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Proceedings. Mathematical, Physical, and Engineering Sciences logoLink to Proceedings. Mathematical, Physical, and Engineering Sciences
. 2021 Jan 27;477(2245):20200668. doi: 10.1098/rspa.2020.0668

A stable, unified model for resonant Faraday cages

B Delourme 1,, E Lunéville 2, J-J Marigo 3, A Maurel 4, J-F Mercier 2, K Pham 5
PMCID: PMC7897637  PMID: 33642929

Abstract

We study some effective transmission conditions able to reproduce the effect of a periodic array of Dirichlet wires on wave propagation, in particular when the array delimits an acoustic Faraday cage able to resonate. In the study of Hewett & Hewitt (2016 Proc. R. Soc. A 472, 20160062 (doi:10.1098/rspa.2016.0062)) different transmission conditions emerge from the asymptotic analysis whose validity depends on the frequency, specifically the distance to a resonance frequency of the cage. In practice, dealing with such conditions is difficult, especially if the problem is set in the time domain. In the present study, we demonstrate the validity of a simpler unified model derived in Marigo & Maurel (2016 Proc. R. Soc. A 472, 20160068 (doi:10.1098/rspa.2016.0068)), where unified means valid whatever the distance to the resonance frequencies. The effectiveness of the model is discussed in the harmonic regime owing to explicit solutions. It is also exemplified in the time domain, where a formulation guaranteeing the stability of the numerical scheme has been implemented.

Keywords: asymptotic analysis, high-order homogenization, homogenized boundary conditions, thin periodic interface

1. Introduction

A Faraday’s cage is a cavity whose metallic boundary acts as a shield against external electrical discharges. When this boundary is punctured the shielding is not perfect anymore. Originally set in the static case, Faraday cage structures have been studied in electromagnetism for applications in filtering and shielding by gratings and grids. In this context, the question of the radiation leakage, for instance from microwave oven doors, has been addressed theoretically [13] and experimentally [4]. More recently, the problem has been revisited and extended to the acoustic case, i.e. governed by the Helmholtz equation [57], and to the electromagnetic case, i.e. governed by Maxwell’s equations [8]. The aim is to evaluate the effectiveness of the shielding when waves propagate outside a cage made of a periodic arrangement of wires; in two dimensions, the distance between the wires is h and their typical extent is e. The low-frequency regime is considered, i.e. kh = O(ε) and ε ≪ 1, where k is the typical wavenumber imposed by the source. In addition, in most of these studies, the thin wire approximation is used, which means that e/h ≪ 1; hence, the shielding is controlled by the number N of wires per unit length. Martin [5] derived explicit solutions using multiple scattering theory for N point-like wires evenly distributed on a line (not a cage) or on a large circle (a cage) [5]. For a cage, Hewett and co-authors showed that the asymptotic limit of large N results in a continuum model involving homogenized transmission conditions across an effective interface [6,7]. For thin wires, these conditions are derived using the specific scaling (e/h) = O(e−(c/ε)) for every c > 0, introduced in [9] for thin Dirichlet fibres in a large volume. This scaling allows the coupling between the two sides of the array to be captured in the limit problem, that is, the zero-order problem provided by the asymptotic analysis. This is a key point in the present context. Indeed, for thick wires with (e/h) = O(1), the coupling cannot be captured by the limit problem; at zero order, the array is crudely replaced by a Dirichlet wall. (In [8], this is used to discriminate between different geometries of arrays producing an efficient shielding.) The coupling is captured at the first order. For the problem of scattering by a linear array in free space considered in [5], this is incidental: the zero-order model predicts zero transmission and the first-order model a small transmission. However, when the array delimits a cavity, the limit problem is ill-posed at the resonances of the close cavity. To overcome this difficulty Hewett & Hewitt [7] derived a model with two different conditions, one valid far from the resonances and the other valid near the resonances.

The problem has been approached differently by Marigo and Maurel [10,11], who derived effective conditions without considering a specific wave problem. These unified conditions, which gather the zero- and first-order conditions, have been further applied to the scattering by a linear array in the free space (not a cage) [10] and to the scattering by the same array at a distance D of a Dirichlet wall with kD = O(1) (a one-dimensional cage); see appendix B in [11]. The underlying idea is that the effective conditions remain valid in any wave problem as long as this problem does not involve a length comparable to that of the array spacing (the microstructure). We can notice that the same idea applies to classical transmission conditions across a flat interface: while no interface is truly flat, at least at the atomic scale, it is commonly admitted that what matters is that it appears to be flat at the scale of the wavelength. Accordingly, their validity is not interrogated whenever a new problem is considered. Intuitively, this should be true after any homogenization process if the resulting conditions have the same, good, properties as the actual ones. In [11] the construction of unified conditions, avoiding an iterative resolution, provides a well-posed effective problem. This being said, well-posedness does not imply effectiveness of the model to approximate the actual solution. We address this question in the case of a cage by constructing asymptotic expansions of the solutions of the actual problem and of the unified, approximate, problem. By construction, the expansions coincide far from the resonances; more interestingly they also coincide near and at the resonances. It is good news for homogenization that no complication occurs in a simple configuration where the unique additional length scale, that of the resonant cavity, is at the largest, wavelength, scale. More generally, this interrogates the pertinence of an iterative resolution which reconstitutes faithfully the expansion of the solution. Indeed, such an expansion can fail in satisfying basic conservation laws. By contrast, a model using unified conditions is shown to enjoy the same good properties of the actual problem (conservation of the fluxes in the harmonic regime and conservation of the energy in the time domain).

The rest of the paper is organized as follows. In §2, we recall the results of the homogenization procedure for an array in free space. The result is the zero- and first-order transmission conditions as used in an iterative resolution and the construction of unified, up-to-first order conditions. We move on to the Faraday cage in §3, where we prove that the solution of the unified problem efficiently approximates the actual solution far, near and on the resonances. Numerical results are collected in §§4 and 5. In the harmonic regime (§4), explicit solutions of the effective models are available. We illustrate the effectiveness of our (unified) model that we compare with the three solutions resulting from an iterative resolution being piecewise-valid far, near and on the resonance. (It is shown that the three solutions coincide with Taylor expansions of the unified one.) In §5, we consider the transient regime which poses the problem of the stability of effective models. The initial formulation of the unified model is shown to belong to a family of formulations with the same asymptotic limit. We show that only a part of this family ensures stability of the model when it is associated with a law of energy conservation involving a positive effective energy. The numerical implementation of a stable effective model allows us to show its effectiveness by comparison with direct numerics. We also illustrate the problem of numerical instability for an unstable formulation and the link with the behaviour of the effective, interfacial energy. Concluding remarks and extensions of the present work are given in §6. We also collect additional calculations and results in four appendices.

We denote (p, u) as the fields satisfying the wave equation in the time domain

ut=p,pt+divu=0 1.1

(the wave speed is c = 1), and in the harmonic regime with time dependance e−iωt, p satisfies the Helmholtz equation

Δp+k2p=0, 1.2

with k = ω/c. We denote x = (x1, x2) as the spatial coordinate and we consider an array of wires whose boundaries are associated with the Dirichlet boundary condition p = 0. The array with spacing h is included in x1 ∈ ( − e1, e1) and it can be unbounded or bounded along x2. Within the array, a wire has a typical extent 2e1 = O(h) along x1 and 2e2 = O(h) along x2 (figure 1). To conduct the asymptotic analysis, we introduce the non-dimensional coordinate x = x/L, x = (x1, x2), with L of the order of a typical wavelength imposed by the source, and we introduce the small parameter

ε=hL1.

Figure 1.

Figure 1.

A linear array in free space (not a cage). Left, the actual problem on pε in rescaled coordinate x = x/L. Right, the resulting effective problem on pap. The asymptotic homogenization, symbolized by the arrow, involves elementary problems on (Q, Q+) set in an elementary cell Y containing a single wire. (Online version in colour.)

2. Reminder: a linear array in the free space (not a cage)

Here we consider the free space and an array of wires evenly distributed on the interface Γ={(0,x2)R2,x2R}, hence unbounded along x2.

(a). Iterative or unified transmission conditions

The asymptotic analyses conducted in [7,10,11] are basically identical and they provide the same results. With p = p0 + εp1 + O2), the zero-order term p0 is found to satisfy the wave equation (1.1) in the transient regime or (1.2) in the harmonic regime with boundary conditions

p0(0±,x2)=0. 2.1

The first-order term p1 is found to satisfy (1.1) or (1.2) with boundary conditions fed by p0, specifically

p1(0,x2)=Ap0x1(0+,x2)Bp0x1(0,x2)andp1(0+,x2)=Bp0x1(0+,x2)Ap0x1(0,x2).} 2.2

The two real constants (A,B) are given by the elementary solution Q+ set in the rescaled coordinate y = x/ε in the domain Y={(y1,y2)R×(0,1)Y^¯}, where Y^((e1/h),e1/h)×(0,1) is a canonical wire that we suppose to be symmetric with respect to the axis of equation y1 = 0 (inset of figure 1). The elementary solution Q+ is the 1-periodic w.r.t the y2 solution to

ΔQ+=0inY,Q+=0onY^,andlimy1Q+=0,limy1+Q+=e1, 2.3

and the constants B and A are defined by

Q+y1A,Q+y1+y1+B. 2.4

A usual resolution consists in solving the problem on p0 with (2.1), then that on p1 using (2.2); we call the conditions (2.1) and (2.2) iterative transmission conditions. Following [1214], unified transmission conditions are constructed by recombining (2.1) and (2.2) in

pap,ε(0,x2)=εApap,εx1(0+,x2)εBpap,εx1(0,x2)andpap,ε(0+,x2)=εBpap,εx1(0+,x2)εApap,εx1(0,x2).} 2.5

Obviously, pap,ε = p0 + εp1 + O2); hence both pap,ε and (p0 + εp1) approximate p up to O2).

Remark 2.1. —

The above relations are written in the case of wires being symmetric with respect to y1; otherwise, an additional elementary solution Q is involved, resulting in an additional constant; see (2.31) in [10]. The elementary solution Q is the 1-periodic w.r.t. the y2 solution to

ΔQ=0inY,Q=0onY^,andlimy1Q=e1,limy1+Q=0. 2.6

For symmetric wires, Q(y1, y2) = −Q+( − y1, y2); hence, Qy1y1B and Qy1+A.

(b). Remark on a simple scattering problem

Let us stress a drawback of an iterative resolution when illuminating the array by an incident wave eikx1 (coming from +∞) at normal incidence on the array, hence a solution of the form

pap(x)=eikx1+Rapeikx1for x1>0,pap(x)=Tapeikx1for x1<0. 2.7

In an iterative resolution, Rap is sought of the form Rap=R0+εR1 up to first order (the same for Tap). The solution p0 ruled by (2.1) provides R0=1 and T0=0. Next p1, of the form R1emkx1 for x1 > 0 and T1eikx1 for x1 < 0, and ruled by (2.2), provides R1=2ikB and T1=2ikA. Reconstructing Rap and Tap up to first order leads to

Rap=(R0+εR1)=(1+2ikhB),Tap=(T0+εT1)=2ikhA, 2.8

which do not satisfy the conservation of the fluxes |Rap|2+|Tap|2=1. (They satisfy the conservation up to O2).) Consider now the solution (2.7) ruled by the unified conditions (2.5). We obtain

Rap=1(kh)2(A2B2)12ikhB+(kh)2(A2B2),Tap=2ikhA12ikhB+(kh)2(A2B2), 2.9

which satisfies exactly |Rap|2+|Tap|2=1. By construction, (R0+εR1) and (T0+εT1) in (2.8) are the expansions up to O2) of Rap and Tap in (2.9). We may say that (2.9) contains non-valuable terms O2); this has no consequence. In contrast, cancelling these terms a posteriori would affect the properties of the solution, here the conservation of the fluxes. We can say as a rule that the solutions of the unified problem do not have to be interrogated again.

3. A linear array on top of a Dirichlet wall (a cage)

We now envision a Faraday cage (figure 2). We consider two rectangular domains Ω+ = (0, d+) × (0, ℓ) and Ω = ( − d, 0) × (0, ℓ), with d±, ℓ > 0, that share the common interface Γ={(0,x2)R2,x2(0,)}. We denote by Ω=Ω+ΩΓ and by Γ± the lateral boundaries of Ω, i.e.

Γ±={(±d±,x2)R2,x2(0,)}.

A large positive integer N > 0 is the number of wires in (0, ℓ), whence Nε, and the analysis holds far from the lateral boundaries at x2 = 0, 1. We puncture the domain Ω along the interface Γ by subtracting the set Lε=1iNε{Y^¯+ie2}. Finally, our domain is the open set Ωε=ΩLε. On that domain, we consider the Helmholtz equation written in non-dimensional form with K = (kL)2: find pε as the solution to

Δpε+Kpε=SinΩε,andnpε=iKpεonΓ+,pε=0onΩεΓ+,} 3.1

where S is a source term compactly supported in Ω+ (figure 2). Providing S is regular enough, problem (3.1) is well-posed.

Figure 2.

Figure 2.

A linear array on top of a Dirichlet wall Γ. The actual problem (3.1) on pε and, as a result of asymptotic analysis, the limit problem (3.2) on p* and of the unified problem (3.3) on pap,ε. (Online version in colour.)

(a). The question put to the unified problem

As ε → 0, problem (3.1) ‘tends’ to the following limit problem: find p* solution to

{Δp*+Kp*=Sin Ω+,np*=iKp*on Γ+,p*=0on Ω+Γ+,{Δp*+Kp*=0in Ω,p*=0on Ω, 3.2

and it turns out that the limit problem uncouples the behaviour of p* above and below Γ. (The limit problem is the zero-order problem, p* = p0, involving the boundary condition (2.1).) As previously said, problem (3.2, right), which is posed in Ω, may be ill-posed while the initial problem is not. Indeed, there exists a sequence of values (Kn*)nN where problem (3.2, right) admits a non-trivial kernel of finite dimension. These values are known as the eigenvalues of the Laplace operator in Ω with Dirichlet boundary conditions which are the perfect resonances of the closed cavity Ω. This ill-posed limit problem reflects the presence of the quasi-resonances for the actual problem (3.1) having a small imaginary part due to radiative damping and a real part close to K*n.

Away from these particular frequencies, we expect that the unified up-to-first-order problem (2.5) can be used. Specifically, pε can be approximated (with an error of order ε2) by solving the following problem: find pap,ε the solution to

{Δpap,ε+Kpap,ε=Sin Ω+,pap,εx1=iKpap,εon Γ+,pap,ε=0on Ω+(ΓΓ+),Δpap,ε+Kpap,ε=Sin Ω,pap,ε=0on ΩΓ,p|0+ap,ε=εBpap,εx1|0+εApap,εx1|0,p|0ap,ε=εApap,εx1|0+εBpap,εx1|0on Γ. 3.3

We emphasize that, unlike the limit problem (3.2), problem (3.3) turns out to be well-posed for any dimensionless frequency K. However, this does not presume that it approximates pε when K is close to an eigenvalue K*n of the limit problem (3.2, right). This is the question addressed in the rest of this section. To do so, we consider K*n to be a simple eigenfrequency of the cavity problem (3.2, right) and the resonance frequency Kn of the actual cavity is close to that eigenfrequency. Being ‘far from’ or ‘close to’ the resonance can be measured by the relative amplitudes of the fields pε inside and outside the cavity. Outside the cavity, pε = O(1) imposed by the source, and we define three cases, as follows.

  • The off-resonance case (1). It corresponds to |K − K*n| = O(1), hence far from the perfect resonance, and we shall see that pε = O(ε) is small within the cavity Ω. This is the case where the validity of (3.3) is not really questioned.

  • The near-resonance case (2i) and on-resonance case (2ii). These cases correspond to K close to K*n with
    K(ε)=Kn*+εκ1+ε2κ2 3.4
    (figure 3). For an arbitrary κ1, pε = O(1) becomes significant within the cavity Ω; it is termed the near-resonance (2i). Arbitrary κ1 means κ1 ≠ κ, κ being a specific value which makes (Kn* + εκ) close to the actual resonance Kn; see (3.9). This on-resonance case (2ii) is characterized by large amplitudes pε = O(1/ε) inside the cavity. In this close vicinity of the actual resonance |K − Kn* − εκ| = O2), the parameter κ2 can be used to get the resonance curve as α2(κ2)=εΩ|pε|2.

Figure 3.

Figure 3.

Resonance curve by means of max| pε| in the cavity Ω close to the resonance Kn (solid red line). The dashed grey line shows the off-resonance solution blowing up at resonance Kn* of the close cavity (its validity is limited to pε = O(ε)). The dashed green line shows the near-resonance solution blowing up at (Kn* + εκ) close to the actual resonance Kn (its validity is limited to pε = O(1)). The inset show the parametrization of the resonance curve in the on-resonance regime whose validity is limited to pε = O(1/ε). (Online version in colour.)

The performance of problem (3.3) to approximate pε in cases (1), (2i) and (2ii) is demonstrated below. The demonstration relies on the construction of asymptotic expansions of pε and pap,ε and we shall see that the leading orders of the two expansions coincide in the three cases. This was expected, by construction, in case (1) but it may appear surprising in the resonant cases (2).

Remark 3.1. —

We restrict ourselves to the case where K*n is a simple eigenfrequency of the cavity problem (3.2, right). The result holds for multiple eigenfrequencies but requires more involved calculations.

(b). Asymptotic behaviour of the exact solution

The determination of the asymptotic behaviour of pε is based on the method of matched asymptotic expansions, which permits the boundary layer effect occurring in the vicinity of the wires to be captured. The main idea is to distinguish between two ‘far-field regions’ located far from Γ and a near-field area located in its vicinity, the two types of expansions matching in some intermediate area. In the present case, we can construct asymptotic expansions of the form

pε={mm0εmpm(x1,x2)far fromΓ(far-field expansion),mm0εmqm(x1ε,x2ε,x2)in the vicinity of Γ(near-field expansion),  3.5

where the integer m0 will be equal to −1 or 0. Since we are interested in the macroscopic behaviour of pε, we present the results on the leading order in the far-field expansion; the step-by-step construction of the asymptotic expansion is technical and is given in appendix A.

(i). The off-resonance case (1)

The off-resonance case consists in taking a fixed K ≠ K*n (independent of ε) that is not an eigenvalue of the cavity problem (3.2, left).

Lemma 3.2. —

Assume that K is not an eigenvalue of the cavity problem (3.2, left). Then, far from Γ, pε admits the following leading-order asymptotic:

pε{P*in Ω+,εApin Ω, 3.6

where P* is the unique solution to (3.2, left) and p is the unique solution to

Δp+Kp=0in Ωandp=0on ΩΓ,p=P*x1on Γ.} 3.7

We point out that pε=εAp is small in the cavity Ω, which means that the array efficiently shields the domain Ω.

(ii). The near-resonance case (2i): κ1 ≠ κ

We consider K*n to be a simple eigenfrequency of the cavity problem (3.2, right), which is for instance the case for the first eigenvalue in two dimensions. We denote by pn* a corresponding real-valued eigenvector such that

Ω(pn*)2dx=1. 3.8
Remark 3.3. —

Obviously the orthogonality condition (3.8) does not entirely define pn* among all the normalized eigenvectors associated with the eigenvalue K*n. Indeed if pn* fulfils (3.8), so does −pn*. Naturally the arbitrary choice of pn* does not change the results below.

Then, we take K(ε) of the form (3.4), which means that we consider frequencies located in an ε-neighbourhood of K*n. At that stage, we introduce the real number κ

κ=BΓ(pn*x1(0,x2))2dx2, 3.9

with B the constant appearing in (3.3). We shall make the distinction between the two sub-cases (2i) κ1 ≠ κ and (2ii) κ1 = κ, and we start here with κ1 ≠ κ.

Lemma 3.4. —

Assume that K is of the form (3.4) and that κ1 ≠ κ. Then, far from Γ, pε admits the following behaviour:

pε{Pn*in Ω+,α1pn*in Ω,withα1=AIκ1κ, 3.10

where P*n is the unique solution to (3.2, left) for K = Kn*, A is the constant appearing in (3.3) and

I=ΓPn*x1(0,x2)pn*x1(0,x2)dx2. 3.11

By contrast to the non-resonant case, pε = α1pn* is of order unity inside the cavity. There is no shielding effect as the fields are as intense inside and outside the cavity.

(iii). The resonant case (2ii): κ1 = κ

Lemma 3.5. —

Assume that K is of the form (3.4) and that κ1 = κ. Then pε has the following behaviour:

pε{Pn*+α2AP+in Ω+,α2εpn*in Ω,withα2=AIκ2A2I++B2I, 3.12

where I is defined in (3.11), I± are defined by

I+=ΓP+x1(0,x2)pn*x1(0,x2)dx2,I=ΓPx1(0,x2)pn*x1(0,x2)dx2 3.13

and P+ and P are the (unique) solutions to

{ΔP++Kn*P+=0in Ω+,P+x1=iKn*P+on Γ+,P+=pn*x1on Γ,P+=0on Ω+(Γ+Γ),{ΔP+Kn*P=κBpn*in Ω,P=0on ΩΓ,P=pn*x1on Γ,ΩPpn*dx=0. 3.14

In the close vicinity of a resonance, the field pε = O(1/ε) in Ω becomes more intense within the cavity than outside and it would blow up as ε vanishes. Indeed, in the limit of zero ε, pε tends to p* and we recover a perfect resonance with unbounded amplitude inside the cavity.

(c). Asymptotic behaviours of the homogenized solution

The obtention of the asymptotic behaviour of the solution pap,ε to (3.3) also relies on the construction of its asymptotic expansion. However, this expansion is much simpler than that of pε. Indeed, the approximate problem does not see the wires and we have a classical expansion of the form

pap,ε=mm0εmpmap(x1,x2)in Ω+Ω, 3.15

where m0 is equal to −1 or 0. Below we show that we recover the off-resonance (3.6) and the two different resonant cases, (3.10) and (3.12), corresponding to (3.4).

(i). The off-resonance case

In that case, as for the exact problem, the formal expansion (3.15) is plugged into (3.3), and we find m0 = 0 (p1ap=0 in Ω+ and Ω). Next, p0ap is a solution to

{Δp0ap+Kp0ap=Sin Ω+,p0apx1=iKp0apon Γ+,p0ap=0on Ω+Γ+,{Δp0ap+Kp0ap=0in Ω,p0ap=0on Ω, 3.16

and as K ≠ Kn* the solution reads

p0ap={P*in Ω+,0in Ω.

In Ω, the first non-zero contribution appears at the order 1, with p1ap a solution to

{Δp1ap+Kp1ap=0in Ω,p1ap=0on ΩΓ,p1ap=AP*x1on Γ.

Remembering that we have denoted p as the unique solution to (3.7), we obtain that p1ap=Ap. Eventually, we get for pap,ε=p0ap+εp1ap+O(ε2) the leading-order asymptotic

pap,ε{P*in Ω+,εApin Ω,

which coincides with (3.6).

(ii). The near-resonance case κ1 ≠ κ

In that case, inserting the formal expansion into (3.3) and separating the different powers of ε, we find again that m0 = 0. But now, p0ap is a solution to

{Δp0ap+Kn*p0ap=Sin Ω+,p0apx1=iKn*p0apon Γ+,p0ap=0on Ω+Γ+,{Δp0ap+Kn*p0ap=0in Ω,p0ap=0on Ω. 3.17

The problem (3.17, left) is identical to (3.16, left) for K = Kn* and we have denoted P*n as its unique solution. By contrast, the problem (3.17, right) is ill-posed at the eigenfrequency Kn* of the close cavity. However, as pn* is the eigenvector associated with Kn*, we can write

p0ap={Pn*in Ω+,α1appn*in Ω,

but α1ap is unknown. (This means that the problem at the dominant first order cannot be solved; it corresponds to the limit problem (3.2) at an eigenvalue of the Laplace operator in Ω.) The value of α1ap is obtained from the first-order problem in Ω; namely, find p1ap as a solution to

{Δp1ap+Kn*p1ap=κ1α1appn*in Ω,p1ap=APn*x1Bα1appn*x1on Γ,p1ap=0on ΩΓ,

which is solvable if and only if

α1ap=Aκ1κΓPn*x1(0,x2)pn*x1(0,x2)dx2

(making use of (3.8) and (3.9)) and we exactly recover (3.10) (with α1ap=α1).

(iii). The on-resonance case κ1 = κ

Inserting the formal expansion (3.15) into (3.3), we find m0 = −1 with p1ap the solution to

{Δp1ap+Kn*p1ap=0in Ω+,p1apx1=iKn*p1apon Γ+,p1ap=0on Ω+Γ+,{Δp1ap+Kn*p1ap=0in Ω,p1ap=0on Ω.

The term p1ap plays basically the same role as p0ap in the near-resonance case. It is the solution to (3.16, left) in Ω+ but without the source S; hence, p1ap=0 in Ω+. It is a solution to the ill-posed problem (3.17, right) in Ω; hence, it is equal to pn* up to an unknown constant α2ap in Ω, namely

p1ap={0in Ω+,α2appn*in Ω.

As in the near-resonant case, α2ap is obtained from the problem at the next order; in the present case, the zero order. At the zero order, p0ap is a solution to

{Δp0ap+Kn*p0ap=Sin Ω+,p0apx1=iKn*p0apon Γ+,p0ap=0on Ω+(Γ+Γ),p0ap=Aα2appn*x1on Γ,{Δp0ap+Kn*p0ap=κα2appn*in Ω,p0ap=0on ΩΓ,p0ap=Bα2appn*x1on Γ.

As P+ is the solution to (3.14, left) and P*n is the solution to (3.2, left) for K = Kn*, we recover that

p0ap=α2apAP++Pn*in Ω+,

as in (3.12), but α2ap has to be determined. In addition, the problem in Ω is solvable by construction (with κ1 = κ) and with P as the solution to (3.14, right) we have

p0ap=α2apBP+βappn*in Ω,

where βap is unknown at this order (but we do not need to determine it). In the same way we determine α1ap in the near-resonance case, we determine the value of α2ap using the solvability condition for p1ap in Ω, the solution to

{Δp1ap+Kn*p1ap=κ1(α2apBP+β*appn*)κ2α2appn*in Ω,p1ap=0on ΩΓ,p1ap=A(α1apAP+x1+Pn*x1)B(α2apPx1+β*appn*x1)on Γ,

and we get that α2ap=AI/(κ2A2I++B2I); hence, we entirely recover (3.12) (α2ap=α2).

4. A one-dimensional cage in the harmonic regime

To begin with, we consider a one-dimensional cage, which means a cage laterally unbounded along x2. In the harmonic regime, the time dependence is e−iωt and the scattering problem is set for an incident wave with wavenumber k=k(cθ,sθ), cθ2+sθ2=1 and k = ω/c (we use c = 1). The wave comes from x1 = +∞ on the array, hence pseudo-periodic conditions along x2 apply. The array is made of square wires e = e1 = e2 and spacing h = 1 (with arbitrary unit) at distance D = 7 of a Dirichlet wall Γ. We call p the solution of the actual problem computed numerically using a modal method described in [10]; we call pap (omitting ε) the solution of the homogenized problem.

(a). Validity of the unified model, comparison with the iterative model

(i). Solution of the unified model

The solution of the scattering problem is explicit using (1.2) along with (2.5).1 It reads pap(x)=pap(x1)eiksθx2 with

pap(x1)={eikcθx1+Rapeikcθx1forx1(0,+),Papsin (kcθ(x1+D))forx1(D,0), 4.1

and

{Rap=z¯z,Pap=2ikcθhAzand z=(1ikcθhB)sin (kcθD)+kcθh(B+ikcθh(A2B2))cos(kcθD). 4.2

Expectedly, |Rap|=1 and Pap is bounded. In addition, defining the resonance as Rap=1 provides the resonance frequency kn and the corresponding amplitude Pmaxap by means of the condition that z is purely imaginary

tan(kncθD)+kncθhB=0,Pmaxap=2Akncθhcos(kncθD), 4.3

hence kncθDnπ(1(hB/D)+(hB/D)2). (We have checked that defining the resonances as the maximum amplitudes within the cavity provides almost the same results for (kn,Pmaxap).)

To begin with, we report in figure 4 the fields p(x) and pap(x) for three frequencies corresponding to the cases (1), (2i) and (2ii) studied in §3. Off-resonance, the incident wave is basically reflected as on a Dirichlet wall with Rap1 resulting in a weak amplitude within the cavity. By contrast, on-resonance Rap1 and the amplitude is large within the cavity. In between, near-resonance, the fields inside and outside the cavity are comparable in amplitude. It is noticeable that the agreement between p(x) and pap(x) from (4.1) with (4.2) is qualitatively very good.

Figure 4.

Figure 4.

Wavefields in a one-dimensional cage—p(x) computed numerically (a) and pap(x) from (4.1) and (4.2) (b). The source is a plane wave of amplitude unity at an oblique incidence of 45° on a periodic array of square wires with spacing h = 1 and with e = e1 = e2 = 0.1 ( x2 ∈ (0, 10)); the Dirichlet wall Γ is at x2 = −7. The amplitude within the cavity is O(ε) off-resonance (k = 0.700), O(1) near-resonance (k = 0.640) and O(1/ε) on-resonance (k = 0.633). (Online version in colour.)

The validity of (4.3) is further illustrated in figures 5 and 6. We have computed the maximum amplitude max|p| within the cavity against k ∈ (0, 2) for e = 0.01, 0.1 and 0.2 (solid blue lines in figure 5). Next, max| pap|, reported by the dashed black lines, is determined from (4.1) to (4.2) (the values of (A,B) for e = 0.01, 0.1 and 0.2 are given in (B 1) in appendix B). Notably, for kcθ D > π/2, we have max|pap|=Pap. Classical trends of the resonance curves are observed. As e increases, the leakage of the cage decreases, resulting in resonances with higher quality factors, that is, thinner in frequency and higher in amplitude. These resonances take place close to kn*cθ D = , in the reported case k1* = 0.635, k2* = 1.270 and k3* = 1.904. The prediction of the unified problem appears to be excellent up to kh = 2, that is, beyond the expected range of validity of the homogenization (with kh = O(ε) assumed to be small), although a slight discrepancy is visible above kh ∼ 1 for e = 0.1 and 0.2.

Figure 5.

Figure 5.

Maximum pressure in the cavity against the dimensionless frequency kh, max|p| from direct numerics (solid blue lines), max| pap,ε| from (4.1) and (4.2) (dashed black lines). The panels in (b) show a zoom of the panels in (a). (Online version in colour.)

Figure 6.

Figure 6.

Variations of the resonance frequency k1 and maximum amplitude Pmax at the resonance against h. Solid lines, computed from direct numerics; dashed black lines, from (4.1). (Online version in colour.)

From figure 5, we have determined the resonance frequency k1 and the corresponding amplitude at the resonance Pmax against h ∈ (0, 3). The results shown in figure 6 demonstrate that the one-dimensional cage has resonances behaving as for its two-dimensional analogue [7] and conform to (4.3). As the effective problem tends to the limit problem for vanishing h, decreasing h makes k1 closer to k1*; next k1 departs from k1* essentially linearly with h. Amusingly, as in the two-dimensional cage, e ≃ 0.1 h is a critical value; below k1 decreases with h, above it increases. From (4.3), kn = kn* is obtained for B=0, and B=0 for e ≃ 0.115 h. In any case, Pmax1/h decreases with h as the leakage increases.

(ii). Comparison with the iterative model

The iterative model consists of three predictions: off-resonance, near-resonance and on-resonance. We have shown in §3 that the asymptotics of the unified model coincide with the iterative solution in the three regimes. However, this does not presume to know how the two solutions compare for a given h. As previously mentioned, the problem is one-dimensional along x1, which makes explicit the various functions needed to define the solutions of the iterative model.2 We give below the resulting expressions in dimensional coordinates with pε(x1,x2)=pε(x1)eiksθx2.

  • Off-resonance case. In this case, pεεAp for x1 < 0 (see (3.6)); hence, using2, pε reads
    pε(x1)m=1+4i(Ah/D)(kcθD/mπ)3sin (mπx1/D)(kcθD/mπ)212iAhD(kcθD)(1+x1D). 4.4
    Expectedly, the amplitude within the cavity blows up at all the perfect resonances of the close cavity kcθ D = . (The solution is valid far from these resonances.)
Remark 4.1. —

The solution (4.4) is the Taylor expansion of pap(x1) in (4.1) at first order in (k h); hence, z ≃ sin (kcθ D) in (4.2).3

  • Near-resonance case. From (3.10) pε ∼ α1pn* for x1 < 0 with α1=AI/(κ1κ) with I=22i(nπ)2, and from (3.9) κ=2B(nπ)2 and κ1 = (K − Kn*)/ε = (D/h)((kcθ D)2 − ()2); see2. Hence, we have
    pε(x1)4i(Ah/D)sin (nπx1/D)(kcθD/nπ)2(12(Bh/D)). 4.5
    Again, this amplitude blows up, but now at a value closer to the actual resonance frequency kn, namely for kcθDnπ(1B(h/D)) corresponding to the first-order expansion of the dispersion relation in (4.3). (The solution is valid far from this resonance.)
Remark 4.2. —

The solution (4.5) coincides with the Taylor expansion of pap(x1) in (4.1) up to O2), around the resonance of the close cavity, namely for kcθD=nπ(1+εk^).4

  • On-resonance case. Here, (3.12) applies; hence, pε ∼ (α2/ε)pn* for x1 < 0 with α2=AI/(κ2A2I++B2I). Next, from (3.13) along with 2, I+ = −2i()3 and I = −3()2 (using5) and by construction κ2=(nπD/h)2[(kcθD/nπ)21+2(Bh/D)]. It follows that
    pε(x1)4i(Ah/D)sin ((nπx1)/D)(kcθD/nπ)2(12(Bh/D)+3(Bh/D)2)+2inπ(Ah/D)2. 4.6
    The leakage of the cavity is recovered, hence the amplitude within the cavity is finite. This solution is valid in the close vicinity of the resonance kn.
Remark 4.3. —

Again, the solution (4.6) coincides with the Taylor expansion of pap(x1) in (4.1) up to O(1), around the resonance of the closed cavity kcθh=nπ(1εB+ε2k~).6 We also obtain that the maximum amplitude is reached for

(kncθ)2=(nπD)2(12hBD+3(hBD)2),

which is the Taylor expansion of the dispersion relation in (4.3).

We end this comparison by reporting in figure 7 the same numerical result as in figure 5. However, now we compare the actual solution with the solutions (4.4) (dashed grey lines) valid far from the resonances, (4.5) (dotted green lines) valid near the first resonance and (4.6) (dashed red lines in the insets) valid in its close vicinity. The results conform with those reported for the two-dimensional cage in [7] and conform with the idea of piecewise-valid solutions. Compared with the unified solution, which is valid in the whole range of frequency, the validity of each prediction is locally as good; the main difficulty in their use is to define the frequency ranges where each of them can be used. Eventually, it can be seen that the result for e = 0.01 is not satisfactory essentially because the off-resonance solution departs significantly from the actual one; this case, which can be treated within the ‘thin wire approximation’, is discussed in appendix C.

Figure 7.

Figure 7.

Same representation as in figure 5. Direct numerics for the actual problem and from the iterative model: off-resonance curve from (4.4), near-resonance curve from (4.5) and on-resonance curve from (4.6). (Online version in colour.)

5. A two-dimensional cage in the transient regime

We now move on to the transient regime and consider a two-dimensional cage, that is, a cage laterally bounded along x2. As the fields depend on time and on space, we consider p(x) → p(x, t).

(a). Enlarged formulations of the model

To begin with, we note that the transmission conditions cannot be used as written in (2.5), that is, written across a zero-thickness interface. Introduced in [12,13], enlarged formulations of the transmission conditions consist in modifying (2.5) by simple Taylor expansions of pap(0±, x2, t) around x1 = ±a with a > 0 resulting in (in dimensional form)

pap(a,x2,t)=hApapx1(a,x2,t)(hB+a)papx1(a,x2,t)andpap(a,x2,t)=(hB+a)papx1(a,x2,t)hApapx1(a,x2,t),} 5.1

and we see that the new pap approximates p up to O2) if a = O(e1) = O(h); see (B.9) in [11]. In other words, it exists as a family of effective models parametrized by a and having the same asymptotic limit. The advantage of the models in enlarged formulations (5.1) is that they enjoy ‘good’ energetic properties as soon as a ≥ ac and we shall see that 0 ≤ ac ≤ e1. For the time being, we show that it is sufficient that a ≥ e1: let us consider the balance of energy in Ω to be a bounded region of the space containing a segment Γ and Ωa=ΩΓa, where Γa = {(x1, x2) ∈ ( − a, a) × Γ} is the enlarged interface ruled by (5.1). Multiplying the first equation of (1.1) by u, the second by p and summing up, we get

ddt(Eap+EΓ)=0,Eap(t;a)=12Ωa((uap)2+(pap)2)dxandEΓ(t;a)=h2Γ((B+ah)(u1ap|a2+u1ap|a2)2Au1ap|au1ap|a)dx2.} 5.2

(u1|±aap stands for u1ap(±a,x2,t).) ‘Good’ energetic properties means that the effective interface provides a positive energy contribution EΓ, a lack of which may lead to severe instability of any time-discretization scheme; this will be illustrated in §5c.

Lemma 5.1. —

The quadratic form (B+(a/h))(α2+β2)2Aαβ is positive if a ≥ e1.

Proof. —

We set Q = αQ+ + βQ with α, β two reals and Q+, Q defined in (2.3), (2.6). Q satisfies

ΔQ=0in Y,Q=0on Y^,and limy1Q=βe1,limy1+Q=αe1. 5.3

We define H(y1) with H(y1<e1/h)=β(y1+(e1/h)), H(|y1| ≤ e1/h) = 0, H(y1 > e1/h) = α(y1 − (e1/h)) and q = Q − H being continuous across any interfaces (in particular at y1 = ±e1/h) and satisfying

qy1αAβ(B+e1h),qy1+α(B+e1h)βA. 5.4

We define the restriction Y*Y with Y*={(y1,y2)(y*,y*)×(0,1)Y^¯} and y* > e1. Integrating qΔQ over Y* and using (5.3) and (5.4) gives

0=Y*qΔQdy=Y*q(q+H)dy+(α2+β2)(B+e1h)2αβA+o(y*),

with limy*+o(y*)=0. Next, integrating HΔQ over Y* leads to

0=Y*HΔQdy=Y*H(q+H)dy+(α2+β2)(y*e1h)+o(y*).

Since Y*HHdy=(α2+β2)(y*e1h), and passing to the limit y* → +∞, we finally find

0Yqqdy=(B+e1h)(α2+β2)2Aαβ,(α,β)R2.

We deduce that, for a ≥ e1, 0(B+ah)(α2+β2)2Aαβ, (α,β)R2. ▪

Transmission conditions have been implemented numerically using a = e1, that is, restoring the actual thickness of the array. The actual problem and the unified problem involving (5.1) have been implemented numerically in a consistent manner. In both cases, the numerical method combines a finite-element scheme in space and a finite-difference scheme in time (FEM-BEM C++ code XLiFE++; see https://uma.ensta-paris.fr/soft/XLiFE++). P2 finite elements are used on a triangular mesh along with a centred order 2 Newmark scheme in time, unconditionally stable without numerical damping [15].

(b). Temporal evolution of the field in the cage

We consider now the two-dimensional cage shown in figure 8; the linear array is composed of 10 circular wires of radius e = 0.1 (hence e1 = e) and spacing h = 1, in x2 ∈ (0, 10). The bottom boundary Γ at x1 = −5 is associated with a Dirichlet boundary condition and radiation boundary conditions are imposed on Γ+ at x1 = 10. Eventually, the lateral boundaries at x2 = 0 and x2 = 10 are associated with a Neumann boundary condition.

Figure 8.

Figure 8.

Snapshots at short times—the p(x, t) solution of the actual problem (a) and of the pap(x, t) solution to the effective problem ruled by (5.1) with a = e (b); both p and pap are computed numerically. (Online version in colour.)

Remark 5.2. —

Note that, in (3.1) the Dirichlet condition was chosen on all boundaries for ease of writing. This choice is however arbitrary and it does not affect the model, whose essential ingredients are the transmission conditions; in addition, the analysis does not apply near the ends of the array where a specific analysis is required, which is outside the scope of the present study [16]. In our simulations, Neumann boundary conditions on the lateral walls of the cavity avoid very small amplitudes within the cavity, which would fall within numerical errors.

We use a source S exciting a range of frequencies. This includes the first three resonances of the cavity, namely S(x, t) = g(x) s(t), with g(x)=1/π(0.1)2 within the disc centred at (x1 = 1, x2 = 5) and of radius 0.1, g(x) = 0 elsewhere. Next, s(t)=eαt2sin (ωst) with α = 5 × 10−3 and ωs = 1 (figure 9). For the actual problem on p, a refined mesh (Δh = 10−2) is used in the vicinity of the wires to ensure that the near-evanescent field of the order of e is well resolved; far from the wires, a coarser mesh (Δh = 0.2) ensures at least 16 points per wavelength up to ω ∼ 2. For the effective problem ruled by (5.1) with a = e, we have checked that a constant mesh step Δh = 0.2 is sufficient to produce converged solutions. In time, we use the same time step for both problems Δt = 4 × 10−2 to facilitate the comparison of the solutions.

Figure 9.

Figure 9.

The source s(t) (a) and its Fourier transform s^(ω) (b); the red arrows show the resonance frequencies of the cage. (Online version in colour.)

To begin with, we report in figures 8 and 10 snapshots of the fields p and pap, both being computed numerically. Three regimes are exemplified:

  • The short times: the source emits, part of the wave train hits the array and it is essentially reflected. The amplitude inside the cavity is weak as the shielding is efficient for most of the frequencies. However, we see in figure 8 that the field is not zero in the cavity both in the actual and effective problems. The cavity is little by little filled in.

  • The intermediate times: the source is still emitting but with weaker amplitude. Meanwhile, the energy within the cavity has increased. At these intermediate times, the amplitudes inside and outside the cavity are comparable.

  • The long times: the source does not emit anymore and the waves issued from the source, directly or after reflection on the array, have left the calculation domain. Now the cavity releases energy very slowly; ‘very slow’ being related to the weak radiative damping of the cavity. The agreement between both solutions is good at short times. More interestingly, the solutions keep on agreeing at intermediate and long times.

Figure 10.

Figure 10.

Same representation as in figure 8 at intermediate times (a) and at long times (b). (Online version in colour.)

More quantitatively, we report in figure 11a the time variations of the quantity P(t) (resp. Pap(t)) being the spatial average of p(x, t) (resp. pap(x, t)) over the upper half-part of the cavity avoiding the near field of the wires in the actual geometry; we choose the domain Ω = {(x1, x2) ∈ (0, 10) × ( − 2.5, − 2e)}, hence

P(t)=Ωp(x,t)dxandPap(t)=Ωpap(x,t)dx. 5.5

The spectral content P^(ω) makes the first three resonance frequencies appear. The quantitative agreement is excellent for kh ∈ (0, 1), with a relative error less than 1%. It reaches 10% at the second resonance. Eventually, although the trends around the third resonance are reasonably captured, the error reaches 100% very locally for kh ∈ (1.77, 1.83) owing to a small shift between the actual resonance and that predicted by the unified model.

Figure 11.

Figure 11.

(a) Time variation of P(t) (solid blue line) and of Pap(t) (dashed black line) for t ∈ (0, 400). (b) Corresponding spectra P^(ω) and Pap^(ω); the dotted grey line shows the spectrum of the error | pap − p|. (Online version in colour.)

(c). Energetic aspects: stability of the model in time

In this section, we move on to energetic aspects of the effective model and we address two different questions. Firstly, we have said that (5.1) ensure stability of the model for a = e as used in the numerics reported in the previous section; we shall see that a ≥ ac with ac ≤ e is sufficient in a specific geometry, that is, when (A,B) are known. If a < ac numerical instabilities in time are fostered, resulting in a blow-up of the solution pap(x, t). Next, the stability is associated with a positive interfacial energy EΓ whose link with the actual energy is inspected.

(i). Stability of the model with enlarged transmission conditions

In lemma 5.1, we have established a criterion of stability of the enlarged transmission conditions (5.1); it is sufficient that a ≥ e to ensure the stability. The criterion can be refined for given (A,B); as EΓ in (5.2) is convex for (B+ah)>0, EΓ0 if

aac=h(|A|B).7 5.6

We report in figure 12a the resulting stability diagram in the plane (a, e) for wires being discs or squares. In both cases, (A,B) are a function of e = e1 = e2 only (the radius of the disc or the half-length of the square). It can be seen that ac ∼ e for squares while ac is significantly lower than e for discs (in both cases, ac ≤ e). While the value of a is incidental in the harmonic regime, it is expected that a < ac produces numerical instability in the transient regime. We have used the transmission conditions (5.1) for various a around ac; for our wires with radius e = 0.1, the critical value of a is ac = 0.030. A typical instability observed numerically by means of the blow-up in time of pap(x, t) is illustrated in figure 12b; we have reported |Pap(t)| from (5.5) against t for a stable formulation a > ac (dashed black line, the solution is bounded) and for an unstable formulation a < ac (solid blue line, the solution blows up exponentially). In the inset for the unstable formulation, EΓ(t;a)<0 diverges exponentially to −∞, being roughly compensated by the exponential growth to +∞ of the energy in the volume Eap(t;a). ‘Roughly’ means that the conservation of the energy (5.2) is not satisfied in our numerics when the fields have too large amplitudes. Note that the stability of the numerical solution in the close vicinity of a = ac depends on the mesh and time step; a complete analysis of this problem, which is outside the scope of the present work, requires the discrete numerical energy associated with the numerical scheme to be identified.

Figure 12.

Figure 12.

Numerical instability in the effective problem ruled by unstable conditions (5.1) when a < ac. (a) Stability diagram for discs and squares. Blue lines show ac(e) from (5.6) for wires of extent e. The red symbols show an estimate of ac determined numerically as the lowest value of a producing a stable solution. (b) Exponential growth in the time of |Pap(t)|, (5.5), for an unstable formulation (a = 0.015 < ac, solid blue lines) and for a stable formulation (a = 0.033 > ac, dashed black lines). The inset shows Eap(t;a) diverging to +∞ and EΓ(t;a) diverging to −∞ for a = 0.015. (Online version in colour.)

(ii). Meaning of the interfacial energy EΓ

It is one thing to know that a > ac ensures the stability as it guarantees EΓ(t;a)>0, but it is quite another to interpret EΓ. Heuristically, EΓ approximates the sum of two actual energetic contributions : (i) that of the evanescent field being approximated by static fields (provided by the elementary problems) and (ii) that of the propagating field being approximated by linear fields (the loadings in the elementary problems). Up to now we have used a = e; hence, EΓ=EΓ(t;e) and we begin with this case. We have computed the actual and the effective energies

{EΩb(t)=12Ωb(u2+p2)dx,Ωb={(x1,x2)(b,b)×Γ},EapΩb(t)=EΓ(t;e)+12ΩbΓe((uap)2+(pap)2)dx,Γe={(x1,x2)(e,e)×Γ},

for b ∈ (e, 5e). The results are reported in figure 13. Figure 13a shows the fields p(x, t0) and pap(x, t0) in the vicinity of the wires (t0 = 19); the contribution to p of the evanescent near-field is visible, which is not reproduced by pap, by construction (the effect of the evanescent field has been encapsulated in the transmission conditions). As b increases, the domain Ωb over which the energy is calculated increases. In the actual problem, EΩb increases accordingly, being supplied by the evanescent field and by the propagating field. By contrast, in the effective problem, EapΩb increases, being supplied by the propagating field only, as EΓ approximates the whole energy of the evanescent field. We expect the two energies to coincide (up to the error of the model) when b is large enough so that the actual energy also contains the whole energy of the evanescent field. The results in figure 13 support this scenario. We observe that EapΩb>EΩb up to b ≃ 2.5e; afterwards, the two energies coincide up to a relative error (about 5%) attributable to the error of the model.

Figure 13.

Figure 13.

Energies in the actual and effective problems. (a) A zoom of p(x, t0) and pap(x, t0) in {(x1, x2) ∈ ( − 1.5, 1.5) × ( − 3, 3)} (t0 = 19). (b) The difference between the time-averaged energies EapΩb and EΩb against b and time variations of the energies for ***** b = e = 0.1 and **** b = 5e = 0.5. (Online version in colour.)

We now move to the influence of a, the enlargement of the interface. We have computed EΓ(t;a) for a ∈ (0.10, 0.25), which we compare with its counterpart in the actual problem

EΩa(t)=12Ωa(u2+p2)dx,Ωa={(x1,x2)(a,a)×Γ}.

From what we have seen from the previous representation, we could expect that EΓ(t;a)EΩa(t) as soon as a > 2.5 e, that is, as soon as EΩa contains the whole contribution of the evanescent field. This is not the case, as illustrated in figures 14 and 15; the reason relies this time on the contribution of the propagating field. For every a, EΓ(t;a) approximates the energetic contribution of the evanescent field but it also has to approximate that of the propagating field. The propagating field is approximated by its expansions, a constant at zero order and a linear function at first order; hence, the approximation becomes cruder as a increases. This demonstrates that the ability of EΓ(t;a) to resemble EΩa is a compromise between the actual extension of the evanescent field and the validity of a linear approximation of the propagating field. From figure 14, it can be seen that, for small a, EΓ(t;a)>EΩa as the contribution of the evanescent field is incomplete in EΩa; conversely, for large a, EΓ(t;a)<EΩa, indicating that EΓ(t;a) underestimates the contribution of the propagating field. The compromise is obtained for a ∼ 1.6 e, although it can be seen from figure 15 that the evanescent field is still strong at x1 = 1.6 e.

Figure 14.

Figure 14.

Relative difference between the time-averaged interface effective energy EΓ(a) and the time-averaged actual energy EΩa against a; time variations of EΓ(t;a) (dashed black lines) and E(t;a) (solid blue lines) for ***** a = 0.1, **** a = 0.15 and *** a = 0.25. (Online version in colour.)

Figure 15.

Figure 15.

Effective fields pap(x, t0) (t0 = 19) in the vicinity of Γ for a = 0.1, a = 0.16 and a = 0.25 (a) and corresponding profiles of p (solid blue lines) and pap (dashed black lines) at x1 = a (b). (Online version in colour.)

Note that, if the comparison of EΓ(t;a) and EΩa(t) is enlightening on the meaning of the interfacial energy, there is no guarantee that the value of a minimizing their difference coincides with the value of a minimizing the error between p and pap in the far field. (In the temporal regime, we do not find a clear minimum of this error as a varies; in the harmonic regime, we have observed a minimum in the scattering coefficients for a ≃ 1.5e.8)

6. Concluding remarks and perspectives

We have shown both theoretically and numerically that the transmission conditions derived in [10,11] for an array of Dirichlet wires in free space apply without additional work when the array delimits a resonant cavity. These conditions, called unified conditions in the present study, have several advantages: (i) they are valid at any frequency and for any size of the wires and (ii) in their enlarged version they guarantee stability in the transient regime. Point (i) is linked to the fact that the unified conditions avoid an iterative resolution of the asymptotic problems, which is at the origin of the problem stressed in [7]. (The zero-order problem is ill-posed at the resonance frequencies of the closed cavity.) Point (ii) is linked to the fact that the effective problem in its enlarged version is associated with a positive interfacial energy, which prevents numerical instabilities.

More generally, we can remark that the construction of a unified, or unique, problem gathering the results of the asymptotic analysis up to first order (or higher orders) follows the construction of the models of continuum mechanics or continuum physics. As for these classical models, the properties of new homogenized models can be analysed in all generality, independently of the specific context in which they will be used, as the sources and the surrounding boundaries. By contrast, an iterative resolution focuses on a specific solution for given sources and surrounding boundaries. As such it reduces the range of applicability of the homogenization, as the work has to be done for each new problem. In addition, as in the example reported in this study, it can lead to unnecessary complications.

Finally, we stress the importance of establishing effective models in the time domain: they enable us to check some good energetic properties, namely the conservation of a positive energy in the bulk and a good balance of the fluxes of energy. (We have given an illustration of the blow-up of the numerical solution in time when these properties are not satisfied.)

Acknowledgements

We thank the reviewers for their constructive comments.

Appendix A. Step-by-step derivation of the resonant cases

In this appendix, we use the ansatz (3.5). We shall use the following result: any harmonic function q(y) in Y satisfying a homogeneous Dirichlet condition on Y^ and with no exponential growth when y1 goes to ±∞ can be written as

q(y)=aQ(y)+bQ+(y), A 1

where Q± are defined in (2.3) and (2.4).

Remark A.1. —

For the sake of conciseness, the proof of the existence and uniqueness of Q and Q+ is not written here (e.g. [8]). It is based on the application of the Lax–Milgram lemma together with a Hardy equality [19, lemma 2.5.7]. A crucial point is that there is no harmonic function in Y satisfying a homogeneous Dirichlet condition on Y^ and behaving like a constant as y1 goes to both ±∞.

(a) The near-resonant case (2i): κ1 ≠ κ

In that case, we make the ansatz (3.5) with m0 = 0. Inserting the formal series into equation (3.1) and separating the different powers of ε leads to a collection of equations for the near- and far-field terms. These equations are linked with the matching conditions that enforce the far- and near-field expansions to coincide in some intermediate area (e.g.[10,12,20]). In the present case, they can be written as

pi(0±,x2)=limy1±(m=1im0(y1)mm!mpimx1m(0±,x2)qi(y,x2))i1. A 2

By convention, the previous sum is empty (and vanishes) if i − m0 < 1. First, the leading-order far-field term p0 and near-field term q0 (1-periodic w.r.t. y2) are solutions to

{Δp0+Kn*p0=Sin Ω±,p0x1=iKn*p0on Γ+,p0=0on (ΩΩ+)(Γ+Γ),{Δq0=0in Y,q0=0on Y^, A 3

complemented (and linked) by the zero-order matching conditions (A 2) (i = 0). In (A 3, right) Y denotes the periodicity cell Y={(y1,y2)R×(12,12)Y^¯}. Using (1), q0 can be written as q0(y, x2) = a(x2)Q(y) + b(x2)Q+(y), and the matching condition indicates that q0 tends to constants as y1 goes to ±∞. From remark A.1, we get a(x2) = b(x2) = 0; hence, p0(0±, x2) = 0. These conditions complement the problem (A 3, left), and the solution reads

p0=Pn*in Ω+andp0=α1pn*in Ω, A 4

where P*n is the unique solution to (3.2, left) and pn* is defined in (3.8). It remains to determine α1. In fact, the value of α1 is imposed by the solvability condition associated with the far-field problem of order 1 in Ω. More specifically, we have

{Δp1+Kn*p1=κ1α1pn*in Ω,p1=0on ΩΓ,{Δq1=0in Y,q1=0on Y^, A 5

with q1 1-periodic w.r.t. y2 and the first-order matching conditions (A 2) (i = 1). As previously, we look for q1(y, x2) = a(x2)Q(y) + b(x2)Q+(y). Identifying in the matching conditions the parts linear in y1 and the constants, we get a(x2) = ∂p0/∂x1(0, x2), b(x2) = ∂p0/∂x1(0+, x2), hence p1(0,x2)=Ba(x2)+Ab(x2), p1(0+,x2)=Aa(x2)+Bb(x2), and using (A 4)

{q1(y,x2)=α1pn*x1(0,x2)Q(y)+Pn*x1(0,x2)Q+(y),p1(0,x2)=APn*x1(0,x2)α1Bpn*x1(0,x2).

Finally, integrating over Ω (A 5, left) after multiplication by pn* and integrating by part, we see that problem (A 5, left) is solvable if and only if

α1(κ1+BΓ(pn*x1(0,x2))2dx2)=AΓPn*x1(0,x2)pn*x1(0,x2)dx2.

In view of the definition (3.9) of κ and since by assumption κ1 ≠ κ, the previous equation entirely defines α1 in (A 4).

(b) The on-resonance case (2ii) : κ1 = κ

In that case, we still make the ansatz (3.5) but we found m0 = −1 (reflecting the presence of a strong resonant effect).

(i) The leading order: i = −1)

As previously, the far-field term p−1 and near-field term q−1 (1-periodic w.r.t. y2) are solutions to

{Δp1+Kn*p1=0in Ω±,p1x1=iKn*p1on Γ+,p1=0on (ΩΩ+)(Γ+Γ),{Δq1=0in Y,q1=0on Y^, A 6

complemented by the matching conditions (A 2) for i = −1. As previously, we deduce from the near-field equation (A 6, right) that q−1(y, x2) = a(x2)Q (y) + b(x2)Q+(y); hence, again, as (A 2) imposes that q−1 tends to a constant as y1 goes to ±∞, we obtain that a(x2) = b(x2) = 0, and therefore q−1 = 0. Consequently p−1(0±, x2) = 0. Together with (A 6, left), we deduce that

p1=0in Ω+,andp1=α2pn*in Ω, A 7

where pn* is defined in (3.8), the constant α2 being undetermined at this stage. Expectedly, in the absence of a source term at order i = −1, the field outside the cavity is zero at this order.

(ii) The order i = 0)

The analysis of the leading order provides neither the leading-order asymptotic for pε in Ω+ nor the constant α2. Therefore, we need to analyse p0 and q0 (1-periodic w.r.t. y2) solutions to

{Δp0+Kn*p0=Sin Ω+,p0x1=iKn*p0on Γ+,p0=0on Ω+(Γ+Γ),{Δp0+Kn*p0=κα2pn*in Ω,p0=0on ΩΓ, A 8

and

Δq0=0in Y,q0=0on Y^, A 9

together with the zero-order matching conditions (A 2) and using (A 7). Looking for q0(y, x2) = a(x2)Q(y) + b(x2)Q+(y) and identifying in the matching conditions the parts linear in y1 and the constants, we get a(x2)=α2pn*x1(0,x2) and b(x2) = 0, hence

q0(y,x2)=α2pn*x1(0,x2)Q(y),p0(0+,x2)=Aα2pn*x1(0,x2),p0(0,x2)=Bα2pn*x1(0,x2). A 10

The above relations provide p0(0±, x2), which complement the problems (A 8) set in Ω+ and Ω; at this stage, they are disconnected. In Ω+, p0 solution to (A 8, left) along with (A 10, centre) reads

p0(x)=α2AP+(x)+Pn*(x)in Ω+, A 11

where P+ and P*n are the (unique) solutions to (3.14, left) and (3.2, left). It then provides the asymptotic behaviour of pε in Ω+ (up to the definition of α2). In Ω, since K*n is a resonance frequency, the far-field problem (A 8, right)–(A 10, right) is not well-posed (it has a kernel of dimension 1 spanned by pn*); however, it is solvable. Indeed, multiplying (A 8, right) by pn* and integrating over Ω gives

α2(κ+BΓ(pn*x1(0,x2))2dx2)=0,

and the above equality is fulfilled for any α2 by definition of κ (see (3.9)). It follows that the p0 solution to (A 8, right)–(A 10, right) reads

p0(x)=α2BP(x)+βpn*(x)in Ω, A 12

where P is the unique solution to (3.14, right) and pn* is the real-valued eigenvector associated with K*n (for the cavity problem (3.2, right)). In (A 12), α2, which reaches back from order i = −1 (see (A 7)), and β are constants that remain to be determined.

(ii) The order i = 1

Here, we shall determine the constant α2 that we need to parametrize locally the resonance curve. To do so, it is enough to investigate the solvability of the far-field problem for p1 in Ω and the near-field problem for q1 (1-periodic w.r.t. y2)); namely,

{Δp1+Kn*p1=κp0κ2α2pn*in Ω,p0=α2BP+βpn*,p1=0,on ΩΓ,{Δq1=2α22pn*x1x2(0,x2)Qy2in Y,q1=0on Y^. A 13

We have used the forms of p−1 in (A 7), of p0 in (A 12) and of q0 in (A 10). The two problems are complemented by the matching conditions (A 2) at order −1 (i = −1) with ∂p−1/∂x1(0±, x2) = 0. We define the Q, 1-periodic w.r.t. y2, unique solution to

ΔQ=2Qy2in Y,Q=0on Y^,limy1±Q=0. A 14

(Here, again, see remark A.1; the well-posedness of (A 14) results from the Lax–Milgram lemma.) As q~1=(q1α2(pn*/x1x2)(0,x2)Q) satisfies Δq~1=0 with q~1=0 on Y^, we look for q1 of the form

q1(y,x2)=a(x2)Q(y)+b(x2)Q+(y)+α22pn*x1x2(0,x2)Q(y).

Inserting q1 in (A 13, right), and identifying the parts linear in y1 and the constants, we obtain that

q1(y,x2)=p0x1(0,x2)Q(y)+p0x1(0+,x2)Q+(y)+α22pn*x1x2(0,x2)Q(y)

and

p1(0,x2)=Bp0x1(0,x2)+Ap0x1(0+,x2).

Eventually, using p0 given by (A 11) and (A 12), we end up with

p1(0,x2)=α2((A)2P+x1(B)2Px1)|x1=0+(APn*x1Bβpn*x1)|x1=0,

which complements problem (A 13, left). It is now sufficient to multiply (A 13, left) by pn* and to integrate over Ω to see that problem (A 13, left) is solvable if and only if α2κ2=Γp1pn*/x1(0,x2)dx2κΩp0pn*dx, resulting in

α2[κ2(A)2Γ(P+x1pn*x1)|x1=0dx2+(B)2Γ(Px1pn*x1)|x1=0dx2]=AΓ(Pn*x1pn*x1)|x1=0dx2, A 15

as mentioned in (3.12) (with (3.11) and (3.13)). In (A 15), note that the term in β has cancelled; also, we have used that P is orthogonal to pn*. Also, we have used that limy1±Q=0 for wires symmetric w.r.t. y2, as Q is an odd function of y2; the result (A 15) on α2 holds for any wire shape.

Appendix B. The elementary problem

Here, we report additional information on the effective parameters (A,B) issued from the elementary solution Q+ to (2.3): figure 16b shows an example of the fields Q+(y) for a wire being a disc or a square, and figure 16a shows the variations of (A,B) against e/h; values of (A,B) used for squares (in the harmonic regime) and for discs (in the transient regime) throughout the paper are given in (B 1).

graphic file with name rspa20200668-e1.jpg B 1

Figure 16.

Figure 16.

(a) Effective parameters (A,B) against e/h for squares (solid lines) and for discs (dashed lines); the dotted grey line shows A0=(1/2π)logsin (2πe/h). (b) Examples of solution Q+ to the elementary problem (2.3). (Online version in colour.)

Appendix C. The thin wire approximation

The thin wire approximation presented in [7] allows us to capture the leakage of the cavity at the dominant order. The reason for this is that the amplitude within the cavity is of order ε, including at the resonance frequency. (This is already visible in figure 5 for e = 0.01 h, where the amplitude Pmax does not overcome 0.1.) This is obtained by choosing a scaling e/h = O(e−(c/ε)) (with c a constant), which means that the wire thickness e vanishes exponentially faster than the array spacing h when ε goes to zero. In this case, it is found that

ptw(0,x2)=hA0(ptwx1(0+,x2)ptwx1(0,x2)), C 1

with ptw continuous. Expectedly, the above condition is consistent with the formulation (2.5) when A=B=A0. For the simple scattering problem considered in §4, the solution reads as in (4.1) with

Rap=z¯z,Pap=2ikcθhA0z,z=1+kcθhA0(cos(kcθD)isin (kcθD)), C 2

and A0=(1/2π)log(sin (2πe/h)), which is consistent with (4.1) and (4.2) in the considered limit. We report the resonance curves in figure 17 as in figure 5. The thin wire model appears to be more limited, its accuracy depending on how close (A,B) are to their asymptotic value A0.

Figure 17.

Figure 17.

Validity of the thin wire approximation; same representation as in figure 5. Solid blue lines, direct numerics; dashed black lines; unified model with (4.1) and (4.2); and dotted green lines, thin wire model with (4.1); see (C 2). The panels in (b) show a zoom of the panels in (a). (Online version in colour.)

Footnotes

1

In dimensional form, ε is replaced by h in (2.5), since ε(/x1)=h(/x1).

2
In non-dimensional form and with L=D, hence x1=x1/D(1,0) (ε=h/D and Kn*=(nπ)2, K=(kcθD)2
{p(x1)=m=1+4iK3/2sin (mπx1)mπ(K(mπ)2)2iK(1+x1),pn*(x1)=2sin (nπx1),Pn*(x1)=einπx1einπx1,P+(x1)=2nπeinπx1,P(x1)=22(mn,m=1+n/msin (mπx1)1(m/n)2+sin (nπx1))2nπ(1+x1).
3

The off-resonance case: (4.4) reads pε(x1)=m=1+4iεA(Kmπ)3sin (mπx1)(K/mπ)212iεAK(1+x1) in non-dimensional form, which coincides with pap(x1)=2ikcθhAsin (kcθD)sin (kcθ(x1+D))+O(ε2) from (4.1) and (4.2) up to O(ε2), using (1+x1)=m2mπsin (mπx1) and sin (K(x1+1))=m2mπsin KK(mπ)2sin (mπx1).

4

The near-resonance case: (4.5) reads pε(x1)2iAsin (nπx1)/(k^+B+ε2k^2), which coincides with pap in (4.1) up to O(ε), using that sin (K(x1+1))=cos(nπ)sin (nπx1)+O(ε) and sin K+εK(cosKisin K)=εnπcos(nπ)(k^+B)+O(ε2).

5

For I we have used that mn,m=1+(2/(1(m/n)2))=3/2 for any n.

6

The on-resonance case: in non-dimensional form (4.6) reads pε(x1)2iAsin (nπx1)/(ε(k~B2+inπA2εBk~+(ε2/2)k~2)), which has the same expansion up to O(1) of pap in (4.1), which reads as pap(x1)=2iAsin (nπx1)/ε(k~B2+i(nπ)A2))+O(1).

7

Denoting Ba=B+(a/h)0, E(α,β)=(Ba(α2+β2)2Aαβ) can be positive if and only if Ba0; in this case, E(α,β) is convex and its minimum with respect to α is Em(β)=1/Ba(Ba2A2)β2. Hence E0 is guaranteed for Ba>|A|>0.

8

The question of the value of a producing the best approximation of the actual solution does not have a theoretical answer. In addition, the answer is not universal: in [12] for a three-phase array distributed on a circle, increasing the values of a produces larger errors; in [17] for a two-phase linear array a minimum of the error was found to occur for a = e; in [18] for a rough Neumann boundary the optimal value was shown to vary with the geometry of the roughness.

Data accessibility

The numerical results of the direct problem in the harmonic regime were obtained using a standard multimodal method as presented in Marigo JJ, Maurel A. 2017 An interface model for homogenization of acoustic metafilms. World Scientific handbook of metamaterials and plasmonics. Volume 2: Elastic, acoustic, and seismic metamaterials (eds R Craster, S Guenneau), pp. 599–645. Singapore: World Scientific. The numerical results in the transient regime were obtained using the FEM-BEM C++ code XLiFE++; see also [15].

Competing interests

We declare we have no competing interests.

Authors' contributions

B.D, J-F.M. and E.L. realized the numerics in the transient regime. A.M. and K.P. realized the numerics in the harmonic regime. All authors participated in the modelling and analysis, contributed to the paper, gave final approval for publication and agree to be held accountable for the work performed herein.

Funding

K.P. is grateful for the support of the Agence de l’Innovation de Défense (AID) from the Direction Générale de l’Armement (DGA), under grant no. 2019 65 0070.

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Data Availability Statement

The numerical results of the direct problem in the harmonic regime were obtained using a standard multimodal method as presented in Marigo JJ, Maurel A. 2017 An interface model for homogenization of acoustic metafilms. World Scientific handbook of metamaterials and plasmonics. Volume 2: Elastic, acoustic, and seismic metamaterials (eds R Craster, S Guenneau), pp. 599–645. Singapore: World Scientific. The numerical results in the transient regime were obtained using the FEM-BEM C++ code XLiFE++; see also [15].


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