Δt2Ek+1HEkH20+˜Ek+1H20+Ek+1H20cH2lexp(ckΔt),1kK1. (3.24)

    Thereupon, we obtain

    (ϖkϖkH)0cHl,1kK. (3.25)

    Further, by the Nitsche technique, we can obtain the following error estimates:

    ϖkϖkH0+H(ϖkϖkH)0cHl+1,1kK. (3.26)

    Combining (3.20) and (3.26) with Theorem 1 yields (3.6).

    (b) Estimate the errors of solutions (ϖkh,φkh) (1kK) of Problem 4 defined on the fine grid h.

    Subtracting (3.2) from (2.4), taking

    υ=υhandϑ=ϑh,

    and setting

    Ekh=ϖkϖkh,ρkh=ϖkRhϖk,ϱkh=Rhϖkϖkh,˜Ekh=φkφkh,˜ρkh=φkRhφk

    and

    ˜ϱkh=Rhφkφkh,

    we obtain

    1Δt2(Ek+1h2Ekh+Ek1h,υh)+12((˜Ek+h+˜Ek1h),υh)+12(˜Ek+1h+˜Ek1h,υh)=12(f(ϖk+1)f(ϖk+1H)+f(ϖk1)f(ϖk1h)f(ϖk+1H)(ϖkhk+1ϖk+1H),υh),υhWh,1kK1, (3.27)
    (Ekh,ϑh)=(˜Ekh,ϑh),ϑHWh,1kK, (3.28)
    E0h=ϖ0Rhϖ0,E1h=ϖ1Rhϖ1,˜E0h=φ0Rhφ0,˜E1h=φ1Rhφ1. (3.29)

    By (3.3), (3.4), (3.27), (3.28), Taylor's formula, the LDMF, the Hölder and Cauchy inequalities, and (3.6) or (3.26), when

    h=O(H1+1/l),

    we obtain

    1Δt2((Ek+1hEkh)20(EkhEk1h)20)+12(˜Ek+1h20˜Ek1h20)+12(˜Ek+1h20˜Ek1h20)=1Δt2((ρk+1h2ρkh+ρk1h),(ρk+1hρk1h))+12((˜ρk+1h+˜ρk1h),(˜ρkh˜ρk1h))+12(˜Ek+1h+˜Ek1h,˜ρk+1h˜ρk1h)+1Δt2(˜Ek+1h2˜Ekh+˜Ek1h,ϱk+1hϱk1h)+12((˜Ek+1h+˜Ek1h),(˜ϱk+1h˜ϱk1h))+12((˜Ekh+˜Ek1h),(˜ϱk+1h˜ϱk1h))=1Δt2((ρk+1h2ρkh+ρk1h),(ρk+1hρk1h))+12((˜ρk+1h+˜ρk1h),(˜ρkh˜ρk1h))+12(˜Ek+1h+˜Ek1h,˜ρk+1h˜ρk1h)12(f(ϖk+1H)(ϖk+1hϖk+1H),˜ϱk+1h˜ϱk1h)+12(f(ϖk+1)f(ϖk+1H)+f(ϖk1)f(ϖk1h),˜ϱk+1h˜ϱk1h)2Δt((Ek+1hEkh)20+(EkhEk1h)20)+cΔth2l+cΔt(˜Ek+1h20+˜Ek1h20),1kK1. (3.30)

    By summing (3.30) from 1 to k (kK1), and using (3.4) and (3.29), we obtain

    1Δt2(Ek+1hEkh)20+12(˜Ek+1h20+˜Ekh20)+12(˜Ek+1h20+˜Ekh20)2Δtki=0(Ei+1hEkh)20+cH2l+2+cΔtki=0˜Ei+1h20,1kK1. (3.31)

    Thus, when Δt is adequately small, satisfying cΔt1/4, by simplifying (3.31), we obtain

    1Δt2(Ek+1hEkh)20+˜Ek+1h20+˜Ek+1h202Δtk1i=0(Ei+1hEkh)20+cH2l+2+cΔtk1i=0˜Ei+1h20,1kK1. (3.32)

    By applying Gronwall's inequality to (3.32), we obtain

    1Δt2(Ek+1hEkh)20+˜Ek+1h20+˜Ek+1h20ch2lexp(ckΔt)ch2l,1kK1. (3.33)

    Thereupon, we obtain

    (φkφkh)0chl,1kK. (3.34)

    By the Nitsche technique (see [5, Theorem 1.3.9]), we easily obtain the following error estimates:

    φkφkh0+h(φkφkh)0chl+1,1kK. (3.35)

    Further, by (3.3), (3.27), (3.28), Taylor's formula, the LDMF, the Hölder and Cauchy inequalities, and (3.6) or (3.26), we get

    1Δt2(Ek+1hEkh20EkhEk1h20)+12(˜Ek+1h20˜Ek1h20)+12(Ek+1h20Ek1h20)=1Δt2(Ek+1h2Ekh+Ek1h,ρk+1hρk1h)+12(˜Ek+1h+˜Ek1h,˜ρk+1h˜ρk1h)+12((ρkh+ρk1h),(ρk+1hρk1h))+1Δt2(Ek+1h2Ekh+Ek1h,ϱk+1hϱk1h)+12(˜Ek+1h+˜Ek1h,˜ϱk+1h˜ϱk1h)+12((Ek+1h+Ek1h),(ϱk+1hϱk1h))=1Δt2(Ek+1h2Ekh+Ek1h,ρk+1hρk1h)+12(˜Ek+1h+˜Ek1h,˜ρk+1h˜ρk1h)+12((ρkh+ρk1h),(ρk+1hρk1h))12(f(ϖk+1H)(ϖk+1hϖk+1H),ϱk+1hϱk1h)+12(f(ϖk+1)f(ϖk+1H)+f(ϖk1)f(ϖk1h),ϱk+1hϱk1h)cΔt(Ek+1HEkH20+EkHEk1H20)+cΔth2l+cΔt(˜Ek+1h20+˜Ek1h20),1kK1. (3.36)

    By summing (3.36) from 1 to k (kK1), and using (3.4) and (3.29), we obtain

    1Δt2Ek+1hEkh20+12(˜Ek+1h20+˜Ekh20)+12(Ek+1h20+Ekh20)cΔtki=0(Ei+1hEkh)20+cH2l+2+cΔtki=0˜Ei+1h20,1kK1. (3.37)

    Thus, when Δt is adequately small, satisfying cΔt1/4, by simplifying (3.37), we obtain

    1Δt2(Ek+1hEkh)20+Ek+1h20+˜Ek+1h20cΔtk1i=0(Ei+1hEkh)20+cH2l+2+cΔtk1i=0˜Ei+1h20,1kK1. (3.38)

    By applying Gronwall's inequality to (3.38), we obtain

    1Δt2(Ek+1hEkh)20+Ek+1h20+˜Ek+1h20ch2lexp(ckΔt)ch2l,1kK1. (3.39)

    Thereupon, we obtain

    (ϖkϖkh)0chl,1kK. (3.40)

    By the Nitsche technique (see [5, Theorem 1.3.9]), we easily deduce the following error estimates

    ϖkϖkh0+h(ϖkϖkh)0chl+1,1kK. (3.41)

    Thereupon, inequality (3.7) is obtained by combining (3.35) and (3.41) with Theorem 1. This completes the proof for Theorem 2.

    Remark 2. Theorem 2 shows that the TGCNMFE solutions are unconditionally stable and their theoretical errors reach optimal order. In Section 4, we use the numerical tests to verify the correctness of the obtained theoretical error estimates.

    In this section, we provide two sets of numerical experiments to verify the correctness of our theoretical results and show the superiorities of the TGCNMFE method.

    For the two-dimensional case, we take

    ˉΩ=[0,1]×[0,1]R2

    and the initial functions

    ϖ0(x)=ϖ1(x)=4sin(πx1)sin(πx2)

    in the NFOSG equation (i.e., Problem 1), in which it may be considered that there is an earthquake focus at center (0.5,0.5) of the region Ω.

    The fine grid division h is composed of squares with diagonal

    h=2/1000

    and all squares parallel to the coordinate axis. When l=1, in order to satisfy

    h=O(H1+1/l),

    i.e.,

    h=O(H2),

    the coarse grid division H is composed of the squares with diagonal

    H=42/1000

    and all squares also parallel to the coordinate axis. According to Theorem 2, the L2 norm error estimates of the TGCNMFE solutions of the NFOSG equation can theoretically reach O(106) when

    Δt=1/1000.

    We first find the TGCNMFE solutions ϖkh and φkh by the TGCNMFE format at t=10, and their contours are respectively shown in Figures 1a and 2a.

    Figure 1.  (a) The contour of the TGCNMFE solution of ϖ at t=10; (b) The contour of the SGCNMFE solution of ϖ at t=10.
    Figure 2.  (a) The contour of the TGCNMFE solution of φ at t=10; (b) The contour of the SGCNMFE solution of φ at t=10.

    In order to show the advantages of the TGCNMFE format, we also find single-grid CNMFE (SGCNMFE) solutions ˆϖkh and ˆφkh at t=10 by the following SGCNMFE format, and their contours are respectively shown in Figures 1b and 2b.

    Problem 5. Find

    (ˆϖkh,ˆφkh)Wh×Wh(1kK)

    defined on the single fine grid h, satisfying the nonlinear system of equations:

    {(ˆϖk+1h2ˆϖkh+ˆϖk1h,υh)+Δt2((ˆφk+1h+ˆφk1h),υh)+Δt2(ˆφk+1h+ˆφk1h,υh)=Δt2(f(ˆϖk+1h)+f(ˆϖk1h),υh),υhWh,1kK1,(ˆϖkh,ϑh)=(ˆφkh,ϑh),ϑhWh,0kK,ˆϖ0h=Rhϖ0(x),ˆφ0h=Rhφ0,ˆϖ1h=Rhϖ1(x),xΩ. (4.1)

    By comparing the contours of each pair of graphs in Figures 1 and 2, it can be easy to see that the TGCNMFE solutions are very close to the SGCNMFE solutions at t=10.

    To truly showcase the benefits of the TGCNMFE format, we record the CPU running time for finding the TGCNMFE and SGCNMFE solutions and their errors when t=2.0, 4.0, 6.0, 8.0, and 10.0, where errors are estimated respectively by ϖkhϖk1h0+φkhφk1h0 and ˆϖkhˆϖk1h0+ˆφkhˆφk1h0, shown in Table 1.

    Table 1.  The errors of the SGCNMFE and TGCNMFE solutions and CPU running-time at t=2,4,6,8, and 10.
    t SGCNMFE solutions errors TGCNMFE solutions errors SGCNMFE method CPU running-time TGCNMFE method CPU running-time
    2.0 2.2316×106 3.0273×106 215.332 s 112.056 s
    4.0 2.4187×106 3.1438×106 216.662 s 113.112 s
    6.0 2.5665×106 3.2662×106 217.153 s 114.224 s
    8.0 2.7782×106 3.3861×106 218.709 s 115.451 s
    10.0 2.8864×106 3.4861×106 219.618 s 116.872 s

     | Show Table
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    The data in Table 1 show that the numerical errors of TGCNMFE and SGCNMFE solutions reach O(106) when t=2.0, 4.0, 6.0, 8.0, and 10.0, which coincide with the obtained theoretical errors, but the CPU running time for finding SGCNMFE solutions is almost twice as long as that for finding SGCNMFE solutions. Therefore, the TGCNMFE method is visibly superior to the SGCNMFE method, and the TGCNMFE method is feasible and effective to solve the NFOSG equation.

    For the three-dimensional NFOSG equation, we take

    ˉΩ=[0,1]×[0,1]×[0,1]R3

    and the initial functions

    ϖ0(x)=ϖ1(x)=sin(πx1)sin(πx2)sin(πx3),

    where it may be considered that there is an earthquake focus at center (0.5,0.5,0.5) of the region Ω.

    The fine grid division h is composed of cubes with diagonal

    h=3/1000

    and all cubes parallel to the coordinate axis. When l=1, in order to satisfy

    h=O(H1+1/l),

    i.e.,

    h = O(H^{2}),

    the coarse grid division \Im_H is composed of cubes with diagonal

    H = \sqrt[4]{3}/\sqrt{1000}

    and all cubes also parallel to the coordinate axis. According to Theorem 2, the L^2 norm errors of the TGCNMFE solutions of the NFOSG equation can also theoretically reach O(10^{-6}) when

    \Delta t = 1/1000.

    We find the TGCNMFE solutions \varpi_h^k and \varphi_h^k by the TGCNMFE format at t = 1 , and their contours are respectively shown in Figures 3a and 4a.

    Figure 3.  (a) The TGCNMFE solution of \varpi at t = 1 . (b) The SGCNMFE solution of \varpi at t = 1 .
    Figure 4.  (a) The TGCNMFE solution of \varphi at t = 1 . (b) The SGCNMFE solution of \varphi at t = 1 .

    To show that the TGCNMFE method is superior to the SGCNMFE method, we also find the SGCNMFE solutions \hat{\varpi}_h^k and \hat{\varphi}_h^k at t = 1 by the SGCNMFE format above (Problem 5), which are respectively shown in Figures 3b and 4b.

    By comparing the each pair of graphs in Figures 3 and 4, it can also be easy to see that the TGCNMFE solutions are almost same as the SGCNMFE solutions at t = 1 .

    To truly showcase the benefits of the TGCNMFE format, we also record the CPU running time for finding the TGCNMFE and SGCNMFE solutions and their errors when t = 0.2 , 0.4 , 0.6 , 0.8 , and 1.0 , where errors are also respectively estimated by \|\varpi_{h}^{k}-\varpi_{h}^{k-1}\|_0+\|\varphi_{h}^{k}-\varphi_{h}^{k-1}\|_0 and \|\hat{\varpi}_{h}^{k}-\hat{\varpi}_{h}^{k-1}\|_0+\|\hat{\varphi}_{h}^{k}-\hat{\varphi}_{h}^{k-1}\|_0 , shown in Table 2.

    Table 2.  The errors of the SGCNMFE and TGCNMMFE solutions and CPU running-time at t = 0.2, 0.4, 0.6, 0.8 , and 1.0 .
    t SGCNMFE solutions errors TGCNMFE solutions errors SGCNMFE method CPU running-time TGCNMFE method CPU running-time
    0.2 2.5781 \times 10^{-6} 3.1563 \times 10^{-6} 422.562 s 211.731 s
    0.4 2.6436 \times 10^{-6} 3.2253 \times 10^{-6} 424.826 s 212.813 s
    0.6 2.7841 \times 10^{-6} 3.3265 \times 10^{-6} 426.716 s 213.832 s
    0.8 2.8862 \times 10^{-6} 3.4453 \times 10^{-6} 428.261 s 214.764 s
    1.0 2.9631 \times 10^{-6} 3.5626 \times 10^{-6} 429.142 s 215.635 s

     | Show Table
    DownLoad: CSV

    The data in Table 2 also show that when t = 0.2 , 0.4 , 0.6 , 0.8 , and 1.0 , the numerical errors of the SGCNMFE and TGCNMFE solutions coincide with the theoretical errors O(10^{-6}) , but the CPU running time for finding SGCNMFE solutions is also almost twice as long as that for finding SGCNMFE solutions. It is further shown that the TGCNMFE method is indeed better than the SGCNMFE method, and the TGCNMFE method is indeed feasible and effective to solve the NFOSG equation.

    Above, we have proposed a new NFOSG equation, a new TSDMCN scheme, and a new TGCNMFE method for the NFOSG equation, and have strictly proved the existence, stability, and error estimates of the TSDMCN and TGCNMFE solutions theoretically. We have also employed the two sets of numerical experiments to confirm the correctness of the obtained theoretical results and showed the superiorities for the TGCNMFE method. The TSDMCN scheme and the TGCNMFE method for the NFOSG equation are first proposed in this paper. They are completely different from the existing methods in [10,11,12]. Therefore, they are original and indeed fire-new.

    Although we only study the TGCNMFE method for the NFOSG equation, the method of this paper can be extended to the more complex nonlinear PDEs, for example, the nonlinear Cahn-Hilliard equation and the Schrödinger equation in [19,20], in addition to the actual engineering nonlinear problems. Therefore, the TGCNMFE method has a wide range of applications.

    Although the TGCNMFE method here can greatly simplify calculation, save CPU operating-time, and improve computational efficiency, when it is applied to settling practical engineering computations, it usually contains many (often more than tens of millions) unknowns and needs to take a long-time to obtain results on a computer. Thus, after a long computer operating time, owing to the accumulation of computing errors, the obtained TGCNMFE solutions could deviate from right solutions, or could even generate floating-point overflow, resulting in erroneous calculation results. Hence, in future study, we will use a proper orthogonal decomposition method (see [5,21,22]) to lessen the unknowns of the TGCNMFE method and develop some new reduced-dimensionality methods for the NFOSG equation.

    Yanjie Zhou: conceptualization, investigation, methodology, validation, writing-original draft, formal analysis; Xianxiang Leng: conceptualization, methodology, formal analysis, writing-review and editing; Yuejie Li: validation, visualization, writing-review and editing; Qiuxiang Deng: inspection, writing-review and editing; Zhendong Luo: conceptualization, investigation, methodology, formal analysis, writing-original draft, writing-review, editing and proofreading. All authors have read and agreed to the published version of the manuscript.

    This work is jointly supported by the National Natural Science Foundation of China (Nos. 42330801, 42374143 and 11671106) and National Natural Science Foundation Joint project Key fund project cooperation project (No. U1839206).

    The authors declare that they have no conflicts of interest to report regarding the present study.



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