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Original article
31 (
4
); 479-484
doi:
10.1016/j.jksus.2017.08.006

Non-polynomial quadratic spline method for solving fourth order singularly perturbed boundary value problems

Department of Mathematics, Jamia Millia Islamia, New Delhi 110025, India
Disclaimer:
This article was originally published by Elsevier and was migrated to Scientific Scholar after the change of Publisher.

Peer review under responsibility of King Saud University.

Abstract

In this paper, a non-polynomial quadratic spline method is described for solving fourth-order boundary value problems whose highest-order derivative is multiplied by a small perturbation parameter. This method is applied directly to the solution of the problem without reducing the order of the problem. Convergence analysis of the fourth order method is discussed. To illustrate the efficiency of the method, a boundary value problem is considered with different type of boundary conditions and obtained numerical results are compared with the existing methods.

Keywords

Fourth order singularly perturbed boundary value problems
Non-polynomial quadratic spline
Convergence analysis
1

1 Introduction

Fourth order singularly perturbed boundary value problems occur frequently in many areas of applied sciences such as solid mechanics, Newtonian fluid mechanics, chemical reactor theory, aerodynamics, hydrodynamics, optimal control, convection diffusion processes, quantum mechanics, etc. These problems have various important applications in fluid dynamics. Ghasemi et al. (2014) gave the analysis of electrohydrodynamic flow in a circular cylindrical conduit using least square method and Hatami and Domairry (2014) investigated the transient vertically motion of a soluble particle in a Newtonian fluid media. Hatami and Ganji (2014) studied the motion of a spherical particle in a fluid forced vortex by DQM and DTM. Hatami et al. (2016) gave the optimization of a circular-wavy cavity filled by nanofluid under the natural convection heat transfer condition. Nadeem and Haq (2014) studied the effect of thermal radiation for megnetohydrodynamic boundary layer flow of a nanofluid past a stretching sheet with convective boundary conditions. Sheikholeslami and Ganji investigated the nanofluid flow and heat transfer between parallel plates considering Brownian motion using DTM in Sheikholeslami and Ganji (2015). Sheikholeslami et al. (2013) gave investigation of squeezing unsteady nanofluid flow using ADM. Sheikholeslami et al. (2012) discussed analytical investigation of Jeffery-Hamel flow with high magnetic field and nanoparticle by Adomian Decomposition Method. Sheikholeslami et al. (2012) investigated the laminar viscous flow in a semi-porous channel in the presence of uniform magnetic field using Optimal Homotopy Asymptotic Method. Zhou et al. (2016) designed the microchannel heat sink with wavy channel and its time-efficient optimization with combined RSM and FVM methods.

Singularly perturbed problems are classified on the fact that how the order of the differential equation is affected if 0 , here is a small positive parameter multiplying the highest order derivative of the differential equation. The solution of singularly perturbed boundary value problem has a multiscale character; that is, there are thin transition layers where the solution varies rapidly, while away from the layers the solution varies very slowly.

In this paper, we develop a computational method to solve fourth order singularly perturbed boundary value problems of the form:

(1)
- y ( 4 ) ( x ) + p ( x ) y ( x ) = q ( x ) , a < x < b subject to the boundary conditions
(2)
Case ( i ) y ( a ) = α 1 , y ( b ) = β 1 , y ( 2 ) ( a ) = α 2 , y ( 2 ) ( b ) = β 2

OR

(3)
Case ( ii ) y ( a ) = α 1 , y ( b ) = β 1 , y ( 1 ) ( a ) = α 2 , y ( 1 ) ( b ) = β 2 where p and q are sufficiently continuously differentiable functions in the interval [ a , b ] , α i s and β i s are real constants and is a small positive parameter.

In literature, we found many numerical methods which were developed for solving second order singularly perturbed BVPs. These methods are exponentially fitted finite difference scheme (Kadalbajoo and Kumar, 2009), non-polynomial spline method (Tirmizi, 2008), cubic spline method (Kumar et al., 2007) and quintic spline method (Rashidinia et al., 2010) etc. There are few methods available for solving higher order singularly perturbed BVPs such as asymptotic finite element method (Babu and Ramanujam, 2007), reproducing kernel method (Akram and Rehman, 2012). Shanthi and Ramanujam (Shanthi and Ramanujam, 2002) solved singularly perturbed fourth-order ordinary differential equations of convection–diffusion type using asymptotic numerical methods. The authors in Akram and Amin (2012, 2013) used quintic spline and septic spline respectively for solving fourth order singularly perturbed BVPs.

However, most of these methods were used to solve fourth-order singularly perturbed boundary value problem by using a higher degree spline. Here, we use a non-polynomial quadratic spline method for solving the problem (1). In this paper, we discuss two types of boundary value problems with boundary conditions (2) and (3). Firstly a numerical system is obtained by using non-polynomial quadratic spline. Then finite difference formula of O ( h 2 ) is used for making the system consistent with the given boundary value problem. Finally the obtained scheme is used to solve fourth order singularly perturbed boundary value problems. After implementation of the problem over the method we get a system of pentadiagonal matrix which is solved by using LU decomposition method. The paper describing a non-polynomial quadratic spline method is organized into five sections. Section 2 gives a brief derivation of the method, along with boundary conditions. In Section 3 truncation error has been obtained for fourth order method. Application of the method for solving fourth order singularly perturbed BVPs is discussed in Section 4. Convergence analysis of the method is discussed in Section 5. In Section 6, numerical examples and their comparison with the existing methods are presented which demonstrate the efficiency of our method. Conclusion and the figures are presented in Section 7 also proves the accuracy.

2

2 Derivation of the scheme

Let a = x 0 < x 1 < x 2 < · · · < x n + 1 = b , we first divide the interval [a,b] into n + 1 equal parts by introducing x i = a + ih , i = 0 , 1 , , n + 1 and h = ( b - a ) / ( n + 1 )

Let

(4)
Q i ( x ) = a i sin τ ( x - x i ) + b i e τ ( x - x i ) + c i be a non-polynomial quadratic spline Q i is defined on [a, b] which interpolates the uniform mesh points x i depends on a parameter τ , reduces to an ordinary quadratic spline in [a,b] as τ 0 and τ > 0 .

To determine the coefficients a i , b i and c i , we define the following interpolatory conditions as

(5)
Q i ( x i ) = y i , Q i ( x i + 1 ) = y i + 1 , Q i ( 2 ) ( x i ) = 1 2 ( D i + D i + 1 ) , i = 0 , 1 , , n

By using above conditions we calculated the coefficients as a i = y i + 1 - y i sin θ + ( 1 - e θ ) 2 τ 2 sin θ ( D i + D i + 1 ) b i = 1 2 τ 2 ( D i + D i + 1 ) c i = y i - 1 2 τ 2 ( D i + D i + 1 ) where, θ = τ h

Using the continuity of first derivative, Q i - 1 m ( x i ) = Q i m ( x i ) , m = 1 the following consistency relation is derived

(6)
α 1 D i - 1 + β D i + α 2 D i + 1 = 1 h 2 ( γ y i - 1 + δ y i + y i + 1 ) , i = 1 , 2 , , n where, α 1 = ( 1 - e θ ) cos θ + e θ sin θ 2 θ 2 β = ( - 1 + e θ ) ( 1 - cos θ ) + ( - 1 + e θ ) sin θ 2 θ 2 α 2 = - 1 + e θ - sin θ 2 θ 2 γ = cos θ δ = - 1 - cos θ
Remark:

Our method reduces to Al-Said (2008) based on quadratic spline when

(7)
( α 1 , β , α 2 ) = 1 4 , 1 2 , 1 4 .

For making the system consistent with the given boundary conditions, we use finite difference formula of O ( h 2 )

(8)
D i - 1 - 2 D i + D i + 1 = h 2 y i ( 4 ) + O ( h 4 ) , i = 1 , 2 , , n

Using (6) and (8), we obtained the following relation γ y i - 2 + ( δ - 2 γ ) y i - 1 + ( 1 - 2 δ + γ ) y i + ( - 2 + δ ) y i + 1 + y i + 2 = h 4 ( α 1 y i - 1 ( 4 ) + β y i ( 4 ) + α 2 y i + 1 ( 4 ) )

(9)
i = 2 , 3 , , n - 1

Eq. (9) form a system of n - 2 linear equations in n unknowns y i , i = 1 , 2 , , n . Thus, we need two more equations, one at each end of the range of integration.

For case (i), the equations are obtained as

(10)
5 y 1 - 4 y 2 + y 3 = 2 y 0 - h 2 y 0 ( 2 ) + h 4 7 90 u 0 ( 4 ) + 49 72 u 1 ( 4 ) + 7 45 u 2 ( 4 ) + 1 360 u 3 ( 4 ) + t 1
(11)
y n - 2 - 4 y n - 1 + 5 y n = 2 y n + 1 - h 2 y n + 1 ( 2 ) + h 4 1 360 u n - 2 ( 4 ) + 7 45 u n - 1 ( 4 ) + 49 72 u n ( 4 ) + 7 90 u n + 1 ( 4 ) + t n

For case (ii), the equations are obtained as

(12)
9 y 1 - 9 2 y 2 + y 3 = 11 2 y 0 - 3 hy 0 ( 1 ) + h 4 8 280 u 0 ( 4 ) + 151 280 u 1 ( 4 ) + 52 280 u 2 ( 4 ) - 1 280 u 3 ( 4 ) + t 1
(13)
y n - 2 - 9 2 y n - 1 + 9 y n = 11 2 y n + 1 - 3 hy n + 1 ( 1 ) + h 4 - 1 280 u n - 2 ( 4 ) + 52 280 u n - 1 ( 4 ) + 151 280 u n ( 4 ) + 8 280 u n + 1 ( 4 ) + t n
where, t 1 and t n are of O ( h 4 ) .

3

3 Truncation error

Expanding (9) by using Taylor series, we obtained the following truncation error

(14)
t i = h 2 ( 1 + γ + δ ) y i ( 2 ) + h 3 ( 1 - γ ) y i ( 3 ) + h 4 14 + 14 γ + 2 δ 4 ! - ( α 1 + α 2 + β ) y i ( 4 ) + h 5 1 - γ 4 - ( - α 1 + α 2 ) y i ( 5 ) + h 6 62 + 62 γ + 2 δ 6 ! - α 1 + α 2 2 ! y i ( 6 ) + h 7 1 - γ 40 - α 2 - α 1 3 ! y i ( 7 ) + h 8 254 + 254 + γ + 2 δ 8 ! - α 1 + α 2 4 ! y i ( 8 ) + h 9 17 - 17 γ 12096 - α 2 - α 1 5 ! y i ( 9 ) + O ( h 10 ) , i = 2 , 3 , n - 1

For different values of parameters, we get the method of second order as well as fourth order. Here we discuss only fourth order method. The local truncation error for (10) and (11) is t i = - 20162 / 3 8 ! h 8 y i ( 8 ) + O ( h 9 ) , i = 1 5904 / 133 8 ! h 8 y i ( 8 ) + O ( h 9 ) , i = n and the local truncation error for (12) and (13) is t i = - 6554 8 ! h 8 y i ( 8 ) + O ( h 9 ) , i = 1 211 8 ! h 8 y i ( 8 ) + O ( h 9 ) , i = n

For ( α 1 , β , α 2 , γ , δ ) = 1 6 , 1 3 , 1 6 , 1 , - 2 the truncation error is t i = - 1 720 h 8 y i ( 8 ) + O ( h 9 ) , i = 2 , 3 , , n - 1

4

4 Application to the fourth order singularly perturbed boundary value problems

We consider a fourth order singularly perturbed boundary value problem of the form - y ( 4 ) ( x ) + p ( x ) y ( x ) = q ( x ) , a < x < b subject to the boundary conditions y ( a ) = α 1 , y ( b ) = β 1 y ( 2 ) ( a ) = α 2 , y ( 2 ) ( b ) = β 2

OR y ( a ) = α 1 , y ( b ) = β 1 y ( 1 ) ( a ) = α 2 , y ( 1 ) ( b ) = β 2 where p , q are sufficiently continuously differentiable functions in the interval [ a , b ] , α i and β i are real constants.

After applying the scheme (9) to the problem (1) with boundary conditions (2) and (3), we get the following relation

(15)
Ay i - 2 + By i - 1 + Cy i + Dy i + 1 + Ey i + 2 = - h 4 ( α 1 q i - 1 + β q i + α 2 q i + 1 ) , i = 2 , 3 , , n - 1 where, A = γ B = ( δ - 2 γ ) - h 4 α 1 p i - 1 C = ( 1 - 2 δ + γ ) - h 4 β p i D = ( - 2 + δ ) - h 4 α 2 p i + 1 E =

Eqs. (10) and (11) takes the form A 1 y 1 + A 2 y 2 + A 3 y 3 = A 0 y 0 - h 2 y 0 ( 2 ) - h 4 7 90 q 0 + 49 72 q 1 + 7 45 q 2 + 1 360 q 3 C n - 2 y n - 2 + C n - 1 y n - 1 + C n y n = C n + 1 y n + 1 - h 2 y n + 1 ( 2 ) - h 4 7 90 q n + 1 + 49 72 q n + 7 45 q n - 1 + 1 360 q n - 2 where, A 0 = 2 - 7 9 h 4 p 0 , A 1 = 5 - 49 72 h 4 p 1 , A 2 = - 4 - 7 45 h 4 p 2 , A 3 = - 1 360 h 4 p 3 C n - 2 = 5 - 49 72 h 4 p n - 2 , C n - 1 = - 4 - 7 45 h 4 p n - 1 , C n = - 1 360 h 4 p n , C n + 1 = 2 - 7 90 h 4 p n + 1

Eqs. (12) and (13) takes the form A 1 y 1 + A 2 y 2 + A 3 y 3 = A 0 y 0 - 3 hy 0 ( 1 ) - h 4 8 280 q 0 + 151 280 q 1 + 52 280 q 2 - 1 280 q 3 C n - 2 y n - 2 + C n - 1 y n - 1 + C n y n = C n + 1 y n + 1 - 3 hy n + 1 ( 1 ) - h 4 8 280 q n + 1 + 151 280 q n + 52 280 q n - 1 - 1 280 q n - 2 where, A 0 = 11 2 - 8 280 h 4 p 0 , A 1 = 9 - 151 280 h 4 p 1 , A 2 = - 9 2 - 52 280 h 4 p 2 , A 3 = + 1 280 h 4 p 3 C n - 2 = 9 - 151 280 h 4 p n - 2 , C n - 1 = - 9 2 - 52 280 h 4 p n - 1 , C n = + 1 280 h 4 p n , C n + 1 = 11 2 - 8 280 h 4 p n + 1

5

5 Convergence analysis

The developed method leads to the following matrix form

(16)
PY = C where, P = A 1 A 2 A 3 B C D E A B C D E A B C D E A B C D C n - 2 C n - 1 C n

Y = [ y 1 , y 2 , , y n - 1 ] T and the right hand side vector is C = [ c 1 , c 2 , , c n - 1 ] T .

For Case (i), we have c 1 = A 0 y 0 - h 2 y 0 ( 2 ) - h 4 7 90 q 0 + 49 72 q 1 + 7 45 q 2 + 1 360 q 3 c 2 = - A y 0 - h 4 ( α 1 q 1 + β q 2 + α 2 q 3 ) c i = - h 4 ( α 1 q i - 1 + β q i + α 2 q i + 1 ) , i = 3 , 4 , , n - 1 c n = C n + 1 y n + 1 - h 2 y n + 1 ( 2 ) - h 4 7 90 q n + 1 + 49 72 q n + 7 45 q n - 1 + 1 360 q n - 2

For Case (ii),we have c 1 = A 0 y 0 - 3 h y 0 ( 1 ) - h 4 8 280 q 0 + 151 280 q 1 + 52 280 q 2 - 1 280 q 3 c 2 = - A y 0 - h 4 ( α 1 q 1 + β q 2 + α 2 q 3 ) c i = - h 4 ( α 1 q i - 1 + β q i + α 2 q i + 1 ) , i = 3 , 4 , , n - 1 c n = C n + 1 y n + 1 - 3 h y n + 1 ( 1 ) - h 4 8 280 q n + 1 + 151 280 q n + 52 280 q n - 1 - 1 280 q n - 2

Also we have,

(17)
P Y ̃ = C + T where Y = [ y ̃ ( x 1 ) , y ̃ ( x 2 ) , , y ̃ ( x n - 1 ) ] T be the exact solution and T = [ T 1 , T 2 , , T n - 1 ] T be the local truncation error.

From (16) and (17) we have P ( Y - Y ) = T PE = T E = Y - Y = [ e 1 , e 2 , , e n - 1 ] T

Definition:

A pentadiagonal matrix P = ( p i , j ) , where p i , j = 0 for | i - j | > 2 , is irreducible iff p i , i - 1 0 , i = 2 ,3, , n p i , i - 2 0 , i = 3 ,4, , n p i , i + 1 0 , i = 1 ,2, , n - 1 a n d p i , i + 2 0 , i = 1 ,2, , n - 1

Now we have to calculate sum of each row of matrix P:

For case (i), S 1 = 2 - 49 72 h 4 p 1 - 7 45 h 4 p 2 - 1 360 h 4 p 3 S 2 = - γ - h 4 α 1 p 1 - h 4 β p 2 - h 4 α 2 p 3 S i = - h 4 α 1 p i - 1 - h 4 β p i - h 4 α 2 p i + 1 , i = 3 , , n - 1 S n = 2 - 49 72 h 4 p n - 2 - 7 45 h 4 p n - 1 - 1 360 h 4 p n

For case (ii), S 1 = 11 2 - 151 280 h 4 p 1 - 52 280 h 4 p 2 + 1 280 h 4 p 3 S 2 = - γ - h 4 α 1 p 1 - h 4 β p 2 - h 4 α 2 p 3 S i = - h 4 α 1 p i - 1 - h 4 β p i - h 4 α 2 p i + 1 , i = 3 , , n - 1 S n = 11 2 - 151 280 h 4 p n - 2 - 52 280 h 4 p n - 1 + 1 280 h 4 p n

Let 0 < M Z + is the minimum of | p i - 1 | , | p i | , | p i + 1 | . For sufficiently small h we can say that:

For case (i), S i 151 180 h 4 M , i = 1 ( α 1 + β + α 2 ) h 4 M , i = 2 ( α 1 + β + α 2 ) h 4 M , i = 3 , , n - 1 151 180 h 4 M , i = n

For case (ii), S i 51 70 h 4 M , i = 1 ( α 1 + β + α 2 ) h 4 M , i = 2 ( α 1 + β + α 2 ) h 4 M , i = 3 , , n - 1 51 70 h 4 M , i = n

Further,we get for case (i) 1 S i 180 151 h 4 M , i = 1 , n 1 ( α 1 + β + α 2 ) h 4 M , i = 2 , 3 , , n - 1

For sufficiently small h, we can easily show that the matrix P is irreducible and monotone. Therefore, P - 1 exist and P - 1 0 . Hence,

(18)
E = P - 1 T and let P - 1 = ( p i , j ) , then by theory of matrices Varga (1962), we get
(19)
i = 1 n - 1 p i , j S i = 1 , j = 1 , , n

Therefore, p i , j 1 S i P - 1 = max 1 i n j = 1 n | p i , j | i = 1 n 1 S i = 1 h 4 M 360 151 + 2 α 1 + β + α 2 , i = 1 , , n and T i = max 1 i n i = 1 n | T i | and error is given by:

For case (i), E = P - 1 T 1 h 4 M 360 151 + 2 α 1 + β + α 2 T

Similarly for Case (ii), the error is given by E = P - 1 T 1 h 4 M 140 51 + 2 α 1 + β + α 2 T

By using (14), we have truncation error T = O ( h 8 ) , then we get E 1 h 4 M 360 151 + 2 α 1 + β + α 2 O ( h 8 ) = O ( h 4 )

Hence, the scheme is fourth order convergent. E = O ( h 4 )

Theorem.

The method given by Eq. (9) for solving the given singularly perturbed boundary value problem for sufficiently small h has a fourth order convergence.

6

6 Numerical illustrations

In the present paper, we consider two linear fourth order singularly perturbed boundary value problems whose exact solutions are known. The maximum absolute errors for h = 1/16, 1/32, 1/64 and 1/128 are tabulated in Tables 1 and 2 and comparison are also shown in graphs 1–2. The obtained results are compared with the results of quintic spline method (Akram and Amin, 2012) and septic spline method (Akram and Naheed, 2013).

Example 1

For - 1 x 1 , consider the following differential equation:

(20)
- y ( 4 ) ( x ) + y ( x ) = ( 2 x 4 + cos x - ( 48 + cos x ) ) , y ( - 1 ) = ( 2 + cos 1 ) , y ( 1 ) = ( 24 - cos 1 ) y ( 2 ) ( - 1 ) = ( 2 + cos 1 ) , y ( 2 ) ( 1 ) = ( 24 - cos 1 ) The analytical solution of the problem (20) is y ( x ) = ( 2 x 4 + cos x ) . Maximum absolute errors for Example 1 are given in Table 1. For the sake of comparison we are reported results of Akram and Amin (2012) in Table 1.

Example 2

For x [ 0 , 1 ] , consider the following differential equation:

(21)
- y ( 4 ) ( x ) + y ( x ) = f ( x ) where f ( x ) = ( x - 1 ) 4 x 8 sin ( x ) - x 4 ( - 16 3 ( x - 1 ) 3 x 3 ( 3 x - 2 ) cos ( x ) + 96 x ( 14 - 84 x + 180 x 2 - 165 x 3 + 55 x 4 ) cos ( x ) + 4 ( x - 1 ) 4 x 4 sin ( x ) - 24 2 ( x - 1 ) 2 x 2 ( 14 - 44 x + 33 x 2 ) sin ( x ) + 24 ( 70 - 504 x + 1260 x 2 - 1320 x 3 + 495 x 4 ) sin ( x ) ) and y ( 0 ) = 0 , y ( 1 ) = 0 , y ( 1 ) ( 0 ) = 0 , y ( 1 ) ( 1 ) = 0 , The analytical solution of (21) is y ( x ) = x 8 ( 1 - x ) 4 sin ( x ) .

Maximum absolute errors for Example 2 are given in Table 2. For the sake of comparison we are also reported results of Akram and Amin (2012) and Akram and Naheed (2013) in the Table 2.

Table 1 Maximum absolute error for Example 1.
h = 1 / 16 h = 1 / 32 h = 1 / 64 h = 1 / 128
Our method 1 / 16 2.6309 × 10 - 9 1.5786 × 10 - 10 1.8007 × 10 - 11 1.2579 × 10 - 10
Akram and Amin (2012) 2.3722 × 10 - 6 5.9529 × 10 - 7 1.4896 × 10 - 7 3.7214 × 10 - 8
Our method 1 / 32 5.0874 × 10 - 10 3.0216 × 10 - 11 3.8255 × 10 - 13 2.4353 × 10 - 11
Akram and Amin (2012) 4.5647 × 10 - 7 1.1462 × 10 - 7 2.8684 × 10 - 8 7.1730 × 10 - 9
Our method 1 / 64 1.1660 × 10 - 10 6.926 × 10 - 12 7.7907 × 10 - 13 6.1730 × 10 - 12
Akram and Amin (2012) 1.0356 × 10 - 7 2.6027 × 10 - 8 6.514 × 10 - 9 1.6304 × 10 - 9
Table 2 Maximum absolute error for Example 2.
h = 1 / 16 h = 1 / 32 h = 1 / 64 h = 1 / 128
Our method 1 / 16 1.0499 × 10 - 7 9.8529 × 10 - 9 7.0265 × 10 - 10 4.6045 × 10 - 11
Akram and Amin (2012) - 1 . 315 × 10 - 6 1 . 617 × 10 - 7 2 . 853 × 10 - 8 6.682 ×  10(-9)
Akram and Naheed (2013) 1.666 × 10 - 6 1.310 × 10 - 7 2.614 × 10 - 9 6.716 × 10 - 11
Our method 1 / 32 5.3745 × 10 - 8 5.0610 × 10 - 9 3.6108 × 10 - 10 2.3663 × 10 - 11
Akram and Amin (2012) 6.703 × 10 - 7 8.170 × 10 - 8 1.434 × 10 - 8 3.355 × 10 - 9
Akram and Naheed (2013) 8.537 × 10 - 7 6.736 × 10 - 8 1.344 × 10 - 9 3.452 × 10 - 11
Our method 1 / 64 2.8376 × 10 - 8 2.6766 × 10 - 9 1.9132 × 10 - 10 1.2538 × 10 - 11
Akram and Amin (2012) 3.489 × 10 - 7 4.177 × 10 - 8 7.249 × 10 - 9 1.692 × 10 - 9
Akram and Naheed (2013) 4.520 × 10 - 7 3.569 × 10 - 8 7.128 × 10 - 10 1.829 × 10 - 11
Our method 1 / 128 1.6215 × 10 - 8 1.5345 × 10 - 9 1.0968 × 10 - 10 7.1910 × 10 - 12
Akram and Amin (2012) 1.195 × 10 - 7 2.201 × 10 - 8 3.717 × 10 - 9 8.619 × 10 - 10
Akram and Naheed (2013) 2.60 × 10 - 7 2.049 × 10 - 8 4.092 × 10 - 10 1.05 × 10 - 11

7

7 Conclusion

Non-polynomial quadratic spline method is developed for the approximate solution of fourth order singularly perturbed boundary value problems with two types of boundary conditions. Convergence analysis of the method proved that our scheme (9) is fourth order convergent. A lower degree non-polynomial quadratic spline is used in this paper. However, in previous papers higher degree quintic and septic splines were used. This method is also applicable to solve linear boundary value problems as 1 . Maximum absolute errors in Tables 1 and 2 shows that our method is better than existing methods. Graphs between exact and approximate solutions for the Examples 1 and 2 are shown in Fig. 1 and 2 respectively which also shows the superiority of our method.

Graph of the exact solution versus the approximate solution for N = 64 for Example 1.
Fig. 1
Graph of the exact solution versus the approximate solution for N = 64 for Example 1.
Graph of the exact solution versus the approximate solution for N = 64 for Example 2.
Fig. 2
Graph of the exact solution versus the approximate solution for N = 64 for Example 2.

Acknowledgement

The second author is thankful to UGC for providing MANJRF. The authors are also thankful to the referees for useful suggestions which improve the quality of the paper.

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