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Article

Hermite Fitted Block Integrator for Solving Second-Order Anisotropic Elliptic Type PDEs

by
Emmanuel Oluseye Adeyefa
1,
Ezekiel Olaoluwa Omole
1,
Ali Shokri
2 and
Shao-Wen Yao
3,*
1
Department of Mathematics, Faculty of Science, Federal University Oye-Ekiti, P.M.B. 373, Oye-Ekiti 370112, Ekiti State, Nigeria
2
Faculty of Mathematical Sciences, University of Maragheh, Maragheh 83111-55181, Iran
3
School of Mathematics and Information Science, Henan Polytechnic University, Jiaozuo 454000, China
*
Author to whom correspondence should be addressed.
Fractal Fract. 2022, 6(9), 497; https://doi.org/10.3390/fractalfract6090497
Submission received: 19 July 2022 / Revised: 27 August 2022 / Accepted: 29 August 2022 / Published: 5 September 2022
(This article belongs to the Special Issue Initial and Boundary Value Problems for Differential Equations)

Abstract

:
A Hermite fitted block integrator (HFBI) for numerically solving second-order anisotropic elliptic partial differential equations (PDEs) was developed, analyzed, and implemented in this study. The method was derived through collocation and interpolation techniques using the Hermite polynomial as the basis function. The Hermite polynomial was interpolated at the first two successive points, while the collocation occurred at all the suitably chosen points. The major scheme and its complementary scheme were united together to form the HFBI. The analysis of the HFBI showed that it had a convergence order of eight with small error constants, was zero-stable, absolutely-stable, and satisfied the condition for convergence. In order to confirm the usefulness, accuracy, and efficiency of the HFBI, the method of lines approach was applied to discretize the second-order anisotropic elliptic partial differential equation PDE into a system of second-order ODEs and consequently used the derived HFBI to obtain the approximate solutions for the PDEs. The computed solution generated by using the HFBI was compared to the exact solutions of the problems and other existing methods in the literature. The proposed method compared favorably with other existing methods, which were validated through test problems whose solutions are presented in tabular form, and the comparisons are illustrated in the curves.

1. Introduction

An anisotropic equation is an example of a second-order elliptic partial differential equation with broad applications in theoretical physics, applied mathematics, engineering, and other fields of study [1]. In [2], the regularization Cauchy problem for matrix factorizations of the Helmholtz equation in a multidimensional bounded domain was discussed. Similarly, Ref. [3] examined the Cauchy problem for degenerate parabolic convolution equations. The asymptotic reduction in the solution space dimension and applications in dynamical systems were proposed in [4]. The solution of fractional differential equations is explored through Geraghty type hybrid contractions in [5], the solution of differential equations through the New integral operator was studied by [6,7] presented a variable compact multipoint upscaling scheme for anisotropic diffusion problems in three dimensions. In this paper, we consider a second-order anisotropic elliptic partial differential equation of the form
2 u = g ( x , y ) ,
Over the years, the numerical solution of Equation (1) has become of great importance to scholars and scientists due to its practical applications in applied mathematics and engineering. The second-order elliptic partial differential equations of the form (1) are usually modeled into linear or nonlinear equations [8]. These types of problems are widely used to model real-life problems, for instance, the transportation of oxygen in a tissue plate at a constant rate of oxygen consumption [9], certain non-smooth oscillators with large nonlinearities with periodic solutions [10], elastohydrodynamic lubrication [11], electromagnetic scattering theory, the flow of air pollutants, velocity potential, micro- and nano-electronic devices in physics [12], the boussinesq-love equation’s inverse boundary value problem with the nonlocal integral condition [13], the modeling of coupled dynamic thermoelastic issues for isotropic solids using mathematics and computers [14], and the estimation of the stability for the difference and delay parabolic equations [15]. As a result, most of these problems or models do not have an exact solution. This results in the fact that it is usually difficult to solve some of these equations or problems analytically. Thus, there is the need to employ an appropriate numerical method to solve them numerically.
Many numerical models have been proposed for the numerical approximation of Equation (1), while some have been developed for the theoretical solutions of (1). Many real-life situations or experimental equations cannot be solved analytically. Therefore, numerical techniques are employed for the numerical approximation of such problems. A countless number of numerical algorithms have been constructed for solving (1). Such techniques include the Adomian Decomposition methods [16,17], the Haar wavelet method [18], trigonometrically fitted block techniques [19,20], the variational homotopy perturbation method [21], the direct solver approach [22], block algorithms [23,24,25,26,27], the finite difference method [28]; transform techniques [29], the Legendre-homotopy method [30], and the cubic spline method [31,32].
The search for numerical methods with better accuracy led us to this present work. In this article, the Hermite fitted block integrator HFBI for solving a class of (1) which is assumed to satisfy the existence and uniqueness of solution within the interval of domain of integration, is proposed. The HFBI possessed a convergent order of eight. We are motivated to propose HFBI as a result of the outstanding features of the block integrator, including that it is more efficient, has good stability properties, and possesses high convergence. This enormous success of block integrators has greatly removed the burden of developing predictors separately, the complexity in computing, the slow convergence, instability, and computational time.
The remaining part of the article is designed as follows: Section 1 defines the introduction, area of applications, and the related literature review. Section 2 details the mathematical formulation of the HFBI. The properties of the HFBI such as order and error, consistency, zero-stability, and the region of absolute stability are analyzed in Section 3. Furthermore, the computational strategy is outlined in Section 4. The numerical examples, comparison of the numerical results of HFBI with the results of existing methods are presented, along with the comparison in curves in Section 5. Finally, the conclusions are discussed based on the numerical results to verify the accuracy, reliability, and efficiency of HFBI in Section 6.

2. Methodology

In this section, we discuss in details the mathematical formulation of HFBI for the numerical solution of (1) where
2 u = ϵ 2 u x 2 ( x , y ) + 2 u y 2 ( x , y ) ,
for all ( x , y ) Ω R 2 , where Ω = ( x , y ) : ( x , y ) [ a , b ] × [ c , d ] with boundary Ω . Related to (1) are the initial conditions
u ( x , a ) = v 1 ( x ) , u y ( x , b ) = v 2 ( x ) , x [ a , b ] ,
or the Dirichlet boundary conditions
u ( x , c ) = v 3 ( x ) , u ( x , d ) = v 4 ( x ) , x [ c , d ] .
With respect to (1), the solution u ( x , y ) is termed the dependent variable, g ( x , y ) is called the forcing function, and x and y are the spatial variables. ϵ < 1 or ϵ > 1 for all ( x , y ) Ω . In addition, Ω is a rectangular domain with appropriate boundary and initial conditions. The variables functions are assumed to be a continuous functions that satisfy the necessary conditions for the existence and uniqueness. The theorems that provide the conditions are discussed extensively in [33,34].

Mathematical Formulation of the HFBI

Here, the numerical solution of (1) is sought on the interval x n to x n + 7 by a Hermite polynomial of the form
u x = i = 0 k + 2 c i H i ( x ) , i = 0 , 1
where ( H i ) are probabilists Hermite polynomials generated by the recursive relation and step-number (k = 7).
H n + 1 x = x H n ( x ) H n ( x )
The first six probabilists Hermite polynomias [35] are
H 0 ( x ) = 1 H 1 ( x ) = x H 2 ( x ) = x 2 1 H 3 ( x ) = x 3 3 x H 4 ( x ) = x 4 6 x 2 + 3 H 5 ( x ) = x 5 10 x 3 + 15 x
u x = i = 2 k + 2 c i H i x , i = 2 , 3 , , k + 2
where k + 2 = c + r 1 , r is the interpolation points, and c is the collocation point. Equation (4) is referred to as the interpolation equation, whereas (5) is the collocation equation. Imposing the following conditions on (4) and (5) gives
u m + j , n = i = 0 k + 2 c i H i x , i , = 0 , 1
f m + j , n = i = 2 k + 2 c i H i x , i , = 2 1 k + 2
The Equations (6) and (7) are joined together to form a system of c + r 1 equations, which is represented by
L C = W
where
L = H 0 ( x n ) H 1 ( x n ) H 2 ( x n ) H 3 ( x n ) H k + 2 ( x n ) H 0 ( x n + 1 ) H 1 ( x n + 1 ) H 2 ( x n + 1 ) H 0 ( x n + 1 ) H k + 2 ( x n + 1 ) H 0 ( x n ) H 1 ( x n ) H 2 ( x n ) H 3 ( x n ) H k + 2 ( x n ) H 0 ( x n + 1 ) H 1 ( x n + 1 ) H 2 ( x n + 1 ) H 3 ( x n + 1 ) H k + 2 ( x n + 1 ) H 0 ( x n + k ) H 1 ( x n + k ) H 2 ( x n + k ) H 3 ( x n + k ) H k + 2 ( x n + k )
C = c 0 c 1 c 2 c 3 c k + 2 W = u m , n u m + 1 , n f m , n f m + 1 , n f m + k , n
Matrix Equation (8) is solved for the unknown values of c i , i = 0 ( 1 ) 9 using Maple 18.0. The values (see Appendix A) are then placed into (4) to obtain the continuous implicit equation together with its derivative in the form
u m + j , n t = γ 0 ( t ) u m , n + γ 1 ( t ) u m + 1 , n + h 2 j = 0 k + 2 ψ j t f m + j , n , j = 0 1 k + 2
where
u m , n = u x n , u m + 1 , n = u x n + 1 , f m + j , n = f x m + j , n , u m + j , n , u m + j , n , t = x x n + 6 h
γ 0 ( t ) = ( t 5 ) γ 1 ( t ) = ( t + 6 ) ψ 0 ( t ) = h 2 s 1 , 814 , 400 5 t 7 + 35 t 6 + 65 t 5 85 t 4 133 t 3 607 t 2 + 3467 t 19 , 927 ψ 1 ( t ) = h 2 s 1 , 814 , 400 35 t 7 + 290 t 6 + 500 t 5 340 t 4 3196 t 3 + 7556 t 2 47 , 716 t + 298 , 196 ψ 2 ( t ) = h 2 s 604 , 800 35 t 7 + 335 t 6 + 665 t 5 565 t 4 2521 t 3 679 t 2 + 7499 t 62 , 119 ψ 3 ( t ) = h 2 s 362 , 880 35 t 7 + 380 t 6 + 950 t 5 766 t 4 2938 t 3 982 t 2 1858 t + 49 , 898 ψ 4 ( t ) = h 2 s 362 , 880 35 t 7 + 425 t 6 + 1355 t 5 439 t 4 5455 t 3 + 1355 t 2 2455 t 13 , 645 ψ 5 ( t ) = h 2 s 604 , 800 35 t 7 + 470 t 6 + 1880 t 5 + 920 t 4 8056 t 3 7024 t 2 + 16 , 544 t + 28 , 736 ψ 6 ( t ) = h 2 s 1 , 814 , 400 35 t 7 + 515 t 6 + 2525 t 5 + 3815 t 4 5701 t 3 22 , 339 t 2 21 , 721 t + 1901 ψ 7 ( t ) = h 2 s 1 , 814 , 400 5 t 7 + 80 t 6 + 470 t 5 + 1250 t 4 + 1382 t 3 + 218 t 2 658 t + 698 s = ( t + 6 ) ( t + 5 )
A U M = B M R 0 + B M M R 1 + h 2 [ D M R 2 + E M R 3 ]
A = 120 , 960 60 , 480 0 0 0 0 0 181 , 440 0 60 , 480 0 0 0 0 120 , 960 0 0 30 , 240 0 0 0 151 , 200 0 0 0 30 , 240 0 0 362 , 880 0 0 0 0 60 , 480 0 60 , 480 0 0 0 0 0 8640 1 , 814 , 400 0 0 0 0 0 0 , U M = u m + 1 , n u m + 2 , n u m + 3 , n u m + 4 , n u m + 5 , n u m + 6 , n u m + 7 , n
B M = 0 0 0 0 0 0 60 , 480 0 0 0 0 0 0 120 , 960 0 0 0 0 0 0 90 , 720 0 0 0 0 0 0 120 , 960 0 0 0 0 0 0 302 , 400 0 0 0 0 0 0 51 , 840 0 0 0 0 0 0 1 , 814 , 400 , R 0 = u m 1 , n u m 2 , n u m 3 , n u m 4 , n u m 5 , n u m 6 , n u m , n
B M M = 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 , 814 , 400 , R 1 = u m 1 , n u m 2 , n u m 3 , n u m 4 , n u m 5 , n u m 6 , n u m , n
D M = 0 0 0 0 0 0 4125 0 0 0 0 0 0 8060 0 0 0 0 0 0 6013 0 0 0 0 0 0 7996 0 0 0 0 0 0 19 , 927 0 0 0 0 0 0 3436 0 0 0 0 0 0 416 , 173 , R 2 = f m 1 , n f m 2 , n f m 3 , n f m 4 , n f m 5 , n f m 6 , n f m , n
E M = 55 , 324 6297 14 , 598 11 , 477 5568 1551 190 116 , 293 37 , 410 33 , 539 21 , 656 10 , 299 2854 349 88 , 412 43 , 815 50 , 374 12 , 661 7296 2063 254 118 , 693 68 , 706 87 , 235 9640 12 , 699 2918 349 298 , 196 186 , 357 249 , 490 68 , 225 86 , 208 1901 698 51 , 065 34 , 410 44 , 719 18 , 824 20 , 103 8194 689 950 , 684 1 , 025 , 097 1 , 059 , 430 768 , 805 362 , 112 99 , 359 12 , 062 , R 3 = f m + 1 , n f m + 2 , n f m + 3 , n f m + 4 , n f m + 5 , n f m + 6 , n f m + 7 , n
We proceed by multiplying Equation (11) by the reciprocal of matrix A, which gives the following HFBI of the form
A 1 A U M = A 1 B M R 0 + A 1 B M M R 1 + h 2 [ A 1 D M R 2 + A 1 E M R 3 ]
A 1 A = I = 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 , U M = u m + 1 , n u m + 2 , n u m + 3 , n u m + 4 , n u m + 5 , n u m + 6 , n u m + 7 , n
A 1 B M = 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 , R 0 = u m 1 , n u m 2 , n u m 3 , n u m 4 , n u m 5 , n u m 6 , n u m , n
A 1 B M M = 0 0 0 0 0 0 1 0 0 0 0 0 0 2 0 0 0 0 0 0 3 0 0 0 0 0 0 4 0 0 0 0 0 0 5 0 0 0 0 0 0 6 0 0 0 0 0 0 7 , R 1 = u m 1 , n u m 2 , n u m 3 , n u m 4 , n u m 5 , n u m 6 , n u m , n
A 1 D M = 0 0 0 0 0 0 416 , 173 1 , 814 , 400 0 0 0 0 0 0 14 , 939 28 , 350 0 0 0 0 0 0 18 , 399 22 , 400 0 0 0 0 0 0 15 , 824 14 , 175 0 0 0 0 0 0 102 , 425 72 , 576 0 0 0 0 0 0 597 350 0 0 0 0 0 0 519 , 253 259 , 200 , R 2 = f m 1 , n f m 2 , n f m 3 , n f m 4 , n f m 5 , n f m 6 , n f m , n
A 1 E M = 33 , 953 64 , 800 341 , 699 604 , 800 105 , 943 181 , 440 153 , 761 362 , 880 943 4725 99 , 359 1 , 814 , 400 6031 907 , 200 27821 14175 833 675 799 567 5881 5670 2321 4725 1916 14 , 175 233 14 , 175 39 , 141 11 , 200 24 , 111 22 , 400 369 160 7299 4480 8613 11 , 200 4737 22 , 400 9 350 71 , 152 14 , 175 3832 4725 11 , 344 2835 856 405 4912 4725 4072 14 , 175 496 14 , 175 59 , 375 9072 13 , 375 24 , 192 21 , 0625 36 , 288 130 , 625 72 , 576 1225 864 26 , 875 72 , 576 1625 36 , 288 1413 175 54 175 267 35 99 70 459 175 9 25 9 175 1 , 241 , 317 129 , 600 2401 86 , 400 12 , 005 1296 40 , 817 51 , 840 160 , 867 43 , 200 146 , 461 259 , 200 8183 64 , 800 , R 3 = f m + 1 , n f m + 2 , n f m + 3 , n f m + 4 , n f m + 5 , n f m + 6 , n f m + 7 , n
The matrix Equation (12) can be written explicitly as follows
u m + 1 , n = u m , n + u m , n h + 416 , 173 1 , 814 , 400 h 2 f m , n + 33 , 953 64 , 800 h 2 f m + 1 , n 341 , 699 604 , 800 h 2 f m + 2 , n + 105 , 943 181 , 440 h 2 f m + 3 , n 153 , 761 362 , 880 h 2 f m + 4 , n + 943 4725 h 2 f m + 5 , n 99 , 359 1 , 814 , 400 h 2 f m + 6 , n + 6031 907 , 200 h 2 f m + 7 , n ,
u m + 2 , n = u m , n + 2 h u m , n + 14 , 939 28 , 350 h 2 f m , n + 27 , 821 14 , 175 h 2 f m + 1 , n 833 675 h 2 f m + 2 , n + 799 567 h 2 f m + 3 , n 5881 5670 h 2 f m + 4 , n + 2321 4725 h 2 f m + 5 , n 1916 14 , 175 h 2 f m + 6 , n + 233 14 , 175 h 2 f m + 7 , n ,
u m + 3 , n = u m , n + 3 h u m , n + 18 , 399 22 , 400 h 2 f m , n + 39 , 141 11 , 200 h 2 f m + 1 , n 24 , 111 22 , 400 h 2 f m + 2 , n + 369 160 h 2 f m + 3 , n 7299 4480 h 2 f m + 4 , n + 8613 11 , 200 h 2 f m + 5 , n 4737 22 , 400 h 2 f m + 6 , n + 9 350 h 2 f m + 7 , n ,
u m + 4 , n = u m , n + 4 h u m , n + 15 , 824 14 , 175 h 2 f m , n + 71 , 152 14 , 175 h 2 f m + 1 , n 3832 4725 h 2 f m + 2 , n + 11 , 344 2835 h 2 f m + 3 , n 856 405 h 2 f m + 4 , n + 4912 4725 h 2 f m + 5 , n 4072 14 , 175 h 2 f m + 6 , n + 496 14 , 175 h 2 f m + 7 , n ,
u m + 5 , n = u m , n + 5 h u m , n + 102 , 425 72 , 576 h 2 f m , n + 59 , 375 9072 h 2 f m + 1 , n 13 , 375 24 , 192 h 2 f m + 2 , n + 210 , 625 36 , 288 h 2 f m + 3 , n 130 , 625 72 , 576 h 2 f m + 4 , n + 1225 864 h 2 f m + 5 , n 26 , 875 72 , 576 h 2 f m + 6 , n + 1625 36 , 288 h 2 f m + 7 , n ,
u m + 6 , n = u m , n + 6 h u m , n + 597 350 h 2 f m , n + 1413 175 h 2 f m + 1 , n 54 175 h 2 f m + 2 , n + 267 35 h 2 f m + 3 , n 99 70 h 2 f m + 4 , n + 459 175 h 2 f m + 5 , n 9 25 h 2 f m + 6 , n + 9 175 h 2 f m + 7 , n ,
u m + 7 , n = u m , n + 7 h u m , n + 519 , 253 259 , 200 h 2 f m , n + 1 , 241 , 317 129 , 600 h 2 f m + 1 , n + 2401 86 , 400 h 2 f m + 2 , n + 12 , 005 1296 h 2 f m + 3 , n 40 , 817 51 , 840 h 2 f m + 4 , n + 160 , 867 43 , 200 h 2 f m + 5 , n + 146 , 461 259 , 200 h 2 f m + 6 , n + 8183 64 , 800 h 2 f m + 7 , n
with the corresponding first derivatives
u m + 1 , n = u m , n + 5257 17 , 280 h f m , n + 139 , 849 120 , 960 h f m + 1 , n 4511 4480 h f m + 2 , n + 123 , 133 120 , 960 h f m + 3 , n 88 , 547 120 , 960 h f m + 4 , n + 1537 4480 h f m + 5 , n 11 , 351 120 , 960 h f m + 6 , n + 275 24 , 192 h f m + 7 , n ,
u m + 2 , n = u m , n + 41 140 h f m , n + 1466 945 h f m + 1 , n 71 420 h f m + 2 , n + 68 105 h f m + 3 , n 1927 3780 h f m + 4 , n + 26 105 h f m + 5 , n 29 420 h f m + 6 , n + 8 945 h f m + 7 , n ,
u m + 3 , n = u m , n + 265 896 h f m , n + 1359 896 h f m + 1 , n + 1377 4480 h f m + 2 , n + 5927 4480 h f m + 3 , n 3033 4480 h f m + 4 , n + 1377 4480 h f m + 5 , n 373 4480 h f m + 6 , n + 9 896 h f m + 7 , n ,
u m + 4 , n = u m , n + 278 945 h f m , n + 1448 945 h f m + 1 , n + 8 35 h f m + 2 , n + 1784 945 h f m + 3 , n 106 945 h f m + 4 , n + 8 35 h f m + 5 , n 64 945 h f m + 6 , n + 8 945 h f m + 7 , n ,
u m + 5 , n = u m , n + 265 896 h f m , n + 36 , 725 24 , 192 h f m + 1 , n + 775 2688 h f m + 2 , n + 4625 2688 h f m + 3 , n + 13 , 625 24 , 192 h f m + 4 , n + 1895 2688 h f m + 5 , n 275 2688 h f m + 6 , n + 275 24 , 192 h f m + 7 , n ,
u m + 6 , n = u m , n + 41 140 h f m , n + 54 35 h f m + 1 , n + 27 140 h f m + 2 , n + 68 35 h f m + 3 , n + 27 140 h f m + 4 , n + 54 35 h f m + 5 , n + 41 140 h f m + 6 , n + 0 h f m + 7 , n ,
u m + 7 , n = u m , n + 5257 17 , 280 h f m , n + 25 , 039 17 , 280 h f m + 1 , n + 343 640 h f m + 2 , n + 20 , 923 17 , 280 h f m + 3 , n + 20 , 923 17 , 280 h f m + 4 , n + 343 640 h f m + 5 , n + 25 , 039 17 , 280 h f m + 6 , n + 5257 17 , 280 h f m + 7 , n
Remark 1.
The integrators (13)–(26) formed the HFBI needed for the implementation of the resulting second-order system of ODEs emerging from the discretization of the PDEs of the form (1).

3. Basic Properties of the HFBI

3.1. Order and Error Terms of the HFBI

The basic properties of the HFBI such as the local truncation error (LTE), order and error terms, zero-stability, and stability nature are investigated in the spirit of Lambert [33] and Henrici [34].
The local truncation error (LTE) of HFBI is expressed by
L [ u ( x ) ; h ] = u ( x + j h , t ) j = 0 ρ [ γ j u ( x + j h , t ) ] h 2 j = 0 μ [ ψ j u ( x + j h , t ) ] ,
where u x is continuously differentiable, ρ = 1 , μ = 7 and j = 0 ( 1 ) 7 .
Expanding u ( x + j h , t ) and u ( x + j h , t ) in (27) in the Taylor series about x n , and collecting the like terms in h and y yields,
L [ u ( x ) ; h ] = F 0 u x + F 1 h u x + F 2 h 2 u x + . . . + F q h q u ( q ) x
where F q , q = 1 , 2 , are given as follows:
F 0 = j = 0 k γ j F 1 = j = 0 k j γ j j = 0 k ψ j F 2 = 1 2 ! j = 0 k j 2 γ j j = 0 k j ψ j F 3 = 1 3 ! j = 0 k j 3 γ j j = 0 k j 2 ψ j . . . F q = 1 q ! j = 0 k j q γ j q j = 0 k j q 1 ψ j
Thus, the method is of order p if F 0 = F 1 = = F p = 0 , F p + 2 0 .
Hence, F p + 2 is the error constant, and F i s are the error constants.
The local truncation error (LTE) is given by
( LTE ) = F p + 2 h p + 2 u ( p + 2 ) x n + O h ( p + 3 )
Remark 2.
The method (13)–(26) is of order p if F 0 = F 1 = = F p + 1 = 0 , and F p + 2 0 .

3.2. Zero-Stability of the HFBI

The matrix difference Equation (12) is given by
A ( 0 ) U w = A ( 1 ) U w 1 + h 2 B ( 0 ) F w + B ( 1 ) F w 1
It should be noted that the matrices A ( 0 ) , A ( 1 ) , B ( 0 ) and B ( 1 ) are square matrices whose entries are the coefficients of (13)–(19) above and are defined as follows:
A ( 0 ) = 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 1 , A ( 1 ) = 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1 0 0 0 0 0 0 1
B ( 0 ) = 33 , 953 64 , 800 341 , 699 604 , 800 105 , 943 181 , 440 153 , 761 362 , 880 943 4725 99 , 359 1 , 814 , 400 6031 907 , 200 27 , 821 14 , 175 833 675 799 567 5881 5670 2321 4725 1916 14 , 175 233 14 , 175 39 , 141 11 , 200 24 , 111 22 , 400 369 160 7299 4480 8613 11 , 200 4737 22 , 400 9 350 71 , 152 14 , 175 3832 4725 11 , 344 2835 856 405 4912 4725 4072 14 , 175 496 14 , 175 59 , 375 9072 13 , 375 24 , 192 210 , 625 36 , 288 130 , 625 72 , 576 1225 864 26 , 875 72 , 576 1625 36 , 288 1413 175 54 175 267 35 99 70 459 175 9 25 9 175 1 , 241 , 317 129 , 600 2401 86 , 400 12 , 005 1296 40 , 817 51 , 840 160 , 867 43 , 200 146 , 461 259 , 200 8183 64 , 800
B ( 1 ) = 0 0 0 0 0 0 416 , 173 1 , 814 , 400 0 0 0 0 0 0 14 , 939 28 , 350 0 0 0 0 0 0 18 , 399 22 , 400 0 0 0 0 0 0 15 , 824 14 , 175 0 0 0 0 0 0 102 , 425 72 , 576 0 0 0 0 0 0 597 350 0 0 0 0 0 0 519 , 253 259 , 200
U w = u m + 1 , n , u m + 2 , n , u m + 3 , n , u m + 4 , n , u m + 5 , n , u m + 6 , n , u m + 7 , n T
U w 1 = u m 6 , n , u m 5 , n , u m 4 , n , u m 3 , n , u m 2 , n , u m 1 , n , u m , n T
F w = f m + 1 , n , f m + 2 , n , f m + 3 , n , f m + 4 , n , f m + 5 , n , f m + 6 , n , f m + 7 , n T
F w 1 = f m 6 , n , f m 5 , n , f m 4 , n , f m 3 , n , f m 2 , n , f m 1 , n , f m , n T
The zero-stability is concerned with the stability of the different systems in the limit as h tends to 0 in (12). Consequently, as h tends 0, the method (31) tends to the different system.
A ( 0 ) U w A ( 1 ) U w 1 = 0
The first characteristics of (32) is given by
ρ R = det R A ( 0 ) A ( 1 ) = 0
det R A ( 0 ) A ( 1 ) = 0
According to Fatunla [36], the new method, HFBI is said to be zero-stable if (34) holds, then
ρ R = R 6 R 1 = R 1 = R 2 = R 3 = R 4 = 0 = R 5 = 0 , R 6 = 0 , R = 1
Hence, the new method, HFBI, is zero-stable [34].

3.3. Consistency

As stated by Lambert in [33], the methods (13)–(19) are consistent if they have order p greater than or equal to 1. Hence, the method is consistent, since (13)–(19) have order p = 8 > 1 (see the details in Table 1). hence it is consistent.

3.4. Convergence

The method (13)–(19) is in the form of general linear multistep method. It is very important that the method be consistent and zero-stable. The method is convergent since it satisfied the conditions for consistency and zero-stability as established by [34].

3.5. Region of Absolute Stability of HFBI

The region of absolute stability of the HFBI was investigated via the procedure discussed in [33,37]. The stability matrix can be expressed as
M ( z ) = z S ( I z W ) 1 U + V
together with the stability function
p ( n , z ) = d e t ( M ( z ) + n I )
For the stability properties, the integrator (13)–(19) was formulated as a general linear method of the form:
Y Y i + 1 = W U S V h 2 f ( u ) Y i 1
where n represents the roots of the first characteristic polynomial of the method (12), and
Y i 1 = u m + 1 , n u m , n , Y i + 1 = u m + 1 , n u m + 7 , n ,
W = 0 0 0 0 0 0 0 0 416 , 173 1 , 814 , 400 33 , 953 64 , 800 341 , 699 604 , 800 105 , 943 181 , 440 153 , 761 362 , 880 943 4725 99 , 359 1 , 814 , 400 6031 907 , 200 14 , 939 28 , 350 27 , 821 14 , 175 833 675 799 567 5881 5670 2321 4725 1916 14 , 175 233 14 , 175 18 , 399 22 , 400 39 , 141 11 , 200 24 , 111 22 , 400 369 160 7299 4480 8613 11 , 200 4737 22 , 400 9 350 15 , 824 14 , 175 71 , 152 14 , 175 3832 4725 11 , 344 2835 856 405 4912 4725 4072 14 , 175 496 14 , 175 102 , 425 72 , 576 59 , 375 9072 13 , 375 24 , 192 210 , 625 36 , 288 130 , 625 72 , 576 1225 864 26 , 875 72 , 576 1625 36 , 288 597 350 1413 175 54 175 267 35 99 70 459 175 9 25 9 175 519 , 253 259 , 200 1 , 241 , 317 129 , 600 2401 86 , 400 12 , 005 1296 40 , 817 51 , 840 160 , 867 43 , 200 146 , 461 259 , 200 8183 64 , 800
S = 416 , 173 1 , 814 , 400 33 , 953 64 , 800 341 , 699 604 , 800 105 , 943 181 , 440 153 , 761 362 , 880 943 4725 99 , 359 1 , 814 , 400 6031 907 , 200 519 , 253 259 , 200 1 , 241 , 317 129 , 600 2401 86 , 400 12 , 005 1296 40 , 817 51 , 840 160 , 867 43 , 200 146 , 461 259 , 200 8183 64 , 800
V = 0 1 0 1 , U = 0 1 0 1 0 1 0 1 0 1 0 1 0 1 , Y = u m + 1 , n u m + 2 , n u m + 3 , n u m + 4 , n u m + 5 , n u m + 6 , n u m + 7 , n , I = 1 0 0 1 , f ( u ) = f m + 1 , n f m + 2 , n f m + 3 , n f m + 4 , n f m + 5 , n f m + 6 , n f m + 7 , n
Now, putting the values of the variables W, S, U, V, M and I into Equations (36) and (37), we obtained the stability function. The stability function and its derivatives were then plotted in the MATLAB (R2012a) environment. It should be noted that M is 8 by 8 identity matrix. The region of absolute stability (RAS) of the HFBI is displayed in the Figure 1 below,
Definition 1.
The method of the class (13)–(26) is said to be p-stable if its interval of periodicity lies within ( 0 , ) . The interval of periodicity of the HFBI lies within (0, 0.091) as ascertained in Figure 1, which shows that the method is p-stable (see [33]).
The shaded portion inside the curve indicates the unstable region, while the external region outside the curve represents the stable region [26].

4. Computational Approach

The method of lines is a very powerful tool for transforming PDEs into ODEs [38]. In this section, the procedures for the discretization of second-order anisotropic elliptic partial differential equations into systems of second-order ordinary differential equations via the MOL approach are illustrated. We applied MOL to transform (1) to a system of second-order ODEs with the initial conditions in the form below. In particular, the y variable was discretized with the mesh spacings,
Δ x = b a M , x i = a + i Δ x , i = 0 , 1 , , M .
For each i = 0 , , M and for a fixed y in [ a , b ] , we define:
Δ t = d c N , t i = c + i Δ t , i = 0 , 1 , , N .
For each i = 0 , , N and for a fixed t in [ c , d ] ,
The following vectors are defined
u i ( y ) u ( x i , y ) , u ( y ) = [ u 0 ( y ) , u 1 ( y ) , u 2 ( y ) , , u M ( y ) ] T ,
f i ( y ) f ( x i , y ) , f ( y ) = [ f 0 ( y ) , f 1 ( y ) , f 2 ( y ) , , f M ( y ) ] T ,
In addition, the partial derivatives 2 u y 2 appearing in (1) are replaced by the second-order central difference approximations
2 u y 2 = u ( x , y m + 1 ) 2 u ( x , y m ) + u ( x , y m 1 , y ) ( y ) 2 , m = 1 , , M 1 .
Hence, problem (1) has the following semi-discretized form given below;
d 2 u m , n d x 2 = u ( x , y m + 1 ) 2 u ( x , y m ) + u ( x , y m 1 , y ) ( y ) 2 + g m , n ]
which could also be written in the form
u = f ( x , u , u ) = T u + g ,
subject to the initial conditions
u ( a ) = u 0 , u ( a ) = u 0 ,
or any of the boundary conditions
u ( a ) = u 0 , u ( a ) = u m , n ,
u ( b ) = u 0 , u ( c ) = u m , n .
T is the tridiagonal matrix given as
T = 2 ( Δ y ) 2 1 ( Δ y ) 2 0 0 0 0 1 ( Δ y ) 2 2 ( Δ y ) 2 1 ( Δ y ) 2 0 0 0 0 1 ( Δ y ) 2 2 ( Δ y ) 2 0 0 0 0 0 0 2 ( Δ y ) 2 1 ( Δ y ) 2 0 0 0 0 1 ( Δ y ) 2 2 ( Δ y ) 2 1 ( Δ y ) 2 0 0 0 0 1 ( Δ y ) 2 2 ( Δ y ) 2
U = [ u , u ] T and g is a vector of constants.
The resulting equation arising from the semi-discretized Equation (42) which is expressed in form (43) and solved by the HFBI.

5. Numerical Examples

The accuracy and efficiency of the HFBI are shown in this section. Three numerical examples of anisotropic elliptic second-order partial differential models sourced from the recent literature were executed using a written program in Mathematica [11.0]. The computational results obtained by the HFBI were investigated in comparison with the existing methods in the literature. The results are presented in tabular form to show the superiority of HFBI in terms of accuracy and efficiency.
The absolute error (AE) is given by AE = Max | u ( x m , t m ) u m ( t n ) |.
It follows that u ( x m , t m ) is the exact solution, and u m ( t n ) is the approximate solution at the mesh point ( x m , t m ) .
Example 1.
The first second-order anisotropic elliptic PDEs are taken from [39]
2 u x 2 ( x , y ) + 2 u y 2 ( x , y ) = 2 π 2 sin ( π x ) cos ( π y ) , for 0 x 1 , 0 y 1
with the conditions below
u ( 0 , y ) = 0 , u ( x , 0 ) = sin ( π x ) , u ( 1 , y ) = 0 , u ( x , 1 ) = sin ( π x )
The theoretical solution of (47) is given as
u ( x , y ) = sin ( π x ) cos ( π y )
We compared the numerical results of the HFBI with the exact solution (49) and the absolute error obtained is also presented. In Table 2, the exact solution, computed solution, and the absolute error for Example 1 are displayed in column 1, column 2, and column 3, respectively. It can be seen that the results of the computed solution were in good agreement or very close to the exact solution. This shows that the method contained a high rate of convergence. In other to access the accuracy of the HFBI, we compared with other researchers in the literature who have also solved the problem namely Wang & Zhang [39] which is denoted with WZ09 and Sun & Zhang [28] represented with SZ04 in Figure 2.
Wang & Zhang in [39] proposed an algorithm entitled a sixth-order compact scheme combined with multigrid method and extrapolation technique, while Sun & Zhang in [28] developed a method titled a high-order finite difference discretization strategy based on extrapolation. In Table 3, we present the comparison of the absolute error in the HFBI, Wang & Zhang in [39] and Sun & Zhang in [28] with N varying from N = 2 , 4 , 8 , 16 , 32 , 64 and 128. It is obvious that generally as N increased, the accuracies also increased. The accuracy also decreased as N decreased. The HFBI performed better than Wang & Zhang [39] which is denoted with WZ09 and Sun & Zhang [28] represented with SZ04 in Figure 2 in terms of convergence and accuracy.
Remark 3.
- means Not Available.
Example 2.
Next, we take the following anisotropic equation solved by [30]
2 u x 2 ( x , y ) + 2 u y 2 ( x , y ) sin ( π x ) sin ( π y ) , 0 < x , y < 1 ,
subjected to the following conditions
u ( x , 0 ) = 0 , u ( 0 , y ) = 0 , u ( x , 1 ) = 0 , u ( 1 , y ) = 0 u x ( 0 , y ) = sin ( π y ) 2 π , u x ( x , 0 ) = 0 , u y ( 0 , x ) = 0 , u y ( x , 0 ) = sin ( π x ) 2 π u x ( 1 , y ) = sin ( π y ) 2 π , u y ( x , 1 ) = 0 , u y ( 1 , y ) = 0 , u y ( x , 1 ) = sin ( π x ) 2 π
The theoretical solution of (50) is given as
u ( x , y ) = sin ( π x ) sin ( π y ) 2 π 2
Now, in Table 4, The numerical computation of the HFBI for problem (50) is presented. Furthermore, the comparison of the absolute error in HFBI is made with Raslan et al. [30], as shown in Table 5. In their article, they proposed an extended cubic B-splines by Raslan et al. in [30] which is denoted with RA21 in Figure 3. The accuracy of the HFBI over Raslan et al. in [30] is also demonstrated in Table 5 and the efficiency curve in Figure 3. Hence, the new method is superior to the existing method of Raslan et al. in [30].
Example 3.
Finally, we take the following inhomogeneous elliptic equation studied by [40]
2 u 2 u = 4 ( 1 x ) ( 1 y ) ( x + y ) e x y , ( x , y ) R = ( 0 , 1 ) × ( 0 , 1 ) ,
which is governed by the homogeneous boundary conditions u = 0 on R .
The analytical smooth solution of (53) is given as
u ( x , y ) = x y ( 1 x ) ( 1 y ) e x y
Remark 4.
S3CPCM: Shifted Third-kind Chebyshev Petro-Galerkin method proposed by [40]. S4CPCM: Shifted Fourth-kind Chebyshev Petro-Galerkin method proposed by [40]. MAE: Maximum absolute error.
S3CPCM—Shifted Third-kind Chebyshev Petro-Galerkin method proposed by [40]
S4CPCM—Shifted Fourth-kind Chebyshev Petro-Galerkin method proposed by [40]
Ashry et al. in [40] proposed the Shifted Third-kind Chebyshev Petro-Galerkin method (S3CPCM) and Shifted Fourth-kind Chebyshev Petro-Galerkin method (S4CPCM) for the treatment of one- and two-dimensional second-order BVPs. The methods were also applied to solve an inhomogeneous elliptic equation. In Table 6, we compare the MAE of the HFBI with the S3CPCM and S4CPCM with N = 3 , 6 , and 9. Figure 4 depicts the comparison of the MAE in curves. Apparently, the HFBI showed some level of high accuracies with minimal error against Ashry et al. [40].

6. Conclusions

In this study, we have successfully developed, analyzed, and implemented an HFBI. The derivation involved a Hermite polynomial as the basic function through the interpolation and collocation techniques. The HFBI of convergence order eight was zero-stable and consistent, and the region of absolute stability was examined through the boundary locus method and found to be absolutely-stable, as shown in Figure 1. The HFBI was applied to solve the resulting second-order ODEs arising from the semi-discretization of the second-order partial differential equations. Three test problems that have applications in physics and engineering were tested on the HFBI, and the results were presented in tabular form. The comparison of the computed solution and the exact solution was made in Table 2 and Table 4 and also compared with existing methods in the recent literature in Table 3, Table 5 and Table 6 for problems 1–3. The comparison of the HFBI in curves was also shown in Figure 2, Figure 3 and Figure 4. Finally, the HFBI was in good agreement with the theoretical solution and compared favorably with the existing methods cited in the literature. The superiority of the results to other approaches shows that the application of Hermite polynomial as a basis function is a good candidate for such a class of problem [35]. The method is computationally reliable, accurate, and efficient.

Author Contributions

Funding acquisition, S.-W.Y.; Investigation, S.-W.Y.; Methodology, E.O.A., E.O.O. and A.S. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by the National Natural Science Foundation of China (No. 71601072), the Fundamental Research Funds for the Universities of Henan Province (No. NSFRF210314), and the Innovative Research Team of Henan Polytechnic University (No. T2022-7).

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Acknowledgments

The authors thank the anonymous referees whose suggestions helped improve this manuscript.

Conflicts of Interest

The authors declare no conflict of interest.

Appendix A

c 0 = u m , n ,
c 1 = 1 1 , 814 , 400 h ( 416 , 173 h 2 f m , n + 950 , 684 h 2 f m + 1 , n 1 , 025 , 097 h 2 f m + 2 , n + 1 , 059 , 430 h 2 f m + 3 , n 768 , 805 h 2 f m + 4 , n + 362 , 112 h 2 f m + 5 , n 99 , 359 h 2 f m + 6 , n + 12 , 062 h 2 f m + 7 , n + 1 , 814 , 400 u m , n 1 , 814 , 400 u m + 1 , n ) ,
c 2 = 1 2 f m , n ,
c 3 = 1 2520 h ( 1089 f m , n 2940 f m + 1 , n + 4410 f m + 2 , n 4900 f m + 3 , n + 3675 f m + 4 , n 1764 f m + 5 , n + 490 f m + 6 , n 60 f m + 7 , n ) ,
c 4 = 1 4320 h 2 ( 938 f m , n 4014 f m + 1 , n + 7911 f m + 2 , n 9490 f m + 3 , n + 7380 f m + 4 , n 3618 f m + 5 , n + 1019 f m + 6 , n 126 f m + 7 , n ) ,
c 5 = 1 14 , 400 h 3 ( 967 f m , n 5104 f m + 1 , n + 11 , 787 f m + 2 , n 15 , 560 f m + 3 , n + 12 , 725 f m + 4 , n 6432 f m + 5 , n + 1849 f m + 6 , n 232 f m + 7 , n ) ,
c 6 = 1 4320 h 4 ( 967 f m , n 5104 f m + 1 , n + 11 , 787 f m + 2 , n 15 , 560 f m + 3 , n + 12 , 725 f m + 4 , n 6432 f m + 5 , n + 1849 f m + 6 , n 232 f m + 7 , n ) ,
c 7 = 1 30 , 240 h 5 ( 46 f m , n 295 f m + 1 , n + 810 f m + 2 , n 1235 f m + 3 , n + 1130 f m + 4 , n 621 f m + 5 , n + 190 f m + 6 , n 25 f m + 7 , n ) ,
c 8 = 1 40 , 320 h 6 ( 4 f m , n 27 f m + 1 , n + 78 f m + 2 , n 125 f m + 3 , n + 120 f m + 4 , n 69 f m + 5 , n + 22 f m + 6 , n 3 f m + 7 , n ) ,
c 9 = 1 362 , 880 h 7 ( f m , n 7 f m + 1 , n + 21 f m + 2 , n 35 f m + 3 , n + 35 f m + 4 , n 21 f m + 5 , n + 7 f m + 6 , n f m + 7 , n )

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Figure 1. RAS of HFBI.
Figure 1. RAS of HFBI.
Fractalfract 06 00497 g001
Figure 2. Efficiency curve for Problem 1.
Figure 2. Efficiency curve for Problem 1.
Fractalfract 06 00497 g002
Figure 3. Efficiency curve for Problem 2.
Figure 3. Efficiency curve for Problem 2.
Fractalfract 06 00497 g003
Figure 4. Efficiency curve for Problem 3.
Figure 4. Efficiency curve for Problem 3.
Fractalfract 06 00497 g004
Table 1. Analysis of the order and error constant of HFBI in (13)–(26).
Table 1. Analysis of the order and error constant of HFBI in (13)–(26).
EquationFormulaeError ConstantOrder p
13 u m + 1 , n 5.537230 × 10 3 8
14 u m + 2 , n 1.378307 × 10 2 8
15 u m + 3 , n 2.159598 × 10 2 8
16 u m + 4 , n 2.948854 × 10 2 8
17 u m + 5 , n 3.746073 × 10 2 8
18 u m + 6 , n 4.500000 × 10 2 8
19 u m + 7 , n 5.524788 × 10 2 8
20 u m + 1 , n 9.356537 × 10 3 8
21 u m + 2 , n 7.345679 × 10 3 8
22 u m + 3 , n 8.236607 × 10 3 8
23 u m + 4 , n 7.548501 × 10 3 8
24 u m + 5 , n 8.439429 × 10 3 8
25 u m + 6 , n 6.428571 × 10 3 8
26 u m + 7 , n 1.578511 × 10 2 8
Table 2. Numerical results of exact-solution, computed-solution, and the Absolute error in HFBI for Problem 2.
Table 2. Numerical results of exact-solution, computed-solution, and the Absolute error in HFBI for Problem 2.
NExact-SolutionComputed-SolutionAE in HFBI
2 0.950651965960978000 0.951056516295153500 4.045503 × 10 4
4 0.703696743499951600 0.703701868763191200 5.125263 × 10 6
8 0.380836408840172200 0.380840707040230040 4.298200 × 10 6
16 0.194151840094070400 0.194150908792011470 9.313021 × 10 7
32 0.098009759640639170 0.098009759819161480 1.785223 × 10 10
64 0.049063979474120880 0.049063979621783700 1.476628 × 10 10
128 0.024539380650971644 0.024539380613539380 3.743227 × 10 11
Table 3. Comparison of AE in HFBI with [39] and AE in [28] for Problem 1.
Table 3. Comparison of AE in HFBI with [39] and AE in [28] for Problem 1.
NAE in HFBIAE in [39]AE in [28]
2 4.045503 × 10 4
4 5.125263 × 10 6
8 4.298200 × 10 6
16 9.313021 × 10 7 1.12 × 10 4 1.12 × 10 4
32 1.785223 × 10 10 2.50 × 10 6 2.50 × 10 6
64 1.476628 × 10 10 4.58 × 10 8 4.58 × 10 8
128 3.743227 × 10 11 7.66 × 10 10 7.66 × 10 10
Table 4. Numerical results of exact-solution, computed-solution and the Absolute error of the HFBI for Problem 2.
Table 4. Numerical results of exact-solution, computed-solution and the Absolute error of the HFBI for Problem 2.
xExact-SolutionComputed-SolutionAE in HFBI
0.1 0.004836992197904119 0.004837656046375394 6.63848 × 10 7
0.2 0.009200505898171044 0.009201768612999936 1.26271 × 10 6
0.3 0.012663409977431005 0.01266514795529222 1.73798 × 10 6
0.4 0.014886731256934604 0.014888774372445875 2.04312 × 10 6
0.5 0.015652835559053807 0.015654983817833652 2.14826 × 10 6
0.6 0.014886731256934628 0.014888774372445875 2.04312 × 10 6
0.7 0.012663409977431019 0.01266514795529222 1.73798 × 10 6
0.8 0.009200505898171032 0.00920176861299994 1.26271 × 10 6
0.9 0.004836992197904098 0.004837656046375396 6.63848 × 10 7
Table 5. Comparison of AE in HFBI with Extended Cubic B-Splines proposed by [30] for Problem 2.
Table 5. Comparison of AE in HFBI with Extended Cubic B-Splines proposed by [30] for Problem 2.
xAE in HFBIAE in [30]
0.2 1.26271 × 10 6 1.04701 × 10 4
0.4 2.04312 × 10 6 1.69408 × 10 4
0.6 2.04312 × 10 6 1.69408 × 10 4
0.8 1.26271 × 10 6 1.04701 × 10 4
Table 6. Comparison of MAE in HFBI with MAE in S3CPCM and S4CPCM both proposed by [40] for Problem 3.
Table 6. Comparison of MAE in HFBI with MAE in S3CPCM and S4CPCM both proposed by [40] for Problem 3.
NMAE in HFBIMAE in S3CPCM [40]MAE in S4CPCM [40]
3 1.60 × 10 8 3.26 × 10 3 4.11 × 10 3
6 4.80 × 10 10 2.53 × 10 5 3.61 × 10 5
9 6.34 × 10 11 5.19 × 10 10 7.46 × 10 10
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Adeyefa, E.O.; Omole, E.O.; Shokri, A.; Yao, S.-W. Hermite Fitted Block Integrator for Solving Second-Order Anisotropic Elliptic Type PDEs. Fractal Fract. 2022, 6, 497. https://doi.org/10.3390/fractalfract6090497

AMA Style

Adeyefa EO, Omole EO, Shokri A, Yao S-W. Hermite Fitted Block Integrator for Solving Second-Order Anisotropic Elliptic Type PDEs. Fractal and Fractional. 2022; 6(9):497. https://doi.org/10.3390/fractalfract6090497

Chicago/Turabian Style

Adeyefa, Emmanuel Oluseye, Ezekiel Olaoluwa Omole, Ali Shokri, and Shao-Wen Yao. 2022. "Hermite Fitted Block Integrator for Solving Second-Order Anisotropic Elliptic Type PDEs" Fractal and Fractional 6, no. 9: 497. https://doi.org/10.3390/fractalfract6090497

APA Style

Adeyefa, E. O., Omole, E. O., Shokri, A., & Yao, S. -W. (2022). Hermite Fitted Block Integrator for Solving Second-Order Anisotropic Elliptic Type PDEs. Fractal and Fractional, 6(9), 497. https://doi.org/10.3390/fractalfract6090497

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