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HAL Id: hal-00009236

https://hal.archives-ouvertes.fr/hal-00009236

Submitted on 29 Sep 2005

HAL is a multi-disciplinary open access archive for the deposit and dissemination of sci- entific research documents, whether they are pub- lished or not. The documents may come from teaching and research institutions in France or

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DETERMINATION OF A TWO-DIMENSIONAL HEAT SOURCE : UNIQUENESS, REGULARIZATION

AND ERROR ESTIMATE

Dang Duc Trong, Pham Hoang Quan, Alain Pham Ngoc Dinh

To cite this version:

Dang Duc Trong, Pham Hoang Quan, Alain Pham Ngoc Dinh. DETERMINATION OF A TWO- DIMENSIONAL HEAT SOURCE : UNIQUENESS, REGULARIZATION AND ERROR ESTIMATE.

Journal of Computational and Applied Mathematics, Elsevier, 2006, 191, pp.50-67. �hal-00009236�

(2)

DETERMINATION OF A TWO-DIMENSIONAL HEAT SOURCE : UNIQUENESS, REGULARIZATION AND ERROR ESTIMATE

D. D. Trong, P. H. Quan by

HoChiMinh City National University, Department of Mathematics and Informatics 227 Nguyen Van Cu, Q5, HoChiMinh City, Vietnam

Email: ddtrong@mathdep.hcmuns.edu.vn

&

P. N. Dinh Alain

Mathematics Department, Mapmo UMR 6628, BP 67-59 45067, Orleans cedex, France

Email: alain.pham@univ-orleans.fr

Abstract : Let Q be a heat conduction body and let ' = ' ( t ) be given. We consider the problem of nding a two-dimensional heat source having the form ' ( t ) f ( x;y ) in Q . The problem is ill-posed. Assuming @Q is insulated and '

6

0, we show that the heat source is dened uniquely by the temperature history on @Q and the temperature distribution in Q at the initial time t = 0 and at the nal time t = 1. Using the method of truncated integration and the Fourier transform, we construct regularized solutions and derive explicitly error estimate.

Key words : error estimate, Fourier transform, ill-posed problems, heat-conduction, heat source, truncated integration.

Mathematics Subject Classication 2000: 35K05, 35K20, 35R30, 42A38

1. Introduction

Let Q be a heat conduction body having a constant conductivity, as- sumed to be equal 1, and having an insulated boundary. In this paper, we consider the problem of identifying a heat source in the inside of Q from the temperature history on a part of @Q and the temperature dis- tribution in Q at the initial time t = 0 and at the nal time t = 1, say.

In other words, the problem has Cauchy data on a part of the boundary.

The problem has been studied intensively for the last three decades (see,

e.g., [STY, WZ, I1, I2, LZ, ATL]). Letting u be the temperature in Q and

(3)

F = F ( x;y;t;u ) be the heat source, one has the equation

?

@u @t + u = F ( x;y;t;u ) :

The problem is severely ill-posed. In fact, because of the extreme sensitiveness to measurement errors (see, e.g., [BBC]), the inverse heat source problem is dicult. Measured data is usually the result of discretely experimental measurements and, of course, is subject to error. Hence, a solution corresponding to the data does not always exist and moreover, solutions, event thought they exist, do not depend continuously on the given data. This, of course, makes a numerical treatment impossible.

Thus, one has to resort to a regularization.

To simplify the problem, many preassumptions on the form of the heat source had been given. Roughly speaking, we can approximate the function F ( x;y;t;u ) by a function which has the form

N

X

n

=0

n ( u ) ' n ( t ) f n ( x;y ) The rst order of the latter form can be written as

F

0

( u ) + '

0

( t ) + f

0

( x;y ) + '

1

( t ) f

1

( x;y ) + :::

In [I1, I2], the author assumed that

F ( x;y;t;u ) = g

0

( x;t ) + f

1

( x ) g

1

( t ) + f

2

( t ) g

2

( x ) where f

1

;f

2

are unknown. In [LZ],

F ( x;y;t;u ) = f ( u ) + r ( x;t )

where f is unknown (see also [K] for a similar form of the heat source).

In [STY, Y, CE1, CE2], we get the separated form F ( x;y;t;u ) = ( t ) f ( x ) in which one of two functions is unknown.

Now, in the present paper, for simplicity, as in [ATL], we shall consider

a model in which the heat source has the separated form ' ( t ) f ( x;y ) where

f is unknown. As we shall see, with minimum smoothness assumption,

(4)

the given Cauchy data is sucient to the uniqueness of solution. However, as discussed the problem is still ill - posed.

Precisely, we assume that Q is represented by the square (0 ; 1)

(0 ; 1).

Letting u = u ( x;y;t ) be the temperature in Q , we consider the problem of identifying a pair of functions ( u;f ) satisfying

?

@u @t + u = ' ( t ) f ( x;y ) (1) for ( x;y;t )

2

Q

(0 ; 1).

Since the boundary of Q is insulated, we have

u x (0 ;y;t ) = u x (1 ;y;t ) = 0 ;

u y ( x; 0 ;t ) = u y ( x; 1 ;t ) = 0 ; ( x;y;t )

2

Q

(0 ; 1) : (2) Finally, we have the temperature history on a part of @Q

u (1 ;y;t ) = u ( x; 1 ;t ) = 0 ( x;y;t )

2

Q

(0 ; 1) ; (3) and the temperature distribution in Q at t = 0 and t = 1,

u ( x;y; 0) = 0; u ( x;y; 1) = g ( x;y ) ( x;y )

2

Q: (4) Here, ';g are given functions. In (3), (4) the conditions, in which u (1 ;y;t ), u ( x; 1 ;t ), u ( x;y; 0) are vanished, are simplied. In fact, the method of our paper can be thoroughly applied to the problem associated with more general data. Hence, to simplify computation and to point out clearly main ideas of the method, we only consider the simplied conditions as in (3), (4).

Our problem is equivalent to the one of nding the function f = f ( x;y ) satisfying a Volterra equation of the rst kind (see, e.g., [F])

K ' f ( x;y ) =

?

g ( x;y ) (5) for ( x;y )

2

Q , where

N ( x;y;t ; ;; ) =

= 1

4 ( t

?

) exp

?

( y

?

)

2

4( t

?

)

exp

?

( x

?

)

2

4( t

?

)

+ exp

?

( x + )

2

4( t

?

)

; K ' f ( x;y ) =

1

Z

0 1

Z

0 1

Z

0

N ( x;y; 1; ;; ) ' ( ) f ( ; ) ddd:

(5)

We note at once that the problem of existence of a solution is not considered here. The set of the ( ';g )'s for which the system (1)-(4) has no solution is dense in L

2

(0 ; 1)

L

2

( Q ). Indeed, from (5) we can show that g is smooth if f

2

L

2

( Q ), '

2

L

2

(0 ; 1). However, in practice, g and ' come from experimental measurements and thus given as nite sets of points that are conveniently patched into L

2

-functions. Hence g is in general non-smooth. With these non-exact data, the system (1)-(4) usually has no solution. Thus, as mentioned, we deal with a problem that possibly has not a solution and hence we would have to resort to a regularization. If we denote by ( g

0

;'

0

) the (probably unknown) exact data corresponding to an exact solution ( u

0

;f

0

) of the system (1)-(4) then, from the (known) non- exact data ( g;' ) approximating ( g

0

;'

0

), we shall construct regularized solutions of (1)-(4).

As we shown in (5), the integral operator K ' depends on the non- ex- act data ' which implies that K ' is also non-exact. Hence, it is dicult to derive error estimate of a regularization method. In the case of one spatial dimension, the linear integral equation has been treated widely in the past few decades (see, e.g., [G, B, TA, ADT] and our recent paper [ATL]). Al- though the mathematical literature in the one-dimensional case is rather impressive, it is quite scarce in the two dimensional case. In the present paper, using a variational form of (1)-(4) we shall transform the problem to the one of nding f from its Fourier transform calculated from the giv- en data ( g;' ) (see Lemma 1 below). Assuming the discrepancy between the exact data ( g

0

;'

0

) and the non-exact data ( g;' ) is of order " > 0, we shall use a new method of truncated integration to construct (from the non-exact data ( g;' )) a regularized solution f " . Moreover, the error between f " and the exact solution f

0

(which depends on the properties of '

0

and the smoothness of f

0

) will be given explicitly. The remainder of the paper is divided into two sections. In Section 2, we shall set some notations and state main results of our paper. In Section 3, we give the proofs of the main results.

2. Notations and Main Results

We recall that Q = (0 ; 1)

(0 ; 1). We denote by C ([0 ; 1] ;H

1

( Q )) the set

of continuous functions u ( :;t ) : [0 ; 1]

!

H

1

( Q ) and by C

1

([0 ; 1] ;L

2

( Q ))

the set of C

1

-functions u ( :;t ) : [0 ; 1]

!

L

2

( Q ). From now on, we shall

assume that g

2

L

2

( Q ) and '

2

L

2

(0 ; 1). We also denote by c ( : ) ;s ( : )

respectively the functions cos ( : ) ; sin ( : ) for short. From (1)-(2) we get

(6)

?

dt < u; > d

?

< u x ; x >

?

< u y ; y > = ' < f; >

8 2

H

1

( Q ) (6) where <;> is the inner product in L

2

( Q ).

Using (6), we rst have the following Lemma.

Lemma 1

If u

2

C

1

([0 ; 1]; L

2

( Q ))

\

C ([0 ; 1]; H

1

( Q )) ;f

2

L

2

( Q ) satisfy (3), (4), (6) then, for all ;

2C

,

e

2+

2

:

1

Z

0 1

Z

0

g ( x;y ) c ( x ) c ( y ) dxdy = (7)

? 1

Z

0

e

(

2+

2)

t ' ( t ) dt

1

Z

0 1

Z

0

f ( x;y ) c ( x ) c ( y ) dxdy We note that, it may undergo nontrivial changes when applied (5) to get an equation as (7).

From Lemma 1, we have in formally

1

Z

0 1

Z

0

f ( x;y ) c ( x ) c ( y ) dxdy =

?

e

2+

2R1

0 1

R

0

g ( x;y ) c ( x ) c ( y ) dxdy

1

R

0

e

(

2+

2)

t ' ( t ) dt : Hence, the function f is possibly identied if the set

8

<

:

( ; )

2R2j

1

Z

0

e

(

2+

2)

t ' ( t ) dt = 0

9

=

;

is negligible in an appropriate sense. In fact, from the properties of ana- lytic functions, we can show that, if '

6

0, the set is a union of countable concentric circles and, hence, the Lebesgue measure of the set is zero.

Moreover, we have

(7)

Lemma 2

Let '

0 2

L

2

(0 ; 1) and R > 0. Put

0

( ) =

1

Z

0

e t

2

'

0

( t ) dt

B R =

n

( ; )

j

0

(

p

2

+

2

) < R

o

v

0

( t ) = t

Z

1

'

0

( s ) ds:

If there exists a

2

(0 ; 1) such that v

0

is nonpositive (or nonnegative) on [ ; 1] and that v

0 6

0 on [ ; 1] then we can nd constants ;R

0 2

(0 ; 1) ;C

0

> 0 independent of R such that

m ( B R )

C

0

R for all 0 < R

R

0

; where m ( B R ) is the Lebesgue measure of B R .

The set of the function '

0

satisfying Lemma 2 is very large. For example, if

'

0

( t ) = (1

?

t ) m ( a + (1

?

t ) ( t )) ;m integer

0 with a

6

= 0 ;

2

L

2

(0 ; 1) ; then v

0

satises the condition of Lemma 2. Now, we have the uniqueness result.

Theorem 1

Let u

1

;u

22

C

1

([0 ; 1]; L

2

( Q ))

\

C ([0 ; 1]; H

1

( Q )) and f

1

;f

22

L

2

( Q ).

If u i ;f i satisfy (1)-(4) ( i = 1 ; 2) and '

6

0, then ( u

1

;f

1

) = ( u

2

;f

2

) : We give two regularization results :

Theorem 2 Let C

0

;" > 0 and let '

0 2

L

2

(0 ; 1) ;g

0 2

L

2

( Q ) and ( u

0

;f

0

) be the exact solution of (1)-(4) corresponding ( '

0

;g

0

) in right hand side. Assume that ';g satisfy

k

'

?

'

0k

L

2(0

;

1)

< ";

k

g

?

g

0k

L

2(

Q

)

< " (8)

(8)

and ' ( t ) > C

0

;'

0

( t ) > C

0

a. e. on (0 ; 1).

Then from g;' we can construct a regularized solution f " , such that

" lim

!0k

f "

?

f

0k

L

2(

Q

)

= 0 (9) If we assume, in addition, that f

0 2

H

2

( Q ), then

k

f "

?

f

0k

L

2(

Q

)

4

s

e

3

C

04

( C

0

+

k

g

0k

L

2(

Q

)

+ 1)

2

" + 384

2 k

f

0k2H2

(Q)

"

1

=

8

: Theorem 3 Let " > 0 ;a

2 ?

0 ;

12

and let assumptions of Lemma 2 hold. If g;' are the measured data satisfying

k

'

?

'

0k

L

2(0

;

1)

< " and

k

g

?

g

0k

L

2(

Q

)

< ":

then, for each a

2 ?

0 ;

12

, we can construct from g;' a function f " such that

" lim

!0k

f "

?

f

0k

L

2(

Q

)

= 0 :

Moreover, if f

0 2

H

2

( Q ) then for each b

2?

max

0 ;

1?44

a ;

1?22

a

, we can nd C b > 0 ; b > 0 independent of f

0

;g

0

;'

0

;" such that

k

f "

?

f

0k

L

2(

Q

)

s

C b "

b

+ 384

2 k

f

0k2

H

2(

Q

)

b ln 1 "

?1

=

2

: 3. Proofs

Proof of Lemma 1

Choosing ( x;y ) = c ( x ) c ( y ) in (6), we get

?

dt d

1

Z

0 1

Z

0

u ( x;y;t ) c ( x ) c ( y ) dxdy +

1

Z

0 1

Z

0

u x ( x;y;t ) s ( x ) c ( y ) dxdy +

1

Z

0 1

Z

0

u y ( x;y;t ) c ( x ) s ( y ) dxdy = ' ( t )

1

Z

0 1

Z

0

f ( x;y ) c ( x ) c ( y ) dxdy: (10)

(9)

Since u (1 ;y;t ) = 0, we have

1

Z

0 1

Z

0

u x ( x;y;t ) s ( x ) c ( y ) dxdy =

?

1

Z

0 1

Z

0

u ( x;y;t ) c ( x ) c ( y ) dxdy: (11) Similarly,

1

Z

0 1

Z

0

u y ( x;y;t ) c ( x ) s ( y ) dxdy =

?

1

Z

0 1

Z

0

u ( x;y;t ) c ( x ) c ( y ) dxdy: (12) Substituting (11), (12) into (10) gives

?

dt d

1

Z

0 1

Z

0

u ( x;y;t ) c ( x ) c ( y ) dxdy

=

1

Z

0 1

Z

0

(

2

+

2

) u ( x;y;t )+ ' ( t ) f ( x;y )

c ( x ) c ( y ) dxdy: (13) Noting that

dt d

0

@

e

(

2+

2)

t

1

Z

0 1

Z

0

u ( x;y;t ) c ( x ) c ( y ) dxdy

1

A

=

?

' ( t ) e

(

2+

2)

t

1

Z

0 1

Z

0

f ( x;y ) c ( x ) c ( y ) dxdy;

we get

e

2+

2

1

Z

0 1

Z

0

g ( x;y ) c ( x ) c ( y ) dxdy =

? 1

Z

0

' ( t ) e

(

2+

2)

t dt

1

Z

0 1

Z

0

f ( x;y ) c ( x ) c ( y ) dxdy:

This completes the proof of Lemma 1.

(10)

Proof of Lemma 2

We shall prove

j

0

( )

j!

+

1

as

!1

. We have

0

( ) =

1

Z

0

e t

2

'

0

( t ) dt =

1

Z

0

e t

2

v

00

( t ) dt

= e t

2

v

0

( t )

1

0

?

2

1

Z

0

v

0

( t ) e t

2

dt =

?

v

0

(0)

?

2

1

Z

0

v

0

( t ) e t

2

dt:

By the properties of v

0

there exist t

0

and "

1

> 0 such that < t

0?

"

1

< t

0

< t

0

+ "

1

< 1 ;

and

v

0

( t ) < 0

8

t

2

[ t

0?

"

1

;t

0

+ "

1

] : We put

C

1

min

[0

;t

0?

"

1]

(

?

v

0

( t )) ;C

2

min

[

t

0?

"

1

;t

0+

"

1]

(

?

v

0

( t )) > 0 : We have

0

( ) =

?

v

0

(0)

?

2

4

t

0Z?

"

1

0

+ t

0 +

"

1

Z

t

0?

"

1

+

1

Z

t

0+

"

1

v

0

( t ) e t

2

dt

3

5

2

?

v

0

(0) +

2

4

C

1

t

0

?

"

1

Z

0

e t

2

dt + C

2

t

0 +

"

1

Z

t

0?

"

1

e t

2

dt

3

5

2

?

v

0

(0) +

h

C

1

e

(

t

0?

"

1)

2 ?

1

+ C

2

e

(

t

0+

"

1)

2?

e

(

t

0?

"

1)

2i

?

v

0

(0) + C

1

e

(

t

0+

"

1)

2

e

?2

"

1

2 ?

e

?(

t

0+

"

1)

2

+ C

2

e

(

t

0+

"

1)

2

1

?

e

?2

"

1

2

:

Therefore

j

0

( )

j!

+

1

as

!1

. Hence, by the analyticity of

0

( ), it follow that

0

( ) has only nite zeros j ;j = 1 ;:::;p on the real axis.

We can write

0

( ) =

1

( )

Y

p

j

=1

(

?

j ) m

j

(11)

where m j = 1 ; 2 ;:::

8

j = 1 ;p ,

j

1

( )

j!

+

1

as

!1

and

1

( )

6

= 0 for every

2R

. By

j

1

( )

j!

+

1

as

!1

and

1

( )

6

= 0 for every , there exists C

3

> 0 such that

j

1

( )

j

C

3

for every . Hence,

0

(

p

2

+

2

)

C

3Y

p

j

=1

p

2

+

2?

j

m

j

: where m j = 1 ; 2 ;::: ;

Without loss of generality, we can assume that 0

1

<

2

< ::: < p

(if j < 0 then

p

2

+

2?

j

j

j

j

).

Putting d = min

1

s

p

?1

( s

+1?

s ), M =

P

p

s

=1

m s and =

p

2

+

2

0 . Choose R

0

= min

f

C

3

d M ;

12

;C

3?

212

m

1

d M

?2

m

1g

and s = C

1=2ms

R

1=2ms

3

d

(M?2ms)=2ms

, 1

s

p we then have

i) If s + s

s

+1?

s

+1

;s = 1 ;p

?

1, we have

j

0

( )

j

C

3Y

p

j

=1

p

2

+

2?

j

m

j

C

3

m s

s

m s

+1s+1

d M

s

= R;

where M s = M

?

m s

?

m s

+1

.

ii) If p + p < , we have

j

0

( )

j

C

3

d M

?

m

p

m p

p

= and the choice p = d

d

M

R C

3

(1

=

2

m

p)

with R

d M C

3

involves that

R . If 0

<

1?

1

the same proof as before with

1

= d

d

M

R C

3

(1

=

2

m

1)

implies that

j

0

( )

j

R .

In the case where

1

= 0 i.e. the roots i are such that 0 =

1

<

2

<

::: < p the previous proof is still valid with R

0

= min

f

C

3

d M ;

12g

. Which means

B R

[

p s

=1

f

( ; ) = s

?

s <

p

2

+

2

< s + s

g

: Hence

m ( B R )

X

p

s

=1

4 s s

4 s max

=1

;p s

X

p

s

=1

s = 4 d max s

=1

;p s

X

p s

=1

R

1

=

2

m

s

C

31

=

2

m

s

d M=

2

m

s

: Choosing = min

1

s

p

n

1

2

m

s

o

, we complete the proof of Lemma 2.

(12)

Proof of Theorem 1

Put v = u

1?

u

2

and f = f

1?

f

2

, then v and f satisfy (6) and

v ( x;y; 1) = 0 : (14)

Put

f ~ ( x;y )

1 4

8

>

>

>

>

<

>

>

>

>

:

f ( x;y ) ( x;y )

2

(0 ; 1)

(0 ; 1) f (

?

x;

?

y ) ( x;y )

2

(

?

1 ; 0)

(

?

1 ; 0) f (

?

x;y ) ( x;y )

2

(

?

1 ; 0)

(0 ; 1) f ( x;

?

y ) ( x;y )

2

(0 ; 1)

(

?

1 ; 0) 0 ( x;y )

2

= (

?

1 ; 1)

(

?

1 ; 1) Then

b

~

f ( ; ) = 12

Z

R 2

f ~ ( x;y ) e

?

i

(

x

+

y

)

dxdy

= 12

1

Z

0 1

Z

0

f ( x;y ) c ( x ) c ( y ) dxdy: (15) By (7) and (15), we get

2

4 1

Z

0

e

(

2+

2)

t ' ( t ) dt

3

5 b

~

f ( ; ) = 0 : (16)

Let

h ( ; )

1

Z

0

e

(

2+

2)

t ' ( t ) dt =

X1

n

=0

(

2

+

2

) n n !

1

Z

0

' ( t ) t n dt:

If h

0, by Weierstrass theorem, we have '

0, which is a contra- diction. Hence h

6

= 0. This implies that there exist (

0

;

0

)

2 C C

and r > 0 such that

j

h ( ; )

j

> 0 for every ( ; )

2

B ((

0

;

0

) ;r ) where B ((

0

;

0

) ;r ) is the ball with center at (

0

;

0

) and radius r.

Therefore

b

~

f ( ; ) = 0

8

( ; )

2

B:

(13)

Since

b

f ~ is an entire function, we get

b

~

f ( ; ) = 0

8

( ; )

2C C

: Hence ~ f = 0 a. e.

This follows f = 0 a. e. on Q which involves v = 0 a. e. on Q since the variational problem (6) has a unique solution.

This completes the proof of Theorem 1.

Before proving two main regularization results, we state and prove a necessary Lemma. Note that it is of independent interest.

Lemma 3

Let D r =

( ; ) =

2

+

2

r

2

and r >

p

2. If f

0 2

H

2

( Q ) then

R

R 2

n

D

r

"

R

Q f

0

( x;y ) c ( x ) c ( y ) dxdy

#

2

dd

1536

k

f

0k2

H

2(

Q

)

r

?1

.

Proof of Lemma 3

From the denseness of C

1

( Q ) in H

2

( Q ), we only consider the case f

02

C

1

( Q ).

We have

1

Z

0 1

Z

0

f

0

( x;y ) c ( x ) c ( y ) dydx =

=

?

1

Z

0 1

Z

0

@f

0

@x ( x;y ) s ( x )

c ( y ) dxdy +

1

Z

0

f

0

( x;y ) s ( x )

x

=1

x

=0

c ( y ) dy

=

?

1

Z

0 1

Z

0

@f

0

@x ( x;y ) s ( x )

c ( y ) dxdy +

1

Z

0

f

0

(1 ;y ) s ( )

c ( y ) dy

=

1

Z

0 1

Z

0

@

2

f

0

@x@y ( x;y ) s ( y ) s ( x )

dxdy

?

1

Z

0

@f

0

@x ( x;y ) s ( y )

y

=1

y

=0

s ( x ) dx

? 1

Z

0

@f

0

@y (1 ;y ) s ( y ) s ( )

dy +

f

0

(1 ;y ) s ( y )

y

=1

y

=0

s ( )

(14)

=

1

Z

0 1

Z

0

@

2

f

0

@x@y ( x;y ) s ( y ) s ( x )

dxdy

?

1

Z

0

@f

0

@x ( x; 1) s ( ) s ( x )

dx

? 1

Z

0

@f

0

@y (1 ;y ) s ( y ) s ( )

dy + f

0

(1 ; 1) s ( ) s ( )

: We have

1

Z

0 1

Z

0

@

2

f

0

@x@y ( x;y ) s ( y ) s ( x )

dxdy

k ( ) k ( )

@

2

f

0

@x@y

L

2(

Q

)

: where

k ( ) =

8

<

:

1 ;

j

j

1

1

j

j

;

j

j

> 1 : We have

f

0

(1 ; 1) =

1

Z

0 1

Z

0

@

2

( xyf

0

)

@x@y dxdy

=

1

Z

0 1

Z

0

f

0

( x;y ) + y@f @y

0

( x;y )+ x@f

0

( x;y )

@x + @

2

f

0

( x;y )

@x@y xy

dxdy;

hence

j

f

0

(1 ; 1)

jk

f

0k

L

2(

Q

)

+

@f

0

@y

L

2(

Q

)

+

@f

0

@x

L

2(

Q

)

+

@

2

f

0

@x@y

L

2(

Q

)

: We have

1

Z

0

@f

0

@x ( x; 1) s ( ) s ( x )

dx

k ( ) k ( )

1

Z

0

1

Z

0

@y @

y@f @x

0

( x;y )

dy

dx

k ( ) k ( )

"

@f

0

@x

L

2(

Q

)

+

@

2

f

0

@x@y

L

2(

Q

)

#

:

(15)

Simultaneously

1

Z

0

@f

0

@y (1 ;y ) s ( y ) s ( )

dy

k ( ) k ( )

"

@f

0

@y

L

2(

Q

)

+

@

2

f

0

@x@y

L

2(

Q

)

#

: Therefore

1

Z

0 1

Z

0

f

0

( x;y ) c ( x ) c ( y ) dxdy

4 k ( ) k ( )

k

f

0k

H

2(

Q

)

: It implies that

Z

R 2

n

D

r

2

6

4 Z

Q f

0

( x;y ) c ( x ) c ( y ) dxdy

3

7

5 2

dd

128

k

f

0k2

H

2(

Q

)

8

>

>

<

>

>

: Z

j

jpr2 Z

j

jpr2

+

Z

j

jpr2 Z

j

jpr2

( k ( ))

2

( k ( ))

2

dd

9

>

>

=

>

>

;

128

k

f

0k2

H

2(

Q

)k

k

k2

L

2(R) Z

j

jpr2

1

2

d

1536 r

k

f

0k2

H

2(

Q

)

:

We complete the proof of Lemma 3.

Proof of Theorem 2

By choosing r =

p81

" > 1 and D =

( ; ) =

2

+

2

r

2

. By (7), we have

e

2+

2

1

Z

0 1

Z

0

g

0

( x;y ) c ( x ) c ( y ) dxdy = 2

2

4

? 1

Z

0

e

(

2+

2)

t '

0

( t ) dt

3

5 b

~

f

0

( ; ) : (17) Therefore

b

~

f

0

( ; ) =

?

e

2+

2

1

R

0 1

R

0

g

0

( x;y ) c ( x ) c ( y ) dxdy 2

R1

0

e

(

2+

2)

t '

0

( t ) dt :

(16)

Hence,

f ~

0

( ; ) = 12

Z

R 2

b

~

f

0

( ; ) :e i

(

+

)

dd (18)

=

?

1 4

2

Z

R 2

e

2+

2

1

R

0 1

R

0

g

0

( x;y ) c ( x ) c ( y ) dxdy

1

R

0

e

(

2+

2)

t '

0

( t ) dt e i

(

+

)

dd:

Let

f ~ " ( ; )

?

1 4

2

Z

D e

2+

2

1

R

0 1

R

0

g ( x;y ) c ( x ) c ( y ) dxdy

1

R

0

e

(

2+

2)

t ' ( t ) dt e i

(

+

)

dd: (19) We denote

k

:

k2

, norm in L

2

(

R2

).

We have

f ~ "

?

f ~

02

2

=

f

b

~ "

?

f

b

~

02

2

(20)

=

Z

D

b

~

f " ( ; )

?

f

b

~

0

( ; )

2

dd +

Z

R 2

n

D

b

~

f

0

( ; )

2

dd:

With ( ; )

2

D , we get 2

f

b

~ " ( ; )

?

f

b

~

0

( ; )

=

=

e

2+

2

2

6

6

6

4 1

R

0 1

R

0

g ( x;y ) c ( x ) c ( y ) dxdy

1

R

0

e

(

2+

2)

t ' ( t ) dt

? 1

R

0 1

R

0

g

0

( x;y ) c ( x ) c ( y ) dxdy

1

R

0

e

(

2+

2)

t '

0

( t ) dt

3

7

7

7

5

=

e

2+

2

2

6

6

6

4 1

R

0 1

R

0

[ g

0

( x;y )

?

g ( x;y )] c ( x ) c ( y ) dxdy

1

R

0

e

(

2+

2)

t '

0

( t ) dt +

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