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Blow-up results for vector-valued nonlinear heat equations with no gradient structure

Hatem Zaag

Universit´e de Cergy-Pontoise, Ecole Normale Sup´erieure ´

1 Introduction

We are interested in the following reaction-diffusion equation:

∂u

∂t = ∆u + (1 + iδ) | u |

p1

u, u(0, x) = u

0

(x), (1) where, δ ∈ IR, p ∈ (1, + ∞ ), p < (N + 2)/(N − 2) if N ≥ 3, and u

0

∈ H = W

1,p+1

(IR

N

, C) I ∩ L

(IR

N

, C). I

(1) is a special case of the vector-valued equation:

∂u

∂t = ∆u + F (u), u(x, 0) = u

0

(x), (2) where u(t) : x ∈ IR

N

→ IR

M

, F : IR

M

→ IR

M

is regular and F is not necessarily a gradient.

For simplicity, we focus on the study of (1) (results for equation (2) will also be presented in section 5).

Equation (1) appears in the study of various physical problems (plasma physics, nonlinear optics). See for example Levermore and Olivier [15] and the references inside. Blow-up results for vector-valued equations have been intensively studied in differential geometry. See for example a review paper by Hamilton [12].

The Cauchy problem for equation (1) can be solved in H. u(t), solution of (1) would exist either on [0, + ∞ ) (global existence), or only on [0, T ), with 0 < T < + ∞ . In this case, | u(t) |

H

→ + ∞ when t → T , we say: u(t) blows-up in finite time T in H. In this paper, we are interested in the finite time blow-up for equation (1).

If δ = 0 and u

0

(x) ∈ IR, then (1) can be considered as real-valued.

Blow-up in this real case has been studied by various authors. Relying on

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the use of monotony properties and maximum principle, Ball [1] and Levine [16] find in this case obstructions to the global in time existence for (1).

Other authors investigated the asymptotic behavior at blow-up of blow-up solutions of (1), δ = 0. See for example Weissler [20], see for a study in the scale of similarity variables Giga and Kohn [11], [10], [9], Filippas and Kohn [5], Filippas and Merle [6],... The notion of asymptotic profile (that is a function from which, after a time dependent scaling, u(t) approaches as t → T ) appears also in various papers: see for example Bricmont and Kupiainen [4], [3], Berger and Kohn [2] for a numerical study. In the scalar case and in one dimension, Herrero and Velazquez give a classification of possible blow-up profiles. They use the maximum principle and the decay in time of the number of oscillations of the solution. Some of their results are generalized to N dimensions in [19].

Most of the techniques used for δ = 0 in the cited papers can not be applied in the case δ 6 = 0, since (1) is complex-valued (no maximum principle applied), and the equation does not derive from a gradient.

Another method has been introduced in [18] in the case δ = 0 (see also [4]): Once an asymptotic profile is derived formally for (1), the existence of a solution u(t) which blows-up in finite time with the suggested profile is proved rigorously, using a nonlinear analysis of equation (2) near the given profile. This approach which does not use maximum principle allows us to find blow-up solutions for vector-valued heat equations (even with no gradient structure). In this paper, we aim at adapting this method to show the existence of a blow-up solution for equation (1) with δ 6 = 0.

Let us remark that the scalar case provides us with a blow-up solution if δ = 0. Unfortunately, this result is a one dimensional result and it fails when we perturb slightly the nonlinearity. Indeed, let us mention the case of the following vectorial equation:

∂u

∂t = ∆u + | u |

p1

u + i | u |

q1

u, u

|∂Ω

= 0 (3) with 1 < q < (p + 1)/2, the method of Ball [1] yields a blow-up solution u(t) : Ω → C where Ω is a bounded domain of IR I

N

, see appendix A for details.

We show that there exists δ

0

> 0 such that for each δ ∈ [ − δ

0

, δ

0

], equa- tion (1) has a blow-up solution. We give in addition a precise description of its blow-up behavior. Indeed,

Theorem 1 (Existence of a blow-up solution for equation (1) for

small δ)

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There exists δ

0

> 0 such that for each δ ∈ [ − δ

0

, δ

0

], there exist initial data u

0

such that equation (1) has a blow-up solution.

This Theorem follows directly from the following proposition which spec- ifies the behavior of u(t) near blow-up. Indeed, up to a time dependent scaling, u(t) approaches a universal profile

(p − 1 + (p − 1)

2

4(p − δ

2

) | z |

2

)

1+iδp−1

(4) when t → T . More precisely:

Proposition 1 (Existence of a blow-up solution for equation (1) with the profile (4) )

There exist δ

0

> 0, T

0

> 0 such that for each δ ∈ [ − δ

0

, δ

0

], for each T ∈ (0, T

0

], for each a ∈ IR

N

,

i) there exist initial data u

0

such that equation (1) has a blow-up solution u(x, t) on IR

N

× [0, T ) which blows-up in finite time T at only one blow-up point: a,

ii) moreover, we have

t

lim

T

k (T − t)

1+iδp−1

u(a+((T − t) | log(T − t) | )

12

z, t) − f

δ

(z)

1+iδ

k

L(

IR

N)

= 0 (5) with f

δ

(z) = (p − 1 + (p − 1)

2

4(p − δ

2

) | z |

2

)

p−11

. (6) iii) There exists u

∈ C (IR

N

\{ a } , C) I such that u(x, t) → u

(x) as t → T uniformly on compact subsets of IR

N

\{ a } , and

u

(x) ∼

"

8(p − δ

2

) | log | x − a ||

(p − 1)

2

| x − a |

2

#1+iδ

p−1

as x → a. (7)

Remark: Estimate (5) is really uniform in z ∈ IR

N

. In previous papers dealing with the case δ = 0, only Bricmont and Kupiainen [4] and Merle and Zaag [18] give such a uniform convergence. In most papers, the same kind convergence is proved, but only uniformly on smaller subsets ( for

| z | ≤ C/

p

| log(T − t) | in [5],...).

Remark: In fact, we show that property iii) is a consequence of ii). We

want to point out that for the heat equation (δ=0), iii) was known just in

dimension one using the decay in time of the number of oscillations of the

solution (Cf Herrero and Velazquez [13]).

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Remark: To prove Proposition 1, we linearize in a way equation (1) around f

δ1+iδ

, and give a nonlinear finite dimensional reduction of the problem.

Then, we solve the finite dimensional problem using index theory. The proof is more difficult than in [18], because of the vectorial structure, the presence of a coupling between coordinates, and the presence of one more neutral direction. These techniques give then as in [18] a stability result with respect to the initial data of the behavior described in Proposition 1 (see section 5).

Remark: Center manifold theory do not apply here. It fails to give a uniform estimate such as ii). One can point out that even if it works, a center manifold theory gives a convergence only uniform in the region {| z |

p

| log(T − t) | ≤ C } . For discussion in the case δ = 0, see Filippas and Kohn [5], page 834-835.

Remark: We see from (6) that 0 < δ

0

< √ p. Since equation (1) is rota- tion invariant, for each ω ∈ S

1

, we can find initial data u

0

such that the corresponding solution has the profile f

δ1+iδ

ω.

From this result, one can ask: what happens for δ > δ

0

? Does equation (1) still have blow-up solutions? We conjecture the existence of ˆ δ

0

> 0 such that for | δ | < ˆ δ

0

, equation (1) has blow-up solutions, while for | δ | > δ

0

, no blow-up is possible for solutions of equation (1). That is, all solutions are globally defined. Indeed, from the formal asymptotic analysis, one can remark that for | δ | > √ p, f

δ1+iδ

is no longer bounded, and the analysis fails. Another question arises: what happens with the critical value δ = ˆ δ

0

? Unfortunately, we are not able here to give a precise value of ˆ δ

0

and a rigorous proof of what is conjectured.

As an extension of Theorem 1, one can mention that using the same techniques, we have the same result for the following vector-valued equation:

du

dt = ∆u + | u |

p1

u + G(u), u(x, 0) = u

0

(x) (8) where

1) u(t) : x ∈ IR

N

→ IR

M

, p ∈ (1, + ∞ ), p < (N + 2)/(N − 2) if N ≥ 3, u

0

∈ H = W

1,p+1

(IR

N

, IR

M

) ∩ L

(IR

N

, IR

M

),

2) G : IR

M

→ IR

M

is a perturbation of | u |

p1

u satisfying: G(u) = G

1

( | u |

2

)u, | G(u) | ≤ C | u |

r

, | G(λu

1

) − G(λu

2

) | ≤ Cλ

r

| u

1

− u

2

| for | u

1

| , | u

2

| ≤ 1, λ ≥ 1, r ∈ [1, p), G

1

: IR

+

→ IR

+

,

Indeed,

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Theorem 2 (Existence of a blow-up solution for equation (8)) . There exist initial data u

0

such that equation (8) has a blow-up solution.

Let us mention briefly the organization of the paper. The proof of Propo- sition 1 relies strongly on a double-scale description of u(t), solution of (1).

We first give in section 2 an equivalent formulation of the problem in the scale of the well known similarity variables (see Giga and Kohn [11],..).

Then, working in the original scale, we prove in section 3 the existence of a single-point blow-up solution for equation (1) such that (5) holds. In section 4, we return to the original scale u(x, t) and use the invariance of equation (1) under the transformation (t

0

, λ) → u

λ

(x, t) = λ

1+iδp−1

u( √

λx, t

0

+ λt) to show that estimate (5) yields the equivalent (7) for the profile u

in the original scale. We conclude in section 5 by giving some comments about the stability of the result of Proposition 1 and detailing the case of equation (8) (M ≥ 3).

Without loss of generality, we can now assume that a = 0 and N = 1.

The same proof holds in higher dimensions (see [18] for the analysis of the case N ≥ 2). We write each complex quantity (number or function) z as z = z

1

+ iz

2

with z

1

, z

2

∈ IR.

The author wants to thank Professor F. Merle for his helpful suggestions and remarks.

2 Formulation of the problem

As we mentioned just before, the proof of Proposition 1 will be completed in two steps. In the first step (section 3), it is enough to construct u(t) a solution of equation (1) satisfying (5), since this implies directly that u(t) blows-up in finite time T at only one blow-up point: 0 (parts i) and ii) of Proposition 1). Indeed, it easily follows from (5) that lim

tT

| u(0, t) | = + ∞ , which means that u(t) blows-up in time T at the point 0, and

lim

tT

(T − t)

p−11

| u(b, t) | = 0 for b 6 = 0, which implies in turn that u(t) does not blow-up at b 6 = 0, and therefore blows-up only at the point 0. This last result follows directly from a Theorem by Giga and Kohn (Theorem 2.1 in [11]).

In a second step (section 4), we show how the behavior of the limiting profile u

(x) near the blow-up point (part iii) of Proposition 1) can be derived from the behavior of u(t) as t → T given by (5).

Hence, our first goal is to construct u(t) a solution of (1) satisfying (5).

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To have an idea about the blow-up growth of u, solution of equation (1), we compare this solution with a blow-up solution of the corresponding differential equation

du

dt = (1 + iδ) | u |

p1

u.

This solution is u(t) = e

((p − 1)(T − t))

1+iδp−1

, with T > 0, θ ∈ IR.

Now, we consider u, a solution of equation (1) which blows-up in finite time T > 0 at one blow-up point 0 ∈ IR. We expect u to grow with a similar rate near blow-up. If we introduce convenient “similarity variables”

y =

x Tt

s = − log(T − t) w(y, s) = (T − t)

1+iδp−1

u(x, t),

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then, we can look for bounded non zero solutions of the following equa- tion (which follows from (1) through (9)):

∂w

∂s = ∆w − 1

2 y ∇ w − (1 + iδ) w

p − 1 + (1 + iδ) | w |

p1

w. (10) 2.1 Formal asymptotic analysis

Since equation (10) is of heat type, one can ask whether it has self-similar solutions, or at least, approximate ones. We have the following lemma:

Lemma 2.1 (Formal asymptotic behavior of w) . i) The only self-similar solutions w(y, s) = v

0

(

y

s

) of (10) are the con- stant ones: v

0

≡ 0, or v

0

≡ κe

, with κ = (p − 1)

p−11

and θ ∈ IR.

ii) If equation (10) has a solution of the form w(y, s) =

+

X

j=0

1 s

j

v

j

( y

√ s ), (11)

with v

j

regular and bounded, then, there exists θ ∈ IR such that v

0

(z) = e

(p − 1 + (p − 1)

2

4(p − δ

2

) z

2

)

1+iδp−1

= e

f

δ

(z)

1+iδ

, (12)

where f

δ

(z)

1+iδ

is the suggested profile in (4).

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Proof:

i) The equations satisfied by such a v

0

are 0 = − 1

2 zv

00

(z) − (1 + iδ) v

0

p − 1 + (1 + iδ) | v

0

|

p1

v

0

, (13) and −

12

zv

00

(z) = v

000

(z). It is easy to see that the only solutions are the constant ones, and that −

pv01

+ | v

0

|

p1

v

0

= 0. This yields the conclusion.

ii) If we substitute the form (11) in equation (10) and set z =

ys

, we find (if s → + ∞ ) that v

0

satisfies (13). Searching a non constant solution v

0

(z) = ρ(z)e

iθ(z)

, with ρ > 0, one finds that v

0

(z) = e

(p − 1 + bz

2

)

1+iδp−1

, with b > 0, θ ∈ IR.

In fact, there is only one possible value of b. Indeed, if we substitute the expanded form (11) in equation (10) and compare elements of order

1

s

, we obtain F (z) = 0, where F (z) =

12

zv

00

+ v

000

12

zv

01

− (1 + iδ)

pv11

+ (1 + iδ) { (p − 1) | v

0

|

p3

v

0

(v

0,1

v

1,1

+ v

0,2

v

1,2

) + | v

0

|

p1

v

1

} , and v

j

= v

j,1

+ iv

j,2

, j = 1, 2. According to regularization properties of equation (10), it is natural to require that v

1

is C

2

, which implies that F is C

2

. F

00

(0) = 0 implies b =

4(p(p1)δ22)

.

Remark: Looking for approximate solutions of (10) or for solutions of (10) in the expanded form (11) is a well known approach used in various problems such as nonlinear optics, and also nonlinear heat equations (see for instance Galaktionov, Kurdyumov and Samarskii [7] for approximate self-similar so- lutions in the case of global existence (in time), see also Galaktionov and Vazquez [8] where an approximate solution is shown to be an admissible blow-up profile in the case of a heat equation with (1 + u) log

2

(1 + u) as a nonlinearity). Unfortunately, computation can not be carried out easily for the form (11) in the present case, and we are unable to show the exis- tence of a solution for equation (10) with such a form. In fact, instead of using this linear approach, we use a nonlinear one in section 3 to show that (10) actually has a solution w(y, s) which approaches (in L

y

) f

δ

(

y

s

)

1+iδ

as s → + ∞ . This approach (instead of the linear one) yields the stability of such a solution (see section 5).

2.2 Transformation of the problem

Using similarity variables (see (9)), we see that proving (5) is equivalent to

proving that (10) has a solution satisfying

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s

lim

→∞

k w(y, s) − f

δ

( y

√ s )

1+iδ

k

L

= 0, (14) where f

δ1+iδ

is given by (4).

In order to prove this, we will not linearize equation (10) around f

δ1+iδ

as it suggested by (14), because the linear operator of the linearized equation has two neutral modes which are difficult to control. We will instead use modulation theory and take advantage of the invariance of (10) under the action of S

1

(T

θ0

: w → e

0

w, for each θ

0

∈ IR): in fact, we introduce q(y, s) : [ − log T, + ∞ ) → C and I θ(s) : [ − log T, + ∞ ) → IR such that

(

w(y, s) = (ϕ(y, s) + q(y, s))e

iθ(s)

0 =

R

χ(y, s)(q

2

(y, s) − δq

1

(y, s))dµ (15) where

ϕ(y, s) = κ

(f

δ

( y

√ s ) + κ

2(p − δ

2

)s )

1+iδ

, κ = (p − 1)

p−11

(16) χ(y, s) = χ

0

( | y |

K

0

s

21

), (17)

χ

0

∈ C

0

([0, + ∞ ), [0, 1]), with χ

0

≡ 1 on [0, 1] and χ

0

≡ 0 on [2, + ∞ ], K

0

is a constant large enough, and

dµ(y) = e

y2/4

√ 4π . (18)

The introduced liberty degree θ(s) is fixed by the second equation of (15). It will appear in the course of the proof that this second equation makes one of the neutral modes of the perturbation q to be zero, which simplifies greatly the control of q.

One can remark that we don’t linearize (10) around e

iθ(s)

f

δ1+iδ

, but around e

iθ(s)

ϕ. Up to the natural action of S

1

(multiplication by κ

) which simplifies the study of the linear operator of the equation on q, these two expressions differ from each other by a term of order

1s

, so that (at least) some components of q are smaller that

1s

, which helps to have q(s) → 0 in L

y

as s → + ∞ .

Now, we claim that proving parts i) and ii) of Proposition 1 reduces to

proving the following proposition:

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Proposition 2.1 (Equivalent formulation of Proposition 1, i) and ii)) There exist δ

0

> 0, S

0

> 0, such that ∀ δ ∈ [ − δ

0

, δ

0

], ∀ s

0

≥ S

0

, ∃ q

s0

− ϕ(., s

0

) + H such that the system

( ∂q

∂s

(y, s) = {L

ϕ

− i

ds

} (q)(y, s) + B(q)(y, s) + R(θ, y, s)

0 =

R

χ(y, s)(q

2

(y, s) − δq

1

(y, s))dµ(y) (19) where

















L

ϕ

(q) = ∆q −

12

y. ∇ q − (1 + iδ)

pq1

+(1 + iδ) { (p − 1) | ϕ |

p3

ϕ(ϕ

1

q

1

+ ϕ

2

q

2

) + | ϕ |

p1

q } , B(q) = (1 + iδ) {| ϕ + q |

p1

(ϕ + q) − | ϕ |

p1

ϕ

− (p − 1) | ϕ |

p3

ϕ(ϕ

1

q

1

+ ϕ

2

q

2

) − | ϕ |

p1

q } , R(θ, y, s) = R

(y, s) − i

ds

ϕ,

R

(y, s) = −

∂ϕ∂s

+ ∆ϕ −

12

y. ∇ ϕ − (1 + iδ)

pϕ1

+ (1 + iδ) | ϕ |

p1

ϕ, (20) with initial data (q(y, s

0

), θ(s

0

)) = (q

s0

(y), 0) at s = s

0

, has a unique solution (q, θ) for s ≥ s

0

, satisfying lim

s+

k q(s) k

L

= 0, and ∃ θ

∈ IR such that θ(s) → θ

as s → + ∞ .

Indeed, due to (15), the first equation in system (19) is equivalent to (10), hence, it is equivalent to (1) (use (9)). In addition, once proposition 2.1 is proved, we have: k w(y, s) − e

i(θδlogκ)

f

δ

(

y

s

)

1+iδ

k

L

≤ k e

iθ(s)

(q(y, s) + ϕ(y, s)) − e

i(θδlogκ)

f

δ

(

y

s

)

1+iδ

k

L

(use (15))

≤ k q(s) k

L

+ k (e

iθ(s)

− e

)ϕ(y, s) k

L

+ k e

(ϕ(y, s) − κ

f

δ

(

ys

)

1+iδ

) k

L

≤ k q(s) k

L

+ C | θ(s) − θ

| + Cs

1

→ 0 as s → + ∞ (see (16)).

Therefore, w(y, s) approaches e

i(θδlogκ)

f

δ

(

y

s

)

1+iδ

in L

(IR) as s → + ∞ . Since (10) is rotation invariant, we can replace w by e

i(θδlogκ)

w to obtain (14), which is equivalent to (5) through similarity variables (see (9)).

Hence, we must study system (19) for (q, θ) ∈ L

(IR) × IR to solve the problem. Its evolution is mostly influenced by its linear part L

ϕ,θ

(q) = ( L

ϕ

− i

ds

)(q). Let us study more carefully this operator. L

ϕ,θ

is a IR-linear operator defined on D ( L

ϕ,θ

) ⊂ L

2

(IR, C, dµ). Since we are interested in the I behavior of (q(s), θ(s)) in L

(IR) × IR as s → + ∞ , let us consider the limit as s → + ∞ of L

ϕ,θ

(r) for a fixed r ∈ L

(IR, C) (note that I L

(IR, C) I ⊂ L

2

(IR, C, dµ)). I

Since θ(s) will be shown to have a limit when s → + ∞ , we can think

that the effect of

ds

appearing in the expression of L

ϕ,θ

(see (20)) will

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be negligible. Therefore, L

ϕ,θ

(r) → L ˜ (r) = ∆r −

12

y. ∇ r + (1 + iδ)r

1

as s → + ∞ (see (20) and (16)). The following lemma provides us with the spectral decomposition of ˜ L :

Lemma 2.2 (Eigenvalues of L ˜ ) .

i) L ˜ is a IR − linear operator defined on L

2

(IR, C, dµ) I and its eigenvalues are given by { 1 −

m2

| m ∈ IN } . Its eigenfunctions are given by

{ (1 + iδ)h

m

, ih

m

| m ∈ IN } where h

m

(y) =

[m2]

X

n=0

m!

n!(m − 2n)! ( − 1)

n

y

m2n

. (21) We have: L ˜ ((1 + iδ)h

m

) = (1 −

m2

)(1 + iδ)h

m

and L ˜ (ih

m

) = −

m2

ih

m

.

ii) Each r ∈ L

2

(IR, C, dµ) I can be uniquely written as

r(y) = (1 + iδ)(

P+m=0

r ˆ

1,m

h

m

(y)) + i(

P+m=0

r ˆ

2,m

h

m

(y)), where ˆ r

j,m

∈ IR.

Proof:

i) From [18], we know that { h

m

| m ∈ IN } is a total family in L

2

(IR, IR, dµ), and that (∆ −

12

y. ∇ )h

m

= −

m2

h

m

. Hence, we decompose each

r ∈ L

2

(IR, C, dµ) as I r(y) =

P+m=0

(r

1,m

+ ir

2,m

)h

m

(y).

λ ∈ IR is an eigenvalue for ˜ L ⇐⇒ ∃ r ∈ L

2

(IR, C, dµ), r I 6 = 0, L ˜ r = λr

⇐⇒ ∃ r 6 = 0 ∀ m ∈ IN

(

(1 −

m2

− λ) r

1,m

= 0 λ r

1,m

+( −

m2

− λ)r

2,m

= 0

⇐⇒ ∃ m ∈ IN λ = 1 −

m2

The computation of eigenfunctions is easy and we shall skip it.

ii) We write r = (1 + iδ)˜ r

1

+ i˜ r

2

, with ˜ r

j

∈ L

2

(IR, IR, dµ), and use the fact that { h

m

| m ∈ IN } is a total family in L

2

(IR, IR, dµ).

Let us consider (q(s), θ(s)) a solution of system (19). We will use an integral formulation of its first equation in terms of the fundamental solution of L

ϕ

. We want k q(s) k

L

→ 0 as s → + ∞ . This L

control will result from the L

control of (1 − χ(y, s))q(y, s) and χ(y, s)q(y, s) (see (17) for χ):

1) in the “regular” region | y | ≥ K

0

s, L

ϕ

behaves in L

2

(IR, C, dµ) I like an operator with a fully negative spectrum. We will show from (20) that the fundamental solution of L

ϕ

between s

0

and s

1

> s

0

is a strict contraction from L

( | y | ≥ K

0

s) to L

(IR). Therefore, the control of (1 − χ(y, s))q(y, s) in L

(IR) will be done without difficulties.

2) in the “singular” region | y | ≤ K

0

s, L

ϕ

behaves in L

2

(IR, C, dµ) like I

L ˜ . In order to control χq(y, s), we expand it with respect to the spectrum

of ˜ L in L

2

(IR, C, dµ), but we will control I χq in L

(IR) and not only in

L

2

(IR, C, dµ) (see section 3 for the rigorous analysis). I

(11)

By lemma 2.2, ˜ L has two expanding directions ((1 + iδ)h

0

, (1 + iδ)h

1

), two null ones ((1 + iδ)h

2

, ih

0

) and countably many negative ones.

Here, the situation is a bit more complicated than in [18], because we have two null directions (instead of only one).

Our strategy to control all the components of χq so that k χq(s) k

L

→ 0 as s → + ∞ is to control the part of χq corresponding to the negative spectrum of ˜ L and the one parallel to (1 + iδ)h

2

(which corresponds to the null eigenvalue) as in [18]. The component parallel to ih

0

(which corresponds also to the the null eigenvalue) has been fixed by the second equation of (19) to be zero (using modulation theory and the phase invariance of the equation).

However, the analysis of system (19) is longer than the equivalent anal- ysis in [18], because of terms with

ds

, and the presence of strong coupling between the two scalar parts: ˜ q

1

and ˜ q

2

of q, satisfying: q = (1 + iδ)˜ q

1

+ i˜ q

2

. Fortunately,

ds

will be controlled near the profile ϕ (see 16), and, although the coupling will be of critical size, its effect will be controlled by δ, which can be chosen small.

3 Existence of a blow-up solution for equation (2)

In this section, we prove proposition 2.1, which implies parts i) and ii) of Proposition 1 and then Theorem 1.

3.1 Geometrical property for q

As in [18], the convergence of k q(s) k

L

to zero as s → + ∞ will follow from a geometrical property: q(s) ∈ V

A

(s), where V

A

(s) ⊂ L

(IR, C) shrinks to I q ≡ 0 as s → + ∞ . The structure of V

A

(s) respects the free-boundary moving in q at the rate √

s, and also the eigenfunctions of the operator ˜ L (Cf lemma 2.2).

In order to define V

A

(s), we introduce the following useful notations:

For each g ∈ L

(IR, IR) and s > 0, we define g

b

(y, s) = χ(y, s)g(y) and

g

e

(y, s) = (1 − χ(y, s))g(y). Since L

(IR, IR) ⊂ L

2

(IR, IR, dµ), we introduce

for each m ∈ IN, g

m

(s) as the L

2

(IR, IR, dµ) projection of g

b

(y, s) on h

m

, (Cf

(21)). We also let g

(y, s) = P

(g

b

) and g

(y, s) = P

(g

b

), where P

and

P

are the L

2

(IR, IR, dµ) projectors respectively on Vect { h

m

| m ≥ 3 } and

(12)

Vect { h

m

| m ≥ 1 } . Thus, we write either g(y) =

2

X

m=0

g

m

(s)h

m

(y) + g

(y, s) + g

e

(y, s) (22) or

g(y) = g

0

(s)h

0

(y) + g

(y, s) + g

e

(y, s). (23) For each z ∈ C, we write in a unique way I z = (1 + iδ)˜ z

1

+ i˜ z

2

, where ˜ z

1

and ˜ z

2

are real.

Hence, if r ∈ L

(IR, C), we write: I r(y) = (1 + iδ)˜ r

1

(y) + i˜ r

2

(y) and expand ˜ r

1

and ˜ r

2

respectively as in (22) and (23). Thus, we write: r(y) = (1 + iδ)˜ r

1

(y) + i˜ r

2

(y)

= (1 + iδ) {

P2m=0

r ˜

1,m

(s)h

m

(y) + ˜ r

1,

(y, s) + ˜ r

1,e

(y, s) }

+ i { r ˜

2,0

(s)h

0

(y) + ˜ r

2,

(y, s) + ˜ r

2,e

(y, s) } . (24) Definition 3.1 For each A > 0, for each s > 0, let V

A

(s) be the set of all functions r in L

(IR, C) I such that

| r ˜

1,m

(s) | ≤ As

2

, f or m = 0, 1,

| r ˜

1,2

(s) | ≤ A

2

(log s)s

2

, | ˜ r

2,0

(s) | ≤ As

2

,

| r ˜

1,

(y, s) | ≤ A(1 + | y |

3

)s

2

, | ˜ r

2,

(y, s) | ≤ A(1 + | y |

3

)s

2

, k ˜ r

1,e

(s) k

L

≤ A

2

s

12

, k r ˜

2,e

(s) k

L

≤ A

2

s

12

,

where r is given by (24).

Remark: We note that L

(IR, C) I ⊂ L

2

(IR, C, dµ), which justifies the ex- I pansion with respect to the eigenvalues of ˜ L in definition 3.1.

Remark: It is easy to see that if q(s) ∈ V

A

(s), then ∀ y ∈ IR, | q(y, s) | ≤ C(A)s

1/2

(see [18] for details). Therefore, k q(s) k

L(

IR

,

C I

)

→ 0 as s → + ∞ , and we obtain a convergence in L

(IR, C) and not only in I L

2

(IR, C, dµ), as in I other papers (see [5],..). We emphasize that a convergence in L

2

(IR, C, dµ) I or more generally in H

m

(IR, C, dµ) yields a convergence in I L

([ − R, R], C) I for each R > 0, and never a uniform convergence on IR.

With this remark, we claim that proposition 2.1 follows from the follow-

ing proposition:

(13)

Proposition 3.1 Equivalent formulation of Proposition 1, i) and ii) There exists A > 0, δ

0

> 0, S

0

> 0, such that ∀ δ ∈ [ − δ

0

, δ

0

], ∀ s

0

≥ S

0

,

∃ (d

0

, d

1

) ∈ IR

2

such that system (19) with initial data at s = s

0





q

d0,d1

(y, s

0

) = (1 + iδ)f

0

(

ys0

)

p

(d

0

+ d

1

y/ √

s

0

) − (

sα

0

)

1+iδ

+ i

sα

0

(sin[δ log(

sα

0

)] − δ cos[δ log(

sα

0

)])f

0

(

ys0

)

p

β(s

0

) θ(s

0

) = 0

(25) (where f

0

is given by (6),

α = κ

2(p − δ

2

) , β(s

0

) =

R

f

0

(

ys0

)

p

χ(y, s

0

)dµ(y)

R

χ(y, s

0

)dµ(y) ) (26) has a unique solution (q, θ)

d0,d1

for s ≥ s

0

, satisfying q(s) ∈ V

A

(s), ∀ s ≥ s

0

. Indeed, once proposition 3.1 is proved, we take for q

s0

the expression in (25). From q(s) ∈ V

A

(s), ∀ s ≥ s

0

, we have k q(s) k

L

→ 0 as s → + ∞ , and ∃ θ

such that θ(s) → θ

as s → + ∞ . Indeed, we have the following lemma:

Lemma 3.1 ∀ A > 0, ∃ s

3

(A) > 0 such that ∀ δ ∈ [ − 1, 1], ∀ s ≥ s

3

(A), if q(s) ∈ V

A

(s), then |

ds

(s) | ≤

sC2

.

This lemma implies

Rs+

0

|

ds

(s) | ds < + ∞ , which gives θ

such that θ(s) → θ

as s → + ∞ . We give the proof of this lemma in the next subsection.

In order to understand the dynamics of q and θ, we derive the equations satisfied by ˜ q

1

and ˜ q

2

(q(y, s) = (1 + iδ)˜ q

1

(y, s) + i˜ q

2

(y, s), Cf decomposition (24)) and θ:

Lemma 3.2 (Equations satisfied by q ˜

1

, q ˜

2

and θ) If q satisfies (19) for s ≥ s

0

, then:

∂ q ˜

1

∂s (y, s) = ( L + V

1,1

(y, s) + δ dθ

ds (s))(˜ q

1

) + (V

1,2

(y, s) + dθ ds (s))˜ q

2

+ B ˜

1

(q(y, s)) + ˜ R

1

(θ, y, s), (27)

∂ q ˜

2

∂s (y, s) = (V

2,1

− (1 + δ

2

) dθ

ds (s))˜ q

1

+ ( L − 1 + V

2,2

(y, s) − δ dθ ds (s))˜ q

2

+ B ˜

2

(q(y, s)) + ˜ R

2

(θ, y, s), (28) dθ

ds

Z

χ(y, s)((1 + δ

2

) ˜ ϕ

1

+ δ ϕ ˜

2

+ (1 + δ

2

)˜ q

1

+ δ q ˜

2

)dµ

(14)

=

Z

χ( L − 1)˜ q

2

dµ +

Z

∂χ

∂s q ˜

2

dµ +

Z

χ(V

2,1

q ˜

1

+ V

2,2

q ˜

2

)dµ +

Z

χ B ˜

2

(q)dµ +

Z

χ(y, s) ˜ R

2

(y, s), (29) where

L = ∆ − 1

2 y. ∇ + 1, (30)









V

1,1

(y, s) = (1 − δ

2

)( | ϕ |

p1

p11

) + (p − 1) | ϕ |

p3

21

− δ

2

ϕ

22

) − 1 V

1,2

(y, s) = − δ( | ϕ |

p1

p11

) + (p − 1) | ϕ |

p3

1

− δϕ

2

2

V

2,1

(y, s) = (1 + δ

2

) { δ( | ϕ |

p1

p11

) + (p − 1) | ϕ |

p3

1

+ δϕ

2

2

} V

2,2

(y, s) = (1 + δ

2

) { ( | ϕ |

p1

p11

) + (p − 1) | ϕ |

p3

ϕ

22

} ,

ϕ is given by (16), (1 + iδ) ˜ B

1

+ i B ˜

2

= B , (1 + iδ) ˜ R

1

+ i R ˜

2

= R, and B, R are given by (20).

Proof: (27) and (28) follow directly from (19). For (29), we note that we derive form (19)

dsd R

χ(y, s)˜ q

2

(y, s)dµ(y) = 0 (˜ q

2

= q

2

− δq

1

). Therefore

R

χ(y, s)

∂˜∂sq2

(y, s)dµ(y) = −

R ∂χ∂s

(y, s)˜ q

2

(y, s)dµ(y). Multiplying (28) by χ and integrating with respect to dµ yields (29).

The proof of Proposition 3.1 follows the general ideas developed in [18].

Indeed, it is divided in two parts:

-In a first part, we reduce the problem of the control in V

A

(s) of all the components of q(s) to the problem of controlling (˜ q

1,0

(s), q ˜

1,1

(s)), which are the components of q corresponding to expanding directions of ˜ L (see (24) and lemma 2.2). That is, we reduce an infinite dimensional problem to a finite dimensional one.

-The second part of the proof is devoted to the solving of the finite dimen- sional problem, using 2-dimensional dynamics of (˜ q

1,0

, q ˜

1,1

)(s) and a topolog- ical argument (index theory) based on the variation of the 2-dimensional pa- rameter (d

0

, d

1

) appearing in the expression (25) of initial data q

d0,d1

(y, s

0

).

3.2 Proof of the geometrical property on q(s)

First, we prove lemma 3.1 which insures that proposition 3.1 implies propo- sition 2.1 and then Proposition 1 i) and ii).

Proof of lemma 3.1:

We control

ds

thanks to equation (29). Let us estimate each term ap- pearing in:

If s

0

≥ s

3

(A), we have the following estimates.

(15)

- Since q ∈ V

A

, the left-hand side of (29) is ≥ C > 0.

- Since L is self-adjoint in L

2

(IR, dµ),

R

χ( L − 1)˜ q

2

dµ =

R

( L − 1)χ q ˜

2

dµ =

R

(

∂y2χ2

12

y

∂χ∂y

)˜ q

2

e

y2/8e−y2/8

dy. From (17), |

∂y2χ2

12

y

∂χ∂y

| ≤ C, and

∂y2χ2

1

2

y

∂χ∂y

≡ 0 for | y | ≤ K

0

s. Hence, we can bound e

y2/8

by e

K02s/8

, and use q(s) ∈ V

A

(s) to obtain |

R

χ( L − 1)˜ q

2

dµ | ≤ Ce

s

(if K

0

is large enough).

- The same argument yields |

R ∂χ∂s

q ˜

2

dµ | ≤ Ce

s

.

- We have | V

i,j

(y, s) | ≤ Cs

1

(1 + | y |

2

) (see lemma B.1 in appendix B). Combining this with Definition 3.1, we get |

R

χ(V

2,1

q ˜

1

+ V

2,2

q ˜

2

)dµ | ≤ Cs

3

log s.

- We have | χ(y, s)B(q(y, s)) | ≤ C | q |

2

for q(s) ∈ V

A

(s) (see lemma B.4).

Therefore, |

R

χ B ˜

2

(q)dµ | ≤

R

χ | q |

2

dµ ≤ Cs

3

.

- From (20), |

R

χ(y, s) ˜ R

2

(y, s) | ≤

sC2

(see lemma B.5).

Combining all the previous estimates gives: |

ds

| ≤

sC2

.

Now, we give the proof of proposition 3.1 following the plan announced in the previous subsection.

Part I: Reduction to a finite dimensional problem

Here, (q, θ) stands for a solution of system (19) with initial data (25). We show through a priori estimates that finding (d

0

, d

1

) ∈ IR

2

such that ∀ s ≥ s

0

q(s) ∈ V

A

(s) is equivalent to finding (d

0

, d

1

) ∈ IR

2

such that ∀ s ≥ s

0

(˜ q

1,0

(s), q ˜

1,1

(s)) ∈ V ˆ

A

(s), where

Definition 3.2 For each A > 0, for each s > 0, we define V ˆ

A

(s) as being the set [ −

sA2

,

sA2

]

2

⊂ IR

2

.

Proposition 3.2 (Control of q(s) by (˜ q

1,0

(s), q ˜

1,1

(s)) in V ˜

A

(s)) There exists A

1

> 0 such that for each A ≥ A

1

, there exists δ

1

(A) > 0, s

1

(A) > 0 such that for each δ ∈ [ − δ

1

, δ

1

], s

0

≥ s

1

(A), we have the following properties:

-if (d

0

, d

1

) is chosen so that (˜ q

1,0

(s

0

), q ˜

1,1

(s

0

)) ∈ V ˆ

A

(s

0

), and,

-if for s

1

≥ s

0

, we have ∀ s ∈ [s

0

, s

1

], q(s) ∈ V

A

(s) and q(s

1

) ∈ ∂V

A

(s

1

), then

i) (˜ q

1,0

(s

1

), q ˜

1,1

(s

1

)) ∈ ∂ V ˆ

A

(s

1

),

ii) (transversality) there exists η

0

> 0 such that ∀ η ∈ (0, η

0

), (˜ q

1,0

(s

1

+ η), q ˜

1,1

(s

1

+ η)) 6∈ V ˆ

A

(s

1

+ η) (hence, q(s

1

+ η) 6∈ V

A

(s

1

+ η)).

Proof: see Proof of Proposition 3.2 below.

Now, we fix A ≥ A

1

, and δ

0

= δ

1

. We note q(d

0

, d

1

) = q

d0,d1

(see

proposition 3.1).

(16)

Part II: Topological argument for the finite dimensional prob- lem

In the following proposition, we initialize the finite dimensional problem and study the Cauchy problem for system (19).

Proposition 3.3 (Initialization and Cauchy problem for system (19)) There exists s

2

(A) > 0 such that for each δ ∈ [ − δ

0

, δ

0

], for each s

0

≥ s

2

(A),

i) there exists a set D

s0

⊂ IR

2

topologically equivalent to a square with the following property:

q(d

0

, d

1

, s

0

) ∈ V

A

(s

0

) if and only if (d

0

, d

1

) ∈ D

s0

.

ii) For each (d

0

, d

1

) ∈ D

s0

, ∃ S = S(d

0

, d

1

) > s

0

(maximal) such that sys- tem (19) with initial data (25) at s = s

0

has a unique solution (q, θ)(d

0

, d

1

) on [s

0

, S ), with q and θ C

2

and q(s) ∈ V

A+1

(s), ∀ s ∈ [s

0

, S).

iii) (q, θ) is continuous with respect to (d

0

, d

1

, s).

Proof:

i) From (25), we have

˜

q

1

(d

0

, d

1

, y, s

0

) = f

0

(

ys0

)

p

(d

0

+ d

1y

s0

) −

sα0

cos[δ log(

sα

0

)] and

˜

q

2

(d

0

, d

1

, y, s

0

) = −

sα0

(δ − sin[δ log(

sα

0

)])(1 − β(s

0

)f

0

(

ys0

)

p

). The expression of ˜ q

1

is similar to the expression of initial data (31) for the similar equation (15) in [18]. ˜ q

2

is a sum of two terms appearing in the mentioned formula (31) in [18]. Hence, one can adapt without difficulties lemmas 3.5 and 3.9 of [18] to conclude (note that ˜ q

2,0

(d

0

, d

1

, s

0

) = 0).

ii) As if to use (15) in a reverse way, we introduce

w(y, s) = e

iθ(s)

(q(y, s) + ϕ(y, s)). (31) Therefore, our problem is equivalent to the following system in (w, θ):

∂w

∂s = ∆w − 1

2 y. ∇ w − (1 + iδ) w

p − 1 + (1 + iδ) | w |

p1

w (32) F ((θ(s), s) = 0

where

F (θ, s) = cos(θ)(w

2,0

(s) − δw

1,0

(s))+sin(θ)( − w

1,0

(s) − δw

2,0

(s)) − ϕ ˜

2,0

(s) = 0, (33) with initial data

w(d

0

, d

1

, s

0

) = q(d

0

, d

1

, s

0

) + ϕ(s

0

), (34)

θ(s

0

) = 0. (35)

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