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Multiple types of exact solutions and conservation laws

of new coupled ( 2 + 1 ) -dimensional Zakharov–Kuznetsov system with time-dependent coefficients

BIKRAMJEET KAUR1and R K GUPTA2,3 ,∗

1School of Mathematics, Thapar Institute of Engineering and Technology, Patiala 147 004, India

2Department of Mathematics and Statistics, Central University of Punjab, Mansa Road, Bathinda 151 001, India

3Department of Mathematics, School of Physical and Mathematical Sciences, Central University of Haryana, Mahendergarh123 031, India

Corresponding author. E-mail: rajeshateli@gmail.com

MS received 29 October 2018; revised 11 March 2019; accepted 13 March 2019

Abstract. This paper investigates the new coupled(2+1)-dimensional Zakharov–Kuznetsov (ZK) system with time-dependent coefficients for multiple types of exact solutions by using the Lie symmetry transformation method.

Similarity transformation reduces the system of equations into ordinary differential equations and further, these are solved for solutions having bright, dark and singular solitons as well as periodic waves. Also, the solutions appeared in terms of time-dependent coefficientβ(t)and analysed graphically to show the effect of this arbitrary function. It is proved that the given system is nonlinear self-adjoint, and some conservation laws are obtained by applying the new conservation theorem.

Keywords. Lie’s infinitesimals criterion; exact solutions; new coupled(2+1)-dimensional Zakharov–Kuznetsov system; conservation laws.

PACS Nos 02.20.Sv; 04.20.Jb; 02.30.Jr; 05.45.Yv

1. Introduction

The nonlinear physical phenomena can be dissemi- nated by solving nonlinear partial differential equations (PDEs). The evolution profile of solutions for such equa- tions plays a key role in mathematical, physical and engineering sciences. Thus, it is required to develop an algorithm to find a variety of solutions. The present work addresses to obtain multiple types of exact solutions for a system of equations by the symmetry transfor- mation method [1–6]. This method reduces the number of independent variables by one at each step. This enables us to reduce the nonlinear PDEs to nonlinear ordinary differential equations (ODEs) which can be solved for exact solutions [7]. Further, the Lie symme- tries are used to construct conservation laws [8–15]. The present report describes one such nonlinearly evolved (2+1)-dimensional new coupled Zakharov–Kuznetsov (ncZK) system with time-dependent coefficients as follows:

1ut +α(t)(uv)x+γ (t)(vw)x

+β(t)(ux x+uyy)x =0,

2vt +λ(t)(uw)x+β(t)(vx x+vyy)x =0, 3wt +λ(t)(uv)x +β(t)(wx x+wyy)x =0, (1.1) whereα(t),β(t),γ (t)andλ(t)are arbitrary functions oft.

The ncZK system models dust-acoustic solitary waves evolved in magnetised dusty plasmas, nonlinear ion- acoustic waves and hot isothermal electrons [16–21].

With constant coefficients, system (1.1) is solved suc- cessfully by Elboree [22], Wei and Tang [23], Khalique [24] and Fahmy [25] for different types of exact solu- tions. System (1.1) with time-dependent coefficients has not been investigated yet by the symmetry trans- formation method for exact solutions as well as for conservation laws. Therefore, the main motive of the present paper is to investigate system (1.1) for exact 0123456789().: V,-vol

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solutions and conservation laws via the symmetry trans- formation method.

The paper is structured as follows. Section2presents the stepwise procedure for determining the Lie infinites- imal symmetries, symmetry groups and optimal sys- tems. Further, in §3, similarity solutions and reduced ODEs are obtained corresponding to vector fields of optimal system, and reduced ODEs are analysed for getting multiple types of exact solutions. Then, some of the solutions are represented graphically. In §4, the nonlinear self-adjointness of the system is proved and the new conservation theorem is employed to determine the non-trivial conservation laws.

2. Lie symmetry transformations

This section presents the Lie symmetry transformation criterion to find exact solutions for system (1.1). For Lie infinitesimal symmetries, consider an infinitesimal generator of the following form [1]:

=ξ1

∂t +ξ2

∂x +ξ3

∂y +η1

∂u +η2

∂v +η3

∂w, (2.1)

where ξ1, ξ2, ξ3, η1, η2 and η3 are functions of (t,x,y,u, v, w). The third-order prolongation Pr3of for system (1.1) is given as follows:

Pr3=+η1t

∂ut +ηx1

∂ux +ηx x x1

∂ux x x

x yy1

∂ux yy +ηt2

∂ut +η2x

∂vx

x x x2

∂vx x x +ηx yy2

∂vx yy +ηt3

∂ut

x3

∂wx +ηx x x3

∂wx x x +ηx yy3

∂wx yy, (2.2) whereηt1,η2t,ηt3,ηx1,η2x,η3x,η1x x x,ηx x x2 ,η3x x x,η1x yy,ηx yy2 andη3x yy are the extended infinitesimals [1]. Equation (2.1) represents the Lie point symmetry of the ncZK system if the following conditions hold:

Pr3(1)|1=0,2=0,3=0=0, Pr3(2)|1=0,2=0,3=0 =0,

Pr3(3)|1=0,2=0,3=0=0. (2.3) The following symmetry equations are obtained from eq. (2.3):

η1t +α(t)ξ1(uv)x+α(t)

×(uηx2+η1vx+ηx1v+uxη2) +γ(t)ξ1(vw)x+γ (t)

×(vη3x+η2wx +ηx2w+vxη3) +β(t)ξ1ux x x+β(t)η1x x x

+β(t)ξ1ux yy+β(t)η1x yy =0, η2t +λ(t)ξ1(uw)x+λ(t)

×(uηx3+η1wx+η1xw+uxη3) +β(t)ξ1vx x x+β(t)ηx x x2 +β(t)ξ1vx yy+β(t)ηx yy2 =0, η3t +λ(t)ξ1(uv)x+λ(t)

×(uηx2+η1vx+ηx1v+uxη2) +β(t)ξ1wx x x+β(t)η3x x x

+β(t)ξ1wx yy+β(t)η3x yy =0. (2.4) Using the extended infinitesimals in eq. (2.4) and by equating the coefficients of like derivatives ofu,vandw, we have obtained the over-determined system of linear PDEs and the solution of over-determining equations reads as follows:

ξ1= 1 β(t)

3a1

β(t)dt+a4

, ξ2 =a1x+a3, ξ3 =a1y+a2,

η1 =a5u, η2 =a5v, η3 =a5w, (2.5) wherea1,a2,a3,a4,a5 are arbitrary constants and the coefficientsα(t),β(t),γ (t),λ(t)follow the subsequent conditions:

β(t)γ (t)(2a1+a5)+(−βtγ (t)+β(t)γ(t))ξ1 =0, β(t)α(t)(2a1+a5)+(−βtα(t)+β(t)α(t))ξ1=0, β(t)λ(t)(2a1+a5)+(−βtλ(t)+β(t)λ(t))ξ1 =0.

(2.6) From eq. (2.5), the one-dimensional Lie algebra [1,11]

is generated by the following vector fields:

1 = 1

β(t)∂t, 2 =∂x, 3=∂y, 4 =u∂u+v∂v+w∂w,

5 =x∂x+y∂y+3

β(t)dt

β(t) ∂t. (2.7)

These vector fields generate one-parameter groups G():

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G1:(x,t,y,u, v, w)

x,t+

β(t),y,u, v, w

, G2:(x,t,y,u, v, w)(x +,t,y,u, v, w), G3:(x,t,y,u, v, w)(x,t,y+,u, v, w), G4:(x,t,y,u, v, w)(x,t,y,ue, ve, we), G5:(x,t,y,u, v, w)

xe,t+3 β(t)dt

β(t) ,ye,u, v, w

, (2.8)

where variousGi (i =1,2, . . . ,5)represent the sym- metry groups and we can state the following theorem that leads to the optimal system [1,11].

Theorem 2.1. Ifu = P(x,t,y), v = Q(x,t,y), w = R(x,t,y)represents the solution of system(1.1), so are the functions

(u(1), v(1), w(1))=

P

x,t β(t),y

, Q

x,t β(t),y

, R

x,t β(t),y

, (u(2), v(2), w(2))=(P(x,t,y),Q(x,t,y),

R(x,t,y)),

(u(3), v(3), w(3))=(P(x,t,y),Q(x,t,y), R(x,t,y)),

(u(4), v(4), w(4))=(eP(x,t,y),eQ(x,t,y), eR(x,t,y)),

(u(5), v(5), w(5))=

P

xe,t−3

β(t)dt β(t) ,ye

, Q

xe,t3 β(t)dt β(t) ,ye

, R

xe,t3

β(t)dt β(t) ,ye

. (2.9) It describes that for each subgroup of symmetry groups Gi (i = 1,2, . . . ,5), there will be a family of group- invariant solutions and in the present case there are an infinite number of such subgroups. Hence, it is not feasi- ble to enlist all the possible group-invariant solutions for ncZK system. The group-invariant solution introduces the concept of an optimal system.

The optimal system is obtained using the adjoint rep- resentation and is given in terms of the Lie series as follows:

Ad(exp(i))j =j[i, j] +2

2 [i,[i, j]] + · · · , (2.10)

Table 1. Adjoint table.

Ad 1 2 3 4 5

1 1 2 3 4 531

2 1 2 3 4 52

3 1 2 3 4 53

4 1 2 3 4 5

5 1e3 2e 3e 4 5

where is the real parameter.[i, j] = ijji

is defined as the Lie bracket. The non-zero Lie brackets from Lie algebra (2.7) are obtained as follows:

[1, 5] = −[5, 1] =31, [2, 5] = −[5, 2] =2,

[3, 5] = −[5, 3] =3. (2.11) The Lie series (2.10) and Lie commutation relation (2.11) further help to write down the adjoint table (table1) of the ncZK system.

Then, the adjoint table is used to construct the optimal system generated by the following vector fields:

(i) 5+ρ4,

(ii) 4+μ3+θ2+ν1, (iii) 3+r2+s1,

(iv) 2+p1, (v) 1,

whereρ,μ,θ,ν,r,sandpare arbitrary constants. These vector fields are used in the next section for similarity reductions.

3. Similarity reductions and exact solutions

For similarity reductions with respect to the vector fields described in the optimal system, the following charac- teristic equations are used:

dt ξ1 = dx

ξ2 = dy ξ3 = du

η1 = dv η2 = dw

η3. (3.1)

3.1 Vector field5+ρ4

The characteristic equation (3.1) for this vector field 5+ρ4gives the following invariants:

ζ1 = x

(

β(t)dt)1/3, ζ2 = y (

β(t)dt)1/3, u(x,t,y)= F(ζ1, ζ2)

β(t)dt ρ/3

,

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v(x,t,y)=G(ζ1, ζ2)

β(t)dt ρ/3

, w(x,t,y)= H(ζ1, ζ2)

β(t)dt ρ/3

. (3.2)

Using eq. (2.6), the time-dependent coefficients can be written as follows:

α(t)= p1β(t)

β(t)dt

−(2+ρ)/3

, γ (t)= p2β(t)

β(t)dt

−(2+ρ)/3

, λ(t)= p3β(t)

β(t)dt

−(2+ρ)/3

, (3.3)

where p1, p2and p3are arbitrary constants. Using the invariants and coefficient functions given in eqs (3.2) and (3.3), the ncZK system is transformed into the fol- lowing reduced PDEs:

Fζ1ζ1+Fζ2ζ2Fρ−3p1F Gζ1−3p1Fζ1G−3p2G Hζ1

−3p2Gζ1H−3Fζ1ζ1ζ1−3Fζ1ζ2ζ2 =0, Gζ1ζ1+Gζ2ζ2−3p3H Fζ1−3p3Hζ1F

−3Gζ1ζ1ζ1−3Gζ1ζ2ζ2 =0,

Hζ1ζ1+Hζ2ζ2Hρ−3p3F Gζ1−3p3Fζ1G−3Hζ1ζ1ζ1

−3Hζ1ζ2ζ2 =0. (3.4)

We are interested in non-trivial solutions for the given system, but the above reduced PDEs possess only trivial solutions. Hence, this case is not physically important.

3.2 Vector field4+μ3+θ2+ν1

In this case, the invariants and the corresponding vari- able coefficients are obtained as follows:

ζ1 = −θ ν

β(t)dt+x, ζ2 = −μ

ν

β(t)dt+y, u(x,t,y)=F(ζ1, ζ2)e1

β(t)dt, v(x,t,y)=G(ζ1, ζ2)e1

β(t)dt, w(x,t,y)= H(ζ1, ζ2)e1

β(t)dt, α(t)=q1β(t)e1

β(t)dt, γ (t)=q2β(t)e−1/νβ(t)dt, λ(t)=q3β(t)e1

β(t)dt, (3.5)

whereq1, q2 andq3 are arbitrary constants. Invariants (3.5) yield the following reduced PDEs for the ncZK system:

Fζ1θFζ2μ+F+q1νF Gζ1+q1νFζ1G+q2νG Hζ1 +q2νGζ1H+νFζ1ζ1ζ1+νFζ1ζ2ζ2 =0,

Gζ1θ+Gζ2μ−Gq3νHFζ1q3νHζ1F

−νGζ1ζ1ζ1νGζ1ζ2ζ2 =0,

Hζ1θHζ2μ+H+q3νF Gζ1+q3νFζ1G

Hζ1ζ1ζ1+νHζ1ζ2ζ2 =0. (3.6) By applying the Lie symmetry transformation algorithm on the reduced PDEs, the following infinitesimals are obtained:

ξ1=q5, ξ2=q4, η1=η2=η3 =0, (3.7) whereq4andq5are arbitrary constants. The new invari- ants are obtained using the characteristic equation

dζ1

ξ1 = dζ2

ξ2 = dF η1 = dG

η2 = dH η3 as follows:

ζ =q4ζ1q5ζ2, F(ζ1, ζ2)= f(ζ ),

G(ζ1, ζ2)=g(ζ ), H(ζ1, ζ2)=h(ζ ). (3.8) Finally, we obtained the reduced ODEs for the ncZK system as follows:

fζq4θ+fζq5μ+f+q1νf gζq4+q1νfζq4g+q2νghζq4

+q2νgζq4h+νfζζζq43+νfζζζq52q4=0, gζq4θgζq5μgq3νh fζq4q3νhζc4f

−νgζζζq43νgζζζq52q4=0,

hζq4θ+hζq5μ+h+q3νf gζq4

+q3νfζc4g+νhζζζq43+νhζζζq52q4 =0. (3.9) The solution of system (3.9) in the form of power series is considered as follows:

f(ζ )=

n=0

Dnζn, g(ζ )=

n=0

Enζn, h(ζ )=

n=0

Knζn, (3.10) whereDn,EnandKn are unknown coefficients and are to be determined later. From the substitution of (3.10) into the reduced ODEs (3.9), we obtained the following recurrence relations:

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Dn+3 = −1

(νq43+νq52q4)(n+1)(n+2)(n+3)

×

(q4θ+q5μ)(n+1)Dn+1+Dn

q1q4

n

l=0

(nl+1)(DlEnl+1+ElDnl+1)

q2q4

n

l=0

(nl+1)(ElKnl+1+KlEnl+1) ,

En+3= 1

(νq43+νq52q4)(n+1)(n+2)(n+3)

×

(q4θq5μ)(n+1)En+1En

−νq3q4

n

l=0

(nl+1)(KlDnl+1+DlKnl+1) ,

Kn+3= 1

(νq43+νq52q4)(n+1)(n+2)(n+3)

×

(q4θq5μ)(n+1)Kn+1Kn

−νq3q4 n

l=0

(nl+1)(DlEn−l+1+ElDn−l+1) , (3.11) whereD0,D1,D2,E0,E1,E2,K0,K1,K2are arbitrary constants, and

D3 = −1

6(νq43+νq52q4)[(q4θ+q5μ)D1

+D0+νq1q4(D0E1+E0D1) +νq2q4(E0K1+K0E1)],

E3 = 1

6(νq43+νq52q4)[(q4θq5μ)E1

E0+νq3q4(K0D1+D0K1)],

K3 = 1

6(νq43+νq52q4)[(q4θq5μ)K1

K0+νq3q4(D0E1+E0D1)].

In this case, the explicit solutions are obtained in the following form:

u(x,t,y)=e1

β(t)dt

×

D0+D1ζ +D2ζ2− 1 6(νq43+νq52q4)

×[(q4θ +q5μ)D1+D0+νq1q4(D0E1+E0D1)q2q4(E0K1+K0E1)]ζ3

n=1

1

(νq43+νq52q4)(n+1)(n+2)(n+3)

×

(q4θ +q5μ)(n+1)Dn+1+Dn

q1q4

n

l=0

(nl+1)(DlEnl+1+ElDnl+1)

q2q4

n

l=0

(nl+1)(ElKnl+1

+KlEnl+1) ζn+3 , v(x,t,y)=e1

β(t)dt

×

E0+E1ζ +E2ζ2+ 1 6(νq43+νq52q4)

×[(q4θq5μ)E1E0

q3q4(K0D1+D0K1)]ζ3 +

n=1

1

(νq43+νq52q4)(n+1)(n+2)(n+3)

×

(q4θq5μ)(n+1)En+1En

q3q4

n

l=0

(nl+1)(KlDnl+1

+DlKnl+1) ζn+3 , w(x,t,y)=e1

β(t)dt

×

K0+K1ζ +K2ζ2+ 1 6(νq43+νq52q4)

×[(q4θq5μ)K1K0

q3q4(D0E1+E0D1)]ζ3 +

n=1

1

(νq43+νq52q4)(n+1)(n+2)(n+3)

×

(q4θq5μ)(n+1)Kn+1Kn

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q3q4 n

l=0

(nl+1)(DlEn−l+1

+ElDnl+1) ζn+3 , (3.12) where

ζ=q4

θ ν

β(t)dt+x

q5

μ ν

β(t)dt+y

. 3.3 Vector field3+r2+s1

The invariants, coefficient functions and reduced PDEs are found to be as follows:

ζ1 = −r s

β(t)dt+x, ζ2= −1 s

β(t)dt+y, u(x,t,y)=F(ζ1, ζ2), v(x,t,y)=G(ζ1, ζ2), w(x,t,y)= H(ζ1, ζ2), α(t)=c1β(t),

γ (t)=c2β(t), λ(t)=c3β(t) (3.13) and

Fζ1rFζ2+c1s F Gζ1+c1s Fζ1G+c2sGHζ1 +c2sGζ1H+s Fζ1ζ1ζ1+s Fζ1ζ2ζ2 =0, Gζ1r +Gζ2c3sHFζ1c3s Hζ1FsGζ1ζ1ζ1

sGζ1ζ2ζ2 =0,

−Hζ1rHζ2+c3s F Gζ1+c3s Fζ1G+s Hζ1ζ1ζ1

+s Hζ1ζ2ζ2 =0, (3.14)

wherec1,c2 andc3are arbitrary constants. Once again the application of similarity transformation gives the infinitesimals as follows:

ξ1 =c5, ξ2 =c4, η1 =η2 =η3=0, (3.15) wherec4andc5are arbitrary constants. The correspond- ing invariants and ODEs are obtained as follows:

ζ =c4ζ1c5ζ2, F(ζ1, ζ2)= f(ζ ),

G(ζ1, ζ2)=g(ζ ), H(ζ1, ζ2)=h(ζ ) (3.16) and

fζc4r + fζc5+c1s f gζc4+c1s fζc4g+c2sghζc4

+c2sgζc4h+s fζζζc34+s fζζζc25c4 =0, gζc4rgζc5c3sh fζc4c3shζc4fsgζζζc34

sgζζζc25c4=0,

hζc4r+hζc5+c3s f gζc4+c3s fζc4g+shζζζc43

+shζζζc25c4=0. (3.17)

These ODEs are solved by the computational software Maple and finally the exact solutions for the ncZK sys- tem become

(i) c2 = 6c27(12c27c25c42+c24c1c8+6c27c44+6c72c45+c25c1c8) c28c3

, u(x,t,y)= 8Ac5+r c4

2c3c4s −6B c3

tanh2

c6+c7

(r c4c5)

β(t)dt+s(−c4x+c5y) s

, v(x,t,y)= −c8(8Ac5+r c4)

12c4s B +c8tanh2

c6+c7

(r c4c5)

β(t)dt+s(−c4x+c5y) s

, w(x,t,y)= −c8(8Ac5+r c4)

12c4s B +c8tanh2

c6+c7

(r c4c5)

β(t)dt+s(−c4x+c5y) s

.

(3.18) (ii) c2= − 3c21

16c3,

u(x,t,y)= −4Ac5+r c4

2c3c4s + 6B c3

sech2

c6+c7

(r c4c5)

β(t)dt+s(−c4x +c5y) s

, v(x,t,y)= 2(−4Ac5+r c4)

3c1sc4 + 8B c1

sech2

c6+c7

(r c4c5)

β(t)dt+s(−c4x +c5y) s

, w(x,t,y)= 2(−4Ac5+r c4)

3c1sc4 + 8B c1 sech2

c6+c7

(r c4c5)

β(t)dt+s(−c4x +c5y) s

. (3.19)

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(iii) c2 = 6c27(12c27c52c24+c24c1c8+6c72c44+6c27c45+c25c1c8) c82c3

,

u(x,t,y)= −−4Ac5+r c4

2c3c4s +6B c3

csch2

c6+c7

(r c4c5)

β(t)dt+s(−c4x+c5y) s

, v(x,t,y)= −c8(−4Ac5+r c4)

12c4s B +c8csch2

c6+c7

(r c4c5)

β(t)dt+s(−c4x+c5y) s

, w(x,t,y)= c8(−4A−c5+r c4)

12c4sc8csch2

c6+c7

(r c4c5)

β(t)dt+s(−c4x+c5y) s

. (3.20) (iv) c2 = 6c72(12c27c52c24+c24c1c8+6c27c44+6c27c45+c52c1c8)

c28c3 ,

u(x,t,y)= −−8Ac5+r c4

2c4sc3 + 6B c3

cot2

c6+c7

(r c4c5)

β(t)dt+s(−c4x +c5y) s

, v(x,t,y)= −c8(−8Ac5+r c4)

12c4s B +c8cot2

c6+c7

(r c4c5)

β(t)dt+s(−c4x +c5y) s

, w(x,t,y)= c8(−8Ac5+r c4)

12c4s Bc8cot2

c6+c7

(r c4c5)

β(t)dt+s(−c4x +c5y) s

.

(3.21) (v) c2= − 3c21

16c3, u(x,t,y)= − C

2c3 +6Bc82

c3c72JacobiNS2

c7+c8

(r c4c5)

β(t)dt+s(−c4x +c5y) s

,c6

, v(x,t,y)= 2C

3c1 −8Bc28

c1c27 JacobiNS2

c7+c8

(r c4c5)

β(t)dt+s(−c4x+c5y) s

,c6

, w(x,t,y)= −2C

3c1 +8Bc28

c1c27 JacobiNS2

c7+c8

(r c4c5)

β(t)dt+s(−c4x+c5y) s

,c6

. (3.22)

(vi) c2 = − 3c12 16c3, u(x,t,y)= − C

2c3 +6c28c62B

c3c27 ×JacobiSN2

c7+c8

(r c4c5)

β(t)dt+s(−c4x+c5y) s

,c6

,

v(x,t,y)= 2C

3c1 − 8c82c26B

c1c27 ×JacobiSN2

c7+c8

(r c4c5)

β(t)dt+s(−c4x+c5y) s

,c6

, w(x,t,y)= −2C

3c1 +8c28c26B

c1c72 ×JacobiSN2

c7+c8

(r c4c5)

β(t)dt+s(−c4x+c5y) s

,c6

.

(3.23)

(8)

Here

A=c72c34s+c72c4sc25, B =c27

c25+c24 ,

C = 4c28c43sc26+4c28c43s+4c28c4sc25c26+4c82c4sc25c5+r c4

c4s , (3.24)

whereci are arbitrary constants.

The dark, bright and periodic wave solutions are pre- sented graphically in figures 1–6 for solutions (3.18), (3.19) and (3.23), respectively, by considering suitable parametric values. Figures1a–1c show the dark soliton solution (3.18) foru,vandw, respectively whenβ(t)= sin(t)by three-dimensional (3D) plots. Figures 2a–2c describe the effect of coefficient function β(t) on the wave profile of the solution by two-dimensional (2D)

plots when it is linear in t, exponential function of t and trigonometric function oft. Figures3a–3c show the bright soliton solution (3.19) at particular β(t) = et and figures 4a–4c show the effect of various β(t) on the solution profile. Figures 5a–5c and 6a–6c show the periodic wave profiles of solution (3.23) by 3D plots for β(t) = t and 2D plots for different β(t), respectively.

Figure 1. Dark soliton solution (3.18) profile withc1 =0.25,c3 = −1,c4 =1,c5 =2,c6 = 0.5,c7 =0.75,c8 = 1.5, r=0.5,s=1,y=1,β(t)=sin(t): (a)u, (b)v, (c)w.

(a) (b) (c)

Figure 2. Effect ofβ(t)on the profile of the solution (3.18) withc1=0.25,c3= −1,c4=1,c5=2,c6=0.5,c7=0.75, c8=1.5,r =0.5,s=1,y=1,t =1: (a)u, (b)v, (c)w.

(9)

Figure 3. Bright soliton profile of solution (3.19) withc1=0.25,c3=1,c4=1,c5=2,c6=0.5,c7=0.75,c8=1.5, r=0.5,s=1,y=1,β(t)=et: (a)u, (b)v, (c)w.

(a) (b) (c)

Figure 4. Effect of time-dependent coefficientβ(t)on solution (3.19) withc1 =0.25,c3=1,c4=1,c5=2,c6=0.5, c7=0.75,c8=1.5,r=0.5,s=1,y=1,t =1: (a)u, (b)v, (c)w.

Figure 5. Periodic wave profile of solution (3.23) withc1=0.25,c3= −1,c4=1,c5=2,c6=0.5,c7=0.75,c8=1.5, r=0.5,s=1,y=1,β(t)=t: (a)u, (b)v, (c)w.

3.4 Vector field2+ p1

By using similar procedure as described in the previous section, the reduced ODEs in this case are obtained as follows:

p fζζζr42+ fζr1p f gζr1p fζgr2pghζ

r2pgζhp fζζζr52=0,

pgζζζr42gζ +r3ph fζ +r3phζ f + pgζζζr52=0,

References

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