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Article

A Comparative Study of the Fractional-Order System of Burgers Equations

1
School of Mechanical Engineering, Shanghai Dianji University, Shanghai 201306, China
2
Department of Mechanical Engineering, Sejong University, Seoul 05006, Korea
3
Department of Mathematics, College of Science, King Khalid University, Abha 61413, Saudi Arabia
*
Authors to whom correspondence should be addressed.
Symmetry 2021, 13(10), 1786; https://doi.org/10.3390/sym13101786
Submission received: 23 July 2021 / Revised: 7 September 2021 / Accepted: 16 September 2021 / Published: 26 September 2021

Abstract

:
This paper is related to the fractional view analysis of coupled Burgers equations, using innovative analytical techniques. The fractional analysis of the proposed problems has been done in terms of the Caputo-operator sense. In the current methodologies, first, we applied the Elzaki transform to the targeted problem. The Adomian decomposition method and homotopy perturbation method are then implemented to obtain the series form solution. After applying the inverse transform, the desire analytical solution is achieved. The suggested procedures are verified through specific examples of the fractional Burgers couple systems. The current methods are found to be effective methods having a close resemblance with the actual solutions. The proposed techniques have less computational cost and a higher rate of convergence. The proposed techniques are, therefore, beneficial to solve other systems of fractional-order problems.

1. Introduction

Fractional calculus (FC) has become an important mathematical approach for explaining non-local behavioural models. Fractional derivatives have mathematically interpreted many physical problems in recent decades; these representations have produced excellent results in real-world modelling issues. Coimbra, Riemann–Liouville, Riesz, Weyl, Hadamard, Liouville–Caputo, Grunwald–Letnikov, Caputo–Fabrizio, Atangana–Baleanu, among others, gave many basic definitions of fractional operators [1,2]. A wide variety of non-linear equations have been developed and commonly implemented in numerous non-linear physical sciences such as biology, chemistry, applied mathematics and various branches of physics such as plasma physics, condensed matter physics, fluid mechanics, field theory, and non-linear optics over the past few years. The exact result of non-linear equations plays a vital role in deciding the characteristics and behaviour of physical processes. A differential equation symmetry is a transformation that makes the differential equation invariant. The existence of such symmetries may aid in the solution of the differential equation. A scheme of differential equations line symmetry is a continous symmetry of a scheme of differential equations. Solving a linked set of ordinary differential equations can reveal symmetries. It is sometimes easier to solve these equations than it is to solve the original differential equations. The symmetry structure of the system consists of integer partial differential equations and fractional-order partial differential equations with the fractional Caputo derivative. Many effective techniques have been used to solved nonlinear FPDEs, for example, the homotopy perturbation transformation technique [3,4], the homotopy analysis transformation technique [5,6], reduced differential transformation technique [7,8], the finite element method [9], the finite difference method [10], and so on.
Harry Bateman first introduced the Burgers equation in 1915 [11], and subsequently called it the Burgers equation [12]. The Burgers equation has several implementations in engineering and science, particularly in problems that have non-linear equations in their form. It is one of the most basic tools for defining the non-linear phenomenon of dispersion and diffusion, such as approximation theory of flow, shock wave theory, dynamics of soil in water, unsaturated oil, seismology and cosmology, and debris flow wave with non-linear kinematics [13]. With the aid of the Burgers equations, the analytical and numerical methods can be understood. Many mathematical techniques are used to find the burgers equations, such as Adomian Pade technique [14], differential transformation method [15], tanh-function method [16], homotopy analysis method [17], natural decomposition method [18] and Chebyshev wavelet method [19].
The homotopy perturbation method (HPM), first suggested by the Chinese scientist J.H. He plays a crucial role in 1998 [20]. Because of the way it approaches the system, it does not require any linearization or discrimination. This method is equitable, effective, and efficient, as it reduces an unconditioned matrix, complicated integrals and infinite series. This technique does not require a particular problem parameter. Tarig Elzaki introduced the Ezaki Transform (E.T.) in 2010. E.T. is a Sumudu and Laplace transform that has been modified. Absolute differential equations with variable coefficients cannot be solved by Laplace and Sumudu transformation when E.T is used [21,22,23]. The homotopy perturbation transformation method (HPTM) combines the Elzaki transformation and the homotopy perturbation method. Numerous researchers have used HPTM to solve various models, such as Navier–Stokes equations [24], heat-like equations [25], gas dynamic equation [26], hyperbolic equation and Fisher’s equation [27]. The Elzaki decomposition technique, which is the mixture of the Elzaki transformation introduces by Elzaki [28] and the Adomian decomposition technique [29,30,31]. The transformation of Elzaki is well-known for its efficiency in solving linear ordinary differential equations, linear partial differential equations and integral equations as seen in [32,33,34].
In the current study, we implemented HPTM and EDM to analyze the fractional-order system of Burgers equations. The methodology of the proposed techniques is effortless and straightforward. The accuracy is determined in terms of absolute error. The solutions have shown the present techniques have the desired accuracy as compare to other analytical techniques.

2. Preliminary Concepts

Definition 1.
The fractional-order Caputo derivative of h ( ) , h C 1 ω , ω N , ω > 0 , is given as
D α h ( ) = I ω α D ω h ( ) = 1 Γ ( ω α ) 0 ( ζ ) ω α 1 h ω ( ζ ) d ζ , w h e r e ω 1 < α ω .
Definition 2.
The fractional-order Caputo derivative of Elzaki transform is define as
E [ D α h ( ) ] = s α E [ h ( ) ] k = 0 ω 1 s 2 α + k h ( k ) ( 0 ) , w h e r e ω 1 < α < ω .
Definition 3.
The fractional-order Riemann–Liouville of integral α > 0 , of a function h C ω , is given as
J α h ( ζ ) = 1 Γ ( α ) 0 ζ ( ζ ) α 1 h ( ) , α , ζ > 0 ,
Basic properties:
For h C ω , α , β 0 a n d γ > 1
J α J β h ( ζ ) = j α + β h ( ζ ) , J α J β h ( ζ ) = J β J α h ( ζ ) , J γ ζ α = Γ ( α + 1 ) ( γ + α + 1 ) ζ γ + α .

Basic Concept of Elzaki Transformation

The Elzaki transformation is a new transformation described for functions of exponential order. We recognize functions in the set A , described as:
A = { h ( ) : | M , k 1 , k 2 > 0 , | h ( ) | < M e | | k j , i f ( ) ( 1 ) j × [ 0 , ) } .
For a given function in the set, the constant M must be a finite number, and the constants k 1 and k 2 must be finite or infinite. The Elzaki transformation, as described by the integral equation
E [ h ( ) ] = T ( s ) = s 0 h ( ) e s d , 0 , k 1 s k 2 .
We can obtain the basic solutions
E [ n ] = n ! s n + 2 , E [ h ( ) ] = T ( s ) s s h ( 0 ) , E [ h ( ) ] = T ( s ) s 2 h ( 0 ) s h ( 0 ) , E [ h ( n ) ( ) ] = T ( s ) s n k = 0 n 1 s 2 n + k h ( k ) ( 0 ) .
Definition 4.
The inverse Elzaki transform is given as
E 1 [ T ( s ) ] = h ( ) = 1 2 π ι α ι α + ι h 1 s e s s d s = Σ r e s i d u e s o f h 1 s e s s .
The inverse Elzaki transform of some of the functions are given by
E 1 { s n } = n 2 ( n 2 ) ! , n = 2 , 3 , 4 , . E 1 s 2 1 a s = e a E 1 s 3 1 + a 2 s 2 = 1 a sin a E 1 s 2 1 + a 2 s 2 = 1 a cos a
Theorem 1.
If T ( s ) is the Elzaki transformation of h ( ) , one can take into consideration the Elzaki transformation of the Riemann–Liouville derivative as follows:
E [ D α h ( ) ] = s α T ( s ) ω = 1 n { D α k h ( 0 ) } ; 1 < n 1 α < n .
Proof. 
The Laplace transformation
h ( ) = d d h ( ) ,
L [ D α h ( ) ] = s α T ( s ) ω = 0 n 1 s ω [ D α ω 1 h ( 0 ) ] ,
= s α T ( s ) ω = 0 n 1 s ω 1 [ D α ω h ( 0 ) ] = s α T ( s ) ω = 0 n 1 s ω 2 [ D α ω h ( 0 ) ] ,
= s α T ( s ) ω = 0 n 1 1 s ω + 2 [ D α ω h ( 0 ) ] = s α T ( s ) ω = 0 n 1 1 s α ω + 2 α [ D α ω h ( 0 ) ] ,
= s α T ( s ) ω = 0 n 1 s α 1 s α ω + 2 [ D α ω h ( 0 ) ] ,
L [ D α h ( ) ] = s α T ( s ) ω = 0 n 1 1 s α ω + 2 [ D α ω h ( 0 ) ] .
Therefore, when we put 1 s for s 2 , the Elzaki transformation of fractional-order of h ( ) is as below:
E [ D α h ( ) ] = s α T ( s ) ω = 0 n s α ω + 2 [ D α ω h ( 0 ) ] .

3. The General Methodology of HPTM

In this section, the HPTM for the solution of fractional partial differential equations [35,36]
D α u ( ξ , ζ , ) + M u ( ξ , ζ , ) + N u ( ξ , ζ , ) = h ( ξ , ζ , ) , > 0 , 0 < α 1 ,
the initial condition is
u ( ζ , 0 ) = h ( ζ ) .
M is linear and N non-linear functions. Using the Elzaki transform of Equation (1)
E [ D α u ( ξ , ζ , ) + M u ( ξ , ζ , ) + N u ( ξ , ζ , ) ] = E [ h ( ξ , ζ , ) ] , > 0 , 0 < α 1 , u ( ξ , ζ , ) = s 2 h ( ζ ) + s α E [ h ( ξ , ζ , ) ] s α E [ M u ( ξ , ζ , ) + N u ( ξ , ζ , ) ] .
Now, by applying inverse transformation, we get
u ( ξ , ζ , ) = E 1 s 2 h ( ζ ) + s α E [ h ( ξ , ζ , ) ] E 1 s α E { M u ( ξ , ζ , ) + N u ( ξ , ζ , ) } ,
where
u ( ξ , ζ , ) = h ( ζ ) + E 1 s α E [ h ( ξ , ζ , ) ] E 1 s α E { M u ( ξ , ζ , ) + N u ( ξ , ζ , ) } ,
The perturbation methodology in based on power series with parameter p is now described as
u ( ξ , ζ , ) = k = 0 p k u k ( ξ , ζ , ) ,
where perturbation term p and p [ 0 , 1 ] .
The non-linear functions can be defined as
N u ( ξ , ζ , ) = k = 0 p k H k ( u k ) ,
where H ω are He’s polynomials of u 0 , u 1 , u 2 , , u ω , and can be determined as
H ω ( u 0 , u 1 , , u ω ) = 1 ω ! ω p ω N k = 0 p k u k p = 0 , ω = 0 , 1 , 2 .
putting Equations (7) and (8) in Equation (4), we have
k = 0 p k u k ( ξ , ζ , ) = h ( ζ ) + E 1 s α E [ h ( ξ , ζ , ) ] p × E 1 { s α E { M k = 0 p k u k ( ξ , ζ , ) + k = 0 p k H k ( u k ) } } .
Both sides comparison coefficient of p, we have
p 0 : u 0 ( ξ , ζ , ) = h ( ζ ) + E 1 s α E [ h ( ξ , ζ , ) ] , p 1 : u 1 ( ξ , ζ , ) = E 1 s α E ( M u 0 ( ξ , ζ , ) + H 0 ( u ) ) , p 2 : u 2 ( ξ , ζ , ) = E 1 s α E ( M u 1 ( ξ , ζ , ) + H 1 ( u ) ) , p k : u k ( ξ , ζ , ) = E 1 s α E ( M u k 1 ( ξ , ζ , ) + H k 1 ( u ) ) , k > 0 , k N .
u ( ξ , ζ , ) = lim M k = 1 M u k ( ξ , ζ , ) .

4. The Methodology of EDM

Consider the general procedure of EDM to solve the fractional partial differential equation.
D α u ( ξ , ζ , ) + L u ( ξ , ζ , ) + N u ( ξ , ζ , ) = q ( ξ , ζ , ) , ξ , ζ , 0 , ω 1 < α < ω ,
with the initial condition
u ( ξ , ζ , 0 ) = k ( ξ ) ,
Where is D α = α α the Caputo fractional derivative of order α , L and N are linear and non-linear functions, respectively and q is source function.
Applying the Elzaki transform to Equation (12),
E D α u ( ξ , ζ , ) + E L u ( ξ , ζ , ) + N u ( ξ , ζ , ) = E q ( ξ , ζ , ) .
Using the differentiation property, we get
1 s α E u ( ξ , ζ , ) s 2 α u ( ξ , ζ , 0 ) = E q ( ξ , ζ , ) E L u ( ξ , ζ , ) + N u ( ξ , ζ , ) ,
E u ( ξ , ζ , ) = s 2 u ( ξ , ζ , 0 ) + s α E q ( ξ , ζ , ) s α E L u ( ξ , ζ , ) + N u ( ξ , ζ , ) ,
Now, u ( ξ , 0 ) = k ( ξ )
E u ( ξ , ζ , ) = s 2 k ( ξ ) + s α E q ( ξ , ζ , ) s α E L u ( ξ , ζ , ) + N u ( ξ , ζ , ) .
The infinite series solution of u ( ξ , ζ , )
u ( ξ , ζ , ) = ω = 0 u ω ( ξ , ζ , ) ,
The nonlinear terms of N to solve with the help of Adomian polynomials is defined as
N u ( ξ , ζ , ) = ω = 0 A ω ,
A ω = 1 ω ! d ω d λ ω N ω = 0 ( λ ω u ω ) λ = 0 , ω = 0 , 1 , 2
Putting Equation (16) and Equation (17) into (15),
E ω = 0 u ω + 1 ( ξ , ζ , ) = s 2 k ( ξ ) + s α E q ( ξ , ζ , ) s α E L ω = 0 u ω ( ξ , ζ , ) + ω = 0 A ω .
Now using EDM, we have
E u 0 ( ξ , ζ , ) = s 2 k ( ξ ) + s α E q ( ξ , ζ , ) ,
Generally, we can write
E u ω + 1 ( ξ , ζ , ) = s α E L u ω ( ξ , ζ , ) + A ω , ω 1 .
Implemented the inverse Elzaki transform of Equations (20) and (21), we get
u 0 ( ξ , ζ , ) = k ( ξ ) + E 1 s α E q ( ξ , ζ , )
u ω + 1 ( ξ , ζ , ) = E 1 s α E L u ω ( ξ , ζ , ) + A ω .
Example 1.
Consider the fractional-order system of Burgers equations
D α u + u u ξ + v u ζ = 1 R e 2 u ξ 2 + 2 u ζ 2 , D β v + u v ξ + v v ζ = 1 R e 2 v ξ 2 + 2 v ζ 2 , 0 < α , β 1 ,
with initial conditions
u ( ξ , ζ , 0 ) = 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) , v ( ξ , ζ , 0 ) = 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) .
Re denotes the Reynolds number. Now, by applying E T to Equation (23), we obtain the following outcome
E [ D α u ( ξ , ζ , ) ] = E u u ξ E v u ζ + 1 R e E 2 u ξ 2 + E 2 u ζ 2 , E [ D β v ( ξ , ζ , ) ] = E u v ξ E v v ζ + 1 R e E 2 v ξ 2 + E 2 v ζ 2 .
Define the non-linear operator as
1 s α E [ u ( ξ , ζ , ) ] s 2 α u ( ξ , ζ , 0 ) = E u u ξ v u ζ + 1 R e 2 u ξ 2 + 2 u ζ 2 , 1 s β E [ v ( ξ , ζ , ) ] s 2 β v ( ξ , ζ , 0 ) = E u v ξ v v ζ + 1 R e 2 u ξ 2 + 2 u ζ 2 .
By the above equation, we get
E [ u ( ξ , ζ , ) ] = s 2 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + s α u u ξ v u ζ + 1 R e 2 u ξ 2 + 2 u ζ 2 , E [ v ( ξ , ζ , ) ] = s 2 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + s β u v ξ v v ζ + 1 R e 2 v ξ 2 + 2 v ζ 2 .
Apply inverse E T on Equation (27) and then reduces to
u ( ξ , ζ , ) = 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + E 1 s α u u ξ v u ζ + 1 R e 2 u ξ 2 + 2 u ζ 2 , v ( ξ , ζ , ) = 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + E 1 s β u v ξ v v ζ + 1 R e 2 v ξ 2 + 2 v ζ 2 .
Now we implement HPM
ω = 0 p ω u ω ( ξ , ζ , ) = 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + p E 1 s α E ω = 0 p ω 1 R e 2 u ω ξ 2 + 2 u ω ζ 2 + ω = 0 p ω H ω ( u ) . ω = 0 p ω v ω ( ξ , ζ , ) = 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + p E 1 s β E ω = 0 p ω 1 R e 2 v m ξ 2 + 2 v ω ζ 2 + ω = 0 p ω H ω ( v ) .
With the help of He’s polynomials H ω ( u ) and H ω ( v ) , the nonlinear terms can be found
Σ ω = 0 p ω H ω ( u ) = u u ξ v u ζ , Σ ω = 0 p ω H ω ( v ) = u v ξ v v ζ .
He’s polynomials are defined as
H 0 ( u ) = u 0 u 0 ξ v 0 u 0 ζ , H 0 ( v ) = u 0 v 0 ξ v 0 v 0 ζ , H 1 ( u ) = ( u 0 u 1 ξ + u 1 u 0 ξ ) ( v 0 u 1 ζ + v 1 u 0 ζ ) , H 1 ( v ) = ( u 0 v 1 ξ + u 1 v 0 ξ ) ( v 0 v 1 ζ + v 1 v 0 ζ ) ,
Comparing p-like coefficients, we get
p 0 : u 0 ( ξ , ζ , ) = 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) , p 0 : v 0 ( ξ , ζ , ) = 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) ,
p 1 : u 1 ( ξ , ζ , ) = E 1 s α E 1 R e 2 u 0 ξ 2 + 2 u 0 ζ 2 + H 0 ( u ) . p 1 : v 1 ( ξ , ζ , ) = E 1 s β E 1 R e 2 v 0 ξ 2 + 2 v 0 ζ 2 + H 0 ( v ) .
p 1 : u 1 ( ξ , ζ , ) = R e exp R e 8 ( ξ ζ ) α 128 ( 1 + exp ( ( R e 8 ) ( ξ ζ ) ) ) 2 Γ ( α + 1 ) , p 1 : v 1 ( ξ , ζ , ) = R e exp R e 8 ( ξ ζ ) β 128 ( 1 + exp ( ( R e 8 ) ( ξ ζ ) ) ) 2 Γ ( β + 1 ) .
p 2 : u 2 ( ξ , ζ , ) = E 1 s α E 1 R e 2 u 1 ξ 2 + 2 u 1 ζ 2 + H 1 ( u ) . p 2 : v 2 ( ξ , ζ , ) = E 1 s β E 1 R e 2 v 1 ξ 2 + 2 v 1 ζ 2 + H 1 ( v ) .
p 2 : u 2 ( ξ , ζ , ) = 1 4096 ( exp ( ( R e 8 ) ( ξ ζ ) ) ) 4 Γ ( α + β + 1 ) exp R e 8 ( ξ ζ ) R e 2 exp ( ( R e 8 ) ( ξ ζ ) ) β Γ ( α + 1 ) + 1 + exp R e 8 ( ξ ζ ) + exp R e 8 ( ξ ζ ) α Γ ( β + 1 ) , p 2 : v 2 ( ξ , ζ , ) = exp R e 8 ( ξ ζ ) 4096 ( exp ( ( R e 8 ) ( ξ ζ ) ) ) 4 Γ ( α + β + 1 ) R e 2 ( 1 + exp ( ( R e / 8 ) ( ξ ζ ) ) + exp ( ( R e / 4 ) ( ξ ζ ) ) ) β Γ ( α + 1 ) + 1 + exp R e 8 ( ξ ζ ) + exp R e 8 ( ξ ζ ) α Γ ( β + 1 ) .
Provides the series form solution is u ( ξ , ζ , ) = Σ ω = 0 u ω ( ξ , ζ , ) and v ( ξ , ζ , ) = Σ ω = 0 v ω ( ξ , ζ , )
u ( ξ , ζ , ) = 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) R e exp R e 8 ( ξ ζ ) α 128 ( 1 + exp ( ( R e 8 ) ( ξ ζ ) ) ) 2 Γ ( α + 1 ) 1 4096 ( exp ( ( R e 8 ) ( ξ ζ ) ) ) 4 Γ ( α + β + 1 ) [ exp R e 8 ( ξ ζ ) R e 2 exp ( ( R e 8 ) ( ξ ζ ) ) β Γ ( α + 1 ) + 1 + exp R e 8 ( ξ ζ ) + exp R e 8 ( ξ ζ ) α Γ ( β + 1 ) ] + , v ( ξ , ζ , ) = 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + R e exp R e 8 ( ξ ζ ) α 128 ( 1 + exp ( ( R e 8 ) ( ξ ζ ) ) ) 2 Γ ( α + 1 ) 1 4096 ( exp ( ( R e 8 ) ( ξ ζ ) ) ) 4 Γ ( α + β + 1 ) [ exp R e 8 ( ξ ζ ) R e 2 ( ( 1 + exp ( ( R e / 8 ) ( ξ ζ ) ) + exp ( ( R e / 4 ) ( ξ ζ ) ) ) ) β Γ ( α + 1 ) + 1 + exp R e 8 ( ξ ζ ) + exp R e 8 ( ξ ζ ) α Γ ( β + 1 ) ] + .
Now we apply the EDM
Assume that the infinite series solution of the unknown functions u ( ξ , ζ , ) and v ( ξ , ζ , ) respectively as follows
u ( ξ , ζ , ) = ω = 0 u ω ( ξ , ζ , ) a n d v ( ξ , ζ , ) = ω = 0 v ω ( ξ , ζ , )
Note that u u ξ = ω = 0 A ω , u v ξ = ω = 0 B ω , v u ξ = ω = 0 C ω and v v ξ = ω = 0 D ω are the Adomian polynomials and they signifying the non-linear terms. Using the these terms, we can rewrite Equation (28) as
ω = 0 u ω + 1 ( ξ , ζ , ) = 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + E 1 s α ω = 0 A ω ω = 0 B ω + 1 R e ω = 0 u ω ξ ξ + ω = 0 u ω ζ ζ , ω = 0 v ω + 1 ( ξ , ζ , ) = 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + E 1 s β ω = 0 C ω ω = 0 D ω + 1 R e ω = 0 v ω ξ ξ + ω = 0 v ω ζ ζ .
Both sides comparing of Equation (33), we can be written as
u 0 ( ξ , ζ , ) = 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) , v 0 ( ξ , ζ , ) = 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) .
u 1 ( ξ , ζ , ) = R e exp R e 8 ( ξ ζ ) α 128 ( 1 + exp ( ( R e 8 ) ( ξ ζ ) ) ) 2 Γ ( α + 1 ) , v 1 ( ξ , ζ , ) = R e exp R e 8 ( ξ ζ ) β 128 ( 1 + exp ( ( R e 8 ) ( ξ ζ ) ) ) 2 Γ ( β + 1 ) . u 2 ( ξ , ζ , ) = 1 4096 ( exp ( ( R e 8 ) ( ξ ζ ) ) ) 4 Γ ( α + β + 1 ) exp R e 8 ( ξ ζ ) R e 2 exp ( ( R e 8 ) ( ξ ζ ) ) β Γ ( α + 1 ) + 1 + exp R e 8 ( ξ ζ ) + exp R e 8 ( ξ ζ ) α Γ ( β + 1 ) , v 2 ( ξ , ζ , ) = 1 4096 ( exp ( ( R e 8 ) ( ξ ζ ) ) ) 4 Γ ( α + β + 1 ) exp R e 8 ( ξ ζ ) R e 2 ( ( 1 + exp ( ( R e / 8 ) ( ξ ζ ) ) + exp ( ( R e / 4 ) ( ξ ζ ) ) ) ) β Γ ( α + 1 ) + 1 + exp R e 8 ( ξ ζ ) + exp R e 8 ( ξ ζ ) α Γ ( β + 1 ) .
Continuing in the same manner, the remaining components of the Elzaki decomposition method solution u ω and v ω ( ω 3 ) can be achieved smoothly. As a result, we arrive at the series solution as
u ( ξ , ζ , ) = ω = 0 u ω ( ξ , ζ , ) = u 0 ( ξ , ζ , ) + u 1 ( ξ , ζ , ) + u 2 ( ξ , ζ , ) + , u ( ξ , ζ , ) = 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) R e exp R e 8 ( ξ ζ ) α 128 ( 1 + exp ( ( R e 8 ) ( ξ ζ ) ) ) 2 Γ ( α + 1 ) 1 4096 ( exp ( ( R e 8 ) ( ξ ζ ) ) ) 4 Γ ( α + β + 1 ) [ exp R e 8 ( ξ ζ ) R e 2 exp ( ( R e 8 ) ( ξ ζ ) ) β Γ ( α + 1 ) + 1 + exp R e 8 ( ξ ζ ) + exp R e 8 ( ξ ζ ) α Γ ( β + 1 ) ] + , v ( ξ , ζ , ) = ω = 0 v ω ( ξ , ζ , ) = v 0 ( ξ , ζ , ) + v 1 ( ξ , ζ , ) + v 2 ( ξ , ζ , ) + , v ( ξ , ζ , ) = 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) + R e exp R e 8 ( ξ ζ ) α 128 ( 1 + exp ( ( R e 8 ) ( ξ ζ ) ) ) 2 Γ ( α + 1 ) 1 4096 ( exp ( ( R e 8 ) ( ξ ζ ) ) ) 4 Γ ( α + β + 1 ) [ exp R e 8 ( ξ ζ ) R e 2 ( ( 1 + exp ( ( R e / 8 ) ( ξ ζ ) ) + exp ( ( R e / 4 ) ( ξ ζ ) ) ) ) β Γ ( α + 1 ) + 1 + exp R e 8 ( ξ ζ ) + exp R e 8 ( ξ ζ ) α Γ ( β + 1 ) ] + .
The exact results for Equation (23) at α = β = 1 are
u ( ξ , ζ , ) = 3 4 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) , v ( ξ , ζ , ) = 3 4 + 1 4 ( 1 + exp ( ( R e / 32 ) 4 ξ + 4 ζ ) ) .
In Figure 1, show that the Elzaki decomposition method and Homotopy perturbation transform method show that the close contact with each other of Example 1. In Figure 2, represent the different fractional-order behaviour of u ( ξ , ζ , ) . Similarly, in Figure 3, show that the Elzaki decomposition method and Homotopy perturbation transform method show that the close contact with each other of Example 1. In Figure 4, represent the different fractional-order behaviour of v ( ξ , ζ , ) . In Table 1 and Table 2 show that the absolute error with different fractional-order with respect to α and β .
Example 2.
Consider the fractional-order system of Burgers equations
D α u = 2 u u ξ + 2 v u ζ + 2 u ξ 2 + 2 u ζ 2 , D β v = 2 u v ξ + 2 v v ζ + 2 v ξ 2 + 2 v ζ 2 , 0 < α , β 1 ,
with initial conditions
u ( ξ , ζ , 0 ) = 1 tanh ( ξ + 2 ζ + 1 ) , v ( ξ , ζ , 0 ) = 1 2 tanh ( ξ + 2 ζ + 1 ) .
Now by using E T on Equation (37), we get series solutions
E [ D α u ( ξ , ζ , ) ] = E 2 u u ξ + E 2 v u ζ + E 2 u ξ 2 + E 2 u ζ 2 , E [ D β v ( ξ , ζ , ) ] = E 2 u v ξ + E 2 v v ζ + E 2 v ξ 2 + E 2 v ζ 2 .
Define the non-linear operator as
1 s α E [ u ( ξ , ζ , ) ] s 2 α u ( ξ , ζ , 0 ) = E 2 u u ξ + 2 v u ζ + 2 u ξ 2 + 2 u ζ 2 , 1 s β E [ v ( ξ , ζ , ) ] s 2 β u ( ξ , ζ , 0 ) = E 2 u v ξ + 2 v v ζ + 2 u ξ 2 + 2 u ζ 2 .
On simplification, the above equation reduces to
E [ u ( ξ , ζ , ) ] = s 2 1 tanh ( ξ + 2 ζ + 1 ) + s α 2 u u ξ + 2 v u ζ + 2 u ξ 2 + 2 u ζ 2 , E [ v ( ξ , ζ , ) ] = s 2 1 + 2 tanh ( ξ + 2 ζ + 1 ) + s β 2 u v ξ + 2 v v ζ + 2 v ξ 2 + 2 v ζ 2 .
Applying inverse E T on Equation (41), we have
u ( ξ , ζ , ) = 1 tanh ( ξ + 2 ζ + 1 ) + E 1 s α 2 u u ξ + 2 v u y + u ξ ξ + u ζ ζ , v ( ξ , ζ , ) = 1 + 2 tanh ( ξ + 2 ζ + 1 ) + E 1 s β 2 u v ξ + 2 v v y + v ξ ξ + v ζ ζ .
Now we implement HPM
ω = 0 p ω u ω ( ξ , ζ , ) = 1 tanh ( ξ + 2 ζ + 1 ) + p E 1 s α E ω = 0 p ω 2 u ω ξ 2 + 2 u ω ζ 2 + ω = 0 p ω H ω ( u ) . ω = 0 p ω v ω ( ξ , ζ , ) = 1 + 2 tanh ( ξ + 2 ζ + 1 ) + p E 1 s β E ω = 0 p ω 2 v ω ξ 2 + 2 v ω ζ 2 + ω = 0 p ω H ω ( v ) .
With the aid of He’s polynomials H ω ( u ) and H ω ( v ) , the nonlinear terms can be found
Σ ω = 0 p ω H ω ( u ) = 2 u u ξ + 2 v u ζ , Σ ω = 0 p ω H ω ( v ) = 2 u v ξ + 2 v v ζ .
He’s polynomials are expressed as
H 0 ( u ) = 2 u 0 u 0 ξ + 2 v 0 u 0 ζ , H 0 ( v ) = 2 u 0 v 0 ξ + 2 v 0 v 0 ζ , H 1 ( u ) = 2 u 0 u 1 ξ + 2 u 1 u 0 ξ + 2 v 0 u 1 ζ + 2 v 1 u 0 ζ , H 1 ( v ) = 2 u 0 v 1 ξ + 2 u 1 v 0 ξ + 2 v 0 v 1 ζ + 2 v 1 v 0 ζ ,
Comparing p-like coefficients, we get
p 0 : u 0 ( ξ , ζ , ) = 1 tanh ( ξ + 2 ζ + 1 ) , p 0 : v 0 ( ξ , ζ , ) = 1 + 2 tanh ( ξ + 2 ζ + 1 ) , p 1 : u 1 ( ξ , ζ , ) = E 1 s α E 2 u 0 ξ 2 + 2 u 0 ζ 2 + H 0 ( u ) . p 1 : v 1 ( ξ , ζ , ) = E 1 s β E 2 v 0 ξ 2 + 2 v 0 ζ 2 + H 0 ( v ) . p 1 : u 1 ( ξ , ζ , ) = 2 s e c h ( ξ + 2 ζ + 1 ) α Γ ( α + 1 ) , p 1 : v 1 ( ξ , ζ , ) = 4 s e c h ( ξ + 2 ζ + 1 ) β Γ ( β + 1 ) .
p 2 : u 2 ( ξ , ζ , ) = E 1 s α E 2 u 1 ξ 2 + 2 u 1 ζ 2 + H 1 ( u ) . p 2 : v 2 ( ξ , ζ , ) = E 1 s β E 2 v 1 ξ 2 + 2 v 1 ζ 2 + H 1 ( v ) . u 2 ( ξ , ζ , ) = 8 s e c h 2 ( ξ + 2 ζ + 1 ) Γ ( α + β + 1 ) ( 2 β Γ ( α + 1 ) s e c h 2 ( ξ + 2 ζ + 1 ) + β Γ ( β + 1 ) ( 2 s e c h 2 ( ξ + 2 ζ + 1 ) + tanh ( ξ + 2 ζ + 1 ) ) ) , v 2 ( ξ , ζ , ) = 8 s e c h 2 ( ξ + 2 ζ + 1 ) Γ ( α + β + 1 ) ( β Γ ( α + 1 ) s e c h 2 ( ξ + 2 ζ + 1 ) + β Γ ( β + 1 ) ( 2 s e c h 2 ( ξ + 2 ζ + 1 ) + 2 tanh ( ξ + 2 ζ + 1 ) ) ) .
Provides the series form result is u ( ξ , ζ , ) = Σ ω = 0 u ω ( ξ , ζ , ) and v ( ξ , ζ , ) = Σ ω = 0 v ω ( ξ , ζ , )
u ( ξ , ζ , ) = 1 tanh ( ξ + 2 ζ + 1 ) 2 s e c h ( ξ + 2 ζ + 1 ) α Γ ( α + 1 ) + 8 s e c h 2 ( ξ + 2 ζ + 1 ) Γ ( α + β + 1 ) ( 2 β Γ ( α + 1 ) s e c h 2 ( ξ + 2 ζ + 1 ) + β Γ ( β + 1 ) ( 2 s e c h 2 ( ξ + 2 ζ + 1 ) + tanh ( ξ + 2 ζ + 1 ) ) ) + , v ( ξ , ζ , ) = 1 + 2 tanh ( ξ + 2 ζ + 1 ) + 4 s e c h ( ξ + 2 ζ + 1 ) β Γ ( β + 1 ) 8 s e c h 2 ( ξ + 2 ζ + 1 ) Γ ( α + β + 1 ) ( β Γ ( α + 1 ) s e c h 2 ( ξ + 2 ζ + 1 ) + β Γ ( β + 1 ) ( 2 s e c h 2 ( ξ + 2 ζ + 1 ) + 2 tanh ( ξ + 2 ζ + 1 ) ) ) + .
Now we apply EDM
Suppose that the unidentified functions have an infinite series result u ( ξ , ζ , ) and v ( ξ , ζ , ) respectively as follows
u ( ξ , ζ , ) = ω = 0 u ω ( ξ , ζ , ) a n d v ( ξ , ζ , ) = ω = 0 v ω ( ξ , ζ , )
Note that u u ξ = ω = 0 A ω , u v ξ = ω = 0 B ω , v u ξ = ω = 0 C ω and v v ξ = ω = 0 D ω are the Adomian polynomials and they signifying the non-linear terms. Applying the these terms, we can be write Equation (42) as
n = 0 u ω ( ξ , ζ , ) = 1 tanh ( ξ + 2 ζ + 1 ) + E 1 s α 2 ω = 0 A ω + 2 ω = 0 B ω + ω = 0 u ω ξ ξ + ω = 0 u ω ζ ζ , n = 0 v ω ( ξ , ζ , ) = 1 + 2 tanh ( ξ + 2 ζ + 1 ) + E 1 s β 2 ω = 0 C ω + 2 ω = 0 D ω + ω = 0 v ω ξ ξ + ω = 0 v ω ζ ζ .
Comparing both sides of Equation (47), they can be written as follows
u 0 ( ξ , ζ , ) = 1 tanh ( ξ + 2 ζ + 1 ) , v 0 ( ξ , ζ , ) = 1 + 2 tanh ( ξ + 2 ζ + 1 ) . u 1 ( ξ , ζ , ) = 2 s e c h ( ξ + 2 ζ + 1 ) α Γ ( α + 1 ) , v 1 ( ξ , ζ , ) = 4 s e c h ( ξ + 2 ζ + 1 ) β Γ ( β + 1 ) . u 2 ( ξ , ζ , ) = 8 s e c h 2 ( ξ + 2 ζ + 1 ) Γ ( α + β + 1 ) ( 2 β Γ ( α + 1 ) s e c h 2 ( ξ + 2 ζ + 1 ) + β Γ ( β + 1 ) ( 2 s e c h 2 ( ξ + 2 ζ + 1 ) + tanh ( ξ + 2 ζ + 1 ) ) ) , v 2 ( ξ , ζ , ) = 8 s e c h 2 ( ξ + 2 ζ + 1 ) Γ ( α + β + 1 ) ( β Γ ( α + 1 ) s e c h 2 ( ξ + 2 ζ + 1 ) + β Γ ( β + 1 ) ( 2 s e c h 2 ( ξ + 2 ζ + 1 ) + 2 tanh ( ξ + 2 ζ + 1 ) ) ) .
Proceeding in the same manner, the remaining components of the Elzaki decomposition method (EDM) solution u ω and v ω ( ω 3 ) can be achieved smoothly. As a result, we arrive at the series solution as
u ( ξ , ζ , ) = ω = 0 u ω ( ξ , ζ , ) = u 0 ( ξ , ζ , ) + u 1 ( ξ , ζ , ) + u 2 ( ξ , ζ , ) + , u ( ξ , ζ , ) = 1 tanh ( ξ + 2 ζ + 1 ) 2 s e c h ( ξ + 2 ζ + 1 ) α Γ ( α + 1 ) + 8 s e c h 2 ( ξ + 2 ζ + 1 ) Γ ( α + β + 1 ) ( 2 β Γ ( α + 1 ) s e c h 2 ( ξ + 2 ζ + 1 ) + β Γ ( β + 1 ) ( 2 s e c h 2 ( ξ + 2 ζ + 1 ) + tanh ( ξ + 2 ζ + 1 ) ) ) + , v ( ξ , ζ , ) = ω = 0 v ω ( ξ , ζ , ) = v 0 ( ξ , ζ , ) + v 1 ( ξ , ζ , ) + v 2 ( ξ , ζ , ) + , v ( ξ , ζ , ) = 1 + 2 tanh ( ξ + 2 ζ + 1 ) + 4 s e c h ( ξ + 2 ζ + 1 ) β Γ ( β + 1 ) 8 s e c h 2 ( ξ + 2 ζ + 1 ) Γ ( α + β + 1 ) ( β Γ ( α + 1 ) s e c h 2 ( ξ + 2 ζ + 1 ) + β Γ ( β + 1 ) ( 2 s e c h 2 ( ξ + 2 ζ + 1 ) + 2 tanh ( ξ + 2 ζ + 1 ) ) ) + .
The exact solution for Equation (37) is given by
u ( ξ , ζ , ) = 1 tanh ( ξ + 2 ζ + 2 + 1 ) , v ( ξ , ζ , ) = 1 + 2 tanh ( ξ + 2 ζ + 2 + 1 ) .
In Figure 5, show that the Elzaki decomposition method and Homotopy perturbation transform method show that the close contact with each other of Example 2. In Figure 6, represent the different fractional-order behaviour of u ( ξ , ζ , ) . Similarly, in Figure 7, show that the Elzaki decomposition method and Homotopy perturbation transform method show that the close contact with each other of Example 2. In Figure 8, represent the different fractional-order behaviour of v ( ξ , ζ , ) .

5. Conclusions

In the present article, the homotopy perturbation method and Elzaki decomposition method are applied for the solution of coupled systems of fractional Burger equations. The graphical and tabular representations of the derived results have been done. These representations of the obtained results have clearly confirmed the higher accuracy of the suggested methods. The solutions are obtained for fractional systems which are closely related to their actual solutions. The convergence of fractional solutions to integer order solution has been shown. The fewer calculations and higher accuracy are the valuable themes of the present methods. The researchers then modified it to solve other systems with fractional partial differential equations.

Author Contributions

Data curation, Y.C.; Investigation, Y.C.; Methodology, S.S.; Project administration, N.A.S.; Software, K.S.; Supervision, J.D.C.; Validation, K.S.; Writing—original draft, N.A.S.; Writing—review & editing, J.D.C. All authors have read and agreed to the published version of the manuscript.

Funding

This research received no external funding.

Data Availability Statement

Not applicable.

Acknowledgments

This work was supported by Korea Institute of Energy Technology Evaluation and Planning (KETEP) grant funded by the Korea government (MOTIE) (20202020900060, The Development and Application of Operational Technology in Smart Farm Utilizing Waste Heat from Particulates Reduced Smokestack). This work was sponsored in part by Aeronautical Science Foundation of China (No. 2015ZB55002) and Natural Science Foundation of Henan Province (No. 182300410239).

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. EDM and HPTM solutions of u ( ξ , ζ , ) of example 1 at α = 1 .
Figure 1. EDM and HPTM solutions of u ( ξ , ζ , ) of example 1 at α = 1 .
Symmetry 13 01786 g001
Figure 2. EDM and HPTM solutions of u ( ξ , ζ , ) of example 1 at different value of α .
Figure 2. EDM and HPTM solutions of u ( ξ , ζ , ) of example 1 at different value of α .
Symmetry 13 01786 g002
Figure 3. EDM and HPTM solutions of v ( ξ , ζ , ) of example 1 at β = 1 .
Figure 3. EDM and HPTM solutions of v ( ξ , ζ , ) of example 1 at β = 1 .
Symmetry 13 01786 g003
Figure 4. EDM and HPTM solutions of v ( ξ , ζ , ) of example 1 at different value of β .
Figure 4. EDM and HPTM solutions of v ( ξ , ζ , ) of example 1 at different value of β .
Symmetry 13 01786 g004
Figure 5. EDM and HPTM solutions of u ( ξ , ζ , ) of example 2 at α = 1 .
Figure 5. EDM and HPTM solutions of u ( ξ , ζ , ) of example 2 at α = 1 .
Symmetry 13 01786 g005
Figure 6. EDM and HPTM solutions of u ( ξ , ζ , ) of example 2 at different value of α .
Figure 6. EDM and HPTM solutions of u ( ξ , ζ , ) of example 2 at different value of α .
Symmetry 13 01786 g006
Figure 7. EDM and HPTM solutions of v ( ξ , ζ , ) of example 2 at β = 1 .
Figure 7. EDM and HPTM solutions of v ( ξ , ζ , ) of example 2 at β = 1 .
Symmetry 13 01786 g007
Figure 8. EDM and HPTM solutions of v ( ξ , ζ , ) of example 2 at different value of β .
Figure 8. EDM and HPTM solutions of v ( ξ , ζ , ) of example 2 at different value of β .
Symmetry 13 01786 g008
Table 1. Numerical analysis of example 1 at u ( ξ , ζ , ) different fractional-order of α .
Table 1. Numerical analysis of example 1 at u ( ξ , ζ , ) different fractional-order of α .
ξ AE ( α = 0.4 )AE ( α = 0.6 )AE ( α = 0.8 ) AE ( α = 1 )
15.1298036 × 10 03 8.5968820 × 10 04 1.1526960 × 10 05 1.4693 × 10 10
21.0533254900 × 10 02 1.7251291 × 10 03 2.3064850 × 10 05 2.1224 × 10 09
0.131.5936706200 × 10 02 2.5905700 × 10 03 3.4602750 × 10 05 2.7754 × 10 09
42.1340157400 × 10 02 3.4560108 × 10 03 4.6140640 × 10 05 3.4285 × 10 09
52.6743608600 × 10 02 4.3214516 × 10 03 5.7678540 × 10 05 4.0815 × 10 09
16.5526269 × 10 03 1.2845443 × 10 04 1.9524030 × 10 05 8.9043500 × 10 08
21.3585147 × 10 02 2.5823037 × 10 03 3.9081030 × 10 05 1.2243480 × 10 08
0.232.0617667100 × 10 03 3.8800631 × 10 03 5.8638020 × 10 05 1.5582620 × 10 08
42.7650187200 × 10 02 5.1778225 × 10 03 7.8195020 × 10 05 1.8921750 × 10 08
53.4682707200 × 10 02 6.4755819 × 10 03 9.7752020 × 10 05 2.2260880 × 10 08
17.5239217 × 10 03 1.6203247 × 10 04 2.6503270 × 10 05 9.9570730 × 10 08
21.5715901300 × 10 02 3.2621458 × 10 03 5.3069340 × 10 05 1.2801951 × 10 08
0.332.3907880800 × 10 02 4.9039669 × 10 03 7.9635420 × 10 05 1.5646829 × 10 08
43.2099860300 × 10 02 6.5457880 × 10 03 1.0620149 × 10 05 1.8491707 × 10 08
54.0291839800 × 10 02 8.1876092 × 10 03 1.3276756 × 10 05 2.1336585 × 10 08
18.2762123 × 10 03 1.9075950 × 10 03 3.2874570 × 10 05 5.7825882 × 10 09
21.7398405800 × 10 02 3.8455493 × 10 03 6.5848290 × 10 05 6.7463529 × 10 08
0.432.6520599300 × 10 02 5.7835036 × 10 03 9.8822010 × 10 05 7.7101176 × 10 08
43.5642792800 × 10 02 7.7214580 × 10 03 1.3179574 × 10 05 8.6738823 × 10 08
54.4764986200 × 10 02 9.6594122 × 10 03 1.6476946 × 10 05 9.6376470 × 10 08
18.8947364 × 10 03 2.1627817 × 10 03 3.8817930 × 10 04 2.3900 × 10 08
21.8806520800 × 10 02 4.3652454 × 10 03 7.7777130 × 10 04 3.5300 × 10 08
0.532.8718305200 × 10 02 6.5677091 × 10 03 1.1673633 × 10 05 4.6600 × 10 08
43.8630089800 × 10 02 8.7701729 × 10 03 1.5569554 × 10 04 5.8 × 10 08
54.8541874400 × 10 02 1.0972636700 × 10 03 1.9465475 × 10 04 6.9300000 × 10 08
Table 2. Numerical analysis of example 1 at v ( ξ , ζ , ) at different fractional-order of α .
Table 2. Numerical analysis of example 1 at v ( ξ , ζ , ) at different fractional-order of α .
ξ AE ( α = 0.4 )AE ( α = 0.6 )AE ( α = 0.8 ) AE ( α = 1 )
15.6770988 × 10 04 8.7119340 × 10 05 1.1548840 × 10 07 1.6326 × 10 10
25.3834512 × 10 03 8.4544080 × 10 04 9.5379000 × 10 07 2.0407510200 × 10 09
0.135.0898036 × 10 03 8.1968820 × 10 04 7.5269600 × 10 07 4.0814857200 × 10 09
44.7961560 × 10 03 7.9393560 × 10 04 5.5160200 × 10 07 6.1222204100 × 10 09
54.5025084 × 10 03 7.6818300 × 10 04 3.5050800 × 10 07 8.1629551100 × 10 09
17.5124132 × 10 04 1.3109744 × 10 05 1.9589970 × 10 07 2.2260880 × 10 08
26.9925200 × 10 03 1.2577593 × 10 04 1.5557000 × 10 07 4.3444869600 × 10 08
0.236.4726268 × 10 03 1.2045442 × 10 04 1.1524030 × 10 07 8.6867478200 × 10 08
45.9527336 × 10 03 1.1513291 × 10 04 7.4910600 × 10 06 1.3029008690 × 10 08
55.4328404 × 10 03 1.0981140 × 10 04 3.4580900 × 10 06 1.7371269560 × 10 08
18.8600372900 × 10 04 1.6633175900 × 10 05 2.6628869 × 10 06 4.2673170 × 10 08
28.1319795 × 10 03 1.5818212 × 10 04 2.0566070 × 10 06 7.2886243900 × 10 08
0.337.4039217 × 10 03 1.5003248 × 10 04 1.4503270 × 10 06 1.4534575610 × 10 08
46.6758639 × 10 03 1.4188284 × 10 04 8.4404700 × 10 06 2.1780526830 × 10 08
55.9478061 × 10 03 1.3373320 × 10 04 2.3776700 × 10 06 2.9026478050 × 10 08
19.9681746700 × 10 04 1.9683136700 × 10 04 3.3072887 × 10 06 3.8550588 × 10 09
29.0421934 × 10 03 1.8579543 × 10 04 2.4973720 × 10 06 1.1668329410 × 10 08
0.438.1162122 × 10 03 1.7475950 × 10 04 1.6874560 × 10 06 2.2951152940 × 10 08
47.1902310 × 10 03 1.6372357 × 10 04 8.7754000 × 10 06 3.4233976470 × 10 08
56.2642497 × 10 03 1.5268763 × 10 04 6.7623000 × 10 06 4.5516800 × 10 08
11.0928832650 × 10 04 2.2421458500 × 10 04 3.9100485 × 10 06 1.2600000 × 10 08
29.8117844 × 10 03 2.1024637 × 10 04 2.8959200 × 10 06 1.0050239900 × 10 08
0.538.6947361 × 10 03 1.9627815 × 10 04 1.8817910 × 10 06 2.0100478600 × 10 08
47.5776879 × 10 03 1.8230994 × 10 04 8.6766300 × 10 06 3.0150717200 × 10 08
56.4606397 × 10 03 1.6834173 × 10 04 1.4646500 × 10 06 4.0200955900 × 10 08
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Cui, Y.; Shah, N.A.; Shi, K.; Saleem, S.; Chung, J.D. A Comparative Study of the Fractional-Order System of Burgers Equations. Symmetry 2021, 13, 1786. https://doi.org/10.3390/sym13101786

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Cui Y, Shah NA, Shi K, Saleem S, Chung JD. A Comparative Study of the Fractional-Order System of Burgers Equations. Symmetry. 2021; 13(10):1786. https://doi.org/10.3390/sym13101786

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Cui, Yanmei, Nehad Ali Shah, Kunju Shi, Salman Saleem, and Jae Dong Chung. 2021. "A Comparative Study of the Fractional-Order System of Burgers Equations" Symmetry 13, no. 10: 1786. https://doi.org/10.3390/sym13101786

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