the homotopy analysis method for solving the time-fractional fornberg–whitham equation and...
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The homotopy analysis method for solving the time-fractional Fornberg-Whith‐
am equation and comparison with Adomian’s decomposition method
Mehmet Giyas Sakar, Fevzi Erdogan
PII: S0307-904X(13)00254-0
DOI: http://dx.doi.org/10.1016/j.apm.2013.03.074
Reference: APM 9443
To appear in: Appl. Math. Modelling
Please cite this article as: M.G. Sakar, F. Erdogan, The homotopy analysis method for solving the time-fractional
Fornberg-Whitham equation and comparison with Adomian’s decomposition method, Appl. Math. Modelling
(2013), doi: http://dx.doi.org/10.1016/j.apm.2013.03.074
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THE HOMOTOPY ANALYSIS METHOD FOR SOLVING THE
TIME-FRACTIONAL FORNBERG-WHITHAM EQUATION AND
COMPARISON WITH ADOMIAN’S DECOMPOSITION METHOD
M. G. SAKAR, F. ERDOGAN
Abstract. In this paper, we applied relatively new analytical techniques, ho-motopy analysis method (HAM) and Adomian’s decomposition method (ADM)for solving time-fractional Fornberg- Whitham equation. The homotopy anal-
ysis method contains the auxilary parameter, which provides us with a simpleway to adjust and control the convergence region of solution series. The frac-tional derivatives are described in the Caputo sense. A comparison is made
the between HAM and ADM results. The present methods performs extremelywell in terms of efficiency and simplicity. Numerical results for different par-ticular cases of the problem are presented.
1. Introduction
In recent years, there has been a growing interest in the field of fractional cal-culus, i.e. the theory of derivatives and integrals of fractional non-integer order.Considerable interest has been devoted to study of the fractional calculus and theirnumerous applications in the areas of science and engineering. Fractional differ-ential equations are increasingly used to model problems in a number of researchareas including description of fractional random walk, control theory of dynami-cal systems, electrical networks, frequency dependent damping behavior materials,signal processing and system identification, diffusion and reaction processes, creep-ing and relaxation for viscoelastic materials [1,2]. Fractional derivatives providean excellent instrument for the description of memory and hereditary properties ofvarious materials and processes [3].
Most fractional differential equations do not have exact analytic solutions so ap-proximation and numerical methods must be used. A great deal of effort has beenexpended in attempting to find robust and stable numerical and analytical meth-ods for solving fractional differential equations of physical interest. These meth-ods include finite difference method [4-6], Adams-Bashforth-Moulton method [7],Homotopy perturbation method [8-10], Generalized differential transform method[11,12], Variational iteration method [13-15] and Adomian’s decomposition method[16,17]. However, neither perturbation nor non-perturbation method can provideus with a simple way to adjust and control the convergence region and rate of givenseries. Homotopy analysis method (HAM) is proposed 1992 by Liao [18-22]. HAMprovides an effective procedure for explicit, approximate analytical solutions of awide and general class of differential equations. Based on homotopy of topology,
Key words and phrases. Homotopy analysis method, time-fractional Fornberg-Whitham equa-tion, Caputo derivative, Adomian’s decompositon method, Auxiliary parameter.
1
2 M. G. SAKAR, F. ERDOGAN
the validity of the HAM is independent of whether or not there exist small param-eters in the considered equation. Therefore, the HAM can overcome the foregoingrestrictions and limitations of perturbation techniques so that it provides us with apossibility to analyze strongly nonlinear problems [23]. HAM has been successfullyapplied to solve many types of nonlinear problems in science and engineering bymany others [24-28].
We consider linear and nonlinear fractional partial differential equations of theform
Dαt u(x, t) = f(u, ux, ut, uxx, uxxx, uxxt), n − 1 < α ≤ n, t > 0, (1.1)
subject to the initial conditions
u(k)(x, 0) = gk(x), k = 0, 1, 2, ..., n − 1, (1.2)
where n is an integer, f is a linear/nonlinear function, and Dαt (.) = ∂α
∂tα(.) is a
fractional differential operator.The operator form of the nonlinear fractional partial differential equations (1.1)
can be written as follows
Dαt u(x, t) = A(ux, uxxt)+B(u, ux, uxx, uxxx)+C(x, t), n−1 < α ≤ n, t > 0
(1.3)
subject to the initial conditions
u(k)(x, 0) = gk(x), k = 0, 1, 2, ..., n − 1, (1.4)
where A is a linear operator, B is a nonlinear operator and C is a known analyticfunction.
In the present paper, we shall apply HAM and ADM to find the approximate ana-lytical solution of a special case of (1.3)-(1.4) the so-called time-fractional Fornberg-Whitham equation and compare it with the exact solution. This equation can bewritten in operator form as
Dαt u(x, t) = −ux+uxxt+u uxxx−u ux+3uxuxx, t > 0, 0 < α ≤ 1, (1.5)
subject to initial condition
u(x, 0) = e1
2x (1.6)
where u(x, t) is the fluid velocity, α is constant and lies in the interval (0, 1], t isthe time and x is the spatial coordinate.
2. Fractional Calculus
Fractional calculus unifies and generalizes the notions of integer-order differenti-ation and n-fold integration. There exists a vast literature on different definitionsof fractional derivatives. The most popular ones are the Riemann-Liouville and theCaputo derivatives. We have chosen to use the Caputo fractional derivative becauseit allows traditional initial and boundary conditions to be included in the formula-tion of the problem, but for homogeneous initial condition assumption, these twooperators coincide. For more details on the geometric and physical interpretationfor fractional derivatives of both the Riemann-Liouville and Caputo types, see [33].We give some basic definitions and properties of fractional calculus theory whichshall be used in this paper:
3
Definition 2.1. A real function f(x), x > 0, is said to be in the space Cµ,µ ∈ R if there exists a real number p (> µ), such that f(x) = xpf1(x), wheref1(x) ∈ C [0,∞), and it is said to be in the space Cm
µ iff f (m) ∈ Cm, m ∈ N. TheRiemann–Liouville fractional integral operator is defined as follows:
Definition 2.2. The Riemann–Liouville fractional integral operator of orderα ≥ 0, of a function f ∈ Cµ, µ ≥ −1, is defined as
Jαf(x) =1
Γ(α)
x∫
0
(x − t)α−1f(t)dt, α > 0, x > 0,
J0f(x) = f(x).
In this paper only real and positive values of α will be considered.Properties of the operator Jα can be found in [1-3] and we mention only the
following: For f ∈ Cµ, µ ≥ −1, α, β ≥ 0, and γ ≥ −1 :
1. JαJβf(x) = Jα+βf(x),
2. JαJβf(x) = JβJαf(x),
3. Jαxγ = Γ(γ+1)Γ(α+γ+1)x
α+γ .
Lemma 2.1. If m − 1 < α ≤ m, m ∈ N and f ∈ Cmµ , µ ≥ −1, then
DαJαf(x) = f(x),
and,
JαDαf(x) = f(x) −m−1∑
i=0
f (i)(0+)xi
i!, x > 0.
Definition 2.3. The fractional derivative of f(x) in Caputo sense is defined as
Dαf(x) = Jm−αDmf(x) = 1Γ(m)
x∫
0
(x − s)m−α−1f (m)(s)ds,
for m − 1 < α ≤ m, m ∈ N, x > 0, f ∈ Cm−1.
Definition 2.4. For m to be the smallest integer that exceeds α, the Caputotime-fractional derivative operator of order α > 0 is defined as
Dαu(x, t) =
1Γ(m−α)
x∫
0
(t − τ)m−α−1 ∂mu(x,t)∂τm
dτ , m − 1 < α < m
∂mu(x,t)∂tm
, α = m ∈ N
3. Basic ideas of Homotopy Analysis method
We consider the following differential equation
N [u (x, t)] = 0, (3.1)
where, N is a nonlinear differential operator, x and t are independent variables,u (x, t) is an unknown function, respectively, By means of generalizing the tradi-tional homotopy method, Liao [18] constructs the so-called zero-order deformation
4 M. G. SAKAR, F. ERDOGAN
equation
(1 − p) L [φ (x, t; p) − u0 (x, t)] = p~H (x, t) N [φ (x, t; p)] , (3.2)
subject to the following initial conditions:
φ(k)(x, 0; p) = gk(x), k = 0, 1, 2, ...,m − 1, (3.3)
where p ∈ [0, 1] is the embedding parameter, ~ 6= 0 is a non-zero auxiliaryparameter, H (x, t) 6= 0 is non-zero auxiliary function, L = Dα
t (n − 1 < α ≤ n) isan auxiliary linear operator with the following property
L[φ(x, t)] = 0 when φ(x, t) = 0. (3.4)
u0 (x, t) is an initial guess of u (x, t), φ (x, t; p) is an unknown function, respectively.It is important that one has great freedom to choose auxiliary things such as ~ andL in homotopy analysis method. Obviously, when p = 0 and p = 1, it holds
φ (x, t; 0) = u0 (x, t) , φ (x, t; 1) = u (x, t) , (3.5)
respectively. Thus, as p increases from 0 to 1, the solution φ (x, t; p) varies from theinitial guesses u0 (x, t) to the solution u (x, t). Expanding φ (x, t; p) in Taylor serieswith respect to p, we have
φ (x, t; p) = u0 (x, t) +
∞∑
m=1
um (x, t) pm, (3.6)
where
um (x, t) =1
m!
∂mφ (x, t; p)
∂pm
∣
∣
∣
∣
p=0
. (3.7)
If the auxiliary linear operator, the initial guess, the auxiliary operator ~, and theauxiliary function are properly chosen, the series (3.6) converges at p = 1, then wehave
u (x, t) = u0 (x, t) +
∞∑
m=1
um (x, t) , (3.8)
Define the vector
−→un = {u0 (x, t) , u1 (x, t) , .., un (x, t)} .
Differentiating equation (3.2) m-times with respect to the embedding parameter p
and then setting p = 0 and finally dividing them by m!, we obtain the mth-orderdeformation equation, with the assumption H (x, t) = 1
L [um (x, t) − χmum−1 (x, t)] = ~Rm(−→u m−1) (3.9)
subject to the following initial conditions:
u(k)m (x, 0) = 0, k = 0, 1, 2, ...,m − 1, (3.10)
where,
Rm(−→u m−1) =1
(m − 1)!
∂m−1N [φ (x, t; p)]
∂pm−1
∣
∣
∣
∣
p=0
. (3.11)
5
and
χm =
{
0, m ≤ 1,
1, m > 1.(3.12)
Substituting (3.1) into (3.11), and since A is linear operator, Rm(−→u m−1) can begiven by
Rm(−→u m−1) = Dαt um−1 − A(u(m−1)x, u(m−1)xxt)
−1
(m − 1)!
∂m−1B (φ, φx, φxx, φxxx)
∂qm−1
∣
∣
∣
∣
q=0
− (1 − χm) C (x, t) (3.13)
We can apply the operator Jα to both sides of (3.9) to obtain
JαDα [um (x, t) − χmum−1 (x, t)] = ~JαRm(−→u m−1). (3.14)
Using the definition (2.3) and the initial conditions (1.2), we obtain
um (x, t) = χmum−1 (x, t) + ~JαRm(−→u m−1). (3.15)
Finally, we will approximate HAM solution (3.8) by the truncated series
φm(x, t) =
m−1∑
k=0
uk (x, t) . (3.16)
The mth-order deformation equation (3.9) is linear and thus can be easily solved,especially by means of symbolic computation software such as Mathematica andMaple.
4. Convergence Theorem of HAM
Theorem 4.1. As long as the series u (x, t) = u0 (x, t)++∞∑
m=1um (x, t) converges,
where um (x, t) is governed by (3.9) under the definitions (3.11) and (3.12), it mustbe a solution of (1.3)
Proof : See [18].
5. Basic ideas of Adomian’s Decomposition Method
The Adomian’s decompositon method requires that the time-fractional Fornberg-Whitham equation (1.5) be expressed in terms of operatorm form as
Dαt u(x, t) + Lu(x, t) + Nu(x, t) = 0 (5.1)
where the notation Lu(x, t) = −Lxxtu(x, t)+Lxu(x, t) symbolizes the linear differ-ential operator and the notation Nu(x, t) = 1
2Lx
[
u2(x, t) − Lxxu2(x, t)]
symbolizesthe nonlinear operator. Applying the operator Jα
t , the inverse operator Dαt to both
side of Eq. (5.1) yields
u (x, t) =
m−1∑
k=0
∂ku
∂tk
(
x, 0+) tk
k!− Jα
t [Lu(x, t) + Nu(x, t)] . (5.2)
6 M. G. SAKAR, F. ERDOGAN
The ADM suggests the solution u(x, t) be decomposed into the infinite series ofcomponents
u (x, t) =∞∑
n=0
un (x, t) (5.3)
and the nonlinear opeartor Nu (x, t) is decomposed as follows:
Nu (x, t) =∞∑
n=0
An (5.4)
where An are so-called the Adomian’s Polynomials. The Adomian’s PolynomialsAn can be calculated for all form of nonlinearity according to specific algorithmsconstructed by Adomian [29,30]. The general form of formula for An Adomian’sPolynomials is
An =1
n!
[
dn
dλnN
(
∞∑
k=0
λkuk (x, t)
)]
λ=0
, n ≥ 0. (5.5)
Substitution the decomposition series (5.3) and (5.4) into both sides of (5.2)gives
∞∑
n=0
u (x, t) =m−1∑
k=0
∂ku
∂tk
(
x, 0+) tk
k!− Jα
[
L
(
∞∑
n=0
un(x, t)
)
+∞∑
n=0
An
]
(5.6)
from this equation, the iterates are determined by following recursive formula
u0 (x, t) =
m−1∑
k=0
∂ku
∂tk
(
x, 0+) tk
k!(5.7)
u1 (x, t) = −Jα [L (u0(x, t)) + A0] (5.8)
u2 (x, t) = −Jα [L (u1(x, t)) + A1] (5.9)
un+1 (x, t) = −Jα [L (un(x, t)) + An] (5.10)
This formula is easy to compute by using symbolic computation software such asMathematica and Maple or by writing a computer code to get as many polynomialsas we need in the calculation of the numerical as well as explicit solutions. Finally,The approximate solution by the truncated series
φk(x, t) =k−1∑
n=0
un (x, t) and u(x, t) = limk→∞
φk(x, t). (5.11)
where φk(x, t) =k−1∑
n=0un (x, t) denote the k-term approximation to u.
The decomposition series solution generally converge very rapidly, A classical ap-proach of convergence of Adomian’s decomposition method is presented by Abbouiand Cherruault [31]
7
6. Application of HAM and ADM
To solve eq.(1.5)-(1.6) by means of HAM, we choose the initial approximation
u0 (x, t) = u (x, 0) = e1
2x (6.1)
Eq. (1.5) suggests the nonlinear operator as
N [φ (x, t; p)] = Dαt φ (x, t; p)−
∂3φ (x, t; p)
∂x2∂t+
∂φ (x, t; p)
∂x−φ (x, t; p)
∂3φ (x, t; p)
∂x3
+φ (x, t; p)∂φ (x, t; p)
∂x− 3
∂φ (x, t; p)
∂x
∂2φ (x, t; p)
∂x2(6.2)
and the linear operator
L [φ (x, t; p)] = Dαt φ (x, t; p) (6.3)
with the property L (C1) = 0 where C1 is the integration constant. Using abovedefinition, with assumption H (x, t) = 1, we construct the zeroth-order deformationequation
(1 − p) L [φ (x, t; p) − u0 (x, t)] = p~N [φ (x, t; p)] , (6.4)
Obviously, when p = 0 and p = 1,
φ (x, t; 0) = u0 (x, t) , φ (x, t; 1) = u (x, t) ,
Therefore , as the embedding operator p increases from 0 to 1, φ (x, t; p) varies fromthe initial guesses u0 (x, t) to the solution u (x, t). Then, we obtain the mth-orderdeformation equation
L [um (x, t) − χmum−1 (x, t)] = ~Rm(−→u m−1), (6.5)
Where
Rm(−→u m−1) = Dαt um−1 (x, t) −
∂3um−1 (x, t)
∂x2∂t+
∂um−1 (x, t)
∂x
+
m−1∑
k=0
[ −uk(x, t)∂3um−1−k(x, t)
∂x3+ uk(x, t)
∂um−1−k(x, t)
∂x]
+m−1∑
k=0
[−3∂um−1−k(x, t)
∂x
∂2um−1−k(x, t)
∂x2]. (6.6)
The solution of mth-order deformation equation (6.5) for m ≥ 1 becomes
um (x, t) = χmum−1 (x, t) + ~J−1Rm(−→u m−1). (6.7)
from (6.1) and (6.7), we now successively obtain
u0(x, t) = e1
2x (6.8)
u1(x, t) =1
2~e
1
2x tα
Γ (α + 1)(6.9)
8 M. G. SAKAR, F. ERDOGAN
u2(x, t) =
(
4~ + 3~2
8
)
e1
2x t2α−1
Γ (2α)+
(
~2
4
)
e1
2x t2α
Γ (2α + 1)(6.10)
u3(x, t) =
(
16~ + 24~2 + 9~
3
32
)
e1
2x t3α−2
Γ (3α − 1)+
(
8~2 + 6~
3
16
)
e1
2x t3α−1
Γ (3α)
+
(
~3
8
)
e1
2x t3α
Γ (3α + 1)(6.11)
u4 (x, t) =
(
64~ + 144~2 + 108~
3 + 27h4
128
)
e1
2x t4α−3
Γ (4α − 2)
+
(
48~2 + 72~
3 + 27~4
64
)
e1
2x t4α−2
Γ (4α − 1)
+
(
12~3 + 9~
4
32
)
e1
2x t4α−1
Γ (4α)+
(
~4
16
)
e1
2x t4α
Γ (4α + 1)(6.12)
u5 (x, t) =
(
256~ + 768~2 + 864~
3 + 432~4 + 815~
5
512
)
e1
2x t5α−4
Γ (5α − 3)
+
(
64~2 + 144~
3 + 108~4 + 27~
5
64
)
e1
2x t5α−3
Γ (5α − 2)
+
(
48~3 + 72~
4 + 27~5
64
)
e1
2x t5α−2
Γ (5α − 1)
+
(
4~4 + 3~
5
16
)
e1
2x t5α−1
Γ (5α)+
(
~5
32
)
e1
2x t5α
Γ (5α + 1)(6.13)
and so on, Therefore, we use six term in evaluating the approximating solutionu (x, t) by the truncated series
uHAM =
5∑
i=0
ui. (6.14)
We remark that the exact travelling wave solution to the above initial valueproblem is given by [10]
u(x, t) = e1
2x− 2
3t (6.15)
To solve eq.(1.5)-(1.6) by means of ADM, Considering the given initial condition,
we can assume u0(x, t) = e1
2x as an initial approximation. We next use the recursive
relations (5.8)-(5.10) to obtain the rest of components of un(x, t)
u1 (x, t) = −Jα [−Lxxt(u0) + Lx(u0) + A0]
u1(x, t) = −1
2e
1
2x tα
Γ (α + 1)(6.16)
u2 (x, t) = −Jα [−Lxxt(u1) + Lx(u1) + A1]
9
u2(x, t) = −1
8e
1
2x t2α−1
Γ (2α)+
1
4e
1
2x t2α
Γ (2α + 1)(6.17)
u3 (x, t) = −Jα [−Lxxt(u2) + Lx(u2) + A2]
u3(x, t) = −1
32e
1
2x t3α−2
Γ (3α − 1)+
1
8e
1
2x t3α−1
Γ (3α)−
1
8e
1
2x t3α
Γ (3α + 1)(6.18)
u4 (x, t) = −Jα [−Lxxt(u3) + Lx(u3) + A3]
u4 (x, t) = −1
128e
1
2x t4α−3
Γ (4α − 2)+
3
64e
1
2x t4α−2
Γ (4α − 1)
−3
32e
1
2x t4α−1
Γ (4α)+
1
16e
1
2x t4α
Γ (4α + 1)(6.19)
u5 (x, t) = −Jα [−Lxxt(u4) + Lx(u4) + A4]
u5 (x, t) = −1
512e
1
2x t5α−4
Γ (5α − 3)+
1
64e
1
2x t5α−3
Γ (5α − 2)
−3
64e
1
2x t5α−2
Γ (5α − 1)+
1
16e
1
2x t5α−1
Γ (5α)−
1
32e
1
2x t5α
Γ (5α + 1)(6.20)
and so on, Therefore, we use six term in evaluating the decomposition solutionu (x, t) by the truncated series
uADM =
5∑
i=0
ui. (6.21)
.. .. .. ¶t H0, 0L
_ _ _ _ ¶tt H0, 0L
- - - - - ¶ttt H0, 0L
.........¶tttt H0, 0L
-2.0 -1.5 -1.0 -0.5 0.0 0.5 1.0 1.5
0
2
4
6
� h
�uHx
,tL
Figure 1. The ~-curve at (0,0) for 6th-order HAM approximatesolution (6.14) when α = 1.
10 M. G. SAKAR, F. ERDOGAN
Table 1. Absolute errors for differences between the exact solu-tion (6.15) and 6th-order HAM approximate given by for ~ = −1(or ADM) and α = 1
xi/ti 0.2 0.4 0.6 0.8 1-4 3.74057E-6 5.04192E-6 1.17973E-5 1.04731E-5 7.66092E-7-2 1.01679E-5 1.37054E-5 3.20684E-5 2.84688E-5 2.08245E-60 2.76393E-5 3.72550E-5 8.71710E-5 7.73862E-5 5.66069E-62 7.51314E-5 1.01270E-4 2.36955E-4 2.10357E-4 1.53873E-54 2.04228E-4 2.75280E-4 6.44112E-4 5.71811E-4 4.18272E-5
Figure 2. For Fornberg-Whitham equation with the initial con-dition of Eq.(1.6), HAM result when ~ = −1 (or ADM) for u(x, t)is, respectively (a) α = 1, (b) α = 0.9, (c) α = 0.8, (d) α = 0.7,(e) exact solution (6.15)
7. Numerical results and discussion
The series (6.14) contain the auxiliary parameter ~. As pointed out by Liao[18], the auxiliary parameter ~ can be employed to adjust the convergence regionof the homotopy analysis solution. This ~-curve, contain a horizontal line segment.
11
aL
0 2 4 6 8 10
0
10
20
30
40
50
60
70
� x
�uH
x,tL
bL
0 2 4 6 8 10
0
10
20
30
40
50
60
70
� x
�uH
x,tL
cL
0 2 4 6 8 10
0
20
40
60
� x
�uH
x,tL
dL
0 2 4 6 8 10
0
20
40
60
80
� x�
uHx,
tL
eL
0 2 4 6 8 10
0
10
20
30
40
50
60
70
� x
�uH
x,tL
Figure 3. For Fornberg-Whitham equation with the initial con-dition of Eq.(1.6), HAM result when ~ = −1 (or ADM) and t = 1for u(x, t) is, respectively (a) α = 1, (b) α = 0.9, (c) α = 0.8, (d)α = 0.7, (e) exact solution (6.15)
Table 2. Absolute errors for differences between the exact solu-tion (6.15) and 6th-order ADM solution (6.21) when t = 6 andα = 1.
xi uexact uADM |uexact-uADM |-4 0.0024787521 0.0056037265 3.12497E-3-2 0.0067379469 0.0152325081 8.49456E-30 0.0183156388 0.0414062500 2.30906E-22 0.0497870683 0.1125538569 6.27667E-24 0.1353352832 0.3059531040 1.70617E-1
This horizontal line segment denotes the valid region of ~ which guaranteed theconvergence of related series. To investigate the influence of ~ on the solution series,we plot the so-called ~-curve of u(0, 0) obtained from the 6th-order HAM solutionas shown in Figure 1. It is observed the valid region for ~ is −1.1 < ~ < −0.9. Weget the same values as in ADM (6.21) or HPM when ~ = -1. Therefore, the HAM
12 M. G. SAKAR, F. ERDOGAN
Table 3. Absolute errors for differences between the exact solu-tion (6.15) and 6th-order HAM solution (6.14) for ~ =-1.04 whent = 6 and α = 1.
xi uexact uHAM |uexact-uHAM |-4 0.0024787521 0.0015123400 9.66413E-4-2 0.0067379469 0.0041109600 2.62698E-30 0.0183156388 0.0111748000 7.14088E-32 0.0497870683 0.0303761000 1.94109E-24 0.1353352832 0.0825709000 5.27644E-2
. . . Exact solution
.......6th order HAM solution ( Ñ= -1.04 )
.. .. 6th order HAM solution ( Ñ= -1.01 )
_ _ _6th order HAM solution ( Ñ= -1)
-5 0 5
0.0
0.2
0.4
0.6
0.8
� x
�uHx
,tL
Figure 4. The results obtained by HAM for various ~ by 6thorder HAM approximate solution (6.14) for α = 1 in comparisonwith the exact solution (6.15) when −8 < x < 8 and t = 6.
is rather general and contains the ADM and HPM. In Table 1, we compute theabsolute errors for differences between the exact solution (6.15) and approximatesolution (6.14) obtained by the HAM (~ = -1). In Table 2, we compute the absoluteerrors for differences between the exact solution (6.15) and ADM (6.21) solutionwhen t = 4 and α = 1. In Figure 2, we study the diagrams of results obtained byHAM (~ = -1) for different particular cases of α. The exact solution (6.14) andHAM solution (6.15) for different particular cases of α are prensented graphicallyin Figure 3, when t = 1. In Figure 4, we study the diagrams of results obtained byHAM for ~ = -1 and ~ = -1.04 in comparison with the exact solution (6.15), onecan see that the best value of ~ in this case is not −1. But then, the HAM solution(6.15) has the same shape as the exact solution for large range of t, i.e., t = 6 asshown in Figure 4 and Table 3, when we take ~ = -1.04. We can remark highterrors for ~ = -1 (see Table 2). Therefore, we can say that HAM is more effectivethan ADM.
13
8. Conclusion
In this paper, the homotopy analysis method has been applied for finding theapproximate analytical solution of the nonlinear time-fractional Fornberg-Whithamequation. The explicit series solution of Fornberg-Whitham equation are obtained,which are the same as those results given by Adomian’s decomposition mehodand Homotopy perturbation method for ~ = -1. This accords with the conclusionthat HAM logically contains the ADM and HPM. The HAM provides us with aconvenient way to the control the convergence region of solution series for largevalues of t, which is a fundamental qualitative difference in analysis between HAMand other methods. The results show that HAM is powerful mathematical tool forsolving nonlinear fractional partial differential equations having wide applicationsin science and engineering.
14 M. G. SAKAR, F. ERDOGAN
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Yuzuncu Yil University, Faculty of Sciences, Department of Mathematics, 65080,
Van, Turkey
E-mail address: [email protected](Sakar), [email protected](Erdogan)