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Variational iteration and homotopy perturbation method for

solving Lorenz system

Mehmet MERDAN*

Karadeniz Technical University, Engineering Faculty of Gümüşhane, Civil Engineering, 29000, Gümüşhane, Turkey

Abstract

In this paper, homotopy perturbation method and variational iteration method are implemented to give approximate and analytical solutions of nonlinear ordinary differential equation systems such as Lorenz system. Homotopy perturbation is compared the variational iteration method for Lorenz system. The variational iteration method is predominant than the other non-linear methods, such as perturbation method. The main property of the VIM method is in its flexibility and ability to solve nonlinear equations accurately and conveniently. In this method, in general Lagrange multipliers are constructed by correction functionals for the systems. Multipliers can be identified by the variational theory. Some plots are presented to compare of the VIM and HPM.

Keywords: Variational iteration method; Homotopy perturbation method; Lorenz

system

Özet

Bu çalışmada, Lorenz sistemi gibi lineer olmayan adi diferensiyel denklem sistemlerinin yaklaşık analitik çözümlerini elde edebilmek için homotopy perturbation ve varyasyonel iterasyon yöntemleri uygulandı. Homotopy perturbation yöntemi varyasyonel iterasyon yöntemi ile mukayese edildi. Varyasyonel iterasyon yöntemi perturbation yöntemi olarak bilinen diğer non lineer yöntemlerden daha üstündür. VIM yönteminin temel özelliği lineer olmayan denklemleri doğru ve uygun çözebilecek esneklikte olmasıdır. Bu yöntemde genelde Lagrange çarpanları sistemler için düzeltme fonksiyoneli ile elde edildi. Çarpanlar varyasyonel teori ile belirlendi. VIM ve HPM yöntemlerini karşılaştırmak için bir kaç tane grafik sunuldu.

Anahtar kelimeler: Varyasyonel iterasyon yöntemi, Homotopy perturbation yöntemi;

Lorenz sistemi

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1. Introduction

Dynamics of chaotic dynamical systems as Lorenz system is examined at the study [2]. The components of the basic tree-component model are proportional to the convective velocity, the temperature difference between descending and ascending flows, and the mean convective heat flow is denoted respectively by x t y t( ), ( ) and (t)z .These quantities satisfy ( ) -dx s y x dt dy rx y xz dt dz xy bz dt=    = − −    =  (1)

with the initial conditions:

1 2 3

(0) , (0) , (0) .

x =M y =M z =M

,

s b and the so-called bifurcation parameter r are real constants.. Throughout this paper, we set s=10,b=8 / 3 and vary the parameter r. It is well-known that chaos sets in around the critical parameter value r = 20.5 [24, 25].

The motivation of this paper is to extend the application of the analytic homotopy-perturbation method (HPM) and variational iteration method[3,6–14,19,21] to solve the Lorenz system (1). The homotopy perturbation method (HPM) was first proposed by Chinese mathematician He [16–22]. The variational iteration method, which was proposed originally by He [13] in 1999, has been proved by many authors to be a powerful mathematical tool for various kinds of nonlinear problems.

2. Variational iteration method

According to the variational iteration method [10], we consider the following differential equation:

( ),

Lu Nu+ = g x (2)

where L is a linear operator, N is a non-linear operator, and ( )g x is an inhomogeneous term. Then, we can construct acorrect functional as follows:

{

}

1 0 ( ) ( ) ( ) ( ) ( ) , x n n n n u + x =u x +

λ Lu s +Nu s%g s ds (3)

where λ is a general Lagrangian multiplier [9–11], which can be identified optimally via variational theory. The second term on the right is called the correction and u% is n considered as a restricted variation, i.e., δu%n =0.

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3. Homotopy perturbation method

To illustrate the homotopy perturbation method (HPM) for solving non-linear differential equations, He [21, 22] considered the following non-linear differential equation:

( )A u = f r( ), r∈ Ω (4)

subject to the boundary condition

, u 0, B u r n ∂   = ∈ Γ    (5)

where A is a general differential operator, B is a boundary operator, f(r) is a known analytic function, Γ is the boundary of the domain Ω and

n

∂ denotes differentiation along the normal vector drawn outwards from Ω . The operator A can generally be divided into two parts M and N. Therefore, (3) can be rewritten as follows:

( )M u +N u( )= f r( ), r∈ Ω (6)

He [22,23] constructed a homotopy v r p( , ) :Ωx

[ ]

0, 1 → ℜ which satisfies

[

0

] [

]

( , ) (1 ) ( ) ( ) ( ) ( ) 0, H v p = − p M vM u + p A vf r = (7) which is equivalent to

[

]

0 0 ( , ) ( ) ( ) ( ) ( ) ( ) 0, H v p =M vM u + pM v + p N vf r = (8)

where p

[ ]

0, 1 is an embedding parameter, and u0 is an initial approximation of (4). Obviously, we have

0

( ,0) ( ) ( ) 0, ( ,1) ( ) ( ) 0.

H v =M vM u = H v = A vf r = (9)

The changing process of p from zero to unity is just that of H(v,p) from

0

( ) ( ) to ( ) ( )

M vM v A vf r . In topology, this is called deformation and

0

( ) ( ) and ( ) ( )

M vM v A vf r are called homotopic. According to the homotopy perturbation method, the parameter p is used as a small parameter, and the solution of Eq. (7) can be expressed as a series in p in the form

2 3

0 1 2 3 ...

v v= + pv + p v + p v + (10)

When 1p→ , Eq. (7) corresponds to the original one, Eqs. (6) and (10) become the approximate solution of Eq. (6), i.e.,

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0 1 2 3 1 lim ... p u v v v v v → = = + + + + (11)

The convergence of the series in Eq. (11) is discussed by He in [21, 22].

4. Applications

In this section, we will apply the homotopy perturbation method to nonlinear ordinary differential systems (1).

4.1 Homotopy perturbation method to Lorenz system

According to homotopy perturbation method, we derive a correct functional as follows:

(

)(

)

(

(

)

)

(

)(

)

(

)

(

)(

)

(

)

1 0 1 1 2 2 0 2 1 2 1 3 3 0 3 1 2 3 1 0, 1 0, 1 0, p v x p v s v v p v y p v rv v v v p v z p v v v bv − − + + − = − − + − + + = − − + − + =

& & & & & &

& &

(12)

where “dot” denotes differentiation with respect to t , and the initial approximations are as follows: 1,0 0 1 2,0 0 2 3,0 0 3 ( ) ( ) (0) , ( ) ( ) (0) , ( ) ( ) (0) . v t x t x M v t y t y M v t z t z M = = = = = = = = = (13) And 2 3 1 1,0 1,1 1,2 1,3 2 3 2 2,0 2,1 2,2 2,3 2 3 3 3,0 3,1 3,2 3,3 ..., ..., ..., v v pv p v p v v v pv p v p v v v pv p v p v = + + + + = + + + + = + + + + (14)

where vi j, , ,i j=1, 2,3,...are functions yet to be determined. Substituting Eqs.(13) and (14) into Eq. (12) and arranging the coefficients of “p” powers, we have

(

) (

)

(

)

(

) (

)

(

)

(

)

2 3 1,1 1 2 1,2 1,1 2,1 1,3 1,2 2,2 2 2,1 1 2 1 3 2,2 1,1 2,1 1 3,1 3 1,1 3 2,3 1,2 2,2 1 3,2 3 1,2 1,1 3,1 3,1 1 2 3 3,2 1 2,1 2 ( ) ( ) ( ) ... 0, ... 0, v s M M p v s v v p v s v v p v rM M M M p v rv v M v M v p v rv v M v M v v v p v M M bM p v M v M + − + + − + + − + = − + + + − + + + + − + + + + + = − + + − −

& & &

& & & &

(

&

)

(

)

2 1,1 3,1 3 3,3 1 2,2 2 1,2 1,1 2,1 3,2 ... 0, v bv p v M v M v v v bv p + + & − − − + + = (15)

In order to obtain the unknowns vi j, ( ), ,t i j=1, 2,3, we must construct and solve the following system which includes nine equations with nine unknowns, considering the initial conditions

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, (0) 0, , 1, 2,3, i j v = i j= 1,1 1 2 1,2 1,1 2,1 1,3 1,2 2,2 2,1 1 2 1 3 2,2 1,1 2,1 1 3,1 3 1,1 2,3 1,2 2,2 1 3,2 3 1,2 1,1 3,1 3,1 1 2 3 3,2 1 2,1 2 1,1 3,1 ( ) 0, ( ) 0, ( ) 0, 0, 0, 0, 0, 0, v s M M v s v v v s v v v rM M M M v rv v M v M v v rv v M v M v v v v M M bM v M v M v bv + − = + − = + − = − + + = − + + + = − + + + + = − + = − − + = & & & & & & & & &3,3 1 2,2 2 1,2 1,1 2,1 3,2 0. vM vM vv v +bv = (16)

From Eq. (11), if the three terms approximations are sufficient, we will obtain:

3 1 1, 1 0 3 2 2, 1 0 3 3 3, 1 0 ( ) lim ( ) ( ), ( ) lim ( ) ( ), ( ) lim ( ) ( ), k p k k p k k p k x t v t v t y t v t v t z t v t v t=== = = = = = =

(17) therefore

(

)

[

]

(

) (

)

(

)

(

) (

)

(

)

1 2 1 2 1 2 1 3 2 1 2 1 1 2 1 3 1 1 2 3 3 3 2 1 1 2 1 3 2 1 2 1 2 1 3 2 2 1 1 2 1 3 1 2 1 3 2 3 ( ) 1 - - -2 - -1 + 6 - - -( ) 1 - - - -2 x t M s M M t rM M M M sM sM t rs M M rM M M M M M M bM t sM M M s rM M M M sM sM y t M rM M M M t rsM rsM rM M M M M M bM M sM M s = + − + + − − − −     − − − +     = + − − + + + + +

(

)

(

) (

)

(

) (

)

(

)

(

)

(

)

(

)

2 1 3 1 2 1 3 2 1 2 1 1 2 1 3 2 1 1 2 3 3 2 1 1 2 1 3 1 3 1 2 2 1 3 1 2 1 3 2 1 1 2 3 2 1 3 1 2 3 1 - - - - -( ) - -1 6 - - -2 ( ) ( ) 1 2 M M t rs rM M M M sM sM rs M M rM M M M M M M bM sM M M rM M M M M t M M M M s M rM M M M sM sM s s M M bM M M z t M M M bM t rM     + − − +     + − + − −   +  +        = + − +

(

) (

)

(

)

(

)

(

)(

)

(

)

(

)

2 2 2 2 2 1 2 1 3 1 2 1 2 2 3 1 2 1 1 2 1 3 1 1 2 3 3 2 1 2 1 2 1 3 2 1 3 2 1 1 2 1 3 1 1 2 1 3 2 2 1 1 1 2 3 - - - -- - ( ) - - -1 , 6 2 - - - -( ) M M M M bM M sM M sM b M t rsM M M rM M M M M M M bM M M M s M rM M M M sM sM s t s M M rM M M M bM rM M M M sM M M bM M M bM  + +    − − − −     − − + +   + +    +    (18)

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Here

1 0, 2 1 and 3 0

M = M = M = for the three-component model.

A few first approximations for ( ), ( ) and ( )x t y t z t are calculated and presented below: Three terms approximations:

2 3 2 3 2 3 ( ) 10 - 55. 526.6666667 , ( ) 1- 103 - 410.1666667 , ( ) 5 - 26.11111111 , x t t t t y t t t t z t t t = + = + = (19)

Four terms approximations:

2 3 4 2 3 4 2 3 4 ( ) 10 - 55. 526.6666667 - 2342.083334 , ( ) 1- 103 - 410.1666667 2789.208335 , ( ) 5 - 26.11111111 420.3240740 , x t t t t t y t t t t t z t t t t = + = + + = + (20)

Five terms approximations:

2 3 4 5 2 3 4 5 2 3 4 5 ( ) 10 - 55. 526.6666667 - 2342.083334 10262.58334 , ( ) 1- 103 - 410.1666667 2789.208335 -10053.16112 , ( ) 5 - 26.11111111 420.3240740 - 2751.256172 , x t t t t t t y t t t t t t z t t t t t = + + = + + = + (21)

Six terms approximations:

2 3 4 5 6 2 3 4 5 6 2 3 4 5 ( ) 10 -55. 526.6666667 - 2342.083334 10262.58334 -33859.5741 , ( ) 1- 103 - 410.1666667 2789.208335 -10053.16112 35360.57242 , ( ) 5 - 26.11111111 420.3240740 - 2751.256172 20773.21 x t t t t t t t y t t t t t t t z t t t t t = + + = + + + = + + 108 ,t6 (22)

The results obtained by homotopy perturbation method with three, four, five and six terms approximations for x t y t( ), ( ) and ( )z t are plotted in Figure 1.

In this next section, we will apply the variational iteration method to nonlinear ordinary differential systems (1).

4.2 Variational iteration method to Lorenz system

According to the variational iteration method, we derive a correct functional as follows:

(

)

{

}

{

}

{

}

1 1 0 1 2 0 1 3 0 ( ) ( ) ( ) ( ) ( ) , ( ) ( ) ( ) ( ) ( ) ( ) ( ) , ( ) ( ) ( ) ( ) ( ) ( ) , t n n n n n t n n n n n n n t n n n n n n x t x t x s y x d y t y t y rx y x z d z t z t v x y bz d λ ξ ξ ξ ξ λ ξ ξ ξ ξ ξ ξ λ ξ ξ ξ ξ ξ + + + ′ = + − − ′ = + − + + ′ = + − +

% % % % % % % % % (23)

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where λ λ1, 2 andλ3 are general Lagrange multipliers,

( )

,

( ) ( )

,

( ) ( ) ( )

, and

( )

n n n n n n n

x% ξ x% ξ y% ξ x% ξ z% ξ y% ξ z% ξ denote restricted variations, i.e.

( )

( ) ( )

( ) ( )

( )

( )

0

n n n n n n n

x x y x z y z

δ% ξ =δ % ξ % ξ =δ% ξ % ξ =δ % ξ =δ % ξ =

Making the above correction functionals stationary, we can obtain following stationary conditions:

( )

( )

( )

( )

( )

( )

1 1 2 2 3 3 0, 1 0, 0, 1 0, 0, 1 0, t t t ξ ξ ξ λ ξ λ ξ λ ξ λ ξ λ ξ λ ξ = = = ′ = + = ′ = + = ′ = + = (24)

The Lagrange multipliers, therefore, can be identified as

1 2 3 1.

λ =λ =λ = − (25)

Substituting Eq. (25) into the correction functional Eq. (23) results in the following iteration formula:

(

)

{

}

{

}

{

}

1 0 1 0 1 0 ( ) ( ) ( ) ( ) ( ) , ( ) ( ) ( ) ( ) ( ) ( ) ( ) , ( ) ( ) ( ) ( ) ( ) ( ) , t n n n n n t n n n n n n n t n n n n n n x t x t x s y x d y t y t y rx y x z d z t z t v x y bz d ξ ξ ξ ξ ξ ξ ξ ξ ξ ξ ξ ξ ξ ξ ξ + + + ′ = − − − ′ = − − + + ′ = − − +

(26)

We start with initial approximations x t0( )=M y t1, 0( )=M2 and z t0( )=M3 . By the

above iteration formula, we can obtain a few first terms being calculated:

(

)

(

)

(

)

1 1 2 1 1 2 1 2 1 3 1 3 1 2 3 ( ) , ( ) , ( ) , x t M s M M t y t M rM M M M t z t M M M bM t = + − = + − − = + − (27)

(8)

(

)

(

)

(

)

2 1 2 1 2 2 2 1 2 1 3 2 1 2 2 1 2 1 3 2 2 2 1 1 2 1 3 1 2 1 3 2 3 1 3 2 2 3 2 1 2 3 1 2 1 3 2 3 1 2 3 ( ) - - -( ) - - - - -( ) x t M s M M t rsM sM sM M s M s M t y t M rM M M M t rsM rsM rM M M M M M bM M sM M sM M t sM M bM M sM M sbM M t z t M M M bM t = + −   + + = + − −   + + + + +   + + + = + − 2 2 2 2 2 1 1 2 1 3 1 2 1 2 2 3 2 2 2 3 2 1 2 2 1 3 1 1 2 1 3 - - - - - - , rM M M M M bM M sM M sM b M t srM M sM sM M M srM sM M sM M t   + + +   + + + (28)

Continuing in this manner, we can find the rest of components. A five terms approximation to the solutions are considered

4 4 4 ( ) , ( ) , ( ) . x t x y t y z t z ≈ ≈ ≈ (29)

This was done with the standard parameter values given above and initial values

1 0, 2 1 and 3 0

M = M = M = for the three-component model.

A few first approximations for ( ), ( ) and ( )x t y t z t are calculated and presented below:

1 1 1 ( ) 10 , ( ) 1 , ( ) 0, x t t y t t z t = = − = (30) 2 2 2 2 2 3 2 ( ) 10 -110 , ( ) 1-1 206 , ( ) 10 10 , x t t t y t t t z t t t = = + = − (31) 3 3 3 4 5 6 3 3 4 5 3 ( ) 10 3160 , ( ) 1-1 - 2461 -100 1200 -1100 , ( ) -126.6666667 2196.666667 - 22660 , x t t t y t t t t t t z t t t t = + = + = + (32) 3 2 4 5 6 7 4 3 4 5 6 2 4 7 8 9 3 4 4 ( ) 10 - 6320 -110 - 56210 -1000 12000 -11000 , ( ) 1- 4922 67541 - 3433.333333 -17666.66667 206 627966.6668 - 6941466.668 71605600 , ( ) 243.3333334 - 3092.222223 57012. x t t t t t t t t y t t t t t t t t t t z t t t = + = + + + + + = + 5 2 6 7 8 9 10 22220 10 59426.66667 - 7764760 - 327000 3792000 - 3476000 , t t t t t t t + + + (33)

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3 4 5 6 5 7 8 9 10 15 11 12 5 ( ) 10 15800 281050 1241510 - 84333.33333 - 230666.6667 6389666.668 - 69414666.68 716056000 , ( ) 1. - .2730823200 12 * - .457100047 11* -.4387306540 12* - 26483 x t t t t t t t t t t y t E t E t E t = + + + + + = + + + 13 16 17 14 18 3 4 5 6 7 8 35556.* -.5257700000 11* .8342400000 11* .2846838133 12* - .3823600000 11* - -12305 - 337205 -1207445.999 192155.5555 - 2314433.333 47558800 - 295092033.5 t E t E t E t E t t t t t t t t t + + + + + + + + 9 10 15 11 12 5 13 16 17 14 3 4 2651872121 , ( ) -.1618108334 12* - 727036000.5 - 71037332.39 -.6316975059 11* .9356233333 12* -.7876616000 12* -.4010279376 13* - 633.3333335 4477.777777 t z t E t t t E t E t E t E t t t + = + + + + + + + 5 6 7 8 9 10 - 243132.9629 -1561885.926 - 3707054.443 - 680557713.3 - 3798460943 176579000.0 , t t t t t + t (34)

These results obtained by HPM, three, four ,five and six terms approximations for ( ), ( ) and ( )

x t y t z t are calculated and presented follow. These results are plotted in Figure 1.

0 0.1 0.2 0.3 0.4 -10 0 10 20 30 t time

Three terms approximations x y z 0 0.1 0.2 0.3 0.4 -50 0 50 100 t time

Four terms approximations x y z 0 0.1 0.2 0.3 0.4 -50 0 50 100 t time

Five terms approximations x y z 0 0.1 0.2 0.3 0.4 -100 0 100 200 t time

Six terms approximations x

y z

Figure. 1. Plots of three, four five and six terms HPM approximations for Lorenz system The HPM was tested by comparing the results with the results of the VIM.

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These results are plotted in Figure 2. 0 0.1 0.2 0.3 0.4 -200 0 200 400 t time Third Approximation x y z 0 0.1 0.2 0.3 0.4 -2 -1 0 1 2x 10 4 t time Fourth Approximation x y z 0 0.1 0.2 0.3 0.4 -15 -10 -5 0 5x 10 6 t time Fifth Approximation x y z 0 0.1 0.2 0.3 0.4 -5 0 5x 10 11 t time Sixth Approximation x y z

Figure. 2. Plots of third, fourth, fifth and sixth approximations obtained by VIM for the Lorenz system

5. Conclusions

In this paper, HPM and VIM was used for finding the solutions of nonlinear ordinary differential equation systems such as Lorenz system. VIM is predominant than the other non-linear methods, such as perturbation method. We apply He’s HPM to calculate certain integrals. It is easy and very beneficial tool for calculating certain difficult integrals or in deriving new integration formula. An interesting state about VIM is that with the fewest number of iterations or even in some cases, once, it can converge to correct results. Some plots are presented to compare of the VIM and HPM

The computations associated with the examples in this paper were performed using Maple 7 and Matlab 7

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References

[1] M. Rafei , H. Daniali, D.D. Ganji, “Variational iteration method for solving the epidemic model and the prey and predator problem”, Applied Mathematics and Computation. 186 (2007) 1701–1709

[2] R. Barrio,_, S. Serrano, A three-parametric study of the Lorenz model, Physica D 229 (2007) 43–51

[3] J.H. He, A coupling method of homotopy technique and perturbation technique for nonlinear problems. Int J Non-Linear Mech 2000;35:37–43.

[4] D.W. Jordan, P. Smith, Nonlinear Ordinary Differential Equations, third ed., Oxford University Press, 1999.

[5] J. Biazar, “Solution of the epidemic model by Adomian decomposition method”, Applied Mathematics and Computation 173 (2) (2006) 1101–1106.

[6] MSH. Chowdhury, I. Hashim, Application of homotopy-perturbation method to Klein–Gordon and sine-Gordon equations. Chaos Solitons & Fractals, in press. [7] J.H. He Homotopy perturbation method for solving boundary value problems. Phys

Lett A 2006;350:87–8.

[8] J. Biazar, M. Ilie, A. Khoshkenar,” A new approach to the solution of the prey and predator problem and comparison of the results with the Adomian method”, Applied Mathematics and Computation 171 (1) (2005) 486–491.

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[12] J.H. He, “Approximate solution of nonlinear differential equations with

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[13] J.H. He,” Variational iteration method—a kind of nonlinear analytical technique”: some examples, International Journal of Nonlinear Mechanics 34 (4) (1999) 699–708.

[14] J.H. He, Some asymptotic methods for strongly nonlinear equations, International Journal of Modern Physics B 20 (10) (2006) 1141–1199.

[15] M.A. Abdou, A.A. Soliman, Variational-iteration method for solving Burger’s and coupled Burger’s equations, Journal of Computational and Applied Mathematics 181 (2) (2005) 245–251.

[16] J.H. He, Homotopy perturbation method for solving boundary value problems. Phys Lett A 2006;350:87–8.

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[18] M. Inokuti et al., General use of the Lagrange multiplier in non-linear mathematical physics, in: S. Nemat-Nasser (Ed.), Variational Method in the Mechanics of Solids, Pergamon Press, Oxford, 1978, pp. 156–162.

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[19] J.H. He, Semi-inverse method of establishing generalized principles for fluid mechanics with emphasis on turbomachinery aerodynamics, International Journal of Turbo Jet-Engines 14 (1) (1997) 23–28.

[20] B.A. Finlayson, The Method of Weighted Residuals and Variational Principles, Academic press, New York, 1972.

[21] He JH. Homotopy perturbation technique. Comput Methods Appl Mech Engrg 1999,178,257–62.

[22] He JH. A coupling method of a homotopy technique and a perturbation technique for non-linear problems. Int J Non-linear Mech 2000,35(1),37–43.

[23] E Coskun, M Merdan. Global stability and periodic solution of a viral dynamic model. Journal of Science of science and art faculty,2007,2(2),256-267.

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