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Article

Lower and Upper Solution Method for Semilinear, Quasi-Linear and Quadratic Singularly Perturbed Neumann Boundary Value Problems

Institute of Applied Informatics, Automation and Mechatronics, Slovak University of Technology in Bratislava, Bottova 25, 917 01 Trnava, Slovakia
Axioms 2023, 12(2), 154; https://doi.org/10.3390/axioms12020154
Submission received: 13 January 2023 / Revised: 27 January 2023 / Accepted: 29 January 2023 / Published: 2 February 2023

Abstract

:
In this paper, by using the method of lower and upper solutions and notion of ( I q )-stability, we established sufficient conditions for the uniform convergence of the solutions of singularly perturbed Neumann boundary value problems for second-order differential equations to the solution of their reduced problems.

1. Introduction

Let us consider a Neumann boundary value problem (BVP) for a singularly perturbed second-order ordinary differential equation
ε y = F ( x , y , y ) , a < x < b , 0 < ε 1 ,
in which F is a continuous function on [ a , b ] × R 2 and the solution y ε ( x ) satisfies the boundary condition:
y ε ( a ) = 0 , y ε ( b ) = 0 .
We discuss here three types of boundary value problems that are special cases of the Neumann boundary value problem (1), (2) and the reason why these particular types are considered is explained in the next part of this section. They are:
ε y = f ( x , y ) , ( 2 )
ε y = p ( x , y ) y + q ( x , y ) , ( 2 )
ε y = p ( x , y ) y 2 + q ( x , y ) , ( 2 ) .
The aim of the paper is to establish the sufficient conditions for the existence and uniform convergence of the solutions of the BVPs (3), (4) and (5) to the solution of a reduced problem F ( x , y , y ) = 0 for ε 0 + on the whole interval [ a , b ] , which we obtain by formally putting ε = 0 in (1). At this point, it may be useful to recall that in the case of the Neumann boundary condition, there is a theoretical possibility for uniform convergence on the entire interval [ a , b ] , which is not possible for some types of boundary value problems (Dirichlet boundary condition, for example) and gives rise to phenomena that are typical for singularly perturbed boundary value problems, e.g., the boundary layers at the endpoints of the interval [ a , b ] .
The question whether the system depends continuously on a parameter is vital in the context of applications where measurements are known with some accuracy only. For BVPs in the theory of ordinary differential equations (ODEs), there are some results on the continuous dependence of a solution on a parameter, see, e.g., [1,2,3] and references therein. A standard requirement (among others) is the continuous dependence of the right-hand sides of differential equations on the parameter, whereas for problem (1), this condition is not satisfied a priori because the function ε 1 F ( x , y , z ) is not continuous for ε 0 + on any nonempty open set in [ a , b ] × R 2 .
In this section, we recall some of the main ideas of the a priori estimation method based on the Bernstein–Nagumo condition. Then, in Section 2, we deal with the problem (3), also referred to as semilinear problem in the literature [4]; in the following sections, we study the asymptotic behavior of the solutions for quasi-linear Neumann BVP (4) (Section 3) and quadratic Neumann BVP (5) (Section 4).
The novelty of the results obtained in the paper lies in the exact expression of the residuals, important in approximating the solutions of the Neumann BVPs by solutions of the reduced problem, that is, by solving lower-order differential equations.
A key role for the a priori solution estimation method is played by the Bernstein–Nagumo condition [5,6,7], which guarantees the boundedness of the first derivative of the solution (Lemma 1), allowing the use of Schauder’s fixed-point theorem to prove the existence of the solution of the BVP
y = f ( x , y , y ) , a < x < b , f C ( [ a , b ] × R 2 ) ,
subject to the boundary condition (2) and its lower and upper bounds. In formulating the general and well-known results that we use later, and which are also valid for the regular case, we do not use subscript “ ε ”.
The differential inequality approach of Nagumo is based on the observation that if there exist sufficiently smooth (say, twice continuously differentiable or in short C 2 ) functions α ( x ) and β ( x ) possessing the following properties:
α ( x ) f ( x , α ( x ) , α ( x ) ) , β ( x ) f ( x , β ( x ) , β ( x ) ) for every x [ a , b ] ,
and
α ( a ) 0 , α ( b ) 0 , β ( a ) 0 , β ( b ) 0 ,
then the problem (6), (2) has a solution y = y ( x ) of class C 2 ( [ a , b ] ) such that
α ( x ) y ( x ) β ( x ) for x [ a , b ] ,
provided that f does not grow “too fast” as a function of y . Bernstein showed that a priori bounds for derivatives of solutions to (6) can be obtained once such bounds are found for the solutions themselves, provided that the nonlinearity in f is at most quadratic in y [8,9]:
Definition 1 
(Bernstein–Nagumo condition, [6,7]). We say that the function f satisfies a Bernstein–Nagumo condition if for each M > 0 , there exists a continuous function h M : [ 0 , ) [ a M , ) with a M > 0 and
s d s h M ( s ) = +
such that for all y , | y | M , all x [ a , b ] and all z R
| f ( x , y , z ) | h M ( | z | ) .
Lemma 1 
([6,7], p. 428). Let f satisfies a Bernstein–Nagumo condition. Let y ( x ) be any solution of (6) on [ a , b ] satisfying the condition | y ( x ) | M , a x b . Then, there exists a number N > 0 depending only on M and h M such that | y ( x ) | N on [ a , b ] . More exactly, N can be taken as the root of the equation
2 M / ( b a ) N s d s h M ( s ) = 2 M .
Remark 1. 
The most common type of Bernstein–Nagumo condition is the following:
f ( x , y , z ) = O ( | z | 2 ) as | z | for all ( x , y ) in [ a , b ] × [ α , β ] ,
and it is obvious that the functions from the right-hand side of differential equations for the problems (3)–(5) satisfy this condition.
Theorem 1. 
If α ( x ) , β ( x ) are lower and upper solutions for the BVP (6), (2) such that α ( x ) β ( x ) on [ a , b ] and f satisfies a Bernstein–Nagumo condition, then there exists a solution y ( x ) C 2 ( [ a , b ] ) of (6), (2) with
α ( x ) y ( x ) β ( x ) , a x b .
The proof of this theorem is a direct adaptation of the proofs carried out in [9,10,11], so we omit them.
Remark 2. 
In the literature, the Neumann boundary condition of the form y ( a ) = A , y ( b ) = B with A , B R is sometimes considered [12,13,14,15], for which the analogous statement as in Theorem 1 holds, replacing the boundary conditions (8) by
β ( a ) A α ( a ) , α ( b ) B β ( b ) ,
but we deal with the more commonly used homogeneous form of the Neumann boundary condition, where A = B = 0 .
In the following definition of stability for the solution y = u ( x ) of the reduced problem F ( x , y , y ) = 0 , we assume that the function h ( x , y ) F ( x , y , u ( x ) ) has the stated number of continuous partial derivatives with respect to y in
D δ ( u ) { ( x , y ) R 2 : a x b , | y u ( x ) | δ } , δ > 0 .
Further, define the sets
D δ , δ 1 , a ( u ) { ( x , y ) R 2 : a x a + δ 1 , y R } D δ ( u ) ,
D δ , δ 1 , b ( u ) { ( x , y ) R 2 : b δ 1 x b , y R } D δ ( u ) ,
where 0 < δ 1 b a .
Definition 2 
([4]). Let q 0 be an integer. The solution y = u ( x ) of the reduced problem is said to be ( I q )-stable in [ a , b ] if there exist positive constants m and δ such that
j h ( x , u ( x ) ) y j j h ( x , y ) y j y = u ( x ) 0 for a x b and j = 0 , 1 , , 2 q ,
and
2 q + 1 h ( x , y ) y 2 q + 1 m > 0 in D δ ( u ) .
To prove the main results of this paper, we need the following two technical results:
Lemma 2. 
Let q 0 be an integer. Let v ε be a solution of the nonhomogeneous Neumann BVP
ε v ε = m ( 2 q + 1 ) ! v ε 2 q + 1 , v ε ( a ) = | u ( a ) | , v ε ( b ) = | u ( b ) | .
Then, the solution v ε ( x ) of the BVP (9) is unique and for q = 0 , the BVP (9) is solvable explicitly, v ε ( x ) = v 1 , ε ( x ) + v 2 , ε ( x ) , where
v 1 , ε ( x ) = | u ( a ) | exp [ m ε ( b x ) ] + exp [ m ε ( x b ) ] m ε exp [ m ε ( b a ) ] exp [ m ε ( a b ) ] = O ε 1 2
( v 1 , ε ( a ) = | u ( a ) | , v 1 , ε ( b ) = 0 )
and
v 2 , ε ( x ) = | u ( b ) | exp [ m ε ( x a ) ] + exp [ m ε ( a x ) ] m ε exp [ m ε ( b a ) ] exp [ m ε ( a b ) ] = O ε 1 2
( v 2 , ε ( a ) = 0 , v 2 , ε ( b ) = | u ( b ) | )
on [ a , b ] as ε 0 + ; for q 1 , the solution of BVP (9) satisfies on [ a , b ] the inequality
0 v ε ( x ) φ 1 , ε ( x ) + φ 2 , ε ( x ) , ε ( 0 , ε Δ ] ,
where
φ 1 , ε ( x ) = | u ( a ) | + Δ σ q q + 1 + σ q ( x a ) 1 q = O σ 1 q for x > a O σ 1 q + 1 for x = a
φ 2 , ε ( x ) = | u ( b ) | + Δ σ q q + 1 + σ q ( b x ) 1 q = O σ 1 q for x < b O σ 1 q + 1 for x = b
as σ , and
σ = m ε ( 2 q + 1 ) ! ( q + 1 ) 1 2 ,
and Δ > 0 is a constant. In summary,
φ 1 , ε ( x ) + φ 2 , ε ( x ) = O ε 1 2 q for a < x < b O ε 1 2 q + 2 for x = a or x = b
as ε 0 + . The value of ε Δ is specified later in the proof.
Proof. 
The case q = 0 has already been analyzed in [16], and therefore we concentrate on the much more complicated case where q 1 , which cannot be solved explicitly. We apply the method of lower and upper solutions for a nonhomogeneous Neumann BVP (9). Define the lower and upper solutions
α ε ( x ) = 0 , β ε ( x ) = φ 1 , ε ( x ) + φ 2 , ε ( x ) ,
where φ i , ε ( x ) , i = 1 , 2 , are the solutions of an initial and final value problem, respectively,
ε φ 1 , ε = m ( 2 q + 1 ) ! φ 1 , ε 2 q + 1 , φ 1 , ε ( a ) = | u ( a ) | + Δ σ 1 q + 1 , φ 1 , ε ( a ) = | u ( a ) | Δ
and
ε φ 2 , ε = m ( 2 q + 1 ) ! φ 2 , ε 2 q + 1 , φ 2 , ε ( b ) = | u ( b ) | + Δ σ 1 q + 1 , φ 2 , ε ( b ) = | u ( b ) | + Δ ,
where Δ > 0 is a constant. Using the standard procedure for second-order equations with the independent variable missing, the solution of the differential equation for φ i , ε ( x ) must satisfy the identity
φ i , ε = ± σ 2 φ i , ε 2 q + 2 + c 1 , i = 1 , 2 ,
and hence, for the initial value problem (10) (the sign “−”)
σ 2 φ 1 , ε 2 q + 2 + c 1 1 2 d φ 1 , ε = x + c 2 , c 1 , c 2 R .
The integral is an elementary function only if c 1 = 0 , and the solution for this choice c 1 is φ 1 , ε ( x ) . This solution decreases to the right.
For (11), we proceed analogously, with the sign “+”,
σ 2 φ 2 , ε 2 q + 2 + c 1 1 2 d φ 2 , ε = x + c 2 , c 1 , c 2 R
and obtain φ 2 , ε ( x ) . It decreases to the left.
The requirements for the bounds α and β that guarantee the existence of a solution for the BVP (9) between α and β are as follows:
α ε ( x ) m ( 2 q + 1 ) ! α ε 2 q + 1 ( x ) , β ε ( x ) m ( 2 q + 1 ) ! β ε 2 q + 1 ( x )
for every x [ a , b ] and
β ε ( a ) | u ( a ) | α ε ( a ) , α ε ( b ) | u ( b ) | β ε ( b ) .
Since φ 1 , ε and φ 2 , ε are positive functions, we have
m ( 2 q + 1 ) ! β ε 2 q + 1 ( x ) β ε ( x ) = m ( 2 q + 1 ) ! ( φ 1 , ε ( x ) + φ 2 , ε ( x ) ) 2 q + 1 ( φ 1 , ε ( x ) + φ 2 , ε ( x ) )
m ( 2 q + 1 ) ! φ 1 , ε ( x ) 2 q + 1 + m ( 2 q + 1 ) ! φ 2 , ε ( x ) 2 q + 1 φ 1 , ε ( x ) φ 2 , ε ( x ) = 0 .
Now, taking into account that
φ 1 , ε ( b ) 0 and φ 2 , ε ( a ) 0 +
as ε 0 + , we have
β ε ( a ) = φ 1 , ε ( a ) + φ 2 , ε ( a ) = | u ( a ) | Δ + φ 2 , ε ( a ) | u ( a ) |
and
β ε ( b ) = φ 1 , ε ( b ) + φ 2 , ε ( b ) = φ 1 , ε ( b ) + | u ( b ) | + Δ | u ( b ) | ,
for every sufficiently small ε such that φ 2 , ε ( a ) Δ , and at the same time, φ 1 , ε ( b ) Δ , say, for ε ( 0 , ε Δ ] .
The uniqueness of the solution follows from the monotonicity of the function on the right-hand side of the differential equation in (9) in the variable v and is a consequence of Peano’s phenomenon [11]. Lemma 2 is proved. □
For illustration purpose, the asymptotics of the function v ε ( x ) for arbitrarily chosen values is provided in Figure 1.
In proving Theorems 3 and 4, we need the following statement about the uniform convergence of a sequence of convex functions and its derivative, which is a consequence of the theory of convex functions developed in [17,18]:
Lemma 3. 
Let f n ( x ) C 2 ( [ a , b ] ) ( n N ) be convex functions on [ a , b ] such that lim n f n ( x ) = 0 . Then, { f n ( x ) } n N converges uniformly to 0 on every closed interval I ( a , b ) .
Proof. 
It is known ([17], Lemma 1) that under the assumptions of the lemma, the sequence { f n ( x ) } n N converges point-wise to 0 for a < x < b . The convexity of the functions f n ( x ) ( n N ) implies that each f n ( x ) is non-decreasing and | f n ( x ) | | f n ( x 0 ) | on I, where x 0 is the right end-point of the interval I and thus, the convergence of { f n ( x ) } n N to 0 on I is uniform. □

2. Semilinear Singularly Perturbed Neumann Problem

We consider the semilinear Neumann BVP (3), namely
ε y = f ( x , y ) , a < x < b , 0 < ε 1 , y ε ( a ) = 0 , y ε ( b ) = 0 .
Theorem 2. 
Assume that the reduced problem f ( x , y ) = 0 has an ( I q )-stable solution y = u ( x ) of class C 2 ( [ a , b ] ) . Then, there exists ε 0 such that for every ε ( 0 , ε 0 ] the BVP (3) has a solution y = y ε ( x ) C 2 ( [ a , b ] ) , which, on the interval [ a , b ] , satisfies
y ε ( x ) u ( x ) v ε ( x ) + C ε 1 2 q + 1 ,
where v ε is a solution of the nonhomogeneous Neumann BVP
ε v = m ( 2 q + 1 ) ! v 2 q + 1 , v ε ( a ) = | u ( a ) | , v ε ( b ) = | u ( b ) |
and
C = γ m 1 2 q + 1 , γ max x [ a , b ] | u ( x ) | ( 2 q + 1 ) !
Proof. 
The theorem follows from Theorem 1 of the previous section, if we can exhibit, by construction, the existence of the lower and the upper bounding functions α ε ( x ) and β ε ( x ) with the required properties.
We now define, for x in [ a , b ] and ε > 0 , the functions
α ε ( x ) = u ( x ) v ε ( x ) Γ ( ε ) , β ε ( x ) = u ( x ) + v ε ( x ) + Γ ( ε ) .
Here, Γ ( ε ) = ε γ / m 1 2 q + 1 , where γ is a positive constant which is specified later.
It is easy to verify that the functions α , β have the following properties: α β on the interval [ a , b ] and they satisfy the boundary conditions required for upper and lower solutions for the BVP (3). Now, it remains to prove that ε α ε ( x ) f ( x , α ε ( x ) ) and ε β ε ( x ) f ( x , β ε ( x ) ) . We treat the case where u ( x ) is ( I q )-stable and consider α ε ( x ) .
From Taylor’s theorem and the hypothesis that u ( x ) is ( I q )-stable, we have
f ( x , α ε ( x ) ) = f ( x , α ε ( x ) ) f ( x , u ( x ) )
= i = 1 2 q 1 i ! i f ( x , u ( x ) ) y i [ α ε ( x ) u ( x ) ] i 1 ( 2 q + 1 ) ! 2 q + 1 f ( x , ξ ε ( x ) ) y 2 q + 1 [ v ε ( x ) + Γ ( ε ) ] 2 q + 1
= 1 ( 2 q + 1 ) ! 2 q + 1 f ( x , ξ ε ( x ) ) y 2 q + 1 [ v ε ( x ) + Γ ( ε ) ] 2 q + 1 ,
where ( x , ξ ε ( x ) ) is a point between ( x , α ε ( x ) ) and ( x , u ( x ) ) ; ( x , ξ ε ( x ) ) D δ ( u ) for a sufficiently small ε , say, for ε ( 0 , ε L ] . Since v ε and Γ are positive functions, we have
f ( x , α ε ( x ) ) m ( 2 q + 1 ) ! [ v ε 2 q + 1 ( x ) + Γ 2 q + 1 ( ε ) ]
and so
ε α ε ( x ) f ( x , α ε ( x ) ) ε u ( x ) v ε ( x ) + m ( 2 q + 1 ) ! [ v ε 2 q + 1 ( x ) + Γ 2 q + 1 ( ε ) ]
ε | u ( x ) | + ε γ ( 2 q + 1 ) !
for every x [ a , b ] . If we choose a constant γ such that γ | u ( x ) | ( 2 q + 1 ) ! , x [ a , b ] , then ε α ε ( x ) f ( x , α ε ( x ) ) .
The verification for β ε ( x ) follows by symmetry. In detail, we have
f ( x , β ε ( x ) ) = f ( x , β ε ( x ) ) f ( x , u ( x ) )
= i = 1 2 q 1 i ! i f ( x , u ( x ) ) y i [ β ε ( x ) u ( x ) ] i + 1 ( 2 q + 1 ) ! 2 q + 1 f ( x , ϑ ε ( x ) ) y 2 q + 1 [ v ε ( x ) + Γ ( ε ) ] 2 q + 1
= 1 ( 2 q + 1 ) ! 2 q + 1 f ( x , ϑ ε ( x ) ) y 2 q + 1 [ v ε ( x ) + Γ ( ε ) ] 2 q + 1 ,
where ( x , ϑ ε ( x ) ) is a point between ( x , u ( x ) ) and ( x , β ε ( x ) ) and ( x , ϑ ε ( x ) ) D δ ( u ) for sufficiently small ε , say, for ε ( 0 , ε U ] . Then
f ( x , β ε ( x ) ) ε β ε ( x ) m ( 2 q + 1 ) ! [ v ε 2 q + 1 ( x ) + Γ 2 q + 1 ( ε ) ] ε u ( x ) v ε ( x )
ε γ ( 2 q + 1 ) ! ε | u ( x ) | .
The end of the proof is now the same as in the case of the lower bound α ε ( x ) . The inequalities for α and β hold simultaneously if the parameter ε is from the interval ( 0 , ε 0 ] , where ε 0 = min { ε L , ε U } . The theorem is proved. □
Remark 3. 
Lemma 2 implies that under the assumptions of Theorem 2, the solutions y ε ( x ) of semilinear Neumann BVP (3) converge uniformly on the interval [ a , b ] to the solution y = u ( x ) of the reduced problem f ( x , y ) = 0 as ε 0 + .
Example 1. 
Let us consider the semilinear problem
ε y = [ y sin 4 π x ] 2 q + 1 , 0 < x < 1 , q 1 , y ε ( 0 ) = y ε ( 1 ) = 0 .
On the basis of Definition 2, the solution of the reduced problem, u ( x ) = sin 4 π x , is ( I q )-stable and Theorem 2 implies for every ε sufficiently small the existence of solutions which uniformly converge to the solution of the reduced problem. Figure 2 and Figure 3 document this convergence and also confirm the claim of Theorem 2 that as q increases, this convergence slows down.

3. Quasi-linear Singularly Perturbed Neumann Problem

We consider now the singularly perturbed quasi-linear Neumann problem (4),
ε y = p ( x , y ) y + q ( x , y ) , a < x < b , 0 < ε 1 , y ε ( a ) = 0 , y ε ( b ) = 0 .
Theorem 3. 
Assume that the reduced problem p ( x , y ) y + q ( x , y ) = 0 has an ( I q )-stable solution y = u ( x ) of class C 2 ( [ a , b ] ) . Let, for some δ 1 ,
  • p ( x , y ) 0 for every ( x , y ) D δ , δ 1 , a ( u ) if u ( a ) 0 ; and
  • p ( x , y ) 0 for every ( x , y ) D δ , δ 1 , b ( u ) if u ( b ) 0 .
Then, there exists ε 0 such that for every ε ( 0 , ε 0 ] , the BVP (4) has a solution y = y ε ( x ) C 2 ( [ a , b ] ) , which, on the interval [ a , b ] , satisfies
y ε ( x ) u ( x ) v ε ( x ) + C ε 1 2 q + 1 ,
where v ε is a solution of the nonhomogeneous Neumann BVP
ε v = m ( 2 q + 1 ) ! v 2 q + 1 , v ε ( a ) = | u ( a ) | , v ε ( b ) = | u ( b ) |
and
C = γ m 1 2 q + 1 , γ C 1 + max x [ a , b ] | u ( x ) | ( 2 q + 1 ) ! ,
where C 1 is a positive constant which is specified later.
Proof. 
Define for x in [ a , b ] and ε > 0 the functions
α ε ( x ) = u ( x ) v ε ( x ) Γ ( ε ) , β ε ( x ) = u ( x ) + v ε ( x ) + Γ ( ε ) , Γ ( ε ) = ε γ / m 1 2 q + 1 .
It is easy to check that α β and that α , β satisfy the boundary conditions required for upper and lower solutions for the BVP (4). From Taylor’s theorem and the ( I q )-stability of the solution of the reduced problem u ( x ) , we have
ε α ε ( x ) F ( x , α ε ( x ) , α ε ( x ) ) = ε α ε ( x ) F ( x , α ε ( x ) , α ε ( x ) ) F ( x , u ( x ) , u ( x ) )
= ε α ε ( x ) ( F ( x , α ε ( x ) , u ( x ) ) F ( x , u ( x ) , u ( x ) ) ) + ( F ( x , α ε ( x ) , α ε ( x ) ) F ( x , α ε ( x ) , u ( x ) ) )
= ε α ε ( x ) + 1 ( 2 q + 1 ) ! 2 q + 1 h ( x , ξ ε ( x ) ) y 2 q + 1 [ v ε ( x ) + Γ ( ε ) ] 2 q + 1 p ( x , α ε ( x ) ) ( α ε ( x ) u ( x ) )
ε u ( x ) ε v ε ( x ) + m ( 2 q + 1 ) ! [ v ε 2 q + 1 ( x ) + Γ 2 q + 1 ( ε ) ] + p ( x , α ε ( x ) ) v ε ( x )
ε | u ( x ) | + ε γ ( 2 q + 1 ) ! + p ( x , α ε ( x ) ) v ε ( x ) ,
and
F ( x , β ε ( x ) , β ε ( x ) ) ε β ε ( x ) ε | u ( x ) | + ε γ ( 2 q + 1 ) ! + p ( x , β ε ( x ) ) v ε ( x ) .
Combining Lemma 2, Lemma 3 and the assumptions of the theorem, there exist positive constants δ ˜ and C 1 such that
p ( x , α ε ( x ) ) v ε ( x ) 0 and p ( x , β ε ( x ) ) v ε ( x ) 0
on the interval [ a , a + δ ˜ ] [ b δ ˜ , b ] and
| p ( x , α ε ( x ) ) v ε ( x ) | C 1 ε and | p ( x , β ε ( x ) ) v ε ( x ) | C 1 ε
on the interval [ a + δ ˜ , b δ ˜ ] for ε ( 0 , ε 0 ] , so the inequalities
ε α ε ( x ) p ( x , α ε ( x ) ) α ε ( x ) + q ( x , α ε ( x ) )
and
ε β ε ( x ) p ( x , β ε ( x ) ) β ε ( x ) + q ( x , β ε ( x ) )
hold. The conclusion of the theorem now follows from Theorem 1. □
Example 2. 
Let us consider the quasi-linear problem
ε y = y y x 1 2 , 0 < x < 1 , y ε ( 0 ) = y ε ( 1 ) = 0
The general solution of the reduced problem is u 2 = x 2 x + k , k R ; however, only y = u ( x ) = x 1 / 2 satisfies the assumptions asked on the solution of the reduced problem. On the basis of Theorem 3, there exists ε 0 such that for every ε ( 0 , ε 0 ] , the problem has a solution satisfying | y ε ( x ) ( x 1 / 2 ) | v ε ( x ) + C 1 ε on [ 0 , 1 ] .  Figure 4 and Figure 5 show the convergence of the solutions to the solution of the reduced problem.

4. Quadratic Singularly Perturbed Neumann Problem

In this section, we investigate the asymptotic behavior of the solutions of the Neumann boundary value problem (5),
ε y = p ( x , y ) y 2 + q ( x , y ) , a < x < b , 0 < ε 1 , y ε ( a ) = 0 , y ε ( b ) = 0 .
The novelty here is the presence of the quadratic term in y . The more general differential equation
ε y = p ( x , y ) y 2 + g ( x , y ) y + q ( x , y )
is not analyzed here, since it can be reduced to the form presented in (5) in some cases, by the usual device of completing the square. The decision to study the simpler equation rather than the more general equation stems from a desire to present a representative result for this “quadratic” class of problems without having to deal with extra complexities in notation.
Theorem 4. 
Assume that the reduced problem p ( x , y ) y 2 + q ( x , y ) = 0 has an ( I q )-stable solution y = u ( x ) of class C 2 ( [ a , b ] ) . Let, for some δ 1 ,
  • p ( x , y ) 0 ( p ( x , y ) 0 ) for every ( x , y ) D δ , δ 1 , a ( u ) if u ( a ) > 0 ( u ( a ) < 0 ); and
  • p ( x , y ) 0 ( p ( x , y ) 0 ) for every ( x , y ) D δ , δ 1 , b ( u ) if u ( b ) < 0 ( u ( b ) > 0 ).
Then, there exists ε 0 such that for every ε ( 0 , ε 0 ] the BVP (5) has a solution y = y ε ( x ) C 2 ( [ a , b ] ) , which, on the interval [ a , b ] , satisfies
| y ε ( x ) u ( x ) | v ε ( x ) + C ε 1 2 q + 1 ,
where v ε is a solution of the nonhomogeneous Neumann BVP
ε v = m ( 2 q + 1 ) ! v 2 q + 1 , v ε ( a ) = | u ( a ) | , v ε ( b ) = | u ( b ) |
and
C = γ m 1 2 q + 1 , γ C 2 + max x [ a , b ] | u ( x ) | ( 2 q + 1 ) ! ,
where C 2 is a positive constant which is specified later.
Proof. 
The idea of the proof is basically the same as in the proof of the previous theorem, so we focus only on its main points. For the functions
α ε ( x ) = u ( x ) v ε ( x ) Γ ( ε ) , β ε ( x ) = u ( x ) + v ε ( x ) + Γ ( ε ) , Γ ( ε ) = ε γ / m 1 2 q + 1 ,
we obtain the inequalities
ε α ε ( x ) F ( x , α ε ( x ) , α ε ( x ) ) ε | u ( x ) | + ε γ ( 2 q + 1 ) ! + p ( x , α ε ( x ) ) v ε ( x ) ( 2 u ( x ) v ε ( x ) )
and
F ( x , β ε ( x ) , β ε ( x ) ) ε β ε ( x ) ε | u ( x ) | + ε γ ( 2 q + 1 ) ! + p ( x , β ε ( x ) ) v ε ( x ) ( 2 u ( x ) v ε ( x ) ) .
Similar to the proof of the previous theorem, we get that
p ( x , α ε ( x ) ) v ε ( x ) ( 2 u ( x ) v ε ( x ) ) 0 and p ( x , β ε ( x ) ) v ε ( x ) ( 2 u ( x ) v ε ( x ) ) 0
on the interval [ a , a + δ ^ ] [ b δ ^ , b ] and
| p ( x , α ε ( x ) ) v ε ( x ) ( 2 u ( x ) v ε ( x ) ) | C 2 ε and | p ( x , β ε ( x ) ) v ε ( x ) ( 2 u ( x ) v ε ( x ) ) | C 2 ε
on the interval [ a + δ ^ , b δ ^ ] for ε ( 0 , ε 0 ] , a sufficiently small δ ^ > 0 and a suitable positive constant C 2 . Therefore, for γ C 2 + max x [ a , b ] | u ( x ) | ( 2 q + 1 ) ! , we have
ε α ε ( x ) p ( x , α ε ( x ) ) α ε 2 ( x ) + q ( x , α ε ( x ) )
and
ε β ε ( x ) p ( x , β ε ( x ) ) β ε 2 ( x ) + q ( x , β ε ( x ) )
on the interval [ a , b ] . Theorem 4 is proved. □
Example 3. 
For the quadratic problem
ε y = y y 2 ( x + 1 ) , 2 < x < 1 , y ε ( 2 ) = y ε ( 1 ) = 0
from the infinitely many solutions y = u ( x ) = [ ± ( x + 1 ) 3 / 2 + c ] 2 / 3 , c R of the reduced problem y y 2 ( x + 1 ) = 0 , only y = u ( x ) = x + 1 satisfies the requirements from Theorem 4. This can also be deduced from the fact that the function F ( x , y , z ) = y z 2 ( x + 1 ) is nondecreasing as a function of y for all ( x , z ) [ a , b ] × R and hence any two solutions of the Neumann problem (for a fixed ε) will differ only by a constant (Peano’s phenomenon [11]), and hence also in the limit for ε going to 0, the functions y = u 1 ( x ) and y = u 2 ( x ) will differ only by a constant, which is not possible from the form of the general solution of the reduced problem. Figure 6 and Figure 7 show the convergence of the solutions as implied by Theorem 4.

5. Conclusions

In this paper, we were concerned with establishing conditions guaranteeing the existence and uniform convergence of solutions of three types of Neumann boundary value problems, namely (3), (4) and (5). The analytical results in Theorem 2, Theorem 3 and Theorem 4, where, using the notion of the ( I q )-stability of the solution of the reduced problem, the uniform convergence of the solutions to the solution of the reduced problem on the interval [ a , b ] was proved.
Future research could focus on noninteger values of q in the definition of the ( I q )-stability (Definition 2) but such that ( Λ ) q = Λ q holds.

Funding

This publication has been published with the support of the Ministry of Education, Science, Research and Sport of the Slovak Republic within project VEGA 1/0193/22 “ Návrh identifikácie a systému monitorovania parametrov výrobných zariadení pre potreby prediktívnej údržby v súlade s konceptom Industry 4.0 s využitím technológií Industrial IoT ” and the Operational Program Integrated Infrastructure within project “ Výskum v sieti SANET a možnosti jej d’alšieho využitia a rozvoja ”, code ITMS 313011W988, cofinanced by the ERDF.

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Acknowledgments

The author thanks the editors and five anonymous reviewers for their helpful feedback on earlier versions of this paper.

Conflicts of Interest

The author declares no conflict of interest.

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Figure 1. Solution v ε ( x ) of BVP (9) with q = 1 , m = 2 , | u ( a ) | = 1 , | u ( b ) | = 2 and ε = 10 7 (left) and ε = 10 10 (right). These functions reach their local minimum at a point asymptotically approaching 1 / 2 .
Figure 1. Solution v ε ( x ) of BVP (9) with q = 1 , m = 2 , | u ( a ) | = 1 , | u ( b ) | = 2 and ε = 10 7 (left) and ε = 10 10 (right). These functions reach their local minimum at a point asymptotically approaching 1 / 2 .
Axioms 12 00154 g001
Figure 2. Solution of the semilinear Neumann problem (12) for q = 1 and ε = 10 3 (left) and ε = 10 5 (right). The dashed line shows the function u ( x ) = sin 4 π x , the solution of the reduced problem.
Figure 2. Solution of the semilinear Neumann problem (12) for q = 1 and ε = 10 3 (left) and ε = 10 5 (right). The dashed line shows the function u ( x ) = sin 4 π x , the solution of the reduced problem.
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Figure 3. Solution of the semilinear Neumann problem (12) for q = 3 and ε = 10 3 (left) and ε = 10 5 (right). The dashed line shows the function u ( x ) = sin 4 π x , the solution of the reduced problem.
Figure 3. Solution of the semilinear Neumann problem (12) for q = 3 and ε = 10 3 (left) and ε = 10 5 (right). The dashed line shows the function u ( x ) = sin 4 π x , the solution of the reduced problem.
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Figure 4. Solution of the quasi-linear Neumann problem (13) with ε = 0.1 (left) and ε = 0.05 (right).
Figure 4. Solution of the quasi-linear Neumann problem (13) with ε = 0.1 (left) and ε = 0.05 (right).
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Figure 5. Solution of the quasi-linear Neumann problem (13) with ε = 0.01 .
Figure 5. Solution of the quasi-linear Neumann problem (13) with ε = 0.01 .
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Figure 6. Solution of the quadratic Neumann problem (14) with ε = 0.75 (left) and ε = 0.5 (right).
Figure 6. Solution of the quadratic Neumann problem (14) with ε = 0.75 (left) and ε = 0.5 (right).
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Figure 7. Solution of the quadratic Neumann problem (14) with ε = 0.1 .
Figure 7. Solution of the quadratic Neumann problem (14) with ε = 0.1 .
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Vrabel, R. Lower and Upper Solution Method for Semilinear, Quasi-Linear and Quadratic Singularly Perturbed Neumann Boundary Value Problems. Axioms 2023, 12, 154. https://doi.org/10.3390/axioms12020154

AMA Style

Vrabel R. Lower and Upper Solution Method for Semilinear, Quasi-Linear and Quadratic Singularly Perturbed Neumann Boundary Value Problems. Axioms. 2023; 12(2):154. https://doi.org/10.3390/axioms12020154

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Vrabel, Robert. 2023. "Lower and Upper Solution Method for Semilinear, Quasi-Linear and Quadratic Singularly Perturbed Neumann Boundary Value Problems" Axioms 12, no. 2: 154. https://doi.org/10.3390/axioms12020154

APA Style

Vrabel, R. (2023). Lower and Upper Solution Method for Semilinear, Quasi-Linear and Quadratic Singularly Perturbed Neumann Boundary Value Problems. Axioms, 12(2), 154. https://doi.org/10.3390/axioms12020154

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