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Multiple soliton solutions and similarity reduction of a (2+1)-dimensional variable-coefficient Korteweg–de Vries system

Yaqing Liu1111Email: [email protected].,    Linyu Peng2222Email: [email protected], corresponding author.
1.1. School of Applied Science, Beijing Information Science and Technology University,
Beijing 100192, China
2.2. Department of Mechanical Engineering, Keio University, Yokohama 223-8522, Japan
Abstract

In this paper, we study the novel nonlinear wave structures of a (2+1)-dimensional variable-coefficient Korteweg–de Vries (KdV) system by its analytic solutions. Its NN-soliton solution are obtained via Hirota’s bilinear method, and in particular, the hybrid solution of lump, breather and line soliton are derived by the long wave limit method. In addition to soliton solutions, similarity reduction, including similarity solutions (also known as group-invariant solutions) and non-autonomous third-order Painlevé equations, is achieved through symmetry analysis. The analytic results, together with illustrative wave interactions, show interesting physical features, that may shed some light on the study of other variable-coefficient nonlinear systems.
Keywords: (2+1)-dimensional variable-coefficient KdV system, Hirota’s bilinear method, soliton solution, symmetry, similarity solution.

1 Introduction

Nonlinear partial differential equations play a crucial role in modeling wave phenomena that arise in various fields, such as fluid mechanics, nonlinear optics, plasma physics, condensed matter physics, etc. Methods for constructing their analytical solutions, that can explicitly describe the dynamical behavior, have attracted much attention, among which there are the Hirota’s bilinear method [18, 21], Darboux transformation [16, 47], the inverse scattering transformation [2, 41], the multiple exp-function method [26], dressing method [29, 22], symmetry method [20, 33, 19, 6, 37], and so on. In the current paper, we will mainly be focused on soliton solutions by Hirota’s bilinear method and similarity solution by symmetry reduction.

Hirota’s bilinear method has been investigated by many scholars (see, e.g., [13, 38]). For integrable nonlinear evolution equations, Hirota’s bilinear method can be used to construct NN-soliton solutions applying the superposition of solutions, and has been extended to obtain breather, lump and their interaction solutions [24], higher-order localized wave [14], rational and semi-rational solution [17]. It was also employed for searching the localized waves of nonlocal evolution equations [48, 49] and variable-coefficient evolution equations [23, 36, 45].

On the other hand, continuous symmetries have also been widely applied to the analysis of differential equations (see, e.g., [7, 34, 35]). They can lead to exact solutions or reductions of differential equations [33, 6], and are closely relevant to their integrability (see, e.g., [30]). In recent years, symmetry analysis of variable-coefficient evolution equations has attracted much attention. For instance, in [32, 31], Mohamed and co-authors investigated lump soliton, solitary waves and exponential solutions of the (3+1) dimensional variable-coefficients Kudryashov–Sinelshchikov equation and the (2+1)-dimensional variable-coefficient Bogoyavlensky–Konopelchenko equation by similarity reduction using their symmetries. In [44], a variable-coefficient Davey–Stewartson system was studied, where the optimal system of symmetries was obtained with adjoint representation. Variable-coefficient Davey–Stewartson system that admits the Kac-Moody-Virasoro symmetry was proposed in [15]. In [46], nonlocal symmetries of the coupled variable-coefficient Newell–Whitehead system were used to calculate its group-invariant solutions. However, few studies have been conduced on the dynamics of higher-order localized waves. In the current paper, we focus on nonlinear wave structures of the following (2+1)-dimensional variable-coefficient Korteweg–de Vries (KdV) system

{ρ(t)ut+3μ(t)(uv)x+σ(t)uxxx=0,ux=vy,\left\{\begin{array}[]{l}\rho(t)u_{t}+3\mu(t)(uv)_{x}+\sigma(t)u_{xxx}=0,\vspace{0.2cm}\\ u_{x}=v_{y},\end{array}\right. (1.1)

and particularly its integrable variant with both μ(t)\mu(t) and σ(t)\sigma(t) constant functions, using both Hirota’s bilinear method and symmetry analysis. Here, uu, vv are the dependent variables and xx, yy and tt are the independent variables. The notations ut=u/tu_{t}=\partial u/\partial t, ux=u/xu_{x}=\partial u/\partial x and so forth are adopted in the current paper. The functions ρ(t)\rho(t), μ(t)\mu(t) and σ(t)\sigma(t) are known but arbitrary functions of tt which are assumed to be smooth enough; when ρ(t)=μ(t)=σ(t)=1\rho(t)=\mu(t)=\sigma(t)=1, the system (1.1) reduces to the constant-coefficient (2+1)-dimensional KdV system [42, 25], derived by Boiti et al. using the weak Lax pair [11]. Furthermore, the system (1.1) reduces to the (1+1)-dimensional KdV equation by setting v=uv=u and x=yx=y.

In Section 2, integrability condition of (1.1) is analyzed by Painlevé analysis and in what follows we will be focused on its integrable version with constant coefficients μ\mu and σ\sigma. In Section 3, NN-soliton solutions and hybrid interaction of line solitons, and breather and lump solitons are obtained through Hirota’s bilinear method, while in Section 4, we invoke the symmetry method to derive Lie point symmetries and obtain the corresponding similarity solutions. In particular, a PDE (see Eq. (4.16) or system (4.14) in the potential form below) passing the Painlevé test is derived by symmetry reduction, that reads

Ur=(a(y)σUrr3μU)y,\displaystyle U_{r}=\left(\frac{a(y)-\sigma U_{rr}}{3\mu U}\right)_{y}, (1.2)

where r,yr,y are the independent variables and UU is the dependent variable, and a(y)a(y) is an arbitrary function. Further symmetry reduction shows that it can be reduced to non-autonomous third-order Painlevé equations, which are in the form of Chazy’s classification of third-order ODEs by Painlevé analysis but not included in Chazy’s 13 classes. The final Section 5 is dedicated to conclusion.

2 Painlevé analysis of the variable-coefficient KdV system

In this section, we study integrability condition of the (2+1)-dimensional variable-coefficient KdV system (1.1) through Painlevé analysis (see, e.g., [40, 43]). Let u=myu=m_{y} and v=mxv=m_{x}, and the system (1.1) becomes

ρ(t)myt+3μ(t)(mxmy)x+σ(t)mxxxy=0,\rho(t)m_{yt}+3\mu(t)(m_{x}m_{y})_{x}+\sigma(t)m_{xxxy}=0, (2.1)

that is assumed to admit a solution as a Laurent expansion about a singular manifold ϕ=ϕ(x,y,t)\phi=\phi(x,y,t) as follows

m(x,y,t)=ϕn(x,y,t)j=0mj(x,y,t)ϕj(x,y,t),n>0.m(x,y,t)=\phi^{-n}(x,y,t)\sum_{j=0}^{\infty}m_{j}(x,y,t){\phi^{j}(x,y,t)},\quad n>0. (2.2)

Here, nn is determined by a leading-term analysis and balancing the dominant terms (mxmy)x(m_{x}m_{y})_{x} and mxxxym_{xxxy}. Straightforward calculation gives n=1n=1 and

m0=2σ(t)μ(t)ϕx.m_{0}=\frac{2\sigma(t)}{\mu(t)}\phi_{x}. (2.3)

Substituting m=m0ϕ1+qϕr1m=m_{0}\phi^{-1}+q\phi^{r-1} back to Eq. (2.2) and balancing the most singular term again, we obtain

q(3μ(t)(4m0(r1)ϕx2ϕy2m0(r1)(r2)ϕx2ϕy)+σ(t)(r1)(r2)(r3)(r4)ϕx3ϕy)=0.q\Big{(}3\mu(t)(4m_{0}(r-1)\phi_{x}^{2}\phi_{y}-2m_{0}(r-1)(r-2)\phi_{x}^{2}\phi_{y})+\sigma(t)(r-1)(r-2)(r-3)(r-4)\phi_{x}^{3}\phi_{y}\Big{)}=0. (2.4)

Combining Eqs. (2.3) and (2.4), qq is arbitrary when r=1,1,4r=-1,1,4 and 66, which are the resonant points. Substitution of (2.2) into Eq. (2.1) then amounts to the recursion relations for the mjm_{j}, which take the form of coupled partial differential equations. Finally, we observe that explicit expressions for m2m_{2}, m3m_{3} and m5m_{5} and compatibility condition to ensure integrability requires μ(t)=μ\mu(t)=\mu, σ(t)=σ\sigma(t)=\sigma to be non-zero constants, but ρ(t)\rho(t) remains to be an arbitrary function of tt. Consequently, m1m_{1}, m4m_{4} and m6m_{6} are arbitrary functions.

To summarize up, we conclude that the following special (2+1)-dimensional time-dependent variable-coefficient KdV system

{ρ(t)ut+3μ(uv)x+σuxxx=0,ux=vy,\left\{\begin{array}[]{l}\rho(t)u_{t}+3\mu(uv)_{x}+\sigma u_{xxx}=0,\vspace{0.2cm}\\ u_{x}=v_{y},\end{array}\right. (2.5)

is integrable as passes the Painlevé test, where μ\mu and σ\sigma are constants. In the rest of the paper, we will be focused on studies of analytic solutions of the integrable system (2.5).

3 Bilinear representation and NN-solitons

The integrable (2+1)-dimensional time-dependent variable-coefficient KdV system (2.5) can be written in bilinear form

(ρ(t)DyDt+σDx3Dy+3αμDx2+3βμDxDy)ff=0\Big{(}\rho(t)D_{y}D_{t}+\sigma D_{x}^{3}D_{y}+3\alpha\mu D_{x}^{2}+3\beta\mu D_{x}D_{y}\Big{)}f\cdot f=0 (3.1)

by the transformation

{u=α+2σμ(log(f))xy,v=β+2σμ(log(f))xx,\left\{\begin{array}[]{l}u=\alpha+\frac{2\sigma}{\mu}\big{(}{\rm log}(f)\big{)}_{xy},\vspace{0.2cm}\\ v=\beta+\frac{2\sigma}{\mu}\big{(}{\rm log}(f)\big{)}_{xx},\\ \end{array}\right. (3.2)

where both α\alpha and β\beta are real-valued parameters, and Hirota’s bilinear differential operators are defined by

DxmDynDtsab=(xx)m(yy)n(tt)sa(x,y,t)b(x,y,t)|x=x,y=y,t=t.\displaystyle{}D_{x}^{m}D_{y}^{n}D_{t}^{s}a\cdot b=(\partial_{x}-\partial_{x^{\prime}})^{m}(\partial_{y}-\partial_{y^{\prime}})^{n}(\partial_{t}-\partial_{t^{\prime}})^{s}a(x,y,t)b(x^{\prime},y^{\prime},t^{\prime})|_{x=x^{\prime},y=y^{\prime},t=t^{\prime}}. (3.3)

The function ff can have the general form as

fN=ς=0,1exp(j=1Nςjθj+1s<jNςsςjAsj),N=1,2,,\displaystyle{}f_{N}=\sum_{\varsigma=0,1}\exp\left(\sum_{j=1}^{N}\varsigma_{j}\theta_{j}+\sum_{1\leq s<j}^{N}\varsigma_{s}\varsigma_{j}A_{sj}\right),\quad N=1,2,\ldots, (3.4)

where

θj=kjx+pjyωj(t)+θ0j with ωj(t)=σkj3pj+3βμkjpj+3αμkj2pjρ(t)𝑑t\displaystyle{}\theta_{j}=k_{{j}}x+p_{{j}}y-\omega_{j}(t)+\theta_{0j}\text{ with }\omega_{j}(t)=\int\frac{\sigma k_{j}^{3}p_{j}+3\beta\mu k_{j}p_{j}+3\alpha\mu k_{j}^{2}}{p_{j}\rho(t)}dt (3.5)

for j=1,2,,Nj=1,2,\ldots,N, and

exp(Asj)=σkskj(kskj)(pspj)pspjαμ(kjpskspj)2σkskj(ks+kj)(ps+pj)pspjαμ(kjpskspj)2,1s<jN.\displaystyle{}\exp(A_{sj})=\frac{\sigma k_{s}k_{j}(k_{s}-k_{j})(p_{s}-p_{j})p_{s}p_{j}-\alpha\mu(k_{j}p_{s}-k_{s}p_{j})^{2}}{\sigma k_{s}k_{j}(k_{s}+k_{j})(p_{s}+p_{j})p_{s}p_{j}-\alpha\mu(k_{j}p_{s}-k_{s}p_{j})^{2}},~{}~{}1\leq s<j\leq N. (3.6)

Here, kj,pj,θ0jk_{j},p_{j},\theta_{0j} are arbitrary constants.

Substituting the function ff in (3.4) and (3.5)-(3.6) into the transformation in (3.2), the NN-solitons of the (2+1)-dimensional time-dependent variable-coefficient KdV system (2.5) can be constructed explicitly.

Two-soliton solution. When N=2N=2, Eq. (3.4) reads

f2=1+exp(θ1)+exp(θ2)+exp(θ1+θ2+A12),\displaystyle{}f_{2}=1+\exp(\theta_{1})+\exp(\theta_{2})+\exp(\theta_{1}+\theta_{2}+A_{12}), (3.7)

and the two-solitons of Eq. (2.5) can be obtained via (3.2). This covers the results of [12] by specifying σ=1,μ=1\sigma=1,\ \ \mu=1 and ρ(t)1\rho(t)\equiv 1. In the following, we always take σ=1,μ=1\sigma=1,\ \ \mu=1 and consider various functions ρ(t)\rho(t). Fig. 1 shows the two-soliton solution with ρ(t)1\rho(t)\equiv 1. The interacting line solitons form H-type and X-type, which were observed in ocean waves [1]. Both H-type and X-type interaction with long stem, the wave form uu have similar structure, while for vv, the stem of H-type has a lower amplitude and X-type has the opposite result.

Refer to caption
Figure 1: Two-soliton solution given by (3.7) at t=0t=0. Top: 3d plots of uu and vv versus bottom: corresponding density. (a1) (a2) (b1) (b2) H-type interaction with parameters k1=0.2,k2=0.3,p1=0.3,p2=0.5,α=0.02,β=1k_{1}=0.2,k_{2}=0.3,p_{1}=0.3,p_{2}=-0.5,\alpha=0.02,\beta=1, and hence eA12=5.6×109e^{A_{12}}=5.6\times 10^{-9}. (c1) (c2) (d1) (d2) X-type interaction with parameters k1=0.2,k2=0.3,p1=0.3,p2=0.5,α=0.025,β=1k_{1}=0.2,k_{2}=0.3,p_{1}=0.3,p_{2}=-0.5,\alpha=0.025,\beta=1, and hence eA12=6×108e^{A_{12}}=6\times 10^{8}.

Three-soliton solution. When N=3N=3, Eq. (3.4) becomes

f3=1+exp(θ1)+exp(θ2)+exp(θ3)+exp(θ1+θ2+A12)+exp(θ1+θ3+A13)+exp(θ2+θ3+A23)+exp(θ1+θ2+θ3+A123),\displaystyle{}\begin{split}f_{3}&=1+\exp(\theta_{1})+\exp(\theta_{2})+\exp(\theta_{3})+\exp(\theta_{1}+\theta_{2}+A_{12})\\ &\quad+\exp(\theta_{1}+\theta_{3}+A_{13})+\exp(\theta_{2}+\theta_{3}+A_{23})+\exp(\theta_{1}+\theta_{2}+\theta_{3}+A_{123}),\end{split} (3.8)

where A123=A12A13A23A_{123}=A_{12}A_{13}A_{23}. Substituting f3f_{3}, i.e., Eq. (3.8), to (3.2), three-soliton solution can be obtained. Fig. 2 shows novel wave structure with respect to various variable coefficients ρ(t)\rho(t). Top and bottom of the figure illustrate the 3d plots of uu and vv, respectively. Figs. 2 (a1)-(d2) are plotted with the same parameters α=0.5,β=0.5\alpha=-0.5,\beta=-0.5, k1=1,k2=2,k3=2,p1=2,p2=2k_{1}=1,k_{2}=2,k_{3}=2,p_{1}=2,p_{2}=2, but different p3p_{3}: (a1) (a2) p3=2p_{3}=-2, (b1) (b2) p3=2p_{3}=-2, (c1) (c2) p3=4p_{3}=4, (d1) (d2) p3=3p_{3}=3. It is observed that shapes of waves are influenced by the variable coefficient ρ(t)\rho(t).

  • For ρ(t)=1/t\rho(t)=1/t, the three-soliton solution shows the interaction among three parabolic solitons (see Figs. 2 (a1) and (a2)).

  • For ρ(t)=1/t2\rho(t)=1/{t^{2}}, the shape of the wave changes from parabolic to cubic, as shown by Figs. 2 (b1) and (b2).

  • For trigonometric functions, periodic waves are obtained. See Figs. 2 (c1), (c2) for ρ(t)=1/sint\rho(t)=1/\sin t and Figs. 2 (d1), (d2) for ρ(t)=1/(sin2t+tanht)\rho(t)=1/\left(\sin 2t+\tanh t\right).

Refer to caption
Figure 2: Three-soliton solution given by (3.8) with different variable coefficients ρ(t)\rho(t): (a1) (a2) ρ(t)=1/t\rho(t)=1/t; (b1) (b2) ρ(t)=1/t2\rho(t)=1/{t^{2}}; (c1) (c2) ρ(t)=1/sint\rho(t)=1/{\sin t}; (d1) (d2) ρ(t)=1/(sin2t+tanht)\rho(t)=1/\left({\sin 2t+\tanh t}\right).

By specifying the conjugate parameters, two linear solitons can be reduced to one breather. By applying the long wave limit method, two linear solitons can be reduced to one lump solution [28]. The following theorem can then be obtained.

Theorem 3.1.

Let

ps=msks,as=lsϵ,s=1,2,,N,\displaystyle p_{s}=m_{s}k_{s},\quad a_{s}=l_{s}\epsilon,\quad s=1,2,\ldots,N,
exp(θ0j)=1,j=1,2,,2M,\displaystyle\exp(\theta_{0j})=-1,\quad j=1,2,\ldots,2M,
mn=mn+M,n=1,2,,M,\displaystyle m_{n}=m_{n+M}^{*},\quad n=1,2,\ldots,M, (3.9)
k2M+l=k2M+L+l,l=1,2,,L,\displaystyle k_{2M+l}=k_{2M+L+l}^{*},\quad l=1,2,\ldots,L,
k2M+2L+h,h=1,2,,Q,\displaystyle k_{2M+2L+h},\quad h=1,2,\ldots,Q,

be constants, where ‘*’ denotes the complex conjugate. Let ϵ0\epsilon\rightarrow 0, and the NN-soliton solution of Eq. (2.5) can be represented as a combination of MM-lump, LL-breather and QQ-line solitons, where N=2M+2L+QN=2M+2L+Q and M,L,QM,L,Q are nonnegative integers [27].

Let M=1,L=1,Q=1M=1,L=1,Q=1 in (3.1), and so N=5N=5. Namely, five-soliton solution can be reduced to the interaction among one lump, one breather and one line soliton. Figs. 3 (a1), (b1) describe the dynamical behavior in the (y,t)(y,t)- plane when x=2x=2, while Figs. 3 (c1), (d1) describe the dynamical behavior in the (x,t)(x,t)- plane when y=2y=2. It is noticed that the lump, breather and line solitons are localized in the parabolic curves and interact with each other.

Refer to caption
Figure 3: The interaction among one lump, one breather and one line solitons with M=1,L=1,Q=1M=1,L=1,Q=1 in Eq. (3.1) and with respect to the variable coefficient ρ(t)=1/t\rho(t)=1/t. Top: 3d plots of uu and vv versus bottom: corresponding density. The parameters are k1=1,k2=1,k3=13,k4=13,k5=1,p1=12+i,p2=12i,p3=13+13i,p4=1313i,p5=1k_{1}=1,k_{2}=1,k_{3}=\frac{1}{3},k_{4}=\frac{1}{3},k_{5}=1,p_{1}=\frac{1}{2}+i,p_{2}=\frac{1}{2}-i,p_{3}=\frac{1}{3}+\frac{1}{3}i,p_{4}=\frac{1}{3}-\frac{1}{3}i,p_{5}=1.

In the following, we will show several other special NN-soliton solutions as corollaries of Theorem 3.1.

Corollary 3.2.

Setting N=2LN=2L and defining the parameters

kj=kL+j=δj+iγj,pj=pL+j=κj+iλj,θj=θL+j=ζj+iξj,θ0j=(θ0,L+j)=ζ0j+iξ0j,k_{j}=k_{L+j}^{*}=\delta_{j}+i\gamma_{j},p_{j}=p_{L+j}^{*}=\kappa_{j}+i\lambda_{j},\theta_{j}=\theta_{L+j}^{*}=\zeta_{j}+i\xi_{j},\\ \theta_{0j}=(\theta_{0,L+j})^{*}=\zeta_{0j}+i\xi_{0j},

for j=1,2,,Lj=1,2,\ldots,L, one can represent the NN-soliton solution of (2.5) as a combination of LL-breather solutions.

Now, the corresponding representation can be obtained from (3.2), if we set

f2L=ς=0,1exp(j=12Lςjθj+1s<j2LςsςjAsj),{}f_{2L}=\sum_{\varsigma=0,1}\exp\left(\sum_{j=1}^{2L}\varsigma_{j}\theta_{j}+\sum_{1\leq s<j}^{2L}\varsigma_{s}\varsigma_{j}A_{sj}\right), (3.10)

with θj=κj+iλj,\theta_{j}=\kappa_{j}+i\lambda_{j}, and exp(Asj)\exp(A_{sj}) defined by (3.5) and (3.6) respectively, and consequently

ζj=δjx+κjyΛjκj2+λj2𝑑t+ζ0j,ξj=γjx+σjyΥjκj2+λj2𝑑t+ξ0j,\begin{split}&\zeta_{j}=\delta_{j}x+\kappa_{j}y-\int\frac{\Lambda_{j}}{\kappa_{j}^{2}+\lambda_{j}^{2}}dt+\zeta_{0j},\\ &\xi_{j}=\gamma_{j}x+\sigma_{j}y-\int\frac{\Upsilon_{j}}{\kappa_{j}^{2}+\lambda_{j}^{2}}dt+\xi_{0j},\end{split} (3.11)

where j=1,2,,Lj=1,2,\ldots,L, and

Λj=σ(κj2+λj2)δj3+3αμδj2κj+3((βμλj2σ)κj2+(2αλjγj+βλj2)μσλj2γj2)δj3αμλj2κj,Υj=σ(κj2+λj2)γj3+3αμγj2λj+3((δj2σ+βμ)λj2+(2ακjδj+κj2β)μ+σκj2δj2)γj3αμδj2λj.\begin{split}&\Lambda_{j}=\sigma(\kappa_{j}^{2}+\lambda_{j}^{2})\delta_{j}^{3}+3\alpha\mu\delta_{j}^{2}\kappa_{j}+3\Big{(}(\beta\mu-\lambda_{j}^{2}\sigma)\kappa_{j}^{2}+(2\alpha\lambda_{j}\gamma_{j}+\beta\lambda_{j}^{2})\mu-\sigma\lambda_{j}^{2}\gamma_{j}^{2}\Big{)}\delta_{j}-3\alpha\mu\lambda_{j}^{2}\kappa_{j},\\ &\Upsilon_{j}=-\sigma(\kappa_{j}^{2}+\lambda_{j}^{2})\gamma_{j}^{3}+3\alpha\mu\gamma_{j}^{2}\lambda_{j}+3\Big{(}(\delta_{j}^{2}\sigma+\beta\mu)\lambda_{j}^{2}+(2\alpha\kappa_{j}\delta_{j}+\kappa_{j}^{2}\beta)\mu+\sigma\kappa_{j}^{2}\delta_{j}^{2}\Big{)}\gamma_{j}-3\alpha\mu\delta_{j}^{2}\lambda_{j}.\end{split}

When L=2L=2, the four-soliton solution reduces to the interaction between two breathers for ρ(t)=1/t2\rho(t)=1/t^{2}. Figs. 4 (a1) and (b1) describe the dynamical behavior in the (y,t)(y,t)- plane when x=0x=0, while Figs. 4 (c1) and (d1) describe the dynamical behavior in the (x,t)(x,t)- plane when y=0y=0.We notice that the two breathers have different amplitudes and periods, but both are with an S-type structure.

Refer to caption
Figure 4: The interaction between two breathers with L=2L=2 in (3.10) and the variable coefficient ρ(t)=1/t2\rho(t)=1/{t^{2}}. Top: 3d plots of uu and vv versus bottom: corresponding density. The parameters are k1=12,k2=12,k3=1,k4=1,p1=13+13i,p2=1313i,p3=13+23i,p4=1323ik_{1}=\frac{1}{2},k_{2}=\frac{1}{2},k_{3}=1,k_{4}=1,p_{1}=\frac{1}{3}+\frac{1}{3}i,p_{2}=\frac{1}{3}-\frac{1}{3}i,p_{3}=\frac{1}{3}+\frac{2}{3}i,p_{4}=\frac{1}{3}-\frac{2}{3}i.
Corollary 3.3.

Set N=2MN=2M, and define the parameters

pj=kjmj,kj=ljϵ,θj0=iπ,j=1,2,,N,\displaystyle p_{j}=k_{j}m_{j},\quad k_{j}=l_{j}\epsilon,\quad\theta_{j}^{0}=i\pi,\quad j=1,2,\ldots,N,
mn=mn+M,n=1,2,,M.\displaystyle m_{n}=m_{n+M}^{*},\quad n=1,2,\ldots,M.

Let ϵ0\epsilon\rightarrow 0, and one can represent NN-soliton solution of (2.5) as a combination of MM-lump solutions [39, 50].

The corresponding representation can be obtained from (3.2) by using

f2M=j=12MΘj+12s,j2Masjls,j2MΘl+12!22s,j,k,m2Masjakmls,j,k,mΘl++1M!2Ms,j,k,m2MasjarlawnMps,j,r,l,,w,n2MΘp+,\displaystyle{}\begin{split}f_{2M}&=\prod_{j=1}^{2M}\Theta_{j}+\frac{1}{2}\sum_{s,j}^{2M}a_{sj}\prod_{l\neq s,j}^{2M}\Theta_{l}+\frac{1}{2!2^{2}}\sum_{s,j,k,m}^{2M}a_{sj}a_{km}\prod_{l\neq s,j,k,m}\Theta_{l}+\cdots\\ &\quad+\frac{1}{M!2^{M}}\sum_{s,j,k,m}^{2M}a_{sj}\overbrace{a_{rl}\cdots a_{wn}}^{M}\prod_{p\neq s,j,r,l,\ldots,w,n}^{2M}\Theta_{p}+\cdots,\end{split} (3.12)

where

Θs=x+psy3μβps+αρ(t)ps𝑑t,s=1,2,,2M,asj=2σpspj(ps+pj)αμ(pspj)2,1s<j2M,\displaystyle\begin{split}&\Theta_{s}=x+p_{s}y-3\mu\int\frac{\beta p_{s}+\alpha}{\rho(t)p_{s}}dt,\quad s=1,2,\ldots,2M,\\ &a_{sj}=\frac{2\sigma p_{s}p_{j}(p_{s}+p_{j})}{\alpha\mu(p_{s}-p_{j})^{2}},\quad 1\leq s<j\leq 2M,\end{split} (3.13)

with psp_{s} (s=1,2,,2Ms=1,2,\ldots,2M) arbitrary complex constants. Let M=2M=2 in (3.12). Fig. 5 shows that the four-soliton solution reduces to the interaction between two lump solutions. The effect of the variable coefficient on the interactions is provided on the (y,t)(y,t)-plane for x=0x=0, i.e., (a1), (a2), (b1), (b2), and (x,t)(x,t)-plane for y=0y=0, i.e., (c1), (c2), (d1), (d2). Obviously the variable coefficient ρ(t)\rho(t), chosen as 1/t1/t in Fig. 5, is closely related to wave shapes.

Refer to caption
Figure 5: The interaction between two lump solutions with M=2M=2 in (3.12) and the variable coefficient ρ(t)=1/t\rho(t)=1/{t}. Top: 3d plots of uu and vv versus bottom: corresponding density. The parameters are k1=1,k2=1,k3=12,k4=12,p1=13+14i,p2=1314i,p3=14+i,p4=14ik_{1}=1,k_{2}=1,k_{3}=\frac{1}{2},k_{4}=\frac{1}{2},p_{1}=\frac{1}{3}+\frac{1}{4}i,p_{2}=\frac{1}{3}-\frac{1}{4}i,p_{3}=\frac{1}{4}+i,p_{4}=\frac{1}{4}-i.
Remark 3.4.

When N=2MN=2M is even, the NN-soliton solution can amount to M-lump or M-breather solitons. When N=2M+1N=2M+1 is odd, the hybrid solution has at least one line soliton.

4 Symmetry analysis and similarity reduction of the integrable variable-coefficient KdV system

In this section, we conduct symmetry analysis and in particular similarity reduction of the (2+1)-dimensional integrable variable-coefficient KdV system (2.5).

4.1 Lie point symmetries

Consider Lie point symmetries with infinitesimal generators

X=τ(x,y,t,u,v)t+ξ(x,y,t,u,v)x+η(x,y,t,u,v)y+φ(x,y,t,u,v)u+ψ(x,y,t,u,v)v\displaystyle X=\tau(x,y,t,u,v)\partial_{t}+\xi(x,y,t,u,v)\partial_{x}+\eta(x,y,t,u,v)\partial_{y}+\varphi(x,y,t,u,v)\partial_{u}+\psi(x,y,t,u,v)\partial_{v} (4.1)

with coefficients to be determined by the linearized symmetry condition [33]. Direct but length calculation amounts to

τ=f1(t),ξ=(13f1(t)13ρρf1(t))x+f2(t),η=f3(y),φ=(13f1(t)13ρρf1(t)+f3(y))u,ψ=19μ(ρf1′′(t)xρ′′f1(t)xρf1(t)x+ρ2ρf1(t)x6μf1(t)v+6μρρf1(t)v+3ρf2(t)),\displaystyle\begin{split}&\tau=f_{1}(t),\\ &\xi=\left(\frac{1}{3}f_{1}^{\prime}(t)-\frac{1}{3}\frac{\rho^{\prime}}{\rho}f_{1}(t)\right)x+f_{2}(t),\\ &\eta=f_{3}(y),\\ &\varphi=-\left(\frac{1}{3}f_{1}^{\prime}(t)-\frac{1}{3}\frac{\rho^{\prime}}{\rho}f_{1}(t)+f_{3}^{\prime}(y)\right)u,\\ &\psi=\frac{1}{9\mu}\left(\rho f_{1}^{\prime\prime}(t)x-\rho^{\prime\prime}f_{1}(t)x-\rho^{\prime}f_{1}^{\prime}(t)x+\frac{\rho^{\prime 2}}{\rho}f_{1}(t)x-6\mu f_{1}^{\prime}(t)v+6\mu\frac{\rho^{\prime}}{\rho}f_{1}(t)v+3\rho f_{2}^{\prime}(t)\right),\end{split} (4.2)

where f1(t)f_{1}(t), f2(t)f_{2}(t) and f3(y)f_{3}(y) are arbitrary function of tt and yy, respectively. Hence Lie point symmetries of the variable-coefficient KdV system (2.5) are infinite dimensional depending on arbitrary functions, and are spanned by the following infinitesimal generators

f1(t)t+13(f1(t)ρρf1(t))xx13(f1(t)ρρf1(t))uu+19μ((ρ2(f1(t)ρ)ρ(ρρ)f1(t))x6μ(f1(t)ρρf1(t))v)v,f2(t)x+13μρf2(t)v,f3(y)yf3(y)uu.\displaystyle\begin{split}&f_{1}(t)\frac{\partial}{\partial t}+\frac{1}{3}\left(f_{1}^{\prime}(t)-\frac{\rho^{\prime}}{\rho}f_{1}(t)\right)x\frac{\partial}{\partial x}-\frac{1}{3}\left(f_{1}^{\prime}(t)-\frac{\rho^{\prime}}{\rho}f_{1}(t)\right)u\frac{\partial}{\partial u}\\ &\quad+\frac{1}{9\mu}\left(\left(\rho^{2}\left(\frac{f_{1}^{\prime}(t)}{\rho}\right)^{\prime}-\rho\left(\frac{\rho^{\prime}}{\rho}\right)^{\prime}f_{1}(t)\right)x-6\mu\left(f_{1}^{\prime}(t)-\frac{\rho^{\prime}}{\rho}f_{1}(t)\right)v\right)\frac{\partial}{\partial v},\\ &f_{2}(t)\frac{\partial}{\partial x}+\frac{1}{3\mu}\rho f_{2}^{\prime}(t)\frac{\partial}{\partial v},\\ &f_{3}(y)\frac{\partial}{\partial y}-f_{3}^{\prime}(y)u\frac{\partial}{\partial u}.\end{split} (4.3)

For simplicity, we will choose linear functions f1(t)=c1t+c2f_{1}(t)=c_{1}t+c_{2}, f2(t)=c3t+c4f_{2}(t)=c_{3}t+c_{4} and f3(y)=c5y+c6f_{3}(y)=c_{5}y+c_{6} in the rest of the paper, where cic_{i}, i=1,2,,6i=1,2,\ldots,6 are constants. Consequently, these symmetries of the variable-coefficient KdV system are generated by the following infinitesimal generators

X1=x,X2=y,X3=tx+ρ3μv,X4=yyuu,X5=t13ρρxx+13ρρuu+19μ(ρ′′x+ρ2ρx+6μρρv)v,X6=tt+13(1ρρt)xx13(1ρρt)uu19μ(ρ′′tx+ρxρ2ρtx+6μv6μρρtv)v.\displaystyle\begin{split}&X_{1}=\frac{\partial}{\partial x},\quad X_{2}=\frac{\partial}{\partial y},\quad X_{3}=t\frac{\partial}{\partial x}+\frac{\rho}{3\mu}\frac{\partial}{\partial v},\quad X_{4}=y\frac{\partial}{\partial y}-u\frac{\partial}{\partial u},\\ &X_{5}=\frac{\partial}{\partial t}-\frac{1}{3}\frac{\rho^{\prime}}{\rho}x\frac{\partial}{\partial x}+\frac{1}{3}\frac{\rho^{\prime}}{\rho}u\frac{\partial}{\partial u}+\frac{1}{9\mu}\left(-\rho^{\prime\prime}x+\frac{\rho^{\prime 2}}{\rho}x+6\mu\frac{\rho^{\prime}}{\rho}v\right)\frac{\partial}{\partial v},\\ &X_{6}=t\frac{\partial}{\partial t}+\frac{1}{3}\left(1-\frac{\rho^{\prime}}{\rho}t\right)x\frac{\partial}{\partial x}-\frac{1}{3}\left(1-\frac{\rho^{\prime}}{\rho}t\right)u\frac{\partial}{\partial u}-\frac{1}{9\mu}\left(\rho^{\prime\prime}tx+\rho^{\prime}x-\frac{\rho^{\prime 2}}{\rho}tx+6\mu v-6\mu\frac{\rho^{\prime}}{\rho}tv\right)\frac{\partial}{\partial v}.\end{split} (4.4)

4.2 Similarity reductions

In this subsection, we will study similarity reductions of the variable-coefficient KdV system (2.5) by using each of the symmetries (4.4). Certainly their linear combinations may lead to further interesting solutions.

(1) X1=xX_{1}=\frac{\partial}{\partial x}. The corresponding invariants are t,y,u,v,t,y,u,v,, and the group-invariant solution is

u=U(y),v=V(t),\displaystyle u=U(y),\ \ v=V(t), (4.5)

where U(y)U(y) and V(t)V(t) are arbitrary function about yy and tt, respectively.

(2) X2=yX_{2}=\frac{\partial}{\partial y}. Direct calculation gives the following group-invariant solution

u=U(t),v=13μU(t)U(t)ρx,\displaystyle u=U(t),\ \ v=-\frac{1}{3\mu}\frac{U^{\prime}(t)}{U(t)}\rho x, (4.6)

where U(t)U(t) is an arbitrary function.

(3) X3=tx+ρ3μvX_{3}=t\frac{\partial}{\partial x}+\frac{\rho}{3\mu}\frac{\partial}{\partial v}. The characteristic equation for determining the invariants reads

dxt=dvρ/3μ,\displaystyle\frac{dx}{t}=\frac{dv}{{\rho}/{3\mu}}, (4.7)

amounting to the following invariants

t,y,U(y,t)=u,V(y,t)=3μρ(v13μρtx).t,\quad y,\quad U(y,t)=u,\quad V(y,t)=\frac{3\mu}{\rho}\left(v-\frac{1}{3\mu}\frac{\rho}{t}x\right). (4.8)

Substituting (4.8) back to the system (2.5) gives

u=R(y)t+K(y),v=13μρtx+13μρV(t),\displaystyle{}u=R(y)t+K(y),\ \ v=\frac{1}{3\mu}\frac{\rho}{t}x+\frac{1}{3\mu}\rho V(t), (4.9)

where R(y)R(y), K(y)K(y) and V(t)V(t) are arbitrary function about yy and tt, respectively. To illustrate this solution, we choose R(y)R(y)=sech(y)(y), K(y)K(y)=sech(y)(y), V(t)V(t)=sech(t)(t), ρ\rho=sech(t)(t) and μ=1\mu=1. The figures of uu and vv are shown in Figs. 6 (a1), (a2),(b1) and (b2). The interaction between two soliton, with the opposite amplitude in the yy-direction, and with the same amplitude in the xx-direction, can be observed.

(4) X4=yyuuX_{4}=y\frac{\partial}{\partial y}-u\frac{\partial}{\partial u}. Similar computation give the following group-invariant solution

u=cy1e3μU(t),v=U(t)ρx+V(t),\displaystyle{}u=cy^{-1}e^{-3\mu U(t)},\ \ v=U^{\prime}(t)\rho x+V(t), (4.10)

where U(t)U(t) and V(t)V(t) are arbitrary function of tt, and cc is a constant. We choose R(t)R(t)=sech(t)(t), V(t)V(t)=sech(t)(t), c=1c=1, ρ=1\rho=1 and μ=1\mu=1, and the resulting solution is shown in Figs. 6 (c1), (c2), (d1) and (d2). The interaction between two solitons, with the same amplitude in the yy-direction, and with the opposite amplitude in the xx-direction can be noticed.

Refer to caption
Figure 6: The interaction between two soliton solutions given by (4.9) (figures (a1), (a2), (b1), (b2)) and (4.10) (figures (c1), (c2), (d1), (d2)). Top: 3d plots of uu and vv versus bottom: corresponding density.

(5) X5=t13ρρxx+13ρρuu+19μ(ρ′′x+ρ2ρx+6μρρv)vX_{5}=\frac{\partial}{\partial t}-\frac{1}{3}\frac{\rho^{\prime}}{\rho}x\frac{\partial}{\partial x}+\frac{1}{3}\frac{\rho^{\prime}}{\rho}u\frac{\partial}{\partial u}+\frac{1}{9\mu}\left(-\rho^{\prime\prime}x+\frac{\rho^{\prime 2}}{\rho}x+6\mu\frac{\rho^{\prime}}{\rho}v\right)\frac{\partial}{\partial v}. Consider the characteristic equations

dx13ρρx=dt1=du13ρρu=dv19μ(ρ′′x+ρ2ρx+6μρρv),\displaystyle\frac{dx}{-\frac{1}{3}\frac{\rho^{\prime}}{\rho}x}=\frac{dt}{1}=\frac{du}{\frac{1}{3}\frac{\rho^{\prime}}{\rho}u}=\frac{dv}{\frac{1}{9\mu}\left(-\rho^{\prime\prime}x+\frac{\rho^{\prime 2}}{\rho}x+6\mu\frac{\rho^{\prime}}{\rho}v\right)}, (4.11)

whose solution give the invariants

ρ13x,y,xu,19μρρρ13x+ρ23v.\displaystyle\rho^{\frac{1}{3}}x,\ \ y,\ \ xu,\ \ \frac{1}{9\mu}\frac{\rho^{\prime}}{\rho}\rho^{\frac{1}{3}}x+\rho^{-\frac{2}{3}}v. (4.12)

To conduct the reduction, we choose

r=ρ13x,y=y,U=xur,V=19μρρr+ρ23v,\displaystyle{}r=\rho^{\frac{1}{3}}x,\ \ y=y,\quad U=\frac{xu}{r},\ \ V=\frac{1}{9\mu}\frac{\rho^{\prime}}{\rho}r+\rho^{-\frac{2}{3}}v, (4.13)

which are substituted back to (2.5), yielding

{3μ(UV)r+σUrrr=0,UrVy=0.\left\{\begin{array}[]{l}3\mu\left(UV\right)_{r}+\sigma U_{rrr}=0,\vspace{0.2cm}\\ U_{r}-V_{y}=0.\\ \end{array}\right. (4.14)

The reduced system (4.14) is still difficult to be solved immediately. In the following, we will conduct one more step of reduction. As shown in (i) below that the system (4.14) can be reduced to one PDE, and we will conduct the symmetry reduction for (4.14) and the PDE, i.e., (4.16), separately. They are related as local and nonlocal symmetries of differential equations (see, e.g., [8] and references therein).

(i) Symmetries of the PDE (4.16). The first equation of (4.14) can be integrated with respect to rr, yielding

V=a(y)σUrr3μU,\displaystyle{}V=\frac{a(y)-\sigma U_{rr}}{3\mu U}, (4.15)

which is then substituted to the second equation. Consequently, the system (4.14) turns into a single PDE

Ur=(a(y)σUrr3μU)y,\displaystyle U_{r}=\left(\frac{a(y)-\sigma U_{rr}}{3\mu U}\right)_{y}, (4.16)

where a(y)a(y) is an arbitrary function.

Remark 4.1.

The PDE (4.16) seems new to us and is potentially integrable by the ARS conjecture [3]. Indeed, it passes the Painlevé test.

Expanding the derivatives, Eq. (4.16) reads

a(y)Ua(y)Uy3μU2Ur+σUyUrrσUUrry=0.\displaystyle{}a^{\prime}(y)U-a(y)U_{y}-3\mu U^{2}U_{r}+\sigma U_{y}U_{rr}-\sigma UU_{rry}=0. (4.17)

Lie point symmetries of (4.17) are generated by the infinitesimal generators

Y1=r,Y2=1a(y)y+a(y)a2(y)UU,Y3=rr3a(y)(a(y)𝑑y)y+U(23a(y)a2(y)a(y)𝑑y)U,\displaystyle\begin{split}&Y_{1}=\frac{\partial}{\partial r},\quad Y_{2}=\frac{1}{a(y)}\frac{\partial}{\partial y}+\frac{a^{\prime}(y)}{a^{2}(y)}U\frac{\partial}{\partial U},\\ &Y_{3}=r\frac{\partial}{\partial r}-\frac{3}{a(y)}\left(\int a(y)dy\right)\frac{\partial}{\partial y}+U\left(2-\frac{3a^{\prime}(y)}{a^{2}(y)}\int a(y)dy\right)\frac{\partial}{\partial U},\end{split} (4.18)

where we assume a(y)0a(y)\neq 0.

(i-1) We firstly use Y1+c0Y2Y_{1}+c_{0}Y_{2} to reduce Eq. (4.17), where c0c_{0} is constant. The invariants are z=c0ra(y)𝑑yz={c_{0}}r-\int a(y)dy and R(z)=U(r,y)/a(y)R(z)=U(r,y)/a(y), and the Eq. (4.17) is reduced to the third-order ODE

σc02R′′′R+c02R′′R+3c0μRR2R=0.\displaystyle-\sigma c_{0}^{2}R^{\prime\prime\prime}R+c_{0}^{2}R^{\prime\prime}R^{\prime}+3c_{0}\mu R^{\prime}R^{2}-R^{\prime}=0. (4.19)

Dividing by R2R^{2} on both sides and integrating it with respect to zz, we obtain a second-order ODE

σc02R′′+3c0μR2+c1R+1=0,\displaystyle-\sigma c_{0}^{2}R^{\prime\prime}+3c_{0}\mu R^{2}+c_{1}R+1=0, (4.20)

By a translation R~=R+c2\widetilde{R}={R}+c_{2}, Eq. (4.20) becomes

σc02R~′′+3c0μR~2+(c16μc0c2)R~+3μc0c22c1c2+1=0.\displaystyle-\sigma c_{0}^{2}\widetilde{R}^{\prime\prime}+3c_{0}\mu\widetilde{R}^{2}+(c_{1}-6\mu c_{0}c_{2})\widetilde{R}+3\mu c_{0}c_{2}^{2}-c_{1}c_{2}+1=0. (4.21)

It is equivalent to the reduced ODE of the KdV equation for searching its traveling wave solutions (see Example 3.4 of [33]), that will appear later, i.e., Eq. (4.35), followed by some special solutions.

(i-2) The invariants with respect to Y3Y_{3} are

z=r(a(y)𝑑y)13,R(z)=1a(y)(a(y)𝑑y)23U(r,y).z=r\left(\int a(y)dy\right)^{\frac{1}{3}},\quad R(z)=\frac{1}{a(y)}\left(\int a(y)dy\right)^{\frac{2}{3}}U(r,y). (4.22)

Now the Eq. (4.17) is reduced to a third-order ODE

σzRR′′′+σzRR′′2σRR′′9μR2RzR+2R=0.\displaystyle\begin{split}-\sigma zRR^{\prime\prime\prime}+\sigma zR^{\prime}R^{\prime\prime}-2\sigma RR^{\prime\prime}-9\mu R^{2}R^{\prime}-zR^{\prime}+2R=0.\end{split} (4.23)

By the transformation

R=(zW),R=(zW)^{\prime}, (4.24)

Eq. (4.23) becomes

σW′′′=3σW′′z9μ(W)29μWWz+c1Wz2+c1Wz3+1z,\sigma W^{\prime\prime\prime}=-3\sigma\frac{W^{\prime\prime}}{z}-9\mu(W^{\prime})^{2}-9\mu\frac{WW^{\prime}}{z}+c_{1}\frac{W^{\prime}}{z^{2}}+c_{1}\frac{W}{z^{3}}+\frac{1}{z}, (4.25)

where c1c_{1} is a constant of integration. Eq. (4.25) is integrable as passing the Painlevé test and is in the form of Chazy’s classification on third-order Painlevé equations of the polynomial type (see, e.g., Eq. (2.1) of [10]). However, some of the coefficients are locally analytic except z=0z=0. Furthermore, Eq. (4.25) is non-autonomous and seems not included in the 13 classes introduced by Chazy in [9].

Remark 4.2.

If a(y)=0a(y)=0, singularity appears in the symmetries (4.18). Now Eq. (4.17) becomes

3μU2Ur+σUyUrrσUUrry=0,\displaystyle{}-3\mu U^{2}U_{r}+\sigma U_{y}U_{rr}-\sigma UU_{rry}=0, (4.26)

and its Lie point symmetries are generated by the infinitesimal generators

Y1=r,Y2=g(y)yUg(y)U,Y3=rrUU.\displaystyle{}\begin{split}Y_{1}=\frac{\partial}{\partial r},\quad Y_{2}=g(y)\frac{\partial}{\partial y}-Ug^{\prime}(y)\frac{\partial}{\partial U},\quad Y_{3}=r\frac{\partial}{\partial r}-U\frac{\partial}{\partial U}.\end{split} (4.27)

For simplicity, let g(y)=1g(y)=1, and consider Y1+c0Y2Y_{1}+c_{0}Y_{2} that is associated to traveling wave solutions. Choose the invariants as

z=c0ry,U.z=c_{0}r-y,\quad U. (4.28)

The Eq. (4.26) is reduced to

σc0U′′3μU2+c1U=0,\sigma c_{0}U^{\prime\prime}-3\mu U^{2}+c_{1}U=0, (4.29)

where U=U(z)U=U(z) and c1c_{1} is a constant. This ODE is equivalent to (4.20) by a translational transformation of UU.

In addition, we take g(y)=yg(y)=y, and consider Y2+cY3Y_{2}+cY_{3}, which corresponding to the scale invariance. The invariants are z=rycz=ry^{-c} and R(z)=yc+1U(r,y)R(z)=y^{c+1}U(r,y), and the Eq. (4.26) is reduced to the third-order ODE

σczRR′′′+σczRR′′2σcRR′′+3μR2R=0.\displaystyle\begin{aligned} -\sigma czRR^{\prime\prime\prime}+\sigma czR^{\prime}R^{\prime\prime}-2\sigma cRR^{\prime\prime}+3\mu R^{2}R^{\prime}=0.\end{aligned} (4.30)

Similar to the derivation of Eq. (4.25), introducing R=(zW)R=(zW)^{\prime}, Eq. (4.30) is equivalent to

σcW′′′=3σcW′′z+3μ(W)2+3μWWz+c1Wz2+c1Wz3,\displaystyle\sigma cW^{\prime\prime\prime}=-3\sigma c\frac{W^{\prime\prime}}{z}+3\mu(W^{\prime})^{2}+3\mu\frac{WW^{\prime}}{z}+c_{1}\frac{W^{\prime}}{z^{2}}+c_{1}\frac{W}{z^{3}}, (4.31)

where c1c_{1} is a constant of integration. It is again a third-order Painlevé equation of polynomial type, which passes the Painlevé test. It is equivalent to Eq. (4.25) except a 1/z1/z term.

(ii) Symmetries of the potential system (4.14). Its Lie point symmetries are generated by

Y1=r,Y2=h(y)yh(y)UU,Y3=rrUU2VV,\displaystyle Y_{1}=\frac{\partial}{\partial r},\ \ Y_{2}=h(y)\frac{\partial}{\partial y}-h^{\prime}(y)U\frac{\partial}{\partial U},\quad Y_{3}=r\frac{\partial}{\partial r}-U\frac{\partial}{\partial U}-2V\frac{\partial}{\partial V}, (4.32)

where h(y)h(y) is an arbitrary function.

(ii-1) Consider a special case by taking h(y)=1h(y)=1, and the second generator becomes

Y2=y.\displaystyle Y_{2}=\frac{\partial}{\partial y}. (4.33)

Consider reductions related to Y1+c0Y2Y_{1}+c_{0}Y_{2}, i.e., traveling wave type of solutions, where c0c_{0} is a constant. The invariants are z=c0ryz=c_{0}r-y, and UU, VV. Now the potential system (4.14) becomes

{3μUV+3μUV+σc02U′′′=0,c0U+V=0.\left\{\begin{array}[]{l}3\mu U^{\prime}V+3\mu UV^{\prime}+\sigma c_{0}^{2}U^{\prime\prime\prime}=0,\vspace{0.2cm}\\ c_{0}U^{\prime}+V^{\prime}=0.\\ \end{array}\right. (4.34)

Both equations in (4.34) can be integrated once and the system is equivalent to the following second-order ODE

σc02U′′(z)+3μc0U23μc1Uc2=0.\displaystyle-\sigma c_{0}^{2}U^{\prime\prime}(z)+3\mu c_{0}U^{2}-3\mu c_{1}U-c_{2}=0. (4.35)

Similar to Eq. (4.20), Eq. (4.35) can also be integrated once, amounting to

12σc02U2(z)=μc0U332μc1U2c2U+c3,\displaystyle\frac{1}{2}\sigma c_{0}^{2}U^{\prime 2}(z)=\mu c_{0}U^{3}-\frac{3}{2}\mu c_{1}U^{2}-c_{2}U+c_{3}, (4.36)

where c1,c2,c3c_{1},c_{2},c_{3} are integration constants. If c20c_{2}\neq 0, Eq. (4.35) is equivalent to Eq. (4.21). In the following, we list its special solutions by properly assigning the parameters.

  • Assume μ=1\mu=-1 without loss of generality, and further let c2=0c_{2}=0 and c3=0c_{3}=0. A special solution of Eq. (4.36) is given by

    U=3c12c0sech2(3σc12σc0(z+δ)),\displaystyle U=\frac{3c_{1}}{2c_{0}}\mathrm{sech}^{2}\left(\frac{\sqrt{3\sigma c_{1}}}{2\sigma c_{0}}(z+\delta)\right), (4.37)

    where δ\delta is a phase shift and we assumed σc1\sigma c_{1} to be positive. This leads to solutions of the system (2.5) as

    u(x,y,t)=3c12c0ρ13sech2(3σc12σc0(c0ρ13xy+δ)),v(x,y,t)=3c12ρ23sech2(3σc12σc0(c0ρ13xy+δ))+c4ρ2319μρx.\displaystyle\begin{split}u(x,y,t)&=\frac{3c_{1}}{2c_{0}}\rho^{\frac{1}{3}}\mathrm{sech}^{2}\left(\frac{\sqrt{3\sigma c_{1}}}{2\sigma c_{0}}\left(c_{0}\rho^{\frac{1}{3}}x-y+\delta\right)\right),\\ v(x,y,t)&=-\frac{3c_{1}}{2}\rho^{\frac{2}{3}}\mathrm{sech}^{2}\left(\frac{\sqrt{3\sigma c_{1}}}{2\sigma c_{0}}\left(c_{0}\rho^{\frac{1}{3}}x-y+\delta\right)\right)+c_{4}\rho^{\frac{2}{3}}-\frac{1}{9\mu}\rho^{\prime}x.\end{split} (4.38)

    where c4c_{4} is an integration constant.

  • If we only assume U(z)U(z) to be bounded similar as [33], Eq. (4.36) has the periodic cnoidal wave solutions

    U=b2+(b3b2)cn2(μ(b3b1)2σc0(z+δ),k),\displaystyle U=b_{2}+(b_{3}-b_{2})\mathrm{cn}^{2}\left(\sqrt{-\frac{\mu(b_{3}-b_{1})}{2\sigma c_{0}}}(z+\delta),k\right), (4.39)

    where cn is the Jacobi elliptic function of modulus k=b3b2b3b1k=\sqrt{\frac{b_{3}-b_{2}}{b_{3}-b_{1}}}, and b1<b2<b3b_{1}<b_{2}<b_{3} are the roots of the cubic polynomial on the right-hand side of Eq. (4.36). The corresponding periodic wave solutions of the system (2.5) are

    u(x,y,t)=ρ13(b2+(b3b2)cn2(μ(b3b1)2σc0(c0ρ13xy+δ),k)),v(x,y,t)=c0ρ23(b2+(b3b2)cn2(μ(b3b1)2σc0(c0ρ13xy+δ),k))+c4ρ2319μρx.\displaystyle\begin{split}u(x,y,t)&=\rho^{\frac{1}{3}}\left(b_{2}+(b_{3}-b_{2})\mathrm{cn}^{2}\left(\sqrt{-\frac{\mu(b_{3}-b_{1})}{2\sigma c_{0}}}\left(c_{0}\rho^{\frac{1}{3}}x-y+\delta\right),k\right)\right),\\ v(x,y,t)&=-c_{0}\rho^{\frac{2}{3}}\left(b_{2}+(b_{3}-b_{2})\mathrm{cn}^{2}\left(\sqrt{-\frac{\mu(b_{3}-b_{1})}{2\sigma c_{0}}}\left(c_{0}\rho^{\frac{1}{3}}x-y+\delta\right),k\right)\right)\\ &\quad+c_{4}\rho^{\frac{2}{3}}-\frac{1}{9\mu}\rho^{\prime}x.\end{split} (4.40)

    Here, we assumed μσc0\mu\sigma c_{0} to be negative.

The traveling wave solutions (4.38) and periodic wave solutions (4.40) of the system (2.5) are shown in Fig. 7 at the time t=2t=2 and with variable coefficient ρ=1/t\rho=1/t. In Figs. 7 (a1), (a2), (b1) and (b2), the parameters are δ=σ=c0=c1=1,c4=3\delta=\sigma=c_{0}=c_{1}=1,c_{4}=-3, while in (c1), (c2), (d1) and (d2), the parameters are δ=0,σ=c0=c1=c3=c4=1,c2=3,μ=1\delta=0,\sigma=c_{0}=c_{1}=c_{3}=c_{4}=1,c_{2}=-3,\mu=-1.

Refer to caption
Figure 7: The traveling wave solutions (4.38) (figures (a1), (a2), (b1), (b2)) and periodic wave solutions (4.40) (figures (c1), (c2), (d1), (d2)). Top: 3d plots of uu and vv versus bottom: corresponding density.

(ii-2) If we choose h(y)=yh(y)=y, then Y2+cY3Y_{2}+cY_{3} corresponds to the scale invariance, the invariants of which are z=rycz=ry^{-c}, R(z)=yc+1U(r,y)R(z)=y^{c+1}U(r,y), F(z)=r2V(r,y)F(z)=r^{2}V(r,y). Then, Eq. (4.14) is reduced to the third-order ODE

σzRR′′′σzRR′′+2σRR′′3μcR2Rc0zR+2c0R=0.\displaystyle\begin{split}\sigma zRR^{\prime\prime\prime}-\sigma zR^{\prime}R^{\prime\prime}+2\sigma RR^{\prime\prime}-\frac{3\mu}{c}R^{2}R^{\prime}-c_{0}zR^{\prime}+2c_{0}R=0.\end{split} (4.41)

It is equivalent to Eq. (4.23) by a scaling of RR providing the constant of integration c00c_{0}\neq 0. If c0=0c_{0}=0, defining

R=(zW),R=(zW)^{\prime}, (4.42)

Eq. (4.41) becomes

σW′′′=3σW′′z+3μc(W)2+3μcWWz+c2Wz2+c2Wz3\sigma W^{\prime\prime\prime}=-3\sigma\frac{W^{\prime\prime}}{z}+\frac{3\mu}{c}(W^{\prime})^{2}+\frac{3\mu}{c}\frac{WW^{\prime}}{z}+c_{2}\frac{W^{\prime}}{z^{2}}+c_{2}\frac{W}{z^{3}} (4.43)

with c2c_{2} a constant of integration. It is exactly Eq. (4.31).

(6) X6=tt+13(1ρρt)xx13(1ρρt)uu19μ(ρ′′tx+ρxρ2ρtx+6μv6μρρtv)vX_{6}=t\frac{\partial}{\partial t}+\frac{1}{3}\left(1-\frac{\rho^{\prime}}{\rho}t\right)x\frac{\partial}{\partial x}-\frac{1}{3}\left(1-\frac{\rho^{\prime}}{\rho}t\right)u\frac{\partial}{\partial u}-\frac{1}{9\mu}\left(\rho^{\prime\prime}tx+\rho^{\prime}x-\frac{\rho^{\prime 2}}{\rho}tx+6\mu v-6\mu\frac{\rho^{\prime}}{\rho}tv\right)\frac{\partial}{\partial v}. The characteristic equations are

dxx3(1ρtρ)=dtt=duu3(ρtρ1)=dv19μ(ρ′′tx+ρxρ2ρtx+6μv6μρρtv),\displaystyle\frac{dx}{\frac{x}{3}\left(1-\frac{\rho^{\prime}t}{\rho}\right)}=\frac{dt}{t}=\frac{du}{\frac{u}{3}\left(\frac{\rho^{\prime}t}{\rho}-1\right)}=\frac{dv}{-\frac{1}{9\mu}\left(\rho^{\prime\prime}tx+\rho^{\prime}x-\frac{\rho^{\prime 2}}{\rho}tx+6\mu v-6\mu\frac{\rho^{\prime}}{\rho}tv\right)}, (4.44)

solving that gives the invariants

(ρt)13x,y,xu,19μρρ(ρt)13tx+(ρt)23v.\displaystyle\left(\frac{\rho}{t}\right)^{\frac{1}{3}}x,\ \ y,\ \ xu,\ \ \frac{1}{9\mu}\frac{\rho^{\prime}}{\rho}\left(\frac{\rho}{t}\right)^{\frac{1}{3}}tx+\left(\frac{\rho}{t}\right)^{-\frac{2}{3}}v. (4.45)

We choose the invariant variables as

r=(ρt)13x,y=y,U=xur,V=19μρρ(ρt)13tx+(ρt)23v,\displaystyle{}r=\left(\frac{\rho}{t}\right)^{\frac{1}{3}}x,\quad y=y,\ \ U=\frac{xu}{r},\ \ V=\frac{1}{9\mu}\frac{\rho^{\prime}}{\rho}\left(\frac{\rho}{t}\right)^{\frac{1}{3}}tx+\left(\frac{\rho}{t}\right)^{-\frac{2}{3}}v, (4.46)

which are substituted into (2.5), yielding

{13(U+Urr)+3μ(UV)r+σUrrr=0,UrVy=0.\left\{\begin{array}[]{l}-\frac{1}{3}(U+U_{r}r)+3\mu(UV)_{r}+\sigma U_{rrr}=0,\vspace{0.2cm}\\ U_{r}-V_{y}=0.\\ \end{array}\right. (4.47)
Remark 4.3.

The system (4.47) is equivalent to (4.14) by the transformation

UU,VV+r9μ.U\mapsto U,\quad V\mapsto V+\frac{r}{9\mu}. (4.48)

In other words, if (U,V)(U,V) is a solution of (4.14), then (U,V+r9μ)(U,V+\frac{r}{9\mu}) is a solution of (4.47). For instance, from (4.38), we obtain other solutions of (2.5) as follows

u(x,y,t)=3c12c0(ρt)13sech2(3σc12σc0(c0(ρt)13xy+δ)),v(x,y,t)=3c12(ρt)23sech2(3σc12σc0(c0(ρt)13xy+δ))+c4(ρt)2319μρx+19μρtx,\displaystyle\begin{split}u(x,y,t)&=\frac{3c_{1}}{2c_{0}}\left(\frac{\rho}{t}\right)^{\frac{1}{3}}\mathrm{sech}^{2}\left(\frac{\sqrt{3\sigma c_{1}}}{2\sigma c_{0}}\left(c_{0}\left(\frac{\rho}{t}\right)^{\frac{1}{3}}x-y+\delta\right)\right),\\ v(x,y,t)&=-\frac{3c_{1}}{2}\left(\frac{\rho}{t}\right)^{\frac{2}{3}}\mathrm{sech}^{2}\left(\frac{\sqrt{3\sigma c_{1}}}{2\sigma c_{0}}\left(c_{0}\left(\frac{\rho}{t}\right)^{\frac{1}{3}}x-y+\delta\right)\right)+c_{4}\left(\frac{\rho}{t}\right)^{\frac{2}{3}}-\frac{1}{9\mu}\rho^{\prime}x+\frac{1}{9\mu}\frac{\rho}{t}x,\end{split} (4.49)

and corresponding to (4.40), we obtain

u(x,y,t)=(ρt)13(b2+(b3b2)cn2(μ(b3b1)2σc0(c0(ρt)13xy+δ),k)),v(x,y,t)=c0(ρt)23(b2+(b3b2)cn2(μ(b3b1)2σc0(c0(ρt)13xy+δ),k))+c4(ρt)2319μρx+19μρtx.\displaystyle\begin{split}u(x,y,t)&=\left(\frac{\rho}{t}\right)^{\frac{1}{3}}\left(b_{2}+(b_{3}-b_{2})\mathrm{cn}^{2}\left(\sqrt{-\frac{\mu(b_{3}-b_{1})}{2\sigma c_{0}}}\left(c_{0}\left(\frac{\rho}{t}\right)^{\frac{1}{3}}x-y+\delta\right),k\right)\right),\\ v(x,y,t)&=-c_{0}\left(\frac{\rho}{t}\right)^{\frac{2}{3}}\left(b_{2}+(b_{3}-b_{2})\mathrm{cn}^{2}\left(\sqrt{-\frac{\mu(b_{3}-b_{1})}{2\sigma c_{0}}}\left(c_{0}\left(\frac{\rho}{t}\right)^{\frac{1}{3}}x-y+\delta\right),k\right)\right)\\ &\quad+c_{4}\left(\frac{\rho}{t}\right)^{\frac{2}{3}}-\frac{1}{9\mu}\rho^{\prime}x+\frac{1}{9\mu}\frac{\rho}{t}x.\end{split} (4.50)

5 Conclusions

In this paper, a (2+1)-dimensional integrable KdV system with time-dependent variable coefficient was studied. Its integrability is analyzed by Painlevé analysis. NN-soliton solutions of the (2+1)-dimensional variable-coefficient KdV system were obtained by using Hirota’s bilinear method. In particular, by choosing appropriate parameters on the NN-soliton solutions, novel wave interaction phenomena were discovered, e.g., the soliton solutions shown in Figs. 1-2, the hybrid interaction of line, lump and breather solitons illustrated by Fig. 3, the interaction of two breathers (Fig. 4), and the interaction of two lump solutions (Fig. 5). Furthermore, group-invariant solutions are derived by similarity reduction, for instance, an interaction between two solitons in Fig. 6 beside other interesting analytic solutions. These results show interesting novel physical features, which should provide new knowledge in the study of variable-coefficient nonlinear systems. As a final remark, the (2+1)-dimensional integrable variable-coefficient KdV system and the reduced PDE (4.16) are among the few examples that can be reduced to third-order Painlevé equations.

Acknowledgements

L. Peng is grateful to Saburo Kakei, Frank Nijhoff and Ralph Willox for helpful discussions. Y. Liu was partially supported by the National Natural Science Foundation of China (No. 11905013), the Beijing Natural Science Foundation (No. 1222005), and Qin Xin Talents Cultivation Program of Beijing Information Science and Technology University (QXTCP C202118). L. Peng was partially supported by JSPS Kakenhi Grant Number JP20K14365, JST-CREST Grant Number JPMJCR1914, and Keio Gijuku Fukuzawa Memorial Fund.

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