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ORIGINAL ARTICLE
24 (
2
); 161-165
doi:
10.1016/j.jksus.2010.08.011

HAM solution of some initial value problems arising in heat radiation equations

Department of Mathematics, Faculty of science Islamic Azad University, Rasht Branch, Iran
Member of Young Researchers Club, Department of Mathematics, Faculty of Science Islamic Azad University, Rasht Branch, Iran

*Corresponding author at: Department of Nanotechnology, Kermanshah University of Technology, Kermanshah, Iran b.ghanbary@yahoo.com (Behzad Ghanbari)

Disclaimer:
This article was originally published by Elsevier and was migrated to Scientific Scholar after the change of Publisher.

Available online 30 August 2010

Abstract

Mathematical modeling of many phenomena, especially in heat transfer, usually leads to a nonlinear equation. Traditional approaches for solving such equations are time consuming and difficult affairs tasks.

In this paper, based on the homotopy analysis method (HAM), a series solution for the problem of unsteady nonlinear convective–radiative equation is obtained.

In HAM, one would be able to control the convergence of approximation series and adjust its convergence region, conveniently. Ability and efficiency of proposed approach are tested via some cases of above mentioned problem.

It is found that homotopy analysis approach provides a greatly accelerated convergence series solution for problem.

Keywords

Homotopy analysis method
Heat transfer
1

1 Introduction

Liao proposed the homotopy analysis method (HAM) in 1992, to get analytic approximations of highly nonlinear equations (Liao, 1992).

Unlike other existing methods, the HAM:

  • Provides us a simple way to ensure the convergence of solution series.

  • Provides great freedom to choose proper base functions.

These advantages point out the method as a powerful and flexible tool in mathematics and engineering, which can be readily distinguished from existing numerically and analytically methods.

This paper is arranged as follows; in Section 2 the basic idea of standard HAM and some its recent optimal modification are reviewed. In Section 3, the implementation of HAM on problem and some comparison discussions are presented. Finally, conclusions are drawn in Section 4.

2

2 Standard HAM and some its optimal modifications

Using the concept of homotopy, Liao (1992) introduced the early form of the homotopy analysis method (HAM) for a given nonlinear differential equation

(1)
N [ u ( x ) ] = 0 , as
(2)
( 1 - p ) L [ U ( x ; p ) - u 0 ( x ) ] = - pN [ U ( x ; p ) ] , p [ 0 , 1 ] .
where L is an auxiliary linear operator and u 0 ( x ) is an initial guess of the solution. It is evident that, at p = 0 and p = 1 , one has U ( x ; 0 ) = u 0 ( x ) and U ( x ; 1 ) = u ( x ) , respectively.

In the view of HAM the solution of original equation is assumed to be as the power series in p as

(3)
u ( x ) = u 0 ( x ) + i = 0 u i ( x ) p i . As proved by Liao (2003), whereas (3) be convergent at p = 1 , its limit must satisfy the original Eq. (1).

Liao introduced more artificial degrees of freedom by using the zeroth-order deformation equation in the following form (Liao, 1997a)

(4)
( 1 - p ) L [ U ( x ; p ) - u 0 ( x ) ] - c 0 pN [ U ( x ; p ) ] = 0 , p [ 0 , 1 ] . Appling recently proposed “ m th-order homotopy-derivative operator” (Liao, 2009) D m ( ϕ ) = 1 m ! m ϕ p m p = 0 . to the both sides of (4), one reads
(5)
L [ u m ( x ) - χ m u m - 1 ( x ) ] = c 0 R m - 1 ( x ) ,
where R m - 1 ( x ) = D m - 1 ( N [ u ( x ; p ) ] ) = 1 ( m - 1 ) ! m - 1 N [ u ( x ; p ) ] p m - 1 p = 0 , and χ m = 1 , m > 1 , 0 , m 1 . In this way, the component solutions of u m , m 1 , are not only dependent upon x but also the auxiliary parameter c 0 .

As it is known, to find a proper convergence-control parameter c 0 , to get a convergent series solution or to get a faster convergent one, there is a classic way of plotting the so-called ‘‘ c 0 -curves” or ‘‘curves for convergence-control parameter”. For example, one can consider the convergence of u ( x ) and u ( x ) of a nonlinear differential equation N [ u ( x ) ] = 0 to find a region say R h so that, each c 0 R h gives a convergent series solution of such kind of quantities. Such a region can be found, although approximately, by plotting the curves of these unknown quantities versus c 0 .

However, it is a pity that curves for convergence-control parameter (i.e. c0-curves) give us only a graphically region and cannot tell us which value of gives the fastest convergent series. Recently in Mehmood et al. (2010), a misinterpreted usage of c0-curves has reported. To find the optimal value for convergence-control parameter c0, an optimal homotopy analysis approach has been presented in Liao (2010).

3

3 Appling method and comparison discussions

In this section some numerical experiments are provided to illustrate the validity of HAM approach described in Section 2.

We consider the problem of unsteady nonlinear convective–radiative equation, which in dimensionless form described as following initial value problem.

(6)
[ 1 + ɛ 1 u ( t ) ] du ( t ) dt + u ( t ) + ɛ 2 u 4 ( t ) = 0 , u ( 0 ) = 1 .

Recently, many authors have taken into consideration of different values of ɛ 1 , ɛ 2 in (6) using different methods, some are discussed in Liao (1997b), Domairry and Nadim (2008), Ganji et al. (2007), Abbasbandy (2006, 2007), Marinca and Herişanu (2008) and Sajid and Hayat (2008).

Considering Eq. (6), we define

(7)
N ( ϕ ) = [ 1 + ɛ 1 ϕ ] d ϕ dt + ϕ + ɛ 2 ϕ 4 , and
(8)
L ( u ) = u + u
as the auxiliary linear and nonlinear operators, respectively.

Subject to the initial condition (6) and linear operator (8), the temperature u ( t ) can be expressed by the following set of base functions { exp ( - kt ) | k > 0 } , as the following series u ( t ) = k = 0 m a m , k exp ( - kt ) .

So, it is evident that initial guess should be as θ 0 ( x ) = e - t .

We first construct the zeroth-order deformation equation defined by

(9)
( 1 - p ) L [ u ( t , p ) - u 0 ( t ) ] = phN [ u ( t , p ) ] .

According to (5) and from initial condition (6), we have

(10)
L [ u m ( t ) - χ m u m - 1 ( t ) ] = hR m ( t ) . subject to initial conditions
(11)
u m ( 0 ) = 0 ,
where R m ( t ) = u m ( x ) + ɛ 1 i = 0 m u i ( t ) u m - i ( t ) + u m ( t ) + ɛ 2 i = 0 m - 1 j = 0 m - 1 - i k = 0 m - 1 - i - j u k ( t ) u m - 1 - i - j - k ( t ) u j ( t ) u i ( t ) .

The corresponding mth-order deformation equation reads u m ( t ) = u m ( t ) + Ce - t . where u m ( t ) is the particular solution of (10) and the constant C are determined by the boundary conditions (11).

To obtain the valid values of c 0 , we have plotted the so-called c 0 -curve of 5th-order HAM approximation of u ( 0 ) for different values of ɛ 2 in cases of ɛ 1 = 1 , ɛ 1 = 2 and ɛ 1 = 3 in Figs. 1–3, respectively.

The c 0 -curves for 5th-order of HAM approximation of u ″ ( 0 ) , for ɛ 1 = 1 and different values of ɛ 2 . Solid line: ɛ 2 = 1 ; dashed line: ɛ 2 = 2 ; dotted line: ɛ 2 = 3 .
Figure 1
The c 0 -curves for 5th-order of HAM approximation of u ( 0 ) , for ɛ 1 = 1 and different values of ɛ 2 . Solid line: ɛ 2 = 1 ; dashed line: ɛ 2 = 2 ; dotted line: ɛ 2 = 3 .
The c 0 -curves for 5th-order of HAM approximation of u ″ ( 0 ) , for ɛ 1 = 2 and different values of ɛ 2 . Solid line: ɛ 2 = 1 ; dashed line: ɛ 2 = 2 ; dotted line: ɛ 2 = 3 .
Figure 2
The c 0 -curves for 5th-order of HAM approximation of u ( 0 ) , for ɛ 1 = 2 and different values of ɛ 2 . Solid line: ɛ 2 = 1 ; dashed line: ɛ 2 = 2 ; dotted line: ɛ 2 = 3 .
The c 0 -curves for 5th-order of HAM approximation of u ″ ( 0 ) , for ɛ 1 = 3 and different values of ɛ 2 . Solid line: ɛ 2 = 1 ; dashed line: ɛ 2 = 2 ; dotted line: ɛ 2 = 3 .
Figure 3
The c 0 -curves for 5th-order of HAM approximation of u ( 0 ) , for ɛ 1 = 3 and different values of ɛ 2 . Solid line: ɛ 2 = 1 ; dashed line: ɛ 2 = 2 ; dotted line: ɛ 2 = 3 .

Comparisons are made between HAM and the homotopy perturbation method, HPM (HAM with c 0 = - 1 ) and numerical results of the fourth order Runge–Kutta method, for some values of ɛ 1 , ɛ 2 are plotted in Figs. 4–6. In Tables 1–3, results of comparisons between evaluated square residual error, similar to what was used in Niu and Wang (2010), as:

(12)
Δ m = Ω N i = 0 m u i ( x ) 2 dx , of different approaches are shown.
Comparison between the results obtained by the different method for ɛ 1 = 2 , ɛ 2 = 3 . Hollow symbols: numerical solution; solid line: present MHAM for h = - 1 / 3 ; dashed line: HPM; dotted line: HAM for h = - 0.8 .
Figure 4
Comparison between the results obtained by the different method for ɛ 1 = 2 , ɛ 2 = 3 . Hollow symbols: numerical solution; solid line: present MHAM for h = - 1 / 3 ; dashed line: HPM; dotted line: HAM for h = - 0.8 .
Comparison between the results obtained by the different method for ɛ 1 = 3 , ɛ 2 = 1 . Hollow symbols: numerical solution; solid line: present MHAM for h = - 1 / 4 ; dashed line: HPM; dotted line: HAM for h = - 0.8 .
Figure 5
Comparison between the results obtained by the different method for ɛ 1 = 3 , ɛ 2 = 1 . Hollow symbols: numerical solution; solid line: present MHAM for h = - 1 / 4 ; dashed line: HPM; dotted line: HAM for h = - 0.8 .
Comparison between the results obtained by the different method for ɛ 1 = 3 , ɛ 2 = 3 . Hollow symbols: numerical solution; solid line: present MHAM for h = - 1 / 4 ; dashed line: HPM; dotted line: HAM for h = - 0.8 .
Figure 6
Comparison between the results obtained by the different method for ɛ 1 = 3 , ɛ 2 = 3 . Hollow symbols: numerical solution; solid line: present MHAM for h = - 1 / 4 ; dashed line: HPM; dotted line: HAM for h = - 0.8 .
Table 1 Comparisons of Δ m of 5th-order solutions of different approaches for ɛ 1 = 1 .
ɛ 2 = 1 ɛ 2 = 2 ɛ 2 = 3
MHAM for h = - 1 / 2 0.00000645794 0.00000225316 0.00185417178
HAM for h = - 0.8 Abbasbandy (2007) 0.00001294614 0.06332372453 4.39671710926
HAM for h = - 0.9 Abbasbandy (2007) 0.00026131005 0.45943918392 270.979958125
HPM (HAM for h = - 1 ) 0.00278084263 2.08587335265 358312.798216
Table 2 Comparisons of Δ m of 5th-order solutions of different approaches for ɛ 1 = 2 .
ɛ 2 = 1 ɛ 2 = 2 ɛ 2 = 3
MHAM for h = - 1 / 3 0.0016937936 0.00043080927 0.00018897928
HAM for h = - 0.8 Abbasbandy (2007) 1.7740609725 0.29707799102 7.73726355555
HAM for h = - 0.9 Abbasbandy (2007) 13.500883632 2.52627773025 24.9031191524
HPM (HAM for h = - 1 ) 86.150467589 18.0667149197 284.907280951
Table 3 Comparisons of Δ m of 5th-order solutions of different approaches for ɛ 1 = 3 .
ɛ 2 = 1 ɛ 2 = 2 ɛ 2 = 3
MHAM for h = - 1 / 4 0.2251073087 0.007103244505 0.00301374746
HAM for h = - 0.8 Abbasbandy (2007) 741.25718288 527.1191196254 140.804634925
HAM for h = - 0.9 Abbasbandy (2007) 9333.2489875 15082.47186259 3983.73926254
HPM (HAM for h = - 1 ) 329295.21567 14603605.62548 314587.045985

From Tables 1–3, it seems that proposed approach gives better approximations than the compared approaches and its results are in good agreement with the exact solution.

Since the results of HPM can be obtained as a special case of HAM when c 0 = - 1 , from Figs. 1–3, it is evident that HPM losses its validity for relatively large values of ɛ 1 .

4

4 Concluding remarks

In this paper a initial value problem in heat transfer has been solved by means of homotopy analysis method are proposed. It is shown that HAM results are in a good agreement with numerical solution of problem. It was shown that homotopy analysis method provides a simple way to control and adjust the convergence regions of solution. It is also pointed out that HPM solutions are not converging in some cases of the understudied problem. Computations are performed by Maple11.

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