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Article

Series Solutions of High-Dimensional Fractional Differential Equations

1
College of Information Technology, Jilin Agricultural University, Changchun 130118, China
2
School of Mathematics, Jilin University, Changchun 130012, China
3
School of Mathematics and Statistics, Northeast Normal University, Changchun 130024, China
*
Author to whom correspondence should be addressed.
Mathematics 2021, 9(17), 2021; https://doi.org/10.3390/math9172021
Submission received: 14 June 2021 / Revised: 17 August 2021 / Accepted: 20 August 2021 / Published: 24 August 2021
(This article belongs to the Special Issue Fractional Differential Equations and Control Problems)

Abstract

:
In the present paper, the series solutions and the approximate solutions of the time–space fractional differential equations are obtained using two different analytical methods. One is the homotopy perturbation Sumudu transform method (HPSTM), and another is the variational iteration Laplace transform method (VILTM). It is observed that the approximate solutions are very close to the exact solutions. The solutions obtained are very useful and significant to analyze many phenomena, and the solutions have not been reported in previous literature. The salient feature of this work is the graphical presentations of the third approximate solutions for different values of order α .

1. Introduction

The fractional derivative has a long history which is as old as the integer derivative and was first mentioned in a letter from Leibniz to L’Hospital in 1695 [1]. Presently, this subject is widely applied in plasma physics, fluid dynamics, solid-state physics, engineering, economics, medicine, financial market, non-Newtonian mechanics, automatic control theory, chemical physics and so on (see [2,3,4,5,6,7,8], for example). In particular, the authors obtained the existence and uniqueness of the solution of fractional epidemiological model for computer viruses [6] and fractional SIR epidemic model of childhood disease [7], respectively. The reason it is widely used in science and engineering community is that fractional derivative is not a local operator. That means the next state of an equation depends not only on its current state but also on all its historical states. This strong memory effects shows that fractional derivative is very important to represent the treatment and to manage the malaria disease and other kinds of problems [7]. However, many definitions of fractional integral and fractional derivative have been proposed without a uniform one, for instance, Riemann–Liouville fractional integral, Caputo fractional derivative, Weyl fractional derivative [9], Caputo–Fabrizio fractional derivative [6], Atanagana–Baleanu fractional derivative [7] and so on. The most commonly used definitions are Riemann–Liouville integral and Caputo derivative.
For general nonlinear equations, it is difficult to derive exact solutions. If they are not available, the obtaining of the series solutions or the numerical solutions may be crucial, because they can interpret many physical phenomena and are useful for physicists. Therefore, the exact solutions can be replaced by the approximate solutions within a certain scale. There are several approximation methods for deriving series solutions of fractional differential equations, including the Adomian decomposition method [10,11], the homotopy analysis method [12,13,14], the variational iteration method [15,16], the homotopy perturbation method [17,18], the Exp-function method [19,20] and the Elzaki projected differential transform method [21] and so on.
In ref. [22], the homotopy perturbation Sumudu transform method was proposed, which was an elegant combination of Sumudu transform and homotopy perturbation method, and it is a powerful mathematical method for solving fractional differential equations. In ref. [23], the authors extended the HPSTM to the time fractional differential equation. In this work, we apply this method to general time–space fractional differential equations. Comparing the HPSTM with other classical numerical methods, we know that the HPSTM not only reduce the volume of computational work but also maintain a high accuracy of the results. At the same time, the HPSTM does not need over restrictive assumption or linearization.
In ref. [24], the authors proposed an analytical method, called the variational iteration Laplace transform method. In this method, Laplace transform can overcome principle drawbacks in applications of the variational iteration method to fractional equations. The VILTM was also investigated by many authors to handle time fractional equations arising in science and engineering [25,26]. In ref. [27], the authors chose Lagrange multiplier as 1 to obtain analytical solutions of fractional wave-like equations. In the VILTM, the main problem is how to determine the Lagrange multiplier. Until now, there is no effective method to identify the Lagrange multiplier. In this work, using the Laplace transform, we can easily derive new variational iteration formula and Lagrange multiplier without tedious calculations.
The rest of the paper is organized as follows. In Section 2, we introduce some basic ideas of fractional calculus, the Sumudu transform and the Laplace transform. In Section 3, we illustrate the concrete steps of the HPSTM, and provide the condition for convergence and error estimates of the method. In Section 4, we illustrate the concrete steps of the VILTM, and provide the condition for convergence and error estimates of the method. In Section 5, we apply the HPSTM and the VILTM to obtain approximation solutions of fractional equations with initial values. We also include some numerical results to illustrate our results. Throughout the paper, the equations with fractional-order derivatives in the Caputo sense are considered.

2. Preliminaries

Definition 1
([9]). A real function f: R + R belongs to C μ , μ R , if there exists a real number k > μ such that f ( x ) = x k g ( x ) , where g ( x ) C [ 0 , + ) , and it is said to be in the space C μ m if f ( m ) C μ , m N .
Definition 2
([9]). The Riemann–Liouville fractional integral of order α 0 of a function f C μ is defined as follows:
I α f ( x ) : = 1 Γ ( α ) 0 x ( x τ ) α 1 f ( τ ) d τ , α > 0 , x > 0 , f ( x ) , α = 0 ,
where μ 1 , Γ is the Gamma function.
Definition 3
([9]). The Caputo fractional derivative operator of order α > 0 of f C μ n ( μ 1 , n N ) is defined as follows:
D α f ( x ) : = 1 Γ ( n α ) 0 x ( x τ ) n α 1 f ( n ) ( τ ) d τ , n 1 < α < n , x > 0 , f ( n ) ( x ) , α = n .
Consider f ( x , t ) as a function of t, if it belongs to C μ n ( μ 1 , n N ) , then we have the following definition for time fractional derivative.
Definition 4
([9]). The Caputo time fractional derivative operator of order α > 0 of f ( x , t ) is defined as follows:
D t α f ( x , t ) : = 1 Γ ( n α ) 0 t ( t τ ) n α 1 n f ( x , τ ) τ n d τ , n 1 < α < n , t > 0 , n f ( x , t ) t n , α = n .
Consider f ( x , t ) as a function of x, if it belongs to C μ n ( μ 1 , n N ) , then we have the following definition for space fractional derivative.
Definition 5
([9]). The Caputo space fractional derivative operator of order β > 0 of f ( x , t ) is defined as follows:
D x β f ( x , t ) : = 1 Γ ( n β ) 0 x ( x τ ) n β 1 n f ( τ , t ) τ n d τ , n 1 < β < n , x > 0 , n f ( x , t ) x n , β = n .
Definition 6
([28]). The Sumudu transform, is defined over the set of function
A = f ( t ) : M , τ 1 , τ 2 > 0 , s . t . | f ( t ) | < M e | t | τ j , if t ( 1 ) j × [ 0 , + )
by the following formula:
S [ f ( t ) ] ( u ) = 0 f ( u t ) e t d t , u ( τ 1 , τ 2 ) .
Definition 7
([25]). The Laplace transform, is defined over the set of function
A = f ( t ) C [ 0 , + ) : M > 0 a n d a R , s . t . | f ( t ) | M e a t
by the following formula:
L [ f ( t ) ] ( s ) = 0 f ( t ) e s t d t , s > a .
Property 1
([29,30]). (i) The Sumudu transform satisfies linear property, i.e.,
S [ a f ( t ) + b h ( t ) ] = a S [ f ( t ) ] + b S [ h ( t ) ] ,
where a , b are constants.
(ii)
S [ t α ] = u α Γ ( α + 1 ) , α > 0 .
Property 2
([25]). (i) The Laplace transform satisfies linear property, i.e.,
L [ a f ( t ) + b h ( t ) ] = a L [ f ( t ) ] + b L [ h ( t ) ] ,
where a , b are constants.
(ii)
L [ t α ] = s α 1 Γ ( α + 1 ) , α > 0 .
Lemma 1
([29,30]). The Sumudu transform of the Caputo fractional derivative is
S [ D t α f ( t ) ] = u α S [ f ( t ) ] k = 0 m u α + k f ( k ) ( 0 ) , m < α m + 1 , m N .
Lemma 2
([25]). The Laplace transform of the Caputo fractional derivative is
L [ D t α f ( t ) ] = s α L [ f ( t ) ] k = 0 m s α k 1 f ( k ) ( 0 ) , m < α m + 1 , m N .

3. Homotopy Perturbation Sumudu Transform Method

In this section, we extend the algorithm of HPSTM [22] to the general fractional nonhomogeneous differential equation in R 3
D t α U ( x , y , z , t ) + R U ( x , y , z , t ) + N U ( x , y , z , t ) = g ( x , y , z , t )
with the initial condition
U ( x , y , z , 0 ) = f ( x , y , z ) ,
where α ( 0 , 1 ] , ( x , y , z ) R 3 , t [ 0 , ) , R and N represent the linear and the nonlinear differential operator, respectively, g ( x , y , z , t ) is the source term.
Applying the Sumudu transform to both sides of (3), we obtain
S [ D t α U ( x , y , z , t ) ] + S [ R U ( x , y , z , t ) ] + S [ N U ( x , y , z , t ) ] = S [ g ( x , y , z , t ) ] .
According to the property (1), we have
S [ U ( x , y , z , t ) ] = f ( x , y , z ) u α S [ R U ( x , y , z , t ) + N U ( x , y , z , t ) g ( x , y , z , t ) ] .
Furthermore, applying the inverse Sumudu transform S 1 to both sides of (5), we can obtain
U ( x , y , z , t ) = M ( x , y , z , t ) S 1 [ u α S [ R U ( x , y , z , t ) + N U ( x , y , z , t ) ] ] ,
where M ( x , y , z , t ) represents the term arising from the initial condition and the source term, i.e.,
M ( x , y , z , t ) = f ( x , y , z ) + S 1 [ u α S [ g ( x , y , z , t ) ] ] .
Now we construct the homotopy perturbation equation as follows
U ( x , y , z , t ) = M ( x , y , z , t ) p × S 1 [ u α S [ R U ( x , y , z , t ) + N U ( x , y , z , t ) ] ] , p [ 0 , 1 ] .
According to standard homotopy perturbation method, the solution of (6) is
U ( x , y , z , t ) = n = 0 p n U n ( x , y , z , t ) ,
and the nonlinear term N U ( x , y , z , t ) can be decomposed into
N U ( x , y , z , t ) = n = 0 p n H n ( U ) ,
where H n ( U ) are Adomian polynomials
H n ( U ) = 1 n ! n p n N k = 0 p k U k | p = 0 .
Now, substituting (7) and (8) into (6), we can obtain
n = 0 p n U n ( x , y , z , t ) = M ( x , y , z , t ) p × S 1 u α S R n = 0 p n U n ( x , y , z , t ) + n = 0 p n H n ( U ) .
Comparing the coefficients of same powers of p, we obtain the following recurrence equations
p 0 : U 0 ( x , y , z , t ) = M ( x , y , z , t ) , p n : U n ( x , y , z , t ) = S 1 u α S [ R U n 1 ( x , y , z , t ) + H n 1 ( U ) ] , n = 1 , 2 , .
According to the HPM, we assume that the solution of (4)–(6) can be written as
V ( x , y , z , t ) = lim n U 0 + U 1 p + U 2 p 2 + + U n p n .
Thus, the solution of (3) and (4) is
U ( x , y , z , t ) = lim p 1 V ( x , y , z , t ) = lim n U 0 + U 1 + U 2 + + U n .
The nonlinear differential operator N determines the convergence of series (10). Since the parameter p may be relatively large (we can take p 1 ), the derivatives of the nonlinear part must be chosen sufficiently small. Actually, the series is convergent for most cases [17]. Moreover, there are many references discussing the convergence of series approximate solutions by the homotopy perturbation method, one can see [31] for example.
In the following, we will provide a condition for the convergence of the HPSTM. To do this, we first define an operator T : X X by
T [ v ( x , y , z , t ) ] = S 1 [ u α S [ v ( x , y , z , t ) ] ] ,
where X = { v ( x , y , z , t ) : v is continuous on ( x , y , z , t ) R 3 × [ 0 , ) } is a Banach space with norm | | v | | . Since S is a linear operator, we know that T is a linear operator. The norm of a linear operator T is defined by
| | T | | = sup { | | T v | | , | | v | | 1 } .
Then we have the following theorem for the convergence of the HPSTM.
Theorem 1.
Suppose that the linear operators T and R satisfy | | TR | | < 1 , and the nonlinear operator N satisfies
| | TN u TN v | | γ | | u v | | , u , v X ,
for some constant 0 < γ < 1 | | TR | | . Then the series solution k = 0 U k ( x , y , z , t ) is convergent.
Proof. 
The recurrence equations become
U n ( x , y , z , t ) = TR U n 1 ( x , y , z , t ) T H n 1 ( U ) , n = 1 , 2 , .
Suppose that { S n ( x , y , z , t ) } is the sequence of partial sums of the series solution, i.e.,
S n ( x , y , z , t ) = k = 0 n U k ( x , y , z , t ) , n = 1 , 2 , .
In ref. [32], it was pointed out that the Adomian polynomials H n ( U ) only depend on U 0 , , U n , and thus we can calculate H n ( U ) in an explicit manner by the following relation
N k = 0 n p k U k ( x , y , z , t ) = k = 0 n p k H k ( U ) .
Let p = 1 , we have
N S n ( x , y , z , t ) = k = 0 n H k ( U ) .
Hence, we have
T H n ( U ) = T N S n ( x , y , z , t ) T N S n 1 ( x , y , z , t ) .
For any n > 0 , we have
| | S n + 1 ( x , y , z , t ) S n ( x , y , z , t ) | | = | | TR U n ( x , y , z , t ) + T H n ( U ) | | | | TR U n ( x , y , z , t ) | | + | | T N S n ( x , y , z , t ) T N S n 1 ( x , y , z , t ) | | ( | | TR | | + γ ) | | U n ( x , y , z , t ) | | ( | | TR | | + γ ) n + 1 | | U 0 ( x , y , z , t ) | | .
For any m > n > 0 , we have
| | S m ( x , y , z , t ) S n ( x , y , z , t ) | | | | S m ( x , y , z , t ) S m 1 ( x , y , z , t ) | | + + | | S n + 1 ( x , y , z , t ) S n ( x , y , z , t ) | | k = n + 1 m ( | | TR | | + γ ) k | | U 0 ( x , y , z , t ) | | < ( | | TR | | + γ ) n + 1 1 ( | | TR | | + γ ) | | U 0 ( x , y , z , t ) | | .
Since 0 < | | TR | | + γ < 1 , we know that { S n ( x , y , z , t ) } is a Cauchy sequence in Banach space X, so it converges, and we have
U ( x , y , z , t ) = lim n k = 0 n U k ( x , y , z , t ) .
Let m in inequality (11), we have the following error estimates
| | U ( x , y , z , t ) S n ( x , y , z , t ) | | < ( | | TR | | + γ ) n + 1 1 ( | | TR | | + γ ) | | U 0 ( x , y , z , t ) | | .
The proof is completed. □
Remark 1.
Comparing the HPSTM with other classical methods, we know that the homotopy series solutions for fractional equations can be constructed without using any overstrict assumption.

4. Variational Iteration Laplace Transform Method

In this section, we introduce the algorithm of VILTM [24,25,26] for the general fractional nonhomogeneous differential Equation (3) with the initial condition (4).
Applying the Laplace transform L to both sides of (3), then the iteration formula of (3) becomes
U n + 1 ( x , y , z , s ) = U n ( x , y , z , s ) + λ ( s ) [ s α U n ( x , y , z , s ) f ( x , y , z ) s α 1 + L [ R [ U n ( x , y , z , t ) ] + N [ U n ( x , y , z , t ) ] g ( x , y , z , t ) ] ] ,
where U n is the n-th order approximate solution. Considering L ( R [ U n ] + N [ U n ] ) as restricted term, the Lagrange multiplier can be identified as
λ = 1 s α .
Applying the inverse Laplace transform L 1 to both sides of (12), we obtain
U n + 1 ( x , y , z , t ) = U n ( x , y , z , t ) L 1 [ s α [ s α U n ( x , y , z , s ) f ( x , y , z ) s α 1 + L [ R [ U n ( x , y , z , t ) ] + N [ U n ( x , y , z , t ) ] g ( x , y , z ) ] ] ] = U 0 ( x , y , z , t ) L 1 [ s α L [ R [ U n ( x , y , z , t ) ] + N [ U n ( x , y , z , t ) ] ] ] ,
where the initial iteration value U 0 ( x , y , z , t ) can be determined as
U 0 ( x , y , z , t ) = f ( x , y , z ) + L 1 [ s α L [ g ( x , y , z , t ) ] ] .
Finally, the approximation solution is
U ( x , y , z , t ) = lim n U n ( x , y , z , t ) .
There are many references discussing the convergence of approximate solutions by variational iteration method, one can see [33] for example. In ref. [33], based on the sufficient condition that guarantees the existence of a unique solution, the authors proved that the series solution is convergence.
The following theorem provides the convergence for the VILTM.
Theorem 2.
Suppose that the conditions of Theorem 1 are satisfied. Then the approximate solution U n ( x , y , z , t ) is convergent.
Proof. 
The Sumudu transform and the Laplace transform exhibit a duality relation expressed as follows:
S [ f ( t ) ] ( 1 s ) = s L [ f ( t ) ] ( s ) , L [ f ( t ) ] ( 1 u ) = u S [ f ( t ) ] ( u ) , for s , u > 0 .
By this duality relation, we can prove that
S 1 [ u α S [ f ( t ) ] ] = L 1 [ s α L [ f ( t ) ] ] .
Then we have
L 1 [ s α L [ u ( x , y , z , t ) ] ] = T [ u ( x , y , z , t ) ] .
Hence, the iteration formula becomes
U n + 1 ( x , y , z , t ) = U 0 ( x , y , z , t ) TR [ U n ( x , y , z , t ) ] TN [ U n ( x , y , z , t ) ] .
For any n > 0 , we have
| | U n + 1 ( x , y , z , t ) U n ( x , y , z , t ) | | | | TR U n ( x , y , z , t ) TR U n 1 ( x , y , z , t ) | | + | | TN U n ( x , y , z , t ) TN U n 1 ( x , y , z , t ) | | ( | | TR | | + γ ) | | U n ( x , y , z , t ) U n 1 ( x , y , z , t ) | | ( | | TR | | + γ ) n | | U 1 ( x , y , z , t ) U 0 ( x , y , z , t ) | | = ( | | TR | | + γ ) n | | TR U 0 ( x , y , z , t ) + TN U 0 ( x , y , z , t ) | | .
For any m > n > 0 , we have
| | U m ( x , y , z , t ) U n ( x , y , z , t ) | | | | U m ( x , y , z , t ) U m 1 ( x , y , z , t ) | | + + | | U n + 1 ( x , y , z , t ) U n ( x , y , z , t ) | | k = n m 1 ( | | TR | | + γ ) k | | TR U 0 ( x , y , z , t ) + TN U 0 ( x , y , z , t ) | | < ( | | TR | | + γ ) n 1 ( | | TR | | + γ ) | | TR U 0 ( x , y , z , t ) + TN U 0 ( x , y , z , t ) | | .
Since 0 < | | TR | | + γ < 1 , we know that { U n ( x , y , z , t ) } is a Cauchy sequence in Banach space X, so it converges, and we have
U ( x , y , z , t ) = lim n U n ( x , y , z , t ) .
Let m in inequality (14), we have the following error estimates
| | U ( x , y , z , t ) U n ( x , y , z , t ) | | < ( | | TR | | + γ ) n 1 ( | | TR | | + γ ) | | TR U 0 ( x , y , z , t ) + TN U 0 ( x , y , z , t ) | | .
The proof is completed. □
Remark 2.
The VILTM is easy to apply, which simplifies the applications of variational iteration method to fractional differential equations, and improves the convergence of iteration.

5. Applications of HPSTM and VILTM to Fractional Differential Equations

5.1. The One-Dimensional Time–Space Fractional KdV Equation

The nonlinear KdV equation is an important mathematical model in physics and engineering. The fractional KdV equation has been applied to model a wide range of physical phenomena, such as internal waves in coastal waters, waves in plasma physics, magma flow and conduit waves, flow in blood vessels, boundary layer behavior and so on. In ref. [34], the author introduced a fractional KdV equation with initial conditions, and the explicit numerical solutions are derived by the Adomian decomposition method. In this section, we employ the HPSTM and the VILTM to obtain the series solutions of the following KdV equation, namely
D t α U ( x , t ) = D x 3 U ( x , t ) + U ( x , t ) D x β U ( x , t )
with the initial condition
U ( x , 0 ) = x 2 ,
where 0 < α , β 1 , ( x , t ) R × [ 0 , ) .

5.1.1. Homotopy Perturbation Sumudu Transform Method

Applying the Sumudu transform to both sides of (15) and taking into account the initial condition, we have
S [ U ( x , t ) ] = x 2 + u α S [ D x 3 U ( x , t ) + U ( x , t ) D x β U ( x , t ) ] .
Then the inverse Sumudu transform of (16) implies that
U ( x , t ) = x 2 + S 1 [ u α S [ D x 3 U ( x , t ) + U ( x , t ) D x β U ( x , t ) ] ] .
Now we apply the homotopy perturbation method to obtain the following equation
n = 0 p n U n ( x , t ) = x 2 + p × S 1 u α S D x 3 n = 0 p n U n ( x , t ) + n = 0 p n H n U ( x , t ) ,
where the nonlinear terms H n U ( x , t ) are Adomian polynomials, which are given by
n = 0 p n H n U ( x , t ) = U ( x , t ) D x β U ( x , t ) .
Set
U n ( x , t ) : = U ˜ n ( x ) t n α Γ ( n α + 1 ) ,
then
H n U ( x , t ) = i = 0 n U ˜ i ( x ) D x β U ˜ n i ( x ) t n α Γ ( i α + 1 ) Γ ( ( n i ) α + 1 ) .
Comparing the coefficients with identical powers in p, we have
p 0 : U 0 ( x , t ) = U ˜ 0 ( x ) = x 2 , p 1 : U 1 ( x , t ) = S 1 [ u α S [ D x 3 U 0 ( x , t ) + H 0 U ( x , t ) ] ] = S 1 [ u α S [ D x 3 U ˜ 0 ( x ) + U ˜ 0 ( x ) D x β U ˜ 0 ( x ) ] ] = t α Γ ( α + 1 ) D x 3 U ˜ 0 ( x ) + U ˜ 0 ( x ) D x β U ˜ 0 ( x ) = t α Γ ( α + 1 ) U ˜ 1 ( x ) .
Proceeding in a similar manner, we have
p k : U k ( x , t ) = t k α Γ ( k α + 1 ) { D x 3 U ˜ k 1 ( x ) + i = 0 k 1 Γ ( ( k 1 ) α + 1 ) Γ ( i α + 1 ) Γ ( ( k i 1 ) α + 1 ) U ˜ i ( x ) D x β U ˜ k 1 i ( x ) } = t k α Γ ( k α + 1 ) U ˜ k ( x ) , k = 1 , 2 , ,
where
U ˜ k ( x ) = D x 3 U ˜ k 1 ( x ) + i = 0 k 1 Γ ( ( k 1 ) α + 1 ) Γ ( i α + 1 ) Γ ( ( k i 1 ) α + 1 ) U ˜ i ( x ) D x β U ˜ k 1 i ( x ) .
Hence, the solution U ( x , t ) is represented as
U ( x , t ) = k = 0 U k ( x , t ) = k = 0 U ˜ k ( x ) t k α Γ ( k α + 1 ) .

5.1.2. Variational Iteration Laplace Transform Method

Applying the Laplace transform to both sides of (15), the iteration formula is given by
U n + 1 ( x , s ) = U n ( x , s ) + λ ( s ) [ s α U n ( x , s ) x 2 s α 1 L [ D x 3 U n ( x , t ) + U n ( x , t ) D x β U n ( x , t ) ] ] .
Considering L [ D x 3 U n ( x , t ) + U ( x , t ) D x β U n ( x , t ) ] as restricted term, we can choose the Lagrange multiplier as λ = s α . Using the inverse Laplace transform L 1 , we obtain the iteration formula of (15)
U n + 1 ( x , t ) = x 2 + L 1 [ s α L [ D x 3 U n ( x , t ) + U n ( x , t ) D x β U n ( x , t ) ] ] .
Set
U 0 ( x , t ) : = U ˜ 0 ( x ) = x 2 .
Substituting it into the iteration formula, we have
U 1 ( x , t ) = x 2 + L 1 [ s α L [ D x 3 U 0 ( x , t ) + U 0 ( x , t ) D x β U 0 ( x , t ) ] ] = x 2 + t α Γ ( α + 1 ) D x 3 U ˜ 0 ( x ) + U ˜ 0 ( x ) D x β U ˜ 0 ( x ) , = x 2 + t α Γ ( α + 1 ) U ˜ 1 ( x ) .
Similarly, substituting
U k ( x , t ) = i = 0 k t i α Γ ( i α + 1 ) U ˜ i ( x )
into the iteration formula, we have
U ˜ k ( x ) = D x 3 U ˜ k 1 ( x ) + i = 0 k 1 Γ ( ( k 1 ) α + 1 ) Γ ( i α + 1 ) Γ ( ( k i 1 ) α + 1 ) U ˜ i ( x ) D x β U ˜ k 1 i ( x ) .
When k , the solution can be represented as
U ( x , t ) = lim k U k ( x , t ) ,
which is the same as the limit approximate solution by the HPSTM.

5.2. The Two-Dimensional Time Fractional Diffusion Equation

In ref. [35], Nigmatullin introduced the fractional diffusion equation in physics, which described the diffusion in media with fractal geometry. The fractional diffusion equation can also be used to describe some physical phenomena, such as Stefan problem, thermophysical process, transition flows of complex fluids and so on. In this section, we apply the HPSTM and the VILTM to the following two-dimensional time fractional diffusion equation [36]
D t α U ( x , y , t ) = D x 2 U ( x , y , t ) + D y 2 U ( x , y , t ) , x , y [ 0 , 1 ] , t > 0 , 0 < α 1
with the initial condition
U ( x , y , 0 ) = e x + y .

5.2.1. Homotopy Perturbation Sumudu Transform Method

Applying the Sumudu transform to both sides of (18) and taking into account the initial condition, we obtain
S [ U ( x , y , t ) ] = e x + y + u α S [ D x 2 U ( x , y , t ) + D y 2 U ( x , y , t ) ] .
Then the inverse Sumudu transform of (19) implies that
U ( x , y , t ) = e x + y + S 1 [ u α S [ D x 2 U ( x , y , t ) + D y 2 U ( x , y , t ) ] ] .
Now applying the HPSTM, we obtain
n = 0 p n U n ( x , y , t ) = e x + y + p × S 1 u α S D x 2 n = 0 p n U n ( x , y , t ) + D y 2 n = 0 p n U n ( x , y , t ) .
Comparing the coefficients with identical powers in p, we have
U 0 ( x , y , t ) = U ( x , y , 0 ) = e x + y , U 1 ( x , y , t ) = t α Γ ( α + 1 ) 2 e x + y , U k ( x , y , t ) = t k α Γ ( k α + 1 ) 2 k e x + y , k N .
Therefore, the HPSTM series solution is
U ( x , y , t ) = k = 0 U k ( x , y , t ) = k = 0 t k α Γ ( k α + 1 ) 2 k e x + y = e x + y k = 0 ( 2 t α ) k Γ ( k α + 1 ) .
Set α = 1 in (18), we obtain the following series solution
U ( x , y , t ) = e x + y k = 0 ( 2 t ) k Γ ( k + 1 ) = e x + y + 2 t ,
which is the exact solution of (18) for α = 1 . In addition, the corresponding third approximate solution is
U a p p ( x , y , t ) = e x + y 1 + 2 t Γ ( 2 ) + 4 t 2 Γ ( 3 ) + 8 t 3 Γ ( 4 ) .
The exact solution (22) and the third approximate solution (23) obtained by the HPSTM at x = 1 , y = 0.5 for α = 1 are shown in Figure 1. It is shown from Figure 1 that the third approximate solution is nearly identical with the exact solution. The physical behaviors of the HPSTM solution (22) are shown in Figure 2. The approximate solutions of (21) for different values α 1 are depicted in Figure 3. The error estimates of the approximate solutions (21) obtained by the HPSTM at x = y = 0 for α = 0.5 are shown in Table 1, Table 2 and Table 3. It can be seen from Table 1, Table 2 and Table 3, to control the error within one thousandth, it only needs 8 steps at t = 0.1 , 20 steps at t = 0.5 and 30 steps at t = 1 , and the time of calculation takes only a few seconds. That means this method is rapidly convergent and relatively efficient.

5.2.2. Variational Iteration Laplace Transform Method

Applying the Laplace transform to both sides of (18), the corresponding iteration formula is given by
U n + 1 ( x , y , s ) = U n ( x , y , s ) + λ ( s ) [ s α U n ( x , y , s ) e x + y s α 1 L [ D x 2 U n ( x , y , t ) + D y 2 U n ( x , y , t ) ] ] .
Considering L [ D x 2 U n ( x , y , t ) + D y 2 U n ( x , y , t ) ] as restricted term, we choose the Lagrange multiplier as λ = s α . Using the inverse Laplace transform L 1 , we have the following approximate solution of (18)
U n + 1 ( x , y , t ) = e x + y + L 1 s α L [ D x 2 U n ( x , y , t ) + D y 2 U n ( x , y , t ) ] .
According to the iteration formula, we have
U 0 ( x , y , t ) = e x + y , U 1 ( x , y , t ) = e x + y + L 1 s α L [ D x 2 U 0 ( x , y , t ) + D y 2 U 0 ( x , y , t ) ] = e x + y + t α Γ ( α + 1 ) 2 e x + y , U 2 ( x , y , t ) = e x + y + L 1 s α L [ D x 2 U 1 ( x , y , t ) + D y 2 U 1 ( x , y , t ) ] = e x + y + t α Γ ( α + 1 ) 2 e x + y + t 2 α Γ ( 2 α + 1 ) 4 e x + y , U k ( x , y , t ) = i = 0 k t i α Γ ( i α + 1 ) 2 i e x + y .
When k , the solution can be represented as
U ( x , y , t ) = lim k e x + y i = 0 k ( 2 t α ) i Γ ( i α + 1 ) ,
which is the same as the limit approximate solution by the HPSTM.

5.3. The Three-Dimensional Time Fractional Differential Equation

In this section, we apply the HPSTM and the VILTM to the following three-dimensional time fractional differential equation [36]
D t α U ( x , y , z , t ) = D x 2 U ( x , y , z , t ) + D y 2 U ( x , y , z , t ) + D z 2 U ( x , y , z , t ) , x , y , z [ 0 , 1 ] , t > 0 , 0 < α 1
with the initial condition
U ( x , y , z , 0 ) = ( 1 y ) e x + z .

5.3.1. Homotopy Perturbation Sumudu Transform Method

Applying the Sumudu transform to both sides of (24) and taking into account the initial condition, we obtain
S [ U ( x , y , z , t ) ] = ( 1 y ) e x + z + u α S [ D x 2 U ( x , y , z , t ) + D y 2 U ( x , y , z , t ) + D z 2 U ( x , y , z , t ) ] .
The inverse Sumudu transform of (25) implies that
U ( x , y , z , t ) = ( 1 y ) e x + z + S 1 [ u α S [ D x 2 U ( x , y , z , t ) + D y 2 U ( x , y , z , t ) + D z 2 U ( x , y , z , t ) ] ] .
Using the HPSTM,
n = 0 p n U n ( x , y , z , t ) = ( 1 y ) e x + z + p × S 1 [ u α S [ D x 2 n = 0 p n U n ( x , y , z , t ) + D y 2 n = 0 p n U n ( x , y , z , t ) + D z 2 n = 0 p n U n ( x , y , z , t ) ] ] .
Comparing the coefficients with identical powers in p, we have
U 0 ( x , y , z , t ) = ( 1 y ) e x + z , U 1 ( x , y , z , t ) = t α Γ ( α + 1 ) 2 ( 1 y ) e x + z , U k ( x , y , z , t ) = t k α Γ ( k α + 1 ) 2 k ( 1 y ) e x + z , k N .
Therefore, the HPSTM series solution is
U ( x , y , z , t ) = k = 0 U k ( x , y , z , t ) = k = 0 t k α Γ ( k α + 1 ) 2 k ( 1 y ) e x + z = ( 1 y ) e x + z k = 0 ( 2 t α ) k Γ ( k α + 1 ) .
When α = 1 , the corresponding series solution is given by
U ( x , y , z , t ) = ( 1 y ) e x + z k = 0 ( 2 t ) k Γ ( k + 1 ) = ( 1 y ) e x + z + 2 t ,
which is the exact solution for α = 1 . In addition, the third approximate solution is
U a p p ( x , y , z , t ) = ( 1 y ) e x + z 1 + 2 t Γ ( 2 ) + 4 t 2 Γ ( 3 ) + 8 t 3 Γ ( 4 ) .
The exact solution (28) and the third approximate solution (29) at x = 1 , y = 0.5 , z = 1 for α = 1 are shown in Figure 4. It is shown from Figure 4 that the third approximate solution is closed to the exact solution. For α = 1 , the approximate solutions at different values of x , y , z , t are shown in Figure 5. The approximate solutions of (27) for different values α 1 are depicted in Figure 6. The error estimates of the approximate solutions (27) at x = y = z = 0 for α = 0.5 are the same as in Table 1, Table 2 and Table 3.

5.3.2. Variational Iteration Laplace Transform Method

Applying the Laplace transform to both sides of (24), we obtain the following iteration formula
U n + 1 ( x , y , z , s ) = U n ( x , y , z , s ) + λ ( s ) [ s α U n ( x , y , z , s ) ( 1 y ) e x + z s α 1 L [ D x 2 U ( x , y , z , t ) + D y 2 U ( x , y , z , t ) + D z 2 U ( x , y , z , t ) ] ] .
Considering L [ D x 2 U ( x , y , z , t ) + D y 2 U ( x , y , z , t ) + D z 2 U ( x , y , z , t ) ] ] as restricted term, we can choose the Lagrange multiplier as λ = s α . Using the inverse Laplace transform L 1 , we obtain the following approximate solution of (24)
U n + 1 ( x , y , z , t ) = ( 1 y ) e x + z + L 1 s α L [ D x 2 U n ( x , y , z , t ) + D y 2 U n ( x , y , z , t ) + D z 2 U n ( x , y , z , t ) ] .
According to the iteration formula, we have
U 0 ( x , y , z , t ) = ( 1 y ) e x + z , U 1 ( x , y , z , t ) = ( 1 y ) e x + z + L 1 s α L [ D x 2 U 0 ( x , y , z , t ) + D y 2 U 0 ( x , y , z , t ) + + D z 2 U 0 ( x , y , z , t ) ] = ( 1 y ) e x + z + t α Γ ( α + 1 ) 2 ( 1 y ) e x + z , U 2 ( x , y , z , t ) = ( 1 y ) e x + z + L 1 s α L [ D x 2 U 1 ( x , y , z , t ) + D y 2 U 1 ( x , y , z , t ) + + D z 2 U 1 ( x , y , z , t ) ] = ( 1 y ) e x + z + t α Γ ( α + 1 ) 2 ( 1 y ) e x + z + t 2 α Γ ( 2 α + 1 ) 4 ( 1 y ) e x + z , U k ( x , y , z , t ) = i = 0 k t i α Γ ( i α + 1 ) 2 i ( 1 y ) e x + z .
When k , we obtain the following series solution
U ( x , y , z , t ) = lim k ( 1 y ) e x + z i = 0 k ( 2 t α ) i Γ ( i α + 1 ) ,
which is the same as the limit approximate solution by the HPSTM.

6. Conclusions

In this paper, we investigate the time–space fractional differential equations by the HPSTM and the VILTM. It can be concluded that these two methods are both important and efficient for obtaining approximate analytical solutions of fractional differential equations. The approximate solutions obtained by the HPSTM are uniformly valid not only for small parameters, but also for very large parameter p [ 0 , 1 ] , which is considered to be a “expansion parameter”. The VILTM does not require specific transformations for nonlinear term as required by some existing techniques.
Comparing these two methods with other classical methods, we know that the approximate solutions can be constructed without using any overstrict assumption or linearization, and the solutions are represented as convergent series with easily computable components and rapid convergence. The advantages of these two methods are their flexibility and ability to solve nonlinear equations efficiently and conveniently, and they not only reduce the volume of computational work but also maintain a high accuracy of the solutions. Meanwhile, the high agreement of solutions obtained by the HPSTM and the VILTM reinforces the conclusion that the efficiency of these two methods.

Author Contributions

Conceptualization, J.C. and J.Z.; Formal analysis, J.C. and J.Z.; Funding acquisition, J.C. and J.Z.; Methodology, J.C. and J.Z.; Software, M.C.; Visualization, M.C.; Writing—original draft, J.C.; Writing—review and editing, J.Z. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by NSFC grant 11701212, EDJP grant JJKH20190913KJ and JJKH20211030KJ.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Acknowledgments

The authors would like to thank the reviewers for useful comments and valuable suggestions.

Conflicts of Interest

The authors declare no conflict of interest. The funders had no role in the design of the study; in the collection, analyses, or interpretation of data; in the writing of the manuscript, or in the decision to publish the results.

Abbreviations

The following abbreviations are used in this manuscript:
HPSTMHomotopy perturbation Sumudu transform method
VILTMVariational iteration Laplace transform method

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Figure 1. Exact solution and third approximate solution for α = 1 .
Figure 1. Exact solution and third approximate solution for α = 1 .
Mathematics 09 02021 g001
Figure 2. (a) The HPSTM solution at y = 0.5 . (b) The HPSTM solution at t = 1 . (c) The HPSTM solution at x = 1 .
Figure 2. (a) The HPSTM solution at y = 0.5 . (b) The HPSTM solution at t = 1 . (c) The HPSTM solution at x = 1 .
Mathematics 09 02021 g002
Figure 3. (a) Approximate solutions for different values of α 1 . (b) Approximate solution for α = 0.5 . (c) Approximate solution for α = 0.8 .
Figure 3. (a) Approximate solutions for different values of α 1 . (b) Approximate solution for α = 0.5 . (c) Approximate solution for α = 0.8 .
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Figure 4. Exact solution and third approximate solution for α = 1 .
Figure 4. Exact solution and third approximate solution for α = 1 .
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Figure 5. (a) HPSTM solution at z = 1 and t = 1 . (b) HPSTM solution at x = 1 and t = 1 . (c) HPSTM solution at y = 0.5 and t = 1 .
Figure 5. (a) HPSTM solution at z = 1 and t = 1 . (b) HPSTM solution at x = 1 and t = 1 . (c) HPSTM solution at y = 0.5 and t = 1 .
Mathematics 09 02021 g005
Figure 6. (a) Approximate solutions for different values of α 1 . (b) Approximate solution for α = 0.5 . (c) Approximate solution for α = 0.8 .
Figure 6. (a) Approximate solutions for different values of α 1 . (b) Approximate solution for α = 0.5 . (c) Approximate solution for α = 0.8 .
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Table 1. Error estimates at x = y = 0 , t = 0.1 for α = 0.5 .
Table 1. Error estimates at x = y = 0 , t = 0.1 for α = 0.5 .
t = 0.1 Exact Solution Approximate Solution Error
n = 2 2.4300431415 2.1136496465 0.3163934950
n = 4 2.4300431415 2.3839562188 0.0460869226
n = 6 2.4300431415 2.4250719371 0.0049712044
n = 8 2.4300431415 2.4296184953 0.0004246462
n = 10 2.4300431415 2.4300131524 0.0000299891
n = 12 2.4300431415 2.4300413376 0.0000018039
n = 14 2.4300431415 2.4300430470 0.0000000945
n = 16 2.4300431415 2.4300431371 0.0000000044
n = 18 2.4300431415 2.4300431413 0.0000000002
n = 20 2.4300431415 2.4300431415 0.0000000000
n = 22 2.4300431415 2.4300431415 0.0000000000
n = 24 2.4300431415 2.4300431415 0.0000000000
n = 26 2.4300431415 2.4300431415 0.0000000000
n = 28 2.4300431415 2.4300431415 0.0000000000
n = 30 2.4300431415 2.4300431415 0.0000000000
Table 2. Error estimates at x = y = 0 , t = 0.5 for α = 0.5 .
Table 2. Error estimates at x = y = 0 , t = 0.5 for α = 0.5 .
t = 0.5 Exact Solution Approximate Solution Error
n = 2 14.4419081954 4.5957691216 9.8461390738
n = 4 14.4419081954 8.7234612837 5.7184469117
n = 6 14.4419081954 11.7589483468 2.6829598486
n = 8 14.4419081954 13.3982742876 1.0436339078
n = 10 14.4419081954 14.0972339650 0.3446742304
n = 12 14.4419081954 14.3433203123 0.0985878831
n = 14 14.4419081954 14.4170855865 0.0248226089
n = 16 14.4419081954 14.4363330458 0.0055777374
n = 18 14.4419081954 14.4407788636 0.0011293310
n = 20 14.4419081954 14.4416999733 0.0002082221
n = 22 14.4419081954 14.4418729796 0.0000352158
n = 24 14.4419081954 14.4419026959 0.0000054995
n = 26 14.4419081954 14.4419073978 0.0000007976
n = 28 14.4419081954 14.4419080875 0.0000001079
n = 30 14.4419081954 14.4419081817 0.0000000144
Table 3. Error estimates at x = y = 0 , t = 1 for α = 0.5 .
Table 3. Error estimates at x = y = 0 , t = 1 for α = 0.5 .
t = 1 Exact Solution Approximate Solution Error
n = 2 108.9409043900 7.2567583342 101.6841460558
n = 4 108.9409043900 21.2747805587 87.6661238313
n = 6 108.9409043900 41.5702827846 67.3706216054
n = 8 108.9409043900 63.2413329475 45.6995714425
n = 10 108.9409043900 81.5563404997 27.3845638903
n = 12 108.9409043900 94.3591742750 14.581730115
n = 14 108.9409043900 101.9877801637 6.9531242263
n = 16 108.9409043900 105.9480101826 2.9928942074
n = 18 108.9409043900 107.7691538039 1.1717505861
n = 20 108.9409043900 108.5207427268 0.4201616632
n = 22 108.9409043900 108.8020586898 0.1388457002
n = 24 108.9409043900 108.8983848776 0.0425195124
n = 26 108.9409043900 108.9287781760 0.0121262140
n = 28 108.9409043900 108.9376695550 0.0032348350
n = 30 108.9409043900 108.9400940351 0.0008103549
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Chang, J.; Zhang, J.; Cai, M. Series Solutions of High-Dimensional Fractional Differential Equations. Mathematics 2021, 9, 2021. https://doi.org/10.3390/math9172021

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Chang, Jing, Jin Zhang, and Ming Cai. 2021. "Series Solutions of High-Dimensional Fractional Differential Equations" Mathematics 9, no. 17: 2021. https://doi.org/10.3390/math9172021

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Chang, J., Zhang, J., & Cai, M. (2021). Series Solutions of High-Dimensional Fractional Differential Equations. Mathematics, 9(17), 2021. https://doi.org/10.3390/math9172021

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