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An optimal system of group-invariant solutions and conserved quantities of a nonlinear fifth-order integrable equation

  • Innocent Simbanefayi and Chaudry Masood Khalique EMAIL logo
Published/Copyright: December 3, 2020

Abstract

In this work, we perform Lie group analysis on a fifth-order integrable nonlinear partial differential equation, which was recently introduced in the literature and contains two dispersive terms. We determine a one-parameter group of transformations, an optimal system of group invariant solutions, and derive the corresponding analytic solutions. Topological kink, periodic and power series solutions are obtained. The existence of a variational principle for the underlying equation is proven using Helmholtz conditions and, thereafter, both local and nonlocal conserved quantities are obtained by utilising Noether’s theorem and a homotopy integral approach.

1 Introduction

The importance of studying nonlinear partial differential equations (NLPDEs) cannot be overemphasised as they model behaviours and interrelations of physical quantities. A large number of scholars continue to research different aspects of NLPDEs, see, for example, ref. [1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27,28,29,30,31,32,33,34,35,36,37,38,39,40,41,42,43,44,45,46,47,48,49]. As the NLPDEs model physical phenomena of the real world, determining their exact solutions is therefore a step further in understanding the world around us. Famous NLPDEs include the Korteweg–de Vries (KdV) equation [3], which replicates the propagation of waves in shallow water, the Benjamin–Bona–Mahony (BBM) equation [4], which models long surface gravity waves with a small amplitude, the Kadomtsev–Petviashvili (KP) equation [5], a model of water waves in cases where the ratio of water depth to wavelength is very small and the Camassa–Holm equation [6], which models shallow water waves, just to mention a few.

The most general form of a fifth-order KdV equation reads [7]

(1.1) u t + α u 2 u x + ν u x u x x + γ u u x x x + u x x x x x = 0

with arbitrary real constants α , ν and γ . Equation (1.1) models long waves propagating in shallow water and in the presence of gravity. Several famous fifth-order KdV equations emanate from equation (1.1), for instance, the fifth-order Sawada–Kotera equation [8]

u t + 45 u 2 u x + 15 u x u x x + 15 u u x x x + u x x x x x = 0

occurs when α = 3 ν , ν = γ and γ = 15 . On the other hand, when α = 5 / 2 ν , ν = 5 / 4 γ and γ = 20 , we have the nonlinear fifth-order Kaup–Kupershmidt equation [9]

u t + 20 u 2 u x + 25 u x u x x + 10 u u x x x + u x x x x x = 0 .

In this article, we study a newly formulated integrable fifth-order equation

(1.2) F β u x x x 4 u t u x x x 12 u x x u t x 8 u x u t x x u t x x x x + u t t t = 0 , β 0 .

Equation (1.2) was developed in ref. [10], where the researchers performed a Painlevé test to prove its integrability. The authors went further to find different types of soliton solutions of (1.2) using Hirota’s method. In a sense, equation (1.2) is a second-generation hybrid between the fifth-order Kawahara equation [11]

(1.3) u t + α u u x + ν u x x x + γ u x x x x x

and another fifth-order equation [12]

(1.4) u x x x 4 u t u x x x 12 u x x u t x 8 u x u t x x u t x x x x + u t t t = 0 .

In other words, equation (1.2) is a progression from equation (1.4) due to the addition of a second dispersive term ( u x x x ), by lending credence from the Kawahara equation, which also has the two dispersive terms ( u x x x ) and ( u t x x x x ). Notwithstanding this backdrop, integrable models are of great interest to mathematicians and physicists for the plethora of information they possess. The integrability of equation (1.2), which has been proven in ref. [10], makes it a significant model and worth studying. In our work, we seek to obtain a more comprehensive set of solutions with the aid of an optimal system of one-dimensional subalgebras. Also, we derive a group of transformations corresponding to the symmetry algebra of (1.2).

Although the solutions of the authors [10] are extensive, it will be seen that our solutions subsume those in ref. [10] since we obtain hyperbolic, parabolic, elliptic and power series solutions. We will go a step further to determine the conserved vectors attributable to this equation.

The dawn of NLPDEs brought about a commensurate surge in methods for obtaining their analytical solutions. One of the most significant of these techniques emanates from the Lie group theory [13,14,15,16,17,18], courtesy of Marius Sophus Lie (1842–1899). Other methods include the multiple exponential function method [19], Hirota’s bilinear approach [20], the ( G / G ) - expansion technique [21,22], the homogeneous balance method [23], the simplest equation method [24], Kudryashov’s method [25], the elliptic function technique [26] and the F-expansion method [27], to mention but a few.

Conserved quantities are a subject of keen interest in the fields such as theoretical and quantum mechanics [15,16,28,29,30,31,32,33,34,35,36,37,38]. In isolated systems, energy, mass, charge, linear and angular momentum are conserved. Conserved vectors may be used to check for integrability of differential equations (DEs) and the fidelity of numerical solution methods. In this article, we employ two different methods of determining conserved quantities, namely, Noether’s approach and the multiplier method.

2 Lie group analysis of (1.2)

2.1 Infinitesimal generators

For a one-parameter group of transformations

t ¯ t + a ξ 1 ( t , x , u ) , x ¯ x + a ξ 2 ( t , x , u ) , u ¯ u + a η ( t , x , u )

with a small parameter a, we have the corresponding infinitesimal generator

(2.5) X = ξ 1 ( t , x , u ) t + ξ 2 ( t , x , u ) x + η ( t , x , u ) u .

The vector field (2.5) in conjunction with (1.2) satisfies the invariance condition

(2.6) pr ( 5 ) X β u x x x 4 u t u x x x 12 u x x u t x 8 u x u t x x u t x x x x + u t t t | F = 0 = 0 .

Here, pr (5) X is the fifth-order extension of (2.5) given by [15]

pr ( 5 ) X = X + ζ t u t + ζ x u x + ζ t x u t x + ζ x x u x x + ζ t t t u t t t + ζ t x x u t x x + ζ x x x u x x x + ζ t x x x x u t x x x x

and ζ t , ζ x , ζ t x , ζ x x , ζ t t t , ζ t x x , ζ x x x , ζ t x x x x are prolongation coefficient functions which can be obtained from the following general formulae:

(2.7) ζ i = D i ( W ) + ξ j u i j , ζ i 1 i s = D i 1 D i s ( W ) + ξ j u j i 1 i s , s > 1 ,

where W is the Lie characteristic function given by

(2.8) W = η ξ i u j

and the total derivatives D t and D x are defined as

(2.9) D t = t + u t u + u t t u t + u t x u x + , D x = x + u x u + u x x u x + u x t u t + .

From (2.6), we obtain the following system of 12 linear homogeneous PDEs:

(2.10) ξ x 1 = 0 , ξ u 1 = 0 , ξ t t 1 = 0 , ξ t x 1 = 0 , ξ t u 1 = 0 , ξ t 2 = 0 , ξ u 2 = 0 , 2 ξ x 2 ξ t 1 = 0 , η t t t = 0 , η x = 0 , ξ t 1 + 2 η u = 0 , 8 η t 3 β ξ t 1 = 0 .

Solving system (2.10) yields the generator coefficients

(2.11) ξ 1 = 8 C 2 3 β t + C 1 , ξ 2 = 4 C 2 3 β x + C 4 , η = 4 C 2 3 β u + C 2 t + C 3 ,

and ultimately we obtain a four-dimensional Lie algebra L 4 , spanned by the generators

(2.12) X 1 = t , X 2 = x , X 3 = 8 t t + 4 x x + ( 3 β t 4 u ) u , X 4 = u .

2.2 Group transformations of known solutions

The one-parameter groups G i of transformations generated by the four-dimensional Lie algebra (2.12) can be obtained by solving the Lie equations [18] and these are

G 1 : ( t , x , u ) ( t + a , x , u ) , G 2 : ( t , x , u ) ( t , x + a , u ) , G 3 : ( t , x , u ) t e 8 a , x e 4 a , u e 4 a + 1 4 β t e 4 a e 12 a 1 , G 4 : ( t , x , u ) ( t , x , u + a ) .

Thus, we have the following theorem.

Theorem

If u = m ( t , x ) is a solution of the PDE (1.2), then so are the functions

G 1 : u ( 1 ) = m ( t a , x ) , G 2 : u ( 2 ) = m ( t , x a ) , G 3 : u ( 3 ) = e 4 a m t e 8 a , x e 4 a + 1 4 β t 1 e 12 a , G 4 : u ( 4 ) = m ( t , x ) + a .

This means that from any known solution of (1.2) one can obtain infinitely many new exact solutions of (1.2) by the repeated use of the above family of solutions.

2.3 Optimal system of one-parameter group-invariant solutions

We now utilise the method given in ref. [15] to find an optimal system of one-dimensional subalgebras corresponding to the Lie algebra (2.12). Accordingly, we begin by determining the commutation relations, [ X i , X j ] = X i ( X j ) X j ( X i ) , between vector fields (2.12). This leads to the commutator table given in Table 1.

Table 1

Commutation relations of four-dimensional Lie algebra (2.12)

[ X i , X j ] X 1 X 2 X 3 X 4
X 1 0 0 8 X 1 + 3 β X 4 0
X 2 0 0 4 X 2 0
X 3 8 X 1 3 β X 4 4 X 2 0 4 X 4
X 4 0 0 4 X 4 0

The Lie series

Ad ( exp ( ε X i ) ) X j = n = 0 ε n n ! ( Ad X i ) n ( X j )

along with the results of Table 1 yields the adjoint representations, which are presented in Table 2.

Table 2

Adjoint table of Lie algebra (2.12)

Ad X 1 X 2 X 3 X 4
X 1 X 1 X 2 8 ϵ X 1 + X 3 3 β ϵ X 4 X 4
X 2 X 1 X 2 4 ϵ X 2 + X 3 X 4
X 3 e 8 ϵ X 1 + 1 4 β e 4 ϵ ( e 12 ϵ 1 ) e 4 ϵ X 2 X 3 e 4 ϵ X 4
X 4 X 1 X 2 X 3 + 4 ϵ X 4 X 4

Using Tables 1 and 2, and the procedure given in ref. [15], we obtain an optimal system of one-dimensional subalgebras spanned by X 1 , X 2 , X 3 , X 1 ± X 2 , X 2 ± X 4 . However, we note that the vector field X 1 X 2 can be mapped to the vector field X 1 + X 2 by the discrete symmetry ( t , x , u ) ( t , x , u ) . This leaves us with the following optimal system of one-dimensional subalgebras of (1.2) that is spanned by

(2.13) X 1 , X 2 , X 3 , X 1 + X 2 , X 2 ± X 4 .

We now determine an optimal system of group-invariant solutions corresponding to (2.13). This will give us closed-form solutions of (1.2).

2.3.1 Cases X 1 , X 2 and X 2 ± X 4

From the generators X 1 , X 2 and X 2 ± X 4 , we obtain the group-invariant solutions:

(2.14) u ( t , x ) = ϕ 1 ( ξ ) , ξ = x ,

(2.15) u ( t , x ) = ϕ 2 ( ξ ) , ξ = t ,

(2.16) u ( t , x ) = ϕ 3 ( ξ ) ± x , ξ = t ,

respectively. Each of the group-invariant solutions in (2.14)–(2.16) transform equation (1.2) into the ODE ϕ j ( ξ ) = 0 , j = 1 , 2 , 3 . This is easily solved to give the solution

(2.17) ϕ j ( ξ ) = 1 2 C 1 ξ 2 + C 2 ξ + C 3 , j = 1 , 2 , 3 ,

with C 1 , C 2 and C 3 integration constants. Thus,

(2.18) u 1 = 1 2 C 1 x 2 + C 2 x + C 3 ,

(2.19) u 2 = 1 2 C 1 t 2 + C 2 t + C 3 ,

(2.20) u 3 = 1 2 C 1 t 2 + C 2 t + C 3 ± x

are the group-invariant solutions of (1.2) under the optimal system elements X 1 , X 2 and X 2 ± X 4 , respectively.

2.3.2 Case X 1 + X 2

We now focus on the optimal system element X 1 + X 2 . Using the usual Lie theory, we obtain the group-invariant solution u ( t , x ) = ϕ ( ξ ) , ξ = x t , which transforms equation (1.2) into the nonlinear ordinary differential equation (NLODE)

(2.21) ϕ + ( β 1 ) ϕ + 12 ( ϕ ϕ + ϕ 2 ) = 0 .

2.3.2.1 Solutions of (1.2) by direct integration of (2.21)

Integrating (2.21) twice with respect to ξ gives

(2.22) ϕ + 6 ϕ 2 + ( β 1 ) ϕ + C 1 ξ + C 2 = 0

with integration constants C 1 and C 2 . Equation (2.22) cannot be solved to produce solutions in terms of classical functions, see for example ref. [39,40,41,42]. At this point, we are compelled to explore two interesting cases which lead to elliptic and hyperbolic solutions.

  1. The Jacobi elliptic function solutions of (1.2)

Consider the NLODE (2.22) with C 1 = 0 and let ϕ ( ξ ) = ( 1 / 2 ) Θ ( ξ ) . Then equation (2.22) becomes

(2.23) Θ + 3 Θ 2 ρ Θ + C 4 = 0 ,

where ρ = 1 β and C 4 = 2 C 2 . The NLODE (2.23) is a principal equation and arises from many famous NLPDEs. See for example [39]. Multiplying (2.23) by Θ and integrating with respect to ξ yield

(2.24) Θ 2 + 2 Θ 3 ρ Θ 2 + 2 C 4 Θ + 2 C 5 = 0 .

Equation (2.24) leads us to the well-known Jacobi elliptic cosine function solution of (2.23), namely [43,44,45]

(2.25) Θ ( ξ ) = μ 2 + ( μ 1 μ 2 ) cn 2 μ 1 μ 3 2 ξ , M 2 , M 2 = μ 1 μ 2 μ 1 μ 3 .

Here μ 1 , μ 2 and μ 3 (with μ 1 μ 2 μ 3 , 0 M 2 1 ) are roots of the algebraic equation

Θ 3 1 2 ρ Θ 2 + C 4 Θ + C 5 = 0

and thus satisfy the DE

Θ 2 = 2 ( Θ μ 1 ) ( Θ μ 2 ) ( Θ μ 3 ) .

Moreover, C 4 = 2 C 2 = μ 1 μ 2 + μ 2 μ 3 + μ 1 μ 3 and C 5 = μ 1 μ 2 μ 3 . Finally, we recuperate the variable u to obtain the solution of (1.2) as

(2.26) u ( t , x ) = ( μ 1 μ 2 ) sn ( A ξ | M 2 ) cos 1 { dn ( A ξ | M 2 ) } A 1 dn ( A ξ | M 2 ) 2 + μ 2 ξ ,

where A = μ 1 μ 3 / 2 , β = 1 2 ( μ 1 + μ 2 + μ 3 ) and ξ = x t .

The analytic solution (2.26) is periodic in nature, and its profile is sketched in Figure 1.

  1. The hyperbolic solutions of (1.2)

Figure 1 
                        Profile of periodic solution (1.2)
Figure 1

Profile of periodic solution (1.2)

By letting the integration constants C 1 and C 2 equal to zero and ϕ ( ξ ) = ψ ( ξ ) in (2.22), equation (2.22) becomes

(2.27) ψ + ( β 1 ) ψ + 6 ψ 2 = 0 .

Multiplying by ψ and integrating with respect to ξ lead us to

(2.28) ψ 2 + 4 ψ 3 + ( β 1 ) ψ 2 = 0 ,

where once again, the integration constant is taken as zero. The solution of equation (2.28) is

(2.29) ψ ( ξ ) = 1 4 ( β 1 ) × 1 tanh 2 1 2 ± 1 β C 3 1 β ξ ,

where C 3 is the integration constant. In order to recover the variable u, we integrate (2.29) with respect to ξ to obtain the topological kink soliton solution

(2.30) u ( t , x ) = 1 β 2 1 β tanh 1 2 1 β ( ξ ± C 3 )

with its profile shown in Figure 2.

Figure 2 
                        Profile of topological kink soliton (2.30).
Figure 2

Profile of topological kink soliton (2.30).

Remark

Travelling wave solutions of (1.2) can be obtained by taking the linear combination X 1 + ν X 2 , where ν is the wave velocity. The corresponding group-invariant solution for this combination of vector fields is u ( t , x ) = ϕ ( ξ ) , ξ = x ν t , which consequently yields the travelling wave solution of (1.2) as

(2.31) u ( t , x ) = ( μ 1 μ 2 ) sn ( A ξ | M 2 ) cos 1 { dn ( A ξ | M 2 ) } A 1 dn ( A ξ | M 2 ) 2 + μ 2 ξ ,

where A = μ 1 μ 3 / 2 , β = ν { ν 2 2 ( μ 1 + μ 2 + μ 3 ) } and ξ = x ν t .

2.3.2.2 Solutions of (1.2) via the ( G / G ) - expansion method

Using the ( G / G ) - expansion technique [21,22], we now solve the NLODE (2.21). Let equation (2.21) have the formal solution

(2.32) ϕ ( ξ ) = i = 0 m A i G ( ξ ) G ( ξ ) i .

We aim to find the values of the coefficients A 0 , A 1 , A m . In the case of the NLODE (2.21), we obtain m = 1 . See, for example [21]. Thus, from (2.32) we have

(2.33) ϕ ( ξ ) = A 0 + A 1 G ( ξ ) G ( ξ ) .

Substituting (2.33) into (2.21) and making use of the linear ODE

(2.34) G ( ξ ) + λ G ( ξ ) + μ G ( ξ ) = 0 ,

where λ and μ take arbitrary real values, we obtain an algebraic equation in A 0 and A 1 , whose solution is

A 0 = A 0 , A 1 = 1 , β = 1 ( λ 2 4 μ ) .

Thus, we have the following three types of solutions for (1.2):

(i) When 1 β > 0 , we have

(2.35) u ( t , x ) = A 0 + Ω 1 B 1 cosh ( Ω 1 ξ ) + B 2 sinh ( Ω 1 ξ ) B 1 sinh ( Ω 1 ξ ) + B 2 cosh ( Ω 1 ξ ) λ 2 ,

where Ω 1 = 1 β / 2 , ξ = x t and A 0 , B 1 and B 2 are arbitrary constants. The solution profile of (2.35) is presented in Figure 3.

Figure 3 
                        Topological kink soliton profile of (2.35).
Figure 3

Topological kink soliton profile of (2.35).

(ii) When 1 β < 0 , we get

(2.36) u ( t , x ) = A 0 + Ω 2 B 1 sin ( Ω 2 ξ ) B 2 cos ( Ω 2 ξ ) B 1 cos ( Ω 2 ξ ) + B 2 sin ( Ω 2 ξ ) λ 2 ,

where Ω 2 = β 1 / 2 , ξ = x t and A 0 , B 1 and B 2 are arbitrary constants. The solution profile of (2.36) is sketched in Figure 4.

Figure 4 
                        Periodic behaviour with singularities for (2.36).
Figure 4

Periodic behaviour with singularities for (2.36).

(iii) When β = 1 , we obtain

(2.37) u ( t , x ) = A 0 + B 2 B 2 ξ + B 1 λ 2 ,

where ξ = x t and A 0 , B 1 and B 2 are arbitrary constants. The profile of solution (2.37) is given in Figure 5.

Figure 5 
                        Bright and dark solitons (2.37) with a singularity.
Figure 5

Bright and dark solitons (2.37) with a singularity.

2.3.3 Case X 3

Finally, we consider the optimal system element X 3 , which culminates in the group-invariant solution u ( t , x ) = ( 1 / t ) ϕ ( ξ ) + 1 / 4 β t , ξ = x / t . Thus, equation (1.2) is transformed into the NLODE

(2.38) 4 ξ ϕ ( 5 ) + 20 ϕ ( 4 ) + 48 ξ ϕ ϕ ξ 3 ϕ + 96 ξ ϕ 2 + 96 ξ ϕ ϕ + 16 ϕ ϕ + 192 ϕ ϕ 33 ξ ϕ 12 ξ 2 ϕ 15 ϕ = 0 .

The power series solution method is ideal for solving such complicated nonlinear differential equation (2.38). See, for example ref. [46,47,48,49]. To begin, let the solution of (2.38) take the form

(2.39) ϕ ( ξ ) = z = 0 g z ξ z

with constants g z , z = 0 , 1 , 2 , , to be determined. The various derivatives of (2.39) are thus

(2.40) ϕ ( ξ ) = z = 0 ( z + 1 ) g z + 1 ξ z , ϕ ( ξ ) = z = 0 ( z + 1 ) ( z + 2 ) g z + 2 ξ z , ϕ ( ξ ) = z = 0 ( z + 1 ) ( z + 2 ) ( z + 3 ) g z + 3 ξ z , ϕ ( 4 ) ( ξ ) = z = 0 ( z + 1 ) ( z + 2 ) ( z + 3 ) ( z + 4 ) g z + 4 ξ z , ϕ ( 5 ) ( ξ ) = z = 0 ( z + 1 ) ( z + 2 ) ( z + 3 ) ( z + 4 ) ( z + 5 ) g z + 5 ξ z .

Substituting the results of (2.40) into (2.38) gives

(2.41) 4 z = 1 z ( z + 1 ) ( z + 2 ) ( z + 3 ) ( z + 4 ) g z + 4 ξ z + 20 z = 0 ( z + 1 ) ( z + 2 ) ( z + 3 ) ( z + 4 ) g z + 4 ξ z + 48 z = 1 j = 0 z 1 ( j + 1 ) ( z j ) ( z + 1 j ) ( z + 2 j ) × g j + 1 g z + 2 j ξ z z = 3 ( z 2 ) ( z 1 ) z g z ξ z + 96 z = 1 j = 0 z 1 ( j + 1 ) ( z j ) g j + 1 g z j ξ z + 96 z = 1 j = 0 z 1 ( z j ) ( z + 1 j ) g j g z + 1 j ξ z + 16 z = 0 j = 0 z ( z + 1 j ) ( z + 2 j ) × ( z + 3 j ) g j g z + 3 j ξ z + 192 z = 0 j = 0 z ( j + 1 ) ( z + 1 j ) × ( z + 2 j ) g j + 1 g z + 2 j ξ z 33 z = 1 z g z ξ z 12 z = 2 ( z 1 ) z g z ξ z 15 z = 0 g z ξ z = 0 .

Equation (2.41) leads to

(2.42) 480 g 5 ξ + 2880 g 6 ξ 2 + 4 z = 3 z ( z + 1 ) ( z + 2 ) × ( z + 3 ) ( z + 4 ) g z + 4 ξ z + 480 g 4 + 2400 g 5 ξ + 7200 g 6 ξ 2 + 20 z = 3 ( z + 1 ) ( z + 2 ) ( z + 3 ) × ( z + 4 ) g z + 4 ξ z + 288 g 1 g 3 ξ + 1152 g 1 g 4 ξ 2 + 48 z = 3 j = 0 z 1 ( j + 1 ) ( z j ) ( z + 1 j ) × ( z + 2 j ) g j + 1 g z + 2 j ξ z z = 3 ( z 2 ) ( z 1 ) z g z ξ z + 96 g 1 2 ξ + 192 g 1 g 2 ξ 2 + 96 z = 3 j = 0 z 1 ( j + 1 ) ( z j ) × g j + 1 g z j ξ z + 192 g 0 g 2 ξ + 576 g 0 g 3 ξ 2 + 96 z = 3 j = 0 z 1 ( z j ) ( z + 1 j ) g j g z + 1 j ξ z + 96 g 0 g 3 + 384 g 0 g 4 ξ + 960 g 0 g 5 ξ 2 + 16 z = 3 j = 0 z ( z + 1 j ) × ( z + 2 j ) ( z + 3 j ) g j g z + 3 j ξ z + 384 g 1 g 2 + 1152 g 1 g 3 ξ + 2304 g 1 g 4 ξ 2 + 192 z = 3 j = 0 z ( j + 1 ) × ( z + 1 j ) ( z + 2 j ) g j + 1 g z + 2 j ξ z 33 g 1 ξ 66 g 2 ξ 2 33 z = 3 z g z ξ z 12 g 2 ξ 2 12 z = 3 ( z 1 ) × z g z ξ z 15 g 0 15 g 1 ξ 15 g 2 ξ 2 15 z = 3 g z ξ z = 0 .

Now comparing coefficients of ξ in equation (2.42) we have, for z = 0 , 1 , 2 :

(2.43) 96 g 0 g 3 + 384 g 1 g 2 15 g 0 + 480 g 4 = 0 ,

(2.44) 192 g 0 g 2 + 384 g 0 g 4 + 96 g 1 2 + 1440 g 1 g 3 48 g 1 + 2880 g 5 = 0 ,

(2.45) 576 g 0 g 3 + 960 g 0 g 5 + 192 g 1 g 2 + 3456 g 1 g 4 93 g 2 + 10080 g 6 = 0

and generally for z 3 we have the recurrence relation

(2.46) g z + 4 = 1 ( 4 z + 20 ) ( z + 1 ) ( z + 2 ) ( z + 3 ) ( z + 4 ) × 48 j = 0 z 1 ( j + 1 ) ( z j ) ( z + 1 j ) ( z + 2 j ) × g j + 1 g z + 2 j 33 z g z 12 ( z 1 ) z g z 15 g m + 96 j = 0 z 1 ( j + 1 ) ( z j ) g j + 1 g z j + 96 j = 0 z 1 ( z j ) ( z + 1 j ) g j g z + 1 j + 16 j = 0 m ( z + 1 j ) ( z + 2 j ) ( z + 3 j ) × g j g z + 3 j ( z 2 ) ( z 1 ) z g z + 192 j = 0 m ( j + 1 ) × ( z + 1 j ) z + 2 j ) g j + 1 g z + 2 j .

From equations (2.43)–(2.45) and for arbitrary g 0 , , g 3 , we have the following:

(2.47) g 4 = 1 32 g 0 1 5 g 0 g 3 4 5 g 1 g 2 , g 5 = 2 75 g 0 2 g 3 1 15 g 0 g 2 + 8 75 g 0 g 1 g 2 1 240 g 0 2 1 30 g 1 2 1 2 g 1 g 3 + 1 60 g 1 , g 6 = 1 2520 g 0 3 4 1575 g 3 g 0 3 16 1575 g 1 g 2 g 0 2 + 2 315 g 2 g 0 2 + 1 315 g 1 2 g 0 31 2520 g 1 g 0 + 61 525 g 1 g 3 g 0 2 35 g 3 g 0 + 48 175 g 1 2 g 2 2 105 g 1 g 2 + 31 3360 g 2 .

Using the recursion formula (2.46), successive terms g m , m = 7 , 8 , , can be determined uniquely. Thus, the power series solution of (2.38) can be written as

(2.48) ϕ ( ξ ) = g 0 + g 1 ξ + g 2 ξ 2 + g 3 ξ 3 + 1 32 g 0 1 5 g 0 g 3 4 4 g 1 g 2 ξ 4 + 2 75 g 0 2 g 3 1 15 g 0 g 2 + 8 75 g 0 g 1 g 2 1 240 g 0 2 1 30 g 1 2 1 2 g 1 g 3 + 1 60 g 1 ξ 5 + 1 2520 g 0 3 4 1575 g 3 g 0 3 16 1575 g 1 g 2 g 0 2 + 2 315 g 2 g 0 2 + 1 315 g 1 2 g 0 31 2520 g 1 g 0 + 61 525 g 1 g 3 g 0 2 35 g 3 g 0 + 48 175 g 1 2 g 2 2 105 g 1 g 2 + 31 3360 g 2 ξ 6 + z = 3 g z + g ξ z + 4 .

Finally, the solution of (1.2) is

(2.49) u ( t , x ) = g 0 + g 1 x t + g 2 x 2 t + g 3 x 3 t 3 / 2 + 1 32 g 0 1 5 g 0 g 3 4 5 g 1 g 2 x 4 t 2 + 2 75 g 0 2 g 3 1 15 g 0 g 2 + 8 75 g 0 g 1 g 2 1 240 g 0 2 1 30 g 1 2 1 2 g 1 g 3 + 1 60 g 1 x 5 t 5 / 2 + 1 2520 g 0 3 4 1575 g 3 g 0 3 16 1575 g 1 g 2 g 0 2 + 2 315 g 2 g 0 2 + 1 315 g 1 2 g 0 31 2520 g 1 g 0 + 61 525 g 1 g 3 g 0 2 35 g 3 g 0 + 48 175 g 1 2 g 2 2 105 g 1 g 2 + 31 3360 g 2 x 6 t 3 z = 3 ( z + 4 ) ! ( 4 z + 20 ) z ! 48 j = 0 z 1 ( j + 1 ) ( z j ) × ( z + 1 j ) ( z + 2 j ) g j + 1 g z + 2 j = 33 z g z 12 ( z 1 ) z g z 15 g z + 96 j = 0 z 1 ( j + 1 ) × ( z j ) g j + 1 g z j + 96 j = 0 z 1 ( z j ) × ( z + 1 j ) g j g z + 1 j + 16 j = 0 z ( z + 1 j ) × ( z + 2 j ) ( z + 3 j ) g j g z + 3 j ( z 2 ) ( z 1 ) z g z + 192 j = 0 z ( j + 1 ) × ( z + 1 j ) ( z + 2 j ) g j + 1 g z + 2 j ) x t z + 4 .

The graphical depiction of the behavioural pattern of solution (2.49) is given in Figure 6.

Figure 6 
                     Depiction of cumulative partial sums up to T
                        6 for solution (2.49).
Figure 6

Depiction of cumulative partial sums up to T 6 for solution (2.49).

3 Conserved quantities of (1.2)

3.1 Noether’s approach

We begin by applying the classical Noether approach [28] to determine conserved quantities of (1.2). The Helmholtz conditions dictate that for an NLPDE to have a variational principle, it must, among other things, have an even-order [29]. Equation (1.2) is of order five and thus cannot have a variational principle. To remedy this we introduce u = v x to transform (1.2) into the sixth-order NLPDE

(3.50) F β v x x x x 4 v t x v x x x x 12 v x x x v t x x 8 v x x v t x x x v t x x x x x + v t t t x = 0 .

For the transformed equation (3.50) to have a variational principle, it must indeed satisfy the Helmholtz conditions

(3.51) F ( q v ) = ( 1 ) q ( E v q ( F ) ) t .

Here q = 1 , , Q , where Q is the order of equation (3.50). Due to the presence of the transpose t, generally the number of field variables v should equal the number of components in system F , else the Helmholtz conditions do not hold and extension F would not possess a variational principle. Also, E v q represents higher Euler operators, which are given by

(3.52) E v ( r ) ( F ) = F ( r v ) r + 1 r D F ( r + 1 v ) + + q r ( D ) q r F ( r v )

with r = 1 q and D represents the total derivatives D = ( D t , D x ) . It can be shown with relative ease that a reckoning of (3.51) will confirm that equation (3.50) indeed has a variational principle. A Lagrangian can thus be recovered for (3.50) as

(3.53) = 8 3 v t x x v v x x x + v x v x x + 4 3 v x x x v v t x x + v x v t x + 1 2 β v x x 2 + 1 2 v x x x v t x x + 1 2 v t t v t x 4 v x x x v v t x x .

The Lagrangian (3.53) conforms with condition δ / δ v = F = 0 , as expected.

In order to obtain the variational symmetries Y = ξ 1 / t + ξ 2 / x + η / v corresponding to Lagrangian (3.53), we shall use the invariance condition

(3.54) pr ( 3 ) Y ( ) + D t ξ 1 + D x ξ 2 = D t B 1 + D x B 2 ,

where pr (3) Y is the third prolongation of Y obtainable from

pr ( 3 ) Y = Y + ζ x v x + ζ t t v t t + ζ t x v t x + ζ x x v x x + ζ t x x v t x x + ζ x x x v x x x .

Note that in (3.54), ξ 1 , ξ 2 , η , B 1 and B 2 are functions of ( t , x , v ) . The invariance condition (3.54) yields the following system of 12 linear PDEs:

(3.55) ξ t 1 = 0 , ξ x 1 = 0 , ξ v 1 = 0 , ξ t 2 = 0 , ξ x 2 = 0 , ξ v 2 = 0 , η t t = 0 , η x = 0 , η v = 0 , B v 1 = 0 , B v 2 = 0 , B t 1 + B x 2 = 0 .

From system (3.55), we can readily infer without any tedious calculations that

ξ 1 = C 1 , ξ 2 = C 2 , η = C 3 t + C 4 , B 1 = F ( t , x ) , B 2 = H ( t , x ) + P ( t )

with H ( t , x ) = F t ( t , x ) d x . The above generator coefficients lead us to the variational symmetries

(3.56) Y 1 = t , B 1 = B 2 = 0 , Y 2 = x , B 1 = B 2 = 0 , Y 3 = t v , B 1 = B 2 = 0 , Y 4 = v , B 1 = B 2 = 0 .

For the Noether symmetry generators (3.56) associated with Lagrangian (3.53), we derive conserved vectors [18]

(3.57) T i = N i ( ) B i , i = 1 , , n

such that D t T t + D x T x = 0 for all solutions of (3.50). Here N i is the Noether operator given by

(3.58) N i = ξ i + W α δ δ v i α + s 1 D i 1 D i s ( W α ) δ δ v i i 1 i 2 i s α , i = 1 , , n ,

where the Euler operators with respect to derivatives of v α are obtained from

(3.59) δ δ v α = v α + s 1 ( 1) s D i 1 D i s v i 1 i 2 i s α , α = 1 , , m ,

by replacing v α with the corresponding derivatives. For example,

(3.60) δ δ v i α = v i α + s 1 ( 1 ) s D j 1 D j s v i j 1 j 2 j s α , i = 1 , , n , α = 1 , , m .

By utilising (3.53), (3.56) and (3.57), we obtain the following nonlocal conserved quantities of equation (1.2):

T 1 t = 1 36 { 2 ( 16 u t + 9 β ) u x 2 + 8 8 u u t x 9 u x x u t d x u x 8 u x x x u t d x 7 u t u x x u + 3 4 u x x u t x + 2 u x x x 3 u t t d x u t + ( 9 u t t 2 u x x x ) u t d x ,

T 1 x = 1 36 4 ( 9 β 34 u t ) u x x u t d x + 2 u u t t d x 3 u t t + 32 u x 2 u t t d x 18 u t x 2 4 9 β u t 20 u t 2 + 56 u t x u t d x + 16 u u t t u x 64 u u t u t x + 8 u u t x x u t d x + 24 u t u t x x 30 u t x x x u t d x + 6 u x x x u t t d x 9 u t t d x 2 + 9 u t d x u t t t d x ;

T 2 t = 1 36 6 u x x x 9 u t t d x 96 u u x x u x 18 u t 2 + 32 u x 3 6 u x x 2 + ( 27 u t t 8 u u x x x 6 u x x x x ) u , T 2 x = 1 36 4 u x x ( 9 β 32 u t ) 30 u t x x x + 9 u t t t d x u + 2 ( 56 u t 9 β ) u x 2 + 8 u 2 u t x x 12 u x x u t x + 8 u x ( 3 u t x x 26 u u t x ) + 3 u t 3 u t t d x + 2 u x x x ;

T 3 t = 1 2 u t + 1 36 t { 72 u x u x x 27 u t t + 8 u u x x x + 6 u x x x x } , T 3 x = 1 36 { 224 t u x u t x 4 ( 2 u + 9 β t 34 t u t ) u x x 8 t u u t x x + 30 t u t x x x + 9 u t t d x 9 t u t t t d x 32 u x 2 6 u x x x ;

T 4 t = 2 u x u x x 3 4 u t t + 2 9 u u x x x + 1 6 u x x x x , T 4 x = 1 36 { 4 ( 34 u t 9 β ) u x x + 224 u x u t x 8 u u t x x + 30 u t x x x 9 u t t t d x .

3.2 Multiplier approach

One advantage of the multiplier approach is that it does not require the existence of a variational principle in order to obtain conserved quantities of DEs [15].

3.2.1 Computation of conserved quantities of (1.2)

The determining condition for a multiplier, namely,

(3.61) δ δ u ( Λ F ) = 0

will give us multipliers Λ ( t , x , u ) with F given by equation (1.2). The Euler operator δ / δ u , in our case, is given by

δ δ u = u D t u t D x u x + D t D x u t x + D x 2 u x x D t 3 u t t t D t D x 2 u t x x D x 3 u x x x D t D x 4 u t x x x x

and D t , D x are given by (2.9). From equation (3.61) and by following the procedure similar to the usual Lie symmetry algorithm, six multiplier determining equations are realised, which are

(3.62) Λ u u = 0 , Λ x u = 0 , Λ x x = 0 , Λ t u = 0 , Λ t x = 0 , Λ t t t = 0 .

Solving equation (3.62) one obtains the multipliers corresponding to equation (1.2) as

(3.63) Λ = C 1 u + C 2 x + 1 2 C 3 t 2 + C 4 t + C 5 ,

where C 1 , , C 5 are constants. We now employ the first homotopy integral formula [29]

(3.64) Φ = 0 1 j = 1 k λ j 1 u ( λ ) l = j k ( D ) l j F Λ ( l u ) u = λ u d λ ,

where k is the highest-order derivative of F with equation (1.2) along with multipliers (3.63). We obtain

T = C 2 u u t t 2 C 1 u u x x 4 C 2 u u x u x x + C 3 u 1 2 C 2 u u x x x x 1 2 C 2 u t 2 C 3 t u t u t C 4 + C 1 x u t t + 1 2 C 3 t 2 u t t + C 4 t u t t + C 5 u t t

and

X = C 5 β u x x C 1 x u t x x x C 4 t u t x x x C 1 β u x 1 2 C 3 t 2 u t x x x + C 1 β x u x x + 1 2 C 3 β t 2 u x x + C 4 β t u x x 1 2 C 2 u u t x x x 8 C 5 u x u t x + 6 C 1 u t u x 1 2 C 2 u t x u x x 4 C 5 u t u x x + 1 2 u t x x C 2 u x + 2 u u t x C 1 + 4 u t C 2 u x 2 + 1 2 C 2 u t u x x x 1 2 C 2 β u x 2 C 5 u t x x x + C 1 u t x x 4 C 2 u u x x u t 4 C 1 x u t u x x 2 C 3 t 2 u t u x x 4 C 4 t u t u x x 8 C 1 x u x u t x 4 C 3 t 2 u x u t x + C 2 β u u x x 8 C 4 t u x u t x 4 C 2 u u t x u x

and consequently, we have the following five conserved quantities of (1.2):

T 1 t = x u t t 2 u u x x , T 1 x = u t x x + β x u x x 8 x u x u t x 4 x u t u x x + 2 u u t x β u x + 6 u t u x x u t x x x ;

T 2 t = u u t t 1 2 u u x x x x 4 u u x u x x 1 2 u t 2 , T 2 x = 4 u t u x 2 1 2 u u t x x x + 1 2 u x u t x x 1 2 u x x u t x + 1 2 u t u x x x 4 u u x u t x + β u u x x 4 u u t u x x 1 2 β u x 2 ;

T 3 t = 1 2 t 2 u t t + u t u t , T 3 x = 1 2 β t 2 u x x 1 2 t 2 u t x x x 2 t 2 u t u x x 4 t 2 u x u t x ;

T 4 t = t u t t u t , T 4 x = β t u x x 8 t u x u t x 4 t u t u x x t u t x x x ;

T 5 t = u t t , T 5 x = β u x x 4 u t u x x 8 u x u t x u t x x x .

Remarks

As can be seen, the conserved vectors obtained here are first integrals of equation (1.2). Again, a casual inspection reveals that these results, unlike those obtained by the Noether approach are trivial conservation laws of the first kind. See ref. [15] for a detailed discussion.

4 Concluding remarks

In this work, we performed an extensive study of a fifth-order integrable NLPDE (1.2), which was lately established in the literature and consisted of two dispersive terms. We obtained group transformations under which the equation (its solutions) remained invariant. Furthermore, we deduced an optimal system of one-dimensional subalgebras culminating in several group-invariant solutions. This resulted in parabolic, trigonometric, hyperbolic, elliptic and power series solutions. The corresponding solution profiles depict topological kink soliton and periodic behaviour. Moreover, we investigated the existence of a variational principle in relation to Helmholtz conditions and went on to derive nonlocal conserved vectors corresponding to the variational principle obtained. Local and low order conserved quantities were computed using a homotopy integral formula and multipliers.

  1. Conflict of interest: The authors declare they have no conflict of interest.

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Received: 2020-08-16
Revised: 2020-10-02
Accepted: 2020-10-03
Published Online: 2020-12-03

© 2020 Innocent Simbanefayi and Chaudry Masood Khalique, published by De Gruyter

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

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