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Exploring the interaction between lump, stripe and double-stripe, and periodic wave solutions of the Konopelchenko–Dubrovsky–Kaup–Kupershmidt system

  • Shami A. M. Alsallami EMAIL logo
Published/Copyright: May 21, 2025
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Abstract

The Konopelchenko–Dubrovsky–Kaup–Kupershmidt system has significant implications in various fields, including fluid mechanics, ocean dynamics, and plasma physics. This system includes various widely recognized nonlinear evolution equations as special cases. In this study, we present a systematic approach to identifying novel wave solutions to the system, examining various combinations of interactions between lumps, stripes, double stripes, and periodic waves. By strategically selecting the arbitrary free parameters, we incorporate various 2D and 3D profiles to clearly demonstrate the dynamic behaviors of the mixed localized wave structures. These graphical representations indicate that some of the identified solutions exhibit periodic wave propagation along a straight line at specific angles to the spatial axes, maintaining constant wavelengths, amplitudes, and velocities. The solutions proposed in this study provide valuable insights into the mechanisms of wave propagation across diverse physical domains. Furthermore, the approach outlined herein is versatile and can be applied to various nonlinear differential equations in mathematical physics.

1 Introduction

Studying nonlinear differential equations is crucial for understanding the complex dynamics governing physical phenomena in fluid dynamics, plasma, and elastic materials [17]. The analytical modeling of several linear and nonlinear, static, and dynamic elasticity models has become increasingly popular in recent years among scholars. Hence, several techniques have been developed for acquiring exact solutions of such models, including Lie group methods [8], Darboux and Bäcklund transformations [9], inverse scattering transform [10], Riemann–Hilbert method [11], the long wave limit method [12], Pfaffian technique [13], Painlevé analysis method [14], and Hirota’s bilinear method [15].

In this contribution, we aim to study the (2+1)-dimensional Konopelchenko–Dubrovsky–Kaup–Kupershmidt system (KDKKS) [16]

(1) φ t + 1 φ x x x + 2 φ φ x + 3 φ x x x x x + 4 v y + 5 φ x x y + 6 ( φ ϑ ) x + 7 ( φ φ x x ) x + 8 φ 2 φ x = 0 , φ y = ϑ x ,

where φ = φ ( x , y , t ) , and the coefficients i ( i = 1, 2 , , 8 ) are the real parameters.

Note that Eq. (1) can be used to describe various phenomena in various fields, including fluid mechanics, ocean dynamics, and plasma physics. It also covers several well-known equations as its special case. For example:

  1. If we take 1 = 1 , 2 = 6 , and 3 = 4 = 5 = 6 = 7 = 8 = 0 , Eq. (1) is reduced to the well-known Korteweg-de Vries equation

    φ t 6 φ φ x + φ x x x = 0 ,

    which describes long waves in shallow water under gravity and ion-acoustic solitons in plasma [17].

  2. If we take 1 = 1 , 2 = 6 , and 3 = 5 = 6 = 7 = 8 = 0 , Eq. (1) is reduced to a (2+1)-dimensional Kadomtsev–Petviashvili equation

    ( φ t + 6 φ φ x + φ x x x ) x + 4 φ y y = 0 ,

    which arises in the investigation of the weakly nonlinear dispersive waves in plasma and also in the modulation of the weakly nonlinear long waterwaves [18].

  3. If we take 2 = 6 1 , 6 = 4 5 , and 3 = 4 = 7 = 8 = 0 , Eq. (1) is reduced to as a (2+1)-dimensional generalized breaking soliton equation or Bogoyavlensky–Konoplechenko (BK) model

    φ t + 1 φ x x x + 6 1 φ φ x + 5 φ x x y + 4 5 φ φ y + 4 5 φ x ( x 1 φ y ) = 0 ,

    for the interaction of a Riemann wave along the y axis and a long wave along the x axis [19,20]. Moreover, the symbol x 1 ( . ) is used for the integral operator with respect to x .

  4. If we take 1 = 2 = 0 , 3 = 1 , 4 = 5 = 5 , and 6 = 15 , 7 = 15 , 8 = 45 , Eq. (1) is reduced to a (2+1)-dimensional B-type Kadomtsev–Petviashvili equation

    φ t + φ x x x x x 5 ( x 1 φ y ) y 5 φ x x y 15 ( φ φ y + φ x ( x 1 φ y ) ) + 15 ( φ x φ x x + φ φ x x x ) + 45 φ 2 φ x = 0 ,

    for the shallow water waves or electrostatic wave potential in plasma [21].

  5. If we take 1 = 2 = 0 , 3 = 1 , 4 = 5 , and 5 = 6 = 7 = 8 = 5 , Eq. (1) is reduced to a (2+1)-dimensional Sawada–Kotera equation

    φ t φ x x x x x + 5 ( x 1 φ y y ) 5 φ x x y 5 ( φ φ y + φ x ( x 1 φ y ) ) 5 ( φ x φ x x + φ φ x x x ) 5 φ 2 φ x = 0 ,

    in the atmosphere, rivers, lakes, and oceans, as well as the conformal field and two-dimensional quantum gravity gauge field [22].

  6. Moreover, the Caudrey–Dodd–Gibbon–Sawada–Kotera equation [23] is also another special case of Eq. (1).

Due to its extensive use in real-world applications, the KDKK equation (Eq. (1)) has been the focus of many fascinating investigations in the literature. For instance, Cheng et al. [16] derived a bilinear form and proved Pfaffian solutions of up to N th order of Eq. (1) using the Hirota method, where N is the positive integer. These solutions reveal various soliton and breather structures, including elastic and inelastic interactions.

In the work presented in the study by Feng et al. [24], Bell’s polynomials and multidimensional Riemann theta functions are employed to suggest a methodical way to investigate periodic wave solutions and the asymptotic behavior of the system. Han and Bao [25] proposed two methods to find higher-order mixed localized wave solutions of the (3+1)-dimensional version of the system in Eq. (1). Furthermore, several numerical simulations and bilinear auto-Bäcklund transformations were used to obtain rich localized structures, including bell-shaped waves, periodic breather waves, and lump waves.

By reexamining the problem with a novel method based on bilinear transformation, a number of traveling wave solutions were obtained in the study by Jia [26]. These solutions include soliton molecules, solitons with double and triple-peaked structures, peak-plateau solitons, and few-cycle-pulse solitons. The focus of the research in the study by Ma et al. [27] is the (2+1)-dimensional generalized Konopelchenko–Dubrovsky–Kaup–Kupershmidt (gKDKK) equation. To achieve fission and fusion solutions, also known as “y-type solutions,” a new constraint condition is added based on Hirota’s bilinear method.

In the study by Li et al. [28], several soliton molecules were discovered by applying a velocity resonance ansatz to N -soliton solutions of the (2+1)-dimensional gKDKK equation. These solitons can transform into asymmetric solitons by adjusting specific parameters. Additionally, it was pointed out that a double-peaked lump solution to the system is constructed using a breather degeneration approach. Moreover, based on the Hirota’s bilinear form of this system, lump waves, lump-off waves, and rogue waves are described in the study by Liu et al. [29]. Deng et al. [30] employed the Pfaffian and Wronskian procedures to obtain the N th-order Pfaffian and Wronskian solutions, respectively. Higher-order lump, breather, and hybrid solutions to the system were also presented in the study of Zhang et al. [31]. As noted, the higher-order lump solutions are generalized through the long-wave limit method, while breather and hybrid solutions composed of solitons, breathers, and lumps are derived.

The (2+1)-dimensional gKDKK equation is solved in the study by Zhao et al. [32] using a bilinear form, yielding lump-type, interaction, and breather solutions. The trajectory, peaks, and valleys of the lump wave are analyzed theoretically and displayed visually through graphs. Feng et al. [33] explored a (3+1)-dimensional form of the Konopelchenko–Dubrovsky–Kaup–Kupershmidt equation using the Hirota method to derive bilinear forms, soliton solutions, breather solutions, and lump solutions. This equation has also been investigated in the study by Tariq et al. [34], where its integrability characteristics and wave patterns are explored. This study employs Hirota’s bilinear form and the exp ( ϕ ( ξ ) ) expansion method to discover novel wave solutions for the model, including bell-shaped bright soliton solutions and periodic wave solutions.

In recent years, bilinear approaches have been widely utilized as essential tools for obtaining soliton wave solutions in higher-order nonlinear differential equations [20,3537]. In this study, we aim to uncover novel traveling wave solutions for the ( 2 + 1 ) -dimensional KDKK system (1), using Hirota’s bilinear transformation and various combinations of interactions between lumps, stripes, and double stripes, as well as periodic waves. These solutions are new and innovative, having not been previously identified in the literature. To achieve our objectives, we have structured this article as follows: Section 2 presents the bilinear differential operator for the system. Then, we investigate novel wave solutions in Section 3 of our work. Section 3 additionally offers several types of 2D and 3D simulations that demonstrate the time evolution of the obtained solutions. The final section of the article summarizes the key conclusions.

2 Bilinear differential operator for Eq. (1)

To obtain the Hirota’s bilinear form of Eq. (1), we start by applying the following Cole–Hopf transformations:

(2) φ = 12 1 2 ( ln Λ ) x x + φ 0 = 12 1 2 Λ x x Λ Λ x 2 Λ 2 + φ 0 , ϑ = 12 1 2 ( ln Λ ) x y + φ 0 = 12 1 2 Λ x y Λ Λ x Λ y Λ 2 + ϑ 0 ,

where φ 0 and ϑ 0 are two constants.

Utilizing the transformations in Eq. (2) along with the following coefficient conditions [16]

(3) 2 l 1 l 2 = 5 l 3 l 7 = l 5 l 6 = l 7 l 8 , l 4 = l 5 2 5 l 3 ,

which can be expressed in an equivalent form

(4) 1 = 7 2 2 8 , 2 = 2 , 3 = 7 2 5 8 , 4 = 6 2 8 , 5 = 6 7 8 , 6 = 6 , 7 = 7 , 8 = 8 ,

the Hirota’s bilinear equation corresponding to Eq. (1) is derived as

(5) 10 8 D x D t + 5 7 ( 2 φ 0 8 + 2 ) D x 4 + 2 7 2 D x 6 + 10 6 7 D x 3 D y 10 6 2 D y 2 + 10 8 6 φ 0 D x D y + 10 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) D x 2 Λ Λ = 0 .

In the Hirota’s bilinear form of (5), the operator of D x m D y n D t s is symbolized as

(6) [ D x m D y n D t s ] Λ 1 · Λ 2 = x x m y y n t t 3 × Λ 1 ( x , y , t ) . Λ 2 ( x , y , t ) t x = x , y = y , t = t .

Using the bilinear differential operator specified in Eq. (6), the constituent equations of Eq. (5) are computed as

(7) [ D x D t ] Λ Λ = 2 Λ 2 t x Λ 2 Λ t Λ x , [ D x 4 ] Λ Λ = 2 Λ 4 Λ x 4 8 Λ x 3 Λ x 3 + 6 2 Λ x 2 2 , [ D x 6 ] Λ Λ = 2 Λ 6 Λ x 6 12 Λ x 5 Λ x 5 + 30 2 Λ x 2 4 Λ x 4 20 3 Λ x 3 2 , [ D x 3 D y ] Λ Λ = 2 Λ 4 x 3 y Λ 2 Λ y 3 Λ x 3 6 Λ x 3 x 2 y Λ + 6 2 x y Λ 2 Λ x 2 , [ D y 2 ] Λ Λ = 2 Λ 2 Λ y 2 2 Λ y 2 , [ D x D y ] Λ Λ = 2 Λ 2 x y Λ 2 Λ x Λ y , [ D x 2 ] Λ Λ = 2 Λ 2 Λ x 2 2 Λ x 2 .

Taking (7) into account, we may reduce the proposed bilinear differential operator in (5) to a more simplified structure, as follows:

(8) 2 7 2 6 Λ x 6 Λ 12 7 2 Λ x 5 Λ x 5 + 5 7 6 7 2 Λ x 2 + Λ ( 2 φ 0 8 + 2 ) 4 Λ x 4 + 10 6 7 4 x 3 y Λ Λ 20 7 2 3 Λ x 3 2 10 7 ( 4 φ 0 8 + 2 2 ) Λ x + Λ y 6 3 Λ x 3 30 6 7 Λ x 3 x 2 y Λ + 15 7 ( 2 φ 0 8 + 2 ) 2 Λ x 2 2 + 10 3 6 7 2 x y Λ + Λ 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) × 2 Λ x 2 + 10 6 8 φ 0 2 x y Λ Λ + 10 8 Λ 2 t x Λ 10 6 2 2 Λ y 2 Λ 10 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) Λ x 2 10 8 6 φ 0 Λ y + Λ t × Λ x + 10 6 2 Λ y 2 = 0 .

3 Interactions of wave solutions for system (6)

The combination of Hirota’s bilinear method and some interaction solutions has always been one of the most interesting and efficient approaches to determining analytical solutions for equations. In this section, we aim to discover several lump solutions of various interactions for Eq. (1). For this purpose, five different structures are considered for the solution of the equation.

3.1 Class 1: Collision among two lump solutions

In this section, we construct the following combination of two lump solutions:

(9) Λ = κ 0 + κ 1 Ξ 1 2 + κ 2 Ξ 2 2 ,

where

Ξ 1 = α 1 x + β 1 y + ρ 1 t , Ξ 2 = α 2 x + β 2 y + ρ 2 t ,

and the unknown constants α i , β i , and ρ i are yet to be determined.

The following solutions for the unknowns are obtained by using symbolic software and plugging Eq. (9) into Eq. (8):

Item 1-1:

β 2 = α 2 ( 2 8 φ 0 + 2 ) 2 6 , κ 1 = 0 , ρ 2 = α 2 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 ,

and α 2 , κ 0 , and κ 2 are the free constants.

Substituting these results into (9) and then using transformation (2), we obtain

(10) Λ 1 = κ 0 + κ 2 t α 2 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 + x α 2 y α 2 ( 2 8 φ 0 + 2 ) 2 6 2 .

Numerical results illustrating the solution, using (10) and (2), and taking 2 = 0.9 , 6 = 0.2 , 7 = 0.2 , 8 = 0.25 , φ 0 = ϑ 0 = 0.3 , along with κ 0 = 1.4 , κ 2 = 0.8 , α 2 = 1.5 , are depicted in Figure 1.

Figure 1 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    1
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{1}\left(x,y,t)
                        
                      using (10) and (2).
Figure 1

Time evolution of the obtained solution φ 1 ( x , y , t ) using (10) and (2).

Item 1-2:

β 1 = α 1 ( 2 8 φ 0 + 2 ) 2 6 , β 2 = α 2 ( 2 8 φ 0 + 2 ) 2 6 , ρ 1 = α 1 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 , ρ 2 = α 2 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 ,

and α 1 , α 2 , κ 0 , κ 1 , and κ 2 are the free constants.

Substituting these results in (9) and then using transformation (2), we obtain

(11) Λ 2 = κ 0 + κ 1 t α 1 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 + x α 1 y α 1 ( 2 8 φ 0 + 2 ) 2 6 2 + κ 2 t α 2 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 + x α 2 y α 2 ( 2 8 φ 0 + 2 ) 2 6 2 .

Numerical results illustrating the solution, using (11) and (2), and taking 2 = 0.2 , 6 = 0.1 , 7 = 0.2 , 8 = 0.05 , φ 0 = ϑ 0 = 0.3 , along with κ 0 = 6.5 , κ 1 = 1.8 , κ 2 = 2.6 , α 1 = 1.75 , and α 2 = 1.5 , are the depicted in Figure 2.

Figure 2 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    2
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{2}\left(x,y,t)
                        
                      using (11) and (2).
Figure 2

Time evolution of the obtained solution φ 2 ( x , y , t ) using (11) and (2).

Item 1-3:

β 1 = α 1 β 2 α 2 , κ 0 = 0 , κ 2 = κ 1 α 1 2 α 2 2 , ρ 1 = ( 2 8 2 α 2 2 φ 0 2 + α 2 ( ( 2 2 φ 0 + 2 6 ϑ 0 ) α 2 + 2 β 2 6 φ 0 + ρ 2 ) 8 2 6 2 β 2 2 ) α 1 α 2 2 8 ,

and κ 1 , α 1 , α 2 , β 2 , ρ 2 are the free constants.

Using these results in (9) and then utilizing transformation (2) yield

Λ 3 = κ 1 t 2 6 2 β 2 2 + ( 2 β 2 6 φ 0 + ρ 2 ) α 2 8 ( 2 2 φ 0 + 2 6 ϑ 0 ) α 2 2 + 2 8 2 α 2 2 φ 0 2 α 1 α 2 2 8 + x α 1 + y α 1 β 2 α 2 2 κ 1 α 1 2 ( t ρ 2 + x α 2 + y β 2 ) 2 α 2 2 .

Item 1-4:

κ 0 = 3 7 κ 1 8 φ 0 + 2 2 α 1 2 + β 1 6 α 1 κ 1 + κ 2 8 φ 0 + 2 2 α 2 + β 2 6 α 2 ( κ 1 α 1 2 + κ 2 α 2 2 ) 2 6 2 κ 1 κ 2 ( α 1 β 2 + α 2 β 1 ) 2 , ρ 1 = β 1 6 α 2 κ 2 ( α 2 8 φ 0 2 β 2 6 ) 8 κ 1 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 1 3 6 8 α 1 2 β 1 κ 1 φ 0 + α 1 ( 8 2 α 2 2 κ 2 φ 0 2 κ 2 α 2 2 ( 2 φ 0 + 6 ϑ 0 ) 8 + 6 2 ( κ 1 β 1 2 κ 2 β 2 2 ) ) 8 ( κ 1 α 1 2 + κ 2 α 2 2 ) , ρ 2 = β 2 6 α 1 κ 1 ( φ 0 8 α 1 + 2 β 1 6 ) 8 κ 2 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 2 3 6 8 α 2 2 β 2 κ 2 φ 0 + α 2 ( 8 2 α 1 2 κ 1 φ 0 2 α 1 2 κ 1 ( 2 φ 0 + 6 ϑ 0 ) 8 6 2 ( κ 1 β 1 2 κ 2 β 2 2 ) ) 8 ( κ 1 α 1 2 + κ 2 α 2 2 ) ,

and α 1 , α 2 , β 1 , β 2 , κ 1 , and κ 2 are the free constants.

Substituting these results into (9) and then using transformation (2), we obtain

Λ 4 = 3 7 κ 1 8 φ 0 + 2 2 α 1 2 + β 1 6 α 1 κ 1 + κ 2 8 φ 0 + 2 2 α 2 + β 2 6 α 2 ( κ 1 α 1 2 + κ 2 α 2 2 ) 2 6 2 κ 1 κ 2 ( α 1 β 2 + α 2 β 1 ) 2 + κ 1 t β 1 6 α 2 κ 2 ( α 2 8 φ 0 2 β 2 6 ) 8 κ 1 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 1 3 6 8 α 1 2 β 1 κ 1 φ 0 + α 1 ( 8 2 α 2 2 κ 2 φ 0 2 κ 2 α 2 2 ( 2 φ 0 + 6 ϑ 0 ) 8 + 6 2 ( κ 1 β 1 2 κ 2 β 2 2 ) ) 8 ( κ 1 α 1 2 + κ 2 α 2 2 ) + x α 1 + y β 1 2

+ κ 2 t β 2 6 α 1 κ 1 ( φ 0 8 α 1 + 2 β 1 6 ) 8 κ 2 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 2 3 6 8 α 2 2 β 2 κ 2 φ 0 + α 2 ( 8 2 α 1 2 κ 1 φ 0 2 α 1 2 κ 1 ( 2 φ 0 + 6 ϑ 0 ) 8 6 2 ( κ 1 β 1 2 κ 2 β 2 2 ) ) 8 ( κ 1 α 1 2 + κ 2 α 2 2 ) + x α 2 + y β 2 2 .

It is noteworthy to note that although the structure (9) employed in our study bears some parallels to that of the publications [3234], our obtained results are more thorough and in general distinct from those reported in these articles.

3.2 Class 2: Collision among two lump solutions and stripe soliton

In this section, we construct a test function of

(12) Λ = κ 0 + Ξ 1 2 + κ 1 Ξ 2 2 + κ 2 exp ( Ξ 3 ) ,

where

Ξ 1 = α 1 x + β 1 y + ρ 1 t , Ξ 2 = α 2 x + β 2 y + ρ 2 t , Ξ 3 = α 3 x + β 3 y + ρ 3 t .

The following solutions for the unknowns are obtained by using symbolic software and plugging Eq. (12) into Eq. (8):

Item 2-1:

β 1 = α 1 ( 2 8 φ 0 + 2 ) 2 6 , β 3 = α 3 ( 2 7 α 3 2 + 2 8 φ 0 + 2 ) 2 6 , κ 1 = 0 , ρ 1 = α 1 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 , ρ 3 = 4 8 2 φ 0 2 + 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 3 4 5 + 4 2 7 α 3 2 + 2 2 α 3 4 8

and α 1 , α 3 , κ 0 , and κ 2 are the free constants.

By considering these results in (12) and subsequently applying transformation (2), we obtain

(13) Λ 5 = κ 0 + t α 1 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 + x α 1 y α 1 ( 2 8 φ 0 + 2 ) 2 6 2 + κ 2 exp t 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 3 4 5 + 4 2 7 α 3 2 + 2 2 α 3 4 8 + x α 3 y α 3 ( 2 7 α 3 2 + 2 8 φ 0 + 2 ) 2 6 .

Numerical results illustrating the solution, using (13) and (2), and taking 2 = 1.4 , 6 = 2.8 , 7 = 0.9 , 8 = 0.3 , φ 0 = ϑ 0 = 0.3 , along with κ 0 = 0.3 , κ 2 = 1.2 , α 1 = 0.35 , α 3 = 0.22 , are depicted in Figure 3.

Figure 3 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    5
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{5}\left(x,y,t)
                        
                      using (13) and (2).
Figure 3

Time evolution of the obtained solution φ 5 ( x , y , t ) using (13) and (2).

Item 2-2:

β 1 = α 1 ( 3 2 7 α 2 α 3 4 + 2 7 2 α 2 α 3 6 + 2 6 2 β 3 ( α 3 β 2 + α 2 β 3 ) + 7 α 3 3 ( 6 ( α 3 β 2 + 4 α 2 β 3 ) + 6 8 α 2 α 3 φ 0 ) ) 6 α 3 ( 7 α 2 α 3 3 + 2 6 ( α 3 β 2 α 2 β 3 ) ) ,

κ 0 = 16 α 1 2 6 β 3 + 1 2 α 3 ( 2 7 α 3 2 + 2 8 φ 0 ) 7 2 α 2 2 α 3 6 + 6 2 ( α 3 β 2 α 2 β 3 ) 2 + 2 7 α 2 2 α 3 3 6 β 3 + 7 α 2 α 3 4 6 β 2 + 3 2 α 2 ( 2 + 2 8 φ 0 ) ( 7 α 2 α 3 4 + 2 6 α 3 ( α 3 β 2 α 2 β 3 ) ) 2 ( 4 6 β 3 + α 3 ( 2 2 + 7 α 3 2 + 4 8 φ 0 ) ) ,

κ 1 = 3 ( 7 α 3 3 + 4 8 α 3 φ 0 + 2 2 α 3 + 4 6 β 3 ) 7 α 1 2 α 3 3 ( 7 α 2 α 3 3 + 2 6 α 2 β 3 2 6 α 3 β 2 ) 2 ,

ρ 1 = α 1 6 7 α 3 5 6 β 2 ( 3 2 + 5 8 φ 0 ) + 7 α 3 2 6 β 2 5 α 2 3 2 10 + 8 φ 0 7 2 α 2 α 3 4 + 8 α 2 ( 6 ϑ 0 φ 0 ( 2 2 + 5 8 φ 0 ) ) × ( 2 6 α 3 β 3 2 ( 6 β 2 + 8 α 2 φ 0 ) + 7 α 3 4 β 3 ( 8 6 β 2 + α 2 ( 3 2 + 2 8 φ 0 ) ) + 2 6 2 α 2 β 3 3 + α 3 2 ( 2 8 ( α 3 β 2 α 2 β 3 ) φ 0 ( 2 + 8 φ 0 ) + 6 ( 3 7 α 2 α 3 β 3 2 + 2 8 ( ( α 3 β 2 α 2 β 3 ) ϑ 0 + β 2 β 3 φ 0 ) ) ) ) 4 α 3 2 1 2 7 α 2 α 3 3 + 6 α 3 β 2 6 α 2 β 3 8 ,

ρ 2 = 7 2 α 2 α 3 6 + 2 6 7 α 2 α 3 3 β 3 + 6 2 β 3 ( 2 α 3 β 2 + α 2 β 3 ) + 7 α 3 4 6 β 2 + 3 2 α 2 ( 2 + 2 8 φ 0 ) + 8 α 3 2 ( α 2 φ 0 ( 2 + 8 φ 0 ) + 6 ( α 2 ϑ 0 + β 2 φ 0 ) ) 8 α 3 2 ,

ρ 3 = 2 7 2 α 3 6 5 7 ( 2 8 φ 0 + 2 ) α 3 4 10 6 7 α 3 3 β 3 10 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 3 2 10 6 8 α 3 β 3 φ 0 + 10 6 2 β 3 2 10 8 α 3 ,

and α 1 , α 2 , α 3 , β 2 , β 3 , and κ 2 are the free constants.

Integrating these results in (12) and then applying transformation (2) yield the analytic solution Λ 6 to the model.

Item 2-3:

β 1 = α 1 ( 2 2 + 3 7 α 3 2 + 4 8 φ 0 ) 4 6 , β 2 = α 2 ( 2 2 + 3 7 α 3 2 + 4 8 φ 0 ) 4 6 , β 3 = α 3 ( α 3 2 7 + 4 φ 0 8 + 2 2 ) 4 6 , ρ 1 = α 1 8 ( φ 0 ( 9 α 3 2 7 + 2 2 ) 4 6 ϑ 0 ) + 3 2 α 3 2 7 + 2 2 + 4 φ 0 2 8 2 4 8 , ρ 2 = α 2 8 ( φ 0 ( 9 α 3 2 7 + 2 2 ) 4 6 ϑ 0 ) + 3 2 α 3 2 7 + 2 2 + 4 φ 0 2 8 2 4 8 , ρ 3 = 4 8 2 φ 0 2 + ( 3 7 α 3 2 φ 0 + 2 2 φ 0 4 6 ϑ 0 ) 8 + 9 7 2 α 3 4 20 + 2 7 α 3 2 + 2 2 α 3 4 8 , κ 1 = α 1 2 α 2 2 ,

and α 1 , α 2 , α 3 , κ 0 , and κ 2 are the free constants.

Taking these results in (12) and then using transformation (2), we obtain

Λ 7 = κ 0 + t 4 8 2 φ 0 2 + 3 7 α 3 2 2 + 2 2 + ( 9 7 α 3 2 φ 0 + 2 2 φ 0 4 6 ϑ 0 ) 8 α 1 4 8 + x α 1 y 3 7 α 3 2 2 + 2 8 φ 0 + 2 α 1 2 6 2 α 1 2 α 2 2 t 4 8 2 φ 0 2 + 3 7 α 3 2 2 + 2 2 + ( 9 7 α 3 2 φ 0 + 2 2 φ 0 4 6 ϑ 0 ) 8 α 2 4 8 + x α 2 y 3 7 α 3 2 2 + 2 8 φ 0 + 2 α 2 2 6 2 + κ 2 exp t 4 8 2 φ 0 2 + 9 7 2 α 3 4 20 + 2 7 α 3 2 + 2 2 ( 3 7 α 3 2 φ 0 + 2 2 φ 0 4 6 ϑ 0 ) 8 α 3 4 8 + x α 3 y α 3 7 α 3 2 2 + 2 8 φ 0 + 2 2 6 .

Item 2-4:

β 1 = α 1 ( 2 8 φ 0 + 2 ) 2 6 , β 2 = α 2 ( 2 8 φ 0 + 2 ) 2 6 , β 3 = α 3 ( 2 7 α 3 2 + 2 8 φ 0 + 2 ) 2 6 , ρ 1 = α 1 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 , ρ 2 = ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) α 2 4 8 , ρ 3 = 4 8 2 φ 0 2 + 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 3 4 5 + 4 2 7 α 3 2 + 2 2 α 3 4 8 ,

and α 1 , α 2 , α 3 , κ 0 , κ 1 , and κ 2 are the free constants.

Taking these results in (12) and then using transformation (2), we obtain

(14) Λ 8 = κ 0 + t α 1 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 + x α 1 y α 1 ( 2 8 φ 0 + 2 ) 2 6 2 + κ 1 t ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) α 2 4 8 + x α 2 y α 2 ( 2 8 φ 0 + 2 ) 2 6 2 + κ 2 exp t 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 3 4 5 + 4 2 7 α 3 2 + 2 2 α 3 4 8 + x α 3 y α 3 ( 2 7 α 3 2 + 2 8 φ 0 + 2 ) 2 6

Numerical results illustrating the solution, using (14) and (2), and taking 2 = 0.4 , 6 = 0.8 , 7 = 0.9 , 8 = 0.17 , φ 0 = ϑ 0 = 0.3 , along with κ 0 = 0.5 , κ 1 = 0.2 , κ 2 = 0.6 , α 1 = 0.75 , α 2 = 2.2 , and α 3 = 0.5 , are the depicted in Figure 4.

Figure 4 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    8
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{8}\left(x,y,t)
                        
                      using (14) and (2).
Figure 4

Time evolution of the obtained solution φ 8 ( x , y , t ) using (14) and (2).

3.3 Class 3: Collision among two stripe solitons

In this section, we consider the following structure:

(15) Λ = 1 + exp ( Ξ 1 ) + exp ( Ξ 2 ) + κ 0 exp ( Ξ 1 + Ξ 2 ) ,

where

Ξ 1 = α 1 x + β 1 y + ρ 1 t , Ξ 2 = α 2 x + β 2 y + ρ 2 t .

The following solutions for the unknowns are obtained by using symbolic software and plugging Eq. (15) into Eq. (8):

Item 3-1:

κ 0 = 2 7 2 α 1 6 α 2 2 6 7 2 α 1 5 α 2 3 + 2 4 7 α 2 3 + 3 8 φ 0 + 2 2 α 2 + 6 β 2 α 2 7 α 1 4 + 4 3 7 α 2 3 2 + 3 8 φ 0 2 2 α 2 + 6 β 1 3 β 2 2 α 2 2 7 α 1 3 + 2 7 2 α 2 6 + 3 7 ( 2 8 φ 0 + 2 ) α 2 4 6 β 1 2 β 2 3 7 6 α 2 3 + 2 6 2 β 2 2 α 1 2 + 2 β 1 ( 6 7 α 2 4 2 6 2 α 2 β 2 ) α 1 + 2 6 2 α 2 2 β 1 2 2 7 2 α 1 6 α 2 2 + 6 7 2 α 1 5 α 2 3 + 2 4 7 α 2 3 + 3 8 φ 0 + 2 2 α 2 + 6 β 2 α 2 7 α 1 4 + 4 3 7 α 2 3 2 + 3 8 φ 0 + 2 2 α 2 + 6 β 1 + 3 β 2 2 α 2 2 7 α 1 3 + 2 7 2 α 2 6 + 3 7 ( 2 8 φ 0 + 2 ) α 2 4 + 6 β 1 + 2 β 2 3 7 6 α 2 3 + 2 6 2 β 2 2 α 1 2 + 2 β 1 ( 6 7 α 2 4 2 6 2 α 2 β 2 ) α 1 + 2 6 2 α 2 2 β 1 2 ,

ρ 1 = 2 7 2 α 1 6 5 7 ( 2 8 φ 0 + 2 ) α 1 4 10 6 7 α 1 3 β 1 10 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 1 2 10 6 8 α 1 β 1 φ 0 + 10 6 2 β 1 2 10 8 α 1 ,

ρ 2 = 2 7 2 α 2 6 5 7 ( 2 8 φ 0 + 2 ) α 2 4 10 6 7 α 2 3 β 2 10 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 2 2 10 6 8 α 2 β 2 φ 0 + 10 6 2 β 2 2 10 8 α 2 ,

and α 1 , α 2 , β 1 , β 2 , and κ 0 are the free constants.

Taking these results in (15) and then using transformation (2), it is secured that

(16) Λ 9 = 1 + Δ + Δ + 2 7 2 α 1 6 α 2 2 6 7 2 α 1 5 α 2 3 + 2 4 7 α 2 3 + 3 8 φ 0 + 2 2 α 2 + 6 β 2 α 2 7 α 1 4 + 4 3 7 α 2 3 2 + 3 8 φ 0 2 2 α 2 + 6 β 1 3 β 2 2 α 2 2 7 α 1 3 + 2 7 2 α 2 6 + 3 7 ( 2 8 φ 0 + 2 ) α 2 4 6 β 1 2 β 2 3 7 6 α 2 3 + 2 6 2 β 2 2 α 1 2 + 2 β 1 ( 6 7 α 2 4 2 6 2 α 2 β 2 ) α 1 + 2 6 2 α 2 2 β 1 2 2 7 2 α 1 6 α 2 2 + 6 7 2 α 1 5 α 2 3 + 2 4 7 α 2 3 + 3 8 φ 0 + 2 2 α 2 + 6 β 2 α 2 7 α 1 4 + 4 3 7 α 2 3 2 + 3 8 φ 0 + 2 2 α 2 + 6 β 1 + 3 β 2 2 α 2 2 7 α 1 3 + 2 7 2 α 2 6 + 3 7 ( 2 8 φ 0 + 2 ) α 2 4 + 6 β 1 + 2 β 2 3 7 6 α 2 3 + 2 6 2 β 2 2 α 1 2 + 2 β 1 ( 6 7 α 2 4 2 6 2 α 2 β 2 ) α 1 + 2 6 2 α 2 2 β 1 2 Δ Δ ,

where

Δ = exp t 2 7 2 α 1 6 5 7 ( 2 8 φ 0 + 2 ) α 1 4 10 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 1 2 10 6 7 α 1 3 β 1 10 6 8 α 1 β 1 φ 0 + 10 6 2 β 1 2 10 8 α 1 + x α 1 + y β 1 ,

Δ = exp t 10 6 2 β 2 2 2 7 2 α 2 6 5 7 ( 2 8 φ 0 + 2 ) α 2 4 10 6 7 α 2 3 β 2 10 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 2 2 10 6 8 α 2 β 2 φ 0 10 8 α 2 + x α 2 + y β 2 .

Numerical results illustrating the solution, using (16) and (2), and taking 2 = 0.7 , 6 = 0.7 , 7 = 0.6 , 8 = 0.2 , φ 0 = ϑ 0 = 0.3 , along with α 3 = 0.8 , κ 1 = 1.5 , κ 3 = 0.4 , are depicted in Figure 5.

Figure 5 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    9
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{9}\left(x,y,t)
                        
                      using (16) and (2).
Figure 5

Time evolution of the obtained solution φ 9 ( x , y , t ) using (16) and (2).

3.4 Class 4: Collision among double-stripe solitons and stripe soliton

In this part, we construct a test function of

(17) Λ = κ 0 + κ 1 cosh ( Ξ 1 ) + κ 2 cos ( Ξ 2 ) + κ 3 cosh ( Ξ 3 ) ,

where

Ξ 1 = α 1 x + β 1 y + ρ 1 t , Ξ 2 = α 2 x + β 2 y + ρ 2 t , Ξ 3 = α 3 x + β 3 y + ρ 3 t .

The following solutions for the unknowns are obtained by using symbolic software and plugging Eq. (17) into Eq. (8):

Item 4-1:

κ 0 = 0 , κ 1 = 0 , κ 2 = 0 , ρ 3 = 16 7 2 α 3 6 10 7 ( 2 8 φ 0 + 2 ) α 3 4 20 6 7 α 3 3 β 3 5 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 3 2 5 6 8 α 3 β 3 φ 0 + 5 6 2 β 3 2 5 8 α 3 ,

and α 3 , β 3 , and κ 3 are the free constants.

Incorporating these results in (17) and then using transformation (2), we obtain

(18) Λ 10 = κ 3 cosh t 16 7 2 α 3 6 10 7 ( 2 8 φ 0 + 2 ) α 3 4 20 6 7 α 3 3 β 3 5 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 3 2 5 6 8 α 3 β 3 φ 0 + 5 6 2 β 3 2 5 8 α 3 + x α 3 + y β 3 .

Item 4-2:

β 3 = α 3 ( 2 α 3 2 7 + 2 8 φ 0 + 2 ) 2 6 , κ 1 = 0 , κ 2 = 0 , ρ 3 = α 3 4 8 2 φ 0 2 + 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 α 3 4 7 2 5 + 4 α 3 2 7 2 + 2 2 4 8 ,

and α 3 , κ 0 , and κ 3 are the free constants.

Considering these results in (17) and then using transformation (2), we obtain

(19) Λ 11 = κ 0 + κ 3 cosh t α 3 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 α 3 4 7 2 5 + 4 α 3 2 7 2 + 2 2 4 8 + x α 3 y α 3 ( 2 α 3 2 7 + 2 8 φ 0 + 2 ) 2 6 .

Numerical results illustrating the solution, using (19) and (2), and taking 2 = 0.7 , 6 = 0.8 , 7 = 0.9 , 8 = 0.1 , φ 0 = ϑ 0 = 0.3 , along with α 3 = 0.5 , κ 0 = 0.3 , κ 3 = 0.6 , are depicted in Figure 6.

Figure 6 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    11
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{11}\left(x,y,t)
                        
                      using (19) and (2).
Figure 6

Time evolution of the obtained solution φ 11 ( x , y , t ) using (19) and (2).

Item 4-3:

κ 0 = 0 , κ 1 = 0 , κ 3 = 0 , ρ 2 = 16 7 2 α 2 6 + 10 7 ( 2 8 φ 0 + 2 ) α 2 4 + 20 6 7 α 2 3 β 2 5 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 2 2 5 6 8 α 2 β 2 φ 0 + 5 6 2 β 2 2 5 8 α 2 ,

and α 2 , β 2 , and κ 2 are the free constants.

Taking these results in (17) and then using transformation (2), we obtain

(20) Λ 12 = κ 2 cos t 16 7 2 α 2 6 + 10 7 ( 2 8 φ 0 + 2 ) α 2 4 + 20 6 7 α 2 3 β 2 5 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 2 2 5 6 8 α 2 β 2 φ 0 + 5 6 2 β 2 2 5 8 α 2 + x α 2 + y β 2 .

Item 4-4:

β 2 = α 2 ( 2 7 α 2 2 + 2 8 φ 0 + 2 ) 2 6 , κ 1 = 0 , κ 3 = 0 , ρ 2 = 4 8 2 φ 0 2 + 2 ( 6 7 α 2 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 2 4 5 4 2 7 α 2 2 + 2 2 α 2 4 8 ,

and α 2 , κ 0 , and κ 2 are the free constants.

Taking these results in (17) and then using transformation (2), it reads

(21) Λ 13 = κ 0 + κ 2 cos t 2 ( 6 7 α 2 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 4 8 2 φ 0 2 + 36 7 2 α 2 4 5 4 2 7 α 2 2 + 2 2 α 2 4 8 + x α 2 y α 2 ( 2 7 α 2 2 + 2 8 φ 0 + 2 ) 2 6 .

Numerical results illustrating the solution, using (21) and (2), and taking 2 = 0.7 , 6 = 0.8 , 7 = 0.9 , 8 = 0.1 , φ 0 = ϑ 0 = 0.3 , along with α 2 = 0.5 , κ 0 = 0.3 , κ 2 = 0.6 , are depicted in Figure 7.

Figure 7 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    13
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{13}\left(x,y,t)
                        
                      using (21) and (2).
Figure 7

Time evolution of the obtained solution φ 13 ( x , y , t ) using (21) and (2).

Item 4-5:

β 2 = α 2 ( 2 7 α 2 2 + 6 7 α 3 2 + 2 φ 0 8 + 2 ) 2 6 , β 3 = α 3 ( 6 7 α 2 2 + 2 7 α 3 2 + 2 φ 0 8 + 2 ) 2 6 , κ 0 = 0 , κ 1 = 0 , ρ 2 = α 2 36 1 5 α 2 4 2 α 3 2 α 2 2 + α 3 4 7 2 4 ( α 2 2 3 α 3 2 ) ( 3 φ 0 8 + 2 ) 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 + 2 2 4 8 , ρ 3 = α 3 36 α 2 4 2 α 3 2 α 2 2 + 1 5 α 3 4 7 2 12 ( 3 φ 0 8 + 2 ) α 2 2 α 3 2 3 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 + 2 2 4 8 ,

and α 1 , α 2 , κ 2 , and κ 3 are the free constants.

Considering these results in (17) and then using transformation (2), we achieve

(22) Λ 14 = κ 2 cos t α 2 2 2 + 36 1 5 α 2 4 2 α 3 2 α 2 2 + α 3 4 7 2 4 ( α 2 2 3 α 3 2 ) ( 3 φ 0 8 + 2 ) 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 4 8 + x α 2 y α 2 2 7 α 2 2 + 6 7 α 3 2 + 2 φ 0 8 + 2 2 6 + κ 3 cosh t α 3 2 2 + 36 α 2 4 2 α 3 2 α 2 2 + 1 5 α 3 4 7 2 12 ( 3 φ 0 8 + 2 ) α 2 2 α 3 2 3 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 4 8 + x α 3 y α 3 6 7 α 2 2 + 2 7 α 3 2 + 2 φ 0 8 + 2 2 6 .

Numerical results illustrating the solution, using (22) and (2), and taking 2 = 0.1 , 6 = 0.7 , 7 = 0.6 , 8 = 0.1 , φ 0 = ϑ 0 = 0.3 , along with α 2 = 0.8 , α 2 = 0.6 , κ 2 = 0.5 , κ 3 = 0.2 , are depicted in Figure 8.

Figure 8 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    14
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{14}\left(x,y,t)
                        
                      using (22) and (2).
Figure 8

Time evolution of the obtained solution φ 14 ( x , y , t ) using (22) and (2).

Item 4-6:

β 2 = ( 7 α 2 2 + 3 7 α 3 2 + 4 φ 0 8 + 2 2 ) α 2 4 6 , β 3 = α 3 ( 3 7 α 2 2 + 7 α 3 2 + 4 φ 0 8 + 2 2 ) 4 6 , κ 1 = 0 , κ 2 = α 3 2 κ 3 α 2 2 , ρ 2 = 9 20 α 2 4 9 2 α 3 2 α 2 2 + 9 4 α 3 4 7 2 ( α 2 2 3 α 3 2 ) ( 3 φ 0 8 + 2 ) 7 + 4 8 2 φ 0 2 + ( 2 2 φ 0 4 6 ϑ 0 ) 8 + 2 2 α 2 4 8 , ρ 3 = 9 4 α 2 4 9 2 α 3 2 α 2 2 + 9 20 α 3 4 7 2 ( 3 φ 0 8 + 2 ) ( 3 α 2 2 α 3 2 ) 7 + 4 8 2 φ 0 2 + ( 2 2 φ 0 4 6 ϑ 0 ) 8 + 2 2 α 3 4 8 ,

and α 2 , α 3 , κ 0 , and κ 3 are the free constants.

Considering these results in (17) and then using transformation (2), we obtain

Λ 15 = κ 0 α 3 2 κ 3 α 2 2 cos t 2 2 + 9 20 α 2 4 9 2 α 3 2 α 2 2 + 9 4 α 3 4 7 2 ( α 2 2 3 α 3 2 ) ( 3 φ 0 8 + 2 ) 7 + 4 8 2 φ 0 2 + ( 2 2 φ 0 4 6 ϑ 0 ) 8 α 2 4 8 + x α 2 y α 2 7 α 2 2 + 3 7 α 3 2 + 4 φ 0 8 + 2 2 4 6 + κ 3 cosh t 2 2 + 9 4 α 2 4 9 2 α 3 2 α 2 2 + 9 20 α 3 4 7 2 ( 3 φ 0 8 + 2 ) ( 3 α 2 2 α 3 2 ) 7 + 4 8 2 φ 0 2 + ( 2 2 φ 0 4 6 ϑ 0 ) 8 α 3 4 8 + x α 3 y α 3 3 7 α 2 2 + 7 α 3 2 + 4 φ 0 8 + 2 2 4 6 .

Item 4-7:

β 1 = α 1 ( 2 7 α 1 2 + 2 φ 0 8 + 2 ) 2 6 , β 3 = α 3 ( 2 7 α 3 2 + 2 φ 0 8 + 2 ) 2 6 , κ 2 = 0 , ρ 1 = 4 8 2 φ 0 2 + 2 ( 6 7 α 1 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 1 4 5 + 4 7 α 1 2 2 + 2 2 α 1 4 8 ,

ρ 3 = 4 8 2 φ 0 2 + 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 3 4 5 + 4 7 α 3 2 2 + 2 2 α 3 4 8 ,

and α 1 , α 2 , κ 0 , κ 1 , and κ 3 are the free constants.

Considering these results in (17) and then using transformation (2), we obtain

Λ 16 = κ 0 + κ 1 cosh t 2 ( 6 7 α 1 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 1 4 5 + 4 7 α 1 2 2 + 2 2 α 1 4 8 + x α 1 y α 1 ( 2 7 α 1 2 + 2 φ 0 8 + 2 ) 2 6 + κ 3 cosh t 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 3 4 5 + 4 7 α 3 2 2 + 2 2 α 3 4 8 + x α 3 y α 3 ( 2 7 α 3 2 + 2 φ 0 8 + 2 ) 2 6 .

Item 4-8:

β 1 = α 1 ( 2 7 α 1 2 + 2 φ 0 8 + 2 ) 2 6 , β 2 = α 2 ( 2 7 α 2 2 + 2 φ 0 8 + 2 ) 2 6 , β 3 = α 3 ( 2 7 α 3 2 + 2 φ 0 8 + 2 ) 2 6 , ρ 1 = 4 8 2 φ 0 2 + 2 ( 6 7 α 1 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 1 4 5 + 4 7 α 1 2 2 + 2 2 α 1 4 8 , ρ 2 = 4 8 2 φ 0 2 + 2 ( 6 7 α 2 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 2 4 5 4 7 2 α 2 2 + 2 2 α 2 4 8 , ρ 3 = 4 8 2 φ 0 2 + 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 3 4 5 + 4 7 α 3 2 2 + 2 2 α 3 4 8 ,

and α 1 , α 2 , α 3 , κ 0 , κ 1 , κ 2 , and κ 3 are the free constants.

Considering these results in (17) and then using transformation (2), we obtain

(23) Λ 17 = κ 0 + κ 1 cosh t 2 ( 6 7 α 1 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 1 4 5 + 4 7 α 1 2 2 + 2 2 α 1 4 8 + x α 1 y α 1 ( 2 7 α 1 2 + 2 φ 0 8 + 2 ) 2 6 + κ 2 cos t 2 ( 6 7 α 2 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 2 4 5 4 7 2 α 2 2 + 2 2 α 2 4 8 + x α 2 y α 2 ( 2 7 α 2 2 + 2 φ 0 8 + 2 ) 2 6 + κ 3 cosh t 2 ( 6 7 α 1 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 3 4 5 + 4 7 α 3 2 2 + 2 2 α 3 4 8 + x α 3 y α 3 ( 2 7 α 3 2 + 2 φ 0 8 + 2 ) 2 6 .

Numerical results illustrating the solution, using (23) and (2), and taking 2 = 0.1 , 6 = 0.2 , 7 = 0.3 , 8 = 0.05 , φ 0 = ϑ 0 = 0.3 , along with α 1 = 0.8 , α 2 = 0.5 , α 3 = 0.2 , κ 0 = 3.5 , κ 1 = 1.2 , κ 2 = 0.5 , κ 3 = 0.7 , are depicted in Figure 9.

Figure 9 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    17
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{17}\left(x,y,t)
                        
                      using (23) and (2).
Figure 9

Time evolution of the obtained solution φ 17 ( x , y , t ) using (23) and (2).

3.5 Class 5: Collision among periodic, stripe soliton, and a double-stripe soliton

In this part, a formal structure is to be interpreted as

(24) Λ = κ 0 + κ 1 sin ( Ξ 1 ) + κ 2 exp ( Ξ 2 ) + κ 3 sinh ( Ξ 3 ) ,

where

Ξ 1 = α 1 x + β 1 y + ρ 1 t , Ξ 2 = α 2 x + β 2 y + ρ 2 t , Ξ 3 = α 3 x + β 3 y + ρ 3 t .

The following solutions for the unknowns are obtained by using symbolic software and plugging Eq. (24) into Eq. (8):

Item 5-1:

κ 1 = 0 , κ 3 = 0 , ρ 2 = 2 7 2 α 2 6 5 7 α 2 4 ( 2 φ 0 8 + 2 ) 10 6 7 α 2 3 β 2 10 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 2 2 10 6 8 α 2 β 2 φ 0 + 10 6 2 β 2 2 10 8 α 2 ,

and α 2 , β 2 , κ 0 , and κ 2 are the free constants.

Substituting these results in (28) and then using transformation (2), we obtain

(25) Λ 18 = κ 0 + κ 2 exp t 10 6 2 β 2 2 2 7 2 α 2 6 5 7 α 2 4 ( 2 φ 0 8 + 2 ) 10 6 7 α 2 3 β 2 10 8 ( 8 φ 0 2 + 2 φ 0 + 6 ϑ 0 ) α 2 2 10 6 8 α 2 β 2 φ 0 10 8 α 2 + x α 2 + y β 2 .

Item 5-2:

β 1 = α 1 ( 2 α 1 2 7 + 6 α 3 2 7 + 2 φ 0 8 + 2 ) 2 6 , β 3 = α 3 ( 6 α 1 2 7 + 2 α 3 2 7 + 2 φ 0 8 + 2 ) 2 6 , κ 0 = 0 , κ 2 = 0 , ρ 1 = 36 1 5 α 1 4 2 α 1 2 α 3 2 + α 3 4 7 2 4 ( α 1 2 3 α 3 2 ) ( 3 φ 0 8 + 2 ) 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 + 2 2 α 1 4 8 , ρ 3 = 36 α 1 4 2 α 1 2 α 3 2 + 1 5 α 3 4 7 2 12 α 1 2 α 3 2 3 ( 3 φ 0 8 + 2 ) 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 + 2 2 α 3 4 8 ,

and α 1 , α 3 , κ 1 , and κ 3 are the free constants.

Substituting these results into (28) and then using transformation (2), we obtain

Λ 19 = κ 1 sin t 2 2 + 36 1 5 α 1 4 2 α 1 2 α 3 2 + α 3 4 7 2 4 ( α 1 2 3 α 3 2 ) ( 3 φ 0 8 + 2 ) 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 α 1 4 8 + x α 1 y α 1 ( 2 α 1 2 7 + 6 α 3 2 7 + 2 φ 0 8 + 2 ) 2 6 + κ 3 sinh t 2 2 + 36 α 1 4 2 α 1 2 α 3 2 + 1 5 α 3 4 7 2 12 α 1 2 α 3 2 3 ( 3 φ 0 8 + 2 ) 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 α 3 4 8 + x α 3 y α 3 ( 6 α 1 2 7 + 2 α 3 2 7 + 2 φ 0 8 + 2 ) 2 6 .

Item 5-3:

β 2 = α 2 ( 2 7 α 2 2 + 2 φ 0 8 + 2 ) 2 6 , β 3 = α 3 ( 2 α 3 2 7 + 2 φ 0 8 + 2 ) 2 6 , κ 1 = 0 , ρ 2 = α 2 4 8 2 φ 0 2 + 2 ( 6 7 α 2 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 2 4 5 + 4 2 7 α 2 2 + 2 2 4 8 , ρ 3 = 4 8 2 φ 0 2 + 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 3 4 5 + 4 2 7 α 3 2 + 2 2 α 3 4 8 ,

and α 2 , α 3 , κ 0 , κ 2 , and κ 3 are the free constants.

Taking these results in (28) and then using transformation (2), it reads

Λ 20 = κ 0 + κ 2 exp t 2 ( 6 7 α 2 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 2 4 5 + 4 2 7 α 2 2 + 2 2 α 2 4 8 + x α 2 y α 2 ( 2 7 α 2 2 + 2 φ 0 8 + 2 ) 2 6 + κ 3 sinh t 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 3 4 5 + 4 2 7 α 3 2 + 2 2 α 3 4 8 + x α 3 y α 3 ( 2 α 3 2 7 + 2 φ 0 8 + 2 ) 2 6 .

Item 5-4:

β 1 = α 1 ( 2 α 1 2 7 + 2 φ 0 8 + 2 ) 2 6 , β 2 = α 2 ( 2 7 α 2 2 + 2 φ 0 8 + 2 ) 2 6 , κ 3 = 0 , ρ 1 = 4 8 2 φ 0 2 + 2 ( 6 7 α 1 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 1 4 5 4 2 7 α 1 2 + 2 2 α 1 4 8 , ρ 2 = α 2 4 8 2 φ 0 2 + 2 ( 6 7 α 2 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 2 4 5 + 4 2 7 α 2 2 + 2 2 4 8 ,

and α 1 , α 2 , κ 0 , κ 1 , κ 2 are the free constants.

Considering these results in (28) and then using transformation (2), we obtain

(26) Λ 21 = κ 0 + κ 1 sin t 2 ( 6 7 α 1 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 1 4 5 4 2 7 α 1 2 + 2 2 α 1 4 8 + x α 1 y α 1 ( 2 α 1 2 7 + 2 φ 0 8 + 2 ) 2 6 + κ 2 exp t 2 ( 6 7 α 2 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 4 8 2 φ 0 2 + 36 7 2 α 2 4 5 + 4 2 7 α 2 2 + 2 2 α 2 4 8 + x α 2 y α 2 ( 2 7 α 2 2 + 2 φ 0 8 + 2 ) 2 6 .

Numerical results illustrating the solution, using (26) and (2), and taking 2 = 1.1 , 6 = 1.8 , 7 = 1.6 , 8 = 0.4 , φ 0 = ϑ 0 = 0.3 , along with α 1 = 1.4 , α 2 = 0.3 , κ 0 = 3.7 , κ 1 = 1.7 , κ 2 = 2.3 , are depicted in Figure 10.

Figure 10 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    21
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{21}\left(x,y,t)
                        
                      using (26) and (2).
Figure 10

Time evolution of the obtained solution φ 21 ( x , y , t ) using (26) and (2).

Item 5-5:

β 1 = α 1 ( 2 α 1 2 7 + 2 φ 0 8 + 2 ) 2 6 , β 2 = α 2 ( 2 7 α 2 2 + 2 φ 0 8 + 2 ) 2 6 , β 3 = α 3 ( 2 α 3 2 7 + 2 φ 0 8 + 2 ) 2 6 , ρ 1 = 4 8 2 φ 0 2 + 2 ( 6 7 α 1 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 1 4 5 4 2 7 α 1 2 + 2 2 α 1 4 8 , ρ 2 = α 2 4 8 2 φ 0 2 + 2 ( 6 7 α 2 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 2 4 5 + 4 2 7 α 2 2 + 2 2 4 8 , ρ 3 = 4 8 2 φ 0 2 + 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 36 7 2 α 3 4 5 + 4 2 7 α 3 2 + 2 2 α 3 4 8 ,

and α 1 , α 2 , α 3 , κ 0 , κ 1 , and κ 2 are the free constants.

Considering these results in (28) and then using transformation (2), we obtain

(27) Λ 22 = κ 0 + κ 1 sin t 2 ( 6 7 α 1 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 2 2 + 4 8 2 φ 0 2 + 36 7 2 α 1 4 5 4 2 7 α 1 2 α 1 4 8 + x α 1 y α 1 ( 2 α 1 2 7 + 2 φ 0 8 + 2 ) 2 6 + κ 2 exp t 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 2 2 + 4 8 2 φ 0 2 + 36 7 2 α 3 4 5 + 4 2 7 α 3 2 α 2 4 8 + x α 2 y α 2 ( 2 7 α 2 2 + 2 φ 0 8 + 2 ) 2 6 + κ 3 sinh t 2 ( 6 7 α 3 2 φ 0 + 2 φ 0 2 6 ϑ 0 ) 8 + 2 2 + 4 8 2 φ 0 2 + 36 7 2 α 3 4 5 + 4 2 7 α 3 2 α 3 4 8 + x α 3 y α 3 ( 2 α 3 2 7 + 2 φ 0 8 + 2 ) 2 6 .

Numerical results illustrating the solution, using (27) and (2), and taking 2 = 6.95 , 6 = 1.3 , 7 = 0.6 , 8 = 3.3 , φ 0 = ϑ 0 = 0.3 , along with α 1 = 0.75 , α 2 = 0.95 , α 3 = 0.4 , κ 0 = 1.5 , κ 1 = 1.4 , κ 2 = 3.2 , are depicted in Figure 11.

Figure 11 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    22
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{22}\left(x,y,t)
                        
                      using (27) and (2).
Figure 11

Time evolution of the obtained solution φ 22 ( x , y , t ) using (27) and (2).

3.6 Class 6: Collision among lump, periodic, and a double-stripe soliton

In this part, we examine the following structure:

(28) Λ = κ 0 + κ 1 Ξ 1 2 + κ 2 cos ( Ξ 2 ) exp ( Ξ 3 ) ,

where

Ξ 1 = α 1 x + β 1 y + ρ 1 t , Ξ 2 = φ 0 x + φ 1 y + φ 2 t + φ 3 , Ξ 3 = θ 0 x + θ 1 y + θ 2 t .

The following solutions for the unknowns are obtained by utilizing symbolic software and plugging Eq. (28) into Eq.(8):

Item 6-1:

β 1 = α 1 ( 2 8 φ 0 + 2 ) 2 6 , β 2 = α 2 ( 2 α 2 2 7 + 6 7 α 3 2 + 2 8 φ 0 + 2 ) 2 6 , β 3 = α 3 ( 6 α 2 2 7 + 2 7 α 3 2 + 2 8 φ 0 + 2 ) 2 6 , ρ 1 = α 1 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 , ρ 2 = α 2 36 1 5 α 2 4 2 α 2 2 α 3 2 + α 3 4 7 2 4 ( α 2 2 3 α 3 2 ) ( 3 8 φ 0 + 2 ) 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 + 2 2 4 8 , ρ 3 = 36 α 2 4 2 α 2 2 α 3 2 + 1 5 α 3 4 7 2 12 ( 3 8 φ 0 + 2 ) α 2 2 α 3 2 3 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 + 2 2 α 3 4 8 ,

and α 1 , α 2 , α 3 , κ 0 , κ 1 , and κ 2 are the free constants.

Substituting these results into (28) and then using transformation (2), we obtain

(29) Λ 23 = κ 0 + κ 1 t α 1 ( 4 8 2 φ 0 2 + 2 2 8 φ 0 4 6 8 ϑ 0 + 2 2 ) 4 8 + x α 1 y α 1 ( 2 8 φ 0 + 2 ) 2 6 2 + κ 2 cos t 2 2 + 36 1 5 α 2 4 2 α 2 2 α 3 2 + α 3 4 7 2 4 ( α 2 2 3 α 3 2 ) ( 3 8 φ 0 + 2 ) 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 α 2 4 8 + x α 2 y α 2 2 8 φ 0 + 2 2 α 2 2 7 + 6 7 α 3 2 2 6 × exp t 2 2 + 36 α 2 4 2 α 2 2 α 3 2 + 1 5 α 3 4 7 2 12 ( 3 8 φ 0 + 2 ) α 2 2 α 3 2 3 7 + 4 8 2 φ 0 2 + 2 ( 2 φ 0 2 6 ϑ 0 ) 8 α 3 4 8 + x α 3 y α 3 2 8 φ 0 + 2 6 α 2 2 7 + 2 7 α 3 2 2 6 .

Numerical results illustrating the solution, using (29) and (2), and taking 2 = 1.1 , 6 = 1.8 , 7 = 1.6 , 8 = 0.3 , φ 0 = ϑ 0 = 0.3 , along with α 1 = 1.4 , α 2 = 0.3 , α 3 = 0.4 , κ 0 = 15 , κ 1 = 1.7 , κ 2 = 1.3 , κ 3 = 0.5 , are depicted in Figure 12.

Figure 12 
                  Time evolution of the obtained solution 
                        
                           
                           
                              
                                 
                                    φ
                                 
                                 
                                    22
                                 
                              
                              
                                 (
                                 
                                    x
                                    ,
                                    y
                                    ,
                                    t
                                 
                                 )
                              
                           
                           {\varphi }_{22}\left(x,y,t)
                        
                      using (29) and (2).
Figure 12

Time evolution of the obtained solution φ 22 ( x , y , t ) using (29) and (2).

As far as we know, the solutions we have discovered for Eq. (6) are totally different in terms of form and structure from previous studies. Furthermore, by incorporating all of the solutions reported in this research into the main equation, the correctness of them has been verified. Specific initial and boundary conditions for the (2+1)-dimensional Konopelchenko–Dubrovsky–Kaup–Kupershmidt system significantly influence the obtained solutions. The initial conditions are set to represent realistic physical scenarios, while the boundary conditions are chosen to ensure appropriate soliton interactions. These conditions significantly influence the characteristics and stability of the obtained solutions, including lump, stripe, and double-stripe solitons. Variations in these conditions can lead to distinct behaviors and dynamics of the solitons, underscoring their critical importance in modeling the system effectively.

4 Conclusion

There has recently been growing interest among mathematical physicists in generalized nonlinear equations due to their wide applications in various physical fields. The present article examines the KDKK system, an essential tool for describing a wide range of phenomena in the fields of fluid mechanics, plasma physics, and ocean dynamics. By selecting appropriate parameter values in the model, the KDKK system can be simplified into several significant nonlinear evolution equations. This study systematically generates various architectures of wave solutions, including combinations of interactions between lump, stripe, double-stripe, and periodic waves. In our analysis, we introduced arbitrary free parameters to explore a broad class of wave solutions derived from our mathematical framework. These parameters, although initially arbitrary, can be linked to physical characteristics pertinent to real-world systems in fluid mechanics and plasma dynamics. By anchoring these free parameters within the context of physical principles and phenomena, researchers can interpret the resulting wave solutions in the context of specific applications, thereby enhancing the relevance of our theoretical findings in practical settings. Additionally, graphical representations that are connected to the solutions are also provided. These demonstration simulations showed that the wave propagation of the derived solution can evolve regularly along a straight line at a particular angle with the spatial axes, even while their wave lengths, amplitudes, and velocities remain constant.

While this study has successfully developed novel wave solutions for the (2+1)-dimensional Konopelchenko–Dubrovsky–Kaup–Kupershmidt system, certain limitations must be acknowledged. The analysis primarily focused on specific classes of solutions, and the conditions under which these solutions hold may not cover all possible physical scenarios, particularly in complex or turbulent media where higher-order effects may become significant. Additionally, the practical applicability of the theoretical results may require further validation through experimental data or numerical simulations.

Future work could explore the incorporation of additional nonlinear effects and parameters to enhance the model’s realism in describing real-world phenomena. Investigating the stability of the derived solutions under various perturbations and initial conditions would provide deeper insights into their robustness. Furthermore, extending the framework to other nonlinear systems could lead to the discovery of a broader range of solution types and interactions, ultimately contributing to the understanding of complex dynamics in fluid mechanics, plasma physics, and other fields.

Acknowledgment

The author like to express sincere gratitude to the editor and the referees for their valuable insights and constructive feedback throughout the review process.

  1. Funding information: The author states no funding involved.

  2. Author contributions: The author has accepted responsibility for the entire content of this manuscript and approved its submission.

  3. Conflict of interest: The author states no conflict of interest.

  4. Data availability statement: Data sharing is not applicable to this article as no datasets were generated or analyzed during the current study.

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Received: 2024-08-25
Revised: 2025-02-24
Accepted: 2025-03-28
Published Online: 2025-05-21

© 2025 the author(s), published by De Gruyter

This work is licensed under the Creative Commons Attribution 4.0 International License.

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