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Blow-Up and Attractor of Solution for Problems of

Nonlinear Schrodinger Equations

Ning Chen*, Jiqian Chen

School of Science, Southwest University of Science and Technology, Mianyang, China Email: *[email protected]

Received September 18, 2012; revised October 18, 2012; accepted October 26, 2012

ABSTRACT

In this paper, the authors study the blow-up of solution for a class of nonlinear Schrodinger equation for some initial boundary problem. On the other hand, the authors give out some analyses and that new conclusion by Eigen-function method. In last section, the authors check the nonlinear parameter for light rule power by using of parameter method to get ground state and excite state correspond case, and discuss the global attractor of some fraction order case, and com- bine numerical test. To illustrate this physics meaning in dimension d = 1, 2 case. So, by numerable solution to give out these wave expression.

Keywords: Nonlinear Schrodinger Equation; Eigen-Function Method; Fractional Order; Blow-Up; Glabal Attractor

1. Introduction

The quantum mechanics theory and application in more field in nature science. The non-linear Schrodinger equa- tion is the basic equation in nonlinear science and widely applied in natural science such as the physics, chemistry, biology, communication and nonlinear optics etc. (See [1-9]) We study this equation to extend them are with important meaning (See[10-12]).

As we all know, the nonlinear Schrodinger equation be description quantum state of microcosmic grain by wave, it is variable for dependent time, and that is most essen- tial equation, which position and action similarly Newton equation in position and action classics mechanics, it is apply to field as optics, plasma physics, laser gather, co- hesions etc, particular on that action of power and trap, search analytical solution for Schrodinger equation is also difficult, and more so difficult for complicated power.

Now, we may extend some results in [4] by using Ei- gen-function method in through paper.

As we all know the solution of initial problem for Schrodinger equation bellow

 

 

 

2

i , , ,

,0 ,

n t

n

u a u f x t x R t

u xx x R

     

 

 



0,

(1.1)

Assume that real part and imaginary part of

   

x ,f x t, ,

are real analytical function for n,

xR then this solu-tion of the problem may expresses in form:

 

 

 

 

2 0 0

i ,

!

, d . k

k k k

t k k

x a

u x t t x

k

t f x

  

 

  

2. Several Theorems

In this section, we consider the blow-up of solutions to the mixed problems for higher-order nonlinear Schrod- inger equation with as bellow.

It is well known the higher order equation:

 

,

i k , 0,

t

u   u f u tx

where

 

2

2 2 1

, ,

n

ixi

     

,etc.

that with new results for higher-order case. Now, we consider the blow-up of solutions to the mixed problems for six-order general Schrodinger equation to extend some results [4] that as bellow form:

 

 

 

 

 

3

2

i , 0, ,

0, , ,

, ,

t

u u f u t x

u x x x

t x u t x u t

  



    



 

  0, 0.

 

(2.1)

Assume that

 

0,

 

4k 1,

 

6

   

,

f f c x H

      

    x

(2)

not identical zero.

Where f holds complex value function with self-

x.

variable for comple 

 

x is also complex value

Theorem 2.1. Suppose that nonlinear term

 

2 2 0, , 1 n

t x R R

    

f of pro-

blem (2.1) satisfy C0,

 

0,

 

4k 1,

 

6

,

f c x H

    

f   

and 

 

x

) must be

not identical zero then the classical solution of (2.1 for blow-up in finite time in

Proof. Let

 

1 0, ; 6 .

C T H

 

2

d d ,

J t

u x uu x

(2.2) Then

 

3 3

 

 

d

i d

t i

d ,

u u uu x

u u u u x u f u uf u x

 

 

     

(2.3)

By the first Green’s formula, we have

J t

  

 

 

2 1

3 2 2

1

d

d d d

i

i i

x i

n

x x

i

u x

u u x u us u u x

  

 

 

    

Substituting it into (2.3), then

3 d 2 d

i

n x

u u x u us u

  

     

 

 

 

3 3

d

d ,

u u

J t i

 uu s

u f u uf u x

 

 

 

 

We may assume 

 

t x, 0,then we have

2 u

u u u uu u

     

 

2

0.

u

     

 

 

   

 

Obviously, from u f u

 

uf u

 

2uf u

 

, and

 

4 1

.

k

f uc u  Therefore, we have

 

 

 

4

d

k

d 2

J t 

u x.

By Schwartz inequality:

u f uuf u xc

2

2

d 1d

u x x

    

4

1

d , here d 0.

u x c x

So,

 

2

4 2

1

d 1 d

u x c u x

  

.

Inductively, we have

 

2

6 3

1 d

c

u x etc.,

12

d 1

u x

 

 

4

 

2

2

1

d 1 d 0.

k k

k

u x c u x

   

Then J t

 

increasing function similar in [4 from ]

  

 

2

4 2

1 1

2 d 2 d

2 1

2 0,

k

k k

k k

J t

c c J t

 

 

and then there exists

c c u x c c u x

such that

 

0

lim ,

t T J t

0 ,

T    

that is

0

2 lim dx .

t T

u

So, we complete the proof of this Theorem 2.1. (As positive integer k1,we get i 3.1 in

[4

r equ

t is theorem ])

onside

Remark. Then we c r that important case is al-ways for the Schrodinge ation may as bellow form

0 :

i 2 2

t

cu   u c uu.

Now, we shall consider also in this similar case:

 

 

 

 

2 3

2

i ,

t

u   u c uu

0, , ,

, , 0, 0.

u x x x

t x u t x u t

  



 

 

      

 

(2.4)

Therefore, we shall obtain the following theorem. Theorem 2.2. Suppose that non-linear term f of

problem (2.1) satisfy

c0

,

 

 

4 1

0, k ,

f f c

    

 

and

 

6

   

, 0, 2 2 0, ,

 

1 n,

x H x t x R R

          

e classical solution of (2.4) must be for blow-up in finite time in

then th

 

1 0, ; 6

C T H  (as positive k1, then

it is theorem 3.2 in [4]).

Proof. Since f u

 

c u2u c,

0

satisfies

 

2 4

0

f c

k

c

       ,

then

 

4k 1.

f  c 

Thus, from theorem 2.1, we complete the proof of m 2.2.

theore

Now, we shall give out the following theorem form. Here, we shall consider the problem:

 

 

 

 

2 3

i , 0, ,

t

u u F u u t x

     

 

2

 

0, , ,

, , 0, 0.

u x x x

t x u t x u t

  



 

 

  

 

(2.5)

(3)

blem (2.5) satisfy

c0

, F

 

 c4k3,

 

x  0,

and

,

 

6

 

, 2 2 0, ,

 

1 n

x H t x

      RR

th bl

(As positive i then it is theorem 3.2 in [4])

oof. Since

en the classical solution of (2.5) must be for ow-up in finite time in 1

C 0, ;T H6

 

 . nteger k1,

Pr f u

 

F u

 

2 u c,

0

, we have that

 

 

2 4 1

,

k

f   F   c 

and

 

2 4k

0.

f c c

       

eorem 2.1, we complet theorem 2.3. (As it is theorem 3.3 in [4])

Now, we may consider the following problem:

Thus, from th e the proof of

1, k

 

 

 

 

2 3

i e 1 , 0, ,

0, , ,

p s t

u u k u t x

u xx x

      

 

 

 (2.6)

wh

Theorem 2.4. that and

then the solution of (2. w-up

me in 2

, , 0, 0.

t x u t x u t

  



  

 

ere constant k0,p0.

Assume

 

x H6

 

, 6) must be for blo

 

x 0,

 

in finite ti 1

0, ; 6

 

C T H  .

Proof. From

 

2 2 1 2 2

e 1

2!

p u

p u p u

   ,

then

 

ep u2 1

f uKu satisfy f

 

 0, and

 

4k

f 1.

It holds the condition of theorem 2.1, then by theorem 2.1 that we know the solution of problem (2. ) must be blow-up in finite time. Therefore, we complete the proof

orem 2.4.

3. Main Results

W

ermore, we will consider eight-order nonlinear Schrodinger equation. In first, stating that lemma 3.1.

Lemma 3.1. This Eigen-value problem (see [4])

kp

  

6

of the

e consider the initial boundary value of some higher order nonlinear Schrodinger equation. By using of eigen- function method, we can get new results bellow.

Let

t, x

Duu D u

, 1, 2 ,

,

n

t x x x

u u u u

 

 

   

 

11 2

, , , , 1, 2, , ,

, , , .

i i x i

i

n

tx x x x x x

x x x x

Du u u u i n

D Du Du Du Du

 

 

Furth

0, ,

0. x

   

    



 

 (*)

As we all know the first Eigen valu1e  1 0 of (*), the corresponding Eigen-function 1

 

x 0, assume it

with

 

1 x dx 1

 

.

Let 

h co

be bounded closed domai smoot nditions of function

n in Rnand by suite

f and g that from

G re

chrodinge ight-order case

reen’s second formula, we easy get follow sults. Now, we consider nonlinear S r equation with e

ing

0i 1,i1, 2

:

 

 

2

4 3

1 2

, x , x f u D u D u

 

, 0, ,

4 3

1 2

i

t

u u u u

g u g u

 

    (3.1)

g u t x

   

 

     

 

, 0 0

 

, ,

u xu x x  (3.2)

0, , 0.

u x  t (3.3)

Clearly, 120, 3.1. Assume

that is theorem 2.1 in [5]. Theorem that problem (3.1)-(3.3) satisfy (where nout normal direction):

 

 

 

 

 

3 2

1 2 1 Im ;u

 

    

3 2

1

0 0,

Re G

I G

n

Gg ug u g u



 

   2Re 

 

 

 

2 4

1 1

3 2

0

Re , , ,

Im Re ,

Re d , 0.

x x

II A f u v D u D u g u

g u u CF u

u x A

   

 

 

  

 

 

F u be continuous, convex and even function, here

1, 0

;

1, 0

C

    

 



   

III F s 0

s

, and

ds F s

 

 . Then

up in finite time. Proof. (I) step, when

the classical solution of (4.1)-(4.3) must be blow-

0, 0

(4)

 

 

 

4 3 1 2 4

Re Re ,

 

 

 

2 1 2 4 3 Re Im

Re , ,

Re . t x x 4 3 1 2 3 2 1 Re Rei Im Im t

u u u u

fg ug u g u

      

 

u u

f u D u D u

g u g u g u

           .4) u u        

   (3

Multiplying by 

 

x the both sides of (3.4) and in-tegral on  forx, it is form:

 

 

4 3

1 2

2 4 3

1 2

Re d Im

Re , , Re d

t

x x

u x u

f u D u D u g u x

                      

Taking a t

 

Re d ,u x then a t

 

Re d ,u xt

and that

 

 

 

 

4 3 1 2 2 4 3 1 2 2 3 2 1 2 3 2 1 2 Im

Re , ,

Re d

d

Re , , d

1 Im d

1 Re d

x x

x x

a t u

f u D u D u

g u x

G G x

f u D u D u x

u x

g u x

                                                             

 (3.5)

By

 G n

 0 in (I) and Green’s se mula:

, (3.6)

Substituting (3.6) into (3.5), we get

cond for-

G G

dx 0

    

 

 

 

2 3 2 1 2 3 2 1 2 2 2 3 2 1 2

Re , ,

Re d

Im

Re d

x x

a t f u D u D u

g u x

Imu

2

 

3 1 Ref u D u D u, x , x

  

 

   u

g u x

                                

    Hence, (3.7)

 

 

2 4 3 1 2 4 3 1 2

Re , ,

Im d

x x

a t f u D u D u

g u u x                      

From A0,

 

 

2 4 3

1 2

4 3

1 2

Re , ,

Im Re

x x

0.

A f u D u D u g u

u CF u

    

    

   

    

Therefore, we have

 

 

2 4 3

1 2 4 3 1 2 , , Im Re x

Re f u Dx D u g u

u CF u

                  u (3.8)

Combing (3.7)-(3.8), and Jensen’s inequality, we ob- tain

 

Re

 

a t F uF

Re du xF a t (3.9)

Here, F a t

 

d d .a t So, t a t da F a

 

, 

there exist T da F a

 

,

 

  , such that

 

lim .

tTa t   (3.10)

From a t

 

Re d ,u x and Holder inequality, we get

1 1 ,

q

 

1

p

 

Re d   Re  ,

a t

u x  Lq u Lp

that is a t

 

Lq 

1 Reu Lp . 

  

Therefore,

 

 

1  

lim Lq lim Re Lp .

t Ta tt T u

 

  

Hence,

 

lim Re Lp , 1 .

tT u       p

(II) step, when A0,0, taking that

 

, 1

,

u x t  u x t

,

then Reu Re .u1 , let

Therefore a t

 

Re

 

u1 d ,x we have

0,

 

   

 

1 , 1 , 1

a t  a t at  a t    

Combine (4.1)-(4.8) and 0,

C 1

, we obtain

that

A

 

1 Re 1 d

a tF u x

  

(3.11) That is also a t1

 

F

Reu1

dx. From Jensen inequality and F s

 

is even function, we have

 

1

 

1 d 1 d ,

F aFaa t

then

 

1 1

dtda F a (3.12)

(5)

 

 

 

 

 

lim Re lim Re ,

1 .

p

p p

L

L L

t T u t t T u t

p

 

     

   

Combine (I)-(II) we comp 3.

1

lim Re , 1 .

tT u      p

lete the proof of theorem 1.

Clearly, 120,that is theorem 2.1 in [5].

Theorem 3.2. Assume that problem (3.1)-(3.3) satisfy:

 

 

 

3 2

1 2

3 2

1 Re

G     g u

1 2

0 0,

1 Im ; G

I G

n

u

 

 

 

    

 

 

 

2 3 2

1 2

Im , x , x

3 2

1 2

Im Re

, Im

f u D u D u g u

II B

    

  

F u

u

F u

    

and

0 ,

1 0, Im d 0

B   

u x

where F s

 

is continuous, convex and even function;

   

III F s 0,

s

and ds F s

 

. 

 

 

 

the classical solution for this problem (3.1)-(3.3) in finite time.

Proof. From Then is blow-up

1 0,

B   we discuss two case:

 

I B 1 0, 0,u x t

 

, iu2

 

x t, , then ImuRe .u2

ing the imag

Tak inary part for both sides of (3.1), similar the method of proof for Theorem 3.1, we can easy have

 

2

lim R , 1 .

tT eu Lp      p

So, we get that

 

 

lim Im Lp , 1 .

tT u t       p

(II)B 1 0,0, we may let u x t

 

,  u

 

x t, ,

then 3

So,

3

ImuIm .u

 

  3

lim Im Lp , 1 .

tT u t       p

ary part for both sides of (1), by (II) and similar the method of proof for theorem 3.1, we can easy have

Taking the imagin

  , 1

p

L     

We

3

lim Re .

tT u p 

get that

 

 

lim Imu t Lp      , 1 p .

3.3. Clearly

tT

Combine (I)-(II), we complete the proof of theorem 3.2.

Corollary 120,

g it for some

that is theorem 2.2 in [5]. By ([13] )lookin applications.

4. Some Higher-Order Case

In the same way, we can consider the higher-order case (integer k0):

4 4 1

 

,

 

 

2 g u g u t, 0

1 2

4 1 i

,

k k

t

k

k

u u u u

x

 

     

2 4

1 , x , x

f u D u D ug u

  

     

(4.1)

 

,0 0

 

,

u xu x x  (4.2)

0, , 0.

u x  t (4.3)

Clearly, k1,that is problem of eight order case.

Theorem 4.1. Assume that problem (4.1)-(4.3) satisfy

 

 

 

 

 

 

Im ;u

4 4 1

2 1 2

4 4

0 0, ,

and Re

k k

k

k k

G

I G P

n

G P g u P

  

 

        

   

 

   

 

2

Im , 4 4 Re

, Im

x , x k k

II B

f u D u D uPg uPu

and

F u

0

1 0, Im d 0,

B   u

x

  

 

F s is continuous, convex and even function;

where

   

III F s 0,

s

and ds F s

 

. 



 

Then the classical solution for this problem (4.1)-(4.3) w-up in finite time.(omit this similar proof ) Remark 4.2. Assume that (here ) is blo

4k3

 

4k 4k 1 4k 2 4k

k

P            3

then we will obtain similar results of theorem 3.2 with more case.

s in an al

4 1 2 3 4 ,

Remark 4.3. (See [6,14]) According to the direction of [6], we may consider that coupled nonlinear Schrod- inger equation as in the following iterative formula

gorithmic form by VIM:

 

 

2 2

0 t i xx i d ,

t

n n n n n

A A A B A

1 , ,

n n

A x t A x t

 

 

  

 

(6)

 

 

1

2 2

0 t i xx i d .

n n

t

n n n n n

B B A B B

, ,

x t B x t B

 

 

  

The solution procedure with initial approximations (omit the details ):

 

 

 

 

 

 

0

0 0

,0 1 cos ,

,0 1 cos .

A A x f x a x

B B x g x b x

 

 

   

   

The other components can be obtained directly:

   

1 , , 1 , , , etc.

A x t B x t

Furthermore, the conserved quantities:

 

2

 

2

2 , d

s s

E A

A x t x and

 

2

 

2

2 , d

s

E B

s B x t x,

where s2π.This numerical results is with higher accuracy.

5. The Global Attractor of the Fractional

NSE

ntly, they also showed that dynamic behavior of large time action to investigate for [15,16], they are deep- going study global attractor and dimen on estimate of

rder non or sea

linear Schrodinger equation in [17]. The au- of [17] an sed on [16-18], and combine [19] obtained the Rece

si

integer o -linear Schrodinger equation in [16]. The auth rch the Cauchy problem for fractional order

non-thor search the global attractor problem for a class fractional order non-linear Schrodinger equation in

d we ba

condition of existence of solution for following fractional order non-linear Schrodinger equation:

 

 

i p i

t

uuF u uu

 

 

 

 

 

ma, express the field of electricity [20], where

is with standard perpendicular base, i is im the function

0

, , 0,

,0 , ,

, , , , 0.

i

f x x t

u x u x x

u x Le t u x t x t

  

  

   



(5.1)

Physics background of (1) is arise the main part of nonlinear interaction for laser and plas u

 

0, n,

0, ,0,1,0, ,0 ,

1, 2, ,

i

l e i n

      

aginary unit,

 

F  is with one order derivative

 

n 2 , 0,p 0,

    where  0with some con-

sume effect, and as  0 express the integral system with soliton solution.

As 3,  c, 1 for (3.1), and (4. ) thirdly

section case, we will obtain global attracto

1

r of initial value problem (5.1) that first give out Lemma as llows.

Lemma 5.1. Let

fo

 

2

   

2

   

0 , , ,

u xLf xLu x t (5.1), an

 

is the solution of problem d

 

 

 

2 2 2 2

0

, e t .

u x tu x     f x (5.2) Proof. Multiply u for the both sides of (**) act as inner product, we have

  

 

 

,

i ,u ut ,

, i ,

p

u u

F u u u u u

 

 

  (**)

and take real part, f x u

2

2

1

2 d u dt u

 

 

 

 

2

2 1

1

Im ,

2 2 ,

f x u f x u

u f x

  

 

 

(5.3)

From (5.3) and by use of Gronwall inequality, we ob-tain

 

2

 

 

,

u x tu0 x 2et  2 f x( ) .2

Lemma 5.2. Let

 

 

2

   

   

u x t,

0 , ,

p

u xH  L   f xH

 

2 

2 , Lp

u u



is the solution of problem (1), then w

oof. To establish inner product for both sides of eq- uation (5.1) with for

ith uniform bounded. Pr

t

u , and take real part, we have that

 

 

 

2 2 1

2   u

  d Im ,

Re , ,

p

t t

t

t

F u u u x u u

f x u

 

easy get that by (5.1),

 

 

 

2 2

Re , t ,

Im ,

d

t

p

u u u

F u u u x



 

f x u

where

 

   

 

 

,

Re , ,

p

Re f x u, t Im f x u F u u

f x u

 

(7)

 

  

 

  

   

 

 

   

 

 

 

 

 

 

 

1 2 1 2 2 1 1 2 2 1 2 2 2 2 1 1 , 2

1 2 1

1 1 2 1 2 d d , .2 d

2 d 2 d

2 2 P P p p t t p p p P t t L

L L t

t t p t P L t

u F u u u u u x

u F u u u u u x

f x u F u u

f x u

f x F u u u

u x

F u u x u x

F u u                                                             

Im 

Im p , p

F u u u F u u

 

  

 

1 

2 2 2 2 1

, 2 P .

P

t t t L

u   uF u

      So,

 

 

 

 

2 2 1 2 2 1 2 d

2 2 d

p t t

p

u F u u u x

u F u u u x

                           

C  

by use of Gronwall inequality, we obtain

 

2

 

, p d

t

u F u u u



x

uniform boundary. Lemma 5.3. Let

,

is the solution of problem (5.1), then

 

2

   

2

   

0 , ,

u xH   f xLu x t

 

 u with uniform bounded.

Proof. To derivative both sides of Equation (5.1) for and take inner product for

t ut, and taking also

imagi-nary part, we have

 

2

 

2

1

2 Im p ,

t t

t

uF u u ut 0

  u Then

 

 

 

 

  2 2 1 2 1

2 t t

t

P

t L

uu

     

By Lemma 5.2 and Young inequality, the (5.4) with form

2 2 2 1

, 2 t L P t t u u

u   uF u

     1 2 Im , 2 p t

F u u u F       

 

2 2 2

2

t t t

t

u    u  uC by use of Gronwall inequality, we obtain

 

2

2 1

0 ,0 e t ,

t

uu x  C Because hold these inequality bellow

 

 

 

 

 

 

2

0 0 0 0

0 0 1 2 ,0 , , p t H t P t L

u x C u F u u u

C u

u F u u u

                p

u u F u u u

   

Hence ut ,

 

u

 are uniform boundary. Similar method of [19,20], we give out that condition of yield global attractor of problem (5.1).

Theorem 5.4. Assume hat

 

   

 

 

2 2

0 , ,

2 , 0, 0,

u x H f x L

n p

 

   

  

then the periodic global attractor of initial value problem (4.1-4.3):

 

0

0 ,

s t s

A S t B

 

  

here S

 

t or semi-group with needing de-e in prov with the bounded attractor set in

w for operat

fin e an for

using of similar proof m

Remark 5.5. Furthermore, we shall study global at-tractor of fraction order non-linear Schrodinger type equation, and the estimate for its dimensions, and that

6. Some Notes for Shake Power and Light

Power

omic transition, is one of the dB0

following in prove processes. Proof. We omit the proof (by ethod in [18,19]).

blowing-up of solution for some fraction order non-linear Schrodinger type equation.

We consider some meaning of physic and Energy for nonlinear Schrodinger equation.The numerical test for solution of nonlinear Schrodinger equation with ground state and excite state.

Atoms absorb energy from the ground state transition to the excited state, learned through experiments in ex- treme case, the ground state solution is not controlled so- lution-Blow-up solution.

(8)

ict

co e atomic transition to the first, second and

 

2 1

2 V

  

       

main methods to produce new material structure. Str

ntrol of th   

ingly.

(6.3)

third excited state is more practical significance, espe- cially the transition to the first excited state. As we all now, the ultra-low temperatures, the atomic gas in the magnetic potential well Boer-Einstein condensation ex- pe

So, by check parameter method in [23] we check nonlinear parameter for light rule power, then we get ground state and excite state correspond

riments [21], promotion of scholars study the macro- scopic quantum behavior of atoms and kinetic character- istics.

By using of above stating method we consider calcu- lat

6.1. One Dimension Case (d = 1)

( )a We consider two class powers (shake power and light power) in (6.3), Setting shake power

e to the ground state solution and excite state of d- dimension BECS (Bose-Einstein condensate) with mix harmonic potential and crystal lattice potential.

The Gross-Pitaevskii equation:

 

2

1

2, 250, 2

V xx bb

taking initial wave

 

21 2

0

2 e

π

b

,

x

x

    

 (6.4)

 

 

 

 

2

2 2

0 ,

i

, ,

2 r t h

t

h

V r NU r t r t

m

 

 

 

   

      

 

 

(6.1)

where d, 1, 2,3. 0,

rR dtm expresses mass of at

to calculate ground state g. For (6.4) we calculate first arouse state 1, space field for the time step for

10 x 10,

  

0.2. t

 

( )b Similar above way, taking

 

2

2

1

2 25sin π 4 , 500, 2,

V xxx bb

oms, h be planck constant, N be number of atoms in cohesion system, V r

 

be outer power,

2

0 4π

Uh a m describe interaction between the at- oms cohesion (as 0, means repel; as0, shows

at appropriate im

and (6.3) for

 

21 2

0

2

: e

π

b

,

x

g x x

 

    

tract each other). Thus, by pass e (6.1) may be

measur- able process, then th written:

 

, 1 2

 

 

2

 

i

2 r t

V r r t r t

t

  

   

  ,  , (6.2)

The parameter

and 10  x 10, and  t 0.2.

On the other hand, by the MATLAB search the solu-tion of Equasolu-tion (6.3) in case (1) and (2) as follow with

0, , ,1 2 3

    (See Figures 1 and 2).

tract corres

for positive, or negative, describe that repel or at ponding, out power V r

 

be

by phys stem for us to s

a c

defined tudy things. By using

of the im ginary time method to alculate it in [22] that let it

ic sy 6.2. Two-Dimension Case (d = 2)

Consider shake power in [14,24]

  substituting it into (6.2), we have

-15 -10 -5 0 5 10 15

-150 -100 -50 0 50 100 150 200 250 300

P hi0 P hi1 P hi2 P hi3

V = x2/2

V(

x

),

Ph

i

[image:8.595.153.444.519.716.2]

X

(9)

 

, 0,0 ,0 ,

, other.

x a y

V x y      

 

b

The grain energy:

1 2

2 2 2 2

1 1 1 2 2 2

π , , 1, 2,3, ; 5, 2.

2

n n

n n

h

E n n a

m a b

 

 

   b

We take initial wave function for

 

1 2 1 2

0 1

π π

4

, sin n x sin n y ,

x y n n

ab a b

 

      2 1.

To calculate ground stateg; For

 

1 2 1 2

10

π π

4

, sin n x sin n y

x y x

ab a b

    

    

 

1 2 1 2

01

π π

4

, sin n x sin n y

x y y

ab a b

 

     ,

and

 

1 2 1 2

11 ,

π π

4

, sin n x sin n y

x y xy

ab a b

    

     

1 2 wherenn 2.

 

10 x y, 

By calculating along the direction of axe

,

x and 10

 

x y, cited of

in direction of axe y, and calculating first ex 11

 

x y, al

ld for

, and space fie

ong direction for axe x and

y 2, time step:

axe 0 x 5, 0 y

0.05, 0.02.

x y

t t

   

,

 

Figures 4-6) Combine these cases as Fig: (See Figures 3(a) and (b),

-15 -10 -5 0 5 10 15

-150 -100 -50 0 300

50 100 150 200 250

X

Phi0 Phi1 Phi2 Phi3 Phi4

V(

x

),

Ph

i

[image:9.595.66.502.81.487.2]

2

Figure 2. Ground state phi0. First excited state phi1. V = x /2 + 25*(sin(pi*x/4))2; b = 500, bi = 2.

0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 5 0

0.5 1 1.5 2 2.5 3 3.5 4 4.5 5

Phi0 Phi1 Phi2 Phi3

Ph

i

X

(10)

0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2 0

0.5 1 1.5 2 2.5 3 3.5 4 4.5 5

Y

P

hi

Phi0 Phi1 Phi2 Phi3

(b)

Figure 3. (a) Ground state phi0. First excited state phi1. a = 5, b = 2. (b) Ground state phi0. First excited state phi1. a = 5, b = 2.

0 1

2 3

4 5

0 0.5 1 1.5 2 0 0.5 1

X

Y

P

hi

[image:10.595.179.418.82.281.2]

0

Figure 4. Ground state phi0 a = 5, b = 2.

0 1

2 3

4 5

0 0.5 1 1.5 2 -3 -2 -1 0 1 2 3

X

Y

P

hi

[image:10.595.174.419.323.714.2] [image:10.595.179.414.323.501.2]
(11)

0 1

2 3

4 5

0 0.5 1 1.5 2 -2 -1 0 1 2

X

Y

P

hi

[image:11.595.162.433.86.490.2] [image:11.595.167.430.87.277.2] [image:11.595.166.430.304.495.2]

Figure 6. First excited state phi2-y a = 5, b = 2.

0 1

2 3

4 5

0 0.5 1 1.5 2 -1.5 -1 -0.5 0 0.5 1 1.5

X

Y

P

hi

Figure 7. First excited state phi3-xy a = 5, b = 2.

We consider three-dimension case, Figure4 for ground state ϕ0

( )

x y, corresponding case, the ϕ10

( )

x y, as

with express along direction of axe x (wave surface) in

Figure5, the ϕ01

( )

x y, as with express along direction

of axe y (wave surface) in Figure 6, the ϕ11

( )

x y, as

for express along direction of axe x and axe y (wave sur- face) in Figure7.

7. Concluding Remarks

Recently, the higher-order Schrodinger differential equa- tions is also a very interesting topic, and that application of some physics and mechanics of for some more fields as nonlinear Schrodinger equations and some compute methods etc. In our future work, we may obtain some better results.

The application of some physics and mechanics of for some more fields with some combine equations (look [7,

13]).

8. Acknowledgements

This work is supported by the Nature Science Foundation (No.11ZB192) of Sichuan Education Bureau (No.11zd 1007 of Southwest University of Science and Technol- ogy).

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Figure

Figure 1. Ground state phi0. First excited state phi1.  V = x2/2; b = 500, bi = 2.
Figure 2. Ground state phi0. First excited state phi1. V = x2 /2 + 25*(sin(pi*x/4))2; b = 500, bi = 2
Figure 3. (a) Ground state phi0. First excited state phi1. a2. = 5, b = 2. (b) Ground state phi0
Figure 6. First excited state phi2-y a = 5, b = 2.

References

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