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Article

Superconvergence Analysis of Discontinuous Galerkin Methods for Systems of Second-Order Boundary Value Problems

Department of Mathematics and Natural Sciences, Gulf University for Science and Technology, Hawally 32093, Kuwait
Computation 2023, 11(11), 228; https://doi.org/10.3390/computation11110228
Submission received: 8 September 2023 / Revised: 21 October 2023 / Accepted: 2 November 2023 / Published: 15 November 2023
(This article belongs to the Section Computational Engineering)

Abstract

:
In this paper, we present an innovative approach to solve a system of boundary value problems (BVPs), using the newly developed discontinuous Galerkin (DG) method, which eliminates the need for auxiliary variables. This work is the first in a series of papers on DG methods applied to partial differential equations (PDEs). By consecutively applying the DG method to each space variable of the PDE using the method of lines, we transform the problem into a system of ordinary differential equations (ODEs). We investigate the convergence criteria of the DG method on systems of ODEs and generalize the error analysis to PDEs. Our analysis demonstrates that the DG error’s leading term is determined by a combination of specific Jacobi polynomials in each element. Thus, we prove that DG solutions are superconvergent at the roots of these polynomials, with an order of convergence of O ( h p + 2 ) .

1. Introduction

The discontinuous Galerkin (DG) technique was first introduced by Reed and Hill [1] in 1973, with the aim of addressing the hyperbolic equation of neutron transport. They developed a discontinuous Galerkin method, a locally conservative and parallelizable method that can effectively handle complex geometries and does not require continuity across element boundaries. These desirable features have contributed to the DG method’s widespread use in solving various challenging real-world problems including, but not limited to, Troesch’s problem [2], α -synuclein spreading in Parkinson’s disease [3], fully coupled hydro-mechanical modeling of two-phase flow in deformable fractured porous media [4], the recovery of conductivity in electrical impedance tomography [5], wave propagation phenomena in thermo-poroelastic media [6], Maxwell’s equations in optics and photonics [7], solidification problems in a semitransparent medium-filled cavity [8], and seismic wave propagation problems [9].
A notable refinement of the DG approach emerged with the introduction of the Runge–Kutta DG scheme by Cockburn et al. This advancement was detailed in a sequence of works [10,11,12,13], where they aimed to tackle nonlinear hyperbolic conservation laws. Over time, the DG methodology has been extended to handle scenarios involving higher-order derivatives. A comprehensive and current overview of the evolution and applications of the DG method was presented by Shu in his surveys [14,15].
In 2007, Adjerid and Temimi [16] developed a novel DG scheme for handling higher-order initial value problems without requiring any auxiliary variables like the local DG methods. Using p-degree piecewise polynomials, they proved that their method achieves a convergence rate of p + 1 . In [17], Chen and Shu introduced a range of ultra-weak discontinuous Galerkin (UWDG) techniques. These methods were designed to address boundary value problems encompassing second-order to fifth-order ordinary differential equations (ODEs). Their strategy combined the DG method for spatial discretization with the TVD high-order Runge–Kutta method for temporal discretization. By carefully selecting numerical fluxes, they demonstrated the stability of their proposed schemes and numerically showed that their method achieves an optimal ( p + 1 ) -th convergence rate despite the theoretical sub-optimal error estimates.
In [18], Adjerid and Temimi expanded upon their earlier research and employed it in the context of the wave equation through the utilization of the method of lines. This approach involves the integration of the standard finite element method and the discontinuous Galerkin method in the spatial and temporal dimensions, respectively. The researchers showcased the efficacy of this new technique by deriving a range of optimal error estimates in both space and time domains. In addition, they conducted a comparative analysis against existing methodologies. Furthermore, the study revealed the superconvergence of the DG solution within each space-time element, specifically at the intersecting points of the Lobatto polynomials in space and the Jacobi polynomials in time. Later, Temimi [19] solved the one-dimensional second-order BVPs using the developed DG scheme and demonstrated that a specific combination of Jacobi polynomials generates the leading term of the discretization error in each element. He proved that the p-degree DG solution achieves an O ( h p + 2 ) superconvergence rate at the roots of these particular polynomials. Baccouch and Temimi [20] further extended the DG error analysis to second-order BVPs and showed that when using p-degree piecewise polynomials, the UWDG solution and its derivative exhibit a superconvergence rate of O ( h 2 p ) at the upwind and downwind endpoints. Moreover, Baccouch and Temimi [21] proposed a novel DG scheme for solving the wave equation based on the method of lines. They demonstrated that the DG solution achieves in the L 2 -norm an optimal rate of convergence.
Recently, several superconvergence studies have elaborated. In [22], Baccouch presented superconvergence results for the local discontinuous Galerkin method applied to the sine-Gordon nonlinear hyperbolic equation in one space dimension. Additionally, Baccouch [23,24] explored the convergence and superconvergence properties of a local discontinuous Galerkin method for nonlinear second-order two-point boundary value problems. Subsequently, Baccouch [25] delved into the convergence and superconvergence properties of an ultra-weak discontinuous Galerkin method for linear fourth-order boundary value problems. In a related vein, Ma [26] presented a comprehensive analysis of superconvergence properties for a wide class of mixed discontinuous Galerkin methods. In [27], Liu et al. investigated the superconvergence properties of local discontinuous Galerkin methods with generalized alternating fluxes for one-dimensional linear convection–diffusion equations. More recently, in 2023, Singh et al. [28] provided a detailed superconvergence error analysis of the discontinuous Galerkin method with interior penalties for 2D elliptic convection–diffusion–reaction problems.
To the best of our knowledge, none of the previous references have investigated a system of boundary value problems or provided a detailed form of the leading term of the DG errors, which serve as a foundation for interesting superconvergence criteria. In our current work, we developed a local error analysis of the DG method for systems of second-order BVPs. Our findings revealed that, within each element, the error’s leading term is a combination of specific Jacobi polynomials. Notably, we demonstrated that the DG solutions are O ( h p + 2 ) superconvergent at these combined Jacobi polynomial roots. These superconvergence results can be further applied to compute efficient a posteriori error estimates and to construct higher-order DG solutions. The results of our current analysis, combined with our previous work involving the method of lines, will be integrated in future phases to develop a fully DG scheme for solving higher-dimensional partial differential equations. We believe that the new scheme will exhibit superior accuracy and efficiency compared to existing methods.
This manuscript is summarized in this way. We develop a DG scheme applied to systems of boundary value problems in Section 2. The local error analysis with DG superconvergence properties are provided in Section 3. Then, we carry out several computational simulations to exhibit the full agreement with theoretical findings in Section 4. Finally, some concluding remarks are stated in Section 5.

2. Model Problem

In this section, we develop the DG formulation of the system of BVPs given by
y ¨ + y ˙ + K y = f ( x ) , x ( a , b ) ,
subject to mixed boundary conditions
y ( a ) = y l , y ˙ ( b ) = y r x .
The Dirichlet boundary conditions scenario is also explored:
y ( a ) = y l , y ( b ) = y r .
where
y ( x ) = y 1 ( x ) y 2 ( x ) y n ( x ) , y l = y 1 , l y 2 , l y n , l , y r x = y 1 , r x y 2 , r x y n , r x , y r = y 1 , r y 2 , r y n , r
where C and K are two matrices defined respectively by C = ( C i j ) 1 i , j n and K = ( K i j ) 1 i , j n . Also, a smooth exact vector solution is achieved by properly choosing the vector function f.
To implement the discontinuous Galerkin method, we initially create a partition h = ( b a ) N + 1 . For k = 0 , 1 , 2 , , N , we let x k = a + k · h and I k = ( x k , x k + 1 ) ; we also construct a finite-dimensional space S N , p
S N , p = { Y : [ a , b ] R n , Y | I k [ P p ] n } ,
where P p designates the p-degree polynomial space.
Next, we multiply (1a) by a vector test function v ( x ) [ H 2 ( [ a , b ] ) ] n . We integrate the resulting system of equations over I k and we integrate it by parts twice to derive the weak discontinuous Galerkin (DG) formulation for (1). Then, for k = 0 , 1 , , N we have
I k v ¨ t y + v ˙ t y + v t K y d x + v t y ˙ | x k x k + 1 v ˙ t y | x k x k + 1 + v t K y | x k x k + 1 = I k v t d x .
In (4), replacing y by Y k ( x ) = Y | [ x k , x k + 1 ] S N , p and v by V S N , p leads to
I k V ¨ t Y k + V ˙ t Y k + V t K Y k d x + V t ( x k + 1 ) Y ˙ ^ k ( x k + 1 ) V t ( x k + ) Y ˙ ^ k ( x k )
V ˙ ( x k + 1 ) t Y ^ k ( x k + 1 ) + V ˙ t ( x k + ) Y ^ k ( x k ) + V t ( x k + 1 ) K Y ^ k ( x k + 1 )
V t ( x k + ) K Y ^ k ( x k ) = I k V t d x , V S N , p
where Y k = [ Y 1 , k , Y 2 , k , , Y n , k ] t and where Y ^ k ( x k ) , Y ^ k ( x k + 1 ) , Y ˙ ^ k ( x k ) and Y ˙ ^ k ( x k + 1 ) denote the numerical fluxes defined by Cheng et al. [17] as follows:
Y ^ 0 ( a ) = y l , Y ^ 0 ( x 1 ) = Y 0 ( x 1 ) , Y ^ k ( x k ) = Y k 1 ( x k ) , Y ^ k ( x k + 1 ) = Y k ( x k + 1 ) , k = 1 , , N ,
Y ˙ ^ k ( x k ) = Y ˙ k ( x k + ) , Y ˙ ^ k ( x k + 1 ) = Y ˙ k + 1 ( x k + 1 + ) , k = 0 , , N 1 , Y ˙ ^ N ( x N ) = Y ˙ N ( x N + ) , Y ˙ ^ N ( b ) = y r x .
The numerical fluxes, for the case of Dirichlet boundary conditions, are given by
Y ^ 0 ( a ) = y l , Y ^ 0 ( x 1 ) = Y 0 ( x 1 ) , Y ^ k ( x k ) = Y k 1 ( x k ) , Y ^ k ( x k + 1 ) = Y k ( x k + 1 ) , k = 1 , , N 1 , Y ^ N ( x N ) = Y N 1 ( x N ) , Y ^ N ( b ) = y r ,
and
Y ˙ ^ 0 ( a ) = Y ˙ 0 ( a + ) , Y ˙ ^ 0 ( x 1 ) = Y ˙ 1 ( x 1 + ) , Y ˙ ^ k ( x k ) = Y ˙ k ( x k + ) , Y ˙ ^ k ( x k + 1 ) = Y ˙ k + 1 ( x k + 1 + ) , k = 1 , , N 1 , Y ˙ ^ N ( x N ) = Y ˙ N ( x N + ) , Y ˙ ^ N ( b ) = Y ˙ N ( b ) + p h ( Y N ( b ) y r ) .
Therefore, the discrete formulation involves finding Y k ( x ) = Y | [ x k , x k + 1 ] S N , p such that V S N , p
I 0 V ¨ t Y 0 + V ˙ t Y 0 + V t K Y 0 d x + V t ( x 1 ) Y ˙ 1 ( x 1 + ) V t ( a + ) Y ˙ 0 ( a + )
V ˙ ( x 1 ) t Y 0 ( x 1 ) + V ˙ t ( a + ) y l + V t ( x 1 ) K Y 0 ( x 1 ) V t ( a + ) K y l = I 0 V t d x ,
For k = 1 , , N 1
I k V ¨ t Y k + V ˙ t Y k + V t K Y k d x + V t ( x k + 1 ) Y ˙ k + 1 ( x k + 1 + ) V t ( x k + ) Y ˙ k ( x k + )
V ˙ ( x k + 1 ) t Y k ( x k + 1 ) + V ˙ t ( x k + ) Y k 1 ( x k ) + V t ( x k + 1 ) K Y k ( x k + 1 )
V t ( x k + ) K Y k 1 ( x k ) = I k V t d x ,
and
I N V ¨ t Y N + V ˙ t Y N + V t K Y N d x + V t ( b ) y r x V t ( x N + ) Y ˙ N ( x N + )
V ˙ ( b ) t Y N ( b ) + V ˙ t ( x N + ) Y N 1 ( x N ) + V t ( b ) K Y N ( b )
V t ( x N + ) K Y N 1 ( x N ) = I N V t d x .
When subjected to Dirichlet boundary conditions, (10c) is written as
I N V ¨ t Y N + V ˙ t Y N + V t K Y N d x + V t ( b ) Y ˙ N ( b ) + p h ( Y N ( b ) y r )
V t ( x N + ) Y ˙ N ( x N + ) V ˙ ( b ) t y r + V ˙ t ( x N + ) Y N 1 ( x N ) + V t ( b ) K y r
V t ( x N + ) K Y N 1 ( x N ) = I N V t d x .

3. Local Error Analysis

In order to perform a complete analysis of the method, we first define the Jacobi polynomials [29] using Rodgrigues’ formula:
P q α , β ( ξ ) = ( 1 ) q 2 q q ! ( 1 ξ ) α ( 1 + ξ ) β d q d ξ q [ ( 1 ξ ) α + q ( 1 + ξ ) β + q ] ,
α , β > 1 , q = 0 , 1 , .
Ref. [30] states some valuable properties of Jacobi polynomials that would be useful to formulate the error’s leading term.
In order to investigate the local behavior of the error, we analyze the problem (1) in its reduced form defined on one reference element [ 0 , h ] :
y ¨ + y ˙ + K y = f ( x ) , x ( 0 , h ) ,
subject to
y ( 0 ) = y l , y ˙ ( h ) = y r x .
Therefore, problem (12) can be written as, for i = 1 , , n ,
y i + j = 1 n K i j y j + j = 1 n C i j y j = f i ( x ) 0 < x < h ,
subject to
y i ( 0 ) = y 1 , l , y i ( h ) = y r x .
This simplified version of the problem, even if it is not the original one, affords identifying the error’s leading term. In this paper, we do not show the scenario of the Dirichlet boundary conditions given that it would be readily achievable by adopting almost identical analysis steps.
Therefore, the weak DG formulation of (13) is given by
y i , r x v h y i 0 + v 0 + y i h v h + y i , l v 0 + +
j = 1 n K i j y j h v h y i , l v 0 + +
0 h y i v j = 1 n K i j y j v + j = 1 n C i j y j v d x = 0 h f i v d x , x [ 0 , h ] ,
and the discrete formulation entails finding Y i ( x ) P p for i = 1 , , n such that V P p
Y i , r x V h Y i 0 + V 0 + Y i h V h + Y i , l V 0 + +
j = 1 n K i j Y j h V h Y i , l V 0 + +
0 h Y i V j = 1 n K i j Y j V + j = 1 n C i j Y j V d x = 0 h f i V d x .
Next, we replace v by V P p in (14) and subtract (15) to achieve the discontinuous Galerkin condition of the local error e i = y i Y i for i = 1 , , n on [ 0 , h ]
e i O + V O + e i h V h + j = 1 n K i j e j h V h +
0 h e i V j = 1 n K i j e j V + j = 1 n C i j e j V d x = 0 , V P p .
By implementing a linear mapping from [ 0 , h ] to the canonical element [ 1 , 1 ] and denoting by e ^ , the mapped local error on [ 1 , 1 ] , (16) becomes
e ^ i ( 1 ) V ( 1 ) e ^ i ( 1 ) V ( 1 ) + h 2 j = 1 n K i j e ^ j ( 1 ) V ( 1 ) +
1 1 e ^ i V h 2 j = 1 n K i j e ^ i V + h 2 2 j = 1 n C i j e ^ j V d ξ = 0 , V P p .
Next, we present and demonstrate our major finding on the local discretization error.
Theorem 1.
Let y [ C 2 p + 2 ] n be the solution of (1) and Y k S N , p , p 2 , solution of (10). Therefore, for each i = 1 , , n , the local discretization error satisfies
e ^ i = l = p + 1 Q i , l ( ξ ) h l ,
where Q i , l ( ξ ) P l , and its leading term is defined by
Q i , p + 1 ( ξ ) = c i , p + 1 ( ξ 1 ) P p 1 , 0 ( ξ ) + p + 1 p 2 P p 1 1 , 0 ( ξ ) .
Proof. 
Given that y i C 2 p + 2 , the local error’s Maclaurin series of e ^ i with respect to h is given by
e ^ i = l = 0 Q i , l ( ξ ) h l .
Replacing (19) in (17) and assembling the terms with the same powers of h leads to
Q i , 0 ( 1 ) V ( 1 ) + 1 1 Q i , 0 V d ξ +
Q i , 1 ( 1 ) V ( 1 ) Q i , 1 ( 1 ) V ( 1 ) + j = 1 n 1 2 K i j Q j , 0 ( 1 ) V ( 1 ) +
1 1 Q i , 1 V j = 1 n 1 2 K i j Q j , 0 V d ξ h +
l = 2 Q i , l ( 1 ) V ( 1 ) Q i , l ( 1 ) V ( 1 ) + j = 1 n 1 2 K i j Q j , l 1 ( 1 ) V ( 1 ) +
1 1 Q i , k V j = 1 n 1 2 K i j Q j , l 1 V + j = 1 n 1 4 C i j Q j , l 2 V d ξ h l = 0 . V P p .
The O ( 1 ) term gives
Q i , 0 ( 1 ) V ( 1 ) + 1 1 Q i , 0 V d ξ = 0 , V P p .
Letting V = ξ 1 leads to Q i , 0 = 0 for i = 1 , , n .
The O ( h ) yields
Q i , 1 ( 1 ) V ( 1 ) Q i , 1 ( 1 ) V ( 1 ) + 1 1 Q i , 1 V d ξ = 0 , V P p .
Using V = 1 gives Q i , 1 ( 1 ) = 0 and V = ξ 1 results in Q i , 1 ( 1 ) = 0 , leading to Q i , 1 = 0 for i = 1 , , n .
Reasoning by induction, we suppose that Q i , m = 0 for m = 0 , 1 , , l 1 where l p 2 . Thus, the O ( h l ) term gives
Q i , l ( 1 ) V ( 1 ) Q i , l ( 1 ) V ( 1 ) + 1 1 Q i , l V d ξ = 0 , V P p .
Using V = 1 gives Q i , l ( 1 ) = 0 and V = ξ 1 results in Q i , l ( 1 ) = 0 , and we obtain
1 1 Q i , l V d ξ = 0 , V P p .
Thus, for l p 2 , Q i , l = 0 .
Moreover, the O ( h p 1 ) term results in to Q i , p 1 = 0 and the O ( h p ) in Q i , p = 0 , for i = 1 , , n .
The O ( h p + 1 ) term gives
Q i , p + 1 ( 1 ) V ( 1 ) Q i , p + 1 ( 1 ) V ( 1 ) + 1 1 Q i , p + 1 V d ξ = 0 , V P p .
Again, using V = 1 gives Q i , p + 1 ( 1 ) = 0 and V = ξ 1 results in Q i , p + 1 ( 1 ) = 0 , for i = 1 , , n , leading to
1 1 Q i , p + 1 V d ξ = 0 , V P p .
We can express Q i , p + 1 ( ξ ) as
Q i , p + 1 ( ξ ) = j = 0 p + 1 β i , j P j 0 , 0 ( ξ ) ,
where P j 0 , 0 are Legendre (specific Jacobi) polynomials of degree j. By plugging (27) in (26), we achieve
Q i , p + 1 ( ξ ) = β i , p 1 P p 1 0 , 0 ( ξ ) + β i , p P p 0 , 0 ( ξ ) + β i , p + 1 P p + 1 0 , 0 ( ξ ) ,
using Q i , p + 1 ( 1 ) = 0 for i = 1 , , n gives
β i , p 1 + β i , p + β i , p + 1 = 0 .
Moreover,
Q p + 1 ( ξ ) = β i , p 1 p 2 P p 2 1 , 1 ( ξ ) + β i , p p + 1 2 P p 1 1 , 1 ( ξ ) + β i , p + 1 p + 2 2 P p 1 , 1 ( ξ ) ,
using Q i , p + 1 ( 1 ) = 0 for i = 1 , , n gives
α i , p 1 ( p 1 ) p + α i , p p ( p + 1 ) + α i , p + 1 ( p + 1 ) ( p + 2 ) = 0
Therefore, for i = 1 , , n
Q p + 1 ( ξ ) = c i , p + 1 P p + 1 0 , 0 ( ξ ) + 2 p + 1 p 2 P p 0 , 0 ( ξ ) p + 1 p 2 P p 1 0 , 0 ( ξ ) ,
Finally, we prove our theorem by using properties of the Jacobi polynomial [30]:
Q p + 1 ( ξ ) = c i , p + 1 ( ξ 1 ) P p 1 , 0 + p + 1 p 2 P p 1 1 , 0 .
In the following corollary, we prove that the DG solutions are superconvergent at some specific interior points.
Corollary 1.
Let y [ C 2 p + 2 ] n be the solution of (1) and Y k S N , p , p 2 , solution of (10); therefore, the DG solutions are superconvergent at x ^ j
e i ( x ˜ j ) = O ( h p + 2 ) , j = 1 , , p , i = 1 , , n ,
where x ˜ j are the roots of P p 1 , 0 ( ξ ) + p + 1 p 2 P p 1 1 , 0 ( ξ ) shifted to each element and the downwind endpoints of each element I k for k = 0 , 1 , , N .
Proof. 
Using Theorem 1, we have that, for each i = 1 , , n , the local discretization error satisfies
e ^ i ( ξ ) = Q i , p + 1 ( ξ ) h p + 1 + l = p + 2 Q i , l ( ξ ) h l ,
using (18b), we obtain
e ^ i ( ξ ) = c i , p + 1 ( ξ 1 ) P p 1 , 0 ( ξ ) + p + 1 p 2 P p 1 1 , 0 ( ξ ) + l = p + 2 Q i , l ( ξ ) h l .
By letting x ˜ j be the roots of P p 1 , 0 ( ξ ) + p + 1 p 2 P p 1 1 , 0 ( ξ ) on [ 1 , 1 ] , (34b) becomes
e ^ i ( x ˜ j ) = l = p + 2 Q i , l ( x ˜ j ) h l .
which can be written as
e ^ i ( x ˜ j ) = Q i , p + 2 ( x ˜ j ) h p + 2 + l = p + 3 Q i , l ( x ˜ j ) h l .
Then, by mapping e ^ i and shifting x ˜ j to each element I k , the proof is achieved. □

4. Numerical Examples

In order to validate our theory, we consider two systems of second-order differential equations subject to Neumann and Dirichlet boundary conditions. The numerical rate of convergence is defined by ln ( e ( N 1 ) / e ( N 2 ) ) ln ( N 1 / N 2 ) , where e ( N ) denotes the error e = y i Y i , for i = 1 , 2 , , n using N elements.
Example 1.
Let us consider the following system of three second-order differential equations
u 1 u 1 + u 2 + u 1 u 2 u 3 = f 1 ( x ) u 2 + u 1 3 u 3 + 3 u 1 + u 2 + u 3 = f 2 ( x ) , x [ 0 , 1 ] , u 3 + 2 u 1 + u 2 + 2 u 3 + 2 u 1 2 u 2 = f 3 ( x )
subject to Neumann and Dirichlet boundary conditions
u 1 ( 0 ) = 0 u 2 ( 0 ) = 0 u 3 ( 0 ) = 0 ,
and
u 1 ( 1 ) = 1 tanh ( 1 ) 2 u 2 ( 1 ) = 2 2 tanh ( 2 ) 2 u 3 ( 1 ) = 3 3 tanh ( 3 ) 2 ,
We choose f 1 , f 2 and f 3 such that the exact solutions are given by
u 1 ( x ) = tanh ( x ) u 2 ( x ) = tanh ( 2 x ) u 3 ( x ) = tanh ( 3 x ) .
We solve problem (37) using a uniform mesh with h = 0.05 and p = 2 , 3 , 4 and plot the errors u i U i , D G for i = 1 , 2 , 3 versus x in Figure 1, Figure 2 and Figure 3. These plots show that the errors are crossing the x-axis at the roots of the polynomial P p 1 , 0 ( ξ ) + p + 1 p 2 P p 1 1 , 0 ( ξ ) shifted to each element and at the downwind endpoints of each element. Therefore, these results confirm the established theory on the leading term of the errors for each of the three solutions.
Moreover, on uniform meshes with N = 10 , 15 , , 30 steps, problem (37) is solved for p = 2 , 3 , 4 , 5 . We exhibit | | u i ( x ˜ j ) U i , D G ( x ˜ j ) | | for i = 1 , 2 , 3 , where x ˜ j are the roots of the mapped polynomials Q i , p + 1 , along with their convergence rates in Table 1, Table 2 and Table 3. We notice that | | u i ( x ˜ j ) U i , D G ( x ˜ j ) | | for i = 1 , 2 , 3 are O ( h p + 2 ) superconvergent. As expected, there is full agreement between these results and the stated theory.
Example 2.
Next, let us consider the following system of ten second-order differential equations:
u + K u + C u = f ( x ) x [ 0 , π ]
subject to Dirichlet boundary conditions
u i ( 0 ) = 0 i = 1 , 2 , , 10 ,
and
u i ( π ) = 0 i = 1 , 2 , , 10 ,
where
K = 0.20 0.00 0.00 0.10 0.25 0.10 0.25 0.00 0.05 0.05 0.10 0.10 0.20 0.15 0.15 0.15 0.15 0.05 0.20 0.25 0.25 0.15 0.00 0.05 0.25 0.20 0.25 0.10 0.00 0.05 0.15 0.25 0.05 0.20 0.05 0.20 0.20 0.00 0.15 0.25 0.25 0.05 0.15 0.10 0.25 0.10 0.05 0.05 0.25 0.20 0.10 0.15 0.15 0.00 0.05 0.00 0.15 0.05 0.10 0.05 0.10 0.20 0.10 0.05 0.25 0.05 0.15 0.20 0.15 0.25 0.15 0.05 0.15 0.05 0.10 0.20 0.25 0.05 0.25 0.05 0.25 0.00 0.25 0.00 0.05 0.25 0.15 0.20 0.05 0.20 0.00 0.10 0.20 0.05 0.20 0.15 0.25 0.15 0.20 0.20 ,
C = 0.25 0.15 0.20 0.15 0.10 0.05 0.05 0.15 0.00 0.05 0.00 0.15 0.25 0.25 0.10 0.05 0.10 0.10 0.10 0.25 0.00 0.10 0.05 0.00 0.20 0.05 0.15 0.10 0.15 0.10 0.00 0.10 0.05 0.20 0.05 0.00 0.20 0.15 0.20 0.20 0.10 0.15 0.05 0.00 0.25 0.10 0.20 0.25 0.05 0.25 0.10 0.20 0.10 0.15 0.20 0.00 0.10 0.25 0.15 0.05 0.25 0.20 0.15 0.10 0.05 0.25 0.15 0.15 0.10 0.00 0.00 0.25 0.25 0.20 0.20 0.20 0.10 0.25 0.25 0.15 0.10 0.10 0.25 0.15 0.25 0.10 0.05 0.05 0.10 0.20 0.10 0.20 0.25 0.05 0.10 0.15 0.25 0.15 0.25 0.20
We choose f i for i = 1 , 2 , , 10 such that the exact solutions are given by
u i ( x ) = sin ( i · x ) i = 1 , 2 , , 10 .
We solve problem (39) using a uniform mesh with h = π 20 and p = 2 , 3 , 4 . Without loss of generality, we plot the errors u 5 U 5 , D G and u 10 U 10 , D G versus x in Figure 4 and Figure 5. These plots indicate that the errors intersect the x-axis at the roots of the polynomial P p 1 , 0 ( ξ ) + p + 1 p 2 P p 1 1 , 0 ( ξ ) shifted to each element and at the downwind endpoints of each element. Thus, these results perfectly support the established theory.
Moreover, on uniform meshes with N = 60 , 65 , , 80 steps, problem (39) is solved for p = 2 , 3 , 4 , 5 . Table 4, Table 5, Table 6 and Table 7 exhibit the maximum of the errors e i = u i U i , D G for i = 3 , 5 , 8 , 10 at the roots of polynomials Q i , p + 1 mapped to each element along with their convergence rates. As we can clearly see, | | u i ( x ˜ j ) U i , D G ( x ˜ j ) | | for i = 3 , 5 , 8 , 10 are O ( h p + 2 ) superconvergent at these specific roots. Consequently, the stated theory is fully supported by these results.

5. Conclusions

In this study, we conducted a local error analysis of the DG method for systems of second-order boundary value problems. We explored the superconvergence criteria and demonstrated that the leading error term on each element is a combination of specific Jacobi polynomials. We established that DG solutions exhibit superconvergence of O ( h p + 2 ) at the roots of these combined Jacobi polynomials. We further validated the established theory through some numerical simulations, and we showed the full agreement between the theory and the computational results. In our forthcoming paper, we will integrate the findings from this analysis with our earlier work involving the method of lines to create a comprehensive DG scheme for solving higher-dimensional partial differential equations. In our future research endeavors, we aim to expand the application of DG methods to address a variety of challenging real-world problems including, but not limited to, the two-dimensional hyperbolic partial differential equation of the Telegraph type [31], the integro-differential Beam problem [32], the nonlinear Bratu problem [33,34], delayed differential equations [35] and nonlinear Boussinesq and Klein–Gordon equations [36].

Funding

This research was funded by the Kuwait Foundation for the Advancement of Sciences grant number PR20-16SM-01.

Data Availability Statement

No new data were created.

Acknowledgments

The author acknowledges the continuous support of the Kuwait Foundation for the Advancement of Sciences (Project Code: PR20-16SM-01).

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. The error u 1 U 1 , D G for problem (37) with p = 2, 3, 4 and N = 20 and + denotes the roots of Q 1 , p + 1 mapped to each element.
Figure 1. The error u 1 U 1 , D G for problem (37) with p = 2, 3, 4 and N = 20 and + denotes the roots of Q 1 , p + 1 mapped to each element.
Computation 11 00228 g001
Figure 2. The error u 2 U 2 , D G for problem (37) with p = 2, 3, 4 and N = 20 and + denotes the roots of Q 2 , p + 1 mapped to each element.
Figure 2. The error u 2 U 2 , D G for problem (37) with p = 2, 3, 4 and N = 20 and + denotes the roots of Q 2 , p + 1 mapped to each element.
Computation 11 00228 g002
Figure 3. The error u 3 U 3 , D G for problem (37) with p = 2, 3, 4 and N = 20 and + denotes the roots of Q 3 , p + 1 mapped to each element.
Figure 3. The error u 3 U 3 , D G for problem (37) with p = 2, 3, 4 and N = 20 and + denotes the roots of Q 3 , p + 1 mapped to each element.
Computation 11 00228 g003
Figure 4. The error u 5 U 5 , D G for problem (39) with p = 2, 3, 4 and N = 20 and + denotes the roots of Q 5 , p + 1 mapped to each element.
Figure 4. The error u 5 U 5 , D G for problem (39) with p = 2, 3, 4 and N = 20 and + denotes the roots of Q 5 , p + 1 mapped to each element.
Computation 11 00228 g004
Figure 5. The error u 10 U 10 , D G for problem (39) with p = 2,3,4 and N = 20 and + denotes the roots of Q 10 , p + 1 mapped to each element.
Figure 5. The error u 10 U 10 , D G for problem (39) with p = 2,3,4 and N = 20 and + denotes the roots of Q 10 , p + 1 mapped to each element.
Computation 11 00228 g005
Table 1. The maximum error | | u 1 ( x ˜ j ) U 1 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of mapped polynomials Q 1 , p + 1 for problem (37) on uniform meshes.
Table 1. The maximum error | | u 1 ( x ˜ j ) U 1 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of mapped polynomials Q 1 , p + 1 for problem (37) on uniform meshes.
p = 2 p = 3 p = 4 p = 5
N | | e 1 ( x ˜ j ) | | Rate | | e 1 ( x ˜ j ) | | Rate | | e 1 ( x ˜ j ) | | Rate | | e 1 ( x ˜ j ) | | Rate
107.5961   ×   10 6 5.8505   ×   10 8 1.2823   ×   10 9 2.5832   ×   10 11
151.5830   ×   10 6 3.877.2451   ×   10 9 5.151.1635   ×   10 10 5.921.4520   ×   10 12 7.09
204.9887   ×   10 7 4.011.6525   ×   10 9 5.132.0909   ×   10 11 5.971.8596   ×   10 13 7.14
252.0541   ×   10 7 3.985.2684   ×   10 10 5.125.5017   ×   10 12 5.983.9774   ×   10 14 6.91
309.9025   ×   10 8 4.002.0754   ×   10 10 5.101.8459   ×   10 12 5.991.1241   ×   10 14 6.93
Table 2. The maximum error | | u 2 ( x ˜ j ) U 2 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of mapped polynomials Q 2 , p + 1 for problem (37) on uniform meshes.
Table 2. The maximum error | | u 2 ( x ˜ j ) U 2 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of mapped polynomials Q 2 , p + 1 for problem (37) on uniform meshes.
p = 2 p = 3 p = 4 p = 5
N | | e 2 ( x ˜ j ) | | Rate | | e 2 ( x ˜ j ) | | Rate | | e 2 ( x ˜ j ) | | Rate | | e 2 ( x ˜ j ) | | Rate
104.5986   ×   10 5 9.0804   ×   10 7 2.3762   ×   10 8 7.1286   ×   10 10
151.0249   ×   10 5 3.701.1199   ×   10 7 5.162.4137   ×   10 9 5.645.3654   ×   10 11 6.38
203.4145   ×   10 6 3.822.7619   ×   10 8 4.874.5279   ×   10 10 5.826.8065   ×   10 12 7.17
251.4386   ×   10 6 3.878.9665   ×   10 9 5.041.2177   ×   10 10 5.881.5068   ×   10 12 6.76
307.0618   ×   10 7 3.903.5610   ×   10 9 5.064.1381   ×   10 11 5.924.1211   ×   10 13 7.11
Table 3. The maximum error | | u 3 ( x ˜ j ) U 3 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of mapped polynomials Q 3 , p + 1 for problem (37) on uniform meshes.
Table 3. The maximum error | | u 3 ( x ˜ j ) U 3 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of mapped polynomials Q 3 , p + 1 for problem (37) on uniform meshes.
p = 2 p = 3 p = 4 p = 5
N | | e 3 ( x ˜ j ) | | Rate | | e 3 ( x ˜ j ) | | Rate | | e 3 ( x ˜ j ) | | Rate | | e 3 ( x ˜ j ) | | Rate
105.2266   ×   10 5 9.7683   ×   10 7 5.1465   ×   10 8 1.5770   ×   10 9
151.0337   ×   10 5 4.001.3039   ×   10 7 4.975.1178   ×   10 9 5.691.0687   ×   10 10 6.64
203.2481   ×   10 6 4.023.0870   ×   10 8 5.009.2283   ×   10 10 5.951.6011   ×   10 11 6.60
251.3376   ×   10 6 3.981.0067   ×   10 8 5.022.3949   ×   10 10 6.043.5490   ×   10 12 6.75
306.5181   ×   10 7 3.944.1795   ×   10 9 4.828.1987   ×   10 11 5.881.0226   ×   10 12 6.82
Table 4. The maximum error | | u 3 ( x ˜ j ) U 3 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of mapped polynomials Q 3 , p + 1 for problem (39) on uniform meshes.
Table 4. The maximum error | | u 3 ( x ˜ j ) U 3 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of mapped polynomials Q 3 , p + 1 for problem (39) on uniform meshes.
p = 2 p = 3 p = 4 p = 5
N | | e 3 ( x ˜ j ) | | Rate | | e 3 ( x ˜ j ) | | Rate | | e 3 ( x ˜ j ) | | Rate | | e 3 ( x ˜ j ) | | Rate
601.1663   ×   10 5 5.5757   ×   10 8 8.1254   ×   10 10 9.1438   ×   10 12
658.5227   ×   10 6 3.923.7016   ×   10 8 5.115.0436   ×   10 10 5.965.1827   ×   10 12 7.09
706.3717   ×   10 6 3.922.5835   ×   10 8 4.853.2419   ×   10 10 5.963.0594   ×   10 12 7.11
754.8584   ×   10 6 3.931.8239   ×   10 8 5.042.1476   ×   10 10 5.971.9088   ×   10 12 6.84
803.7688   ×   10 6 3.931.3070   ×   10 8 5.161.4606   ×   10 10 5.971.2143   ×   10 12 7.00
Table 5. The maximum error | | u 5 ( x ˜ j ) U 5 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of Q 5 , p + 1 for problem (39) on uniform meshes.
Table 5. The maximum error | | u 5 ( x ˜ j ) U 5 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of Q 5 , p + 1 for problem (39) on uniform meshes.
p = 2 p = 3 p = 4 p = 5
N | | e 5 ( x ˜ j ) | | Rate | | e 5 ( x ˜ j ) | | Rate | | e 5 ( x ˜ j ) | | Rate | | e 5 ( x ˜ j ) | | Rate
605.3921   ×   10 5 1.2012   ×   10 7 9.8735   ×   10 9 2.6052   ×   10 11
653.9423   ×   10 5 3.917.9812   ×   10 8 5.106.1964   ×   10 9 5.821.4974   ×   10 11 6.92
702.9484   ×   10 5 3.925.5651   ×   10 8 4.864.0216   ×   10 9 5.838.8272   ×   10 12 7.13
752.2488   ×   10 5 3.933.9720   ×   10 8 4.892.6872   ×   10 9 5.845.4370   ×   10 12 7.02
801.7449   ×   10 5 3.932.8855   ×   10 8 4.951.8417   ×   10 9 5.853.4998   ×   10 12 6.82
Table 6. The maximum error | | u 8 ( x ˜ j ) U 8 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of Q 8 , p + 1 for problem (39) on uniform meshes.
Table 6. The maximum error | | u 8 ( x ˜ j ) U 8 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of Q 8 , p + 1 for problem (39) on uniform meshes.
p = 2 p = 3 p = 4 p = 5
N | | e 8 ( x ˜ j ) | | Rate | | e 8 ( x ˜ j ) | | Rate | | e 8 ( x ˜ j ) | | Rate | | e 8 ( x ˜ j ) | | Rate
606.1027   ×   10 5 3.7466   ×   10 7 3.7554   ×   10 8 9.3362   ×   10 11
654.4357   ×   10 5 3.992.5290   ×   10 7 4.912.3550   ×   10 8 5.835.2846   ×   10 11 7.11
703.3004   ×   10 5 3.991.7440   ×   10 7 5.011.5273   ×   10 8 5.843.1868   ×   10 11 6.82
752.5058   ×   10 5 3.991.2363   ×   10 7 4.991.0198   ×   10 8 5.851.9518   ×   10 11 7.10
801.9364   ×   10 5 3.998.9393   ×   10 8 5.026.9847   ×   10 9 5.861.2476   ×   10 11 6.93
Table 7. The maximum error | | u 10 ( x ˜ j ) U 10 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of Q 10 , p + 1 for problem (39) on uniform meshes.
Table 7. The maximum error | | u 10 ( x ˜ j ) U 10 , D G ( x ˜ j ) | | at ( x ˜ j ) the roots of Q 10 , p + 1 for problem (39) on uniform meshes.
p = 2 p = 3 p = 4 p = 5
N | | e 10 ( x ˜ j ) | | Rate | | e 10 ( x ˜ j ) | | Rate | | e 10 ( x ˜ j ) | | Rate | | e 10 ( x ˜ j ) | | Rate
601.1247   ×   10 4 1.2042   ×   10 6 1.1329   ×   10 7 4.4964   ×   10 10
658.1578   ×   10 5 4.018.0998   ×   10 7 4.957.1090   ×   10 8 5.822.6198   ×   10 10 6.75
706.0586   ×   10 5 4.015.6076   ×   10 7 4.964.6127   ×   10 8 5.841.5403   ×   10 10 7.16
754.5924   ×   10 5 4.013.9802   ×   10 7 4.973.0810   ×   10 8 5.859.6233   ×   10 11 6.82
803.5435   ×   10 5 4.012.8874   ×   10 7 4.972.1107   ×   10 8 5.866.0768   ×   10 11 7.12
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Temimi, H. Superconvergence Analysis of Discontinuous Galerkin Methods for Systems of Second-Order Boundary Value Problems. Computation 2023, 11, 228. https://doi.org/10.3390/computation11110228

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Temimi H. Superconvergence Analysis of Discontinuous Galerkin Methods for Systems of Second-Order Boundary Value Problems. Computation. 2023; 11(11):228. https://doi.org/10.3390/computation11110228

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Temimi, Helmi. 2023. "Superconvergence Analysis of Discontinuous Galerkin Methods for Systems of Second-Order Boundary Value Problems" Computation 11, no. 11: 228. https://doi.org/10.3390/computation11110228

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