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Duality Principles and Numerical Procedures for a Large Class of Non-convex Models in the Calculus of Variations

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11 September 2023

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12 September 2023

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Abstract
This article develops duality principles and numerical results for a large class of non-convex variational models. The main results are based on fundamental tools of convex analysis, duality theory and calculus of variations. More specifically the approach is established for a class of non-convex functionals similar as those found in some models in phase transition. Finally, in some sections we present concerning numerical examples and the respective softwares.
Keywords: 
Subject: Computer Science and Mathematics  -   Applied Mathematics

MSC:  49N15

1. Introduction

In this section we establish a dual formulation for a large class of models in non-convex optimization.
The main duality principle is applied to double well models similar as those found in the phase transition theory.
Such results are based on the works of J.J. Telega and W.R. Bielski [2,3,15,16] and on a D.C. optimization approach developed in Toland [17].
About the other references, details on the Sobolev spaces involved are found in [1]. Related results on convex analysis and duality theory are addressed in [5,7,8,10,14].
Finally, in this text we adopt the standard Einstein convention of summing up repeated indices, unless otherwise indicated.
In order to clarify the notation, here we introduce the definition of topological dual space.
Definition 1.1 
(Topological dual spaces). Let U be a Banach space. We shall define its dual topological space, as the set of all linear continuous functionals defined on U. We suppose such a dual space of U, may be represented by another Banach space U * , through a bilinear form · , · U : U × U * R (here we are referring to standard representations of dual spaces of Sobolev and Lebesgue spaces). Thus, given f : U R linear and continuous, we assume the existence of a unique u * U * such that
f ( u ) = u , u * U , u U .
The norm of f , denoted by f U * , is defined as
f U * = sup u U { | u , u * U | : u U 1 } u * U * .
At this point we start to describe the primal and dual variational formulations.

2. A general duality principle non-convex optimization

In this section we present a duality principle applicable to a model in phase transition.
This case corresponds to the vectorial one in the calculus of variations.
Let Ω R n be an open, bounded, connected set with a regular (Lipschitzian) boundary denoted by Ω .
Consider a functional J : V R where
J ( u ) = F ( u 1 , , u N ) + G ( u 1 , , u N ) u i , f i L 2 ,
and where
V = { u = ( u 1 , , u N ) W 1 , p ( Ω ; R N ) : u = u 0 on Ω } ,
f L 2 ( Ω ; R N ) , and 1 < p < + .
We assume there exists α R such that
α = inf u V J ( u ) .
Moreover, suppose F and G are Fréchet differentiable but not necessarily convex. A global optimum point may not be attained for J so that the problem of finding a global minimum for J may not be a solution.
Anyway, one question remains, how the minimizing sequences behave close the infimum of J.
We intend to use duality theory to approximately solve such a global optimization problem.
Denoting V 0 = W 0 1 , p ( Ω ; R N ) , Y 1 = Y 1 * = L 2 ( Ω ; R N × n ) , Y 2 = Y 2 * = L 2 ( Ω ; R N × n ) , Y 3 = Y 3 * = L 2 ( Ω ; R N ) , at this point we define, F 1 : V × V 0 R , G 1 : V R , G 2 : V R , G 3 : V 0 R and G 4 : V R , by
F 1 ( u , ϕ ) = F ( u 1 + ϕ 1 , , u N + ϕ N ) + K 2 Ω u j · u j d x + K 2 2 Ω ϕ j · ϕ j d x
and
G 1 ( u 1 , , u n ) = G ( u 1 , , u N ) + K 1 2 Ω u j u j d x u i , f i L 2 ,
G 2 ( u 1 , , u N ) = K 1 2 Ω u j · u j d x ,
G 3 ( ϕ 1 , , ϕ N ) = K 2 2 Ω ϕ j · ϕ j d x ,
and
G 4 ( u 1 , , u N ) = K 1 2 Ω u j u j d x .
Define now J 1 : V × V 0 R ,
J 1 ( u , ϕ ) = F ( u + ϕ ) + G ( u ) u i , f i L 2 .
Observe that
J 1 ( u , ϕ ) = F 1 ( u , ϕ ) + G 1 ( u ) G 2 ( u ) G 3 ( ϕ ) G 4 ( u ) F 1 ( u , ϕ ) + G 1 ( u ) u , z 1 * L 2 ϕ , z 2 * L 2 u , z 3 * L 2 + sup v 1 Y 1 { v 1 , z 1 * L 2 G 2 ( v 1 ) } + sup v 2 Y 2 { v 2 , z 2 * L 2 G 3 ( v 2 ) } + sup u V { u , z 3 * L 2 G 4 ( u ) } = F 1 ( u , ϕ ) + G 1 ( u ) u , z 1 * L 2 ϕ , z 2 * L 2 u , z 3 * L 2 + G 2 * ( z 1 * ) + G 3 * ( z 2 * ) + G 4 * ( z 3 * ) = J 1 * ( u , ϕ , z * ) ,
u V , ϕ V 0 , z * = ( z 1 * , z 2 * , z 3 * ) Y * = Y 1 * × Y 2 * × Y 3 * .
From the general results in [17], we may infer that
inf ( u , ϕ ) V × V 0 J ( u , ϕ ) = inf ( u , ϕ , z * ) V × V 0 × Y * J 1 * ( u , ϕ , z * ) .
On the other hand
inf u V J ( u ) inf ( u , ϕ ) V × V 0 J 1 ( u , ϕ ) .
From these last two results we may obtain
inf u V J ( u ) inf ( u , ϕ , z * ) V × V 0 × Y * J 1 * ( u , ϕ , z * ) .
Moreover, from standards results on convex analysis, we may have
inf u V J 1 * ( u , ϕ , z * ) = inf u V { F 1 ( u , ϕ ) + G 1 ( u ) u , z 1 * L 2 ϕ , z 2 * L 2 u , z 3 * L 2 + G 2 * ( z 1 * ) + G 3 * ( z 2 * ) + G 4 * ( z 3 * ) } = sup ( v 1 * , v 2 * ) C * { F 1 * ( v 1 * + z 1 * , ϕ ) G 1 * ( v 2 * + z 3 * ) ϕ , z 2 * L 2 + G 2 * ( z 1 * ) + G 3 * ( z 2 * ) + G 4 * ( z 3 * ) } ,
where
C * = { v * = ( v 1 * , v 2 * ) Y 1 * × Y 3 * : div ( v 1 * ) i + ( v 2 * ) i = 0 , i { 1 , , N } } ,
F 1 * ( v 1 * + z 1 * , ϕ ) = sup v 1 Y 1 { v 1 , z 1 * + v 1 * L 2 F 1 ( v 1 , ϕ ) } ,
and
G 1 * ( v 2 * + z 2 * ) = sup u V { u , v 2 * + z 2 * L 2 G 1 ( u ) } .
Thus, defining
J 2 * ( ϕ , z * , v * ) = F 1 * ( v 1 * + z 1 * , ϕ ) G 1 * ( v 2 * + z 3 * ) ϕ , z 2 * L 2 + G 2 * ( z 1 * ) + G 3 * ( z 2 * ) + G 4 * ( z 3 * ) ,
we have got
inf u V J ( u ) inf ( u , ϕ ) V × V 0 J 1 ( u , ϕ ) = inf ( u , ϕ , z * ) V × V 0 × Y * J 1 * ( u , ϕ , z * ) = inf z * Y * inf ϕ V 0 sup v * C * J 2 * ( ϕ , z * , v * ) .
Finally, observe that
inf u V J ( u ) inf z * Y * inf ϕ V 0 sup v * C * J 2 * ( ϕ , z * , v * ) sup v * C * inf ( z * , ϕ ) Y * × V 0 J 2 * ( ϕ , z * , v * ) .
This last variational formulation corresponds to a concave relaxed formulation in v * concerning the original primal formulation.

3. Another duality principle for a simpler related model in phase transition with a respective numerical example

In this section we present another duality principle for a related model in phase transition.
Let Ω = [ 0 , 1 ] R and consider a functional J : V R where
J ( u ) = 1 2 Ω ( ( u ) 2 1 ) 2 d x + 1 2 Ω u 2 d x u , f L 2 ,
and where
V = { u W 1 , 4 ( Ω ) : u ( 0 ) = 0 and u ( 1 ) = 1 / 2 }
and f L 2 ( Ω ) .
A global optimum point is not attained for J so that the problem of finding a global minimum for J has no solution.
Anyway, one question remains, how the minimizing sequences behave close the infimum of J.
We intend to use duality theory to approximately solve such a global optimization problem.
Denoting V 0 = W 0 1 , 4 ( Ω ) , at this point we define, F : V R and F 1 : V × V 0 R by
F ( u ) = 1 2 Ω ( ( u ) 2 1 ) 2 d x ,
and
F 1 ( u , ϕ ) = 1 2 Ω ( ( u + ϕ ) 2 1 ) 2 d x .
Observe that
F ( u ) inf ϕ V 0 F 1 ( u , ϕ ) , u V .
In order to restrict the action of ϕ on the region where the primal functional is non-convex, we redefine a not relabeled
V 0 = ϕ W 0 1 , 4 ( Ω ) : ( ϕ ) 2 1 0 , in Ω
and define also
F 2 : V × V 0 R ,
F 3 : V × V 0 R
and
G : V × V 0 R
by
F 2 ( u , ϕ ) = 1 2 Ω ( ( u + ϕ ) 2 1 ) 2 d x + 1 2 Ω u 2 d x u , f L 2 ,
F 3 ( u , ϕ ) = F 2 ( u , ϕ ) + K 2 Ω ( u ) 2 d x + K 1 2 Ω ( ϕ ) 2 d x
and
G ( u , ϕ ) = K 2 Ω ( u ) 2 d x + K 1 2 Ω ( ϕ ) 2 d x
Denoting Y = Y * = L 2 ( Ω ) we also define the polar functional G * : Y * × Y * R by
G * ( v * , v 0 * ) = sup ( u , ϕ ) V × V 0 { u , v * L 2 + ϕ , v 0 * L 2 G ( u , ϕ ) } .
Observe that
inf u U J ( u ) inf ( ( u , ϕ ) , ( v * , v 0 * ) ) V × V 0 × [ Y * ] 2 { G * ( v * , v 0 * ) u , v * L 2 ϕ , v 0 * L 2 + F 3 ( u , ϕ ) } .
With such results in mind, we define a relaxed primal dual variational formulation for the primal problem, represented by J 1 * : V × V 0 × [ Y * ] 2 R , where
J 1 * ( u , ϕ , v * , v 0 * ) = G * ( v * , v 0 * ) u , v * L 2 ϕ , v 0 * L 2 + F 3 ( u , ϕ ) .
Having defined such a functional, we may obtain numerical results by solving a sequence of convex auxiliary sub-problems, through the following algorithm (in order to obtain the concerning critical points, at first we have neglected the constraint ( ϕ ) 2 1 0 in Ω ).
1.
Set K 0.1 and K 1 = 120.0 and 0 < ε 1 .
2.
Choose ( u 1 , ϕ 1 ) V × V 0 , such that u 1 1 , < 1 and ϕ 1 1 , < 1 .
3.
Set n = 1 .
4.
Calculate ( v n * , ( v 0 * ) n ) solution of the system of equations:
J 1 * ( u n , ϕ n , v n * , ( v 0 * ) n ) v * = 0
and
J 1 * ( u n , ϕ n , v n * , ( v 0 * ) n ) v 0 * = 0 ,
that is
G * ( v n * , ( v 0 * ) n ) v * u n = 0
and
G * ( v n * , ( v 0 * ) n ) v 0 * ϕ n = 0
so that
v n * = G ( u n , ϕ n ) u
and
( v 0 * ) n * = G ( u n , ϕ n ) ϕ
5.
Calculate ( u n + 1 , ϕ n + 1 ) by solving the system of equations:
J 1 * ( u n + 1 , ϕ n + 1 , v n * , ( v 0 * ) n ) u = 0
and
J 1 * ( u n + 1 , ϕ n + 1 , v n * , ( v 0 * ) n ) ϕ = 0
that is
v n * + F 3 ( u n + 1 , ϕ n + 1 ) u = 0
and
( v 0 * ) n + F 3 ( u n + 1 , ϕ n + 1 ) ϕ = 0
6.
If max { u n u n + 1 , ϕ n + 1 ϕ n } ε , then stop, else set n : = n + 1 and go to item 4.
At this point, we present the corresponding software in MAT-LAB, in finite differences and based on the one-dimensional version of the generalized method of lines.
Here the software.
***********************
1.
clear all
m8=300;
d=1/m8;
K=0.1;
K1=120;
for i=1:m8
u o ( i , 1 ) = i 2 * d / 2 ;
vo(i,1)=i*d/10;
yo(i,1)=sin(i*d*pi)/2;
end;
k=1;
b12=1.0;
while ( b 12 > 10 4.3 ) and ( k < 230000 )
k=k+1;
for i=1:m8-1
duo(i,1)=(uo(i+1,1)-uo(i,1))/d;
dvo(i,1)=(vo(i+1,1)-vo(i,1))/d;
end;
m9=zeros(2,2);
m9(1,1)=1;
i=1;
f 1 = 6 * ( d u o ( i , 1 ) + d v o ( i , 1 ) ) 2 2 ;
m80(1,1,i)=-f1-K;
m80(1,2,i)=-f1;
m80(2,1,i)=-f1;
m80(2,2,i)=-f1-K1;
y 11 ( 1 , i ) = K * ( u o ( i + 1 , 1 ) 2 * u o ( i , 1 ) ) / d 2 y o ( i , 1 ) ;
y 11 ( 2 , i ) = K 1 * ( v o ( i + 1 , 1 ) 2 * v o ( i , 1 ) ) / d 2 ;
m 12 = 2 * m 80 ( : , : , i ) m 9 * d 2 ;
m50(:,:,i)=m80(:,:,i)*inv(m12);
z(:,i)=inv(m12)*y11(:,i)* d 2 ;
for i=2:m8-1
f 1 = 6 * ( d u o ( i , 1 ) + d v o ( i , 1 ) ) 2 2 ;
m80(1,1,i)=-f1-K;
m80(1,2,i)=-f1;
m80(2,1,i)=-f1;
m80(2,2,i)=-f1-K1;
y 11 ( 1 , i ) = K * ( u o ( i + 1 , 1 ) 2 * u o ( i , 1 ) + u o ( i 1 , 1 ) ) / d 2 y o ( i , 1 ) ;
y 11 ( 2 , i ) = K 1 * ( v o ( i + 1 , 1 ) 2 * v o ( i , 1 ) + v o ( i 1 , 1 ) ) / d 2 ;
m 12 = 2 * m 80 ( : , : , i ) m 9 * d 2 m 80 ( : , : , i ) * m 50 ( : , : , i 1 ) ;
m50(:,:,i)=inv(m12)*m80(:,:,i);
z ( : , i ) = i n v ( m 12 ) * ( y 11 ( : , i ) * d 2 + m 80 ( : , : , i ) * z ( : , i 1 ) ) ;
end;
U(1,m8)=1/2;
U(2,m8)=0.0;
for i=1:m8-1
U(:,m8-i)=m50(:,:,m8-i)*U(:,m8-i+1)+z(:,m8-i);
end;
for i=1:m8
u(i,1)=U(1,i);
v(i,1)=U(2,i);
end;
b12=max(abs(u-uo))
uo=u;
vo=v;
u(m8/2,1)
end;
for i=1:m8
y(i)=i*d;
end;
plot(y,uo)
**************************************
For the case in which f ( x ) = 0 , we have obtained numerical results for K = 0.1 and K 1 = 120 . For such a concerning solution u 0 obtained, please see Figure 1. For the case in which f ( x ) = sin ( π x ) / 2 , we have obtained numerical results also for K = 0.1 and K 1 = 120 . For such a concerning solution u 0 obtained, please see Figure 2.
Remark 3.1. 
Observe that the solutions obtained are approximate critical points. They are not, in a classical sense, the global solutions for the related optimization problems. Indeed, such solutions reflect the average behavior of weak cluster points for concerning minimizing sequences.

3.1. A general proposal for relaxation

Let Ω R n be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω .
Consider a functional J : V R where
J ( u ) = F ( u ) + G ( u ) u , f 1 L 2 ,
where
V = u W 1 , 4 ( Ω ; R N ) : u = u 0 on Ω ,
u 0 C 1 ( Ω ; R N ) ,
f 1 L 2 ( Ω ; R N ) , G : V R is convex and Fréchet differentiable, and
F ( u ) = Ω f ( u ) d x ,
where f : R N × n R is also Fréchet differentiable.
Assume there exists N ^ N such that
W h y R N × n : f * * ( y ) < f ( y ) = j = 1 N ^ W j
where for each j { 1 , , N ^ } W j R N × n is an open connected set such that W j is regular. We also suppose
W j ¯ W k ¯ = , j k .
Define
W ^ j = v j W 0 1 , 4 ( Ω ; R N ) ; v j ( x ) W j , a . e . in Ω
and define also
W = v = ( v 1 , , v N ^ ) : v j W ^ j j { 1 , , N ^ } and supp v j supp v k = , j k .
At this point we define
h 5 ( u ( x ) , v ( x ) ) = f ( u ( x ) + v j ( x ) ) , if u ( x ) W j , f ( u ( x ) ) , if u ( x ) W h ,
and
H ( u ) = inf v W u Ω h 5 ( u , v ) d x ,
where
W u = { v W : u ( x ) + v j ( x ) W j , if u ( x ) W j , a . e . in Ω , j { 1 , , N ^ } } .
Moreover, we propose the relaxed functional
J 1 ( u ) = H ( u ) + G ( u ) u , f 1 L 2 .
Observe that clearly
inf u V J 1 ( u ) inf u V J ( u ) .

4. A convex dual variational formulation for a third similar model

In this section we present another duality principle for a third related model in phase transition.
Let Ω = [ 0 , 1 ] R and consider a functional J : V R where
J ( u ) = 1 2 Ω min { ( u 1 ) 2 , ( u + 1 ) 2 } d x + 1 2 Ω u 2 d x u , f L 2 ,
and where
V = { u W 1 , 2 ( Ω ) : u ( 0 ) = 0 and u ( 1 ) = 1 / 2 }
and f L 2 ( Ω ) .
A global optimum point is not attained for J so that the problem of finding a global minimum for J has no solution.
Anyway, one question remains, how the minimizing sequences behave close to the infimum of J.
We intend to use the duality theory to solve such a global optimization problem in an appropriate sense to be specified.
At this point we define, F : V R and G : V R by
F ( u ) = 1 2 Ω min { ( u 1 ) 2 , ( u + 1 ) 2 } d x = 1 2 Ω ( u ) 2 d x Ω | u | d x + 1 / 2 F 1 ( u ) ,
and
G ( u ) = 1 2 Ω u 2 d x u , f L 2 .
Denoting Y = Y * = L 2 ( Ω ) we also define the polar functional F 1 * : Y * R and G * : Y * R by
F 1 * ( v * ) = sup v Y { v , v * L 2 F 1 ( v ) } = 1 2 Ω ( v * ) 2 d x + Ω | v * | d x ,
and
G * ( ( v * ) ) = sup u V { u , v * L 2 G ( u ) } = 1 2 Ω ( ( v * ) + f ) 2 d x 1 2 v * ( 1 ) .
Observe this is the scalar case of the calculus of variations, so that from the standard results on convex analysis, we have
inf u V J ( u ) = max v * Y * { F 1 * ( v * ) G * ( ( v * ) ) } .
Indeed, from the direct method of the calculus of variations, the maximum for the dual formulation is attained at some v ^ * Y * .
Moreover, the corresponding solution u 0 V is obtained from the equation
u 0 = G ( ( v ^ * ) ) ( v * ) = ( v ^ * ) + f .
Finally, the Euler-Lagrange equations for the dual problem stands for
( v * ) + f v * sign ( v * ) = 0 , in Ω , ( v * ) ( 0 ) + f ( 0 ) = 0 , ( v * ) ( 1 ) + f ( 1 ) = 1 / 2 ,
where sign ( v * ( x ) ) = 1 if v * ( x ) > 0 , sign ( v * ( x ) ) = 1 , if v * ( x ) < 0 and
1 sign ( v * ( x ) ) 1 ,
if v * ( x ) = 0 .
We have computed the solutions v * and corresponding solutions u 0 V for the cases in which f ( x ) = 0 and f ( x ) = sin ( π x ) / 2 .
For the solution u 0 ( x ) for the case in which f ( x ) = 0 , please see Figure 3.
For the solution u 0 ( x ) for the case in which f ( x ) = sin ( π x ) / 2 , please see Figure 4.
Remark 4.1. 
Observe that such solutions u 0 obtained are not the global solutions for the related primal optimization problems. Indeed, such solutions reflect the average behavior of weak cluster points for concerning minimizing sequences.

4.1. The algorithm through which we have obtained the numerical results

In this subsection we present the software in MATLAB through which we have obtained the last numerical results.
This algorithm is for solving the concerning Euler-Lagrange equations for the dual problem, that is, for solving the equation
( v * ) + f v * sign ( v * ) = 0 , in Ω , ( v * ) ( 0 ) = 0 , ( v * ) ( 1 ) = 1 / 2 .
Here the concerning software in MATLAB. We emphasize to have used the smooth approximation
| v * | ( v * ) 2 + e 1 ,
where a small value for e 1 is specified in the next lines.
*************************************
1.
clear all
2.
m 8 = 800 ; (number of nodes)
3.
d = 1 / m 8 ;
4.
e 1 = 0.00001 ;
5.
f o r i = 1 : m 8
y o ( i , 1 ) = 0.01 ;
y 1 ( i , 1 ) = sin ( π * i / m 8 ) / 2 ;
e n d ;
6.
f o r i = 1 : m 8 1
d y 1 ( i , 1 ) = ( y 1 ( i + 1 , 1 ) y 1 ( i , 1 ) ) / d ;
e n d ;
7.
f o r k = 1 : 3000 (we have fixed the number of iterations)
i = 1 ;
h 3 = 1 / v o ( i , 1 ) 2 + e 1 ;
m 12 = 1 + d 2 * h 3 + d 2 ;
m 50 ( i ) = 1 / m 12 ;
z ( i ) = m 50 ( i ) * ( d y 1 ( i , 1 ) * d 2 ) ;
8.
f o r i = 2 : m 8 1
h 3 = 1 / v o ( i , 1 ) 2 + e 1 ;
m 12 = 2 + h 3 * d 2 + d 2 m 50 ( i 1 ) ;
m 50 ( i ) = 1 / m 12 ;
z ( i ) = m 50 ( i ) * ( z ( i 1 ) + d y 1 ( i , 1 ) * d 2 ) ;
e n d ;
9.
v ( m 8 , 1 ) = ( d / 2 + z ( m 8 1 ) ) / ( 1 m 50 ( m 8 1 ) ) ;
10.
f o r i = 1 : m 8 1
v ( m 8 i , 1 ) = m 50 ( m 8 i ) * v ( m 8 i + 1 ) + z ( m 8 i ) ;
e n d ;
11.
v ( m 8 / 2 , 1 )
12.
v o = v ;
e n d ;
13.
f o r i = 1 : m 8 1
u ( i , 1 ) = ( v ( i + 1 , 1 ) v ( i , 1 ) ) / d + y 1 ( i , 1 ) ;
e n d ;
14.
f o r i = 1 : m 8 1
x ( i ) = i * d ;
e n d ;
p l o t ( x , u ( : , 1 ) )
********************************

5. An improvement of the convexity conditions for a non-convex related model through an approximate primal formulation

In this section we develop an approximate primal dual formulation suitable for a large class of variational models.
Here, the applications are for the Kirchhoff-Love plate model, which may be found in Ciarlet, [11].
At this point we start to describe the primal variational formulation.
Let Ω R 2 be an open, bounded, connected set which represents the middle surface of a plate of thickness h. The boundary of Ω , which is assumed to be regular (Lipschitzian), is denoted by Ω . The vectorial basis related to the cartesian system { x 1 , x 2 , x 3 } is denoted by ( a α , a 3 ) , where α = 1 , 2 (in general Greek indices stand for 1 or 2), and where a 3 is the vector normal to Ω , whereas a 1 and a 2 are orthogonal vectors parallel to Ω . Also, n is the outward normal to the plate surface.
The displacements will be denoted by
u ^ = { u ^ α , u ^ 3 } = u ^ α a α + u ^ 3 a 3 .
The Kirchhoff-Love relations are
u ^ α ( x 1 , x 2 , x 3 ) = u α ( x 1 , x 2 ) x 3 w ( x 1 , x 2 ) , α and u ^ 3 ( x 1 , x 2 , x 3 ) = w ( x 1 , x 2 ) .
Here h / 2 x 3 h / 2 so that we have u = ( u α , w ) U where
U = u = ( u α , w ) W 1 , 2 ( Ω ; R 2 ) × W 2 , 2 ( Ω ) , u α = w = w n = 0 on Ω = W 0 1 , 2 ( Ω ; R 2 ) × W 0 2 , 2 ( Ω ) .
It is worth emphasizing that the boundary conditions here specified refer to a clamped plate.
We also define the operator Λ : U Y × Y , where Y = Y * = L 2 ( Ω ; R 2 × 2 ) , by
Λ ( u ) = { γ ( u ) , κ ( u ) } ,
γ α β ( u ) = u α , β + u β , α 2 + w , α w , β 2 ,
κ α β ( u ) = w , α β .
The constitutive relations are given by
N α β ( u ) = H α β λ μ γ λ μ ( u ) ,
M α β ( u ) = h α β λ μ κ λ μ ( u ) ,
where: { H α β λ μ } and h α β λ μ = h 2 12 H α β λ μ , are symmetric positive definite fourth order tensors. From now on, we denote { H ¯ α β λ μ } = { H α β λ μ } 1 and { h ¯ α β λ μ } = { h α β λ μ } 1 .
Furthermore { N α β } denote the membrane force tensor and { M α β } the moment one. The plate stored energy, represented by ( G Λ ) : U R is expressed by
( G Λ ) ( u ) = 1 2 Ω N α β ( u ) γ α β ( u ) d x + 1 2 Ω M α β ( u ) κ α β ( u ) d x
and the external work, represented by F : U R , is given by
F ( u ) = w , P L 2 + u α , P α L 2 ,
where P , P 1 , P 2 L 2 ( Ω ) are external loads in the directions a 3 , a 1 and a 2 respectively. The potential energy, denoted by J : U R is expressed by:
J ( u ) = ( G Λ ) ( u ) F ( u )
Define now J 3 : U ˜ R by
J 3 ( u ) = J ( u ) + J 5 ( w ) .
where
J 5 ( w ) = 10 Ω a K b w ln ( a ) K 3 / 2 d x + 10 Ω a K ( b w 1 / 100 ) ln ( a ) K 3 / 2 d x .
In such a case for a = 2.71 , K = 185 , b = P / | P | in Ω and
U ˜ = { u U : w 0.01 and P w 0 a . e . in Ω } ,
we get
J 3 ( u ) w = J ( u ) w + J 5 ( u ) w J ( u ) w + O ( ± 3.0 ) ,
and
2 J 3 ( u ) w 2 = 2 J ( u ) w 2 + 2 J 5 ( u ) w 2 2 J ( u ) w 2 + O ( 850 ) .
This new functional J 3 has a relevant improvement in the convexity conditions concerning the previous functional J.
Indeed, we have obtained a gain in positiveness for the second variation 2 J ( u ) w 2 , which has increased of order O ( 700 1000 ) .
Moreover the difference between the approximate and exact equation
J ( u ) w = 0
is of order O ( ± 3.0 ) which corresponds to a small perturbation in the original equation for a load of P = 1500 N / m 2 , for example. Summarizing, the exact equation may be approximately solved in an appropriate sense.

5.1. A duality principle for the concerning quasi-convex envelope

In this section, denoting
V 1 = { ϕ = ϕ ( x , y ) W 1 , 2 ( Ω × Ω ; R 2 ) : ϕ = 0 on Ω × Ω } ,
we define the functional J 1 : U × V 1 R , where
J 1 ( u , ϕ ) = G 1 ( { w , α β } ) + G 2 1 2 ( u α , β + u β , α ) + ϕ α , y β + 1 2 w , α w , β w , P L 2 u α , P α L 2 .
where
G 1 ( { w , α β } ) = 1 2 Ω h α β λ μ w , α β w , λ μ d x
and,
G 2 1 2 ( u α , β + u β , α ) + ϕ α , y β + 1 2 w , α w , β = 1 2 | Ω | Ω Ω H α β λ μ 1 2 ( u α , β + u β , α ) + ϕ α , y β ( x , y ) + 1 2 w , α w , β × 1 2 ( u λ , μ + u λ , μ ) + ϕ λ , y μ ( x , y ) + 1 2 w , λ w , μ d x d y
We define also
J 2 ( { u α } , ϕ ) = inf w W 0 2 , 2 ( Ω ) J 1 ( u , ϕ ) ,
and
J 3 ( { u α } ) = inf ϕ V 1 J 2 ( { u α } , ϕ ) .
It is a well known result from the modern Calculus of Variations theory that
inf u U J ( u ) = inf { u α } W 0 1 , 2 ( Ω ; R 2 ) J 3 ( { u α } ) .
At this point we denote
Y 1 = Y 1 * = Y 3 = Y 3 * L 2 ( Ω × Ω ; R 4 )
and
Y 2 = Y 2 * L 2 ( Ω × Ω ; R 2 ) .
Observe that
J ( u ) = G 1 ( { w , α β } ) + G 2 1 2 ( u α , β + u β , α ) + ϕ α , y β + 1 2 w , α w , β w , P L 2 u α , P α L 2 = G 1 ( { w , α β } ) w , α β , M α β L 2 + w , α β , M α β L 2 + 1 | Ω | Ω Ω w , α ( x ) , Q α ( x , y ) d x d y w , P L 2 1 | Ω | Ω Ω w , α ( x ) , Q α ( x , y ) d x d y + G 2 1 2 ( u α , β + u β , α ) + ϕ α , y β + 1 2 w , α w , β 1 | Ω | Ω Ω 1 2 ( u α , β + u β , α ) + ϕ α , y β + 1 2 w , α w , β , v α β * ( x , y ) d x d y + 1 | Ω | Ω Ω 1 2 ( u α , β + u β , α ) + ϕ α , y β + 1 2 w , α w , β , v α β * ( x , y ) d x d y u α , P α L 2 inf v 3 Y 3 { ( v 3 ) α β , M α β L 2 + G 1 ( ( v 3 ) α β ) } + inf w W 0 2 , 2 ( Ω ) w , α β , M α β L 2 + 1 | Ω | Ω Ω w , α ( x ) Q α ( x , y ) d x d y w , P L 2 + inf v Y 1 1 | Ω | Ω Ω v α β v α β * d x d y + G 2 ( { v α β } ) + inf ( v 2 , { u α } ) Y 2 × W 0 1 , 2 ( Ω ; R 2 ) 1 | Ω | Ω Ω 1 2 ( u α , β + u β , α ) + ϕ α , y β + 1 2 ( v 2 ) α ( x , y ) ( v 2 ) β ( x , y ) × v α β * ( x , y ) d x d y u α , P α L 2 + 1 | Ω | Ω Ω ( v 2 ) α ( x , y ) Q α ( x , y ) d x d y G 1 * ( M ) 1 2 | Ω | Ω Ω v α β * ¯ Q α Q β d x d y 1 2 | Ω | Ω Ω H ¯ α β λ μ v α β * v λ μ * d x d y ,
u U , ( M , Q ) C * , v = { v α β } A * where A * = A 1 * A 2 * B * ,
A 1 * = { { v α β * } Y 1 * : ( v α β * ) , y β = 0 , in Ω } ,
A 2 * = { v α β * } Y 1 * : 1 | Ω | Ω v α β * d y , x β + P α = 0 , in Ω ,
B * = { v α β * } Y 1 * : v α β * ( x , y ) is positive definite in Ω × Ω .
and
C * = ( M , Q ) Y 3 * × Y 2 * : M α β , α β Ω Q α d y , x α P = 0 , in Ω .
Also
v α β * ¯ = v α β * 1 ,
and
{ H ¯ α β λ μ } = { H α β λ μ }
in an appropriate tensor sense.
Here it is worth highlighting we have denoted,
G 1 * ( M ) = sup v 3 Y 3 { ( v 3 ) α β , M α β L 2 G 1 ( v 3 ) } = 1 2 Ω h ¯ α β λ μ M α β M λ μ d x ,
where we recall that
{ h ¯ α β λ μ } = { h α β λ μ } 1
in an appropriate tensorial sense.
Summarizing, defining J * : C * × A * R by
J * ( ( M , Q ) , v * ) = G 1 * ( M ) 1 2 | Ω | Ω Ω v α β * ¯ Q α Q β d x d y 1 2 | Ω | Ω Ω H ¯ α β λ μ v α β * v λ μ * d x d y ,
we have got
inf u U J ( u ) sup ( ( M , Q ) , v * ) C * × A * J * ( ( M , Q ) , v * ) .
Remark 5.1. 
This last dual functional is concave and such a concerning inequality corresponds a duality principle for the relaxed primal formulation.
We emphasize such results are extensions and in some sense complement the original duality principles in the works of Telega and Bielski, [2,3,15].
Moreover, if ( ( M 0 , Q 0 ) , v 0 * ) C * × A * is such that
δ J * ( ( M 0 , Q 0 ) , v 0 * ) = 0 ,
it is a well known result from the Legendre transform proprieties that the corresponding ( u 0 , ϕ 0 ) V × V 1 such that
( w 0 ) , α β = h ¯ α β λ μ ( M 0 ) λ μ ,
and
( v 0 * ) α β = H α β λ ( u 0 ) λ , μ + ( u 0 ) μ , λ 2 + ( ϕ 0 ) λ , y μ + ( ϕ 0 ) μ , y λ 2 + 1 2 ( v 2 0 ) λ ( v 2 0 ) μ ,
( v 0 * ) α β , y β = 0 ,
is also such that
δ J 1 ( u 0 , ϕ 0 ) = 0
and
J 1 ( u 0 , ϕ 0 ) = J * ( ( M 0 , Q 0 ) , v 0 * ) .
From this and
inf u V J ( u ) = inf ( u , ϕ ) V × V 1 J 1 ( u , ϕ ) sup ( ( M , Q ) , v * ) C * × A * J * ( ( M , Q ) , v * ) ,
we obtain
J 1 ( u 0 , ϕ 0 ) = inf ( u , ϕ ) V × V 1 J 1 ( u , ϕ ) = sup ( ( M , Q ) , v * ) C * × A * J * ( ( M , Q ) , v * ) = J * ( ( M 0 , Q 0 ) , v 0 * ) = inf u V J ( u ) .
Also, from the modern calculus of variations theory, there exists a sequence { u n } V such that
u n u 0 , weakly in V ,
and
J ( u n ) J 1 ( u 0 , ϕ 0 ) = inf u V J ( u ) .
From this and the Ekeland variational principle, there exists { v n } V such that
u n v n V 1 / n ,
J ( v n ) inf u V J ( u ) + 1 / n ,
and
δ J ( v n ) V * 1 / n , n N ,
so that
v n u 0 , weakly in V ,
and
J ( v n ) J 1 ( u 0 , ϕ 0 ) = inf u V J ( u ) .
Assume now we are dealing with a finite dimensional version of such a model, in a finite elements of finite differences context, for example.
In such a case we have
v n u 0 , strongly in R N
for an appropriate N N .
From continuity we obtain
δ J ( v n ) δ J ( u 0 ) = 0 ,
J ( v n ) J ( u 0 ) .
Summarizing, we have got
J ( u 0 ) = inf u V J ( u ) ,
δ J ( u 0 ) = 0 .
Here we highlight such last results are valid just for this finite-dimensional model version.

6. An exact convex dual variational formulation for a non-convex primal one

In this section we develop a convex dual variational formulation suitable to compute a critical point for the corresponding primal one.
Let Ω R 2 be an open, bounded, connected set with a regular (Lipschitzian) boundary denoted by Ω .
Consider a functional J : V R where
J ( u ) = F ( u x , u y ) u , f L 2 ,
V = W 0 1 , 2 ( Ω ) and f L 2 ( Ω ) .
Here we denote Y = Y * = L 2 ( Ω ) and Y 1 = Y 1 * = L 2 ( Ω ) × L 2 ( Ω ) .
Defining
V 1 = { u V : u 1 , K 1 }
for some appropriate K 1 > 0 , suppose also F is twice Fréchet differentiable and
det 2 F ( u x , u y ) v 1 v 2 0 ,
u V 1 .
Define now F 1 : V R and F 2 : V R by
F 1 ( u x , u y ) = F ( u x , u y ) + ε 2 Ω u x 2 d x + ε 2 Ω u y 2 d x ,
and
F 2 ( u x , u y ) = ε 2 Ω u x 2 d x + ε 2 Ω u y 2 d x ,
where here we denote d x = d x 1 d x 2 .
Moreover, we define the respective Legendre transform functionals F 1 * and F 2 * as
F 1 * ( v * ) = v 1 , v 1 * L 2 + v 2 , v 2 * L 2 F 1 ( v 1 , v 2 ) ,
where v 1 , v 2 Y are such that
v 1 * = F 1 ( v 1 , v 2 ) v 1 ,
v 2 * = F 1 ( v 1 , v 2 ) v 2 ,
and
F 2 * ( v * ) = v 1 , v 1 * + f 1 L 2 + v 2 , v 2 * L 2 F 2 ( v 1 , v 2 ) ,
where v 1 , v 2 Y are such that
v 1 * + f 1 = F 2 ( v 1 , v 2 ) v 1 ,
v 2 * = F 2 ( v 1 , v 2 ) v 2 .
Here f 1 is any function such that
( f 1 ) x = f , in Ω .
Furthermore, we define
J * ( v * ) = F 1 * ( v * ) + F 2 * ( v * ) = F 1 * ( v * ) + 1 2 ε Ω ( v 1 * + f 1 ) 2 d x + 1 2 ε Ω ( v 2 * ) 2 d x .
Observe that through the target conditions
v 1 * + f 1 = ε u x ,
v 2 * = ε u y ,
we may obtain the compatibility condition
( v 1 * + f 1 ) y ( v 2 * ) x = 0 .
Define now
A * = { v * = ( v 1 * , v 2 * ) B r ( 0 , 0 ) Y 1 * : ( v 1 * + f 1 ) y ( v 2 * ) x = 0 , in Ω } ,
for some appropriate r > 0 such that J * is convex in B r ( 0 , 0 ) .
Consider the problem of minimizing J * subject to v * A * .
Assuming r > 0 is large enough so that the restriction in r is not active, at this point we define the associated Lagrangian
J 1 * ( v * , φ ) = J * ( v * ) + φ , ( v 1 * + f ) y ( v 2 * ) x L 2 ,
where φ is an appropriate Lagrange multiplier.
Therefore
J 1 * ( v * ) = F 1 * ( v * ) + 1 2 ε Ω ( v 1 * + f 1 ) 2 d x + 1 2 ε Ω ( v 2 * ) 2 d x + φ , ( v 1 * + f ) y ( v 2 * ) x L 2 .
The optimal point in question will be a solution of the corresponding Euler-Lagrange equations for J 1 * .
From the variation of J 1 * in v 1 * we obtain
F 1 * ( v * ) v 1 * + v 1 * + f ε φ y = 0 .
From the variation of J 1 * in v 2 * we obtain
F 1 * ( v * ) v 2 * + v 2 * ε + φ x = 0 .
From the variation of J 1 * in φ we have
( v 1 * + f ) y ( v 2 * ) x = 0 .
From this last equation, we may obtain u V such that
v 1 * + f = ε u x ,
and
v 2 * = ε u y .
From this and the previous extremal equations indicated we have
F 1 * ( v * ) v 1 * + u x φ y = 0 ,
and
F 1 * ( v * ) v 2 * + u y + φ x = 0 .
so that
v 1 * + f = F 1 ( u x φ y , u y + φ x ) v 1 ,
and
v 2 * = F 1 ( u x φ y , u y + φ x ) v 2 .
From this and equation (31) and (32) we have
ε F 1 * ( v * ) v 1 * x ε F 1 * ( v * ) v 2 * y + ( v 1 * + f 1 ) x + ( v 2 * ) y = ε u x x ε u y y + ( v 1 * ) x + ( v 2 * ) y + f = 0 .
Replacing the expressions of v 1 * and v 2 * into this last equation, we have
ε u x x ε u y y + F 1 ( u x φ y , u y + φ x ) v 1 x + F 1 ( u x φ y , u y + φ x ) v 2 y + f = 0 ,
so that
F ( u x φ y , u y + φ x ) v 1 x + F ( u x φ y , u y + φ x ) v 2 y + f = 0 , in Ω .
Observe that if
2 φ = 0
then there exists u ^ such that u and φ are also such that
u x φ y = u ^ x
and
u y + φ x = u ^ y .
The boundary conditions for φ must be such that u ^ W 0 1 , 2 .
From this and equation (34) we obtain
δ J ( u ^ ) = 0 .
Summarizing, we may obtain a solution u ^ W 0 1 , 2 of equation δ J ( u ^ ) = 0 by minimizing J * on A * .
Finally, observe that clearly J * is convex in an appropriate large ball B r ( 0 , 0 ) for some appropriate r > 0

7. Another primal dual formulation for a related model

Let Ω R 3 be an open, bounded and connected set with a regular boundary denoted by Ω .
Consider the functional J : V R where
J ( u ) = γ 2 Ω u · u d x + α 2 Ω ( u 2 β ) 2 d x u , f L 2 ,
α > 0 , β > 0 , γ > 0 , V = W 0 1 , 2 ( Ω ) and f L 2 ( Ω ) .
Denoting Y = Y * = L 2 ( Ω ) , define now J 1 * : V × Y * R by
J 1 * ( u , v 0 * ) = γ 2 Ω u · u d x u 2 , v 0 * L 2 + K 1 2 Ω ( γ 2 u + 2 v 0 * u f ) 2 d x + u , f L 2 + 1 2 α Ω ( v 0 * ) 2 d x + β Ω v 0 * d x ,
Define also
A + = { u V : u f 0 , a . e . in Ω } ,
V 2 = { u V : u K 3 } ,
and
V 1 = V 2 A +
for some appropriate K 3 > 0 to be specified.
Moreover define
B * = { v 0 * Y * : v 0 * K }
for some appropriate K > 0 to be specified.
Observe that, denoting
φ = γ 2 u + 2 v 0 * u f
we have
2 J 1 * ( u , v 0 * ) ( v 0 * ) 2 = 1 α + 4 K 1 u 2
2 J 1 * ( u , v 0 * ) u 2 = γ 2 2 v 0 * + K 1 ( γ 2 + 2 v 0 * ) 2
and
2 J 1 * ( u , v 0 * ) u v 0 * = K 1 ( 2 φ + 2 ( γ 2 u + 2 v 0 * u ) ) 2 u
so that
det { δ 2 J 1 * ( u , v 0 * ) } = 2 J 1 * ( u , v 0 * ) ( v 0 * ) 2 2 J 1 * ( u , v 0 * ) u 2 2 J 1 * ( u , v 0 * ) u v 0 * 2 = K 1 ( γ 2 + 2 v 0 * ) 2 α γ 2 + 2 v 0 * + 4 α u 2 α 4 K 1 2 φ 2 8 K 1 φ ( γ 2 + 2 v 0 * ) u + 8 K 1 φ u + 4 K 1 ( γ 2 u + 2 v 0 * u ) u .
Observe now that a critical point φ = 0 and ( γ 2 u + 2 v 0 * u ) u = f u 0 in Ω .
Therefore, for an appropriate large K 1 > 0 , also at a critical point, we have
det { δ 2 J 1 * ( u , v 0 * ) } = 4 K 1 f u δ 2 J ( u ) α + K 1 ( γ 2 + 2 v 0 * ) 2 α > 0 .
Remark 7.1. 
From this last equation we may observe that J 1 * has a large region of convexity about any critical point ( u 0 , v ^ 0 * ) , that is, there exists a large r > 0 such that J 1 * is convex on B r ( u 0 , v ^ 0 * ) .
With such results in mind, we may easily prove the following theorem.
Theorem 7.2. 
Assume K 1 max { 1 , K , K 3 } and suppose ( u 0 , v ^ 0 * ) V 1 × B * is such that
δ J 1 * ( u 0 , v ^ 0 * ) = 0 .
Under such hypotheses, there exists r > 0 such that J 1 * is convex in E * = B r ( u 0 , v ^ 0 * ) ( V 1 × B * ) ,
δ J ( u 0 ) = 0 ,
and
J ( u 0 ) = J 1 ( u 0 , v ^ 0 * ) = inf ( u , v 0 * ) E * J 1 * ( u , v 0 * ) .

8. A third primal dual formulation for a related model

Let Ω R 3 be an open, bounded and connected set with a regular boundary denoted by Ω .
Consider the functional J : V R where
J ( u ) = γ 2 Ω u · u d x + α 2 Ω ( u 2 β ) 2 d x u , f L 2 ,
α > 0 , β > 0 , γ > 0 , V = W 0 1 , 2 ( Ω ) and f L 2 ( Ω ) .
Denoting Y = Y * = L 2 ( Ω ) , define now J 1 * : V × Y * × Y * R by
J 1 * ( u , v 0 * , v 1 * ) = γ 2 Ω u · u d x + 1 2 Ω K u 2 d x u , v 1 * L 2 + 1 2 Ω ( v 1 * ) 2 ( 2 v 0 * + K ) d x + 1 2 ( α + ε ) Ω ( v 0 * α ( u 2 β ) ) 2 d x + u , f L 2 1 2 α Ω ( v 0 * ) 2 d x β Ω v 0 * d x ,
where ε > 0 is a small real constant.
Define also
A + = { u V : u f 0 , a . e . in Ω } ,
V 2 = { u V : u K 3 } ,
and
V 1 = V 2 A +
for some appropriate K 3 > 0 to be specified.
Moreover define
B * = { v 0 * Y * : v 0 * K 4 }
and
D * = { v 1 * Y * : v 1 * K 5 } ,
for some appropriate real constants K 4 , K 5 > 0 to be specified.
Remark 8.1. 
Define now
H 1 ( u , v 0 * ) = γ 2 + 2 v 0 * + 4 α u 2
For an appropriate function (or, in a more general fashion, an appropriate bounded operator) M 1 define
B 1 * = { v 0 * B * : 2 v 0 * + M 1 ε 1 } ,
for some small parameter ε 1 > 0 .
Moreover, define
E * = { u V 1 : 4 α | u | | M 1 + γ 2 | .
Since for ( u , v 0 * ) V 1 × B 1 * we have u f 0 , in Ω , so that for u 1 , u 2 V 1 we have
sign ( u 1 ) = sign ( u 2 ) in Ω ,
we may infer that E * is a convex set.
Moreover if ( u , v 0 * ) E * × B 1 * , then
4 α | u | | M 1 + γ 2 |
so that
4 α u 2 M 1 + γ 2
and
2 v 0 * + M 1 ε 1
so that
H 1 ( u , v 0 * ) = γ 2 + 2 v 0 * + 4 α u 2 ε 1 .
Such a result we will be used many times in the next sections.
Observe that, defining
φ = v 0 * α ( u 2 β )
we may obtain
2 J 1 * ( u , v 0 * , v 1 * ) u 2 = γ 2 + K + α α + ε 4 u 2 2 φ α α + ε
2 J 1 * ( u , v 0 * , v 1 * ) ( v 1 * ) 2 = 1 2 v 0 * + K
and
2 J 1 * ( u , v 0 * , v 1 * ) u v 1 * = 1
so that
det 2 J 1 * ( u , v 0 * , v 1 * ) u v 1 * = 2 J 1 * ( u , v 1 * , v 0 * ) ( v 1 * ) 2 2 J 1 * ( u , v 1 * , v 0 * ) u 2 2 J 1 * ( u , v 1 * , v 0 * ) u v 1 * 2 = γ 2 + 2 v 0 * + 4 α 2 α + ε u 2 2 α α + ε φ 2 v 0 * + K H ( u , v 0 * ) .
However, at a critical point, we have φ = 0 so that, for a fixed v 0 * B * we define the non-active but convex restriction
( C 1 ) v 0 * * = { u V 1 : ( φ ) 2 ε } ,
for a small parameter ε > 0 .
From such results, assuming K max { K 3 , K 4 , K 5 } , and 0 < ε ε 1 1 , we have that
H ( u , v 0 * ) > 0 ,
for v 0 * B 1 * and u E * ( C 1 ) v 0 * * .
With such results in mind, we may easily prove the following theorem.
Theorem 8.2. 
Suppose ( u 0 , v ^ 1 * , v ^ 0 * ) ( E * ( C 1 ) v ^ 0 * * ) × D * × B 1 * is such that
δ J 1 * ( u 0 , v ^ 1 * , v ^ 0 * ) = 0 .
Under such hypotheses, we have that
δ J ( u 0 ) = 0
and
J ( u 0 ) = inf u ( C 1 ) v ^ 0 * * J ( u ) = J 1 * ( u 0 , v ^ 1 * , v ^ 0 * ) = inf ( u , v 1 * ) ( C 1 ) v ^ 0 * * × D * sup v 0 * B * J 1 * ( u , v 1 * , v 0 * ) = sup v 0 * B * inf ( u , v 1 * ) ( C 1 ) v ^ 0 * * × D * J 1 * ( u , v 1 * , v 0 * ) .
Proof. 
The proof that
δ J ( u 0 ) = 0
and
J ( u 0 ) = J 1 * ( u 0 , v ^ 1 * , v ^ 0 * )
may be easily made similarly as in the previous sections.
Moreover, observe that for K > 0 sufficiently large, we have
2 J 1 * ( u 0 , v ^ 1 * , v 0 * ) ( v 0 * ) 2 < 0 , v 0 * B *
so that this and the other hypotheses, we have also
J 1 * ( u 0 , v ^ 1 * , v ^ 0 * ) = inf ( u , v 1 * ) ( C 1 ) v ^ 0 * * × D * J 1 * ( u , v 1 * , v ^ 0 * )
and
J 1 * ( u 0 , v ^ 1 * , v ^ 0 * ) = sup v 0 * B * J 1 * ( u 0 , v ^ 1 * , v 0 * ) .
From this, from a standard saddle point theorem and the remaining hypotheses, we may infer that
J ( u 0 ) = J 1 * ( u 0 , v ^ 1 * , v ^ 0 * ) = inf ( u , v 1 * ) ( C 1 ) v ^ 0 * * × D * sup v 0 * B * J 1 * ( u , v 1 * , v 0 * ) = sup v 0 * B * inf ( u , v 1 * ) ( C 1 ) v ^ 0 * * × D * J 1 * ( u , v 1 * , v 0 * ) .
Moreover, observe that
J 1 * ( u 0 , v ^ 1 * , v ^ 0 * ) = inf ( u , v 1 * ) ( C 1 ) v ^ 0 * * × D * J 1 * ( u , v 1 * , v ^ 0 * ) γ 2 Ω u · u d x + K 2 Ω u 2 d x + u 2 , v ^ 0 * L 2 K 2 Ω u 2 d x 1 2 α Ω ( v ^ 0 * ) 2 d x β Ω v ^ 0 * d x + 1 2 ( α + ε ) Ω ( v ^ 0 * α ( u 2 β ) ) 2 d x u , f L 2 sup v 0 * Y * γ 2 Ω u · u d x + u 2 , v 0 * 1 2 α Ω ( v 0 * ) 2 d x β Ω v 0 * d x + 1 2 ( α + ε ) Ω ( v 0 * α ( u 2 β ) ) 2 d x u , f L 2 = γ 2 Ω u · u d x + α 2 Ω ( u 2 β ) 2 d x u , f L 2 , u ( C 1 ) v ^ 0 * * .
Summarizing, we have got
J ( u 0 ) = J 1 * ( u 0 , v ^ 1 * , v ^ 0 * ) inf u ( C 1 ) v ^ 0 * * J ( u ) .
From such results, we may infer that
J ( u 0 ) = inf u ( C 1 ) v ^ 0 * * J ( u ) = J 1 * ( u 0 , v ^ 1 * , v ^ 0 * ) = inf ( u , v 1 * ) ( C 1 ) v ^ 0 * * × D * sup v 0 * B * J 1 * ( u , v 1 * , v 0 * ) = sup v 0 * B * inf ( u , v 1 * ) ( C 1 ) v ^ 0 * * × D * J 1 * ( u , v 1 * , v 0 * ) .
The proof is complete. □

9. An algorithm for a related model in shape optimization

The next two subsections have been previously published by Fabio Silva Botelho and Alexandre Molter in [5], Chapter 21.

9.1. Introduction

Consider an elastic solid which the volume corresponds to an open, bounded, connected set, denoted by Ω R 3 with a regular (Lipschitzian) boundary denoted by Ω = Γ 0 Γ t where Γ 0 Γ t = . Consider also the problem of minimizing the functional J ^ : U × B R where
J ^ ( u , t ) = 1 2 u i , f i L 2 ( Ω ) + 1 2 u i , f ^ i L 2 ( Γ t ) ,
subject to
( H i j k l ( t ) e k l ( u ) ) , j + f i = 0 in Ω , H i j k l ( t ) e k l ( u ) n j f ^ i = 0 , on Γ t , i { 1 , 2 , 3 } .
Here n = ( n 1 , n 2 , n 3 ) denotes the outward normal to Ω and
U = { u = ( u 1 , u 2 , u 3 ) W 1 , 2 ( Ω ; R 3 ) : u = ( 0 , 0 , 0 ) = 0 on Γ 0 } ,
B = t : Ω [ 0 , 1 ] measurable : Ω t ( x ) d x = t 1 | Ω | ,
where
0 < t 1 < 1
and | Ω | denotes the Lebesgue measure of Ω .
Moreover u = ( u 1 , u 2 , u 3 ) W 1 , 2 ( Ω ; R 3 ) is the field of displacements relating the cartesian system ( 0 , x 1 , x 2 , x 3 ) , resulting from the action of the external loads f L 2 ( Ω ; R 3 ) and f ^ L 2 ( Γ t ; R 3 ) .
We also define the stress tensor { σ i j } Y * = Y = L 2 ( Ω ; R 3 × 3 ) , by
σ i j ( u ) = H i j k l ( t ) e k l ( u ) ,
and the strain tensor e : U L 2 ( Ω ; R 3 × 3 ) by
e i j ( u ) = 1 2 ( u i , j + u j , i ) , i , j { 1 , 2 , 3 } .
Finally,
{ H i j k l ( t ) } = { t H i j k l 0 + ( 1 t ) H i j k l 1 } ,
where H 0 corresponds to a strong material and H 1 to a very soft material, intending to simulate voids along the solid structure.
The variable t is the design one, which the optimal distribution values along the structure are intended to minimize its inner work with a volume restriction indicated through the set B.
The duality principle obtained is developed inspired by the works in [2,3]. Similar theoretical results have been developed in [10], however we believe the proof here presented, which is based on the min-max theorem is easier to follow (indeed we thank an anonymous referee for his suggestion about applying the min-max theorem to complete the proof). We highlight throughout this text we have used the standard Einstein sum convention of repeated indices.
Moreover, details on the Sobolev spaces addressed may be found in [1]. In addition, the primal variational development of the topology optimization problem has been described in [10].
The main contributions of this work are to present the detailed development, through duality theory, for such a kind of optimization problems. We emphasize that to avoid the check-board standard and obtain appropriate robust optimized structures without the use of filters, it is necessary to discretize more in the load direction, in which the displacements are much larger.

9.2. Mathematical formulation of the topology optimization problem

Our mathematical topology optimization problem is summarized by the following theorem.
Theorem 9.1. 
Consider the statements and assumptions indicated in the last section, in particular those refereing to Ω and the functional J ^ : U × B R .
Define J 1 : U × B R by
J 1 ( u , t ) = G ( e ( u ) , t ) + u i , f i L 2 ( Ω ) + u i , f ^ i L 2 ( Γ t ) ,
where
G ( e ( u ) , t ) = 1 2 Ω H i j k l ( t ) e i j ( u ) e k l ( u ) d x ,
and where
d x = d x 1 d x 2 d x 3 .
Define also J * : U R by
J * ( u ) = inf t B { J 1 ( u , t ) } = inf t B { G ( e ( u ) , t ) + u i , f i L 2 ( Ω ) + u i , f ^ i L 2 ( Γ t ) } .
Assume there exists c 0 , c 1 > 0 such that
H i j k l 0 z i j z k l > c 0 z i j z i j
and
H i j k l 1 z i j z k l > c 1 z i j z i j , z = { z i j } R 3 × 3 , such that z 0 .
Finally, define J : U × B R { + } by
J ( u , t ) = J ^ ( u , t ) + I n d ( u , t ) ,
where
I n d ( u , t ) = 0 , if ( u , t ) A * , + , otherwise ,
where A * = A 1 A 2 ,
A 1 = { ( u , t ) U × B : ( σ i j ( u ) ) , j + f i = 0 , in Ω , i { 1 , 2 , 3 } }
and
A 2 = { ( u , t ) U × B : σ i j ( u ) n j f ^ i = 0 , on Γ t , i { 1 , 2 , 3 } } .
Under such hypotheses, there exists ( u 0 , t 0 ) U × B such that
J ( u 0 , t 0 ) = inf ( u , t ) U × B J ( u , t ) = sup u ^ U J * ( u ^ ) = J * ( u 0 ) = J ^ ( u 0 , t 0 ) = inf ( t , σ ) B × C * G * ( σ , t ) = G * ( σ ( u 0 ) , t 0 ) ,
where
G * ( σ , t ) = sup v Y { v i j , σ i j L 2 ( Ω ) G ( v , t ) } = 1 2 Ω H ¯ i j k l ( t ) σ i j σ k l d x ,
{ H ¯ i j k l ( t ) } = { H i j k l ( t ) } 1
and C * = C 1 C 2 , where
C 1 = { σ Y * : σ i j , j + f i = 0 , in Ω , i { 1 , 2 , 3 } }
and
C 2 = { σ Y * : σ i j n j f ^ i = 0 , on Γ t , i { 1 , 2 , 3 } } .
Proof. 
Observe that
inf ( u , t ) U × B J ( u , t ) = inf t B inf u U J ( u , t ) = inf t B sup u ^ U inf u U 1 2 Ω H i j k l ( t ) e i j ( u ) e k l ( u ) d x + u ^ i , ( H i j k l ( t ) e k l ( u ) ) , j + f i L 2 ( Ω ) u ^ i , H i j k l ( t ) e k l ( u ) n j f ^ i L 2 ( Γ t ) = inf t B sup u ^ U inf u U 1 2 Ω H i j k l ( t ) e i j ( u ) e k l ( u ) d x Ω H i j k l ( t ) e i j ( u ^ ) e k l ( u ) d x + u ^ i , f i L 2 ( Ω ) + u ^ i , f ^ i L 2 ( Γ t ) = inf t B sup u ^ U Ω H i j k l ( t ) e i j ( u ^ ) e k l ( u ^ ) d x u ^ i , f i L 2 ( Ω ) + u ^ i , f ^ i L 2 ( Γ t ) = inf t B inf σ C * G * ( σ , t ) .
Also, from this and the min-max theorem, there exist ( u 0 , t 0 ) U × B such that
inf ( u , t ) U × B J ( u , t ) = inf t B sup u ^ U J 1 ( u , t ) = sup u U inf t B J 1 ( u , t ) = J 1 ( u 0 , t 0 ) = inf t B J 1 ( u 0 , t ) = J * ( u 0 ) .
Finally, from the extremal necessary condition
J 1 ( u 0 , t 0 ) u = 0
we obtain
( H i j k l ( t 0 ) e k l ( u 0 ) ) , j + f i = 0 in Ω ,
and
H i j k l ( t 0 ) e k l ( u 0 ) n j f ^ i = 0 on Γ t , i { 1 , 2 , 3 } ,
so that
G ( e ( u 0 ) ) = 1 2 ( u 0 ) i , f i L 2 ( Ω ) + 1 2 ( u 0 ) i , f ^ i L 2 ( Γ t ) .
Hence ( u 0 , t 0 ) A * so that I n d ( u 0 , t 0 ) = 0 and σ ( u 0 ) C * .
Moreover
J * ( u 0 ) = G ( e ( u 0 ) ) + ( u 0 ) i , f i L 2 ( Ω ) + ( u 0 ) i , f ^ i L 2 ( Γ t ) = G ( e ( u 0 ) ) = G ( e ( u 0 ) ) + I n d ( u 0 , t 0 ) = J ( u 0 , t 0 ) = G * ( σ ( u 0 ) , t 0 ) .
This completes the proof. □

9.3. About a concerning algorithm and related numerical method

For numerically solve this optimization problem in question, we present the following algorithm
1.
Set t 1 = 0.5 in Ω and n = 1 .
2.
Calculate u n U such that
J 1 ( u n , t n ) = sup u U J 1 ( u , t n ) .
3.
Calculate t n + 1 B such that
J 1 ( u n , t n + 1 ) = inf t B J 1 ( u n , t ) .
4.
If t n + 1 t n < 10 4 or n > 100 then stop, else set n : = n + 1 and go to item 2.
We have developed a software in finite differences for solving such a problem.
Here the software.
**************************************
1
clear all
global P m8 d w u v Ea Eb Lo d1 z1 m9 du1 du2 dv1 dv2 c3
m8=27;
m9=24;
c3=0.95;
d=1.0/m8;
d1=0.5/m9;
Ea= 210 * 10 5 ; (stronger material)
Eb=1000; (softer material simulating voids)
w=0.30;
P=-42000000;
z1=(m8-1)*(m9-1);
A3=zeros(z1,z1);
for i=1:z1
A3(1,i)=1.0;
end;
b=zeros(z1,1);
uo=0.000001*ones(z1,1);
u1=ones(z1,1);
b(1,1)=c3*z1;
for i=1:m9-1
for j=1:m8-1
Lo(i,j)=c3;
end; end;
for i=1:z1
x1(i)=c3*z1;
end;
for i=1:2*m8*m9
xo(i)=0.000;
end;
xw=xo;
xv=Lo;
for k2=1:24
c3=0.98*c3;
b(1,1)=c3*z1;
k2
b14=1.0;
k3=0;
while ( b 14 > 10 3.5 ) and ( k 3 < 5 )
k3=k3+1;
b12=1.0;
k=0;
while ( b 12 > 10 4.0 ) and ( k < 120 )
k=k+1;
k2
k3
k
X=fminunc(’funbeam’,xo);
xo=X;
b12=max(abs(xw-xo));
xw=X;
end;
for i=1:m9-1
for j=1:m8-1
E 1 = L o ( i , j ) 2 * ( E a E b ) ;
ex=du1(i,j);
ey=dv2(i,j);
exy=1/2*(dv1(i,j)+du2(i,j));
S x = E 1 * ( e x + w * e y ) / ( 1 w 2 ) ;
S y = E 1 * ( w * e x + e y ) / ( 1 w 2 ) ;
Sxy=E1/(2*(1+w))*exy;
dc3(i,j)=-(Sx*ex+Sy*ey+2*Sxy*exy);
end;
end;
for i=1:m9-1
for j=1:m8-1
f(j+(i-1)*(m8-1))=dc3(i,j);
end;
end;
for k1=1:1
k1
X1=linprog(f, [ ] , [ ] ,A3,b,uo,u1,x1);
x1=X1;
end;
for i=1:m9-1
for j=1:m8-1
Lo(i,j)=X1(j+(m8-1)*(i-1));
end;
end;
b14=max(max(abs(Lo-xv)))
xv=Lo;
colormap(gray); imagesc(-Lo); axis equal; axis tight; axis off;pause(1e-6)
end;
end;
****************************************************
Here the auxiliary Function ’funbeam’
function S=funbeam(x)
global P m8 d w u v Ea Eb Lo d1 m9 du1 du2 dv1 dv2
for i=1:m9
for j=1:m8
u(i,j)=x(j+(m8)*(i-1));
v(i,j)=x(m8*m9+(i-1)*m8+j);
end;
end;
for i=1:m9
end;
u(m9-1,1)=0;
v(m9-1,1)=0;
u(m9-1,m8-1)=0;
v(m9-1,m8-1)=0;
for i=1:m9-1
for j=1:m8-1
du1(i,j)=(u(i,j+1)-u(i,j))/d;
du2(i,j)=(u(i+1,j)-u(i,j))/d1;
dv1(i,j)=(v(i,j+1)-v(i,j))/d;
dv2(i,j)=(v(i+1,j)-v(i,j))/d1;
end;
end;
S=0;
for i=1:m9-1
for j=1:m8-1
E 1 = L o ( i , j ) 3 * E a + ( 1 L o ( i , j ) 3 ) * E b ;
ex=du1(i,j);
ey=dv2(i,j);
exy=1/2*(dv1(i,j)+du2(i,j));
S x = E 1 * ( e x + w * e y ) / ( 1 w 2 ) ;
S y = E 1 * ( w * e x + e y ) / ( 1 w 2 ) ;
Sxy=E1/(2*(1+w))*exy;
S=S+1/2*(Sx*ex+Sy*ey+2*Sxy*exy);
end;
end;
S=S*d*d1-P*v(2,(m8)/3)*d*d1;
***********************************************
For a two dimensional beam of dimensions 1 m × 0.5 m and t 1 = 0.63 we have obtained the following results:
1.
Case A: For the optimal shape for a clamped beam at left (cantilever) and load P = 4 10 6 N j at ( x , y ) = ( 1 , 0.25 ) , please Figure 5.
2.
Case B :For the optimal shape for a simply supported beam at ( 0 , 0 ) and ( 1 , 0 ) and load P = 4 10 6 N j at ( x , y ) = ( 1 / 3 , 0.5 ) , please Figure 6.
In the first case the mesh was 28 × 24 . In the second one the mesh was 27 × 24

10. A duality principle for a general vectorial case in the calculus of variations

In this section we develop a duality principle for a general vectorial case in variational optimization.
Let Ω R 3 be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω . Let J : V R be a functional where
J ( u ) = G ( u 1 , , u N ) u , f L 2 ,
where
V = W 0 1 , 2 ( Ω ; R N )
and
f = ( f 1 , , f N ) L 2 ( Ω ; R N ) .
Here we have denoted u = ( u 1 , , u N ) V and
u , f L 2 = u i , f i L 2 ,
so that we may also denote
J ( u ) = G ( u ) u , f L 2 .
Assume
G ( u ) = Ω g ( u ) d x
where g : R 3 N R is a differentiable function such that
g ( y ) +
as | y | . Moreover, suppose there exists α R such that
α = inf u V J ( u ) .
It is well known that
α = inf u V J ( u ) = inf u V J * * ( u ) = inf u V { ( G ) * * ( u ) u , f L 2 } .
Under some mild hypotheses, from convexity, we have that
inf u V { ( G ) * * ( u ) u , f L 2 } = sup v * A * { ( G ) * ( d i v v * ) } = ( G ) * ( f ) ,
where
A * = { v * Y = Y * = L 2 ( Ω ; R 3 N ) : d i v v * + f = 0 } .
Now observe that the restriction v = u for some u V is equivalent to the restriction
curl v i = 0 , in Ω
where v = { v i } = { v i j } j = 1 3 , i { 1 , , N } , with appropriate boundary conditions, so that with an appropriate Lagrange multiplier ϕ = { ϕ i } , we obtain
( G ) * ( d i v v * ) = sup u V { u , d i v v * L 2 G ( u ) } = sup u V { u , v * L 2 G ( u ) } inf ϕ Y * sup v Y { v , v * L 2 G ( v ) + ϕ , curl v L 2 = inf ϕ Y * G * ( v * + curl ϕ ) .
where we have denoted
curl v = { curl v i }
and
curl ϕ = { curl ϕ i } .
Joining the pieces, we have got
inf u V J ( u ) = inf u V { G ( u ) u , f L 2 } sup ( v * , ϕ ) A * × Y * { G * ( v * + curl ϕ ) } ,
where we recall that Y = Y * = L 2 ( Ω ; R 3 N ) .
We emphasize such a dual formulation in ( v * , ϕ ) is convex (in fact concave).

11. A note on the Galerkin Functional

Let Ω R 3 be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω .
Consider the functional J : V R where
J ( u ) = γ 2 Ω u · u d x + α 4 Ω u 4 d x β 2 Ω u 2 d x u , f L 2
Here V = W 0 1 , 2 ( Ω ) , γ > 0 , α > 0 , β > 0 .
We denote also
Y = Y * = L 2 ( Ω ) .
At this point we define
A + = { u V : u f 0 , in Ω } ,
V 2 = { u V : u K 3 } ,
for some appropriate real constant K 3 > 0 and
V 1 = A + V 2 .
Observe that
J ( u ) = γ 2 u + α u 3 β f ,
so that we define the Galerkin functional J 1 : V R by
J 1 ( u ) = 1 2 J ( u ) 2 2 = 1 2 Ω ( γ 2 u + α u 3 β u f ) 2 d x .
From this, we get
2 J 1 ( u ) u 2 = ( γ u + α u 3 β u f ) 6 α u + ( γ 2 + 3 α u 2 β ) 2 .
Define now
φ 2 = ( γ 2 u + α u 3 β u f ) 2 .
At this point, for an appropriate small real constant ε 1 > 0 and bounded constant operator M 1 > ε 1 , we set the intended non-active restriction
3 α | u | | M 1 + γ 2 + β | ,
and define
B 1 = { u V 1 : 3 α | u | | M 1 + γ 2 + β | } .
Observe that since for u V 1 we have u f 0 in Ω so that if u 1 , u 2 V 1 then
sign ( u 1 ) = sign ( u 2 ) , in Ω ,
we may infer that B 1 is a convex set.
Furthermore, if u B 1 , then
3 α | u | | M 1 + γ 2 + β | ,
so that
3 α u 2 M 1 + γ 2 + β ,
and hence
δ 2 J ( u ) = γ 2 + 3 α u 2 β M 1 > ε 1 > 0 .
For a small parameter ε > 0 we define the intended non-active restriction
φ 2 ε , in Ω ,
and define
B 2 = { u V 1 : φ 2 ε , in Ω } .
Observe that for α > 0 and β > 0 sufficiently large φ 2 is convex in V 1 (positive definite Hessian) so that B 2 is a convex set. Assuming 0 < ε ε 1 1 , define B 3 = B 1 B 2 , which is a convex set.
Summarizing, if u B 3 , then
δ 2 J 1 ( u ) 0 .
With such results in mind, we define the following convex optimization problem for finding a critical point of J.
Minimize
J 1 ( u ) = 1 2 J ( u ) 2 2 = 1 2 Ω ( γ 2 u + α u 3 β u f ) 2 d x ,
subject to
u B 3 .
Observe that a critical point u 0 B 3 of J 1 , from such a concerning convexity of J 1 on the convex set B 1 , is also such that
J ( u 0 ) = min u B 3 J 1 ( u ) .
Finally, we may also define the convex optimization problem of minimizing
J 3 ( u ) = K 1 J 1 ( u ) + J ( u ) = K 1 2 Ω ( γ 2 u + α u 3 β u f ) 2 d x + γ 2 Ω u · u d x + α 4 Ω u 4 d x β 2 Ω u 2 d x u , f L 2 ,
subject to
u B 3 .
Here K 1 > 0 is a large real constant.
Such a functional J 3 is also convex on B 3 so that a critical point u 0 B 3 of J is also a critical point of J 3 , and thus
J 3 ( u 0 ) = min u B 3 J 3 ( u ) .

12. A note on the Legendre-Galerkin functional

Let Ω R 3 be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω .
Consider the functional J : V R where
J ( u ) = γ 2 Ω u · u d x + α 4 Ω u 4 d x β 2 Ω u 2 d x u , f L 2
Here V = W 0 1 , 2 ( Ω ) , γ > 0 , α > 0 , β > 0 .
We denote also
Y = Y * = L 2 ( Ω )
and F 1 : V R , F 2 : V R and F 3 : V R by
F 1 ( u ) = γ 2 Ω u · u d x ,
F 2 ( u ) = α 4 Ω u 4 d x ,
F 3 ( u ) = β 2 Ω u 2 d x .
Moreover, we define F 1 * , F 2 * , F 3 * : Y * R by
F 1 * ( v 1 * ) = sup u V { u , v 1 * L 2 F 1 ( u ) } = 1 2 Ω ( v 1 * ) 2 γ 2 d x ,
F 2 * ( v 2 * ) = sup u V { u , v 2 * L 2 F 2 ( u ) } = 3 4 Ω ( v 2 * ) 4 / 3 α 1 / 3 d x ,
F 3 * ( v 3 * ) = sup u V { u , v 3 * L 2 F 3 ( u ) } = 1 2 β Ω ( v 3 * ) 2 d x .
Observe now that these three last suprema are attained through the equations,
v 1 * = F 1 ( u ) u = γ 2 u ,
v 2 * = F 2 ( u ) u = α u 3
v 3 * = F 3 ( u ) u = β u .
From such results, at a critical point, we obtain the following compatibility conditions
u = v 1 * γ 2 = v 2 * β 1 / 3 = v 3 * β .
From such relations we have
v 1 * γ 2 = v 3 * β ,
and
v 2 * = α v 3 * β 3 ,
so that
v 1 * = γ 2 v 3 * β ,
and
v 2 * = α v 3 * β 3 .
Moreover, we define the functional F 4 * : Y * R , by
F 4 * ( v * ) = sup u V { u , v 1 * + v 2 * v 3 * L 2 u , f L 2 } .
Therefore
F 4 * ( v * ) = 0 , if v 1 * + v 2 * v 3 * f = 0 , in Ω , + , otherwise .
Hence, a critical point of J corresponds to the solution of the following system of equations
v 1 * = γ 2 v 3 * β ,
v 2 * = α v 3 * β 3 ,
and
v 1 * + v 2 * v 3 * f = 0 , in Ω .
From this last equation we may obtain
v 1 * = v 2 * + v 3 * + f ,
so that the final equations to be solved are
v 2 * + v 3 * + f + γ 2 v 3 * β = 0
and
v 2 * α v 3 * β 3 = 0 , in Ω ,
with the boundary conditions
u = v 3 * β = 0 , on Ω .
With such results in mind, we define the Legendre-Galerkin functional J * : [ Y * ] 2 R , where
J * ( v * ) = 1 2 Ω v 2 * + v 3 * + f + γ 2 v 3 * β 2 d x + 1 2 Ω v 2 * α v 3 * β 3 2 d x .
At this point, defining
φ = v 2 * α v 3 * β 3 ,
we obtain
2 J * ( v * ) ( v 2 * ) 2 = 2 ;
2 J * ( v * ) ( v 3 * ) 2 = 1 γ 2 β 2 + 9 α 2 ( v 3 * ) 4 β 6 + O ( φ ) ,
2 J * ( v * ) v 2 * v 3 * = 3 α ( v 3 * ) 2 β 3 + 1 γ 2 β .
From such results we may infer that
det 2 J * ( v * ) v 2 * v 3 * = 2 J * ( v * ) ( v 2 * ) 2 2 J * ( v * ) ( v 3 * ) 2 2 J * ( v * ) v 2 * v 3 * 2 = 1 γ 2 β + 3 α ( v 3 * ) 2 β 3 2 + O ( φ )
Observe that a critical point φ = 0 so that δ 2 J * ( v * ) > 0 at a neighborhood of any critical point.
At this point we define
A + = v * = ( v 2 * , v 3 * ) [ Y * ] 2 : v 3 * β f 0 , in Ω ,
D * = { v * = ( v 2 * , v 3 * ) [ Y * ] 2 : v * K } ,
for an appropriate real constant K > 0 .
Define now E * = A + D * ,
C 1 * = { v * = ( v 2 * , v 3 * ) E * : φ 2 ε , in Ω } ,
for a small real constant ε > 0 ,
C 2 * = v * = ( v 2 * , v 3 * ) E * : 1 γ 2 β + 3 α ( v 3 * ) 2 β 3 ε 1 ,
and
C * = C 1 * C 2 * .
Similarly as done in the previous section, we may prove that C * is a convex set.
Furthermore, for 0 < ε ε 1 1 , we have that J * is convex on C * .
Summarizing, we may define the following convex optimization problem to obtain a critical point of the primal functional J,
Minimize J * ( v 2 * , v 3 * ) subject to v * = ( v 2 * , v 3 * ) C * .
We call J * the Legendre-Galerkin functional associated to J.

12.1. Numerical examples

We have obtained numerical solutions for two one-dimensional examples.
1.
For γ = 1.0 , α = 3.0 , β = 30.0 , f 10 , in Ω = [ 0 , 1 ] .
For the respective solution please see Figure 7.
2.
For γ = 0.01 , α = 3.0 , β = 30.0 , f 10 , in Ω = [ 0 , 1 ] .
For the respective solution please see Figure 8.

13. A general concave dual variational formulation for global optimization

Let Ω R 3 be an open, bounded and connected set a regular (Lipschitzian) boundary denoted by Ω .
Consider a functional J : V R where
J ( u ) = G ( u ) u , f L 2 , u V .
Here V = W 0 1 , 2 ( Ω ) , f L 2 ( Ω ) and we also denote Y = Y * = L 2 ( Ω ) .
Assume there exists α R such that
α = inf u V J ( u ) .
Furthermore, suppose G is three times Fréchet differentiable and there exists K > 0 such that
2 G ( u ) u 2 + K > 0 , u V .
Define now J 1 : V × Y R where,
J 1 ( u , v ) = G 1 ( u , v ) + F ( u ) ,
where
G 1 ( u , v ) = G ( v ) ε 2 Ω v 2 d x + K 2 Ω ( v u ) 2 d x ,
and
F ( u ) = ε 2 Ω u 2 d x u , f L 2 .
Moreover, we define the polar functionals G 1 * : Y * × V R and F * : Y * R , where
G 1 * ( v * , u ) = sup v Y { v , v * L 2 G 1 ( u , v ) } = G K ε * ( v * + K u ) + K 2 Ω u 2 d x ,
G K ε * ( v * + K u ) = sup v Y v , v * L 2 G ( v ) K 2 Ω v 2 d x + ε 2 Ω v 2 d x ,
and
F * ( v * ) = sup u V { u , v * L 2 F ( u ) } = 1 2 ε Ω ( v * f ) 2 d x .
At this point we define the functional J 2 * : Y * × V R by
J 2 * ( v * , u ) = G K ε * ( v * + K u ) + K 2 Ω u 2 d x F * ( v * ) .
With such results in mind we define
V 1 = { u V : u K 3 } ,
and
D * = { v * Y * : v * K 4 } ,
for appropriated real constants K 3 > 0 and K 4 > 0 .
Moreover, we define also the penalized functional J 3 * : Y * × V R where
J 3 * ( v * , u ) = J 2 * ( v * , u ) K 1 2 Ω v * G ( u ) u + ε u 2 d x .
Finally, we remark that for ε > 0 sufficiently small and K 1 > 0 sufficiently large, J 3 * is concave in D * × V 1 around a concerning critical point. We recall that a critical point
v * G ( u ) u + ε u = 0 , in Ω .

14. A related restricted problem in phase transition

In this section we develop a convex (in fact concave) dual variational for a model similar to those found in phase transition problems.
Let Ω = [ 0 , 1 ] R . Consider the functional J : V R where
J ( u ) = 1 2 Ω min { ( u + 1 ) 2 , ( u 1 ) 2 } d x + 1 2 Ω u 2 d x u , f L 2 = 1 2 Ω ( u ) 2 d x Ω | u | d x + 1 / 2 + 1 2 Ω u 2 d x u , f L 2 .
Here
V = { u W 1 , 2 ( Ω ) : u ( 0 ) = 0 and u ( 1 ) = 1 / 2 } .
We also denote V 1 = W 0 1 , 2 ( Ω ) , and Y = Y * = L 2 ( Ω ) .
Furthermore, we define the functionals G and F : V × V 1 R by
G ( u , v ) = 1 2 Ω ( u + v ) 2 d x Ω | u + v | d x + 1 / 2 ,
and
F ( u , v ) = 1 2 Ω u 2 d x u , f L 2 .
Moreover we define J 1 : V × V 1 R by
J 1 ( u , v ) = G ( u , v ) + F ( u , v ) ,
and consider the problem of minimizing J 1 on the set
A = { ( u , v ) V × V 1 : ( v ) 2 K 2 , in Ω } .
Already including the Lagrange multiplier ϕ concerning such restrictions, we define
J 2 ( u , v , ϕ ) = J 1 ( u , v ) + 1 2 ϕ 2 , ( v ) 2 K 2 L 2 .
Observe now that
J 2 ( u , v , ϕ ) = J 1 ( u , v ) + 1 2 ϕ 2 , ( v ) 2 K 2 L 2 = G ( u , v ) + 1 2 ϕ 2 , ( v ) 2 K 2 L 2 + F ( u , v ) = u , v 1 * L 2 v , v 2 * L 2 + G ( u , v ) + 1 2 ϕ 2 , ( v ) 2 K 2 L 2 u , v 1 * L 2 + v , v 2 * L 2 + F ( u , v ) inf ( v 1 , v 2 ) Y × Y v 1 , v 1 * L 2 v 2 , v 2 * L 2 + G 1 ( v 1 , v 2 , ϕ ) + 1 2 ϕ 2 , ( v 2 ) 2 K 2 L 2 + inf ( u , v ) V × V 1 { u , v 1 * L 2 + v , v 2 * L 2 + F ( u , v ) } = G 1 * ( v 1 * , v 2 * , ϕ ) F ˜ * ( v 1 * , v 2 * ) , ( u , v ) V × V 1 , ( v 1 * , v 2 * , ϕ ) [ Y * ] 3 ,
where
G 1 ( u , v , ϕ ) = G ( u , v ) + 1 2 ϕ 2 , ( v ) 2 K 2 L 2 .
Also,
G 1 * ( v 1 * , v 2 * , ϕ ) = sup ( v 1 , v 2 ) Y × Y { v 1 , v 1 * L 2 + v 1 , v 1 * L 2 G 1 ( v 1 , v 2 , ϕ ) } = 1 2 Ω ( v 1 * ) 2 d x + Ω | v 1 * | d x + 1 2 Ω ( v 1 * v 2 * ) 2 ϕ 2 + K 2 2 Ω ϕ 2 d x ,
where
F ˜ * ( v * ) = 1 2 Ω ( ( v 1 * ) + f ) 2 d x v 1 * ( 1 ) u ( 1 ) , if ( v 2 * ) = 0 , in Ω , + , otherwise .
From this we may infer that v 2 * = c , in Ω , for some c R .
Summarizing, denoting v * = ( v 1 * , v 2 * ) = ( v 1 * , c ) , and
J * ( v * , ϕ ) = G 1 * ( v * , ϕ ) F ˜ * ( v * )
we have got
inf ( u , v ) A J 1 ( u , v ) sup ( v * , ϕ ) Y * × R × Y * J * ( v * ϕ ) .
We have developed numerical results by maximizing the dual functional J * for two examples, namely.
1.
Example A: In this case, we consider f ( x ) = cos ( π x ) / 2 , K 2 = 10 4 .
For the optimal
u 0 = ( v 1 * ) + f ,
please see Figure 9.
2.
Example B: In this case, we consider f ( x ) = cos ( π x ) / 2 , K 2 = 30 .
For the optimal
u 0 = ( v 1 * ) + f ,
please see Figure 10.

15. One more dual variational formulation

In this section we develop one more dual variational formulation for a related model.
Let Ω = [ 0 , 1 ] R and consider the functional J : V R defined by
J ( u ) = 1 2 Ω ( ( u ) 2 1 ) 2 d x + 1 2 Ω u 2 d x u , f L 2 ,
where
V = { u W 1 , 4 ( Ω ) : u ( 0 ) = 0 and u ( 1 ) = 1 / 2 } .
We define also the relaxed functional J 1 : V × V 0 R , already including a concerning restriction and corresponding non-negative Lagrange multiplier Λ 2 , where
J 1 ( u , v , Λ ) = 1 2 Ω ( ( u + v ) 2 1 ) 2 d x + 1 2 Ω u 2 d x u , f L 2 + Λ 2 , ( v ) 2 K L 2 .
where
V 0 = { v W 0 1 , 4 ( Ω ) : ( v ) 2 K 0 in Ω } .
Observe that
1 2 Ω ( ( u + v ) 2 1 ) 2 d x + 1 2 Ω u 2 d x u , f L 2 + Λ 2 , ( v ) 2 K L 2 = v 0 * , ( u + v ) 2 1 L 2 + 1 2 Ω ( ( u + v ) 2 1 ) 2 d x + v 0 * , ( u + v ) 2 1 L 2 + Λ 2 , ( v ) 2 K L 2 u , v 1 * L 2 v , v 2 * L 2 + u , v 1 * L 2 + v , v 2 * L 2 + 1 2 Ω u 2 d x u , f L 2 inf w Y v 0 * , w L 2 + 1 2 Ω ( w ) 2 d x inf ( v 1 , v 2 ) Y × Y v 0 * , ( v 1 + v 2 ) 2 1 L 2 + Λ 2 , ( v 2 ) 2 K L 2 v 1 , v 1 * L 2 v 2 , v 2 * L 2 + inf ( u , v ) V × V 0 u , v 1 * L 2 + v , v 2 * L 2 + 1 2 Ω u 2 d x u , f L 2 = 1 2 Ω ( v 0 * ) 2 d x Ω v 0 * d x 1 4 Ω ( v 1 * ) 2 v 0 * d x 1 2 Ω ( v 1 * v 2 * ) 2 2 Λ 2 d x 1 2 Ω ( ( v 1 * ) + f ) 2 d x 1 2 Ω K Λ 2 d x + v 1 * ( 1 ) u ( 1 ) .
Here, we highlight v 2 * = c R in Ω , for some real constant c.
Hence, denoting
J 1 * ( v * , Λ ) = 1 2 Ω ( v 0 * ) 2 d x Ω v 0 * d x 1 4 Ω ( v 1 * ) 2 v 0 * d x 1 2 Ω ( v 1 * v 2 * ) 2 2 Λ 2 d x 1 2 Ω ( ( v 1 * ) + f ) 2 d x 1 2 Ω K Λ 2 d x + v 1 * ( 1 ) u ( 1 )
and
J 2 ( u , v ) = 1 2 Ω ( ( u + v ) 2 1 ) 2 d x + 1 2 Ω u 2 d x u , f L 2 ,
we have obtained
inf ( u , v ) V × V 0 J 2 ( u , v ) } sup ( v * , Λ ) A * × [ Y * ] × R × Y * J 1 * ( v * , Λ ) .
Finally, for
A * = { v 0 * Y * : v 0 * ε in Ω }
we emphasize J 1 * is concave on A * × [ Y * ] × R × Y * .
Here ε > 0 is a small regularizing real constant.
Remark 15.1. 
The constraint ( v ) 2 K 0 , in Ω is included to restrict the action of v on the region where the primal functional is non-convex, through an appropriate constant K > 0 .

16. A duality principle for a related relaxed formulation concerning the vectorial approach in the calculus of variations

In this section we develop a duality principle for a related vectorial model in the calculus of variations.
Let Ω R n be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω = Γ .
For 1 < p < + , consider a functional J : V R where
J ( u ) = G ( u ) + F ( u ) u , f L 2 ,
where
V = u W 1 , p ( Ω ; R N ) : u = u 0 on Ω ,
u 0 C 1 ( Ω ¯ ; R N ) and f L 2 ( Ω ; R N ) .
We assume G : Y R and F : V R are Fréchet differentiable and F is also convex.
Also
G ( u ) = Ω g ( u ) d x ,
where g : R N × n R it is supposed to be Fréchet differentiable. Here we have denoted Y = L p ( Ω ; R N × n ) .
We define also J 1 : V × Y 1 R by
J 1 ( u , ϕ ) = G 1 ( u + y ϕ ) + F ( u ) u , f L 2 ,
where
Y 1 = W 1 , p ( Ω × Ω ; R N )
and
G 1 ( u + y ϕ ) = 1 | Ω | Ω Ω g ( u ( x ) + y ϕ ( x , y ) ) d x d y .
Moreover, we define the relaxed functional J 2 : V R by
J 2 ( u ) = inf ϕ V 0 J 1 ( u , ϕ ) ,
where
V 0 = { ϕ Y 1 : ϕ ( x , y ) = 0 , on Ω × Ω } .
Now observe that
J 1 ( u , ϕ ) = G 1 ( u + y ϕ ) + F ( u ) u , f L 2 = 1 | Ω | Ω Ω v * ( x , y ) · ( u + y ϕ ( x , y ) ) d y d x + G 1 ( u + y ϕ ) + 1 | Ω | Ω Ω v * ( x , y ) · ( u + y ϕ ( x , y ) ) d y d x + F ( u ) u , f L 2 inf v Y 2 1 | Ω | Ω Ω v * ( x , y ) · v ( x , y ) d y d x + G 1 ( v ) + inf ( v , ϕ ) V × V 0 1 | Ω | Ω Ω v * ( x , y ) · ( u + y ϕ ( x , y ) ) d y d x + F ( u ) u , f L 2 = G 1 * ( v * ) F * div x 1 | Ω | Ω v * ( x , y ) d y + f + 1 | Ω | Ω Ω v * ( x , y ) d y n u 0 d Γ ,
( u , ϕ ) V × V 0 , v * A * , where
A * = { v * Y 2 * : div y v * ( x , y ) = 0 , in Ω } .
Here we have denoted
G 1 * ( v * ) = sup v Y 2 1 | Ω | Ω Ω v * ( x , y ) · v ( x , y ) d y d x G 1 ( v ) ,
where Y 2 = L p ( Ω × Ω ; R N × n ) , Y 2 * = L q ( Ω × Ω ; R N × n ) , and where
1 p + 1 q = 1 .
Furthermore, for v * A * , we have
F * div x 1 | Ω | Ω v * ( x , y ) d y + f 1 | Ω | Ω Ω v * ( x , y ) d y n u 0 d Γ = sup ( v , ϕ ) V × V 0 1 | Ω | Ω Ω v * ( x , y ) · ( u + y ϕ ( x , y ) ) d y d x F ( u ) + u , f L 2 ,
Therefore, denoting J 3 * : Y 2 * R by
J 3 * ( v * ) = G 1 * ( v * ) F * div x Ω v * ( x , y ) d y + f + 1 | Ω | Ω Ω v * ( x , y ) d y n u 0 d Γ ,
we have got
inf u V J 2 ( u ) sup v * A * J 3 * ( v * ) .
Finally, we highlight such a dual functional J 3 * is convex (in fact concave).

16.1. An example in finite elasticity

In this section we develop an application of results obtained in the last section to a model in non-linear elasticity.
Let Ω R 3 be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω .
Concerning a standard model in non-linear elasticity, consider a functional J : V R where
J ( u ) = 1 2 Ω H i j k l u i , j + u j , i 2 + 1 2 u m , i u m , j u k , l + u j , i 2 + 1 2 u m , k u m , l d x u i , f i L 2
where f L 2 ( Ω ; R 3 ) and V = W 0 1 , 2 ( Ω ; R 3 ) .
Here { H i j k l } is a fourth-order and positive definite symmetric tensor (in an appropriate standard sense). Moreover, u = ( u 1 , u 2 , u 3 ) V is a field of displacements resulting from the f load field action on the volume comprised by Ω .
At this point, we define the functional J 1 : V × V 1 R , where
J 1 ( u , ϕ ) = 1 2 | Ω | Ω Ω H i j k l u i , j + u j , i 2 + ϕ i , y j + ϕ j , y i 2 1 2 ( u m , i + ϕ m , y i ) ( u m , j + ϕ m , y j ) × u k , l + u l , k 2 + ϕ k , y l + ϕ l , y k 2 + 1 2 ( u m , k + ϕ m , y k ) ( u m , l + ϕ m , y l ) d x d y u i , f i L 2 ,
where
V 1 = { ϕ W 1 , 2 ( Ω × Ω ; R 3 ) : ϕ = 0 on Ω × Ω } .
We define also the quasi-convex envelop of J, denoted by Q J : V R , as
Q J ( u ) = inf ϕ V 1 J 1 ( u , ϕ ) .
It is a well known result from the modern calculus of variations theory that
inf u V J ( u ) = inf u V Q J ( u ) .
Observe now that, denoting Y 1 = Y 1 * = L 2 ( Ω × Ω ; R 9 ) , Y 2 = Y 2 * = L 2 ( Ω × Ω ; R 3 ) , and
G 1 u i , j + u j , i 2 + ϕ i , y j + ϕ j , y i 2 + 1 2 ( u m , i + ϕ m , y i ) ( u m , j + ϕ m , y j ) = 1 2 | Ω | Ω Ω H i j k l u i , j + u j , i 2 + ϕ i , y j + ϕ j , y i 2 + 1 2 ( u m , i + ϕ m , y i ) ( u m , j + ϕ m , y j ) × u k , l + u l , k 2 + ϕ k , y l + ϕ l , y k 2 + 1 2 ( u m , k + ϕ m , y k ) ( u m , l + ϕ m , y l ) d x d y
we have that
J 1 ( u , ϕ ) = G 1 u i , j + u j , i 2 + ϕ i , y j + ϕ j , y i 2 + 1 2 ( u m , i + ϕ m , y i ) ( u m , j + ϕ m , y j ) u i , f i L 2 = 1 | Ω | Ω Ω u i , j + u j , i 2 + ϕ i , y j + ϕ j , y i 2 + 1 2 ( u m , i + ϕ m , y i ) ( u m , j + ϕ m , y j ) σ i j d x d y + G 1 u i , j + u j , i 2 + ϕ i , y j + ϕ j , y i 2 + 1 2 ( u m , i + ϕ m , y i ) ( u m , j + ϕ m , y j ) + 1 | Ω | Ω Ω u i , j + u j , i 2 + ϕ i , y j + ϕ j , y i 2 + 1 2 ( u m , i + ϕ m , y i ) ( u m , j + ϕ m , y j ) σ i j d x d y u i , f i L 2 inf v Y 1 1 | Ω | Ω Ω v i j σ i j d x d y G 1 { v i j } + inf v 2 Y 1 1 | Ω | Ω Ω ( v 2 ) i j Q i j d x d y + 1 | Ω | Ω Ω σ i j 1 2 ( ( v 2 ) m i ( v 2 ) m j ) d x d y + inf ( u , ϕ ) V × V 1 1 | Ω | Ω Ω ( σ i j + Q i j ) u i , j + u j , i 2 + ϕ i , y j + ϕ j , y i 2 d x d y u i , f i L 2 1 2 | Ω | Ω Ω H ¯ i j k l σ i j σ k l d x d y 1 2 | Ω | Ω Ω σ i j ¯ Q m i Q m k d x d y ,
( u , ϕ ) V × V 1 , ( σ , Q ) A * , where A * = A 1 * A 2 * A 3 * ,
A 1 * = { ( σ , Q ) Y 1 * × Y 1 * : σ i j , y j + Q i j , y j = 0 , in Ω × Ω } .
A 2 * = ( σ , Q ) Y 1 * × Y 1 * : 1 | Ω | Ω ( σ i j ) d y x j + 1 | Ω | Ω ( Q i j ) d y x j + f i = 0 , in Ω ,
A 3 * = { ( σ , Q ) Y 1 * × Y 1 * : { σ i j } is positive definite in Ω × Ω } .
Hence, denoting
J * ( σ , Q ) = 1 2 | Ω | Ω Ω H ¯ i j k l σ i j σ k l d x d y 1 2 | Ω | Ω Ω σ i j ¯ Q m i Q m k d x d y ,
we have obtained
inf u V J ( u ) sup ( σ , Q ) A * J * ( σ , Q ) .
Remark 16.1. 
This last dual functional is concave and such a concerning inequality corresponds a duality principle for the relaxed primal formulation.
We emphasize again such results are also extensions and in some sense complement the original duality principles in the works of Telega and Bielski, [2,3,15].
We emphasize such results are extensions and in some sense complement the original duality principles in the works of Telega and Bielski, [2,3,15].
Moreover, if ( σ 0 , Q 0 ) A * is such that
δ J * ( σ 0 , Q 0 ) = 0 ,
it is a well known result from the Legendre transform proprieties that the corresponding ( u 0 , ϕ 0 ) V × V 1 such that
( σ 0 ) i j = H i j k l u k , l + u l , k 2 + ϕ k , y l + ϕ l , y k 2 + 1 2 ( u m , k + ϕ m , y k ) ( u m , l + ϕ m , y l )
and
( Q 0 ) i j = ( σ 0 ) i m ( v 2 0 ) m j ,
is also such that
δ J 1 ( u 0 , ϕ 0 ) = 0
and
J 1 ( u 0 , ϕ 0 ) = J * ( σ 0 , Q 0 ) .
From this and
inf u V J ( u ) = inf ( u , ϕ ) V × V 1 J 1 ( u , ϕ ) sup ( σ , Q ) A * J * ( σ , Q ) ,
we obtain
J 1 ( u 0 , ϕ 0 ) = inf ( u , ϕ ) V × V 1 J 1 ( u , ϕ ) = sup ( σ , Q ) A * J * ( σ , Q ) = J * ( σ 0 , Q 0 ) = inf u V J ( u ) .
Also, from the modern calculus of variations theory, there exists a sequence { u n } V such that
u n u 0 , weakly in V ,
and
J ( u n ) J 1 ( u 0 , ϕ 0 ) = inf u V J ( u ) .
From this and the Ekeland variational principle, there exists { v n } V such that
u n v n V 1 / n ,
J ( v n ) inf u V J ( u ) + 1 / n ,
and
δ J ( v n ) V * 1 / n , n N ,
so that
v n u 0 , weakly in V ,
and
J ( v n ) J 1 ( u 0 , ϕ 0 ) = inf u V J ( u ) .
Assume now we are dealing with a finite dimensional version of such a model, in a finite elements of finite differences context, for example.
In such a case we have
v n u 0 , strongly in R N
for an appropriate N N .
From continuity we obtain
δ J ( v n ) δ J ( u 0 ) = 0 ,
J ( v n ) J ( u 0 ) .
Summarizing, we have got
J ( u 0 ) = inf u V J ( u ) ,
δ J ( u 0 ) = 0 .
Here we highlight such last results are valid just for this finite-dimensional model version.

17. A model in superconductivity through an eigenvalue approach

In this section we intend to model superconductivity through a two phase eigenvalue approach.
Let Ω = [ 0 , 5 ] R be a straight wire corresponding to a one-dimensional super-conducting sample.
Consider the functional J : V × V × R R where
J ( u , v , E ) = γ 1 2 Ω u · u d x + α 1 2 Ω | u | 4 d x ω 2 2 Ω | u | 2 d x + γ 2 2 Ω v · v d x + α 2 2 Ω | v | 4 d x ω 1 2 2 K 3 2 Ω | v | 2 d x E 2 Ω ( | u | 2 + | v | 2 ) d x m T .
Here, in atomic units, m T is the total electronic charge, V = W 0 1 , 2 ( Ω ) and we set α 1 = 10 4 corresponding to higher self-interacting energy which is related to a normal phase. We also set α 2 = 10 1 corresponding to a lower self-interacting energy which is related to a super-conducting phase and respective super-currents.
Moreover, we set γ 1 = γ 2 = 1 , and initially ω = 1.8 which is gradually decreased to ω = 1.0 .
Furthermore, we define
| ϕ N | 2 = | u | 2 | u | 2 + | v | 2
and
| ϕ S | 2 = | v | 2 | u | 2 + | v | 2
where ϕ N corresponds to a normal phase and ϕ S to a super-conducting one.
At this point we observe that the temperature T = T ( x , t ) is proportional the frequency ω / ( 2 π ) of vibration for the normal phase.
We start the process with ω = 1.8 which in atomic units corresponds to a higher temperature and gradually decreases it to the value ω = 1.0
Between ω = 1.2 and ω = 1.0 the system changes from an almost total normal phase to an almost total super-conducting phase, as expected.
We highlight that the temperature is proportional to the vibrational kinetics energy
E 1 ( t ) = 1 2 Ω | u | 2 r N ( x , t ) t · r N ( x , t ) t d x
so that for
r N ( x , t ) = e i ω t w 5 ( x )
and for a suitable vectorial function w 5 , we have
T E 1 ω 2
so that we may model the decreasing of temperature T through the decreasing of ω 2 .
For ω = 1.8 , for the corresponding normal phase ϕ N and super-conducting phase ϕ S , please se Figure 11 and Figure 12, respectively.
For ω = 1.0 , for the corresponding normal phase ϕ N and super-conducting phase ϕ S , please se Figure 13 and Figure 14, respectively.
Finally, we have set ω 1 / K 3 1 which for large ω 1 corresponds to the super-currents.

18. A simplified qualitative many body model for the hydrogen nuclear fusion

In this section we develop a qualitative simple model for the hydrogen nuclear fusion.
Let Ω = [ 0 , L ] 3 R 3 be a box in which is confined a gas comprised by an amount of ionized deuterium and tritium isotopes of hydrogen.
Though a suitable increasing in temperature, we intend to develop the following nuclear reaction
Deuterium + + Tritium + Helium + + + Neutron ( energetic ) .
We recall that the ionized Deuterium atom comprises a proton and a neutron and the ionized Tritium atom comprises a proton and two neutrons.
Under certain conditions and at a suitable high temperature the ionized Deuterium and Tritium atoms react chemically resulting in an ionized Helium atom, comprised by two protons and two neutrons and resulting also in one more single energetic neutron. We emphasize the higher kinetics neutron energy level has many potential practical applications, including its conversion in electric energy.
At this point we denote by m D , m T , m H e and m N the masses of the ionized Deuterium, Tritium and Helium atoms, and the single neutron, respectively.
Therefore, we have the following mass relation
m D + m T = m H e + m N .
To simplify our analysis, in such a chemical reaction, denoting the total masses of ionized Deuterium, Tritium, Helium and single Neutrons by ( m D ) T , ( m T ) T , ( m H e ) T and ( m N ) T we assume there is a real constant c > 0 such that
( m D ) T = c m D , ( m T ) T = c m T , ( m H e ) T = c m H e , ( m N ) T = c m N .
With such statements and definitions in mind, we define the following functional J, where
J ( ϕ , r ) = J ( ϕ D , ϕ T , ϕ H e , ϕ N , r ) = G ( ϕ ) + F ( ϕ ) + E c ( ϕ , r ) ,
where, in a simplified many body context,
| ϕ D ( x , y ) | 2 = | ϕ p D ( y ) | 2 + | ϕ N D ( x , y ) | 2 | ϕ p D ( y ) | 2 1 m p ,
| ϕ T ( x , y ) | 2 = | ϕ p T ( y ) | 2 + ( | ϕ N 1 T ( x , y ) | 2 + | ϕ N 2 T ( x , y ) | 2 ) | ϕ p T ( y ) | 2 1 m p ,
| ϕ H e ( x , y ) | 2 = | ϕ 2 P H e ( y ) | 2 + ( | ϕ N 1 H e ( x , y ) | 2 + | ϕ N 2 H e ( x , y ) | 2 ) | ϕ 2 P H e ( y ) | 2 1 2 m p ,
ϕ N = ϕ N ( x ) .
Here x , y Ω R 3 refers to the particle densities.
Furthermore, we assume γ p D > 0 , γ p T > 0 , γ N D > 0 , γ N 1 T > 0 , γ N 2 T > 0 , γ 2 p H e > 0 , γ N 1 H e > 0 ,   γ N 2 H e > 0 , γ N > 0 , and α D > 0 , α T > 0 , α H e > 0 , α N > 0 , α D T > 0 , α H e N > 0 , so that
G ( ϕ ) = γ p D 2 Ω ( ϕ p D ) · ( ϕ p D ) d y + γ N D 2 Ω ( ϕ N D ) · ( ϕ N D ) d x d y γ p T 2 Ω ( ϕ p T ) · ( ϕ p T ) d y + γ N 1 T 2 Ω ( ϕ N 1 T ) · ( ϕ N 1 T ) d x d y + γ N 2 T 2 Ω ( ϕ N 2 T ) · ( ϕ N 2 T ) d x d y + γ 2 p H e 2 Ω ( ϕ 2 p H e ) · ( ϕ 2 p H e ) d y + γ N 1 H e 2 Ω ( ϕ N 1 H e ) · ( ϕ N 1 H e ) d x d y + γ N 2 H e 2 Ω ( ϕ N 2 H e ) · ( ϕ N 2 H e ) d x d y + γ N 2 Ω ( ϕ N ) · ( ϕ N ) d x ,
and,
F ( ϕ ) = α D 2 Ω | ϕ D ( x ξ 1 , y ξ 2 ) | 2 | ϕ D ( ξ 1 , ξ 2 ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 + α T 2 Ω | ϕ T ( x ξ 1 , y ξ 2 ) | 2 | ϕ T ( ξ 1 , ξ 2 ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 + α D T 2 Ω | ϕ D ( x ξ 1 , y ξ 2 ) | 2 | ϕ T ( ξ 1 , ξ 2 ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 + α H e 2 Ω | ϕ H e ( x ξ 1 , y ξ 2 ) | 2 | ϕ H e ( ξ 1 , ξ 2 ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 + α N 2 0 t f Ω | ϕ N ( x ξ ) | 2 | ϕ N ( ξ ) | 2 | x ξ | d x d ξ + j = 1 2 α H e N 2 Ω | ϕ H e ( x 1 ξ 1 , y ξ 2 ) | 2 | ϕ N ( ξ j ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2
and the kinetics energy is expressed by
E c ( ϕ , r ) = 1 2 Ω | ϕ D | 2 r D t · r D t d x d y + 1 2 Ω | ϕ T | 2 r T t · r T t d x d y + 1 2 Ω | ϕ H e | 2 r H e t · r H e t d x d y + 1 2 Ω | ϕ N | 2 r N t · r N t d x d y ,
where we also assume
r D e i ω t w 5 ( x , y ) ,
r T e i ω t w 6 ( x , y ) ,
so that considering such a vibrational motion, the temperature T is proportional to ω 2 , that is
T ω 2 .
Therefore, an increasing in T corresponds to a proportional increasing in ω 2 .
Summarizing, we have supposed
E c ( ϕ , r ) 1 2 ω 2 Ω | ϕ D | 2 + | ϕ T | 2 d x C 1 + 1 2 ω 1 2 Ω | ϕ N | 2 d x C 2 ,
so that we represent the increasing in T through an increasing in ω 2 .
Moreover, we denote by m N the mass of a single neutron and by m p the mass of a single proton.
Thus, denoting also by λ 1 , λ 2 the proportion of non-reacted and reacted masses respectively, we have the following constraints.
1.
Ω | ϕ N D ( x , y ) | 2 d x = m N ,
2.
Ω | ϕ N 1 T ( x , y ) | 2 d x = m N ,
3.
Ω | ϕ N 2 T ( x , y ) | 2 d x = m N ,
4.
Ω | ϕ N 1 H e ( x , y ) | 2 d x = m N ,
5.
Ω | ϕ N 2 H e ( x , y ) | 2 d x = m N ,
6.
Ω | ϕ p D ( y ) | 2 d y = λ 1 c m p ,
7.
Ω | ϕ p T ( y ) | 2 d y = λ 1 c m p ,
8.
Ω | ϕ 2 P H e ( y ) | 2 d y = λ 2 ( 2 c m p ) ,
Similar constraints are valid corresponding to the charge of a single proton.
We have also the following complementing constraints,
1.
Ω | ϕ D | 2 d x d y = λ 1 ( m D ) T ,
2.
Ω | ϕ T | 2 d x d y = λ 1 ( m T ) T ,
3.
Ω | ϕ H e | 2 d x d y = λ 2 ( m H e ) T ,
4.
Ω | ϕ N | 2 d x d y = λ 2 ( m N ) T ,
5.
λ 1 + λ 2 = 1 .
With such results and statements in mind and simplifying the interacting terms, we re-define the functional J now denoting it by J 1 , here already including the Lagrange multipliers concerning the constraints, where
J 1 ( ϕ , ω , E , λ ) = γ p D 2 Ω ( ϕ p D ) · ( ϕ p D ) d y + γ N D 2 Ω ( ϕ N D ) · ( ϕ N D ) d x d y γ p T 2 Ω ( ϕ p T ) · ( ϕ p T ) d y + γ N 1 T 2 Ω ( ϕ N 1 T ) · ( ϕ N 1 T ) d x d y + γ N 2 T 2 Ω ( ϕ N 2 T ) · ( ϕ N 2 T ) d x d y + γ 2 p H e 2 Ω ( ϕ 2 p H e ) · ( ϕ 2 p H e ) d y + γ N 1 H e 2 Ω ( ϕ N 1 H e ) · ( ϕ N 1 H e ) d x d y + γ N 2 H e 2 Ω ( ϕ N 2 H e ) · ( ϕ N 2 H e ) d x d y + γ N 2 Ω ( ϕ N ) · ( ϕ N ) d x + α D 2 Ω | ϕ D | 4 d x + α T 2 Ω | ϕ T | 4 d x + α H e 2 Ω | ϕ H e | 4 d x + α N 2 Ω | ϕ N | 4 d x ω 2 Ω ( | ϕ D | 2 + | ϕ T | 2 ) d x ω 1 2 Ω | ϕ N | 2 d x + J A u x ,
where the functional J A u x stands for
J A u x = Ω ( E N D ) 5 ( y ) Ω | ϕ N D ( x , y ) | 2 d x m N d y Ω ( E N 1 T ) 6 ( y ) Ω | ϕ N 1 T ( x , y ) | 2 d x m N d y Ω ( E N 2 T ) 7 ( y ) Ω | ϕ N 2 T ( x , y ) | 2 d x m N d y Ω ( E N 1 H e ) 8 ( y ) Ω | ϕ N 1 H e ( x , y ) | 2 d x m N d y Ω ( E N 2 H e ) 9 ( y ) Ω | ϕ N 2 H e ( x , y ) | 2 d x m N d y ( E D ) 2 Ω | ϕ p D ( y ) | 2 d y λ 1 c m p ( E T ) 3 Ω | ϕ p T ( y ) | 2 d y λ 1 c m p ( E H e ) 3 Ω | ϕ 2 P H e ( x , y ) | 2 d y λ 2 2 c m p E 5 Ω | ϕ D | 2 d x d y λ 1 ( m D ) T E 6 Ω | ϕ T | 2 d x d y λ 1 ( m T ) T E 7 Ω | ϕ H e | 2 d x d y λ 2 ( m H e ) T E 8 Ω | ϕ N | 2 d x d y λ 2 ( m N ) T E 9 ( λ 1 + λ 2 1 ) .
Remark 18.1. 
In order to obtain consistent results it is necessary to set
( α N , α H e ) ( α D , α T ) .
In such a case, a higher temperature corresponding to a large ω 2 , though such a nuclear reaction, will result in a small λ 1 and a higher kinetics energy for the neutron field, corresponding to a large ω 1 2 and λ 2 closer to 1.

19. A more detailed mathematical description of the hydrogen nuclear fusion

In this section we develop in more details another model for the hydrogen nuclear fusion.
Let Ω R 3 be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω .
Here such a set Ω stands for a control volume in which an ionized gas (plasma) flows. Such a gas comprises ionized Deuterium and Tritium atoms intended, through a suitable higher temperature, to chemically react resulting in atoms of Hellion and a field of single energetic Neutrons.
Symbolically such a reaction stands for
Deuterium + + Tritium + Helium + + + Neutron ( energetic ) .
We recall that the ionized Deuterium atom is comprised by a proton and a neutron and the ionized Tritium atom is comprised by a proton and two neutrons.
Moreover, the ionized Helium atom is comprised by two protons and two neutrons.
As previously mentioned, resulting from such a chemical reaction up surges also an energetic neutron which the higher kinetics energy has a great variety of applications, including its conversion in electric energy.
We highlight the model here presented includes electric and magnetic fields and the corresponding potential ones.
Denoting by t the time on the interval [ 0 , t f ] , at this point we define the following density functions:
1.
For the Deuterium field
| ϕ D ( x , y , t ) | 2 = | ϕ p D ( y , t ) | 2 + | ϕ N D ( x , y , t ) | 2 | ϕ p D ( y , t ) | 2 1 m p ,
2.
For the Tritium field
| ϕ T ( x , y , t ) | 2 = | ϕ p T ( y , t ) | 2 + ( | ϕ N 1 T ( x , y , t ) | 2 + | ϕ N 2 T ( x , y , t ) | 2 ) | ϕ p T ( y , t ) | 2 1 m p ,
3.
For the Helium field
| ϕ H e ( x , y , t ) | 2 = | ϕ 2 p H e ( y , t ) | 2 + ( | ϕ N 1 H e ( x , y , t ) | 2 + | ϕ N 2 H e ( x , y , t ) | 2 ) | ϕ 2 p H e ( y , t ) | 2 1 2 m p ,
4.
For the Neutron field
ϕ N = ϕ N ( x , t ) ,
5.
For the electronic field resulting from the ionization
ϕ e = ϕ e ( x , y , t ) .
Furthermore, we define also the related densities
1.
ρ D ( y , t ) = Ω | ϕ D ( x , y , t ) | 2 d x ,
2.
ρ T ( y , t ) = Ω | ϕ T ( x , y , t ) | 2 d x ,
ρ H e ( y , t ) = Ω | ϕ H e ( x , y , t ) | 2 d x ,
ρ N ( x , t ) = | ϕ N ( x , t ) | 2 ,
ρ e ( y , t ) = Ω | ϕ e ( x , y , t ) | 2 d x .
For the chemical reaction in question we consider that one unit of mass of fractional proportion α D of ionized Deuterium and α T of ionized Tritium results in one unit of mass of fractional proportion α H e of ionized Helium and α N of neutrons.
Symbolic, this stands for
1 = α D + α T = α H e + α N .
Concerning the control volume Ω in question and related surface control Ω , we assume such a volume has an initial (fot t = 0 ) amount of ionized Deuterium of ( m D ) 0 and an initial amount of ionized Tritium of ( m T ) 0 . The initial amount of ionized Helium and single neutrons are supposed to be zero.
On the other hand, about the surface control Ω , we assume there is a part Ω 1 Ω for which is allowed the entrance and exit of Deuterium and Tritium ionized atoms.
We assume also there is another part Ω 2 Ω such that Ω 1 Ω 2 = for which is allowed only the exit of ionized Helium atoms and neutrons, but not their entrance.
In Ω 2 is allowed the exit only (not the entrance) of ionized Deuterium and Tritium atoms.
Indeed, we assume the following relations for the masses:
1.
( m H e , N ) T ( t ) = m H e , N ( t ) + 0 t Ω 2 ( ρ H e ( x , τ ) + ρ N ( x , τ ) ) u · n d S d τ ,
2.
m H e , N ( t ) = m H e ( t ) + m N ( t ) ,
3.
m H e ( t ) = Ω ρ H e ( x , t ) d x ,
4.
m N ( t ) = Ω ρ N ( x , t ) d x ,
5.
( m H e ) T ( t ) = Ω ρ H e ( x , t ) d x + 0 t Ω 2 ρ H e ( x , τ ) u · n d Γ d τ ,
6.
( m N ) T ( t ) = Ω ρ N ( x , t ) d x + 0 t Ω 2 ρ N ( x , τ ) u · n d Γ d τ ,
7.
( m N ) T ( t ) ( m H e ) T ( t ) = α N α H e ,
so that
α N m H e ) T ( t ) = α H e ( m N ) T ( t ) ,
8.
( m D ) ( t ) = ( m D ) 0 0 t Ω 1 Ω 2 ( ρ D ( x , τ ) ) u · n d S d τ α D ( m H e , N ) T ( t ) ,
9.
( m T ) ( t ) = ( m T ) 0 0 t Ω 1 Ω 2 ( ρ T ( x , τ ) ) u · n d S d τ α T ( m H e , N ) T ( t ) ,
10.
( m e ) T ( t ) = m e ( t ) + 0 t Ω 2 ( ρ e ( x , τ ) ) u · n d S d τ ,
11.
m e ( t ) = Ω ρ e ( x , t ) d x .
12.
m e ( t ) = Ω | ϕ p D ( x , t ) | 2 d x m e m p + Ω | ϕ p T ( x , t ) | 2 d x m e m p + Ω | ϕ 2 p H e ( x , t ) | 2 d x m e m p .
Here n denotes the outward normal vectorial fields to the concerning surfaces.
Having clarified such masses relations, we define the functional
J ( ϕ , ρ , r , u , E , A , B )
where
J = G ( u ) + F ( ϕ ) + E c ( ϕ , r ) + F 1 + F 2 + F 3 ,
and where we assume γ p D > 0 , γ p T > 0 , γ N D > 0 , γ N 1 T > 0 , γ N 2 T > 0 , γ 2 p H e > 0 , γ N 1 H e > 0 ,   γ N 2 H e > 0 , γ N > 0 , γ e > 0 and α D > 0 , α T > 0 , α H e > 0 , α N > 0 , α D T > 0 , α H e N > 0 , α e , e > 0 , α H e , e < 0 so that
G ( ϕ ) = γ p D 2 0 t f Ω ( ϕ p D ) · ( ϕ p D ) d y d t + γ N D 2 0 t f Ω ( ϕ N D ) · ( ϕ N D ) d x d y d t γ p T 2 0 t f Ω ( ϕ p T ) · ( ϕ p T ) d y d t + γ N 1 T 2 0 t f Ω ( ϕ N 1 T ) · ( ϕ N 1 T ) d x d y d t + γ N 2 T 2 0 t f Ω ( ϕ N 2 T ) · ( ϕ N 2 T ) d x d y d t + γ 2 p H e 2 0 t f Ω ( ϕ 2 p H e ) · ( ϕ 2 p H e ) d y d t + γ N 1 H e 2 0 t f Ω ( ϕ N 1 H e ) · ( ϕ N 1 H e ) d x d y d t + γ N 2 H e 2 0 t f Ω ( ϕ N 2 H e ) · ( ϕ N 2 H e ) d x d y d t + γ N 2 0 t f Ω ( ϕ N ) · ( ϕ N ) d x d t + γ e 2 0 t f Ω ( ϕ e ) · ( ϕ e ) d x d y d t ,
and
F ( ϕ ) = α D 2 0 t f Ω | ϕ D ( x ξ 1 , y ξ 2 , t ) | 2 | ϕ D ( ξ 1 , ξ 2 , t ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d t + α T 2 0 t f Ω | ϕ T ( x ξ 1 , y ξ 2 , t ) | 2 | ϕ T ( ξ 1 , ξ 2 , t ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d t + α D T 2 0 t f Ω | ϕ D ( x ξ 1 , y ξ 2 , t ) | 2 | ϕ T ( ξ 1 , ξ 2 , t ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d t + α H e 2 0 t f Ω | ϕ H e ( x ξ 1 , y ξ 2 , t ) | 2 | ϕ H e ( ξ 1 , ξ 2 , t ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d t + α N 2 0 t f Ω | ϕ N ( x ξ , t ) | 2 | ϕ N ( ξ ) | 2 | x ξ , t | d x d ξ d t + j = 1 2 α H e N 2 0 t f Ω | ϕ H e ( x 1 ξ 1 , y ξ 2 , t ) | 2 | ϕ N ( ξ j , t ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d t + α H e , e 2 0 t f Ω | ϕ H e ( x ξ 1 , y ξ 2 , t ) | 2 | ϕ e ( ξ 1 , ξ 2 , t ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d t + α e , e 2 0 t f Ω | ϕ e ( x ξ 1 , y ξ 2 , t ) | 2 | ϕ e ( ξ 1 , ξ 2 , t ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d t
and the internal kinetics energy is expressed by
E c ( ϕ , r ) = 1 2 0 t f Ω | ϕ D | 2 r D t · r D t d x d y d t + 1 2 0 t f Ω | ϕ T | 2 r T t · r T t d x d y d t + 1 2 0 t f Ω | ϕ H e | 2 r H e t · r H e t d x d y d t + 1 2 0 t f Ω | ϕ N | 2 r N t · r N t d x d y d t + 1 2 0 t f Ω | ϕ e | 2 r e t · r e t d x d y d t ,
Here it is worth highlighting we have approximated the initially discrete set of indices s of particles as a continuous positive real variable s.
Moreover,
F 1 = 1 4 π 0 t f curl A B 0 2 d t ,
F 2 = 0 t f Ω E i n d · K p | ϕ p D | 2 u + r D t d x d y d t + 0 t f Ω E i n d · K p | ϕ p T | 2 u + r T t d x d y d t + 0 t f Ω E i n d · K p | ϕ 2 p H e | 2 u + r H e t d x d y d t + 0 t f Ω E i n d · K e | ϕ e | 2 u + r e t d x d y d t ,
where K p and K e are appropriate real constants related to the respective charges.
Here u = ( u 1 , u 2 , u 3 ) is the fluid velocity field and
r D , r T , r H e , r N , r e
are fields of displacements for the corresponding atom fields.
Also A denotes the magnetic potential, B 0 an external magnetic field and B is the total magnetic field.
Moreover, E i n d is an induced electric field.
Finally,
F 3 = C D 2 0 t f Ω ( x , y ) r D · ( x , y ) r D d x d y d t + C T 2 0 t f Ω ( x , y ) r T · ( x , y ) r T d x d y d t C H e 2 0 t f Ω ( x , y ) r H e · ( x , y ) r H e d x d y d t + C N 2 0 t f Ω ( x , y ) r N · ( x , y ) r N d x d y d t C e 2 0 t f Ω ( x , y ) r e · ( x , y ) r e d x d y d t ,
for appropriate real positive constants C D C T , C H e , C N , C e .
Such a functional J is subject to the following constraints:
1.
The momentum conservation equation for the fluid motion
ρ u k t + u j u k x j = ρ f k P x k + τ k j , j + ( F E ) k + ( F M ) k ,
k { 1 , 2 , 3 } .
Here ρ = ρ D + ρ T + ρ H e + ρ N + ρ e is the total density and P is the fluid pressure field.
Furthermore,
τ i j = μ u i x j + u j x i 2 3 δ i j k = 1 3 u k x k ,
i , j { 1 , 2 , 3 } ,
F E = { ( F E ) k } = K p ( | ϕ p D | 2 + | ϕ p T | 2 + | ϕ 2 p H e | 2 ) + K e Ω | ϕ e | 2 d x E ,
and
F M = { ( F M ) k } = K p | ϕ p D | 2 u + r D t | ϕ p T | 2 u + r T t + | ϕ 2 p H e | 2 u + r H e t + K e | ϕ e | 2 u + r e t × B .
(2)
Mass conservation equation:
ρ t + div ( ρ u ) = 0 .
(3)
Energy equation
ρ D e D t + P ( div u ) = Q t div q ,
where we assume the Fourier law
q = K T ,
where T = T ( x , t ) is the scalar field of temperature.
Also,
e = ρ 2 u · u + ρ D 2 r D t · r D t + ρ T 2 r T t · r T t + ρ H e 2 r H e t · r H e t + ρ N 2 r N t · r N t + ρ e 2 r e t · r e t
and
D e D t = e t + u j e x j .
(4)
P = F 7 ( ρ , T ) ,
for an appropriate scalar function F 7 .
(5)
Mass relations
(a)
m D ( t ) = Ω ρ D ( x , t ) d x ,
(b)
m T ( t ) = Ω ρ T ( x , t ) d x ,
(c)
m H e ( t ) = Ω ρ H e ( x , t ) d x ,
(d)
m N ( t ) = Ω ρ N ( x , t ) d x ,
(e)
m e ( t ) = Ω ρ e ( x , t ) d x ,
(f)
( m H e ) T ( t ) = Ω ρ H e ( x , t ) d x + 0 t Ω 2 ρ H e ( x , τ ) u · n d Γ d τ ,
(g)
( m N ) T ( t ) = Ω ρ N ( x , t ) d x + 0 t Ω 2 ρ N ( x , τ ) u · n d Γ d τ ,
(h)
( m N ) T ( t ) ( m H e ) T ( t ) = α N α H e ,
so that
α N m H e ) T ( t ) = α H e ( m N ) T ( t ) ,
where,
(a)
( m H e , N ) T ( t ) = m H e , N ( t ) + 0 t Ω 2 ( ρ H e ( x , τ ) ) u · n d S d τ ,
(b)
m H e , N ( t ) = m H e ( t ) + m N ( t ) ,
(c)
( m D ) ( t ) = ( m D ) 0 0 t Ω 1 Ω 2 ( ρ D ( x , τ ) ) u · n d S d τ α D ( m H e , N ) T ( t ) ,
(d)
( m T ) ( t ) = ( m T ) 0 0 t Ω 1 Ω 2 ( ρ T ( x , τ ) ) u · n d S d τ α T ( m H e , N ) T ( t ) ,
(e)
( m e ) T ( t ) = m e ( t ) + 0 t Ω 2 ( ρ T ( x , τ ) ) u · n d S d τ .
(f)
m e ( t ) = Ω | ϕ p D ( x , t ) | 2 d x m e m p + Ω | ϕ p T ( x , t ) | 2 d x m e m p + Ω | ϕ 2 p H e ( x , t ) | 2 d x m e m p .
(6)
Other mass constraints
(a)
Ω | ϕ N D ( x , y , t ) | 2 d x = m N ,
(b)
Ω | ϕ N 1 T ( x , y , t ) | 2 d x = m N ,
(c)
Ω | ϕ N 2 T ( x , y , t ) | 2 d x = m N ,
(d)
Ω | ϕ N 1 H e ( x , y , t ) | 2 d x = m N ,
(e)
Ω | ϕ N 2 H e ( x , y , t ) | 2 d x = m N .
7.
For the induced electric field, we must have
curl E i n d + 1 c curl K ^ p | ϕ p D | 2 u + r D t + K ^ p | ϕ p T | 2 u + r T t + K ^ p | ϕ 2 p H e | 2 u + r H e t + K ^ e Ω | ϕ e ( x , y , t ) | 2 u ( y , t ) + r e ( x , y , t ) t d x × curl A B 0 1 c t curl A B 0 = 0 ,
where K ^ p and K ^ e are appropriate real constants related to the respective charges.
8.
A Maxwell equation:
div B = 0 ,
where
B = B 0 curl A .
9.
Another Maxwell equation:
div E = 4 π K p ( | ϕ p D | 2 + | ϕ p T | 2 + | ϕ 2 p H e | 2 ) + K e Ω | ϕ e ( x , y , t ) | 2 d x ,
where the total electric field E stands for
E = E i n d + E ρ ,
and where generically denoting
F ( ϕ ) = Ω f 5 ( ϕ , x , ξ ) d x d ξ ,
we have also
E ρ = Ω f 5 ( ϕ , x , ξ ) x k d ξ .
At this point we generically denote
h 1 , h 2 L 2 = 0 t f Ω h 1 h 2 d x d y d t .
Thus, already including the Lagrange multipliers concerning the restrictions indicated, the extended functional J 3 stands for
J 3 = J 3 ( ϕ , u , r , P , A , B , E , Λ , E ) = G ( ϕ ) + F ( ϕ ) + E c ( ϕ , r ) + F 1 + F 2 + F 3 + Λ k , ρ u k t + u j u k x j ρ f k + P x k τ k j , j ( F E ) k ( F M ) k L 2 + Λ 4 , ρ t + div ( ρ u ) L 2 + J A u x 1 + J A u x 2 + J A u x 3 + J A u x 4 ,
where,
J A u x 1 = Λ 5 , ρ D e D t + P ( div u ) Q t + div q L 2 + Λ 6 , P F 7 ( ρ , T ) L 2 ,
J A u x 2 = Λ 7 , m D ( t ) Ω ρ D ( x , t ) d x L 2 + Λ 8 , m T ( t ) Ω ρ T ( x , t ) d x L 2 Λ 9 , m H e ( t ) Ω ρ H e ( x , t ) d x L 2 Λ 10 , m N ( t ) Ω ρ N ( x , t ) d x L 2 Λ 11 , m e ( t ) Ω ρ e ( x , t ) d x L 2 0 t f E 1 2 ( t ) ( α N m H e ) T ( t ) α H e ( m N ) T ( t ) ) d t ,
J A u x 3 = 0 t f Ω ( E N D ) 5 ( y , t ) Ω | ϕ N D ( x , y , t ) | 2 d x m N d y d t 0 t f Ω ( E N 1 T ) 6 ( y , t ) Ω | ϕ N 1 T ( x , y , t ) | 2 d x m N d y d t 0 t f Ω ( E N 2 T ) 7 ( y , t ) Ω | ϕ N 2 T ( x , y , t ) | 2 d x m N d y d t 0 t f Ω ( E N 1 H e ) 8 ( y , t ) Ω | ϕ N 1 H e ( x , y , t ) | 2 d x m N d y d t 0 t f Ω ( E N 2 H e ) 9 ( y , t ) Ω | ϕ N 2 H e ( x , y , t ) | 2 d x m N d y d t ,
J A u x 4 = Λ 12 , curl E i n d + 1 c curl K ^ p | ϕ p D | 2 u + r D t + K ^ p | ϕ p T | 2 u + r T t + K ^ p | ϕ 2 p H e | 2 u + r H e t + K ^ e Ω | ϕ e ( x , y , t ) | 2 u ( y , t ) + r e ( x , y , t ) t d x × curl A B 0 1 c t curl A B 0 L 2 + Λ 13 , div B L 2 + Λ 14 , div E 4 π K p ( | ϕ p D | 2 + | ϕ p T | 2 + | ϕ 2 p H e | 2 ) + K e Ω | ϕ e ( x , y , t ) | 2 d x L 2 .
Here we recall the following definitions and relations:
1.
For the Deuterium field
| ϕ D ( x , y , t ) | 2 = | ϕ p D ( y , t ) | 2 + | ϕ N D ( x , y , t ) | 2 | ϕ p D ( y , t ) | 2 1 m p ,
2.
For the Tritium field
| ϕ D ( x , y , t ) | 2 = | ϕ p D ( y , t ) | 2 + ( | ϕ N 1 D ( x , y , t ) | 2 + | ϕ N 2 D ( x , y , t ) | 2 ) | ϕ p D ( y , t ) | 2 1 m p ,
3.
For the Helium field
| ϕ H e ( x , y , t ) | 2 = | ϕ 2 p H e ( y , t ) | 2 + ( | ϕ N 1 H e ( x , y , t ) | 2 + | ϕ N 2 H e ( x , y , t ) | 2 ) | ϕ 2 p H e ( y , t ) | 2 1 2 m p ,
4.
For the Neutron field
ϕ N = ϕ N ( x , t ) ,
5.
For the electronic field resulting from the ionization
ϕ e = ϕ e ( x , y , t ) .
1.
ρ D ( y , t ) = Ω | ϕ D ( x , y , t ) | 2 d x ,
2.
ρ T ( y , t ) = Ω | ϕ T ( x , y , t ) | 2 d x ,
ρ H e ( y , t ) = Ω | ϕ H e ( x , y , t ) | 2 d x ,
ρ N ( x , t ) = | ϕ N ( x , t ) | 2 ,
ρ e ( y , t ) = Ω | ϕ e ( x , y , t ) | 2 d x .
Also,
ρ = ρ D + ρ T + ρ H e + ρ N + ρ e ,
1.
( m H e , N ) T ( t ) = m H e , N ( t ) + 0 t Ω 2 ( ρ H e ( x , τ ) + ρ N ( x , τ ) ) u · n d S d τ ,
2.
m H e , N ( t ) = m H e ( t ) + m N ( t ) ,
3.
m H e ( t ) = Ω ρ H e ( x , t ) d x ,
4.
m N ( t ) = Ω ρ N ( x , t ) d x ,
5.
( m D ) ( t ) = ( m D ) 0 0 t Ω 1 Ω 2 ( ρ D ( x , τ ) ) u · n d S d τ α D ( m H e , N ) T ( t ) ,
6.
( m T ) ( t ) = ( m T ) 0 0 t Ω 1 Ω 2 ( ρ T ( x , τ ) ) u · n d S d τ α T ( m H e , N ) T ( t ) ,
7.
( m H e ) T ( t ) = Ω ρ H e ( x , t ) d x + 0 t Ω 2 ρ H e ( x , τ ) u · n d Γ d τ ,
8.
( m N ) T ( t ) = Ω ρ N ( x , t ) d x + 0 t Ω 2 ρ N ( x , τ ) u · n d Γ d τ ,
9.
( m N ) T ( t ) ( m H e ) T ( t ) = α N α H e ,
so that
α N m H e ) T ( t ) = α H e ( m N ) T ( t ) ,
10.
( m e ) T ( t ) = m e ( t ) 0 t Ω 2 ( ρ e ( x , τ ) ) u · n d S d τ ,
11.
m e ( t ) = Ω ρ e ( x , t ) d x .
12.
m e ( t ) = Ω | ϕ p D ( x , t ) | 2 d x m e m p + Ω | ϕ p T ( x , t ) | 2 d x m e m p + Ω | ϕ 2 p H e ( x , t ) | 2 d x m e m p .
Finally,
E = E i n d + E ρ ,
and where generically denoting
F ( ϕ ) = Ω f 5 ( ϕ , x , ξ ) d x d ξ ,
we have also
E ρ = Ω f 5 ( ϕ , x , ξ ) x k d ξ .
and,
B = B 0 curl A .

20. A final mathematical description of the hydrogen nuclear fusion

In this section we develop in even more details another model for the hydrogen nuclear fusion.
Let Ω R 3 be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω .
Here such a set Ω stands for a control volume in which an ionized gas (plasma) flows. Such a gas comprises ionized Deuterium and Tritium atoms intended, through a suitable higher temperature, to chemically react resulting in atoms of Helium and a field of single energetic Neutrons.
Symbolically such a reaction stands for
Deuterium + + Tritium + Helium + + + Neutron ( energetic ) .
We recall that the ionized Deuterium atom is comprised by a proton and a neutron and the ionized Tritium atom is comprised by a proton and two neutrons.
Moreover, the ionized Helium atom is comprised by two protons and two neutrons.
As previously mentioned, resulting from such a chemical reaction up surges also an energetic neutron which the higher kinetics energy has a great variety of applications, including its conversion in electric energy.
We highlight the model here presented includes electric and magnetic fields and the corresponding potential ones.
Denoting by t the time on the interval [ 0 , t f ] , at this point we define the following density functions:
1.
For a single Deuterium atom indexed by s:
| ϕ D ( x , y , t , s ) | 2 = | ϕ p D ( y , t , s ) | 2 + | ϕ N D ( x , y , t , s ) | 2 | ϕ p D ( y , t , s ) | 2 1 m p ,
2.
For a single Tritium atom indexed by s:
| ϕ T ( x , y , t , s ) | 2 = | ϕ p T ( y , t , s ) | 2 + ( | ϕ N 1 T ( x , y , t , s ) | 2 + | ϕ N 2 T ( x , y , t , s ) | 2 ) | ϕ p T ( y , t , s ) | 2 1 m p ,
3.
For a single Helium atom indexed by s:
| ϕ H e ( x , y , t , s ) | 2 = | ϕ 2 p H e ( y , t , s ) | 2 + ( | ϕ N 1 H e ( x , y , t , s ) | 2 + | ϕ N 2 H e ( x , y , t , s ) | 2 ) | ϕ 2 p H e ( y , t , s ) | 2 1 2 m p ,
4.
For the Neutron field:
ϕ N = ϕ N ( x , t , s ) ,
5.
For the electronic field resulting from the ionization
ϕ e = ϕ e ( x , y , t , s ) .
Furthermore, we define also the related densities
1.
ρ D ( y , t ) = 0 N D ( t ) Ω | ϕ D ( x , y , t , s ) | 2 d x d s ,
2.
ρ T ( y , t ) = 0 N T ( t ) Ω | ϕ T ( x , y , t , s ) | 2 d x d s ,
ρ H e ( y , t ) = 0 N H e ( t ) Ω | ϕ H e ( x , y , t , s ) | 2 d x d s ,
ρ N ( x , t ) = 0 N N ( t ) | ϕ N ( x , t , s ) | 2 d s ,
ρ e ( y , t ) = 0 N e ( t ) Ω | ϕ e ( x , y , t , s ) | 2 d x d s .
For the chemical reaction in question we consider that one unit of mass of fractional proportion α D of ionized Deuterium and α T of ionized Tritium results in one unit of mass of fractional proportion α H e of ionized Helium and α N of neutrons.
Symbolically, this stands for
1 = α D + α T = α H e + α N .
Concerning the control volume Ω in question and related surface control Ω , we assume such a volume has an initial (fot t = 0 ) amount of ionized Deuterium of ( m D ) 0 and an initial amount of ionized Tritium of ( m T ) 0 . The initial amount of ionized Helium and single neutrons are supposed to be zero.
On the other hand, about the surface control Ω , we assume there is a part Ω 1 Ω for which is allowed the entrance and exit of Deuterium and Tritium ionized atoms.
We assume also there is another part Ω 2 Ω such that Ω 1 Ω 2 = for which is allowed only the exit of ionized Helium atoms and neutrons, but not their entrance.
In Ω 2 is allowed the exit only (not the entrance) of ionized Deuterium and Tritium atoms.
Indeed, we assume the following relations for the masses:
1.
( m H e , N ) T ( t ) = m H e , N ( t ) + 0 t Ω 2 ( ρ H e ( x , τ ) + ρ N ( x , τ ) ) u · n d S d τ ,
2.
m H e , N ( t ) = m H e ( t ) + m N ( t ) ,
3.
m H e ( t ) = Ω ρ H e ( x , t ) d x ,
4.
m N ( t ) = Ω ρ N ( x , t ) d x ,
5.
( m D ) ( t ) = ( m D ) 0 0 t Ω 1 Ω 2 ( ρ D ( x , τ ) ) u · n d S d τ α D ( m H e , N ) T ( t ) ,
6.
( m T ) ( t ) = ( m T ) 0 0 t Ω 1 Ω 2 ( ρ T ( x , τ ) ) u · n d S d τ α T ( m H e , N ) T ( t ) ,
7.
( m H e ) T ( t ) = Ω ρ H e ( x , t ) d x + 0 t Ω 2 ρ H e ( x , τ ) u · n d Γ d τ ,
8.
( m N ) T ( t ) = Ω ρ N ( x , t ) d x + 0 t Ω 2 ρ N ( x , τ ) u · n d Γ d τ ,
9.
( m N ) T ( t ) ( m H e ) T ( t ) = α N α H e ,
so that
α N m H e ) T ( t ) = α H e ( m N ) T ( t ) ,
10.
( m e ) T ( t ) = m e ( t ) + 0 t Ω 2 ( ρ e ( x , τ ) ) u · n d S d τ ,
11.
m e ( t ) = Ω ρ e ( x , t ) d x .
12.
m e ( t ) = 0 N D ( t ) Ω | ϕ p D ( y , t , s ) | 2 d y d s m e m p + 0 N T ( t ) Ω | ϕ p T ( y , t , s ) | 2 d y d s m e m p + 0 N p ( t ) Ω | ϕ 2 p H e ( y , t , s ) | 2 d y d s m e m p .
Here n denotes the outward normal vectorial fields to the concerning surfaces.
Having clarified such masses relations, denoting by N D ( t ) N T ( t ) , N H e ( t ) , N N ( t ) , N e ( t ) the respective indexed number of particles at time t, we define the functional
J ( ϕ , ρ , r , u , E , A , B , { N D , N T , N H e , N N , N e } )
where
J = G ( u ) + F ( ϕ ) + E c ( ϕ , r ) + F 1 + F 2 + F 3 + F 4 ,
and where we assume γ p D > 0 , γ p T > 0 , γ N D > 0 , γ N 1 T > 0 , γ N 2 T > 0 , γ 2 p H e > 0 , γ N 1 H e > 0 ,   γ N 2 H e > 0 , γ N > 0 , γ e > 0 and α D > 0 , α T > 0 , α H e > 0 , α N > 0 , α D T > 0 , α H e N > 0 , α e , e > 0 , α H e , e < 0 so that
G ( ϕ ) = γ p D 2 0 t f 0 N D ( t ) Ω ( ϕ p D ) · ( ϕ p D ) d y d s d t + γ N D 2 0 t f 0 N D ( t ) Ω ( ϕ N D ) · ( ϕ N D ) d x d y d s d t γ p T 2 0 t f 0 N T ( t ) Ω ( ϕ p T ) · ( ϕ p T ) d y d s d t + γ N 1 T 2 0 t f 0 N T ( t ) Ω ( ϕ N 1 T ) · ( ϕ N 1 T ) d x d y d s d t + γ N 2 T 2 0 t f 0 N T ( t ) Ω ( ϕ N 2 T ) · ( ϕ N 2 T ) d x d y d s d t + γ 2 p H e 2 0 t f 0 N H e ( t ) Ω ( ϕ 2 p H e ) · ( ϕ 2 p H e ) d y d s d t + γ N 1 H e 2 0 t f 0 N H e ( t ) Ω ( ϕ N 1 H e ) · ( ϕ N 1 H e ) d x d y d s d t + γ N 2 H e 2 0 t f 0 N H e ( t ) Ω ( ϕ N 2 H e ) · ( ϕ N 2 H e ) d x d y d s d t + γ N 2 0 t f 0 N N ( t ) Ω ( ϕ N ) · ( ϕ N ) d x d s d t + γ e 2 0 t f 0 N e ( t ) Ω ( ϕ e ) · ( ϕ e ) d x d y d s d t ,
and
F ( ϕ ) = α D 2 0 t f 0 N D ( t ) 0 N D ( t ) Ω | ϕ D ( x ξ 1 , y ξ 2 , t , s s 1 ) | 2 | ϕ D ( ξ 1 , ξ 2 , t , s 1 ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d s d s 1 d t + α T 2 0 t f 0 N T ( t ) 0 N T ( t ) Ω | ϕ T ( x ξ 1 , y ξ 2 , t , s s 1 ) | 2 | ϕ T ( ξ 1 , ξ 2 , t , s 1 ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d s d s 1 d t + α D T 2 0 t f 0 N D ( t ) 0 N T ( t ) Ω | ϕ D ( x ξ 1 , y ξ 2 , t , s s 1 ) | 2 | ϕ T ( ξ 1 , ξ 2 , t , s 1 ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d t + α H e 2 0 t f 0 N H e ( t ) 0 N H e ( t ) Ω | ϕ H e ( x ξ 1 , y ξ 2 , t , s s 1 ) | 2 | ϕ H e ( ξ 1 , ξ 2 , t ) | 2 | ( x , y ) ( ξ 1 , ξ 2 , s 1 ) | d x d y d ξ 1 d ξ 2 d s d s 1 d t + α N 2 0 t f 0 N N ( t ) 0 N N ( t ) Ω | ϕ N ( x ξ , t , s s 1 ) | 2 | ϕ N ( ξ , t , s 1 ) | 2 | x ξ | d x d ξ d s d s 1 d t + j = 1 2 α H e N 2 0 t f 0 N H e ( t ) 0 N D ( t ) Ω | ϕ H e ( x 1 ξ 1 , y ξ 2 , t ) | 2 | ϕ N ( ξ j , t ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d s d s 1 d t + α H e , e 2 0 t f 0 N H e ( t ) 0 N e ( t ) Ω | ϕ H e ( x ξ 1 , y ξ 2 , t , s s 1 ) | 2 | ϕ e ( ξ 1 , ξ 2 , t , s 1 ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d s d s 1 d t + α e , e 2 0 t f 0 N e ( t ) 0 N e ( t ) Ω | ϕ e ( x ξ 1 , y ξ 2 , t , s s 1 ) | 2 | ϕ e ( ξ 1 , ξ 2 , t , s 1 ) | 2 | ( x , y ) ( ξ 1 , ξ 2 ) | d x d y d ξ 1 d ξ 2 d s d s 1 d t
and the internal kinetics energy is expressed by
E c ( ϕ , r ) = 1 2 0 t f 0 N D ( t ) Ω | ϕ D | 2 r D t · r D t d x d y d s d t + 1 2 0 t f 0 N T ( t ) Ω | ϕ T | 2 r T t · r T t d x d y d s d t + 1 2 0 t f 0 N H e ( t ) Ω | ϕ H e | 2 r H e t · r H e t d x d y d s d t + 1 2 0 t f 0 N N ( t ) Ω | ϕ N | 2 r N t · r N t d x d y d s d t + 1 2 0 t f 0 N e ( t ) Ω | ϕ e | 2 r e t · r e t d x d y d s d t ,
Moreover,
F 1 = 1 4 π 0 t f curl A B 0 2 d t ,
F 2 = 0 t f 0 N D ( t ) Ω E i n d · K p | ϕ p D | 2 u + r D t d x d y d s d t + 0 t f 0 N T ( t ) Ω E i n d · K p | ϕ p T | 2 u + r T t d x d y d s d t + 0 t f 0 N H e ( t ) Ω E i n d · K p | ϕ 2 p H e | 2 u + r H e t d x d y d s d t + 0 t f 0 N e ( t ) Ω E i n d · K e | ϕ e | 2 u + r e t d x d y d s d t ,
where K p and K e are appropriate real constants related to the respective charges.
Here u = ( u 1 , u 2 , u 3 ) is the fluid velocity field and
r D , r T , r H e , r N , r e
are fields of displacements for the corresponding particle fields.
Also A denotes the magnetic potential, B 0 an external magnetic field and B is the total magnetic field.
Moreover, E i n d is an induced electric field.
Also,
F 3 = C D 2 0 t f 0 N D ( t ) Ω ( x , y ) r D · ( x , y ) r D d x d y d s d t + C T 2 0 t f 0 N T ( t ) Ω ( x , y ) r T · ( x , y ) r T d x d y d s d t + C H e 2 0 t f 0 N H e ( t ) Ω ( x , y ) r H e · ( x , y ) r H e d x d y d s d t + C N 2 0 t f 0 N N ( t ) Ω ( x , y ) r N · ( x , y ) r N d x d y d s d t C e 2 0 t f 0 N e ( t ) Ω ( x , y ) r e · ( x , y ) r e d x d y d s d t ,
for appropriate real positive constants C D C T , C H e , C N , C e .
Finally,
F 4 = ε D 2 0 t f N D ( t ) t 2 d t + ε T 2 0 t f N D ( t ) t 2 d t + ε N 2 0 t f N N ( t ) t 2 d t + ε H e 2 0 t f N H e ( t ) t 2 d t + ε e 2 0 t f N e ( t ) t 2 d t ,
where ε D , ε T , ε N , ε H e , ε e are small real positive constants.
Such a functional J is subject to the following constraints:
1.
The momentum conservation equation for the fluid motion
ρ u k t + u j u k x j = ρ f k P x k + τ k j , j + ( F E ) k + ( F M ) k ,
k { 1 , 2 , 3 } .
Here ρ = ρ D + ρ T + ρ H e + ρ N + ρ e is the total density and P is the fluid pressure field.
Furthermore,
τ i j = μ u i x j + u j x i 2 3 δ i j k = 1 3 u k x k ,
i , j { 1 , 2 , 3 } ,
F E = { ( F E ) k } = K p 0 N D ( t ) | ϕ p D | 2 d s + 0 N T ( t ) | ϕ p T | 2 d s + 0 N H e ( t ) | ϕ 2 p H e | 2 d s + K e 0 N e ( t ) | ϕ e | 2 d s E ,
and
F M = { ( F M ) k } = K p 0 N D ( t ) | ϕ p D | 2 u + r D t d s 0 N T ( t ) | ϕ p T | 2 u + r T t d s + 0 N H e ( t ) | ϕ 2 p H e | 2 u + r H e t d s + K e 0 N e ( t ) | ϕ e | 2 u + r e t d s × B .
2.
Mass conservation equation:
ρ t + div ( ρ u ) = 0 .
3.
Energy equation
ρ D e D t + P ( div u ) = Q t div q ,
where we assume the Fourier law
q = K T ,
where T = T ( x , t ) is the scalar field of temperature.
Also,
e = ρ 2 u · u + ρ D 2 r D t · r D t + ρ T 2 r T t · r T t + ρ H e 2 r H e t · r H e t + ρ N 2 r N t · r N t + ρ e 2 r e t · r e t
and
D e D t = e t + u j e x j .
4.
P = F 7 ( ρ , T ) ,
for an appropriate scalar function F 7 .
5.
Mass relations
(a)
m D ( t ) = Ω ρ D ( x , t ) d x ,
(b)
m T ( t ) = Ω ρ T ( x , t ) d x ,
(c)
m H e ( t ) = Ω ρ H e ( x , t ) d x ,
(d)
m N ( t ) = Ω ρ N ( x , t ) d x ,
(e)
m e ( t ) = Ω ρ e ( x , t ) d x ,
where,
(a)
( m H e , N ) T ( t ) = m H e , N ( t ) + 0 t Ω 2 ( ρ H e ( x , τ ) ) u · n d S d τ ,
(b)
m H e , N ( t ) = m H e ( t ) + m N ( t ) ,
(c)
( m D ) ( t ) = ( m D ) 0 0 t Ω 1 Ω 2 ( ρ D ( x , τ ) ) u · n d S d τ α D ( m H e , N ) T ( t ) ,
(d)
( m T ) ( t ) = ( m T ) 0 0 t Ω 1 Ω 2 ( ρ T ( x , τ ) ) u · n d S d τ α T ( m H e , N ) T ( t ) ,
(e)
( m H e ) T ( t ) = Ω ρ H e ( x , t ) d x + 0 t Ω 2 ρ H e ( x , τ ) u · n d Γ d τ ,
(f)
( m N ) T ( t ) = Ω ρ N ( x , t ) d x + 0 t Ω 2 ρ N ( x , τ ) u · n d Γ d τ ,
(g)
( m N ) T ( t ) ( m H e ) T ( t ) = α N α H e ,
so that
α N m H e ) T ( t ) = α H e ( m N ) T ( t ) ,
(h)
( m e ) T ( t ) = m e ( t ) + 0 t Ω 2 ( ρ T ( x , τ ) ) u · n d S d τ .
(i)
m e ( t ) = 0 N D ( t ) Ω | ϕ p D ( y , t , s ) | 2 d y d y d s m e m p + 0 N T ( t ) Ω | ϕ p T ( y , t , s ) | 2 d y d s m e m p + 0 N p ( t ) Ω | ϕ 2 p H e ( y , t , s ) | 2 d y d s m e m p .
6.
Other mass constraints
(a)
Ω | ϕ N D ( x , y , t , s ) | 2 d x = m N ,
(b)
Ω | ϕ N 1 T ( x , y , t , s ) | 2 d x = m N ,
(c)
Ω | ϕ N 2 T ( x , y , t , s ) | 2 d x = m N ,
(d)
Ω | ϕ N 1 H e ( x , y , t , s ) | 2 d x = m N ,
(e)
Ω | ϕ N 2 H e ( x , y , t , s ) | 2 d x = m N ,
(f)
Ω | ϕ p D ( x , t , s ) | 2 d x = m p ,
(g)
Ω | ϕ p T ( x , t , s ) | 2 d x = m p ,
(h)
Ω | ϕ 2 p H e ( x , t , s ) | 2 d x = 2 m p ,
7.
m D ( t ) = m p N D ( t ) + m N N D ( t )
m T ( t ) = m p N T ( t ) + m N N T ( t ) ,
m H e ( t ) = 2 m p N H e ( t ) + 2 m N N H e ( t ) ,
m e ( t ) = m e N D ( t ) + m e N T ( t ) + 2 m e N H e ( t ) .
8.
For the induced electric field, we must have
curl E i n d + 1 c curl K ^ p 0 N D ( t ) | ϕ p D | 2 u + r D t d s + K ^ p 0 N T ( t ) | ϕ p T | 2 u + r T t d s + K ^ p 0 N H e ( t ) | ϕ 2 p H e | 2 u + r H e t d s + K ^ e 0 N e ( t ) Ω | ϕ e ( x , y , t , s ) | 2 u ( y , t ) + r e ( x , y , t ) t d x d s × curl A B 0 1 c t curl A B 0 = 0 ,
where K ^ p and K ^ e are appropriate real constants related to the respective charges.
9.
A Maxwell equation:
div B = 0 ,
where
B = B 0 curl A .
10.
Another Maxwell equation:
div E = 4 π K p 0 N D ( t ) | ϕ p D | 2 d s + 0 N T ( t ) | ϕ p T | 2 d s + 0 N H e ( t ) | ϕ 2 p H e | 2 d s + K e 0 N e ( t ) Ω | ϕ e ( x , y , t , s ) | 2 d x d s ,
where the total electric field E stands for
E = E i n d + E ρ ,
and where generically denoting
F ( ϕ ) = Ω f 5 ( ϕ , x , t ξ , s ) d x d ξ d s ,
we have also
E ρ = Ω f 5 ( ϕ , x , t , ξ , s ) x k d ξ d s .
At this point we generically denote
h 1 , h 2 L 2 = 0 t f Ω h 1 h 2 d x d y d t .
Thus, already including the Lagrange multipliers concerning the restrictions indicated, the extended functional J 3 stands for
J 3 = J 3 ( ϕ , u , r , P , A , B , E , Λ , E , { N D , N T , N H e , N N , N e } ) = G ( ϕ ) + F ( ϕ ) + E c ( ϕ , r ) + F 1 + F 2 + F 3 + F 4 + Λ k , ρ u k t + u j u k x j ρ f k + P x k τ k j , j ( F E ) k ( F M ) k L 2 + Λ 4 , ρ t + div ( ρ u ) L 2 + J A u x 1 + J A u x 2 + J A u x 3 + J A u x 4 + J A u x 5 ,
where,
J A u x 1 = Λ 5 , ρ D e D t + P ( div u ) Q t + div q L 2 + Λ 6 , P F 7 ( ρ , T ) L 2 ,
J A u x 2 = Λ 7 , m D ( t ) Ω ρ D ( x , t ) d x L 2 + Λ 8 , m T ( t ) Ω ρ T ( x , t ) d x L 2 Λ 9 , m H e ( t ) Ω ρ H e ( x , t ) d x L 2 Λ 10 , m N ( t ) Ω ρ N ( x , t ) d x L 2 Λ 11 , m e ( t ) Ω ρ e ( x , t ) d x L 2 0 t f E 12 ( t ) ( α N m H e ) T ( t ) α H e ( m N ) T ( t ) ) d t ,
J A u x 3 = 0 t f Ω ( E N D ) 5 ( y , t , s ) Ω | ϕ N D ( x , y , t , s ) | 2 d x m N d y d t 0 t f Ω ( E N 1 T ) 6 ( y , t , s ) Ω | ϕ N 1 T ( x , y , t , s ) | 2 d x m N d y d t 0 t f Ω ( E N 2 T ) 7 ( y , t , s ) Ω | ϕ N 2 T ( x , y , t , s ) | 2 d x m N d y d t 0 t f Ω ( E N 1 H e ) 8 ( y , t , s ) Ω | ϕ N 1 H e ( x , y , t , s ) | 2 d x m N d y d t 0 t f Ω ( E N 2 H e ) 9 ( y , t , s ) Ω | ϕ N 2 H e ( x , y , t , s ) | 2 d x m N d y d t , 0 t f Ω ( E p D ) ( t , s ) Ω | ϕ p D ( y , t , s ) | 2 d y m p d s d t , 0 t f Ω ( E p T ) ( t , s ) Ω | ϕ p T ( y , t , s ) | 2 d y m p d s d t , 0 t f Ω ( E 2 p H e ) ( t , s ) Ω | ϕ 2 p H e ( y , t , s ) | 2 d y 2 m p d s d t ,
J A u x 4 = Λ 12 , curl E i n d + 1 c curl K ^ p 0 N D ( t ) | ϕ p D | 2 u + r D t d s + K ^ p 0 N T ( t ) | ϕ p T | 2 u + r T t d s + K ^ p 0 N H e ( t ) | ϕ 2 p H e | 2 u + r H e t d s + K ^ e 0 N e ( t ) Ω | ϕ e ( x , y , t , s ) | 2 u ( y , t ) + r e ( x , y , t , s ) t d x d s × curl A B 0 1 c t curl A B 0 L 2 + Λ 13 , div B L 2 + Λ 14 , div E 4 π K p 0 N D ( t ) | ϕ p D | 2 d s + 0 N T ( t ) | ϕ p T | 2 d s + 0 N H e ( t ) | ϕ 2 p H e | 2 d s + K e Ω | ϕ e | 2 d x d s L 2 .
J A u x 5 = Λ 15 , m D ( t ) ( m p N D ( t ) + m N N D ( t ) ) L 2 + Λ 16 , m T ( t ) ( m p N T ( t ) + m N N T ( t ) ) L 2 + Λ 17 , m H e ( t ) ( 2 m p N H e ( t ) + 2 m N N H e ( t ) ) L 2 + Λ 18 , m e ( t ) ( m e N D ( t ) + m e N T ( t ) + 2 m e N H e ( t ) ) L 2 .
Here we recall the following definitions and relations:
1.
For the Deuterium field
| ϕ D ( x , y , t , s ) | 2 = | ϕ p D ( y , t , s ) | 2 + | ϕ N D ( x , y , t , s ) | 2 | ϕ p D ( y , t , s ) | 2 1 m p ,
2.
For the Tritium field
| ϕ T ( x , y , t , s ) | 2 = | ϕ p T ( y , t , s ) | 2 + ( | ϕ N 1 T ( x , y , t , s ) | 2 + | ϕ N 2 T ( x , y , t , s ) | 2 ) | ϕ p D ( y , t , s ) | 2 1 m p ,
3.
For the Helium field
| ϕ H e ( x , y , t , s ) | 2 = | ϕ 2 p H e ( y , t , s ) | 2 + ( | ϕ N 1 H e ( x , y , t , s ) | 2 + | ϕ N 2 H e ( x , y , t , s ) | 2 ) | ϕ 2 p H e ( y , t , s ) | 2 1 2 m p ,
4.
For the Neutron field
ϕ N = ϕ N ( x , t , s ) ,
5.
For the electronic field resulting from the ionization
ϕ e = ϕ e ( x , y , t , s ) .
1.
ρ D ( y , t ) = 0 N D ( t ) Ω | ϕ D ( x , y , t , s ) | 2 d x d s ,
2.
ρ T ( y , t ) = 0 N T ( t ) Ω | ϕ T ( x , y , t , s ) | 2 d x d s ,
ρ H e ( y , t ) = 0 N H e ( t ) Ω | ϕ H e ( x , y , t , s ) | 2 d x d s ,
ρ N ( x , t ) = 0 N N ( t ) | ϕ N ( x , t , s ) | 2 d s ,
ρ e ( y , t ) = 0 N e ( t ) Ω | ϕ e ( x , y , t , s ) | 2 d x d s .
Also,
ρ = ρ D + ρ T + ρ H e + ρ N + ρ e ,
1.
( m H e , N ) T ( t ) = m H e , N ( t ) + 0 t Ω 2 ( ρ H e ( x , τ ) + ρ N ( x , τ ) ) u · n d S d τ ,
2.
m H e , N ( t ) = m H e ( t ) + m N ( t ) ,
3.
m H e ( t ) = Ω ρ H e ( x , t ) d x ,
4.
m N ( t ) = Ω ρ N ( x , t ) d x ,
5.
( m D ) ( t ) = ( m D ) 0 0 t Ω 1 Ω 2 ( ρ D ( x , τ ) ) u · n d S d τ α D ( m H e , N ) T ( t ) ,
6.
( m T ) ( t ) = ( m T ) 0 0 t Ω 1 Ω 2 ( ρ T ( x , τ ) ) u · n d S d τ α T ( m H e , N ) T ( t ) ,
7.
( m H e ) T ( t ) = Ω ρ H e ( x , t ) d x + 0 t Ω 2 ρ H e ( x , τ ) u · n d Γ d τ ,
8.
( m N ) T ( t ) = Ω ρ N ( x , t ) d x + 0 t Ω 2 ρ N ( x , τ ) u · n d Γ d τ ,
9.
( m N ) T ( t ) ( m H e ) T ( t ) = α N α H e ,
so that
α N ( m H e ) T ( t ) = α H e ( m N ) T ( t ) ,
10.
( m e ) T ( t ) = m e ( t ) 0 t Ω 2 ( ρ e ( x , τ ) ) u · n d Γ d τ ,
11.
m e ( t ) = Ω ρ e ( x , t ) d x .
12.
m e ( t ) = 0 N D ( t ) Ω | ϕ p D ( y , t , s ) | 2 d y d y d s m e m p + 0 N T ( t ) Ω | ϕ p T ( y , t , s ) | 2 d y d s m e m p + 0 N p ( t ) Ω | ϕ 2 p H e ( y , t , s ) | 2 d y d s m e m p .
Finally,
E = E i n d + E ρ ,
and where generically denoting
F ( ϕ ) = Ω f 5 ( ϕ , x , t , ξ , s ) d x d ξ d s ,
we have also
E ρ = Ω f 5 ( ϕ , x , t , ξ , s ) x k d ξ d s .
and,
B = B 0 curl A .

21. A qualitative modeling for a general phase transition process

In this section we develop a general qualitative modeling for a phase transition process.
Let Ω R 3 be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω .
Such a set Ω is supposed to a be a fixed volume in which an amount of mass of a substance A with a density function u will develop phase a transition for another phase with corresponding density function v . The total mass m T is suppose to be kept constant throughout such a process.
We model such transition in phase through a functional J : V × V R where
J ( u , v ) = γ 1 2 Ω u · u d x + α 1 2 Ω u 4 d x γ 2 2 Ω v · v d x + α 2 2 Ω v 4 d x 1 2 Ω ω 2 ( u 2 + v 2 ) d x E 2 Ω ( u 2 + v 2 ) d x m T .
Here γ 1 > 0 , γ 2 > 0 , α 1 > 0 , α 2 > 0 and V = W 1 , 2 ( Ω ) .
The phases corresponding to u and v are connected through a Lagrange multiplier E, which represents the chemical potential of the chemical process in question.
We assume the temperature is directly proportional to the internal kinetics E C energy where
E C = 1 2 Ω u 2 r u t · r u t d x .
For a internal vibrational motion, we assume approximately
r u e i ω t w 5 ( x ) ,
for an appropriate frequency ω and vectorial function w 5 .
Thus, the temperature T = T ( x , t ) is indeed proportional to ω 2 , that is, symbolically, we may write
T E 1 ω 2 .
Therefore, we start with the system with a phase corresponding to u 1 and v 0 at ω = 1 . Gradually increasing the temperature to a corresponding ω = 15 , we obtain a transition to a phase corresponding to u 0 and v 1 .
At this point, we also define the index normalized corresponding densities
ϕ u = u 2 u 2 + v 2
and
ϕ v = v 2 u 2 + v 2 .
Finally, we have obtained some numerical results for the following parameters:
Ω = [ 0 , 1 ] R , γ 1 = γ 2 = 1 , α = 0.1 , α 2 = 10 3 .
1.
We start with ω = 1 corresponding to ϕ u 1 and ϕ v 0 in Ω .
For the corresponding solutions ϕ u and ϕ v , please see Figure 15 and Figure 16, respectively.
2.
We end the process with ω = 15 corresponding to ϕ u 0 and ϕ v 1 in Ω .
For the corresponding solutions ϕ u and ϕ v , please see Figure 17 and Figure 18, respectively.

22. A mathematical description of a hydrogen molecule in a quantum mechanics context

In this section we develop a mathematical description for a hydrogen molecule.
Let Ω R 3 be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω .
Observe that a single hydrogen molecule comprises two hydrogen atoms physically linked through their electrons.
We recall that each hydrogen atom comprises one proton, one neutron and one electron.
Since the electric charge interaction effects are much higher than those related to the respective masses, in a first analysis we neglect the single neutron densities.
Denoting ( x , y , z ) Ω × Ω × Ω and time t [ 0 , t f ] , generically, for a particle p j k l at the atom A k l in the molecule M l , we define the following general density:
| ϕ ( p j k l ) T ( x , y , z , t ) | 2 = | ϕ p j k l ( x , y , z , t ) | 2 | ϕ A k l ( y , z , t ) | 2 | ϕ M l ( z , t ) | 2 m A j k m M l .
Here we have the particle density | ϕ p j k l ( x , y , z , t ) | 2 in the atom A k l with density | ϕ A k l ( y , z , t ) | 2 , at the molecule M l with a global density | ϕ M l ( z , t ) | 2 .
Here we have also denoted, m p j k l the particle mass, m A k l the mass of atom A k l and m M l the mass of molecule M l , so that we set the following constraints:
1.
Ω | ϕ p j k l ( x , y , z , t ) | 2 d x = m p j k l ,
2.
Ω | ϕ A k l ( y , z , t ) | 2 d y = m A k l ,
3.
Ω | ϕ M l ( z , t ) | 2 d z = m M l .
At this point we denote for the atoms A 1 e A 2 of a hydrogen molecule:
1.
m e j = m e : mass of electron e j in the atom A j , where j { 1 , 2 } .
2.
m p j = m p : mass of proton p j in the atom A j , where j { 1 , 2 } .
Therefore, considering the respective indexed densities for the particles in question, we define the total hydrogen molecule density, denoted by | ϕ H 2 ( x , y , z , t ) | 2 as
| ϕ H 2 ( x , y , z , t ) | 2 = | ϕ p 1 ( x , y , z , t ) | 2 | ϕ A 1 ( y , z , t ) | 2 | ϕ M ( z , t ) | 2 m A 1 m M + | ϕ e 1 ( x , y , z , t ) | 2 | ϕ A 1 ( y , z , t ) | 2 | ϕ M ( z , t ) | 2 m A 1 m M + | ϕ p 2 ( x , y , z , t ) | 2 | ϕ A 2 ( y , z , t ) | 2 | ϕ M ( z , t ) | 2 m A 2 m M + | ϕ e 2 ( x , y , z , t ) | 2 | ϕ A 2 ( y , z , t ) | 2 | ϕ M ( z , t ) | 2 m A 2 m M .
Such system is subject to the following constraints:
1.
From the proton p 1 in the atom A 1 :
Ω | ϕ p 1 ( x , y , z , t ) | 2 d x = m p ,
2.
For the proton p 2 in the atom A 2 :
Ω | ϕ p 2 ( x , y , z , t ) | 2 d x = m p ,
3.
For the atom A 1 :
Ω | ϕ A 1 ( y , z , t ) | 2 d y = m A 1 ,
4.
For the atom A 2 :
Ω | ϕ A 2 ( y , z , t ) | 2 d y = m A 2 ,
5.
For the electrons e 1 and e 2 , concerning the physical electronic link between the atoms:
Ω | ϕ e 1 ( x , y , z , t ) | 2 d x + Ω | ϕ e 2 ( x , y , z , t ) | 2 d x = 2 m e .
6.
For the total molecular density:
Ω | ϕ M ( z , t ) | 2 d z = m M .
Therefore, already including the Lagrange multipliers, the corresponding variational formulation for such a system stands for J : V R , where
J ( ϕ , E ) = G ( ϕ ) + F ( ϕ ) + J A u x ( ϕ , E ) .
Here we denote
| ( ϕ p j ) T | 2 = | ϕ p j ( x , y , z , t ) | 2 | ϕ A j ( y , z , t ) | 2 | ϕ M ( z , t ) | 2 m A j m M ,
| ( ϕ e j ) T | 2 = | ϕ e j ( x , y , z , t ) | 2 | ϕ A j ( y , z , t ) | 2 | ϕ M ( z , t ) | 2 m A j m M , j { 1 , 2 }
we assume γ ( p j ) > 0 , γ e j > 0 , γ A j > 0 , γ M > 0 , α ( p j ) T > 0 , α ( e j ) T > 0 α ( p j e k ) T < 0 , j , k { 1 , 2 } ,
G ( ϕ ) = γ p j 2 0 t f Ω ( ϕ p j ) · ( ϕ p j ) d x d y d z d t + γ e j 2 0 t f Ω ( ϕ e j ) · ( ϕ e j ) d x d y d z d t γ A j 2 Ω ( ϕ A j ) · ( ϕ A j ) d y d z d t + γ M 2 0 t f Ω ( ϕ M ) · ( ϕ M ) d z d t
and
F ( ϕ ) = α ( p j ) T 2 0 t f Ω | ϕ ( p j ) T ( x ξ 1 , y ξ 2 , z ξ 3 , t ) | 2 | ϕ ( p j ) T ( ξ 1 , ξ 2 , ξ 3 , t ) | 2 | ( x , y , z ) ( ξ 1 , ξ 2 , ξ 3 ) | d x d y d z ; d ξ 1 d ξ 2 d ξ 3 d t + α ( e j ) T 2 0 t f Ω | ϕ ( e j ) T ( x ξ 1 , y ξ 2 , z ξ 3 , t ) | 2 | ϕ ( e j ) T ( ξ 1 , ξ 2 , ξ 3 , t ) | 2 | ( x , y , z ) ( ξ 1 , ξ 2 , ξ 3 ) | d x d y d z d ξ 1 d ξ 2 d ξ 3 d t + α ( p j e k ) T 2 0 t f Ω | ϕ ( p j ) T ( x ξ 1 , y ξ 2 , z ξ 3 , t ) | 2 | ϕ ( e k ) T ( ξ 1 , ξ 2 , ξ 3 , t ) | 2 | ( x , y , z ) ( ξ 1 , ξ 2 , ξ 3 ) | d x d y d z d ξ 1 d ξ 2 d ξ 3 d t
Finally,
J A u x ( ϕ , E ) = 0 t f Ω ( E p ) j ( y , z , t ) Ω | ϕ p j ( x , y , z , t ) | 2 d x m p d y d z d t 0 t f Ω ( E e ) ( y , z , t ) Ω ( | ϕ e 1 ( x , y , z , t ) | 2 + | ϕ e 2 ( x , y , z , t ) | 2 ) d x 2 m e d y d z d t 0 t f Ω ( E A ) j ( z , t ) Ω | ϕ A j ( y , z , t ) | 2 d y m A j d z d t 0 t f ( E M ) ( t ) Ω | ϕ M ( z , t ) | 2 d z m M d t .
Remark 22.1. 
We highlight the two electrons which link the atoms are at same level of energy E e . Morever, each atom has its energy level E A j and the molecule as a whole has also its energy level E M .

23. A mathematical model for the water hydrolysis

In this section we develop a modeling for a chemical reaction known as the water hydrolysis.
Let Ω R 3 be an open, bounded and connected set with a regular (Lipschitzian) boundary denoted by Ω .
In such a volume Ω containing a total mass m T of water initially at the temperature 25 C with pressure 1 atm, we intend to model the following reaction
H 2 O O H + H +
which as previously mentioned is the well known water hydrolysis.
We highlight H 2 O stand for a water molecule which subject to an appropriate electric potential is decomposed into a ionized O H molecule and ionized H + atom.
It is also well known that the water symbol H 2 O corresponds to a molecule with two hydrogen (H) atoms and one oxygen (O) atom.
Moreover, the oxygen atom O has 8 protons, 8 neutrons and 8 electrons whereas the hydrogen atom H has one proton, one neutron and one electron.
Remark 23.1. 
Here we have assumed that a unit mass of H 2 O reacts into a fractional mass α B of O H and a fractional mass α C of H + .
Symbolically, we have:
1 = α B + α C .
To clarify the notation we set the conventions:
1.
H 2 O molecule generically corresponds to wave function ϕ 1 .
2.
O H molecule corresponds to wave function ϕ 2 .
3.
H + hydrogen atom corresponds to wave function ϕ 3 .
At this point we define the following densities:
1.
For the H 2 O water density (for charges), denoted by | ϕ 1 | 2 , we have
| ϕ 1 ( x , y , z , t ) | 2 = K p j = 1 2 | ( ϕ 1 H ) p j ( x , y , z , t ) | 2 | ( ϕ 1 H ) A j ( y , z , t ) | 2 | ( ϕ 1 ) M ( z , t ) | 2 ( m ) A j H ( m 1 ) M + K e j = 1 2 | ( ϕ 1 H ) e j ( x , y , z , t ) | 2 | ( ϕ 1 H ) A j ( y , z , t ) | 2 | ( ϕ 1 ) M ( z , t ) | 2 ( m 1 ) A j H ( m 1 ) M + K p j = 1 8 | ( ϕ 1 O ) p j ( x , y , z , t ) | 2 | ( ϕ 1 O ) A ( y , z , t ) | 2 | ( ϕ 1 ) M ( z , t ) | 2 ( m ) A O ( m 1 ) M + K e j = 1 8 | ( ϕ 1 O ) e j ( x , y , z , t ) | 2 | ( ϕ 1 O ) A ( y , z , t ) | 2 | ( ϕ 1 ) M ( z , t ) | 2 ( m ) A O ( m 1 ) M
where ( m 1 ) M is the mass of a single water molecule and generically | ( ϕ 1 H ) p j ( x , y , z , t ) | 2 refers to the hydrogen proton p j at the hydrogen atom A j concerning the H 2 O molecular density and so on.
2.
For the O H density, denoted by | ϕ 2 | 2 , we have
| ϕ 2 ( x , y , z , t ) | 2 = K p | ( ϕ 2 H ) p ( x , y , z , t ) | 2 | ( ϕ 2 H ) A ( y , z , t ) | 2 | ( ϕ 2 ) M ( z , t ) | 2 ( m ) A H ( m 2 ) M + K e | ( ϕ 2 H ) e 1 ( x , y , z , t ) | 2 | ( ϕ 2 H ) A ( y , z , t ) | 2 | ( ϕ 2 ) M ( z , t ) | 2 ( m ) A H ( m 2 ) M + K e | ( ϕ 2 O H ) e 2 ( x , z , t ) | 2 | ( ϕ 2 ) M ( z , t ) | 2 ( m 2 ) M + K p j = 1 8 | ( ϕ 2 O ) p j ( x , y , z , t ) | 2 | ( ϕ 2 O ) A ( y , z , t ) | 2 | ( ϕ 2 ) M ( z , t ) | 2 ( m ) A O ( m 2 ) M + K e j = 1 8 | ( ϕ 2 O ) e j ( x , y , z , t ) | 2 | ( ϕ 2 O ) A ( y , z , t ) | 2 | ( ϕ 2 ) M ( z , t ) | 2 ( m ) A O ( m 2 ) M ,
where ( m 2 ) M is the mass of a single molecule of O H .
3.
For the ionized hydrogen atom have
| ϕ 3 ( x , y , t ) | 2 = K p | ( ϕ 3 H ) p ( x , y , t ) | 2 | ( ϕ 3 H ) A ( y , t ) | 2 ( m 3 ) A .
where we have denoted ( m 3 ) A is the mass of a single atom of H + .
Here K p > 0 and K e < 0 are appropriate real constants concerning a proton and an electron charge, respectively.
The system is subject to the following constraints:
1.
Ω | ( ϕ 1 H ) p j ( x , y , z , t ) | 2 d x = m p , j { 1 , 2 } ,
2.
Ω | ( ϕ 1 H ) e j ( x , y , z , t ) | 2 d x = m e , j { 1 , 2 } ,
3.
Ω | ( ϕ 1 O ) p j ( x , y , z , t ) | 2 d x = m p , j { 1 , 8 } ,
4.
Ω | ( ϕ 1 O ) e j ( x , y , z , t ) | 2 d x = m e , j { 1 , 8 } ,
5.
Ω | ( ϕ 2 H ) p ( x , y , z , t ) | 2 d x = m p ,
6.
Ω | ( ϕ 2 H ) e 1 ( x , y , z , t ) | 2 d x = m e ,
7.
Ω | ( ϕ 2 H ) e 2 ( x , y , z , t ) | 2 d x = m e ,
8.
Ω | ( ϕ 2 O ) p j ( x , y , z , t ) | 2 d x = m p , j { 1 , 8 } ,
9.
Ω | ( ϕ 2 O ) e j ( x , y , z , t ) | 2 d x = m e , j { 1 , 8 } ,
10.
Ω | ( ϕ 3 H ) p ( x , z , t ) | 2 d x = m p ,
11.
Ω | ( ϕ 1 H ) A j ( y , z , t ) | 2 d y = m A H , j { 1 , 2 } ,
12.
Ω | ( ϕ 1 O ) A ( y , z , t ) | 2 d y = m A O ,
13.
Ω | ( ϕ 2 H ) A ( y , z , t ) | 2 d y = m A H ,
14.
Ω | ( ϕ 2 O ) A ( y , z , t ) | 2 d y = m A O ,
15.
Ω | ( ϕ 3 H ) A ( y , z , t ) | 2 d y = m A H ,
16.
Ω ( | ( ϕ 1 ) M ( z , t ) | 2 + | ( ϕ 2 ) M ( z , t ) | 2 + | ( ϕ 3 ) M ( z , t ) | 2 ) d z = m T ,
17.
Ω ( α C | ( ϕ 2 ) M ( z , t ) | 2 α B | ( ϕ 3 ) M ( z , t ) | 2 ) d z = 0 .
Already including the Lagrange multipliers for the constraints, the variational formulation for such system. denoted by the functional J ( ϕ , E ) stands for
J ( ϕ , E ) = G ( ϕ ) + F ( ϕ ) + F 1 ( ϕ ) J A u x ( ϕ , E ) ,
where
G ( ϕ ) = γ p 2 j = 1 2 0 t f Ω ( ϕ 1 H ) p j · ( ϕ 1 H ) p j d x d y d z d t + γ e 2 j = 1 2 0 t f Ω ( ϕ 1 H ) e j · ( ϕ 1 H ) e j d x d y d z d t + γ p 2 j = 8 2 0 t f Ω ( ϕ 1 O ) p j · ( ϕ 1 O ) p j d x d y d z d t + γ e 2 j = 1 2 0 t f Ω ( ϕ 1 O ) e j · ( ϕ 1 O ) e j d x d y d z d t + γ p 2 0 t f Ω ( ϕ 2 H ) p · ( ϕ 2 H ) p d x d y d z d t + γ e 2 0 t f Ω ( ϕ 2 H ) e 1 · ( ϕ 2 H ) e 1 d x d y d z d t + γ e 2 j = 1 2 0 t f Ω ( ϕ 2 O H ) e 2 · ( ϕ 1 O H ) e 2 d x d z d t + γ p 2 j = 8 2 0 t f Ω ( ϕ 2 O ) p j · ( ϕ 2 O ) p j d x d y d z d t + γ e 2 j = 1 2 0 t f Ω ( ϕ 2 O ) e j · ( ϕ 2 O ) e j d x d y d z d t + γ p 2 j = 1 2 0 t f Ω ( ϕ 2 H ) p · ( ϕ 2 O ) p d x d y d t + γ A H 2 j = 1 2 0 t f Ω ( ϕ 1 H ) A j · ( ϕ 1 H ) A j d y d z d t + γ A O 2 0 t f Ω ( ϕ 1 O ) A · ( ϕ 1 O ) A d y d z d t + γ A H 2 0 t f Ω ( ϕ 2 H ) A · ( ϕ 2 H ) A d y d z d t + γ A O 2 0 t f Ω ( ϕ 2 O ) A · ( ϕ 2 O ) A d y d z d t + γ M 1 2 0 t f Ω ( ϕ 1 ) M · ( ϕ 1 ) M d z d t + γ M 2 2 0 t f Ω ( ϕ 2 ) M · ( ϕ 2 ) M d z d t γ A 3 2 0 t f Ω ( ϕ 3 ) A · ( ϕ 3 ) A d y d t .
Here γ p > 0 , γ e > 0 , γ A H > 0 , , γ A O > 0 , γ M 1 > 0 , γ M 2 > 0 , γ A 3 > 0 .
Moreover,
F ( ϕ ) = α 1 2 0 t f Ω | ϕ 1 ( x ξ 1 , y ξ 2 , z ξ 3 , t ) | 2 | ϕ 1 ( ξ 1 , ξ 2 , ξ 3 , t ) | 2 | ( x , y , z ) ( ξ 1 , ξ 2 , ξ 3 ) | d x d y d z d x 1 d x 2 d x 3 d t + α 2 2 0 t f Ω | ϕ 2 ( x ξ 1 , y ξ 2 , z ξ 3 , t ) | 2 | ϕ 2 ( ξ 1 , ξ 2 , ξ 3 , t ) | 2 | ( x , y , z ) ( ξ 1 , ξ 2 , ξ 3 ) | d x d y d z d x 1 d x 2 d x 3 d t + α 3 2 0 t f Ω | ϕ 3 ( x ξ 1 , z ξ 3 , t ) | 2 | ϕ 3 ( ξ 1 , ξ 3 , t ) | 2 | ( x , y , z ) ( ξ 1 , ξ 2 , ξ 3 ) | d x d y d z d x 1 d x 3 d t + α 23 2 0 t f Ω | ϕ 2 ( x ξ 1 , y ξ 2 , z ξ 3 , t ) | 2 | ϕ 3 ( ξ 1 , ξ 3 , t ) | 2 | ( x , y , z ) ( ξ 1 , ξ 2 , ξ 3 ) | d x d y d z d x 1 d x 2 d x 3 d t
where α 1 > 0 , α 2 > 0 , α 3 > 0 and α 23 > 0 .
Furthermore,
F 1 ( ϕ ) = 0 t f Ω V ( x , y , z , t ) ( | ϕ 1 | 2 + | ϕ 2 | 2 + | ϕ 3 | 2 ) d x d y d z d t ,
where V = V ( x , y , z , t ) is an electric potential originated from an external electric field E applied on Ω .
Finally,
J A u x ( ϕ , E ) = j = 1 2 0 t f Ω ( E 1 ) p j H ( y , z , t ) Ω | ( ϕ 1 H ) p j ( x , y , z , t ) | 2 d x m p d y d z d t + j = 1 2 0 t f Ω ( E 1 ) e j H ( y , z , t ) Ω | ( ϕ 1 H ) e j ( x , y , z , t ) | 2 d x m e d y d z d t + j = 8 2 0 t f Ω ( E 1 ) p j O ( y , z , t ) Ω | ( ϕ 1 O ) p j ( x , y , z , t ) | 2 d x m p d y d z d t + j = 8 2 0 t f Ω ( E 1 ) e j O ( y , z , t ) Ω | ( ϕ 1 O ) e j ( x , y , z , t ) | 2 d x m e d y d z d t + 0 t f Ω ( E 2 ) p H ( y , z , t ) Ω | ( ϕ 2 H ) p ( x , y , z , t ) | 2 d x m p d y d z d t + j = 8 2 0 t f Ω ( E 2 ) p j O ( y , z , t ) Ω | ( ϕ 2 O ) p j ( x , y , z , t ) | 2 d x m p d y d z d t + j = 8 2 0 t f Ω ( E 2 ) e j O ( y , z , t ) Ω | ( ϕ 2 O ) e j ( x , y , z , t ) | 2 d x m e d y d z d t + 0 t f Ω ( E 3 ) p H ( y , t ) Ω | ( ϕ 3 H ) p ( x , y , t ) | 2 d x m p d y d t + j = 1 2 0 t f Ω ( E 4 ) A j H ( z , t ) Ω ( | ( ϕ 1 ) A j H ( y , z , t ) | 2 d y m A j H d z d t + 0 t f Ω Ω ( E 4 ) A O ( z , t ) Ω ( | ( ϕ 1 ) A O ( y , z , t ) | 2 d y m A O d z d t + 0 t f Ω ( E 5 ) A H ( z , t ) Ω ( | ( ϕ 2 ) A H ( y , z , t ) | 2 d y m A H d z d t + 0 t f Ω ( E 5 ) A O ( z , t ) Ω ( | ( ϕ 2 ) A O ( y , z , t ) | 2 d y m A O d z d t 0 t f ( E 6 ) A H ( t ) Ω ( | ( ϕ 3 ) A H ( y , t ) | 2 d y m A H d t + 0 t f ( E 7 ) ( t ) Ω ( | ( ϕ 1 ) M ( z , t ) | 2 + | ( ϕ 2 ) M ( z , t ) | 2 + | ( ϕ 3 ) M ( z , t ) | 2 ) d z m T d t + 0 t f ( E 8 ) ( t ) Ω ( α C | ( ϕ 2 ) M ( z , t ) | 2 α B | ( ϕ 3 ) M ( z , t ) | 2 ) d z d t .

24. A mathematical model for the Austenite and Martensite phase transition

In this section we consider a phase transition of a solid solution of γ F e ( γ i r o n ) and carbon with a 0.75 / 100 proportion of carbon, known as austenite, initially at a temperature above and close to 723 C and rapidly cooled to a temperature of about 25 C , developing a phase transition which generates a solid solution of α F e ( α i r o n ) and carbon known as martensite.
Let Ω R 3 be an open, bounded and connected set with a regular boundary denoted by Ω which contains an amount of austenite at 723 C and which is rapidly cooled to a temperature 25 C on a time interval [ 0 , t f ] , resulting a phase known as martensite.
We recall the γ F e of austenite phase presents a multi-faced cubic crystalline structure in a micro-structure with carbon atoms.
On the other hand, α F e structure of the martensite phase has a C C C cubic centralized crystalline structure in a micro-structure with carbon atoms.
At this point, we also recall that the F e (iron) atom has 26 protons, 26 electrons and 30 neutrons.
On the other hand a C a r b o n 12 atom has 6 protons and this same number of electrons and neutrons.
Here we define the density function ϕ 1 , representing the Austenite phase, where:
| ϕ 1 ( x , y , z , t ) | 2 = j = 1 26 | ϕ p j γ F e ( x , y , z , t ) | 2 | ϕ A γ F e ( y , z , t ) | 2 | ϕ 1 γ ( z , t ) | 2 1 ( m A γ ) 2 + j = 1 26 | ϕ e j γ F e ( x , y , z , t ) | 2 | ϕ A γ F e ( y , z , t ) | 2 | ϕ 1 γ ( z , t ) | 2 1 ( m A γ ) 2 + j = 1 30 | ϕ N j γ F e ( x , y , z , t ) | 2 | ϕ A γ F e ( y , z , t ) | 2 | ϕ 1 γ ( z , t ) | 2 1 ( m A γ ) 2 + j = 1 6 | ( ϕ 1 C ) p j ( x , y , z , t ) | 2 | ( ϕ 1 C ) A ( y , z , t ) | 2 | ϕ 1 C ( z , t ) | 2 1 ( m A C ) 2 + j = 1 6 | ( ϕ 1 C ) e j ( x , y , z , t ) | 2 | ( ϕ 1 C ) A ( y , z , t ) | 2 | ϕ 1 C ( z , t ) | 2 1 ( m A C ) 2 + j = 1 6 | ( ϕ 1 C ) N j ( x , y , z , t ) | 2 | ( ϕ 1 C ) A ( y , z , t ) | 2 | ϕ 1 C ( z , t ) | 2 1 ( m A C ) 2 .
Similarly, we define the density function for the Martensite phase, which is denoted by ϕ 2 , where:
| ϕ 2 ( x , y , z , t ) | 2 = j = 1 26 | ϕ p j α F e ( x , y , z , t ) | 2 | ϕ A γ F e ( y , z , t ) | 2 | ϕ 1 α ( z , t ) | 2 1 ( m A α ) 2 + j = 1 26 | ϕ e j α F e ( x , y , z , t ) | 2 | ϕ A α F e ( y , z , t ) | 2 | ϕ 1 γ ( z , t ) | 2 1 ( m A α ) 2 + j = 1 30 | ϕ N j α F e ( x , y , z , t ) | 2 | ϕ A α F e ( y , z , t ) | 2 | ϕ 1 α ( z , t ) | 2 1 ( m A α ) 2 + j = 1 6 | ( ϕ 1 C ) p j ( x , y , z , t ) | 2 | ( ϕ 1 C ) A ( y , z , t ) | 2 | ϕ 1 C ( z , t ) | 2 1 ( m A C ) 2 + j = 1 6 | ( ϕ 2 C ) e j ( x , y , z , t ) | 2 | ( ϕ 2 C ) A ( y , z , t ) | 2 | ϕ 2 C ( z , t ) | 2 1 ( m A C ) 2 + j = 1 6 | ( ϕ 2 C ) N j ( x , y , z , t ) | 2 | ( ϕ 2 C ) A ( y , z , t ) | 2 | ϕ 2 C ( z , t ) | 2 1 ( m A C ) 2 .
For the C F C γ F e ( γ i r o n ) corresponding to the Austenite phase, such density functions are subject to the following constraints:
Defining
C γ = { ( ε 1 , 0 , 0 ) , ( 0 , ε 2 , 0 ) , ( 0 , 0 , ε 3 ) , : ε j { + 1 , 1 } , j { 1 , 2 , 3 } } ,
( C γ ) 1 = { ( ε 1 , ε 2 , ε 3 ) , : ε j { + 1 , 1 } , j { 1 , 2 , 3 } } ,
and
C γ = { ( ε 1 , ε 2 , 0 ) , ( ε 1 , 0 , ε 3 ) , ( 0 , ε 2 , ε 3 ) , : ε j { + 1 , 1 } , j { 1 , 2 , 3 } } ,
we must have
ϕ A γ F e ( y , z 1 + ε 1 δ z , z 2 + ε 2 δ z , z 3 + ε 3 δ z , t ) = ϕ A γ F e ( y , z 1 + ε ˜ 1 δ z , z 2 + ε ˜ 2 δ z , z 3 + ε ˜ 3 δ z , t ) ,
ε , ε ˜ C γ , where δ z R + is a small real parameter related to γ F e crystalline structure dimensions.
We must have also,
ϕ A γ F e ( y , z 1 + ε 1 δ z , z 2 + ε 2 δ z , z 3 + ε 3 δ z , t ) = ϕ A γ F e ( y , z 1 + ε ˜ 1 δ z , z 2 + ε ˜ 2 δ z , z 3 + ε ˜ 3 δ z , t ) ,
ε , ε ˜ ( C γ ) 1 and,
( ϕ 1 C ) A ( y , z 1 + ε 1 δ z , z 2 + ε 2 δ z , z 3 + ε 3 δ z , t ) = ( ϕ 1 C ) A ( y , z 1 + ε ˜ 1 δ z , z 2 + ε ˜ 2 δ z , z 3 + ε ˜ 3 δ z , t ) ,
ε , ε ˜ ( C γ ) 2 .
For the C C C α F e ( α i r o n ) corresponding to the Austenite phase, such density functions are subject to the following constraints:
Defining
C α = { ( ε 1 , ε 2 , ε 3 ) , : ε j { + 1 , 1 } , j { 1 , 2 , 3 } } ,
( C α ) 1 = { ( ε 1 , ε 2 , ε 3 ) , : ε 1 , ε 2 { + 1 , 1 } and ε 3 = 0 } ,
( C α ) 2 = { ( ε 1 , ε 2 , ε 3 ) , : ε 1 = ε 2 = 0 and ε 3 { + 1 , 1 } } ,
we must have
ϕ A α F e ( y , z 1 + ε 1 δ ^ z , z 2 + ε 2 δ ^ z , z 3 + ε 3 δ ^ z , t ) = ϕ A α F e ( y , z 1 + ε ˜ 1 δ ^ z , z 2 + ε ˜ 2 δ ^ z , z 3 + ε ˜ 3 δ ^ z , t ) ,
ε , ε ˜ C α , where δ ^ z R + is a small real parameter related to α F e crystalline structure dimensions.
We must have also,
( ϕ 2 C ) A ( y , z 1 + ε 1 δ ^ z , z 2 + ε 2 δ ^ z , z 3 + ε 3 δ ^ z , t ) = ( ϕ 2 C ) A ( y , z 1 + ε ˜ 1 δ ^ z , z 2 + ε ˜ 2 δ ^ z , z 3 + ε ˜ 3 δ ^ z , t ) ,
ε , ε ˜ ( C α ) 1 ( C α ) 2 .
The other constraints for the densities are given by:
1.
For the Austenite phase:
(a)
Ω | ϕ p j γ F e ( x , y , z , t ) | 2 d x = m p , j { 1 , 26 } ,
(b)
Ω | ϕ e j γ F e ( x , y , z , t ) | 2 d x = m e , j { 1 , 26 } ,
(c)
Ω | ϕ N j γ F e ( x , y , z , t ) | 2 d x = m N , j { 1 , 30 } ,
(d)
Ω | ϕ A γ F e ( x , y , z , t ) | 2 d x = m A γ ,
(e)
Ω | ( ϕ 1 C ) p j ( x , y , z , t ) | 2 d x = m p , j { 1 , 6 } ,
(f)
Ω | ( ϕ 1 C ) e j ( x , y , z , t ) | 2 d x = m e , j { 1 , 6 } ,
(g)
Ω | ( ϕ 1 C ) N j ( x , y , z , t ) | 2 d x = m N , j { 1 , 6 } ,
(h)
Ω | ( ϕ 1 C ) A ( x , y , z , t ) | 2 d x = m A C ,
2.
For the Martensite phase:
(a)
Ω | ϕ p j α F e ( x , y , z , t ) | 2 d x = m p , j { 1 , 26 } ,
(b)
Ω | ϕ e j α F e ( x , y , z , t ) | 2 d x = m e , j { 1 , 26 } ,
(c)
Ω | ϕ N j α F e ( x , y , z , t ) | 2 d x = m N , j { 1 , 30 } ,
(d)
Ω | ϕ A α F e ( x , y , z , t ) | 2 d x = m A α ,
(e)
Ω | ( ϕ 2 C ) p j ( x , y , z , t ) | 2 d x = m p , j { 1 , 6 } ,
(f)
Ω | ( ϕ 2 C ) e j ( x , y , z , t ) | 2 d x = m e , j { 1 , 6 } ,
(g)
Ω | ( ϕ 2 C ) N j ( x , y , z , t ) | 2 d x = m N , j { 1 , 6 } ,
(h)
Ω | ( ϕ 2 C ) A ( x , y , z , t ) | 2 d x = m A C .
3.
For the total F e (iron) mass,
Ω | ϕ 1 γ ( z , t ) | 2 d z + Ω | ϕ 2 γ ( z , t ) | 2 d z = ( m F e ) T ,
4.
For the total Carbon mass
Ω | ϕ 1 C ( z , t ) | 2 d z + Ω | ϕ 2 C ( z , t ) | 2 d z = ( m C ) T .
At this point we define the functional J which models such a pahse transition in question, where
J ( ϕ , E ) = G ( ϕ ) + F ( ϕ ) + F 1 ( ϕ ) + J A u x ( ϕ , E )
where
G ( ϕ ) = j = 1 26 γ ^ p γ F e 2 0 t f Ω ϕ p j γ F e · ϕ p j γ F e d x d y d z d t + j = 1 26 γ ^ e γ F e 2 0 t f Ω ϕ e j γ F e · ϕ e j γ F e d x d y d z d t + j = 1 30 γ ^ N γ F e 2 0 t f Ω ϕ N j γ F e · ϕ N j γ F e d x d y d z d t + j = 1 26 γ ^ p α F e 2 0 t f Ω ϕ p j α F e · ϕ p j α F e d x d y d z d t + j = 1 26 γ ^ e α F e 2 0 t f Ω ϕ e j α F e · ϕ e j γ F e d x d y d z d t + j = 1 30 γ ^ N α F e 2 0 t f Ω ϕ N j α F e · ϕ N j α F e d x d y d z d t + γ ^ A γ 2 0 t f Ω ( ϕ A γ F e ( y , z , t ) · ϕ A γ F e ( y , z , t ) ) d y d z d t + γ ^ A α 2 0 t f Ω ( ϕ A α F e ( y , z , t ) · ϕ A α F e ( y , z , t ) ) d y d z d t + j = 1 6 γ ^ p C 2 0 t f Ω ( ϕ 1 C ) p j · ( ϕ 1 C ) p j d x d y d z d t + j = 1 6 γ ^ e C 2 0 t f Ω ( ϕ 1 C ) e j · ( ϕ 1 C ) e j d x d y d z d t + j = 1 6 γ ^ N C 2 0 t f Ω ( ϕ 1 C ) N j · ( ϕ 1 C ) N j d x d y d z d t + j = 1 6 γ ^ p C 2 0 t f Ω ( ϕ 2 C ) p j · ( ϕ 2 C ) p j d x d y d z d t + j = 1 6 γ ^ e C 2 0 t f Ω ( ϕ 2 C ) e j · ( ϕ 2 C ) e j d x d y d z d t + j = 1 6 γ ^ N C 2 0 t f Ω ( ϕ 2 C ) N j · ( ϕ 2 C ) N j d x d y d z d t + γ ^ A C 2 0 t f Ω ( ( ϕ 1 C ) A · ( ϕ 1 C ) A ) d y d z d t + γ ^ A C 2 0 t f Ω ( ( ϕ 2 C ) A · ( ϕ 2 C ) A ) d y d z d t + γ ^ T γ 2 0 t f Ω ( ( ϕ 1 γ ) · ( ϕ 1 γ ) ) d z d t + γ ^ T γ 2 0 t f Ω ( ( ϕ 1 α ) · ( ϕ 1 α ) ) d z d t + γ ^ T C 2 0 t f Ω ( ( ϕ 1 C ) · ( ϕ 1 C ) ) d z d t + γ ^ T γ 2 0 t f Ω ( ( ϕ 2 C ) · ( ϕ 2 C ) ) d z d t
Also,
F ( ϕ ) = α ^ 1 2 0 t f Ω | ϕ 1 ( x ξ 1 , y ξ 2 , z ξ 3 , t ) | 2 | | ϕ 1 ( ξ 1 , ξ 2 , ξ 3 , t ) | 2 | ( x , y , z ) ( ξ 1 , ξ 2 , ξ 3 ) | d x d y d z d ξ 1 d ξ 2 d ξ 3 d t + α ^ 2 2 0 t f Ω | ϕ 2 ( x ξ 1 , y ξ 2 , z ξ 3 , t ) | 2 | | ϕ 2 ( ξ 1 , ξ 2 , ξ 3 , t ) | 2 | ( x , y , z ) ( ξ 1 , ξ 2 , ξ 3 ) | d x d y d z d ξ 1 d ξ 2 d ξ 3 d t ,
F 1 ( ϕ ) = 0 t f Ω w 2 ( z , t ) ( | ϕ 1 ( z , t ) | 2 + ϕ 2 ( z , t ) | 2 ) d z d t ,
Finally, J A u x = J A u x 1 + J A u x 2 + J A u x 3 + J A u x 4 + J A u x 5 , where
J A u x 1 = j = 1 26 0 t f Ω E p j γ F e ( y , z , t ) Ω | ϕ p j γ F e ( x , y , z , t ) | 2 d x m p d y d z d t + j = 1 26 0 t f Ω E e j γ F e ( y , z , t ) Ω | ϕ e j γ F e ( x , y , z , t ) | 2 d x m e d y d z d t + j = 1 30 0 t f Ω E N j γ F e ( y , z , t ) Ω | ϕ N j γ F e ( x , y , z , t ) | 2 d x m N d y d z d t j = 1 26 0 t f Ω E p j α F e ( y , z , t ) Ω | ϕ p j α F e ( x , y , z , t ) | 2 d x m p d y d z d t + j = 1 26 0 t f Ω E e j α F e ( y , z , t ) Ω | ϕ e j α F e ( x , y , z , t ) | 2 d x m e d y d z d t + j = 1 30 0 t f Ω E N j α F e ( y , z , t ) Ω | ϕ N j α F e ( x , y , z , t ) | 2 d x m N d y d z d t + 0 t f Ω E A γ F e ( y , t ) Ω | ϕ A γ F e ( y , z , t ) | 2 d y m A γ d z d t + 0 t f Ω E A α F e ( y , t ) Ω | ϕ A α F e ( y , z , t ) | 2 d y m A α d z d t
J A u x 2 = j = 1 26 0 t f Ω ( E 1 C ) p j ( y , z , t ) Ω | ( ϕ 1 C ) p j ( x , y , z , t ) | 2 d x m p d y d z d t j = 1 26 0 t f Ω ( E 1 C ) e j ( y , z , t ) Ω | ( ϕ 1 C ) e j ( x , y , z , t ) | 2 d x m e d y d z d t j = 1 26 0 t f Ω ( E 1 C ) N j ( y , z , t ) Ω | ( ϕ 1 C ) N j ( x , y , z , t ) | 2 d x m N d y d z d t j = 1 26 0 t f Ω ( E 2 C ) p j ( y , z , t ) Ω | ( ϕ 2 C ) p j ( x , y , z , t ) | 2 d x m p d y d z d t j = 1 26 0 t f Ω ( E 2 C ) e j ( y , z , t ) Ω | ( ϕ 2 C ) e j ( x , y , z , t ) | 2 d x m e d y d z d t j = 1 26 0 t f Ω ( E 2 C ) N j ( y , z , t ) Ω | ( ϕ 2 C ) N j ( x , y , z , t ) | 2 d x m N d y d z d t 0 t f Ω ( E 1 C ) A ( y , t ) Ω | ( ϕ 1 C ) A ( y , z , t ) | 2 d y m A C d z d t + 0 t f Ω ( E 2 C ) A ( y , t ) Ω | ( ϕ 2 C ) A ( y , z , t ) | 2 d y m A C d z d t
and,
J A u x 3 = 0 t f E 3 γ , α ( t ) Ω ( | ϕ 1 γ ( z , t ) | 2 + | ϕ 2 α ( z , t ) | 2 ) d z ( m F e ) T d t + 0 t f E 3 C ( t ) Ω ( | ϕ 1 C ( z , t ) | 2 + | ϕ 2 C ( z , t ) | 2 ) d z ( m C ) T d t .
J A u x 4 = + ε , ε ˜ C γ 0 t f Ω E 4 ε , ε ˜ ( y , z , t ) ( ϕ A γ F e ( y , z 1 + ε 1 δ z , z 2 + ε 2 δ z , z 3 + ε 3 δ z , t ) ϕ A γ F e ( y , z 1 + ε ˜ 1 δ z , z 2 + ε ˜ 2 δ z , z 3 + ε ˜ 3 δ z , t ) ) d y d z d t ε , ε ˜ ( C γ ) 1 0 t f Ω E 5 ε , ε ˜ ( y , z , t ) ϕ A γ F e ( y , z 1 + ε 1 δ z , z 2 + ε 2 δ z , z 3 + ε 3 δ z , t ) ϕ A γ F e ( y , z 1 + ε ˜ 1 δ z , z 2 + ε ˜ 2 δ z , z 3 + ε ˜ 3 δ z , t ) ) d y d z d t + ε , ε ˜ ( C γ ) 2 0 t f Ω E 6 ε , ε ˜ ( y , z , t ) ( ϕ 1 C ) A ( y , z 1 + ε 1 δ z , z 2 + ε 2 δ z , z 3 + ε 3 δ z , t ) ( ϕ 1 C ) A ( y , z 1 + ε ˜ 1 δ z , z 2 + ε ˜ 2 δ z , z 3 + ε ˜ 3 δ z , t ) ) d y d z d t + ε , ε ˜ ( C α ) 0 t f Ω E 7 ε , ε ˜ ( y , z , t ) ( ϕ A α F e ( y , z 1 + ε 1 δ ^ z , z 2 + ε 2 δ ^ z , z 3 + ε 3 δ ^ z , t ) ϕ A α F e ( y , z 1 + ε ˜ 1 δ ^ z , z 2 + ε ˜ 2 δ ^ z , z 3 + ε ˜ 3 δ ^ z , t ) ) d y d z d t + ε , ε ˜ ( C α ) 1 ( C α ) 2 0 t f Ω E 8 ε , ε ˜ ( y , z , t ) ( ( ϕ 2 C ) A ( y , z 1 + ε 1 δ ^ z , z 2 + ε 2 δ ^ z , z 3 + ε 3 δ ^ z , t ) ( ϕ 2 C ) A ( y , z 1 + ε ˜ 1 δ ^ z , z 2 + ε ˜ 2 δ ^ z , z 3 + ε ˜ 3 δ ^ z , t ) ) d y d z d t .
Finally, for a field of displacements u = ( u 1 , u 2 , u 3 ) resulting from the action of a external load field f = ( f 1 , f 2 , f 3 ) and temperature variations, we define
J A u x 5 = 1 2 0 t f Ω Λ 1 ( x , t ) H i j k l 1 ( ( e i j ( u ) e i j 1 ( w ) ) ( e k l ( u ) e k l 2 ( w ) ) ) + Λ 2 ( z , t ) H i j k l 2 ( ( e i j ( u ) e i j 2 ( w ) ) ( e k l ( u ) e k l 2 ( w ) ) ) d x d t 1 2 0 t f Ω ρ ( x , t ) u t ( x , t ) · u t ( x , t ) d x d t u i , f i L 2 ,
where
e i j ( u ) = 1 2 u i x j + u j x i ,
ρ 1 ( z , t ) = Ω | ϕ 1 ( x , y , z , t ) | 2 d x d y ,
ρ 2 ( z , t ) = Ω | ϕ 2 ( x , y , z , t ) | 2 d x d y ,
ρ ( z , t ) = ρ 1 ( z , t ) + ρ 2 ( z , t ) ,
and
Λ 1 ( z , t ) = ρ 1 ( z , t ) ρ 1 ( z , t ) + ρ 2 ( z , t ) ,
Λ 2 ( z , t ) = ρ 2 ( z , t ) ρ 1 ( z , t ) + ρ 2 ( z , t ) .
Remark 24.1. 
The system temperature is suppose to be directly proportional to w ( z , t ) 2 , which is in this model is a known function obtained experimentally. Finally, the strain tensors { e i j 1 ( w ) } and { e i j 2 ( w ) } refer to austenite and martensite phases, respectively. Such tensors also depend on the temperature and must be also obtained experimentally.

References

  1. R.A. Adams and J.F. Fournier, Sobolev Spaces, 2nd edn. (Elsevier, New York, 2003).
  2. W.R. Bielski, A. W.R. Bielski, A. Galka, J.J. Telega, The Complementary Energy Principle and Duality for Geometrically Nonlinear Elastic Shells. I. Simple case of moderate rotations around a tangent to the middle surface. Bulletin of the Polish Academy of Sciences, Technical Sciences, Vol. 38, No. 7-9, 1988.
  3. W.R. Bielski and J.J. Telega, A Contribution to Contact Problems for a Class of Solids and Structures, Arch. Mech., 37, 4-5, pp. 303-320, Warszawa 1985.
  4. J.F. Annet, Superconductivity, Superfluids and Condensates, 2nd edn. (Oxford Master Series in Condensed Matter Physics, Oxford University Press, Reprint, 2010). 2010.
  5. F.S. Botelho, Functional Analysis, Calculus of Variations and Numerical Methods in Physics and Engineering, CRC Taylor and Francis, Florida, 2020.
  6. F.S. Botelho, Advanced Calculus and its Applications in Variational Quantum Mechanics and Relativity Theory, CRC Taylor and Francis, Florida, 2021.
  7. F.S. Botelho, Variational Convex Analysis, Ph.D. thesis, Virginia Tech, Blacksburg, VA -USA, (2009).
  8. F. Botelho, Topics on Functional Analysis, Calculus of Variations and Duality, Academic Publications, Sofia, (2011).
  9. F. Botelho, Existence of solution for the Ginzburg-Landau system, a related optimal control problem and its computation by the generalized method of lines, Applied Mathematics and Computation, 218, 11976-11989, (2012). [CrossRef]
  10. F. Botelho, Functional Analysis and Applied Optimization in Banach Spaces, Springer Switzerland, 2014.
  11. P.Ciarlet, Mathematical Elasticity, Vol. II – Theory of Plates, North Holland Elsevier (1997).
  12. J.C. Strikwerda, Finite Difference Schemes and Partial Differential Equations, SIAM, second edition (Philadelphia, 2004).
  13. L.D. Landau and E.M. Lifschits, Course of Theoretical Physics, Vol. 5- Statistical Physics, part 1. (Butterworth-Heinemann, Elsevier, reprint 2008).
  14. R.T. Rockafellar, Convex Analysis, Princeton Univ. Press, (1970).
  15. J.J. Telega, On the complementary energy principle in non-linear elasticity. Part I: Von Karman plates and three dimensional solids, C.R. Acad. Sci. Paris, Serie II, 308, 1193-1198; Part II: Linear elastic solid and non-convex boundary condition. Minimax approach, ibid, pp. 1313-1317 (1989).
  16. A.Galka and J.J.Telega Duality and the complementary energy principle for a class of geometrically non-linear structures. Part I. Five parameter shell model; Part II. Anomalous dual variational priciples for compressed elastic beams, Arch. Mech. 47 (1995) 677-698, 699-724.
  17. J.F. Toland, A duality principle for non-convex optimisation and the calculus of variations, Arch. Rat. Mech. Anal., 71, No. 1 (1979), 41-61. [CrossRef]
Figure 1. solution u 0 ( x ) for the case f ( x ) = 0 .
Figure 1. solution u 0 ( x ) for the case f ( x ) = 0 .
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Figure 2. solution u 0 ( x ) for the case f ( x ) = sin ( π x ) / 2 .
Figure 2. solution u 0 ( x ) for the case f ( x ) = sin ( π x ) / 2 .
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Figure 3. solution u 0 ( x ) for the case f ( x ) = 0 .
Figure 3. solution u 0 ( x ) for the case f ( x ) = 0 .
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Figure 4. solution u 0 ( x ) for the case f ( x ) = sin ( π x ) / 2 .
Figure 4. solution u 0 ( x ) for the case f ( x ) = sin ( π x ) / 2 .
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Figure 5. Density t ( x , y ) for the Case A.
Figure 5. Density t ( x , y ) for the Case A.
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Figure 6. Density t ( x , y ) for the Case B.
Figure 6. Density t ( x , y ) for the Case B.
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Figure 7. Solution u ( x ) = v 3 * ( x ) / β for the example 1.
Figure 7. Solution u ( x ) = v 3 * ( x ) / β for the example 1.
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Figure 8. Solution u ( x ) = v 3 * ( x ) / β for the example 2.
Figure 8. Solution u ( x ) = v 3 * ( x ) / β for the example 2.
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Figure 9. Solution u 0 ( x ) for the example A.
Figure 9. Solution u 0 ( x ) for the example A.
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Figure 10. Solution u 0 ( x ) for the example B.
Figure 10. Solution u 0 ( x ) for the example B.
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Figure 11. Solution ϕ N ( x ) for the ω = 1.8 .
Figure 11. Solution ϕ N ( x ) for the ω = 1.8 .
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Figure 12. Solution ϕ S ( x ) for the ω = 1.8 .
Figure 12. Solution ϕ S ( x ) for the ω = 1.8 .
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Figure 13. Solution ϕ N ( x ) for the ω = 1.0 .
Figure 13. Solution ϕ N ( x ) for the ω = 1.0 .
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Figure 14. Solution ϕ S ( x ) for the ω = 1.0 .
Figure 14. Solution ϕ S ( x ) for the ω = 1.0 .
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Figure 15. Solution ϕ u ( x ) for ω = 1 .
Figure 15. Solution ϕ u ( x ) for ω = 1 .
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Figure 16. Solution ϕ v ( x ) for ω = 1 .
Figure 16. Solution ϕ v ( x ) for ω = 1 .
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Figure 17. Solution ϕ u ( x ) for ω = 15 .
Figure 17. Solution ϕ u ( x ) for ω = 15 .
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Figure 18. Solution ϕ v ( x ) for ω = 15 .
Figure 18. Solution ϕ v ( x ) for ω = 15 .
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