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Article

Existence, Uniqueness and Stability Analysis with the Multiple Exp Function Method for NPDEs

by
Safoura Rezaei Aderyani
1,
Reza Saadati
1,*,
Donal O’Regan
2 and
Fehaid Salem Alshammari
3
1
School of Mathematics, Iran University of Science and Technology, Narmak, Tehran 13114-16846, Iran
2
School of Mathematical and Statistical Sciences, National University of Ireland, Galway, University Road, H91 TK33 Galway, Ireland
3
Department of Mathematics and Statistics, Faculty of Science, Imam Mohammad Ibn Saud Islamic University, Riyadh 11432, Saudi Arabia
*
Author to whom correspondence should be addressed.
Mathematics 2022, 10(21), 4151; https://doi.org/10.3390/math10214151
Submission received: 6 October 2022 / Revised: 21 October 2022 / Accepted: 31 October 2022 / Published: 6 November 2022

Abstract

:
In this study, firstly, through an alternative theorem, we study the existence and uniqueness of solution of some nonlinear PDEs and then investigate the Ulam–Hyers–Rassias stability of solution. Secondly, we apply a relatively novel analytical technique, the multiple exp function method, to obtain the multiple wave solutions of presented nonlinear equations. Finally, we propose the numerical results on tables and discuss the advantages and disadvantages of the method.
MSC:
83C15; 35A20; 35C05; 35C07; 35C08

1. Introduction

In the Fall term of the year 1940, Ulam gave an expansive talk about a number of significant unsolvable problems. Among those was the following issue concerning the stability of homomorphisms:
〈Suppose T 1 is a group and suppose T 2 is a metric group with the metric δ ( . , . ) . Given ϵ > 0 , is there a ρ > 0 s.t. if a mapping λ : T 1 T 2 , satisfies δ ( λ ( x y ) , λ ( x ) λ ( y ) ) < δ , for each x , y T 1 , then there is a homomorphism A : T 1 T 2 , with δ ( λ ( x ) , A ( x ) < ϵ ) , for all x T 1 ?〉
Hyers (1941) has exceptionally answered this question of Ulam for the case that T 1 , T 2 are Banach spaces:
〈Let B : G 1 G 2 , be a mapping between Banach spaces s.t. B ( y + x ) B ( y ) B ( x ) ρ for all y , x G 1 , and some ρ > 0 . Then the limit Θ ( x ) = lim n B ( 2 n x ) 2 n exists for each x G 1 and Θ : G 1 G 2 , is the single mapping s.t. B ( x ) Θ ( x ) ρ , for each x G 1 .
Taking this well-known consequence into consideration, the equation B ( y + x ) = B ( y ) + B ( x ) , is said to have the UH stability on ( T , G ) , in which T and G are given spaces, if for each mapping B : T G satisfying the inequality B ( x + y ) B ( y ) B ( x ) ρ , for some ρ 0 and each y , x T , there is a mapping Θ : T G , s.t. B Θ is bounded on T .
Rassias (1978) tried to reduce the condition for the bound of the norm of B ( y + x ) B ( y ) B ( x ) and showed a excellently generalized result of Hyers. In fact, he investigated the following issue:
〈Suppose B : G 1 G 2 is a mapping among Banach spaces. If B satisfies B ( y + x ) B ( y ) B ( x ) σ ( y p + x p ) , foe each y , x G 1 and some σ > 0 , and 0 p < 1 , then there is a unique mapping Θ : G 1 G 2 , s.t. B ( x ) Θ ( x ) 2 σ 2 2 p x p , for any x G 1 .
The above result was a significant generalization of that of Hyers and stimulated many mathematicians to study the stability issues of several equations. By considering an extensive effect of Rassias on the study of stability problems of diverse equations, the UH stability of such type is called the UHR stability. During the last twenty years, a lot of results for the UHR stability of diverse equations have been solved by many authors.
Through the Cadariu–Radu approach dependent on the Diaz–Margolis theorem, we can prove the uniqueness and existence of solution of nonlinear PDEs and then investigate the stability of it. Finally, by means of an analytical method, we can achieve the exact solution mentioned.
Recently, various analytical approaches have been applied to solve nonlinear differential equations, such as: the sine–cosine technique, the first integral technique and functional variable technique [1], the variational iteration technique [2], the tanh–sech technique [3], the Trial equation technique and the modified Trial technique [4], the Jacobi elliptic function technique [5], the bifurcation technique, the homogenous balance technique [6], the direct algebraic method and the Sine–Gordon expansion technique [7], the homotopy perturbation technique [8], the Hirotas bilinear techniques, the F-expansion technique [9], the extended tanh technique [10] and others.
The above approaches are only concerned about traveling wave solutions of NPDEs. It is obvious that there exist multiple wave solutions to NPDEs, for example, multi-soliton solutions to diverse important models such as the Toda lattice equation, Kdv equation and the Hirota bilinear equations. Thus, there should be an analogous analytical approach for earning multiple wave solutions to NPDEs.
In the present study, we propose an answer by formulating a solution algorithm for calculating the multiple wave solutions to NPDEs.
Consider the following (3+1)-dimensional nonlinear PDE [11]
u t u y u x u z + u x t + u z y = 0
and the following (2+1)-dimensional nonlinear PDE [11]
u t + u x + ν u y + u x y + ϑ u y t + υ u t x = 0 , ν , ϑ , υ R ,
for the following special cases:
u t + u x + 3 u y + u x y + u y t + u t x = 0 ,
and
u t + u x 3 u y + u x y u y t u t x = 0 .
In this study, firstly by means of an fixed point approaches, we investigate the uniqueness, existence and UHR stability of (1) and (3) in Banach spaces. Then, we apply MEFM to construct the new exact solutions for (1), (3) and (4).
The paper is organized as follows: In Section 2, firstly, we propose the fixed point theorem, secondly, through a fixed point theorem, we investigate the UHRS for (1) and (3) in Banach spaces. In Section 3, first we propose the basic idea of MEFM. Then as an application we apply the mentioned method to construct the new exact solutions for (1), (3) and (4). In Section 4, we discuss the proposed approach. Finally, in Section 5, we present the conclusion.

2. Applying Cadariu–Radu Method

Here, using a fixed point theorem, we investigate the UHR stability for (1) and (3) in Banach spaces.
First we state the alternative fixed point method from the literature [12].
Theorem 1. 
Consider the complete [ 0 , ] -valued metric ϵ on χ and Θ on χ with
ϵ ( Θ Ω , Θ ) ϵ ( Ω , ) , in which < 1 is a Lipschitz constant. Suppose χ . If we can find a ρ 0 N s.t. ϵ ( Θ ρ , Θ ρ + 1 ) < , for any ρ ρ 0 , then we have
  • the fixed point Ω * of Θ is the convergence point of the sequence { Θ ρ } ;
  • in the set { Ω χ ϵ ( Θ ρ 0 , Ω ) < } , Ω * is the single fixed point of Θ;
  • ( 1 ) ϵ ( Ω , Ω * ) ϵ ( Ω , Θ Ω ) for every Ω χ .

2.1. Stability Result for (1)

Consider (1). Assume a variation given by
μ = S x + R y + A z ω t , u : = U ( μ ) ,
where S , R and A are constants. We now rewrite Equation (1) in the following NODE
( ω + R + S + A ) U + ( R A ω S ) U = 0 .
Integrating Equation (6) twice leads to
( ω + R + S + A ) 0 μ U ( s ) d s + ( R A ω S ) U + = 0 ,
where ∁ is a constant. We rewrite (7), as follows:
N 0 μ U ( s ) d s + M U + = 0 ,
in which N : = ( ω + R + S + A ) and M : = R A ω S .
Theorem 2. 
Assume U C [ 0 , T ] , ( T > 0 ) , satisfies the following integral inequality:
| N 0 μ U ( s ) d s + M U ( μ ) + | ϕ ( μ )
and also, assume
0 μ ϕ ( s ) d s ϱ ϕ ( μ ) f o r s o m e ϱ > 0 ,
where ϕ : [ 0 , T ] ( 0 , ) is a continuous function. Suppose 0 < | N M | ϱ < 1 . Then can find a U C [ 0 , T ] , such that
U = N M 0 μ U ( s ) d s ,
and
| U ( μ ) U ( μ ) | 1 1 | N M | ϱ ϕ ( μ ) .
Proof. 
Let χ : = C [ 0 , T ] , and define a mapping ϵ : χ [ 0 , ] , given by
ϵ ( U ( μ ) , U ^ ( μ ) ) = inf Ξ 0 : | U ( μ ) U ^ ( μ ) | Ξ ϕ ( μ ) , μ [ 0 , T ] .
It is straight forward to prove that ( χ , ε ) is a complete generalized metric space.
Now, define Θ : χ χ as
Θ U = N M 0 μ U ( s ) d s .
We prove that the self-mapping Θ is contractive on χ . Assume U , U ^ χ , Ξ 0 , and ϵ ( U ( μ ) , U ^ ( μ ) ) Ξ . Now for any μ [ 0 , T ] , we have
| Θ U ( μ ) Θ U ^ ( μ ) | | N M | 0 μ | U ( s ) U ^ ( s ) | d s | N M | 0 μ Ξ ϕ ( s ) d s | N M | ϱ Ξ ϕ ( μ ) .
Therefore we obtain
ϵ ( Θ U ( μ ) , Θ U ^ ( μ ) ) | N M | ϱ ϵ ( U ( μ ) , U ^ ( μ ) ) .
and we have the contractive property of Θ , because 0 < | N M | ϱ < 1 .
On the other hand, according to (9), we have
ϵ ( Θ U ( μ ) , U ( μ ) ) < 1 .
Thus, the assumptions of Theorem 1 are satisfied, and we have
| U ( μ ) U ( μ ) | 1 1 | N M | ϱ ϕ ( μ ) .
where U = N M 0 μ U ( s ) d s is a unique map in κ χ : ϵ ( Θ U , κ ) < .

2.2. Stability Result for (1)

In this subsection, using a fixed point theorem, we investigate the UHRS for (3), in Banach spaces.
Consider (3). Assume a complete variation given by
μ = S x + R y ω t , u : = U ( μ ) ,
where S , R and ω are constants. We now rewrite Equation (3) in the following NODE
( ω + S + 3 R ) U + ( S R ω S ω R ) U = 0 .
Integrating Equation (17) twice leads:
( ω + S + 3 R ) 0 μ U ( s ) d s + ( S R ω S ω R ) U + = 0 ,
where ∁ is a constant. We rewrite (18), as follows:
N 0 μ U ( s ) d s + M U + = 0 ,
in which N : = ω + S + 3 R and M : = S R ω S ω R .
Theorem 3. 
Assume U C [ 0 , T ] , ( T > 0 ) , satisfies the following integral inequality:
| N 0 μ U ( s ) d s + M U ( μ ) + | ϕ ( μ )
and also, assume
0 μ ϕ ( s ) d s ϱ ϕ ( μ ) , ϱ > 0 ,
where ϕ : [ 0 , T ] ( 0 , ) is a continuous function. Let 0 < | N M | ϱ < 1 . Then there exists a unique function U C [ 0 , T ] , which satisfies
U = N M 0 μ U ( s ) d s ,
and
| U ( μ ) U ( μ ) | 1 1 | N M | ϱ ϕ ( μ ) .
Proof. 
Let χ : = C [ 0 , T ] , and define a mapping ϵ : χ [ 0 , ] , given by
ϵ ( U ( μ ) , U ^ ( μ ) ) = inf Ξ 0 : | U ( μ ) U ^ ( μ ) | Ξ ϕ ( μ ) , μ [ 0 , T ] .
It is straight forward to prove that ( χ , ε ) is a complete generalized metric space [12].
Now, define Θ : χ χ as
Θ U = N M 0 μ U ( s ) d s .
We now show that Θ is contractive on χ . Assume U , U ^ χ , Ξ 0 , and ϵ ( U ( μ ) , U ^ ( μ ) ) Ξ . Therefore for any μ [ 0 , T ] , we have
| Θ U ( μ ) Θ U ^ ( μ ) | < | N M | 0 μ | U ( s ) U ^ ( s ) | d s | N M | 0 μ Ξ ϕ ( s ) d s | N M | Ξ ϱ ϕ ( μ ) .
Therefore we obtain
ϵ ( Θ U ( μ ) , Θ U ^ ( μ ) ) | N M | ϱ ϵ ( U ( μ ) , U ^ ( μ ) ) .
which concludes the contractive property of Θ , because 0 < | N M | ϱ < 1 .
On the other hand, according to (20), we obtain
ϵ ( Θ U ( μ ) , U ( μ ) ) 1 .
Thus the assumptions of Theorem 1 are satisfied, and we have
| U ( μ ) U ( μ ) | 1 1 | N M | ϱ ϕ ( μ ) .
where U = N M 0 μ U ( s ) d s is a unique map in κ χ : ϵ ( Θ U , κ ) < .

3. Applying MEFM

In this section, first we propose the basic idea of MEFM [13]. Then, as an application, we apply the mentioned method to construct the new exact solutions for some nonlinear PDEs.

3.1. The Algorithm of MEFM

Here, we formulate the multi-exp-function method by considering
N ( t , x , u x , u t , u x x , u t t , u x x x , ) = 0 , u = u ( x , t ) .
• Step 1: Let
μ i = c i exp ( μ i ) , μ i = S i x ω i t , μ i = μ i ( x , t ) , i [ 1 , n ] ,
where c i , S i and ω i are arbitrary constants, angular wave numbers and wave frequencies, respectively. Note that
μ i , x = S i μ i , μ i , t = ω i μ i , i [ 1 , n ] .
• Step 2: Now, let
u ( x , t ) : = K ( μ 1 , μ 2 , , μ n ) H ( μ 1 , μ 2 , , μ n ) , K : = r , s = 1 n i , j = 0 M P r s , i j μ r i μ s j , H : = r , s = 1 n i , j = 0 N Q r s , i j μ r i μ s j ,
where Q r s , i j and P r s , i j are constants to be determined from Equation (27).
Here, we obtain
N ˜ ( x , t , μ 1 , μ 2 , , μ n ) = 0 .
• Step 3: By solving a system of algebraic equations on variables k i , w i , P r s , i j and Q r s , i j , the multiple wave solutions u reads
u ( x , t ) = K ( c 1 exp ( S 1 x ω 1 t ) , , c n exp ( S n x ω n t ) ) H ( c 1 exp ( S 1 x ω 1 t ) , , c n exp ( S n x ω n t ) ) .

3.2. Application

We apply MEFM to construct the analytical solutions for (3+1)-dimensional nonlinear PDE (1) and spacial cases of (2+1)-dimensional nonlinear PDE (2).

3.2.1. Example 1

Here, we apply MEFM to construct the analytical solutions for (3+1)-dimensional nonlinear PDE presented in (1).
• One wave solutions for (1):
First introduce a variable μ 1 = μ 1 ( x , y , z , t ) as follows
μ 1 = ϖ 1 exp ( S 1 x + R 1 y + A 1 z ω 1 t ) ,
where ϖ 1 , S 1 , R 1 , A 1 and ω 1 are constants. Note μ 1 has the following linear partial differential relations
μ 1 , x = S 1 μ 1 , μ 1 , y = R 1 μ 1 , μ 1 , z = A 1 μ 1 , μ 1 , t = ω 1 μ 1 .
Then, we consider a pair of polynomials of degree one
K ( μ 1 ) = P 0 + P 1 μ 1 ,
H ( μ 1 ) = Q 0 + Q 1 μ 1 ,
where P 0 , P 1 , Q 0 , and Q 1 are constants to be determined from (1). Therefore, we have
u ( x , t ) = K ( μ 1 ) H ( μ 1 ) = P 0 + P 1 μ 1 Q 0 + Q 1 μ 1 .
Now, by substituting (36) into (1) and solving the system of algebraic equations, we obtain:
P 1 = Q 1 P 0 Q 0 , ω 1 : arbitrary ,
and
P 1 = arbitrary , ω 1 : R 1 , A 1 = S 1 .
Thus, the one wave solutions can be proposed by
u 1 , 1 ( x , t ) = P 0 + Q 1 P 0 Q 0 exp ( S 1 x + R 1 y + A 1 z ω 1 t ) Q 0 + Q 1 exp ( S 1 x + R 1 y + A 1 z ω 1 t )
and
u 1 , 2 ( x , t ) = P 0 + P 1 exp ( S 1 x + R 1 y S 1 z + R 1 t ) Q 0 + Q 1 exp ( S 1 x + R 1 y S 1 z + R 1 t ) .
Equation (39) is displayed in Figure 1 for S 1 = Q 1 = 0.70 , R 1 = P 0 = 0.90 , Q 0 = 0.40 , ω 1 = 0.5 , (1), (4) and (7) are three dimensional with y = z = 2 . Now (2), (5) and (8) exploits the z axis orientation. (3), (6) and (9) are contour plots. Further, Equation (40) is displayed in Figure 2 for S 1 = 3.70 , R 1 = 2.90 , Q 0 = 0.40 , Q 1 = 0.70 , P 0 = 0.90 , P 1 = 3 , (1), (4) and (7) are three dimensional with y = z = 2 . Now (2), (5) and (8) exploits the z axis orientation. (3), (6) and (9) are contour plots.
• Two wave solutions for (1):
Here, introduce a variable μ i = μ i ( x , y , z , t ) , i = 1 , 2 , as follows
μ i = ϖ i exp ( S i x + R i y + A 1 z ω i t ) , i = 1 , 2
where ϖ i , S i , R i , A i and ω i are constants. Note μ i has the following linear partial differential relations
μ i , x = S i μ i , μ i , y = R i , μ i , z = A i μ 1 , μ i , t = ω i μ i , i = 1 , 2 .
Then, we consider a pair of polynomials of degree two
K ( μ 1 , μ 2 ) = 2 ( S 1 μ 1 + S 2 μ 2 + P 12 ( S 1 + S 2 ) μ 1 μ 2 ) ,
H ( μ 1 , μ 2 ) = 1 + μ 1 + μ 2 + P 12 μ 1 μ 2 ,
where P 12 is a constant to be determined from (1). Therefore, we have
u ( x , t ) = 2 ( S 1 μ 1 + S 2 μ 2 + P 12 ( S 1 + S 2 ) μ 1 μ 2 ) 1 + μ 1 + μ 2 + P 12 μ 1 μ 2 .
Now, by substituting (45) into (1) and solving the system of algebraic equations, we obtain:
P 12 = 1 , R 2 = S 2 , A 1 = S 1 , ω 1 = R 1 , ω 2 = A 2 ,
and
P 12 = 1 , R 1 = S 1 , A 2 = S 2 , ω 1 = A 1 , ω 2 = R 2 .
By setting the above values in (45), the two wave solutions can be proposed by
u 2 , 1 ( x , t ) = [ 2 ( S 1 exp ( S 1 x + R 1 y S 1 z + R 1 t ) + S 2 exp ( S 2 x S 2 y + A 2 z + A 2 t ) + ( S 1 + S 2 ) exp ( S 1 x + R 1 y S 1 z + R 1 t ) exp ( S 2 x S 2 y + A 2 z + A 2 t ) ) ] / [ 1 + exp ( S 1 x + R 1 y S 1 z + R 1 t ) + exp ( S 2 x S 2 y + A 2 z + A 2 t ) + exp ( S 1 x + R 1 y S 1 z + R 1 t ) exp ( S 2 x S 2 y + A 2 z + A 2 t ) ] ,
and
u 2 , 2 ( x , t ) = [ 2 ( S 1 exp ( S 1 x S 1 y + A 1 z + A 1 t ) + S 2 exp ( S 2 x + R 2 y S 2 z + R 2 t ) + ( S 1 + S 2 ) exp ( S 1 x S 1 y + A 1 z + A 1 t ) exp ( S 2 x + R 2 y S 2 z + R 2 t ) ) ] / [ 1 + exp ( S 1 x S 1 y + A 1 z + A 1 t ) + exp ( S 2 x + R 2 y S 2 z + R 2 t ) + exp ( S 1 x S 1 y + A 1 z + A 1 t ) exp ( S 2 x + R 2 y S 2 z + R 2 t ) ] .
Equation (46) is displayed in Figure 3 for R 1 = 0.80 , A 2 = 0.40 , S 1 = 0.90 , S 2 = 7 , (1), (4) and (7) are three dimensional with y = 3 , z = 2 . Now (2), (5) and (8) exploits the z axis orientation. (3), (6) and (9) are contour plots. Further, Equation (47) is displayed in Figure 4 for R 2 = 3.90 , A 1 = 5.60 , S 1 = 5.90 , S 2 = 7.70 , (1), (4) and (7) are three dimensional with y = 3 , z = 2 . Now (2), (5) and (8) exploits the z axis orientation. (3), (6) and (9) are contour plots.
• Three wave solutions for (1):
Here, introduce a variable μ i = μ i ( x , y , z , t ) , i = 1 , 2 , 3 , as follows
μ i = ϖ i exp ( S i x + R i y + A i z ω i t ) , i = 1 , 2 , 3
where ϖ i , S i , R i , A I and ω i are constants. Note μ i has the following linear partial differential relations
μ i , x = S i μ i , μ i , y = R i μ 1 , μ i , z = A i μ 1 , μ i , t = ω i μ i , i = 1 , 2 , 3 .
Then, we consider a pair of polynomials of degree three
K ( μ 1 , μ 2 , μ 3 ) = 2 ( S 1 μ 1 + S 2 μ 2 + S 3 μ 3 + P 12 ( S 1 + S 2 ) μ 1 μ 2 + P 13 ( S 1 + S 3 ) μ 1 μ 3 + P 23 ( S 2 + S 3 ) μ 2 μ 3 + P 12 P 13 P 23 ( S 1 + S 2 + S 3 ) μ 1 μ 2 μ 3 ) ,
and
H ( μ 1 , μ 2 , μ 3 ) = 1 + μ 1 + μ 2 + μ 3 + P 12 μ 1 μ 2 + P 13 μ 1 μ 3 + P 23 μ 2 μ 3 + P 12 P 13 P 23 μ 1 μ 2 μ 3 ,
where P 12 , P 13 , and P 23 are constants to be determined from (1). Therefore, we have
u ( x , t ) = [ 2 ( S 1 μ 1 + S 2 μ 2 + S 3 μ 3 + P 12 ( S 1 + S 2 ) μ 1 μ 2 + P 13 ( S 1 + S 3 ) μ 1 μ 3 + P 23 ( S 2 + S 3 ) μ 2 μ 3 + P 12 P 13 P 23 ( S 1 + S 2 + S 3 ) μ 1 μ 2 μ 3 ) ] / [ 1 + μ 1 + μ 2 + μ 3 + P 12 μ 1 μ 2 + P 13 μ 1 μ 3 + P 23 μ 2 μ 3 + P 12 P 13 P 23 μ 1 μ 2 μ 3 ] .
Now, by substituting (50) into (1) and solving the system of algebraic equations, we obtain:
P 12 = 1 , P 13 = 0 , P 23 = 1 , A 1 = S 1 , A 3 = S 3 , R 2 = S 2 , ω 1 = R 1 , ω 2 = A 2 , ω 3 = R 3 ,
P 12 = 0 , P 13 = 1 , P 23 = 1 , A 1 = S 1 , A 2 = S 2 , R 3 = S 3 , ω 1 = R 1 , ω 2 = R 2 , ω 3 = A 3 ,
P 12 = 0 , P 13 = 1 , P 23 = 1 , R 1 = S 1 , R 2 = S 2 , A 3 = S 3 , ω 1 = A 1 , ω 2 = A 2 , ω 3 = R 3 ,
P 12 = arbitrary , P 13 = 0 , P 23 = 0 , R 1 = S 1 , R 2 = S 2 , R 3 = S 3 , ω 1 = A 1 , ω 2 = A 2 , ω 3 = A 3 .
Thus, the three wave solutions can be proposed by
u 3 , 1 ( x , t ) = [ 2 ( S 1 exp ( S 1 x + R 1 y S 1 z + R 1 t ) + S 2 exp ( S 2 x S 2 y + A 2 z + A 2 t ) + S 3 exp ( S 3 x + R 3 y S 3 z + R 3 t ) + ( S 1 + S 2 ) exp ( S 1 x + R 1 y A 1 z + R 1 t ) exp ( S 2 x S 2 y + A 2 z + A 2 t ) + ( S 2 + S 3 ) exp ( S 2 x S 2 y + A 2 z + A 2 t ) exp ( S 3 x + R 3 y S 3 z + R 3 t ) ) ] / [ 1 + exp ( S 1 x + R 1 y A 1 z + R 1 t ) + exp ( S 2 x S 2 y + A 2 z + A 2 t ) + exp ( S 3 x + R 3 y S 3 z + R 3 t ) + exp ( S 1 x + R 1 y S 1 z + R 1 t ) exp ( S 2 x S 2 y + A 2 z + A 2 t ) + exp ( S 2 x S 2 y + A 2 z + A 2 t ) exp ( S 3 x + R 3 y S 3 z + R 3 t ) ] ,
and also, by inserting (51), (52), and (53) in (50), we obtain u 3 , 2 ( x , t ) , u 3 , 3 ( x , t ) and u 3 , 4 ( x , t ) , respectively.
Equation (54) is displayed in Figure 5 for R 1 = 0.50 , R 3 = 0.70 , S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.30 , A 1 = 0.80 , and equation u 3 , 2 is displayed in Figure 6 for R 1 = 0.50 , R 2 = 0.70 , S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.30 , A 3 = 0.80 , in different domains. Equation u 3 , 3 is displayed in Figure 7 for R 3 = 2.70 , A 1 = 2.70 , A 2 = 2.80 , S 1 = 2.20 , S 2 = 2.70 , S 3 = 2.30 , (1), (4) and (7) are three dimensional with y = z = 2 . Now (2), (5) and (8) exploit the z axis orientation. (3), (6) and (9) are contour plots. Further, equation u 3 , 4 is displayed in Figure 8 for P 12 = 3.50 , A 1 = 3 , A 2 = 5 , A 3 = 7 , S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.30 , (1), (4) and (7) are three dimensional with y = z = 2 . Now (2), (5) and (8) exploit the z axis orientation. (3), (6) and (9) are contour plots.

3.2.2. Example 2

Here, we apply MEFM to construct the new exact solutions for the (2+1)-dimensional Equation (3).
• One wave solutions for (3):
Firstly, introduce a variable μ 1 = μ 1 ( x , y , t ) as follows
μ 1 = ϖ 1 exp ( S 1 x + R 1 y ω 1 t ) ,
where ϖ 1 , S 1 , R 1 and ω 1 are constants. Obviously, μ 1 has the following linear partial differential relations
μ 1 , x = S 1 μ 1 , μ 1 , y = R 1 μ 1 , μ 1 , t = ω 1 μ 1 .
Therefore, we consider a pair of polynomials of degree one
K ( μ 1 ) = P 0 + P 1 μ 1 ,
H ( μ 1 ) = Q 0 + Q 1 μ 1 ,
where P 0 , P 1 , Q 0 , and Q 1 are constants to be determined from (1). Therefore, we have
u ( x , t ) = K ( μ 1 ) H ( μ 1 ) = P 0 + P 1 μ 1 Q 0 + Q 1 μ 1 .
Now, by substituting (59) into (3) and solving the system of algebraic equations, we obtain:
P 1 : arbitrary , ω 1 = ( 1.500 + 0.866 i ) R 1 , S 1 = R 1 ( 1.500 + 0.866 i ) R 1 1.500 + 0.866 i ) R 1 + ( 1.500 + 0.866 i ) R 1 1 .
Thus, the one wave solutions can be proposed by
u 1 ( x , t ) = P 0 + P 1 exp ( R 1 ( 1.500 + 0.866 i ) R 1 1.500 + 0.866 i ) R 1 + ( 1.500 + 0.866 i ) R 1 1 x + R 1 y ( 1.500 + 0.866 i ) R 1 ) t ) / Q 0 + Q 1 exp ( R 1 ( 1.500 + 0.866 i ) R 1 1.500 + 0.866 i ) R 1 + ( 1.500 + 0.866 i ) R 1 1 x + R 1 y ( 1.500 + 0.866 i ) R 1 ) t )
The real and imaginary part of Equation (61) are displayed in Figure 9 and Figure 10 for P 1 = 0.20 , P 0 = 0.90 , Q 0 = 0.70 , Q 1 = 0.50 , R 1 = 0.90 . (1) is three dimensional with y = z = 2 . (2), (4) and (5) exploit z axis, x axis, y axis orientation, respectively, and (3) is contour plot.
• Two wave solutions for (3):
Here, introduce a variable μ i = μ i ( x , y , t ) , i = 1 , 2 , as follows
μ i = ϖ i exp ( S i x + R i y ω i t ) , i = 1 , 2
where ϖ i , S i , R i , and ω i are constants. Obviously, μ i has the following linear partial differential relations
μ i , x = S i μ i , μ i , y = R i , μ i , t = ω i μ i , i = 1 , 2 .
Then, we consider a pair of polynomials of degree two
K ( μ 1 , μ 2 ) = 2 ( S 1 μ 1 + S 2 μ 2 + P 12 ( S 1 + S 2 ) μ 1 μ 2 ) ,
H ( μ 1 , μ 2 ) = 1 + μ 1 + μ 2 + P 12 μ 1 μ 2 ,
where P 12 is a constant to be determined from (1). Therefore, we have
u ( x , t ) = 2 ( S 1 μ 1 + S 2 μ 2 + P 12 ( S 1 + S 2 ) μ 1 μ 2 ) 1 + μ 1 + μ 2 + P 12 μ 1 μ 2 .
Now, by substituting (66) into (3) and solving the system of algebraic equations, we obtain:
P 12 = 1 , S 1 = ( 3 2 + 1 2 3 i ) R 1 , S 2 = ( 3 2 + 1 2 3 i ) R 2 , ω 1 = R 1 ( ( 3 2 + 1 2 3 i ) R 1 + 3 2 + 1 2 3 i ) ( 3 2 + 1 2 3 i ) R 1 + R 1 + 1 , ω 2 = R 2 ( ( 3 2 + 1 2 3 i ) R 2 + 3 2 + 1 2 3 i ) ( 3 2 + 1 2 3 i ) R 2 + R 2 + 1 .
By setting above values in (66), the two wave solutions can be proposed by u 2 ( x , t ) .
The real and imaginary part of equation u 2 ( x , t ) are displayed in Figure 11 and Figure 12 for R 1 = 0.90 , R 2 = 0.80 . (1) is three dimensional with y = z = 2 . (2), (4) and (5) exploit z axis, x axis, y axis orientation, respectively, and (3) is contour plot.
• Three wave solutions for (3):
Here, introduce a variable μ i = μ i ( x , y , t ) , i = 1 , 2 , 3 , as follows
μ i = ϖ i exp ( S i x + R i y ω i t ) , i = 1 , 2 , 3
where ϖ i , S i , R i , and ω i are constants. Obviously, μ i has the following linear partial differential relations
μ i , x = S i μ i , μ i , y = R i μ 1 , μ i , t = ω i μ i , i = 1 , 2 , 3 .
Then, we consider a pair of polynomials of degree three
K ( μ 1 , μ 2 , μ 3 ) = 2 ( S 1 μ 1 + S 2 μ 2 + S 3 μ 3 + P 12 ( S 1 + S 2 ) μ 1 μ 2 + P 13 ( S 1 + S 3 ) μ 1 μ 3 + P 23 ( S 2 + S 3 ) μ 2 μ 3 + P 12 P 13 P 23 ( S 1 + S 2 + S 3 ) μ 1 μ 2 μ 3 ) ,
and
H ( μ 1 , μ 2 , μ 3 ) = 1 + μ 1 + μ 2 + μ 3 + P 12 μ 1 μ 2 + P 13 μ 1 μ 3 + P 23 μ 2 μ 3 + P 12 P 13 P 23 μ 1 μ 2 μ 3 ,
where P 12 , P 13 , and P 23 are constants to be determined from (1). Therefore, we have
u ( x , t ) = [ 2 ( S 1 μ 1 + S 2 μ 2 + S 3 μ 3 + P 12 ( S 1 + S 2 ) μ 1 μ 2 + P 13 ( S 1 + S 3 ) μ 1 μ 3 + P 23 ( S 2 + S 3 ) μ 2 μ 3 + P 12 P 13 P 23 ( S 1 + S 2 + S 3 ) μ 1 μ 2 μ 3 ) ] / 1 + μ 1 + μ 2 + μ 3 + P 12 μ 1 μ 2 + P 13 μ 1 μ 3 + P 23 μ 2 μ 3 + P 12 P 13 P 23 μ 1 μ 2 μ 3 .
Now, by substituting (69) into (3) and solving the system of algebraic equations, we obtain:
P 12 = 1 , P 13 = 1 , P 23 = 1 , R 1 = S 1 ( ( 0.500 + 0.866 i ) S 1 1.500 + 0.866 i ) ) S 1 + ( 0.500 + 0.866 i ) S 1 3 , R 2 = S 2 ( ( 0.500 + 0.866 i ) S 2 1.500 + 0.866 i ) ) S 2 + ( 0.500 + 0.866 i ) S 2 3 , R 3 = S 3 ( ( 0.500 + 0.866 i ) S 3 1.500 + 0.866 i ) ) S 3 + ( 0.500 + 0.866 i ) S 3 3 , ω 1 = ( 0.500 + 0.866 i ) S 1 , ω 2 = ( 0.500 + 0.866 i ) S 2 , ω 3 = ( 0.500 + 0.866 i ) S 3 ,
and
P 12 = 0 , P 13 : arbitrary , P 23 = 0 , R 1 = ( 0.500 + 0.288 i ) S 1 , R 2 = S 2 ( ( 0.500 + 0.866 i ) S 2 1.500 + 0.866 i ) ) S 2 + ( 0.500 + 0.866 i ) S 2 3 , R 3 = ( 0.500 + 0.288 i ) S 3 , ω 1 = S 1 ( ( 1.500 + 0.866 i S 1 ) ( 0.500 + 0.866 i ) S 1 + 1.500 + 0.866 i + S 1 , ω 2 = ( 0.500 + 0.866 i ) S 2 , ω 3 = S 3 ( ( 1.500 + 0.866 i S 3 ) ( 0.500 + 0.866 i ) S 3 + 1.500 + 0.866 i + S 3 .
By inserting above values in (69), we obtain u 3 , 1 ( x , t ) , u 3 , 2 ( x , t ) , respectively.
The real and imaginary part of equation u 3 , 1 ( x , t ) and u 3 , 2 ( x , t ) are displayed in Figure 13, Figure 14, Figure 15 and Figure 16 for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . (1) is three dimensional with y = z = 2 . (2), (4) and (5) exploit z axis, x axis, y axis orientation, respectively, and (3) is contour plot, in different domains.

3.2.3. Example 3

Here, we apply MEFM to construct the new exact solutions for the (2+1)-dimensional equation (4).
• One wave solutions for (4):
P 1 : arbitrary , R 1 = S 1 ( 3.302 S 1 2.302 ) 4.302 S 1 3 , ω 1 = 3.302 S 1 .
According to the above values, we obtain u 1 ( x , t ) . , respectively.
Equation u 1 ( x , t ) is displayed in Figure 17 for S 1 = 0.90 , P 0 = 0.90 , P 1 = 0.20 , Q 0 = 0.70 , Q 1 = 0.50 . (1) is three dimensional with y = z = 2 . (2), (4) and (5) exploit z axis, x axis, y axis orientation, respectively, and (3) is contour plot, in different domains.
• Two wave solutions for (4):
P 12 = 1 , R 1 = S 1 ( ( 3 2 + 1 2 13 ) S 1 1 2 1 2 13 ) S 1 + ( 3 2 + 1 2 13 ) S 1 3 , R 2 = ( 1 6 + 1 6 13 ) S 2 , ω 1 = ( 3 2 + 1 2 13 ) S 1 , ω 2 = S 2 ( ( 1 6 + 1 6 13 ) S 2 + 3 2 1 2 13 ) S 2 + ( 1 6 + 1 6 13 ) S 2 1 .
According to the above values, we obtain u 2 ( x , t ) . respectively.
Equation u 2 ( x , t ) is displayed in Figure 18 for S 1 = 0.90 , S 2 = 0.70 . (1) is three dimensional with y = z = 2 . (2), (4) and (5) exploit z axis, x axis, y axis orientation, respectively, and (3) is contour plot, in different domains.
• Three wave solutions for (4):
P 12 = 1 , P 13 = 1 , P 23 = 1 , R 1 = S 1 ( 3.302 S 1 2.302 ) 4.302 S 1 3 , R 2 = S 2 ( 3.302 S 2 2.302 ) 4.302 S 2 3 , R 3 = 0.432 S 3 , ω 1 = 3.302 S 1 , ω 2 = 3.302 S 2 , ω 3 = S 3 ( 0.434 S 3 0.302 ) 1.434 S 3 1 ,
and
P 12 = 1 , P 13 = 0 , P 23 = 1 , R 1 = S 1 ( 3.302 S 1 2.302 ) 4.302 S 1 3 , R 2 = S 2 ( 3.302 S 2 2.302 ) 4.302 S 2 3 , R 3 = 0.767 S 3 , ω 1 = 3.302 S 1 , ω 2 = 3.302 S 2 , ω 3 = S 3 ( 4.302 S 3 ) 0.302 S 3 1.302 .
According to the above values, we obtain u 3 , 1 ( x , t ) and u 3 , 2 ( x , t ) . , respectively.
Equation u 3 , 1 ( x , t ) is displayed in Figure 19 for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . (1) is three dimensional with y = z = 2 . (2), (4) and (5) exploit z axis, x axis, y axis orientation, respectively, and (3) is contour plot, in different domains. Equation u 3 , 2 ( x , t ) is displayed in Figure 20 for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . (1) is three dimensional with y = z = 2 . (2), (4) and (5) exploit z axis, x axis, y axis orientation, respectively, and (3) is contour plot, in different domains.

4. Results and Discussion

In Figures Table 1, Table 2 and Table 3, for specific values, we propose the numerical solutions of (1). As you can see, in each stage, the obtained results are nearer to each other than the previous stages. We can conclude that the presented MEFM results in the unique solution of nonlinear PDEs in higher stages.
Indeed, in Section 2, we studied the existence and uniqueness the solution of (1), and then we investigated the stability of that. Next, by an analytical method, MEFM, we obtained the solutions of the mentioned nonlinear PDE. Now, in this section, according to Table 1, Table 2 and Table 3, we can prove that in higher stages of MEFM, the obtained solutions overlap each other. In other words, we can observe the uniqueness of solution of (1).
Although this method can construct the multiple wave solutions to nonlinear equations, calculating each wave solution separately takes a lot of time; this can be one of the shortcomings of this method.

5. Conclusions

In this study, firstly, through an alternative theorem, we studied the existence and uniqueness of solution of some nonlinear PDEs which contains high nonlinear terms and then investigated the UHR stability of solution. Secondly, we applied a relatively novel analytical technique, the MEFM, to obtain the multiple wave solutions of presented nonlinear equations. Finally, we presented the numerical results in tables and discuss the advantages and disadvantages of the presented method.

Author Contributions

S.R.A., writing—original draft preparation. R.S., methodology and project administration. D.O., methodology, writing—original draft preparation and project administration. F.S.A., writing—original draft preparation and project administration. All authors conceived of the study, participated in its design and coordination, drafted the manuscript, participated in the sequence alignment and read and approved the final manuscript. All authors have read and agreed to the published version of the manuscript.

Funding

The authors extend their appreciation to the Deanship of Scientific Research at Imam Mohammad Ibn Saud Islamic University (IMSIU) for funding and supporting this work through Research Partnership Program no RP-21-09-08.

Data Availability Statement

Not applicable.

Conflicts of Interest

The authors declare that they have no competing interests.

References

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Figure 1. The 3D and 2D with the diagram of Equation (39), in three different domains.
Figure 1. The 3D and 2D with the diagram of Equation (39), in three different domains.
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Figure 2. The 3D and 2D with the diagram of Equation (40), in three different domains.
Figure 2. The 3D and 2D with the diagram of Equation (40), in three different domains.
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Figure 3. The 3D and 2D with the diagram of u 2 , 1 , in three different domains.
Figure 3. The 3D and 2D with the diagram of u 2 , 1 , in three different domains.
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Figure 4. The 3D and 2D with the diagram of equation u 2 , 2 , in three different domains.
Figure 4. The 3D and 2D with the diagram of equation u 2 , 2 , in three different domains.
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Figure 5. The 3D and 2D with the diagram of u 3 , 1 , in four different domains, for R 1 = 0.50 , R 3 = 0.70 , S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.30 , and A 1 = 0.80 . ( 2 ) , ( 8 ) , ( 14 ) , ( 20 ) display the x axis orientation, ( 3 ) , ( 9 ) , ( 15 ) , ( 21 ) display the y axis orientation, ( 4 ) , ( 10 ) , ( 16 ) , ( 22 ) , ( 5 ) , ( 11 ) , ( 17 ) , ( 23 ) display the z axis orientation, and ( 6 ) , ( 12 ) , ( 18 ) , ( 24 ) are contour plots.
Figure 5. The 3D and 2D with the diagram of u 3 , 1 , in four different domains, for R 1 = 0.50 , R 3 = 0.70 , S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.30 , and A 1 = 0.80 . ( 2 ) , ( 8 ) , ( 14 ) , ( 20 ) display the x axis orientation, ( 3 ) , ( 9 ) , ( 15 ) , ( 21 ) display the y axis orientation, ( 4 ) , ( 10 ) , ( 16 ) , ( 22 ) , ( 5 ) , ( 11 ) , ( 17 ) , ( 23 ) display the z axis orientation, and ( 6 ) , ( 12 ) , ( 18 ) , ( 24 ) are contour plots.
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Figure 6. The 3D and 2D with the diagram of u 3 , 2 , in four different domains, in four different domains, for R 1 = 0.50 , R 2 = 0.70 , S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.30 , and A 3 = 0.80 . ( 2 ) , ( 8 ) , ( 14 ) , ( 20 ) diasplay the x axis orientation, ( 3 ) , ( 9 ) , ( 15 ) , ( 21 ) display the y axis orientation, ( 4 ) , ( 10 ) , ( 16 ) , ( 22 ) , ( 5 ) , ( 11 ) , ( 17 ) , ( 23 ) display the z axis orientation, and ( 6 ) , ( 12 ) , ( 18 ) , ( 24 ) are contour plots.
Figure 6. The 3D and 2D with the diagram of u 3 , 2 , in four different domains, in four different domains, for R 1 = 0.50 , R 2 = 0.70 , S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.30 , and A 3 = 0.80 . ( 2 ) , ( 8 ) , ( 14 ) , ( 20 ) diasplay the x axis orientation, ( 3 ) , ( 9 ) , ( 15 ) , ( 21 ) display the y axis orientation, ( 4 ) , ( 10 ) , ( 16 ) , ( 22 ) , ( 5 ) , ( 11 ) , ( 17 ) , ( 23 ) display the z axis orientation, and ( 6 ) , ( 12 ) , ( 18 ) , ( 24 ) are contour plots.
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Figure 7. The 3D and 2D with the diagram of u 3 , 3 , in three different domains, for R 3 = 2.70 , A 1 = 2.70 , A 2 = 2.80 , S 1 = 2.20 , S 2 = 2.70 , and S 3 = 2.30 . ( 2 ) , ( 5 ) and ( 8 ) display the z axis orientation and ( 3 ) , ( 6 ) and ( 9 ) are contour plots.
Figure 7. The 3D and 2D with the diagram of u 3 , 3 , in three different domains, for R 3 = 2.70 , A 1 = 2.70 , A 2 = 2.80 , S 1 = 2.20 , S 2 = 2.70 , and S 3 = 2.30 . ( 2 ) , ( 5 ) and ( 8 ) display the z axis orientation and ( 3 ) , ( 6 ) and ( 9 ) are contour plots.
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Figure 8. The 3D and 2D with the diagram of u 3 , 4 , in three different domains, for P 12 = 3.50 , A 1 = 3 , A 2 = 5 , A 3 = 7 , S 1 = 0.20 , S 2 = 0.70 , and S 3 = 0.30 . ( 2 ) , ( 5 ) and ( 8 ) display the z axis orientation and ( 3 ) , ( 6 ) and ( 9 ) are contour plots.
Figure 8. The 3D and 2D with the diagram of u 3 , 4 , in three different domains, for P 12 = 3.50 , A 1 = 3 , A 2 = 5 , A 3 = 7 , S 1 = 0.20 , S 2 = 0.70 , and S 3 = 0.30 . ( 2 ) , ( 5 ) and ( 8 ) display the z axis orientation and ( 3 ) , ( 6 ) and ( 9 ) are contour plots.
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Figure 9. The 3D and 2D with the diagram of real part of Equation (61).
Figure 9. The 3D and 2D with the diagram of real part of Equation (61).
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Figure 10. The 3D and 2D with the diagram of imaginary part of Equation (61).
Figure 10. The 3D and 2D with the diagram of imaginary part of Equation (61).
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Figure 11. The 3D and 2D with the diagram of the real part of equation u 2 ( x , t ) .
Figure 11. The 3D and 2D with the diagram of the real part of equation u 2 ( x , t ) .
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Figure 12. The 3D and 2D with the diagram of the imaginary part of equation u 2 ( x , t ) .
Figure 12. The 3D and 2D with the diagram of the imaginary part of equation u 2 ( x , t ) .
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Figure 13. The 3D and 2D with the diagrams of the real part of equation u 3 , 1 , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) , and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis and y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
Figure 13. The 3D and 2D with the diagrams of the real part of equation u 3 , 1 , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) , and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis and y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
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Figure 14. The 3D and 2D with the diagram of the imaginary part of equation u 3 , 1 , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) , and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis and y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
Figure 14. The 3D and 2D with the diagram of the imaginary part of equation u 3 , 1 , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) , and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis and y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
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Figure 15. The 3D and 2D with the diagram of the real part of equation u 3 , 2 , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) , and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis and y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
Figure 15. The 3D and 2D with the diagram of the real part of equation u 3 , 2 , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) , and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis and y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
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Figure 16. The 3D and 2D with the diagram of the imaginary part of equation u 3 , 2 , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) , and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis and y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
Figure 16. The 3D and 2D with the diagram of the imaginary part of equation u 3 , 2 , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) , and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis and y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
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Figure 17. The 3D and 2D with the diagram of equation u 1 ( x , t ) .
Figure 17. The 3D and 2D with the diagram of equation u 1 ( x , t ) .
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Figure 18. The 3D and 2D with the diagram of equation u 2 ( x , t ) .
Figure 18. The 3D and 2D with the diagram of equation u 2 ( x , t ) .
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Figure 19. The 3D and 2D with the diagram of equation u 3 , 1 ( x , t ) , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , and S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis, y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
Figure 19. The 3D and 2D with the diagram of equation u 3 , 1 ( x , t ) , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , and S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis, y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
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Figure 20. The 3D and 2D with the diagram of equation u 3 , 2 ( x , t ) , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , and S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis, y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
Figure 20. The 3D and 2D with the diagram of equation u 3 , 2 ( x , t ) , in three different domains, for S 1 = 0.20 , S 2 = 0.70 , and S 3 = 0.50 . ( 2 ) , ( 7 ) , ( 12 ) , ( 4 ) , ( 9 ) , ( 14 ) and ( 5 ) , ( 10 ) , ( 15 ) display z axis, x axis, y axis orientations, respectively, and ( 3 ) , ( 8 ) , ( 13 ) are contour plots, in different domains.
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Table 1. Numerical solutions for one wave solutions of (1).
Table 1. Numerical solutions for one wave solutions of (1).
x, y, z, t u 11 ( x , y , z , t ) u 12 ( x , y , z , t )
0.0010.8889770.555496
0.010.8897780.554962
0.10.8978640.549552
1.0010.9845860.491037
Table 2. Numerical solutions for two wave solutions of (1).
Table 2. Numerical solutions for two wave solutions of (1).
x, y, z, t u 21 ( x , y , z , t ) u 22 ( x , y , z , t )
0.0010.4251640.425174
0.010.4266480.426748
0.10.4413060.442298
1.0010.5624200.570334
Table 3. Numerical solutions for three wave solutions of (1).
Table 3. Numerical solutions for three wave solutions of (1).
x, y, z, t u 31 ( x , y , z , t ) u 32 ( x , y , z , t ) u 33 ( x , y , z , t ) u 34 ( x , y , z , t )
0.0011.0338661.0338661.0338521.033919
0.011.0386661.0386661.0385211.039200
0.11.0866271.0866271.0850621.092440
1.0011.5189801.5189801.5016741.576044
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Aderyani, S.R.; Saadati, R.; O’Regan, D.; Alshammari, F.S. Existence, Uniqueness and Stability Analysis with the Multiple Exp Function Method for NPDEs. Mathematics 2022, 10, 4151. https://doi.org/10.3390/math10214151

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Aderyani SR, Saadati R, O’Regan D, Alshammari FS. Existence, Uniqueness and Stability Analysis with the Multiple Exp Function Method for NPDEs. Mathematics. 2022; 10(21):4151. https://doi.org/10.3390/math10214151

Chicago/Turabian Style

Aderyani, Safoura Rezaei, Reza Saadati, Donal O’Regan, and Fehaid Salem Alshammari. 2022. "Existence, Uniqueness and Stability Analysis with the Multiple Exp Function Method for NPDEs" Mathematics 10, no. 21: 4151. https://doi.org/10.3390/math10214151

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