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International Journal of Differential Equations
Volume 2013 (2013), Article ID 532987, 13 pages
Analysis of Mixed Elliptic and Parabolic Boundary Layers with Corners
1Department of Mathematics, University of California, Riverside, 900 University Avenue, Riverside, CA 92521, USA
2Ulsan National Institute of Science and Technology, San 194, Banyeon-ri, Eonyang-eup, Ulju Gun, Ulsan 689-798, Republic of Korea
3The Institute for Scientific Computing and Applied Mathematics, Indiana University, 831 East Third Street, Bloomington, IN 47405, USA
Received 27 January 2013; Accepted 1 April 2013
Academic Editor: Norio Yoshida
Copyright © 2013 Gung-Min Gie et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
We study the asymptotic behavior at small diffusivity of the solutions, , to a convection-diffusion equation in a rectangular domain . The diffusive equation is supplemented with a Dirichlet boundary condition, which is smooth along the edges and continuous at the corners. To resolve the discrepancy, on , between and the corresponding limit solution, , we propose asymptotic expansions of at any arbitrary, but fixed, order. In order to manage some singular effects near the four corners of , the so-called elliptic and ordinary corner correctors are added in the asymptotic expansions as well as the parabolic and classical boundary layer functions. Then, performing the energy estimates on the difference of and the proposed expansions, the validity of our asymptotic expansions is established in suitable Sobolev spaces.
We consider a singularly perturbed convection-diffusion equation in a rectangular domain : Here is a small but strictly positive diffusivity parameter, and is a given smooth data with , independent of , for some 's as needed in the analysis below. The function is assumed to be continuous on and smooth on each edge of . Namely, defining the restriction of to the edges of as follows: we assume that If these compatibility conditions were not satisfied, some additional considerations would be necessary, which we do not address here.
In what follows, we study the asymptotic behavior of the solutions to (1) at small diffusivity .
In a very nice related earlier work, , the asymptotic behavior of the solutions of a convection-diffusion equation similar to (1) was discussed. More precisely, in a rectangular domain , the authors considered where , are constants and is a given smooth function in . The function , satisfying the analogue version of (3) in , is assumed to be continuous and piecewise smooth on . By constructing, in , asymptotic expansions of with respect to a small diffusivity , the boundary layers of (4) were analyzed in a systematic way. The validity of their asymptotic expansions was established using the maximum principle.
Using a simple change of variables which maps to , and setting with a suitable , one can transform (4) to (1) where the two diffusivity parameters and , respectively, in (1) and (4) are compatible; that is, is of order one. Hence, via this transformation, our analysis of (1) in this paper is applicable to (4) as well. Our motivations for conducting the present study appear below. In particular we significantly simplify the proofs of  and make the study suitable for more general equations or systems, in particular, those which do not satisfy the maximum principle.
In the boundary layer analysis associated with the convection-diffusion equation (1) (or (4)), one of the most important and difficult points is to resolve any possible singularity near the four corners of the rectangular domain . Towards this end, we simplify and improve the method used in . More precisely, concerning the asymptotic expansion of , we introduce the so-called elliptic boundary layer corrector, appearing in Section 3.2, near the inflow boundary at only, while in , it was used near both the inflow and outflow boundaries at and . This simplification in the construction of the asymptotic expansions is mainly based on an observation that the corner singularities at and (where the flows go out) can be handled by the ordinary corner corrector, appearing in Section 3.4 (which is much easier to analyze than the elliptic corrector). Using the energy estimates rather than the maximum principle as in , we prove the validity of our proposed asymptotic expansions in suitable Sobolev spaces. Here we make use of the Hardy inequality (see, e.g., ) in the estimates. As we said above, our energy estimation approach can be easily extended to some higher order equations or systems which do not admit a maximum principle.
This paper is organized as follows. In Section 2, we introduce a formal expansion of as the sum of the outer and inner expansions. The outer expansion (outside of the boundary layers), which is easy to obtain, appears in Section 2. Then, in Section 3, by performing the boundary layer analysis in a systematic way, we construct the inner expansion (inside the boundary layers). In Section 4, we state and prove the main convergence result, Theorem 9, concerning the difference between and the proposed asymptotic expansion at a given order. In addition, in the appendix, we prove Lemma 1 that contains some delicate pointwise estimates on the parabolic boundary layer correctors introduced in Section 3.1. The study of the elliptic corrector and its approximation also appears in the appendix.
Throughout this paper, we use the notation conventions below.
Notation 1. is a constant depending on the data, but independent of ; here is the fixed (but arbitrary) order of the asymptotic expansion, as it appears in (6).
Notation 2. An . is a function (or a constant) whose norm in all Sobolev spaces (and thus spaces ) is exponentially small with, for each , a bound of the form ,, , depending possibly on .
Notation 3. For a fixed , we define the energy norm of ,
2. Asymptotic Expansions
To study the asymptotic behavior of , solution of (1), we propose an asymptotic expansion of the following type: Here, at each order of , , corresponds to the outer expansion (outside of the boundary layer) of . To balance the discrepancy on the boundary of and of the , , we introduce the correctors , , which will contribute mainly inside of the boundary layer: will be itself the sum of several boundary layer functions as we will see below. The asymptotic expansion (6) is made at order . As we will see below, the expansion itself depends on , but , which is set at the beginning of the study, can be chosen arbitrary large.
To determine the asymptotic expansion (6), we start with the outer expansion for , . Inserting this expansion into (1), we formally find the equations for the : We supplement these equations with the following inflow boundary conditions (see (1)–(3)): While (7) are “natural”, the choice of the boundary conditions in (8) is not obvious; it will be eventually justified by the convergence theorem below. Then, by integrating the equations in , we find the smooth outer solutions in the following form:
Under this construction of the outer expansion, we notice that satisfies the boundary condition (1)2 along the edge only, and not on the three other sides of , , , and (in general). Hence, we expect boundary layers to occur near those edges, and the so-called correctors (corresponding to the ) will be necessary to account for these discrepancies.
In Section 3, performing the boundary layer analysis, we define, for each , the corrector appearing in (11) below. Then, in Section 4, using (6), (9), (10), and (11), we prove our main result which is stated as Theorem 9.
3. Construction of the Correctors: Boundary Layers Analysis
We want the boundary value of to match that of its approximation. In general, the boundary values of the diffusive solution and the outer expansion match only at , but not on the other sides of , , , and . Hence, we expect that some boundary layers will occur near those three edges. To resolve this inconsistency, we will define a number of boundary layer functions on the sides and corners of , following an analysis reminiscent of the theory of the Prandtl boundary layer in [3–6].
For the moment, comparing with a finite sum , we infer from the definition of the in (7)–(10) that the values of these functions coincide on the segment . In general, they will not coincide anywhere else on . First, to correct the inconsistency on the sides , we will define the so-called parabolic correctors . Then, to correct the inconsistency at , we will introduce the (classical) corrector . However, this will not be enough because additional inconsistencies appear at the corners of , and, as we shall see below, it will be necessary to introduce additional correctors , , and to handle these inconsistencies.
In summary, in the subsections below, we will define the in the form, where the role and location of each corrector are explained, respectively, in Box 1 and Figure 1. The stretched variables of the corrector functions, which will be introduced and used in the following subsections, are indicated in the following equation:
3.1. Parabolic Boundary Layers (PBL)
At the bottom (or top) boundary, that is, at (or ), to balance the discrepancy of and the outer expansion , (see the as defined in (9) and (10)), we construct below the parabolic boundary layer correctors , .
We formally insert the asymptotic expansion into (1). Using the arguments similar to those of the Prandtl theory, we see that the thickness of the boundary layer near or should be of order . Then, by collecting the terms at the same order of , , we find the equations of the parabolic boundary layer correctors: where we set .
We will show below how to actually construct . For the moment, comparing the functions and for some , we see that the boundary values of these functions coincide at and . However this has been achieved at the price of introducing some new inconsistencies. Indeed we notice, in (14), that, for each , the boundary conditions at and are not consistent with that at . That is, in general, for any , Due to this inconsistency of the boundary data, if we define , , as a solution of (13) with (14), some derivatives of , get singular at the two corners , . Therefore, to define smooth (smoother) correctors , , we will modify the boundary conditions (14) as introduced in (23).
3.1.1. On Modification of Boundary Conditions for Smooth Correctors at
Equation (13) with initial and boundary conditions (14) is a parabolic problem (heat equation), in which is the (positive) time like variable so that the boundary conditions at are the analogue of the initial conditions for an evolution problem, and the possible inconsistencies in (15) correspond to the (analogue of) the compatibility conditions between the initial and boundary values for a parabolic equation; see [7–9] and the references therein. Due to the lack of consistency at the corners and , the correctors constructed as in (13) and (14) might get singular derivatives at those corners. We will overcome this difficulty by considering some corner functions at and , similar to what is done in [10, 11] or  for the compatibility issue in parabolic problems; see  as well.
Defining as a smooth cut-off function, independent of , such that we set where Note that the , , depend on , but this dependency is not made explicit to make the notations (slightly) simpler. Note also (comparing to (15)) that, at , for each ,
We introduce the stretched variables, Then, using (13), (14), (17), and (20), we define the parabolic corrector, , , as where and (lower and upper parts of , resp.) are defined as the solutions of the 1D heat equations below.
For , Here the , , , are defined by Note that the smooth boundary conditions , , , along or are compatible with the other 0 boundary (initial) conditions at in the sense that, for each ,
3.1.2. Estimates on the Parabolic Boundary Layers
We now state some pointwise estimates for the and , , which are proved in the appendix.
Lemma 1. For each and , one has the following pointwise estimates: for a generic constant independent of , , and .
From Lemma 1, it is easy to deduce the following estimates.
Lemma 2. For each and , one has, for ,
3.2. Elliptic Boundary Layers (EBL)
In Section 3.1, to construct the consistent parabolic boundary layer correctors , , we considered the modified boundary conditions (23), including , instead of the natural boundary conditions (14). Here, on the two sides and of , to cancel which is exactly the difference of (14) and (23), we introduce elliptic boundary layer correctors , , which, like or , depend on the order of the asymptotic expansion in (6).
Using (17), we define where and are the solutions of the elliptic systems below.
For , The systems (33) being elliptic equations, their well-posedness are easy to verify, and hence, we omit the proof here.
The equations satisfied by the elliptic correctors read as follows.
In the error analysis below in Section 4, we will see that no extra terms related to the appear; see (65) below. This is because the , as appearing in (34), satisfies the same equation as for , supplemented with the (exact) boundary conditions that we need. From this observation, as it will be justified in Section 4, we notice that our main result in Theorem 9 does not require any estimate on the .
As an extra information which might be useful elsewhere, but not in this paper, by performing the energy estimate on (34), we find that In the appendix, we introduce an explicit approximate of . Then, thanks to the estimates on , one can obtain some pointwise estimates on as well; see Appendix B.
We will now deal with the side and construct the ordinary boundary layer and the ordinary corner layer functions (correctors) .
3.3. Ordinary Boundary Layers (OBL)
To handle the discrepancy of and at , which is a part of appearing in (36), the so-called ordinary boundary layer corrector is introduced in this section. We insert a formal expansion into the diffusive equation (1). Then, using the stretched variable , we find the equations of : where we set .
The main role of the is, at each order of , to cancel the error at . Hence, we supplement (37) with the boundary conditions The explicit expressions of , , are inductively shown to be of the form where is a polynomial in of degree whose coefficients, independent of , are linear combinations of the , , and .
According to (39), we deduce the following lemmas.
Lemma 3. For each , one has the pointwise estimates: for a constant independent of , , and .
Lemma 4. For each , one has
Thanks to Lemma 3, we notice that the effect of near the boundary is exponentially small:
3.4. Ordinary Corner Layers (OCL)
To account for the value at , which is exactly the difference of and at (see (43)), we introduce the ordinary corner layer correctors , , in the form where the (or ) are the correctors near the corner (or ) as constructed below.
To define (or ), we insert a formal expansion into (1). Then, using the stretched variables and near and using and near , we collect the terms of order , . As a result, we find the equations for (or ): Here, we set for .
At each order of , , to cancel the error near the corner or , we supplement (45) with the boundary conditions
The explicit solutions of (45) and (46), , are inductively found to be of the following form: where is a polynomial in of degree whose coefficients, independent of , are linear combinations of the quantities , . In the same manner, the explicit forms of the , can be found as well.
Lemma 5. For each and , one has the pointwise estimates: for a generic constant independent of , , and .
Lemma 6. For each and , one has, for ,
3.5. Supplementary Correctors
Now, our task is to handle, at each order , the effects of and along the top and bottom boundaries . To this end, using (51), we construct the supplementary correctors in the form where
Lemma 7. For each and , one has the pointwise estimates: for a constant independent of , , and .
Lemma 8. For each and , one has
4. Asymptotic Error Analysis: The Main Result
We define where as defined in (11).
We construct an extension of in the form where Then one can verify that and
Thanks to the elliptic regularity theory and (67), we also find that
Remark 10. Due to the continuity of as appearing in (3), can be omitted in (11) for at order . Then one can verify that which gives a convergence estimate that a factor of is worse than what is stated in (69) for .
A. Proof of Lemma 1
Now, to prove (A.1), we use an induction on .(1) We begin with .
From (25), since for , differentiating in we find that
Since , , we now notice that Integrating by parts in the last integral, we deduce that Hence, for , , using again, we note from (A.5) that thus (A.6) holds for , and this proves (A.1) for , , . Hence, (A.1) is proved for .(2) We now assume that (A.1) holds at any order less than or equal to , and we want to prove it at the order .
At order , we perform the analysis as follows.
We first note that the homogeneous solution of , that is the first integral of (26) for , can be similarly estimated. We just replace by in the above analysis.
Since for , the first integral is then estimated as in (A.1) for . We just replace the above by . We now estimate the particular solution of , that is, the second integral of (26) denoted by . For simplicity in the analysis below, we write that Using the induction assumption at order , from (A.1) for , we note that for , that is, , Thanks to (A.8), differentiating , the second integral of (26), we find that Since , , from (A.9) we find that for , This proves (A.1) for , .
Since , differentiating (A.10) in we observe that where . Here, we note that . Thanks to the induction assumption on , from (A.1) we thus note that for , that is, , and for , that is, , As in (A.11) we similarly find that for , Hence, for , , using the induction assumption at order , from (A.1) we note that for , from (A.18) we also note that Using again we thus find that This proves (A.1) for , , . Hence, the lemma is proved.
B. Study of the Elliptic Corner Correctors
For each , using the stretched variables one can define an approximation of as a solution of the system, The explicit expression of is given as (see )