Abstract
In this article, we consider a singularly perturbed nonlinear reaction-diffusion equation whose solutions display thin boundary layers near the boundary of the domain. We fully analyse the singular behaviours of the solutions at any given order with respect to the small parameter ε, with suitable asymptotic expansions consisting of the outer solutions and of the boundary layer correctors. The systematic treatment of the nonlinear reaction terms at any given order is novel along the singular perturbation analysis. We believe that the analysis can be suitably extended to other nonlinear problems.
1 Introduction
Nonlinear reaction-diffusion equations arise in many areas in systems consisting of interacting components. The equations describe, e.g., chemical reactions, pattern-formation, population dynamics, predator-prey equations, and competition dynamics in biological systems (see, e.g., [7, 11, 12, 31, 32, 33, 39]). One can consider a typical form of systems of reaction-diffusion equations in the form
where
In real applications like a fast reaction system, the magnitude of some coefficients in the diffusion matrix D is relatively small and hence the system can be singularly perturbed.
In this article, for the singular perturbation and boundary layer analysis aimed here, we consider the steady state system of (1.1) and study the following scalar nonlinear singularly perturbed problem which can serve as a guide for more general systems:
Here,
For example,
For small
Another motivation of studying boundary layers is the vanishing viscosity problem in fluid dynamics, see, e.g., [2, 5, 6, 24, 25, 8, 13, 28, 30, 23, 27, 35, 36, 37]. The typical question is on the behaviour of the Navier–Stokes flows at small viscosity, i.e., the limit behaviour or convergence to Euler flows as the viscosity tends to zero. The boundary layers play a crucial role for connecting the Navier–Stokes and Euler flows and they also do so for the singular perturbation analysis in the nonlinear reaction-diffusion equations considered here.
An additional motivation comes from the computational aspects in numerical simulations. Due to the thin boundary layers, the computational meshes are classically refined near the boundary
In what follows, we discuss the problems posed on a channel domain in Section 2 which is relatively easier to handle thanks to the simple geometry of the boundary. In Section 3, we cast the nonlinear reaction-diffusion equations in a general domain. We need to take into account the geometrical properties, like curvature, using the boundary fitted coordinates. Throughout this paper, we systematically handle the nonlinear term g along the singular perturbation analysis at any orders. This nonlinear treatment can apply to other nonlinear problems.
For the analysis below, we shall consider the Sobolev spaces
An exponentially small term, denoted e.s.t., is a function whose norm in all Sobolev spaces
2 Channel domains
For general domains, which will be studied in Section 3, we consider the domains with smooth boundaries. Since the boundary layer correctors act locally in the inward direction normal to the boundaries, transforming the Cartesian coordinate into the so-called boundary fitted one, the boundary layers can be described in channel domains, which are relatively easy to analyse. We thus consider first the simpler case of channel domains, which possess boundary layers only on one side at a flat boundary.
Let us consider the problem in a channel domain as follows:
where
Since g is invertible, we write
To give an idea on how to construct the boundary layers, for now we assume
which, as we will see, reduces the boundary layer at
Thanks to (1.3) and (2.3),
2.1 Boundary layer analysis at order ε 0
We now construct a zeroth order corrector to account for the discrepancy between
Using the stretched variable
However, in general
Although
Lemma 2.1.
The corrector
Proof.
Setting
Multiplying (2.8) by
This implies
We can also deduce some norm estimates.
Lemma 2.2.
There exists a constant
Proof.
The second estimate of (2.9) directly follows from (2.7). To obtain the first estimate, we introduce
where the last inequality follows from the mean value theorem and the
Theorem 2.3.
Assume that (2.4) holds. Then, there exists a constant
Proof.
Let
Multiplying by w and integrating over Ω we find that
Here, the
We can also obtain the lower bound of
Lemma 2.4.
The corrector
where
Proof.
From Lemma 2.1 and (2.3), we note that
Fixing y, we first prove (2.12) for the case
Multiplying by
This implies
Remark 2.5.
Thanks to the estimate for
Furthermore, for
Indeed, from Lemma 2.4 and Theorem 2.3, we find that
2.2 Boundary layer analysis at arbitrary order ε n , n ≥ 0
Outer expansion.
We now consider the higher order outer expansions
Dropping
We identify at the order
We then obtain, e.g.,
More generally, we recursively obtain
To construct the higher order correctors, we assume, for simplicity, that f is infinitely flat at
using the multi-index notation
This implies that the
Thus, we only have boundary layers at
We subtract (2.14) from (2.19) to obtain
We first need to handle the nonlinear term to identify the quantities of order
2.3 Treatment of the nonlinear term g ( u )
In this section, we formally write the nonlinear term
Here, we formally consider
We first observe that
where
using the multi-index notation
and
We similarly find that
where
Hence, we note that
using the notation (2.21).
To arrange the terms at each order
Hence, using the multi-index notations in (2.23), we formally write
For the analysis below, we estimate the truncation error corresponding to the expansion (2.24).
Lemma 2.6.
There exists a constant
where
and the multi-index notations are given in (2.23).
Proof.
We first note that the
Thanks to the multinomial theorem, we observe that
where
On the other hand, we find from Taylor’s theorem that
where
Here,
We now define the boundary layer correctors
Dividing by
we rewrite (2.28) as
and for
We supplement the boundary condition on
Remark 2.7.
We note that the corrector equations for
Lemma 2.8.
The correctors
Proof.
We use the maximum principle to prove the lemma. Let
For
We introduce a barrier function
by the mean value theorem, for some η between
Since
By the boundary conditions of
where
We suppose by induction that for
We then find that
where
We infer from the boundary conditions for
and using the maximum principle we obtain that
where
where
By the boundary condition on
We find from (2.35) and (2.36) that for
by the maximum principle where
To prove (2.31) at order
it suffices to show that for any
To prove this, we note that
and using the factorization
where
We now estimate, for each
Summing (2.28) for
Thanks to Lemma 2.6, this can be written in the form
with
Adding the two above equations (2.41) and (2.42), we find
Subtracting (2.44) and from the first equation in (2.1), we find
We multiply (2.45) by
We hence proved the following convergence theorem.
2.4 Without the assumption (2.17)
If we consider a general smooth function f, i.e., if we remove the assumptions (2.17), we also expect similar boundary layers at
Then, we define the boundary layers
Since the corrector equations for
Here,
where
We now note that
which is an exponentially small term. Then, the convergence analysis similarly follows as in the above, from which we infer the following theorem.
3 General domains
We now return to the case of a general smooth domain, where equation (1.2) is posed:
Here, Ω is a general smooth domain,
The outer solutions
However, the boundary layers appear in the direction normal to the curved boundary. Thus, the boundary fitted coordinates, i.e., the normal and tangential components along the boundary, are necessary to devise the boundary layer correctors. Here, we consider smooth boundaries
We then define the boundary fitted coordinates:
where
3.1 Boundary fitted coordinates
We introduce the local orthogonal coordinate basis
where
Here, we note that differentiating (3.5) implies (3.6).
The curvature
and, by the Frenet–Serret relation,
For the variables
since
The gradient and Laplacian operators are then defined as follows:
where
where
Then, the model equation in (3.1), can be written as
Remark 3.1.
On the unit circle domain, using polar coordinates, we find
3.2 Boundary layer analysis at orders ε 0 and ε 1 2
Unlike the channel domain (2.1), we will need to introduce a corrector
In general, to find appropriate asymptotic expansions for the boundary layers, we preform the following expansions near the boundary
To address the terms at all the orders of ε in the boundary layers, we have to resolve the effect of curvature
By comparing the terms of the same order
We now find two leading order correctors
By the Taylor expansion, dropping smaller terms and using the stretched variable
and from (3.13) at order
These equations are supplemented with the respective boundary conditions, i.e.,
Then, we extend
where
Remark 3.2.
We obtain
Lemma 3.3.
The following pointwise estimate holds for
Furthermore, the derivatives of
Proof.
We first set
which implies
Thanks to (3.16), multiplying (3.20) by
This implies
We now find the estimates for the derivatives as in (3.19). For
Multiplying by
Then, at higher orders l, we use the multi-index
Thanks to the mean value theorem, we observe that
and we can thus inductively prove (3.19) for any
For
Integrating over
where
Then,
and integrating over
Let
and
Let us choose
Thus,
To estimate
Here, from (3.21) with
We similarly derive the pointwise estimate for
Lemma 3.4.
The corrector
Proof.
Let
We repeat the same argument as in the proof of Lemma 3.3. For
We integrate over
where
Let
Following then the same procedure as in the proof of Lemma 3.3 with the boundary conditions (3.16), we can obtain (3.24) for
For
We now find the norm estimate in
Lemma 3.5.
Let
We now introduce the analogue of Theorem 2.3.
Theorem 3.6.
Assume f is a general smooth function and Ω is a general smooth domain.
Then, there exists a positive constant
Proof.
We set
Here, we recall that
thanks to (3.14). Here,
Since
Taking the inner product of (3.3) and (3.1), respectively, with w, we write
From (3.29), (3.30) and (3.31), we find that
Theorem 3.7.
Assume that f is a general smooth function and Ω is a general smooth domain.
Then, there exists a positive constant
Proof.
We define
by (3.14) and by (3.15), where
We note that thanks to the Taylor expansion, we have
where
On the other hand,
by Remark 3.2 and (3.27). We infer from Lemma 3.4, (3.34) and (3.35) that
while
We then find from (3.36) and the mean value theorem that
for some ζ between
which implies
3.3 Boundary layer analysis at arbitrary orders ε n and ε n + 1 2 , n ≥ 0
Similarly as in (2.20), we formally write
Because of the one-dimensional nature of these boundary layers near the boundary in the direction normal to the boundary, we now introduce the boundary fitted coordinates. We transform the Laplacian Δ as in (3.7) and (3.8).
Using the geometric series expansions
we formally write, e.g.,
Then,
Using
we rearrange the terms according to the order of ε and then we find the last expression in (3.39). The
where
We note that when the upper limit and exponents in the expressions of
Lemma 3.8.
There exists a constant
where, for
and the multi-index notations are defined, for
with
We now construct high order boundary layers. From the formal sum (3.37) and Lemma 3.8 with
We then observe that at order
Incorporating (3.39) and (3.40), and from (3.47) at
where the multi-index notation is described in (3.46). On the other hand, at order
The two equations (3.48) and (3.49) are, respectively, supplemented with the boundary conditions
As before, we extend
Multiplying, respectively, (3.14) by
where
Lemma 3.9.
For
Moreover,
Proof.
Using Lemma 3.3 and Lemma 3.4 and the induction on j,
from (3.48) and (3.49), we obtain the estimates (3.19) and (3.25) for
Lemma 3.10.
There exists
where
with
Proof.
Using the Laplacian (3.7) in terms of
where
We now only have to prove that
Noting that
Then, we find
where in the last inequality we used Lemma 3.9.
Note that in (3.42) and (3.43) the sum
We use Lemmas 3.8 and 3.10, and equation (3.50), to find that
where
As before, we define now
Theorem 3.11.
Assume that f is a smooth function, Ω is a general smooth domain and
Proof.
We set
We use the smooth cut-off function
where
where
Here, we used (2.41) which is obtained from summing (3.3).
We finally obtain from the mean value theorem that, for some ζ between
This proves (3.56). From Lemma 3.9, we note that
Funding source: National Science Foundation
Award Identifier / Grant number: DMS 1206438
Award Identifier / Grant number: DMS 1510249
Funding source: National Research Foundation of Korea
Award Identifier / Grant number: 2015K2A1A2070543
Award Identifier / Grant number: 2015R1D1A1A01059837
Funding statement: This work was supported in part by NSF grants DMS 1206438 and 1510249, by a research fund of Indiana University. Chang-Yeol Jung was supported under the framework of international cooperation program managed by the National Research Foundation of Korea (grant no. 2015K2A1A2070543) and supported by the National Research Foundation of Korea grant funded by the Ministry of Education (grant no. 2015R1D1A1A01059837).
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Artikel in diesem Heft
- Frontmatter
- Boundary layer analysis of nonlinear reaction-diffusion equations in a smooth domain
- Existence and asymptotic behavior of ground state solutions of semilinear elliptic system
- A new perspective on the Riesz potential
- Positive solutions of fractional elliptic equation with critical and singular nonlinearity
Artikel in diesem Heft
- Frontmatter
- Boundary layer analysis of nonlinear reaction-diffusion equations in a smooth domain
- Existence and asymptotic behavior of ground state solutions of semilinear elliptic system
- A new perspective on the Riesz potential
- Positive solutions of fractional elliptic equation with critical and singular nonlinearity