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Blow-up phenomena and stability of solitary waves for a generalized Dullin-Gottwald-Holm equation

Boundary Value Problems20132013:226

https://doi.org/10.1186/1687-2770-2013-226

©  Dündar and Polat; licensee Springer. 2013

Received: 21 May 2013

Accepted: 3 September 2013

Published: 7 November 2013

Abstract

In this work, we consider the Cauchy problem of the generalized Dullin-Gottwald-Holm equation. We establish a blow-up result for the generalized Dullin-Gottwald-Holm equation. In addition to this, we investigate the stability of solitary wave solutions of the equation.

Keywords

the generalized Dullin-Gottwald-Holm equation blow-up stability solitary wave solution

1 Introduction

The nonlinear evolution equation
y t + c 0 u x + u y x + 2 y u x + γ u x x x = 0 , t > 0 , x ∈ R
(1)

is, in the dimensionless space-time variable ( x , t ) , a model for unidirectional shallow water waves over a flat bottom. Here, y = u − α 2 u x x is a momentum variable, the constants α 2 and γ c 0 are squares of length scales, and c 0 = g h > 0 (where c 0 = 2 ω ) is the linear wave speed for undisturbed water at rest at spatial infinity, where h is the mean fluid depth and g is the gravitational constant. Dullin, Gottwald and Holm derived Eq. (1) by using asymptotic expansions directly in the Hamiltonian for Euler’s equations in the shallow water regime in [1]. Eq. (1) was shown to be bi-Hamiltonian and to have a Lax pair formulation. The Dullin-Gottwald-Holm equation (we call it DGH equation for short) is an integrable system via the inverse scattering transform (IST) method and contains both the Korteweg-de Vries (KdV) and Camassa-Holm (CH) equations [2] as limiting cases.

Using the notation y = u − α 2 u x x , we can rewrite the initial value problem of Eq. (1) as
{ u t − α 2 u x x t + 2 ω u x + 3 u u x + γ u x x x = α 2 ( 2 u x u x x + u u x x x ) , t > 0 , x ∈ R , u ( 0 , x ) = u 0 ( x ) , x ∈ R .
(2)
Eq. (2) relates two separately integrable soliton equations for water waves. Formally, when α = 0 and γ ≠ 0 , this equation becomes the KdV equation
u t + 2 ω u x + 3 u u x + γ u x x x = 0 .
For α = 1 and γ = 0 , Eq. (2) becomes the Camassa-Holm equation
u t − u x x t + 2 ω u x + 3 u u x = 2 u x u x x + u u x x x .

Recently, the DGH equation has been studied by many authors. Tian et al. [3] studied the well-posedness of the Cauchy problem and the scattering problem for the DGH equation. In [4], Hakkaev proved the orbital stability of the peaked solitary waves for the DGH equation by using the method in [5]. It was shown that the DGH equation has global solutions and blow-up solutions in [6–9].

If the term 3 u u x is replaced with 3 u m u x in the DGH equation, then it is known as the generalized DGH equation and has the following form:
u t − α 2 u x x t + 2 ω u x + 3 u m u x + γ u x x x = α 2 ( 2 u x u x x + u u x x x ) , m > 0 .
(3)

Eq. (3) was studied in [10, 11]. In [10], Lu et al. studied the local well-posedness of the Cauchy problem for Eq. (3). In [11], the conservation laws for the generalized DGH equation were derived.

Recently, the local well-posedness problem for the following generalization of the DGH equation:
{ u t − α 2 u x x t + h ( u ) x + γ u x x x = α 2 ( g ′ ( u ) 2 u x 2 + g ( u ) u x x ) x , t > 0 , x ∈ R , u ( 0 , x ) = u 0 ( x ) , x ∈ R ,
(4)

was studied in [12]. For h ( u ) = 2 ω u + 3 2 u 2 and g ( u ) = u , Eq. (4) becomes DGH Eq. (2).

Eq. (4) can be written as the following Hamiltonian form:
u t + J F ′ ( u ) = 0 ,
where J = ( I − α 2 ∂ x 2 ) − 1 ∂ x is a skew-symmetric operator and
F ( u ) = 1 2 ∫ R ( 2 H ( u ) + α 2 g ( u ) u x 2 − γ u x 2 ) d x ,
where H ′ ( s ) = h ( s ) . We note that the functional F ( u ) is formally conserved. Moreover, the other conserved quantity is
E ( u ) = 1 2 ∫ R ( u 2 + α 2 u x 2 ) d x .

One of the aims of this paper is to give the precise blow-up scenario and to show that Eq. (4) has blow-up solutions for g ( u ) = u . In addition to this, we investigate the stability of solitary wave solutions of Eq. (4) with h ( u ) = 2 ω u + p + 2 2 u p + 1 and g ( u ) = u p .

The remainder of the paper is organized as follows. In Section 2, we give our basic notation and recall some required results. In Section 3, we investigate blow-up of solutions for Eq. (4). In Section 4, we prove the stability of solitary wave solutions with the help of the orbital stability theory [13].

2 Preliminaries

Firstly, we start by summarizing some notations. Λ s = ( 1 − ∂ x 2 ) s / 2 , s ∈ R ; H s = H s ( R ) with the norm
∥ f ∥ H s = ∥ f ∥ s = ( ∫ R ( 1 + | ξ | 2 ) s | f ˆ ( ξ ) | 2 d ξ ) 1 / 2

and ( ⋅ , ⋅ ) for its inner product. For the sake of simplicity, we employ the same symbol c for different positive constants.

Some useful lemmas are as follows.

Lemma 2.1 [14]

Assume that s > 0 . Then we have
∥ [ Λ s , g ] f ∥ L 2 ≤ c ( ∥ ∂ x g ∥ L ∞ ∥ Λ s − 1 f ∥ L 2 + ∥ Λ s g ∥ L 2 ∥ f ∥ L ∞ ) .

Here c is a constant depending only on s.

Lemma 2.2 [15]

Assume that F ∈ C m + 2 ( R , R ) with F ( 0 ) = 0 . Then, for every 1 2 < s ≤ m , we have that
∥ F ( u ) ∥ s ≤ F ˜ ( ∥ u ∥ L ∞ ) ∥ u ∥ s , u ∈ H s ,

where F ˜ is a monotone increasing function depending only on F and s.

Lemma 2.3 [14]

Assume that s > 0 . Then H s ∩ L ∞ is an algebra. Moreover,
∥ f g ∥ s ≤ c ( ∥ f ∥ L ∞ ∥ g ∥ s + ∥ f ∥ s ∥ g ∥ L ∞ ) ,

where c is a constant depending only on s.

Lemma 2.4 [16]

Let T > 0 and u ∈ C 1 ( [ 0 , T ) ; H 2 ) . Then, for every t ∈ [ 0 , T ) , there exists at least one pair of points ξ ( t ) , ζ ( t ) ∈ R such that
m ( t ) = inf x ∈ R [ u x ( t , x ) ] = u x ( t , ξ ( t ) ) , M ( t ) = sup x ∈ R [ u x ( t , x ) ] = u x ( t , ζ ( t ) ) ,
and m ( t ) , M ( t ) are absolutely continuous in ( 0 , T ) . Moreover,
d m ( t ) d t = u t x ( t , ξ ( t ) ) , d M ( t ) d t = u t x ( t , ζ ( t ) ) , a.e. on ( 0 , T ) .

Theorem 2.1 [12]

Assume that h , g ∈ C m + 3 ( R , R ) , m ≥ 2 and h ( 0 ) = g ( 0 ) = 0 . Given u 0 ∈ H s , 3 2 < s ≤ m , there exists a maximal T = T ( u 0 ) > 0 and a unique solution u to Eq. (4) such that
u = u ( ⋅ , u 0 ) ∈ C ( [ 0 , T ) ; H s ) ∩ C 1 ( [ 0 , T ) ; H s − 1 ) .
Moreover, the solution depends continuously on the initial data, i.e., the mapping
u 0 → u ( ⋅ , u 0 ) : H s → C ( [ 0 , T ) ; H s ) ∩ C 1 ( [ 0 , T ) ; H s − 1 )

is continuous.

Lemma 2.5 [12]

Let u ( t , x ) be a solution of Eq. (4). Then the functionals
E ( u ) = 1 2 ∫ R ( u 2 + α 2 u x 2 ) d x , F ( u ) = 1 2 ∫ R ( 2 H ( u ) + α 2 g ( u ) u x 2 − γ u x 2 ) d x

are constant with respect to t, where H ′ ( s ) = h ( s ) .

3 Blow-up phenomena

In this section, we discuss the blow-up phenomena of Eq. (4) with g ( u ) = u . For Eq. (4), which describes shallow water waves, the blow-up occurs only in the form of wave-breaking, i.e. the solution remains bounded but its slope becomes unbounded in finite time.

Set p ( x ) = 1 2 α e − | x α | , x ∈ R , then ( 1 − α 2 ∂ x 2 ) − 1 f = p ∗ f for all f ∈ L 2 ( R ) . Using this identity, we can rewrite Eq. (4) as follows:
{ u t + ( u − γ α 2 ) u x + ∂ x p ∗ k ( u ) = 0 , t > 0 , x ∈ R , u ( 0 , x ) = u 0 ( x ) , x ∈ R ,
(5)
or in the equivalent form:
{ u t + ( u − γ α 2 ) u x = − ∂ x ( 1 − α 2 ∂ x 2 ) − 1 k ( u ) , t > 0 , x ∈ R , u ( 0 , x ) = u 0 ( x ) , x ∈ R ,
(6)

where k ( u ) = ( h ( u ) + α 2 2 u x 2 − 1 2 u 2 + γ α 2 u ) .

We now prove the following result.

Theorem 3.1 Let h ∈ C m + 3 ( R , R ) , m ≥ 2 , and u 0 ∈ H r , 3 2 < r ≤ m . If T is the existence time of the corresponding solution of initial data u 0 , then the H r -norm of u ( t , x ) to Eq. (4) (or (6)) blows up on [ 0 , T ) if and only if
lim ¯ t → T { ∥ u ( t , x ) ∥ L ∞ + ∥ u x ( t , x ) ∥ L ∞ } = ∞ .
Proof Let u ( t , x ) be the solution of Eq. (4) with the initial data u 0 ∈ H r , 3 2 < r ≤ m , which is guaranteed by Theorem 2.1. If
lim ¯ t → T { ∥ u ( t , x ) ∥ L ∞ + ∥ u x ( t , x ) ∥ L ∞ } = ∞ ,

by Sobolev’s embedding theorem, we obtain that the solution u ( t , x ) will blow up in finite time.

Next, applying the operator Λ r to Eq. (6), multiplying by Λ r u , and integrating over R, we obtain
d d t ( u , u ) r = − 2 ( u u x , u ) r + 2 ( f ( u ) , u ) r .
(7)
Here, f ( u ) = − ∂ x ( 1 − α 2 ∂ x 2 ) − 1 ( h ( u ) + α 2 2 u x 2 − 1 2 u 2 + γ α 2 u ) . Assume that there exists R > 0 such that
lim ¯ t → T { ∥ u ( t , x ) ∥ L ∞ + ∥ u x ( t , x ) ∥ L ∞ } ≤ R .
Similar to [18], using Lemma 2.1 with s = r , we get
| ( u u x , u ) r | ≤ c ∥ u x ∥ L ∞ ∥ u ∥ r 2 ≤ c R ∥ u ∥ r 2 .
(8)
On the other hand, we estimate the second term of the right-hand side of Eq. (7)
( f ( u ) , u ) r = ( − ∂ x ( 1 − α 2 ∂ x 2 ) − 1 ( h ( u ) + α 2 2 u x 2 − 1 2 u 2 + γ α 2 u ) , u ) r ≤ c ∥ u ∥ r ( ∥ h ( u ) ∥ r − 1 + ∥ u x 2 ∥ r − 1 + ∥ u 2 ∥ r − 1 + ∥ u ∥ r − 1 ) ≤ c ( h ˜ ( ∥ u ∥ L ∞ ) + ∥ u x ∥ L ∞ + ∥ u ∥ L ∞ + 1 ) ∥ u ∥ r 2 ≤ c ( h ˜ ( R ) + R + 1 ) ∥ u ∥ r 2 .
(9)
Here, we applied Lemma 2.2 with F ( u ) = h ( u ) and s = r − 1 , Lemma 2.3 with s = r − 1 . From (7)-(9), we obtain
d d t ∥ u ∥ r 2 ≤ c ( h ˜ ( R ) + R + 1 ) ∥ u ∥ r 2 .
Thus, by Gronwall’s inequality, we get
∥ u ( t ) ∥ r 2 ≤ ∥ u 0 ∥ r 2 exp ( h ˜ ( R ) + R + 1 ) t .

This completes the proof of Theorem 3.1. □

We have the following blow-up scenario for Eq. (4).

Theorem 3.2 Assume that h ∈ C m + 3 ( R , R ) , m ≥ 3 . Given u 0 ∈ H r , 3 ≤ r ≤ m , the solution u = u ( u 0 , ⋅ ) of Eq. (4) is uniformly bounded. Blow-up in finite time T < + ∞ occurs if and only if
lim inf t → T { inf x ∈ R [ u x ( t , x ) ] } = − ∞ .
Proof E ( u ) = 1 2 ∫ R ( u 2 + α 2 u x 2 ) d x is an invariant for Eq. (4). According to the inequalities
∫ R ( u 2 + u x 2 ) d x ≤ ∫ R ( u 2 + α 2 u x 2 ) d x = 2 E ( u ) ( α ≥ 1 ) , ∫ R ( u 2 + u x 2 ) d x ≤ 1 α 2 ∫ R ( u 2 + α 2 u x 2 ) d x = 2 α 2 E ( u ) ( α ≤ 1 ) ,

the invariance of E ( u ) ensures that the solution u is uniformly bounded as long as they exist.

If the slope of the solution u ( t , x ) becomes unbounded from below in finite time, then by Theorem 2.1 and Sobolev’s embedding theorem, we can see that the solution u ( t , x ) blows up in finite time.

Next, if the slope of the solution is bounded from below in finite time, then we deduce that the solution will not blow up in finite time. Differentiating Eq. (5) with respect to x, in view of the identity ∂ x 2 ( p ∗ f ) = 1 α 2 ( p ∗ f − f ) , we have
u t x = − 1 2 u x 2 − u u x x + γ α 2 u x x + 1 α 2 h ( u ) − 1 2 α 2 u 2 + γ α 4 u − 1 α 2 p ∗ ( h ( u ) + α 2 2 u x 2 − 1 2 u 2 + γ α 2 u ) .
(10)
Note that p ∗ ( 1 2 u x 2 ) ≥ 0 and
∥ u ∥ L ∞ 2 ≤ 1 2 ∥ u ∥ 1 2 ≤ max ( 1 , 1 α 2 ) E ( u 0 ) ≤ max ( 1 , 1 α 4 ) ∥ u 0 ∥ 1 2 .
By Young’s inequality, we get
∥ p ∗ h ( u ) ∥ L ∞ ≤ ∥ p ∥ L 1 ∥ h ( u ) ∥ L ∞ ≤ ∥ h ( u ) ∥ L ∞ ≤ sup | v | ≤ max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 | h ( v ) | , ∥ p ∗ u 2 ∥ L ∞ ≤ ∥ p ∥ L 1 ∥ u 2 ∥ L ∞ ≤ ∥ u ∥ L ∞ 2 ≤ max ( 1 , 1 α 4 ) ∥ u 0 ∥ 1 2 ,
and
∥ p ∗ u ∥ L ∞ ≤ ∥ p ∥ L 1 ∥ u ∥ L ∞ ≤ ∥ u ∥ L ∞ ≤ max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 .
Define M ( t ) = u x ( t , ζ ( t ) ) = sup x ∈ R [ u x ( t , x ) ] . Since u x x ( t , ζ ( t ) ) = 0 for all t ∈ [ 0 , T ) , it follows that a.e. on [ 0 , T )
M ′ ( t ) = − 1 2 M 2 ( t ) + 1 α 2 h ( u ( t , ζ ( t ) ) ) − 1 2 α 2 u 2 ( t , ζ ( t ) ) + γ α 4 u ( t , ζ ( t ) ) − 1 α 2 p ∗ ( h ( u ) + α 2 2 u x 2 − 1 2 u 2 + γ α 2 u ) .
Then
M ′ ( t ) ≤ − 1 2 M 2 ( t ) + A 0 2 ,
where
A 0 = ( 2 γ α 4 max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 + 1 2 α 2 max ( 1 , 1 α 4 ) ∥ u 0 ∥ 1 2 + 2 α 2 G 0 ) 1 2
by
G 0 = sup | v | ≤ max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 | h ( v ) | .
If M ( t ) > 2 A 0 , then M ′ ( t ) < 0 and M ( t ) is decreasing. Otherwise, M ( t ) ≤ 2 A 0 . Thus we get
m ( t ) ≤ M ( t ) ≤ max { M ( 0 ) , 2 A 0 } , t ∈ [ 0 , T ) .

By Theorem 3.1 and the above inequality, we have that if the slope of the solution is bounded from below in finite time, then the solution will not blow up in finite time. □

Next, we present the following blow-up result.

Theorem 3.3 Assume that h ∈ C m + 3 ( R , R ) , m ≥ 3 . Given α > 0 , u 0 ∈ H r , 3 ≤ r ≤ m , assume that we can find x 0 ∈ R with
u 0 ′ ( x 0 ) < − ( 4 γ α 4 max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 + 1 α 2 max ( 1 , 1 α 4 ) ∥ u 0 ∥ 1 2 + 4 α 2 G 0 ) 1 2 = − B 0 ,
where
G 0 = sup | v | ≤ max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 | h ( v ) | .
Then the corresponding solution to Eq. (4) for g ( u ) = u blows up in finite time. Moreover, the maximal time of existence T satisfies the inequality
T ≤ 2 c ( c 2 − B 0 ) − 1 , where c = − u 0 ′ ( x 0 ) .
Proof Now define m ( t ) = inf x ∈ R [ u x ( t , x ) ] = u x ( t , ξ ( t ) ) by Lemma 2.4, and let ξ ( t ) ∈ R be a point where this infimum is attained. From Eq. (10), we have
m ′ ( t ) = − 1 2 m 2 ( t ) + 1 α 2 h ( u ( t , ξ ( t ) ) ) − 1 2 α 2 u 2 ( t , ξ ( t ) ) + γ α 4 u ( t , ξ ( t ) ) − 1 α 2 p ∗ ( h ( u ) + α 2 2 u x 2 − 1 2 u 2 + γ α 2 u ) .
For x = ξ ( t ) , since u x x ( t , ξ ( t ) ) = 0 , we arrive at
m ′ ( t ) ≤ − 1 2 m 2 ( t ) + K ( u ) a.e. on  ( 0 , T ) ,
where
K ( u ) = γ α 4 ∥ u ∥ L ∞ + 1 α 2 ( sup | v | ≤ ∥ u ∥ L ∞ | h ( v ) | ) + ∥ 1 α 2 p ∗ ( h ( u ) + 1 2 u 2 + γ α 2 u ) ∥ L ∞ .
Note that
∥ u ∥ L ∞ 2 ≤ 1 2 ∥ u ∥ 1 2 ≤ max ( 1 , 1 α 2 ) E ( u 0 ) ≤ max ( 1 , 1 α 4 ) ∥ u 0 ∥ 1 2 .
By Young’s inequality, we get
∥ p ∗ h ( u ) ∥ L ∞ ≤ sup | v | ≤ max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 | h ( v ) | , ∥ p ∗ u 2 ∥ L ∞ ≤ max ( 1 , 1 α 4 ) ∥ u 0 ∥ 1 2
and
∥ p ∗ u ∥ L ∞ ≤ max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 .
So, it follows that
m ′ ( t ) ≤ − 1 2 m 2 ( t ) + K 0 ,
(11)
where (note that A 0 2 = K 0 )
G 0 = sup | v | ≤ max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 | h ( v ) | , K 0 = 2 γ α 4 max ( 1 , 1 α 2 ) ∥ u 0 ∥ 1 + 1 2 α 2 max ( 1 , 1 α 4 ) ∥ u 0 ∥ 1 2 + 2 α 2 G 0 .
The absolute continuity of the locally Lipschitz function m ( t ) allows us to perform an integration over [ 0 , t ] and to have
m ( t ) ≤ m ( 0 ) − 1 2 ∫ 0 t m 2 ( τ ) d τ + K 0 t , t ∈ [ 0 , T ) .
We claim now that m ( t ) < − c for all t ∈ ( 0 , T ) , where c > 2 K 0 is fixed arbitrarily provided that m ( 0 ) < − c . In fact, assuming the contrary, in view of m ( t ) being continuous, ensure the existence of t 0 ∈ ( 0 , T ) such that m ( t ) < − c in ( 0 , t 0 ) and m ( t 0 ) = c . Then we deduce that
m ( t ) ≤ m ( 0 ) − ∫ 0 t K 0 d τ + K 0 t = m ( 0 ) < − c , t ∈ [ 0 , t 0 ] ,
and a contradiction appears as we take t = t 0 . Using (11), we get
m ′ ( t ) ≤ − 1 2 m 2 ( t ) + K 0 ≤ − 1 2 m 2 ( t ) + ( 1 2 − ε ) c 2 ≤ − 1 2 m 2 ( t ) + ( 1 2 − ε ) m 2 ( t ) ≤ − ε m 2 ( t ) a.e. on  ( 0 , T ) ,
where ε ∈ ( 0 , 1 2 − K 0 c 2 ) . Since m ( t ) < − c , and m ( t ) is locally Lipschitz, it follows that 1 m ( t ) is locally Lipschitz as well. This gives
d d t ( 1 m ( t ) ) = − m ′ ( t ) m 2 ( t ) ≥ ε a.e. on  ( 0 , T ) .
Integration of this inequality yields
− 1 m ( t ) + 1 m ( 0 ) ≤ − ε t .
Since m ( t ) < 0 , we obtain
0 ≤ t < 1 ε ( − m ( 0 ) ) , t ∈ [ 0 , T ) .
In fact, as a consequence of these considerations, we obtain that the maximal existence time
T ≤ 1 ε ( − m ( 0 ) ) for all  ε ∈ ( 0 , 1 2 − K 0 c 2 ) .
An estimation from the above for T is obtained immediately, namely
T ≤ 2 c 2 ( − m ( 0 ) ) ( c 2 − 2 K 0 ) .

The conclusion is reached by letting c → − m ( 0 ) . □

4 Stability of solitary waves

In this section, we discuss the stability of solitary wave solutions of Eq. (4) with h ( u ) = 2 ω u + p + 2 2 u p + 1 and g ( u ) = u p . In this case, Eq. (4) turns into the following equation:
{ u t − α 2 u x x t + ( 2 ω u + p + 2 2 u p + 1 ) x + γ u x x x = α 2 ( p 2 u p − 1 u x 2 + u p u x x ) x , u ( 0 , x ) = u 0 ( x ) ,
(12)
where p > 0 . When h ( u ) = 2 ω u + p + 2 2 u p + 1 and g ( u ) = u p , the conservation law F ( u ) takes the form
F ( u ) = ∫ R ( ω u 2 + u p + 2 2 + α 2 u p 2 u x 2 − γ 2 u x 2 ) d x .

The appropriate notion of stability for the solitary waves here is orbital stability: a wave starting close to a solitary wave should stay close, as long as it exists, to some translate of the solitary wave. The orbit of a solitary wave is the set of all its translates [17].

We define the orbit φ ( ⋅ − η ) = { τ ( η ) φ ( ⋅ ) : η ∈ R } , where τ is a one-parameter group of unitary operators on H 2 defined by τ ( s ) u ( ⋅ ) = u ( ⋅ − s ) , s ∈ R , u ∈ H 2 . They may be interpreted physically as ‘solitary waves’ or ‘bound states.’

Definition The φ-orbit is stable if for all ε > 0 , there exists δ > 0 with the following property. If ∥ u ( 0 , ⋅ ) − φ ( ⋅ ) ∥ H 2 < δ and u is a solution of Eq. (12) in some interval [ 0 , T ) with u ( 0 , ⋅ ) = u 0 , then u can be continued to a solution in 0 ≤ t < ∞ and
sup t inf η ∥ u ( t , ⋅ ) − φ ( ⋅ − η ) ∥ H 2 < ε .

Otherwise, the φ-orbit is called unstable.

Definition can be seen in reference [13].

Substituting u ( x , t ) = φ ( x − c t ) = φ ( σ ) into Eq. (12) and integrating once with respect to σ, we obtain
c φ − c α 2 φ ″ − 2 ω φ − p + 2 2 φ p + 1 − γ φ ″ + α 2 ( p 2 φ p − 1 φ ′ 2 + φ p φ ″ ) = 0 .
(13)
In terms of the functionals E and F,
E ′ ( φ ) = φ − α 2 φ ″ , F ′ ( φ ) = 2 ω φ + p + 2 2 φ p + 1 + γ φ ″ − α 2 ( p 2 φ p − 1 φ ′ 2 + φ p φ ″ ) ,
and according to Eq. (13), we can obtain that c E ′ ( φ ) − F ′ ( φ ) = 0 , where E ′ and F ′ are the Fréchet derivatives of E and F, respectively. To study the orbital stability of the solitary waves of Eq. (12), we need the operator H c and the function d ( c ) = c E ( φ ) − F ( φ ) . The linearized operator H c around φ is defined by
H c = c E ″ ( φ ) − F ″ ( φ ) = α 2 ∂ x [ ( φ p − ( c + γ α 2 ) ) ∂ x ] + α 2 ( p φ p − 1 φ ″ + p ( p − 1 ) 2 φ p − 2 φ ′ 2 ) − ( p + 2 ) ( p + 1 ) 2 φ p + c − 2 ω .
(14)

Lemma 4.1 For each c ∈ ( 2 ω , ∞ ) , H c = c E ″ ( φ ) − F ″ ( φ ) has a unique simple negative eigenvalue, zero is a simple eigenvalue, and the rest of its spectrum is bounded away from zero.

Proof For any u , v ∈ H 2 , we have ∫ R u x x v d x = ∫ R u v x x d x and
∫ R φ p u x x v d x = ∫ R p φ p − 1 φ x v x u d x + ∫ R φ p v x x u d x − ∫ R p φ p − 1 φ x u x v d x .
Therefore,
〈 ∂ x ( φ p − ( c + γ α 2 ) ) ∂ x u , v 〉 = 〈 ∂ x ( φ p − ( c + γ α 2 ) ) ∂ x v , u 〉 .
By (14), we know that H c is a self-adjoint operator and
H c φ ′ = α 2 [ ( φ p − ( c + γ α 2 ) ) φ ‴ ] + α 2 ( 2 p φ p − 1 φ ′ φ ″ + p ( p − 1 ) 2 φ p − 2 φ ′ 3 ) − ( p + 2 ) ( p + 1 ) 2 φ p φ ′ + ( c − 2 ω ) φ ′ .
(15)

Differentiating (13) with respect to σ, we find that the right-hand side of Eq. (15) equals zero, that is, H c φ ′ = 0 . The behavior of the function φ tells us that φ ′ has exactly one zero. So, the zero eigenvalue of the operator H c is simple, and by using the Sturm-Liouville theorem, we have that H c only has a negative eigenvalue. Using Weyl’s theorem, the essential spectrum of H c belongs to [ c − 2 ω α 2 , + ∞ ) . That completes the proof. □

As for the above results, it is known [13] that stability would be ensured by the convexity of the scalar function d ( c ) = c E ( φ ) − F ( φ ) , c > 2 ω . So, we obtain the following theorem under the condition 2 ω α 2 + γ = 0 .

Theorem 4.1 Suppose that φ ( ⋅ − η ) is a solitary wave solution for c > 2 ω , if d ″ ( c ) > 0 , then φ ( ⋅ − η ) is stable.

Define the functionals
I ( u ) = I ( u ; ω , c ) = ∫ R [ ( c − 2 ω ) u 2 + α 2 ( c − 2 ω ) u x 2 ] d x
and
K ( u ) = ∫ R ( u p + 2 + α 2 u p u x 2 ) d x .
For λ > 0 , we consider the following constrained minimization problem on H 2 :
M λ = { inf I ( u ) : u ∈ H 2 , K ( u ) = λ } .
(16)
Then if ψ ∈ H 2 achieves the minimum of problem (16), for some λ > 0 , then there exists a Lagrange multiplier ϑ such that
( 2 c − 4 ω ) ψ − α 2 ( 2 c − 4 ω ) ψ ″ = ϑ [ ( p + 2 ) ψ p + 1 − α 2 ( p ψ p − 1 φ ′ 2 + 2 φ p φ ″ ) ] .
Hence φ = ϑ 1 p ψ is a solution of solitary wave equation (13). By homogeneity of I ( u ) and K ( u ) , φ satisfies
m = m ( ω , c ) = inf { I ( u ) K ( u ) 2 p + 2 : u ∈ H 2 , K ( u ) > 0 } ,
and it follows that
M λ = m λ 2 p + 2 .

Multiplying solitary wave equation (13) by φ and integrating the resulting equation gives I ( φ ) = ( p + 2 ) 2 K ( φ ) .

We say that ψ k is a minimizing sequence if for some λ > 0 , lim k → ∞ I ( ψ k ) = M λ and lim k → ∞ K ( ψ k ) = λ .

Theorem 4.2 Let { ψ k } be a minimizing sequence for some λ > 0 . If c > 2 ω , then there exists a subsequence { ψ k j } , scalars y j ∈ R and ψ ∈ H 2 such that ψ k j → ψ in H 2 . The function ψ achieves the minimum I ( ψ ) = M λ subject to the constraint K ( ψ ) = λ .

Proof The result is an application of the concentration compactness lemma of Lions [19, 20]. Proof is similar to [21–23] according to the definition of I ( u ) and K ( u ) .

In this section, we show that the stability of solitary wave solutions is determined by the convexity of the function d ( c ) .

We state the basic properties of the function d.

A simple calculation gives
d ( c ) = c E ( u ) − F ( u ) = 1 2 ( I ( u ) − K ( u ) ) .
(17)
By using I ( φ ) = ( p + 2 ) 2 K ( φ ) , we obtain
d ( c ) = p 2 ( p + 2 ) I ( φ ) = p 4 K ( φ ) = p 4 ( 2 p + 2 m ) p + 2 p .
(18)

Therefore, d is well defined, and we may deduce its properties by examining the function m ( ω , c ) . □

Lemma 4.2 For fixed ω ∈ R , m ( ω , c ) is monotonically increasing in c.

Proof We assume that φ c 1 , φ c 2 are solutions of Eq. (13) corresponding to c = c 1 , c = c 2 , respectively. Without loss of generality, let be c 1 < c 2 , then we have
m ( ω , c 1 ) ≤ I c ( φ c 2 ; ω , c 1 ) K ( φ c 2 ) 2 p + 2 = ∫ R [ ( c 1 − 2 ω ) φ c 2 2 + α 2 ( c 1 − 2 ω ) ( φ c 2 ′ ) 2 ] d x K ( φ c 2 ) 2 p + 2 = ∫ R [ ( c 2 − 2 ω ) φ c 2 2 + α 2 ( c 2 − 2 ω ) ( φ c 2 ′ ) 2 ] d x K ( φ c 2 ) 2 p + 2 + − c 2 ∫ R [ φ c 2 2 + α 2 ( φ c 2 ′ ) 2 ] d x + c 1 ∫ R [ φ c 2 2 + α 2 ( φ c 2 ′ ) 2 ] d x K ( φ c 2 ) 2 p + 2 = m ( ω , c 2 ) + ( c 1 − c 2 ) ∫ R [ φ c 2 2 + α 2 ( φ c 2 ′ ) 2 ] d x K ( φ c 2 ) 2 p + 2 ≤ m ( ω , c 2 ) .

This shows that m is monotonically increasing in c, so that by (18), d must be monotonically increasing as well.

A tubular neighborhood around the orbital φ ( ⋅ − η ) is defined by
U ω , c ; ε = { u ∈ H 2 : inf η ∈ R ∥ u − φ ( ⋅ − η ) ∥ H 2 < ε } .
It follows from (18) and the fact that d ( c ) is monotonically increasing in c that
c ( u ) = d − 1 ( p 4 K ( u ) ) .
(19)

 □

The following lemma is helpful in order to prove the stability of solitary waves.

Lemma 4.3 If d ″ ( c ) > 0 , then there exists ε > 0 such that for any u ∈ U ω , c ; ε , we have
c ( u ) [ E ( u ) − E ( φ ) ] − [ F ( u ) − F ( φ ) ] ≥ 1 4 d ″ ( c ) | c ( u ) − c | 2 .
Proof By using d ′ ( c ) = E ( φ ) and Taylor’s formula, we have the expansion
d ( c ˜ ) = d ( c ) + E ( φ ) ( c ˜ − c ) + 1 2 d ″ ( c ) ( c ˜ − c ) 2 + o ( | c ˜ − c | 2 )
for c ˜ near c. Using the continuity of c ( u ) and choosing ε sufficiently small, we get that
d ( c ( u ) ) ≥ d ( c ) + E ( φ ) ( c ( u ) − c ) + 1 4 d ″ ( c ) ( c ( u ) − c ) 2 = c ( u ) E ( φ ) − F ( φ ) + 1 4 d ″ ( c ) ( c ( u ) − c ) 2 .
It follows from (18) and (19) that K ( φ c ( u ) ) = 4 p d ( c ) = K ( u ) . Since φ c ( u ) is a minimizer of I ( u ; ω , c ( u ) ) subject to the constraint K ( u ) = K ( φ c ( u ) ) , we then have
c ( u ) E ( u ) − F ( u ) = 1 2 ( I ( u ; ω , c ( u ) ) − K ( u ) ) ≥ 1 2 ( I ( φ c ( u ) ; ω , c ( u ) ) − K ( φ c ( u ) ) ) = d ( c ( u ) )
and
c ( u ) E ( u ) − F ( u ) ≥ c ( u ) E ( φ ) − F ( φ ) + 1 4 d ″ ( c ) ( c ( u ) − c ) 2 .

 □

Proof of Theorem 4.1 Suppose that φ ( ⋅ − η ) is unstable. Then there exists ε 0 and a sequence of initial data u k ( 0 ) satisfying
inf η ∥ u k ( 0 ) − φ ( ⋅ ) ∥ H 2 → 0 ;
however,
sup t inf η ∥ u k ( t ) − φ ( ⋅ − η ) ∥ H 2 ≥ ε 0 ,
where u k ( t ) is a solution of Eq. (12) with initial datum u k ( 0 ) . Then, by Theorem 2.1, u k is continuous in t, and there exist times t k such that
inf η ∥ u k ( t k ) − φ ( ⋅ − η ) ∥ H 2 = ε 0 .
(20)
When t k → 0 , ∥ u k ( 0 ) − φ ( ⋅ ) ∥ H 2 → 0 , E and F are invariants of (12) so that
E ( u k ( t k ) ) = E ( u k ( 0 ) ) → E ( φ ) , F ( u k ( t k ) ) = F ( u k ( 0 ) ) → F ( φ ) ,
(21)
by Lemma 4.3, we have
c ( u k ( t k ) ) [ E ( u k ( t k ) ) − E ( φ ) ] − [ F ( u k ( t k ) ) − F ( φ ) ] ≥ 1 4 d ″ ( c ) | c ( u k ( t k ) ) − c | 2 .

This implies that c ( u k ( t k ) ) → c , as k → ∞ , since u k ( t k ) is uniformly bounded for k.

The continuity of d implies that
lim k → ∞ K ( u k ( t k ) ) = lim k → ∞ ( 4 p d ( c ( u k ( t k ) ) ) ) = 4 p d ( c ) .
(22)
Using (17) and the fact that d ( c ) = c E ( φ ) − F ( φ ) , we have
1 2 I ( u k ( t k ) ) = c E ( u k ( t k ) ) − F ( u k ( t k ) ) + 1 2 K ( u k ( t k ) ) = d ( c ) − F ( u k ( t k ) ) + F ( φ ) − c ( E ( φ ) − E ( u k ( t k ) ) ) + 1 2 K ( u k ( t k ) ) ,
so it follows from (21) and (22) that
lim k → ∞ I ( u k ( t k ) ) = 2 ( p + 2 ) p d ( c ) .
(23)

From (22) and (23), u k ( t k ) is a minimizing sequence for the pair I, K and thus by Theorem 4.2 has a subsequence, named u k j ( t k j ) , that converges in H 2 to some φ. This contradicts (20). The proof is completed. □

Declarations

Acknowledgements

This work was supported by Grant No. 13-FF-46 of the Dicle University of Scientific Research Projects Coordination (DUBAP), Diyarbakir, Turkey.

Authors’ Affiliations

(1)
Department of Mathematics, Dicle University

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© Dündar and Polat; licensee Springer. 2013

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