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Direct and Inverse scattering in a three-dimensional planar waveguide

Yan Chang School of Mathematics, Harbin Institute of Technology, Harbin 150000, China, ([email protected]).    Yukun Guo School of Mathematics, Harbin Institute of Technology, Harbin 150000, China, ([email protected]).    Yue Zhao School of Mathematics and Statistics, Central China Normal University, Wuhan 430079, China, ([email protected]).
Abstract

In this paper, we study the direct and inverse scattering of the Schrödinger equation in a three-dimensional planar waveguide. For the direct problem, we derive a resonance-free region and resolvent estimates for the resolvent of the Schrödinger operator in such a geometry. Based on the analysis of the resolvent, several inverse problems are investigated. First, given the potential function, we prove the uniqueness of the inverse source problem with multi-frequency data. We also develop a Fourier-based method to reconstruct the source function. The capability of this method is numerically illustrated by examples. Second, the uniqueness and increased stability of an inverse potential problem from data generated by incident waves are achieved in the absence of the source function. To derive the stability estimate, we use an argument of quantitative analytic continuation in complex theory. Third, we prove the uniqueness of simultaneously determining the source and potential by active boundary data generated by incident waves. In these inverse problems, we only use the limited lateral Dirichlet boundary data at multiple wavenumbers within a finite interval.

Keywords: Schrödinger equation, waveguide, scattering resonances, inverse scattering, uniqueness, Fourier method

1 Introduction

We consider the direct and inverse scattering problems in a three-dimensional planar waveguide. Let D3D\subset\mathbb{R}^{3} be an infinite slab between two parallel hyperplanes Γ+\Gamma^{+} and Γ\Gamma^{-} with width LL. Without loss of generality, we assume that

D={x=(x~,x3)3:x~=(x1,x2)2, 0<x3<L},L>0,D=\{x=(\tilde{x},x_{3})\in\mathbb{R}^{3}:\tilde{x}=(x_{1},x_{2})\in\mathbb{R}^{2},\ 0<x_{3}<L\},\quad L>0,

and

Γ+={x3:x3=L},Γ={x3:x3=0}.\Gamma^{+}=\{x\in\mathbb{R}^{3}:x_{3}=L\},\quad\Gamma^{-}=\{x\in\mathbb{R}^{3}:x_{3}=0\}.

Consider the following Schrödinger equation

Δu+Vuk2u=f,inD,-\Delta u+Vu-k^{2}u=f,\quad\text{in}\ D, (1)

where k>0k>0 is the wavenumber, VV is the potential function, and ff is the source function. Let B~R={x~2:|x~|R}\widetilde{B}_{R}=\{\tilde{x}\in\mathbb{R}^{2}:|\tilde{x}|\leq R\} be a two-dimensional disk and CR=B~R×[0,L]C_{R}=\widetilde{B}_{R}\times[0,L] be a cylinder in the waveguide. Denote the lateral boundary of CRC_{R} by ΓR=B~R×[0,L]\Gamma_{R}=\partial\widetilde{B}_{R}\times[0,L]. Assume that both fL2(D)f\in L^{2}(D) and VL(D)V\in L^{\infty}(D) are compactly supported in CRC_{R}. We also assume that the potential function VV is invariant in the x3x_{3}-variable, i.e., V=V(x~)V=V(\tilde{x}). Let uu satisfy the Neumann and Dirichlet boundary conditions, respectively,

ux3=0onΓ+,u=0onΓ.\frac{\partial u}{\partial x_{3}}=0\quad\text{on}\,\,\Gamma^{+},\quad u=0\quad\text{on}\,\,\Gamma^{-}. (2)

An important application of this waveguide problem is to provide a simplified but effective model for the propagation of time-harmonic acoustic waves in the ocean [1, 8]. In this model, the Dirichlet boundary condition models the surface of the ocean, while the Neumann boundary condition models the seabed underneath. In this paper, we begin by analyzing the direct scattering problem to seek a resonance-free region and derive the resolvent estimates for the resolvent (Δλ2+V)1(-\Delta-\lambda^{2}+V)^{-1} of the Schrödinger operator in the waveguide. These studies enable us to gain some insights into the inverse problems. As an application of the resolvent estimates, we continue to study the inverse problems of determining the source and potential functions from the knowledge of the scattered field measured on ΓR\Gamma_{R} corresponding to the wavenumber given in a finite interval. The framework developed in this paper is unified and can be applied to the configuration of a tubular waveguide.

ffx1x_{1}x2x_{2}x3x_{3}B~R\tilde{B}_{R}DDCRC_{R}OOLLRRΓR\Gamma_{R}Γ+\Gamma^{+}Γ\Gamma^{-}
Figure 1: An illustration of the scattering problem in the waveguide.

The direct scattering problems in a planar waveguide corresponding to a positive wavenumber have been well studied in the literature. In this case, resonances may occur at a sequence of special frequencies, and this fact leads to the non-uniqueness of the direct problem [2]. However, the analysis of the scattering resonances for the resolvent (Δλ2+V)1(-\Delta-\lambda^{2}+V)^{-1} in this geometry remains open. In scattering theory, the resonances are considered to be the poles of the meromorphic extension of the resolvent with respect to λ\lambda which could be a complex number. The phenomenon of scattering resonances naturally occurs and has significant applications in a wide range of scientific and engineering areas. For instance, the properties of scattering resonances can be applied to long-time asymptotics of the wave equation, which leads to resonance expansions of waves [11]. In this paper, we analyze the direct scattering and derive a resonance-free region and resolvent estimates for the resolvent of the Schrödinger operator in a three-dimensional planar waveguide.

The existing results on the inverse source problem in a waveguide are mainly focused on the delta-type/point-like sources and numerics [6, 7, 19, 20]. In [21], the author studied the inverse problem of qualitatively recovering the support of a source function by the multi-frequency far-field pattern with certain assumptions on the source function. To our knowledge, this article makes the novel attempt to establish the theoretical foundation and provide a feasible numerical scheme for quantitatively determining a general source function in the waveguide. We refer to [13, 18] and the references cited therein for the corresponding inverse boundary value problems, where the data is the Dirichlet-to-Neumann (DtN) map and the main mathematical tool is the construction of complex geometric optics (CGO) solutions. In this paper, since multi-wavenumber data is available, our treatment does not resort to the construction of CGO solutions.

The first part of this paper is concerned with the direct problem. In our setting, the direct problem is to investigate the resolvent (Δλ2+V)1(-\Delta-\lambda^{2}+V)^{-1} where λ\lambda could be complex. Unfortunately, as discussed above, the scattering waveguides have a special feature that is not present in free space: there may exist a sequence of scattering resonances for which the uniqueness of solutions does not hold. Another special feature is that the scattered field consists of an infinite number of exponentially decaying evanescent modes. This will bring difficulty in the analytic continuation of the resolvent to the lower-half complex plane. To resolve this issue, we assume that the source function only admits a finite number of Fourier modes with respect to the x3x_{3} variable. As a consequence, the scattered field also consists of a finite number of Fourier modes. We derive the desired resonance-free region and resolvent estimates by studying the analytic continuation of the complex wavenumber corresponding to each mode and applying the recent results on the resolvent of the Schrödinger operator in the free two-dimensional space in [27]. As a special case, we also consider the free resolvent (Δλ2)1(-\Delta-\lambda^{2})^{-1}. In this case, we show that a larger sectorial analytic domain can be obtained in the absence of the potential function.

The study of direct scattering problems paves the way for delving into the inverse problems. The second part of this paper is devoted to three prototypical inverse scattering problems: recovering respectively the source ff, the potential VV, and the co-recovery of both ff and VV. The aforementioned analysis of the resolvent is indispensable in establishing the stability of the inverse problems. For the inverse scattering problems by using multi-wavenumber data, a key question shall be usually answered: whether one can find a resonance-free region that contains an infinite interval of the positive real axis. If this is true, then one can apply the analytic continuation principle. Based upon the analysis of the resolvent, the stability and uniqueness issues of the three inverse problems are mathematically investigated. The analysis employs the limited lateral near-field Dirichlet data on ΓR\Gamma_{R} at multiple frequencies.

For the first inverse problem of determining the source with known potential, we establish the theoretical results of uniqueness and stability. For such problems, the use of multi-wavenumber is usually necessary to overcome the non-uniqueness issue [4]. We construct an orthogonal basis in L2(CR)L^{2}(C_{R}) and deduce integral equations that connect the scattering data and the source function. As a consequence, we derive uniqueness for the inverse source problem. Similar techniques can be found in, e.g.,[3]. In particular, in the case V=0V=0, we develop a numerical scheme to reconstruct the source from the multi-frequency radiated field. The proposed approach can be viewed as a novel extension of the Fourier method for solving the multi-frequency inverse source problem of acoustic wave [28]. The Fourier method has been applied to the inverse source problems for electromagnetic wave [23, 24], elastic wave [22, 26], and recently the biharmonic wave [9]. Nevertheless, it is not trivial to design the Fourier method for recovering the source in the waveguide because different Fourier modes inherently intertwine with each other. To tackle this obstruction, we adopted the variable separation strategy to first represent the radiated field via a series expression, with the expansion coefficients corresponding to the Fourier modes. Then the Fourier method can be adopted to reconstruct the Fourier modes of the source function, and thus the series expansions can be used as the reconstruction. In addition, it deserves noting that, compared with the direct problem where we assume that the source function only admits a finite number of Fourier modes for the x3x_{3} variable, the Fourier method developed here is feasible for recovering a more general source. Furthermore, we also discuss the extension of the inverse source problem with far-field data.

Next, we consider the inverse potential problem in the absence of the source function, we prove the uniqueness and increasing stability of the inverse potential problem by the scattered field generated by incident waves. The proof relies on the resolvent estimate and does not resort to the method of constructing CGO solutions as in [13, 18] since multi-wavenumber data is available. Based on the resonance-free region and resolvent estimates, the increased stability is obtained by applying an argument of analytic continuation developed in [27].

The last inverse problem is the more challenging co-inversion from the active boundary measurements generated by both the endogenous source and the exogenous excitation waves. We show that the unknown potential and source can be uniquely determined simultaneously. For the simultaneous determination of the source and potential of the random Schrödinger equation in free space, we refer the reader to [14, 15]. We also refer to [5] for the simultaneous recovery of a potential and a point source in the Schrödinger equation from Cauchy data. Note that a promising feature of the current study is that only limited-aperture Dirichlet boundary measurements at multiple wavenumbers are needed throughout the analysis.

The rest of the paper is organized as follows. Section 2 is concerned with the direct scattering problem. An analytic domain and resolvent estimates of the resolvent in the waveguide are derived. Sections 3 to 5 are dedicated to the inverse problems with the help of the analysis of the resolvent. First, we consider theoretical uniqueness and develop a numerical method for the inverse source problem in section 3. Then, in the absence of the source function, the inverse potential scattering problem is investigated in section 4. The third inverse problem of identifying the source-potential pair is tackled in section 4. Here we present a uniqueness result of simultaneously recovering the source and potential by active measurements. Finally, we conclude this article by summarizing the contributions and shedding light on future works in section 6.

2 Direct scattering

In this section, we investigate the resolvent in the planar waveguide. Consider the following Schrödinger equation

Δu+Vuλ2u=f,λ+.-\Delta u+Vu-\lambda^{2}u=f,\quad\lambda\in\mathbb{R}^{+}. (3)

Denote the resolvent by

RV(λ)=(Δλ2+V)1R_{V}(\lambda)=(-\Delta-\lambda^{2}+V)^{-1}

which gives

u(x,λ)=RV(λ)f(x).u(x,\lambda)=R_{V}(\lambda)f(x).

We carry out the separation of variables in x~\tilde{x} and x3x_{3} for the scattered field and the source functions, which leads to series expansions as follows

u(x~,x3)=n=1un(x~)sin(αnx3),f(x~,x3)=n=1fn(x~)sin(αnx3),u(\tilde{x},x_{3})=\sum_{n=1}^{\infty}u_{n}(\tilde{x})\sin(\alpha_{n}x_{3}),\quad f(\tilde{x},x_{3})=\sum_{n=1}^{\infty}f_{n}(\tilde{x})\sin(\alpha_{n}x_{3}), (4)

with αn=(2n1)π2L\alpha_{n}=\frac{(2n-1)\pi}{2L} and the modes unu_{n} of uu and fnf_{n} of ff are given by

un(x~)=2L0Lu(x)sin(αnx3)dx3,fn(x~)=2L0Lf(x)sin(αnx3)dx3.\displaystyle u_{n}(\tilde{x})=\frac{2}{L}\int_{0}^{L}u(x)\sin(\alpha_{n}x_{3}){\rm d}x_{3},\quad f_{n}(\tilde{x})=\frac{2}{L}\int_{0}^{L}f(x)\sin(\alpha_{n}x_{3}){\rm d}x_{3}. (5)

The modes unu_{n} are required to satisfy the two-dimensional Helmholtz equation

Δx~unβn2(λ)un+Vun=fn-\Delta_{\tilde{x}}u_{n}-\beta_{n}^{2}(\lambda)u_{n}+Vu_{n}=f_{n} (6)

where

βn2(λ)=λ2αn2withβn(λ)0,\beta_{n}^{2}(\lambda)=\lambda^{2}-\alpha_{n}^{2}\,\,\text{with}\,\,\Im\beta_{n}(\lambda)\geq 0,

and the Sommerfeld radiation condition proposed in [12]

limrr1/2(runiβnun)=0,r=|x~|.\displaystyle\lim_{r\to\infty}r^{1/2}(\partial_{r}u_{n}-{\rm i}\beta_{n}u_{n})=0,\quad r=|\tilde{x}|. (7)

Denote the resolvent of the Schrödinger operator Δx~λ2+V-\Delta_{\tilde{x}}-\lambda^{2}+V in two dimensions by

R~V(λ)=(Δx~λ2+V)1.\widetilde{R}_{V}(\lambda)=(-\Delta_{\tilde{x}}-\lambda^{2}+V)^{-1}.

Thus, we have a formal representation of the resolvent

RV(λ)(f)=n=1R~V(βn(λ))(fn)sin(αnx3),λ+\n=0{αn}.\displaystyle R_{V}(\lambda)(f)=\sum_{n=1}^{\infty}\widetilde{R}_{V}(\beta_{n}(\lambda))(f_{n})\sin(\alpha_{n}x_{3}),\quad\lambda\in{\mathbb{R}}^{+}\backslash\cup_{n=0}^{\infty}\{\alpha_{n}\}. (8)

In what follows, we shall delineate the analyticity of R~V(βn(λ))\widetilde{R}_{V}(\beta_{n}(\lambda)) and its resolvent estimates concerning complex λ\lambda.

2.1 Analytic continuation

In this subsection, we would resort to the analytic continuation technique to extend the domain of βn(λ)\beta_{n}(\lambda) from λ+\lambda\in\mathbb{R}^{+} to the complex plane such that βn(λ)\beta_{n}(\lambda) is complex analytic. Let λ=λ1+iλ2\lambda=\lambda_{1}+{\rm i}\lambda_{2}\in\mathbb{C}. We have

βn2(λ1,λ2)=γn+iη\beta_{n}^{2}(\lambda_{1},\lambda_{2})=\gamma_{n}+{\rm i}\eta

where

γn=λ12λ22αn2,η=2λ1λ2.\gamma_{n}=\lambda_{1}^{2}-\lambda_{2}^{2}-\alpha_{n}^{2},\quad\eta=2\lambda_{1}\lambda_{2}. (9)

Moreover, a direct calculation yields

βn(λ1,λ2)=an(λ1,λ2)+ibn(λ1,λ2),forλ10,λ20,\beta_{n}(\lambda_{1},\lambda_{2})=a_{n}(\lambda_{1},\lambda_{2})+{\rm i}b_{n}(\lambda_{1},\lambda_{2}),\quad\text{for}\,\,\lambda_{1}\geq 0,\,\,\lambda_{2}\geq 0,

where

an(λ1,λ2)=(γn2+η2+γn2)1/2,bn(λ1,λ2)=(γn2+η2γn2)1/2.\displaystyle a_{n}(\lambda_{1},\lambda_{2})=\left(\frac{\sqrt{\gamma_{n}^{2}+\eta^{2}}+\gamma_{n}}{2}\right)^{1/2},\quad b_{n}(\lambda_{1},\lambda_{2})=\left(\frac{\sqrt{\gamma_{n}^{2}+\eta^{2}}-\gamma_{n}}{2}\right)^{1/2}.

Now we extend the real analytic functions ana_{n} and bnb_{n} analytically from the first quadrant {λ10,λ20}\{\lambda_{1}\geq 0,\,\lambda_{2}\geq 0\} to 2[αn,αn]\mathbb{R}^{2}\setminus[-\alpha_{n},\alpha_{n}] by excluding the resonance αn\alpha_{n}, which will lead to the complex analyticity of βn(λ)\beta_{n}(\lambda). First, noting that λ2an(λ1,λ2)=0\partial_{\lambda_{2}}a_{n}(\lambda_{1},\lambda_{2})=0 and bn(λ1,λ2)=0b_{n}(\lambda_{1},\lambda_{2})=0 on {λ2:λ2=0}[αn,αn]\{\lambda\in\mathbb{R}^{2}:\lambda_{2}=0\}\setminus[-\alpha_{n},\alpha_{n}], we apply the even extension to an(λ1,λ2)a_{n}(\lambda_{1},\lambda_{2}) and the odd extension to bn(λ1,λ2)b_{n}(\lambda_{1},\lambda_{2}) with respect to the variable λ2\lambda_{2} which gives the analytic extensions of ana_{n} and bnb_{n} from the first quadrant to the right half plane {λ10}[0,αn]\{\lambda_{1}\geq 0\}\setminus[0,\alpha_{n}] as follows

βn(λ1,λ2)={an(λ1,λ2),λ20,an(λ1,λ2),λ2<0,\displaystyle\Re\beta_{n}(\lambda_{1},\lambda_{2})=\begin{cases}a_{n}(\lambda_{1},\lambda_{2}),\quad&\lambda_{2}\geq 0,\\[2.0pt] a_{n}(\lambda_{1},-\lambda_{2}),\quad&\lambda_{2}<0,\end{cases}

and

βn(λ1,λ2)={bn(λ1,λ2),λ20,bn(λ1,λ2),λ2<0.\displaystyle\Im\beta_{n}(\lambda_{1},\lambda_{2})=\begin{cases}b_{n}(\lambda_{1},\lambda_{2}),\quad&\lambda_{2}\geq 0,\\[2.0pt] -b_{n}(\lambda_{1},-\lambda_{2}),\quad&\lambda_{2}<0.\end{cases}

Next, noting that an(λ1,λ2)=0a_{n}(\lambda_{1},\lambda_{2})=0 and λ1bn(λ1,λ2)=0\partial_{\lambda_{1}}b_{n}(\lambda_{1},\lambda_{2})=0 on the axis {λ2:λ1=0}\{\lambda\in\mathbb{R}^{2}:\lambda_{1}=0\}, we apply the odd extension to an(λ1,λ2)a_{n}(\lambda_{1},\lambda_{2}) and the even extension to bn(λ1,λ2)b_{n}(\lambda_{1},\lambda_{2}) with respect to the variable λ1\lambda_{1} by

βn(λ1,λ2)={an(λ1,λ2),λ10,an(λ1,λ2),λ1<0,\displaystyle\Re\beta_{n}(\lambda_{1},\lambda_{2})=\begin{cases}a_{n}(\lambda_{1},\lambda_{2}),\quad&\lambda_{1}\geq 0,\\[2.0pt] -a_{n}(-\lambda_{1},\lambda_{2}),\quad&\lambda_{1}<0,\end{cases}

and

βn(λ1,λ2)={bn(λ1,λ2),λ10,bn(λ1,λ2),λ1<0.\displaystyle\Im\beta_{n}(\lambda_{1},\lambda_{2})=\begin{cases}b_{n}(\lambda_{1},\lambda_{2}),\quad&\lambda_{1}\geq 0,\\[2.0pt] b_{n}(-\lambda_{1},\lambda_{2}),\quad&\lambda_{1}<0.\end{cases}

In this way, we analytically extend ana_{n} and bnb_{n} to the left half plane {λ10}[αn,0]\{\lambda_{1}\leq 0\}\setminus[-\alpha_{n},0]. Therefore, the real part βn(λ1,λ2)\Re\beta_{n}(\lambda_{1},\lambda_{2}) and imaginary part βn(λ1,λ2)\Im\beta_{n}(\lambda_{1},\lambda_{2}) are both extended as real analytic functions for λ2[αn,αn]\lambda\in\mathbb{R}^{2}\setminus[-\alpha_{n},\alpha_{n}]. As a consequence of the above extension, we can show that βn(λ)=βn(λ1,λ2)+iβn(λ1,λ2)\beta_{n}(\lambda)=\Re\beta_{n}(\lambda_{1},\lambda_{2})+{\rm i}\Im\beta_{n}(\lambda_{1},\lambda_{2}) is complex analytic for λ=λ1+iλ2[αn,αn]\lambda=\lambda_{1}+{\rm i}\lambda_{2}\in\mathbb{C}\setminus[-\alpha_{n},\alpha_{n}] by the Cauchy-Riemann equations

λ1an(λ1,λ2)=λ2bn(λ1,λ2),λ2an(λ1,λ2)=λ1bn(λ1,λ2).\partial_{\lambda_{1}}a_{n}(\lambda_{1},\lambda_{2})=\partial_{\lambda_{2}}b_{n}(\lambda_{1},\lambda_{2}),\quad\partial_{\lambda_{2}}a_{n}(\lambda_{1},\lambda_{2})=-\partial_{\lambda_{1}}b_{n}(\lambda_{1},\lambda_{2}).

Notice that based on the above analytic extension of βn(λ)\beta_{n}(\lambda), the imaginary part βn(λ)\Im\beta_{n}(\lambda) is negative in \mathbb{C}^{-} now. Therefore, for large αn\alpha_{n} the kernel of R~0(βn(λ))\widetilde{R}_{0}(\beta_{n}(\lambda)) satisfies

H0(1)(βn(λ)|x~y~|)eαn|x~y~|,H_{0}^{(1)}(\beta_{n}(\lambda)|\tilde{x}-\tilde{y}|)\sim\mathrm{e}^{\alpha_{n}|\tilde{x}-\tilde{y}|}, (10)

Throughout, Hm(1)H_{m}^{(1)} denotes the Hankel function of the first kind of order mm. The asymptotic behavior (10) implies that the series in (8) may not converge. To resolve this issue and study the analytic continuation of the resolvent RV(λ)R_{V}(\lambda), we shall make the following assumption:

  • (A)

    The source function f(x)f(x) has only a finite number of modes defined in (5), i.e., there exits a positive integer N0>0N_{0}>0 such that

    f(x)=n=1N0fn(x~)sin(αnx3).f(x)=\sum_{n=1}^{N_{0}}f_{n}(\tilde{x})\sin(\alpha_{n}x_{3}).

2.2 Resolvent estimates

Based on the preparations in the previous subsection, we are now ready to establish several crucial estimates on the resolvent. We begin with a few notations. For θ(0,π2)\theta\in(0,\frac{\pi}{2}), denote the sectorial domain SθS_{\theta} by

Sθ={z:argz(θ,θ)(πθ,π+θ),z0}.S_{\theta}=\{z\in\mathbb{C}:\arg z\in(-\theta,\theta)\cup(\pi-\theta,\pi+\theta),\ z\neq 0\}.

Hereafter, we denote by t:=max{t,0}t_{-}:=\max\{-t,0\} and diam(suppρ):=sup{|x~y~|:x~,y~suppρ}{\rm diam}({\rm supp}\rho):=\sup\{|\tilde{x}-\tilde{y}|:\tilde{x},\tilde{y}\in{\rm supp}\rho\} for ρC0(2)\rho\in C_{0}^{\infty}(\mathbb{R}^{2}). We also sometimes simplify the relation “aCba\leq Cb” as “aba\lesssim b” with a nonessential constant C>0C>0 that might differ at each occurrence.

The following proposition concerns the analytic continuation of the free resolvent R~V(z)=(Δx~z2+V)1\widetilde{R}_{V}(z)=(-\Delta_{\tilde{x}}-z^{2}+V)^{-1} in two dimensions.

Proposition 2.1.

[27, Theorem 3] Let ρC0(2)\rho\in C_{0}^{\infty}(\mathbb{R}^{2}) with ρ=1\rho=1 on suppV\mathrm{supp}V. The resolvent ρR~V(z)ρ\rho\widetilde{R}_{V}(z)\rho is a meromorphic family of operators in SθS_{\theta}. Moreover, ρR~V(z)ρ\rho\widetilde{R}_{V}(z)\rho is analytic for zSθΩδz\in S_{\theta}\cap\Omega_{\delta} with the following resolvent estimates

ρR~V(z)ρL2(2)Hj(2)|z|1/2(1+|z|2)j/2eL(z),j=0,1,2,\displaystyle\|\rho\widetilde{R}_{V}(z)\rho\|_{L^{2}(\mathbb{R}^{2})\rightarrow H^{j}(\mathbb{R}^{2})}\lesssim|z|^{-1/2}(1+|z|^{2})^{j/2}\mathrm{e}^{L(\Im z)_{-}},\quad j=0,1,2,

where L>diam(suppρ)L>{\rm diam}({\rm supp}\rho). Here Ωδ\Omega_{\delta} is defined as

Ωδ:={z:zδlog(1+|z|),|z|C0},\displaystyle\Omega_{\delta}:=\{z:{\Im}z\geq-\delta{\rm log}(1+|z|),\ |z|\geq C_{0}\},

where C0C_{0} is a positive constant and δ\delta satisfies 0<δ<14L0<\delta<\frac{1}{4L}. In particular, there are only finitely many poles in the domain

{z:zδlog(1+|z|),|z|C0}Sθ.\{z\in\mathbb{C}:{\Im}z\geq-\delta{\rm log}(1+|z|),\ |z|\leq C_{0}\}\cap S_{\theta}.

We represent the solution to (6)–(7) by un=R~V(βn(λ))fnu_{n}=\widetilde{R}_{V}(\beta_{n}(\lambda))f_{n}. Let MM and hh be positive constants such that M>αN0M>\alpha_{N_{0}}, and denote the strip \mathcal{R} by :=[M,+)×[h,h]\mathcal{R}:=[M,+\infty)\times[-h,h]. We next show that βn(λ)SθΩδ\beta_{n}(\lambda)\in S_{\theta}\cap\Omega_{\delta} which is complex analytic for λ\lambda\in\mathcal{R}\cup-\mathcal{R} with appropriate choices of hh and MM. From the analytic extension discussed above, βn(λ)\beta_{n}(\lambda) is complex analytic in [αN0,αN0]\mathbb{C}\setminus[-\alpha_{N_{0}},\alpha_{N_{0}}]. For hh being sufficiently small and MM being sufficiently large, we have γn>0\gamma_{n}>0 in (9) and then |βn||βn||\Im\beta_{n}|\leq|\Re\beta_{n}| for λ\lambda\in\mathcal{R}\cup-\mathcal{R} which yields βnSθΩδ\beta_{n}\in S_{\theta}\cap\Omega_{\delta}. We can also have |βn|>C0|\Re\beta_{n}|>C_{0} where C0C_{0} is specified in Proposition 2.1. Moreover, the following estimate holds

|βn(λ)|=(γn2+η2γn2)1/2h|λ1|.|\Im\beta_{n}(\lambda)|=\left(\frac{\sqrt{\gamma_{n}^{2}+\eta^{2}}-\gamma_{n}}{2}\right)^{1/2}\lesssim h|\lambda_{1}|.

As a consequence, the resolvent R~V(βn(λ)):Lcomp2(2)Hlocj(2)\widetilde{R}_{V}(\beta_{n}(\lambda)):L_{\rm comp}^{2}(\mathbb{R}^{2})\rightarrow H^{j}_{\rm loc}(\mathbb{R}^{2}) is analytic for λ\lambda\in\mathcal{R}\cup-\mathcal{R} with the following resolvent estimates given a fixed ρC0(2)\rho\in C_{0}^{\infty}(\mathbb{R}^{2})

ρR~V(βn(λ))ρL2(2)Hj(2)C|λ|1/2(1+|λ|2)j/2eC|λ|,j=0,1,2.\|\rho\widetilde{R}_{V}(\beta_{n}(\lambda))\rho\|_{L^{2}(\mathbb{R}^{2})\rightarrow H^{j}(\mathbb{R}^{2})}\leq C|\lambda|^{-1/2}(1+|\lambda|^{2})^{j/2}\mathrm{e}^{C|\lambda|},\quad j=0,1,2.

Noting

RV(λ)=n=1N0R~V(βn(λ))(fn),R_{V}(\lambda)=\sum_{n=1}^{N_{0}}\widetilde{R}_{V}(\beta_{n}(\lambda))(f_{n}),

we have the following theorem which provides a resonance-free region and resolvent estimates in the geometry of a planar waveguide. It will play an important role in the subsequent study of the inverse problem.

Theorem 2.1.

Let ηC0(D)\eta\in C_{0}^{\infty}(D) with η=1\eta=1 on suppV\text{supp}V and let ff satisfy Assumption (A). There exist M>0M>0 and h>0h>0 such that the resolvent ηRV(λ)η:L2(D)L2(D)\eta R_{V}(\lambda)\eta:L^{2}(D)\rightarrow L^{2}(D) is an analytic family of operators for λ\lambda\in\mathcal{R}\cup-\mathcal{R} with the following resolvent estimates

ηRV(λ)ηfL2(D)Hj(D)C|λ|1/2(1+|λ|2)j/2eC|λ|fL2(D),j=0,1,2,\displaystyle\|\eta R_{V}(\lambda)\eta f\|_{L^{2}(D)\rightarrow H^{j}(D)}\leq C|\lambda|^{-1/2}(1+|\lambda|^{2})^{j/2}\mathrm{e}^{C|\lambda|}\|f\|_{L^{2}(D)},\quad j=0,1,2,

where CC is a positive constant.

In what follows, we consider the case that V=0V=0. More precisely, we investigate the free resolvent R0(λ)=(Δλ2)1R_{0}(\lambda)=(-\Delta-\lambda^{2})^{-1}. We will see that in this case, the free resolvent has a larger analytic domain.

The following proposition concerns the analytic continuation of the free resolvent R~0(z)=(Δx~z2)1\widetilde{R}_{0}(z)=(-\Delta_{\tilde{x}}-z^{2})^{-1} in 2\mathbb{R}^{2}.

Proposition 2.2.

[27, Theorem 10]The free resolvent R~0(z)\widetilde{R}_{0}(z) is analytic for zSθ,z>0z\in S_{\theta},\Im z>0 as a family of operators

R~0(z):L2(2)L2(2)\displaystyle\widetilde{R}_{0}(z):L^{2}(\mathbb{R}^{2})\to L^{2}(\mathbb{R}^{2})

where R~0(z)L2(2)L2(2)=𝒪(1/|z|1/2)\|\widetilde{R}_{0}(z)\|_{L^{2}(\mathbb{R}^{2})\to L^{2}(\mathbb{R}^{2})}=\mathcal{O}(1/|z|^{1/2}). Moreover, for each ρC0(2)\rho\in C_{0}^{\infty}(\mathbb{R}^{2}) the free resolvent R0(λ)R_{0}(\lambda) extends to a family of analytic operators for zSθz\in S_{\theta} as follows

ρR~0(z)ρ:L2(2)L2(2)\displaystyle\rho\widetilde{R}_{0}(z)\rho:L^{2}(\mathbb{R}^{2})\to L^{2}(\mathbb{R}^{2})

with the resolvent estimates

ρR~0(z)ρL2(2)Hj(2)|z|1/2(1+|z|2)j/2eL(z),j=0,1,2,\displaystyle\|\rho\widetilde{R}_{0}(z)\rho\|_{L^{2}(\mathbb{R}^{2})\rightarrow H^{j}(\mathbb{R}^{2})}\lesssim|z|^{-1/2}(1+|z|^{2})^{j/2}\mathrm{e}^{L(\Im z)_{-}},\quad j=0,1,2,

where L>diam(suppρ)L>{\rm diam}({\rm supp}\rho).

We denote the solution to (6)–(7) when V=0V=0 by un(x~,λ)=R~0(βn(λ))fn(x~)u_{n}(\tilde{x},\lambda)=\widetilde{R}_{0}(\beta_{n}(\lambda))f_{n}(\tilde{x}). We next prove that the resolvent R~0(βn(λ)):Lcomp2(2)Lloc2(2)\widetilde{R}_{0}(\beta_{n}(\lambda)):L^{2}_{\rm comp}(\mathbb{R}^{2})\to L^{2}_{\rm loc}(\mathbb{R}^{2}) is an analytic family of bounded operators for λSθ[αN0,αN0]\lambda\in S_{\theta}\setminus[-\alpha_{N_{0}},\alpha_{N_{0}}]. To achieve this goal, it suffices to show that the range of βn(λ)\beta_{n}(\lambda) is contained in some sectorial domain Sθ1S_{\theta_{1}} for λSθ[αN0,αN0]\lambda\in S_{\theta}\setminus[-\alpha_{N_{0}},\alpha_{N_{0}}]. Indeed, from the analytic extension discussed above, βn(λ)\beta_{n}(\lambda) is complex analytic in [αN0,αN0]\mathbb{C}\setminus[-\alpha_{N_{0}},\alpha_{N_{0}}]. As a result, we have that R~0(βn(λ))\widetilde{R}_{0}(\beta_{n}(\lambda)) is analytic for λSθ[αN0,αN0]\lambda\in S_{\theta}\setminus[-\alpha_{N_{0}},\alpha_{N_{0}}] since R~0(z)\widetilde{R}_{0}(z) is analytic for zSθ1z\in S_{\theta_{1}}.

Since λS[αN0,αN0]\lambda\in S\setminus[-\alpha_{N_{0}},\alpha_{N_{0}}], we have that there exists some c>0c>0 such that |λ|c|λ||\Im\lambda|\leq c|\Re\lambda|. Thus, the ratio of |βn||\Im\beta_{n}| and |βn||\Re\beta_{n}| satisfies

lim¯|λ||λ||λ|=lim¯|λ||bn||an|=c1,λSθ[αN0,αN0],\overline{\lim}_{|\lambda|\to\infty}\frac{|\Im\lambda|}{|\Re\lambda|}=\overline{\lim}_{|\lambda|\to\infty}\frac{|b_{n}|}{|a_{n}|}=c_{1},\quad\lambda\in S_{\theta}\setminus[-\alpha_{N_{0}},\alpha_{N_{0}}],

where c1c_{1} is a finite positive constant. This implies that the range of βn(λ)\beta_{n}(\lambda) is contained in some sectorial domain Sθ1S_{\theta_{1}}. Therefore, we have that R~0(βn(λ))\widetilde{R}_{0}(\beta_{n}(\lambda)) is analytic for λSθ[αN0,αN0]\lambda\in S_{\theta}\setminus[-\alpha_{N_{0}},\alpha_{N_{0}}]. As a consequence, the resolvent R~0(βn(λ)):Lcomp2(2)Hlocj(2)\widetilde{R}_{0}(\beta_{n}(\lambda)):L_{\rm comp}^{2}(\mathbb{R}^{2})\rightarrow H^{j}_{\rm loc}(\mathbb{R}^{2}) is also analytic for λSθ[αN0,αN0]\lambda\in S_{\theta}\setminus[-\alpha_{N_{0}},\alpha_{N_{0}}] with the following resolvent estimates given a fixed ρC0(2)\rho\in C_{0}^{\infty}(\mathbb{R}^{2})

ρR~0(βn(λ))ρL2(2)Hj(2)C|λ|1/2(1+|λ|2)j/2eC|λ|,j=0,1,2.\|\rho\widetilde{R}_{0}(\beta_{n}(\lambda))\rho\|_{L^{2}(\mathbb{R}^{2})\rightarrow H^{j}(\mathbb{R}^{2})}\leq C|\lambda|^{-1/2}(1+|\lambda|^{2})^{j/2}\mathrm{e}^{C|\lambda|},\quad j=0,1,2.

Noting

R0(λ)=n=1N0R~0(βn(λ))(fn)sinαnx3,R_{0}(\lambda)=\sum_{n=1}^{N_{0}}\widetilde{R}_{0}(\beta_{n}(\lambda))(f_{n})\sin\alpha_{n}x_{3},

we have the following theorem for the free resolvent.

Theorem 2.2.

Let ηC0(D)\eta\in C_{0}^{\infty}(D) and let ff satisfy Assumption (A). The resolvent ηR0(λ)η:L2(D)L2(D)\eta R_{0}(\lambda)\eta:L^{2}(D)\rightarrow L^{2}(D) is an analytic family of operators for λSθ\lambda\in S_{\theta} with θ(0,π2)\theta\in(0,\frac{\pi}{2}). Moreover, the following resolvent estimates hold

ηR0(λ)ηfL2(D)Hj(D)C|λ|1/2(1+|λ|2)j/2eC|λ|fL2(D),j=0,1,2,\displaystyle\|\eta R_{0}(\lambda)\eta f\|_{L^{2}(D)\rightarrow H^{j}(D)}\leq C|\lambda|^{-1/2}(1+|\lambda|^{2})^{j/2}\mathrm{e}^{C|\lambda|}\|f\|_{L^{2}(D)},\quad j=0,1,2,

where CC is a positive constant.

3 Inverse problem I: source identification

In this section, we investigate the inverse source problem. The uniqueness of the inverse source problem is established given wavenumbers only in a bounded domain. We also develop a multi-wavenumber numerical scheme to reconstruct the source term from limited aperture Dirichlet boundary measurements. Then several numerical examples are provided to verify the effectiveness of the method. This section ends with an extensional glimpse into the uniqueness in the far-field case.

3.1 Uniqueness

In this subsection, we study the unique determination of the source from multi-wavenumber boundary measurements. We further assume that V0V\geq 0 is a real-valued function.

We consider the spectrum of the Schrödinger operator Δx~+V-\Delta_{\tilde{x}}+V with the Dirichlet boundary condition in B~R\widetilde{B}_{R}. Specifically, we let {μj,ϕj}j=1\{\mu_{j},\phi_{j}\}_{j=1}^{\infty} be the positive increasing eigenvalues and eigenfunctions of Δx~+V-\Delta_{\tilde{x}}+V in B~R\widetilde{B}_{R}, where ϕj\phi_{j} and μj\mu_{j} satisfy

{(Δx~+V)ϕj=μjϕjin B~R,ϕj=0on B~R.\begin{cases}(-\Delta_{\tilde{x}}+V)\phi_{j}=\mu_{j}\phi_{j}&\quad\text{in }\widetilde{B}_{R},\\ \hskip 48.36967pt\phi_{j}=0&\quad\text{on }\partial\widetilde{B}_{R}.\end{cases}

Let kn,j2:=μj+αn2,1nN0,j+k^{2}_{n,j}:=\mu_{j}+\alpha_{n}^{2},1\leq n\leq N_{0},j\in\mathbb{N}^{+} denote the eigenfrequencies. To properly formulate the inverse source problem, we additionally require that kn,j{αi}i=1N0k_{n,j}\notin\{\alpha_{i}\}_{i=1}^{N_{0}} to avoid the resonances. In fact, due to the finiteness of the resonances {αn}n=1N\{\alpha_{n}\}_{n=1}^{N}, this requirement could be fulfilled in certain scenarios. For instance, a large width LL of the waveguide would narrow down the range of the resonance distribution, such that the resonances are confined in a small vicinity of zero, and thus we may have kn,jαN0k_{n,j}\geq\alpha_{N_{0}}.

Assume that ϕj\phi_{j} is normalized such that

B~R|ϕj(x~)|2dx~=1.\int_{\widetilde{B}_{R}}|\phi_{j}(\tilde{x})|^{2}{\rm d}\tilde{x}=1.

Since {ϕj(x~)sinαnx3}j+,1nN0\{\phi_{j}(\tilde{x})\sin\alpha_{n}x_{3}\}_{j\in\mathbb{N}^{+},1\leq n\leq N_{0}} forms an orthogonal basis of the space

𝒞Q:={fLcomp2(D):fsatisfies Assumption (A),suppfCR,fL2(D)Q},\mathcal{C}_{Q}:=\{f\in L_{\rm comp}^{2}(D):f\,\,\text{satisfies Assumption (A)},\,\text{supp}f\subset C_{R},\,\|f\|_{L^{2}(D)}\leq Q\},

the orthogonality leads to the spectral decomposition of ff:

f(x)=n=1N0j=1fn,jϕj(x~)sinαnx3withfn,j=CRf(x)ϕj¯(x~)sinαnx3dx.f(x)=\sum_{n=1}^{N_{0}}\sum_{j=1}^{\infty}f_{n,j}\phi_{j}(\tilde{x})\sin\alpha_{n}x_{3}\ \text{with}\ f_{n,j}=\int_{C_{R}}f(x)\overline{\phi_{j}}(\tilde{x})\sin\alpha_{n}x_{3}{\rm d}x.

Let u(x,kn,j)u(x,k_{n,j}) be the radiating solution to (3) with wavenumber kn,jk_{n,j}. Noting the boundary conditions (2), multiplying both sides of (3) by ϕj¯(x~)sinαnx3\overline{\phi_{j}}(\tilde{x})\sin\alpha_{n}x_{3} and integrating by parts over CRC_{R} gives

fn,j\displaystyle f_{n,j} =ΓR(u(x,kn,j)νx~ϕj¯(x~)sinαnx3νx~u(x,kn,j)ϕj¯(x~)sinαnx3)dx~dx3\displaystyle=\int_{\Gamma_{R}}\left(u(x,k_{n,j})\partial_{\nu_{\tilde{x}}}\overline{\phi_{j}}(\tilde{x})\sin\alpha_{n}x_{3}-\partial_{\nu_{\tilde{x}}}u(x,k_{n,j})\overline{\phi_{j}}(\tilde{x})\sin\alpha_{n}x_{3}\right){\rm d}\tilde{x}{\rm d}x_{3}
=B~Run(x~,kn,j)νx~ϕj¯(x~)dx~B~Rνx~un(x~,kn,j)ϕj¯(x~)dx~\displaystyle=\int_{\partial\widetilde{B}_{R}}u_{n}(\tilde{x},k_{n,j})\partial_{\nu_{\tilde{x}}}\overline{\phi_{j}}(\tilde{x}){\rm d}\tilde{x}-\int_{\partial\widetilde{B}_{R}}\partial_{\nu_{\tilde{x}}}u_{n}(\tilde{x},k_{n,j})\overline{\phi_{j}}(\tilde{x})\,{\rm d}\tilde{x}
=B~Run(x~,kn,j)νx~ϕj¯(x~)dx~,\displaystyle=\int_{\partial\widetilde{B}_{R}}u_{n}(\tilde{x},k_{n,j})\partial_{\nu_{\tilde{x}}}\overline{\phi_{j}}(\tilde{x})\,{\rm d}\tilde{x}, (11)

where

un(x~,kn,j)=2L0Lu(x,kn,j)sinαnx3dx3.u_{n}(\tilde{x},k_{n,j})=\frac{2}{L}\int_{0}^{L}u(x,k_{n,j})\sin\alpha_{n}x_{3}{\rm d}x_{3}.

The following lemma [17, Lemma A.2] is useful in the subsequent analysis.

Lemma 3.1.

Let {μj,ϕj}j=1\{\mu_{j},\phi_{j}\}_{j=1}^{\infty} be the eigensystem of Δx~+V-\Delta_{\tilde{x}}+V in B~R\widetilde{B}_{R}. Then it holds

νx~ϕjL2(B~R)2Cμj,\|\partial_{\nu_{\tilde{x}}}\phi_{j}\|^{2}_{L^{2}(\partial\widetilde{B}_{R})}\leq C\mu_{j},

where the positive constant CC is independent of jj.

If given u(x,k)u(x,k) at all eigenfrequencies {kn,j,1nN0,j+}\{k_{n,j},1\leq n\leq N_{0},j\in\mathbb{N}^{+}\}, we have the following Lipschitz stability estimate.

Theorem 3.1.

The following stability estimate holds:

fL2(CR)2n=1N0j=1kn,jun(x~,kn,j)L2(B~R)2.\|f\|^{2}_{L^{2}(C_{R})}\lesssim\sum_{n=1}^{N_{0}}\sum_{j=1}^{\infty}k_{n,j}\|u_{n}(\tilde{x},k_{n,j})\|^{2}_{L^{2}(\partial\widetilde{B}_{R})}.
Proof.

By the integral identity (11) and Lemma 3.1 we have

|fn,j|2kn,jun(x~,kn,j)L2(B~R)2,|f_{n,j}|^{2}\lesssim k_{n,j}\|u_{n}(\tilde{x},k_{n,j})\|^{2}_{L^{2}(\partial\widetilde{B}_{R})},

which completes the proof with the aid of the energy relation

fL2(CR)2=L2n=1N0j=1|fn,j|2.\|f\|^{2}_{L^{2}(C_{R})}=\frac{L}{2}\sum_{n=1}^{N_{0}}\sum_{j=1}^{\infty}|f_{n,j}|^{2}.

The above Lipschitz stability estimate implies the uniqueness of the inverse source problem, but it requires the boundary data at all kn,jk_{n,j}. In practical applications, however, it is more reasonable to collect data only at wavenumbers in a finite interval. By analyticity of the data proved in Theorem 2.1, we establish the following uniqueness result for the inverse source problem with wavenumbers in a finite interval.

Theorem 3.2.

Let fL2(CR)f\in L^{2}(C_{R}) and I:=(M,M+δ)+I:=(M,M+\delta)\subset\mathbb{R}^{+} be an open interval, where MM is the constant specified in Theorem 2.1 and δ\delta is any positive constant. Then the source term ff can be uniquely determined by the multi-frequency data {u(x,k):xΓR,kI}{u(x,kn,j):xΓR,kn,j2M}\{u(x,k):x\in\Gamma_{R},k\in I\}\cup\{u(x,k_{n,j}):x\in\Gamma_{R},k_{n,j}^{2}\leq M\}.

Proof.

Let u(x,k)=0u(x,k)=0 for xΓRx\in\Gamma_{R} and kI{kj:jα}k\in I\cup\{k_{j}:j\in\alpha\}. It suffices to show that f(x)=0f(x)=0. Since u(x,k)u(x,k) is analytic in \mathcal{R} for xΓRx\in\Gamma_{R}, it holds that u(x,k)=0u(x,k)=0 for all k2>Mk^{2}>M. As the data {u(x,kj):xΓR,kn,j2M}\{u(x,k_{j}):x\in\Gamma_{R},k_{n,j}^{2}\leq M\} is also available, we have that

B~Run(x~)νx~ϕj¯dx~=0\int_{\partial\widetilde{B}_{R}}u_{n}(\tilde{x})\partial_{\nu_{\tilde{x}}}\overline{\phi_{j}}\,{\rm d}\tilde{x}=0

for all j+j\in\mathbb{N}^{+} and 1nN01\leq n\leq N_{0}. It follows from (11) that

fn,j=0,j+, 1nN0,f_{n,j}=0,\quad j\in\mathbb{N}^{+},\,1\leq n\leq N_{0},

which implies f=0f=0. ∎

Remark 3.1.

Motivated by (11) and the Fourier method in [28], we aim to approximate the unknown source function by a finite Fourier expansion of the form

fN(x~,x3)=n=1Nj=1Jfn,jϕj(x~)sinαnx3,N,J+.f_{N}(\tilde{x},x_{3})=\sum_{n=1}^{N}\sum_{j=1}^{J}f_{n,j}\phi_{j}(\tilde{x})\sin\alpha_{n}x_{3},\quad N,J\in\mathbb{N}^{+}.

For numerics, Assumption (A) is not necessary.

3.2 Reconstruction algorithm

This subsection deals with the numerical scheme for the null-potential inverse source problem, i.e., recover ff in the case V=0V=0. Now the radiated field uu satisfies the Helmholtz equation

Δuk2u=f,inD-\Delta u-k^{2}u=f,\quad\text{in}\ D (12)

with k+.k\in\mathbb{R}^{+}. Let {kj}j\{k_{j}\}_{j} be a finite number of frequencies, then the multi-frequency inverse source problem under consideration in this subsection is to reconstruct the source function f(x)f(x) in (12) from the measurement {u(x;k):xΓR,k{kj}j}.\{u(x;k):\,x\in\Gamma_{R},\ k\in\{k_{j}\}_{j}\}.

In terms of the series expansions (4), it is readily seen that each Fourier mode un(x~)u_{n}(\widetilde{x}) satisfies the Sommerfeld radiated condition (7) and

Δx~un+βn2(k)un=fn,\displaystyle\Delta_{\widetilde{x}}u_{n}+\beta_{n}^{2}(k)u_{n}=-f_{n}, (13)

where fnf_{n} is the Fourier mode of ff given by (5), and βn(k)=k2αn2\beta_{n}(k)=\sqrt{k^{2}-\alpha_{n}^{2}} with βn(k)0\Im\beta_{n}(k)\geq 0. In addition, the assumption that suppfCR\mathrm{supp}f\subset C_{R}, without loss of generality, implies that there exists V0=(a/2,a/2)2(a>0)V_{0}=(-a/2,a/2)^{2}(a>0) such that suppfnV0B~R.\mathrm{supp}f_{n}\subset V_{0}\subset\widetilde{B}_{R}.

Though the modal wavenumber βn(k)\beta_{n}(k) is determined by kk and αn\alpha_{n}, from another point of view, once αn\alpha_{n} and β\beta are given in advance, the wavenumber kk can be obtained correspondingly through kn,β=αn2+β2k_{n,\beta}=\sqrt{\alpha_{n}^{2}+\beta^{2}}. This further makes it possible to choose β\beta flexibly and it is unnecessary to relate the modal wavenumber β\beta with nn explicitly. In this view, (13) can be rewritten as

Δx~un(x~)+β2un(x~)=fn(x~).\Delta_{\widetilde{x}}u_{n}(\widetilde{x})+\beta^{2}u_{n}(\widetilde{x})=-f_{n}(\widetilde{x}).

Once the mode fnf_{n} is recovered, the source function ff is correspondingly determined uniquely through (4). Thus, in the rest of this subsection, we aim to recover fnf_{n} for n=1,2,n=1,2,\cdots from {un(x;β):xΓR,βN}\{u_{n}(x;\beta):x\in\Gamma_{R},\beta\in\mathcal{B}_{N}\} with N\mathcal{B}_{N} being the set of admissible modal wavenumbers, which is defined by

Definition 3.1 (Admissible modal wavenumbers).

Let N+,N\in\mathbb{N}_{+}, and β+\beta^{*}\in\mathbb{R}_{+} be a small modal wavenumber such that 0<βR<1.0<\beta^{*}R<1. Then the admissible set of modal wavenumbers is given by

N={πa||:2:1||N}{β}.\displaystyle\mathcal{B}_{N}=\left\{\frac{\pi}{a}|\bm{\ell}|:{\bm{\ell}}\in\mathbb{Z}^{2}:1\leq|\bm{\ell}|_{\infty}\leq N\right\}\cup\{\beta^{*}\}.

The basic idea is to approximate fnf_{n} by the following Fourier expansion

fnN(x~)=||Nf^,nϕ(x~)withϕ(x~)=ei2πax~,n=1,2,,\displaystyle f_{n}^{N}(\widetilde{x})=\sum_{|\bm{\ell}|\leq N}\widehat{f}_{{\bm{\ell}},n}\phi_{\bm{\ell}}(\widetilde{x})\ \text{with}\ \phi_{\bm{\ell}}(\widetilde{x})=\mathrm{e}^{\mathrm{i}\frac{2\pi}{a}{\bm{\ell}}\cdot\widetilde{x}},\quad n=1,2,\cdots, (14)

where =(1,2)2{\bm{\ell}}=(\ell_{1},\ell_{2})\in\mathbb{Z}^{2} and ϕ\phi_{\bm{\ell}} are the Fourier basis functions. In eq. 14, f^,n\widehat{f}_{{\bm{\ell}},n} are the Fourier coefficients corresponding to the index \bm{\ell} and the nn-th Fourier mode fnf_{n},

f^,n=1a2V0fn(x~)ϕ¯(x~)dx~,n=1,2,.\displaystyle\widehat{f}_{{\bm{\ell}},n}=\frac{1}{a^{2}}\int_{V_{0}}f_{n}(\widetilde{x})\overline{\phi_{\bm{\ell}}}(\widetilde{x})\mathrm{d}\widetilde{x},\quad n=1,2,\cdots.

Let νρ\nu_{\rho} be the unit outward normal to Γρ:={x~2:|x~|=ρ>R}.\Gamma_{\rho}:=\{\widetilde{x}\in\mathbb{R}^{2}:|\widetilde{x}|=\rho>R\}. Define

wn(x~;β)\displaystyle w_{n}(\widetilde{x};\beta) :=mHm(1)(βρ)Hm(1)(βR)u^β,n,meimθ,x~Γρ,n=1,2,,\displaystyle:=\sum_{m\in\mathbb{Z}}\frac{H_{m}^{(1)}(\beta\rho)}{H_{m}^{(1)}(\beta R)}\widehat{u}_{\beta,n,m}\mathrm{e}^{\mathrm{i}m\theta},\quad\widetilde{x}\in\Gamma_{\rho},\quad n=1,2,\cdots, (15)
νρwn(x~;β)\displaystyle\partial_{\nu_{\rho}}w_{n}(\widetilde{x};\beta) :=mβHm(1)(βρ)Hm(1)(βR)u^β,n,meimθ,x~Γρ,n=1,2,,\displaystyle:=\sum_{m\in\mathbb{Z}}\beta\frac{{H_{m}^{(1)}}^{\prime}(\beta\rho)}{H_{m}^{(1)}(\beta R)}\widehat{u}_{\beta,n,m}\mathrm{e}^{\mathrm{i}m\theta},\quad\widetilde{x}\in\Gamma_{\rho},\quad n=1,2,\cdots, (16)

where βN,\beta\in\mathcal{B}_{N}, and

u^β,n,m=12π02πun(R,θ;β)eimθdθ.\displaystyle\widehat{u}_{\beta,n,m}=\frac{1}{2\pi}\int_{0}^{2\pi}u_{n}(R,\theta;\beta)\mathrm{e}^{-\mathrm{i}m\theta}\,\mathrm{d}\theta.

Following [28], the Fourier coefficients f^,n\widehat{f}_{{\bm{\ell}},n} are explicitly given by

f^,n\displaystyle\widehat{f}_{{\bm{\ell}},n} =1a2Γρ(νρwn(x~;β)+i2πa(νρ)wn(x~;β))ϕ¯(x~)dsx~, 1||N,\displaystyle=\frac{1}{a^{2}}\int_{\Gamma_{\rho}}\left(\partial_{\nu_{\rho}}w_{n}(\widetilde{x};\beta)+\mathrm{i}\frac{2\pi}{a}({\bm{\ell}}\cdot\nu_{\rho})w_{n}(\widetilde{x};\beta)\right)\overline{\phi}_{\bm{\ell}}(\widetilde{x})\,\mathrm{d}s_{\widetilde{x}},\,1\leq|\bm{\ell}|_{\infty}\leq N, (17)
f^𝟎,n\displaystyle\widehat{f}_{{\bm{0}},n} =ϑπa2sinϑπΓρ(νρwn(x~;β)+i2πa(νρ)wn(x~;β))ϕ¯(x~)dsx~\displaystyle=\frac{\vartheta\pi}{a^{2}\sin\vartheta\pi}\int_{\Gamma_{\rho}}\left(\partial_{\nu_{\rho}}w_{n}(\widetilde{x};\beta^{*})+\mathrm{i}\frac{2\pi}{a}({\bm{\ell}}^{*}\cdot\nu_{\rho})w_{n}(\widetilde{x};\beta^{*})\right)\overline{\phi}_{{\bm{\ell}}^{*}}(\widetilde{x})\,\mathrm{d}s_{\widetilde{x}}
ϑπa2sinϑπ1||Nf^,nV0ϕ(x~)ϕ¯(x~)dx~,\displaystyle\quad-\frac{\vartheta\pi}{a^{2}\sin\vartheta\pi}\sum_{1\leq|\bm{\ell}|_{\infty}\leq N}\widehat{f}_{{\bm{\ell}},n}\int_{V_{0}}\phi_{\bm{\ell}}(\widetilde{x})\overline{\phi}_{{\bm{\ell}}^{*}}(\widetilde{x})\,\mathrm{d}\widetilde{x}, (18)

where ϑ\vartheta is a constant such that 0<ϑ<a2π,=(ϑ,0)0<\vartheta<\frac{a}{2\pi},\,{\bm{\ell}}^{*}=(\vartheta,0) and β=πϑa.\beta^{*}=\frac{\pi\vartheta}{a}. Hence,

fN(x~,x3)=2Ln=1fnN(x~)sin(αnx3),\displaystyle f_{N}(\widetilde{x},x_{3})=\frac{2}{L}\sum_{n=1}^{\infty}f_{n}^{N}(\widetilde{x})\sin(\alpha_{n}x_{3}), (19)

can be taken as the reconstruction to f(x)f(x). We finally remark that following [28], the stability of the Fourier method can be analogously deduced.

3.3 Numerical verification

We shall conduct several numerical experiments to verify the performance of the Fourier method proposed for the inverse source problem arising in the waveguide. The synthetic radiated fields were generated by solving the forward problem via direct integration. Utilizing the Green’s function

G(x,y)=i2Ln=1N0H0(1)(βn(k)|x~y~|)sin(αny3)sin(αnx3),x,yD,x~y~,G(x,y)=\frac{\rm i}{2L}\sum_{n=1}^{N_{0}}H_{0}^{(1)}(\beta_{n}(k)|\tilde{x}-\tilde{y}|)\sin(\alpha_{n}y_{3})\sin(\alpha_{n}x_{3}),\quad x,y\in D,\ \tilde{x}\neq\tilde{y}, (20)

the radiating solution to the Helmholtz equation (12) is given by

u(x;k)=V1G(x,y)f(y)dy,u(x;k)=-\int_{V_{1}}G(x,y)f(y)\mathrm{d}y,

where V1=V0×[0,L]V_{1}=V_{0}\times[0,L]. The Gauss quadrature is adopted to calculate the volume integrals over the 50350^{3} Gauss-Legendre points. Then the synthetic data is corrupted by artificial noise via uδ:=u+δr1|u|eiπr2u^{\delta}:=u+\delta r_{1}|u|\mathrm{e}^{\mathrm{i}\pi r_{2}} where r1r_{1} and r2r_{2} are two uniformly distributed random numbers ranging from 1-1 to 1, δ\delta is the noise level.

Now, we specify the details of the implementational aspects of the Fourier method. Let V0=[0.3,0.3]2,L=2.V_{0}=[-0.3,0.3]^{2},\,L=2. We aim to reconstruct the true source S(x),xV1S(x),x\in V_{1} by the Fourier expansion SN(x),xV1.S_{N}(x),\,x\in V_{1}. Throughout our numerical experiment, the Green’s function (20) is numerically truncated by N0=80.N_{0}=80. Further, given N+,N\in\mathbb{N}^{+}, the modal wavenumbers are set to be

N={10π3||:2,1||N}{102π3}.\mathcal{B}_{N}=\left\{\frac{10\pi}{3}|\bm{\ell}|:{\bm{\ell}}\in\mathbb{Z}^{2},1\leq|\bm{\ell}|_{\infty}\leq N\right\}\bigcup\left\{\frac{10^{-2}\pi}{3}\right\}.

The radiated data

{u(R,θj,zξ;αn2+β2):\displaystyle\Bigg{\{}u\left(R,\theta_{j},z_{\xi};\sqrt{\alpha_{n}^{2}+\beta_{\bm{\ell}}^{2}}\right): θj=jπ150,j=1,,300;zξ=ξL40,ξ=1,,40;\displaystyle\theta_{j}=\frac{j\pi}{150},j=1,\cdots,300;z_{\xi}=\frac{\xi L}{40},\,\xi=1,\cdots,40;
αn=2n12Lπ,n=0,1,,40;βN}\displaystyle\alpha_{n}=\frac{2n-1}{2L}\pi,\,n=0,1,\cdots,40;\beta_{\bm{\ell}}\in\mathcal{B}_{N}\Bigg{\}}

are measured on ΓR\Gamma_{R} with R=0.5R=0.5. For a visualization of the measurement surface, we refer to Figure 2 where the red points denote the receivers.

Refer to caption
Figure 2: Illustration of the measurement surface.

Once the radiated field is measured, the corresponding modes of the radiated data can be written as

{un(R,θj;β):θj=jπ150,j=1,,300,βN},n=1,2,.\left\{u_{n}\left(R,\theta_{j};{\beta_{\bm{\ell}}}\right):\theta_{j}=\frac{j\pi}{150},j=1,\cdots,300,\beta_{\bm{\ell}}\in\mathcal{B}_{N}\right\},\quad n=1,2,\cdots.

Next, in terms of (15)–(16) with ρ=0.6\rho=0.6 and truncation |m|70|m|\leq 70, we compute the following artificial Cauchy data of the Fourier modes

{un(ρ,Θj;β),νρun(ρ,Θj;β):Θj=jπ400,j=1,,800,βN},n=1,2,.\left\{u_{n}(\rho,\Theta_{j};\beta_{\bm{\ell}}),\partial_{\nu_{\rho}}u_{n}(\rho,\Theta_{j};\beta_{\bm{\ell}}):\Theta_{j}=\frac{j\pi}{400},j=1,\cdots,800,\beta_{\bm{\ell}}\in\mathcal{B}_{N}\right\},\ n=1,2,\cdots.

To calculate the Fourier coefficients f^,n,\widehat{f}_{{\bm{\ell}},n}, and f^𝟎,n\widehat{f}_{{\bm{0}},n} in (17) and (18), respectively, we use the trapezoidal rule to evaluate the surface integrals over Γρ\Gamma_{\rho} and the volume integral over V0V_{0} is evaluated over a 200×200200\times 200 grid of uniformly spaced points xmV0,m=1,,2002.x_{m}\in V_{0},m=1,\cdots,200^{2}. Finally, we compute the point-wise values fN(x~,x3)f_{N}(\widetilde{x},x_{3}) by (19) with fnN(x~)f_{n}^{N}(\widetilde{x}) determined by (14).

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Figure 3: The exact source mode f~\widetilde{f}. Left: surface plot; Right: contour plot.
Example 1.

In the first example, we test the performance of the method by considering the reconstruction of the source function which has finite Fourier modes. Specifically, the source function is given by

f1(x1,x2,x3)=2Ln=140f~(x1,x2)sinαnx3,f_{1}(x_{1},x_{2},x_{3})=\frac{2}{L}\sum_{n=1}^{40}\widetilde{f}(x_{1},x_{2})\sin\alpha_{n}x_{3},

with

f~(x1,x2)=1.1e200((x10.01)2+(x20.12)2)100(x22x12)e90(x12+x22).\widetilde{f}(x_{1},x_{2})=1.1\mathrm{e}^{-200\left((x_{1}-0.01)^{2}+(x_{2}-0.12)^{2}\right)}-100\left(x_{2}^{2}-x_{1}^{2}\right)\mathrm{e}^{-90\left(x_{1}^{2}+x_{2}^{2}\right)}.

In this example, we set δ=5%\delta=5\% and N=4N=4. The nn-th Fourier mode fnf_{n} of the exact source function is independent of nn and fn(x1,x2)f~(x1,x2),n=1,2,f_{n}(x_{1},x_{2})\equiv\widetilde{f}(x_{1},x_{2}),\,n=1,2,\cdots. We refer to Figure 3 for a display of f~\widetilde{f}. Theoretically, once a Fourier mode is recovered, the source function can be approximated by multiplying the factor n=140sinαnx3\sum_{n=1}^{40}\sin\alpha_{n}x_{3}. Nevertheless, we have yet to determine the precise expression of the exact source. Thus, for each n=1,2,,40,n=1,2,\cdots,40, we reconstruct the Fourier modes f~n(x1,x2)\widetilde{f}_{n}(x_{1},x_{2}) and exhibit the reconstruction of several different Fourier modes in Figure 4. The results in Figure 3 and Figure 4 demonstrate that all the Fourier modes are well recovered, and the reconstruction error is around 4.53%4.53\%.

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Figure 4: The recovered Fourier mode f~n\widetilde{f}_{n} of the source f1f_{1}. Row 1: surface plots; Row 2: contour plots. Column 1: n=1n=1; Column 2: n=15n=15; Column 3: n=30n=30.

Next, we reconstruct the source at different slices: x3=0.15,0.85x_{3}=0.15,0.85, and 1.351.35. The reconstructions are depicted in Figure 5, which illustrate that the profile of the source function can be well captured at these locations.

This example shows that when the exact source has limited Fourier modes, these Fourier modes can be well-reconstructed. Furthermore, the source can also be recovered satisfactorily under the Fourier expansion. However, most of the source functions may not have limited Fourier expansions. So we shall reconstruct a more general source function in the next example.

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Figure 5: The exact source f1f_{1} and recovered source fNf_{N} at different x3x_{3}. Row 1: exact sources; Row 2: reconstructions; Column 1: x3=0.15x_{3}=0.15; Column 2: x3=0.85x_{3}=0.85; Column 3: x3=1.35x_{3}=1.35.
Example 2.

The second example is devoted to reconstructing a mountain-shaped function described by

f2(x1,x2,x3)=1.1e200((x10.01)2+(x20.12)2+x32)100(x12x22)e90(x12+x22+x32).f_{2}(x_{1},x_{2},x_{3})=1.1\mathrm{e}^{-200\left((x_{1}-0.01)^{2}+(x_{2}-0.12)^{2}+x_{3}^{2}\right)}-100\left(x_{1}^{2}-x_{2}^{2}\right)\mathrm{e}^{-90\left(x_{1}^{2}+x_{2}^{2}+x_{3}^{2}\right)}.

Different from f1f_{1} which has limited Fourier expansion with the same Fourier mode, the source function f2f_{2} is more general. Here the truncation N=N(δ)N=N(\delta) is set to be 5[logδ],5\left[\log\delta\right], with [X][X] denoting the largest integer that is smaller than X+1X+1. In this way, the influence of the magnitude of noise is investigated in this example. For a quantitative evaluation of the inversion scheme, we compute the relative L2L^{2} errors

Err=fNfL2(V1)fL2(V1)anderr(x3)=fN(,x3)f(,x3)L2(V0)f(,x3)L2(V0),x3[0,L].Err=\frac{\|f_{N}-f\|_{L^{2}(V_{1})}}{\|f\|_{L^{2}(V_{1})}}\ \text{and}\ err(x_{3})=\frac{\|f_{N}(\cdot,x_{3})-f(\cdot,x_{3})\|_{L^{2}(V_{0})}}{\|f(\cdot,x_{3})\|_{L^{2}(V_{0})}},\quad x_{3}\in[0,L].

First, δ=5%\delta=5\% is used and we compare ff and fNf_{N} at x3=0.25x_{3}=0.25 in Figure 6. One can see from the results that the source function is well-reconstructed. For an in-depth slice view, we plot several cross-sections of them in Figure 7. We can see from Figure 7 that the reconstruction matches almost perfectly with the exact source at these typical cross sections. Especially, even if the source value is close to 0,0, the reconstruction is still satisfactory (see Figure 7(b) for example).

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Figure 6: The exact source f2f_{2} and recovered source fNf_{N} at x3=0.25x_{3}=0.25. Row 1: exact source. Row 2: reconstruction. Column 1: surface plots; Column 2: contour plots.
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(a) x2=0.002,x3=0.4x_{2}=-0.002,x_{3}=0.4
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(b) x2=0.002,x3=0.6x_{2}=-0.002,x_{3}=0.6
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(c) x2=0.002,x3=0.15x_{2}=-0.002,x_{3}=0.15
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(d) x2=0.082,x3=0.15x_{2}=-0.082,x_{3}=0.15
Figure 7: The reconstructed source is plotted against the exact source f2f_{2} at different cross-sections.

Further, we compute the recovery errors at different x3x_{3} locations subject to different noise levels δ.\delta. Table 1 shows that the reconstructions are reasonably stable in the sense that the quality of the inversion improves as the noise level decreases.

Table 1: The relative errors of the reconstruction of f2f_{2} with different noise levels δ.\delta.
δ\delta 1%1\% 5%5\% 10%10\% 20%20\%
N(δ)N(\delta) 2020 1010 1010 55
err(0.2)err(0.2) 1.18%1.18\% 1.96%1.96\% 3.72%3.72\% 5.27%5.27\%
err(0.3)err(0.3) 1.15%1.15\% 1.90%1.90\% 3.81%3.81\% 8.42%8.42\%
err(0.4)err(0.4) 1.23%1.23\% 1.52%1.52\% 3.20%3.20\% 6.30%6.30\%
ErrErr 2.77%2.77\% 3.03%3.03\% 4.65%4.65\% 9.39%9.39\%

3.4 The far-field case

In this last subsection, we briefly discuss the inverse source problem using the far-field data. We assume V=0V=0 in this case. Under Assumption (A) the outgoing solution to (3) can be represented by

u(x,k)=i4n=1N0B~RH0(1)(βn(k)|x~y~|)fn(y~)dy~sin(αnx3).u(x,k)=\frac{\rm i}{4}\sum_{n=1}^{N_{0}}\int_{\widetilde{B}_{R}}H_{0}^{(1)}(\beta_{n}(k)|\tilde{x}-\tilde{y}|)f_{n}(\tilde{y}){\rm d}\tilde{y}\sin(\alpha_{n}x_{3}).

From the asymptotic expansion of the fundamental solution iH0(1)(k|x~y~|)/4\mathrm{i}H^{(1)}_{0}(k|\tilde{x}-\tilde{y}|)/4 of the two-dimensional Helmholtz equation [10] as |x~||\tilde{x}|\to\infty, we have

u(x,k)=i4n=1N01+i4πkeiβn(k)|x~||x~|2eiβn(k)y~x~^fn(y~)dy~sin(αnx3)+𝒪(1|x~|),\displaystyle u(x,k)=\frac{\rm i}{4}\sum_{n=1}^{N_{0}}\frac{1+\rm i}{4\sqrt{\pi k}}\frac{\mathrm{e}^{{\rm i}\beta_{n}(k)|\tilde{x}|}}{\sqrt{|\tilde{x}|}}\int_{\mathbb{R}^{2}}\mathrm{e}^{-{\rm i}\beta_{n}(k)\tilde{y}\cdot\hat{\tilde{x}}}f_{n}(\tilde{y}){\rm d}\tilde{y}\sin(\alpha_{n}x_{3})+\mathcal{O}\left(\frac{1}{|\tilde{x}|}\right),

where x~^=x~/|x~|𝕊={x~2:|x~|=1}\hat{\tilde{x}}=\tilde{x}/|\tilde{x}|\in\mathbb{S}=\{\tilde{x}\in\mathbb{R}^{2}:\,|\tilde{x}|=1\} is the observation angle. Since eiβn(k)|x~|\mathrm{e}^{{\rm i}\beta_{n}(k)|\tilde{x}|} is exponentially decaying for those nn such that k<αnk<\alpha_{n}, we define the far-field pattern 𝒜(k,x~^,x3)\mathcal{A}_{\infty}(k,\hat{\tilde{x}},x_{3}) as follows

𝒜(k,x~^,x3)\displaystyle\mathcal{A}_{\infty}(k,\hat{\tilde{x}},x_{3}) ={n:k>αn}2eiβn(k)y~x~^fn(y~)dy~sin(αnx3)\displaystyle=\sum_{\{n:k>\alpha_{n}\}}\int_{\mathbb{R}^{2}}\mathrm{e}^{-{\rm i}\beta_{n}(k)\tilde{y}\cdot\hat{\tilde{x}}}f_{n}(\tilde{y}){\rm d}\tilde{y}\sin(\alpha_{n}x_{3})
={n:k>αn}f^n(βn(k)x~^)sin(αnx3).\displaystyle=\sum_{\{n:k>\alpha_{n}\}}\hat{f}_{n}(\beta_{n}(k)\hat{\tilde{x}})\sin(\alpha_{n}x_{3}). (21)

Let I1I_{1} be an interval such that I1(α1,α2)I_{1}\subset(\alpha_{1},\alpha_{2}) and let x3x_{3} be fixed such that sinα1x30\sin\alpha_{1}x_{3}\neq 0. As can be seen in (3.4), if the multi-wavenumber far-field data {𝒜(k,x~^,x3):x~^𝕊,kI1}\{\mathcal{A}_{\infty}(k,\hat{\tilde{x}},x_{3}):\hat{\tilde{x}}\in\mathbb{S},k\in I_{1}\} is given, then

𝒜(k,x~^,x3)=f^1(β2(k)x~^)sin(α1x3).\mathcal{A}_{\infty}\left(k,\hat{\tilde{x}},x_{3}\right)=\hat{f}_{1}\left(\beta_{2}(k)\hat{\tilde{x}}\right)\sin(\alpha_{1}x_{3}).

This implies that the far field of only one propagating mode corresponding to f1f_{1} is detected which gives the following Fourier transform

{f^1(ξ~):|ξ~|<α22α12}.\left\{\hat{f}_{1}(\tilde{\xi}):|\tilde{\xi}|<\sqrt{\alpha_{2}^{2}-\alpha_{1}^{2}}\right\}.

Thus, by the analyticity of f^1(ξ~)\hat{f}_{1}(\tilde{\xi}) and the inverse Fourier transform we can determine f1f_{1} and even derive a stability estimate by analytic continuation. Moreover, let I2(α2,α3)I_{2}\subset(\alpha_{2},\alpha_{3}), if f1f_{1} is recovered and {𝒜(k,x~^,x3):x~^𝕊,kI2}\{\mathcal{A}_{\infty}(k,\hat{\tilde{x}},x_{3}):\hat{\tilde{x}}\in\mathbb{S},k\in I_{2}\} is available, in a similar manner we can determine f2f_{2} by detecting the far-field of the corresponding single mode. Proceeding recursively in this way, we get the following uniqueness result.

Theorem 3.3.

Let x3x_{3} be chosen such that sinαnx30\sin\alpha_{n}x_{3}\neq 0 for 1nN01\leq n\leq N_{0}. The far-field {𝒜(k,x~^,x3):x~^𝕊,ki=1N0Ii,Ii(αi,αi+1)}\{\mathcal{A}_{\infty}(k,\hat{\tilde{x}},x_{3}):\hat{\tilde{x}}\in\mathbb{S},k\in\cup_{i=1}^{N_{0}}I_{i},\,I_{i}\subset(\alpha_{i},\alpha_{i+1})\} uniquely determines ff.

Remark 3.2.

Compared with Theorem 3.2, Theorem 3.3 requires data measured at more wavenumbers. Physically speaking, a possible reason accounting for the necessity of this extra data is that part of the information is only involved in the evanescent modes which decay drastically. Hence, this information cannot be accessed or retrieved from the far-field data. Thus, more far-field data is inevitably needed to compensate for the lack of information towards establishing the uniqueness.

Remark 3.3.

We would like to highlight that the uniqueness of the inverse source problem is established by incorporating the far-field due to a single mode one by one from low to high wavenumbers. This framework of derivation has the advantage of avoiding the situation where multiple propagating modes are concurrently present. Conversely, for instance, if we only collect the data {𝒜(k,x~^):x~^𝕊,kI2}\{\mathcal{A}_{\infty}(k,\hat{\tilde{x}}):\hat{\tilde{x}}\in\mathbb{S},k\in I_{2}\}, then we are only able to find the superposed quantity f^1(β1(k)x~^)+f^2(β2(k)x~^)\hat{f}_{1}(\beta_{1}(k)\hat{\tilde{x}})+\hat{f}_{2}(\beta_{2}(k)\hat{\tilde{x}}). In this case, it would be difficult to separate and recover either f1f_{1} or f2f_{2} from the sum.

4 Inverse problem II: determining the potential

In this section, an inverse potential problem in the waveguide is considered. We assume that VV is real-valued and f0f\equiv 0 in this section. The key ingredient in the analysis is applying results in Theorem 2.1 and an argument of analytic continuation.

Let k>α1k>\alpha_{1} and d𝕊d\in\mathbb{S} be respectively the wavenumber and incident direction, and denote uinc(x,k,d)=eik2α12x~dsinα1x3u^{\rm inc}(x,k,d)=\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d}\sin\alpha_{1}x_{3} the incident field. Then the total field is given by u=uinc+usu=u^{\rm inc}+u^{s} where usu^{s} is the scattered field produced by uincu^{\rm inc} and the potential V(x~)V(\tilde{x}). Consider the following homogeneous Schrödinger equation with uu satisfying the boundary conditions (2)

Δu+Vuk2u=0,in D.-\Delta u+Vu-k^{2}u=0,\quad\text{in }D. (22)

We are interested in the inverse problem of determining VV from u(x,k,d)u(x,k,d) on ΓR\Gamma_{R}. Here we employ u(x,k,d)u(x,k,d) to signify the dependence of uu on kk and dd.

Under the above configuration, the scattered field satisfies

Δus+Vusk2us=Vuinc,in D-\Delta u^{s}+Vu^{s}-k^{2}u^{s}=-Vu^{\rm inc},\quad\text{in }D (23)

and the boundary conditions (2). Multiplying both sides of (23) by the factor eik2α12x~d1sinα1x3\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\sin\alpha_{1}x_{3} with d1𝕊d_{1}\in\mathbb{S} and integrating by parts over CRC_{R}, we obtain

B~RVeik2α12(d+d1)dx~=B~R(νx~u1(x~,k)eik2α12x~d1ik2α12d1νx~u1(x~,k)eik2α12x~d1)dx~CRVuseik2α12x~d1sinα1x3dx=B~R(νx~u1(x~,k)eik2α12x~d1ik2α12d1νx~u1(x~,k)eik2α12x~d1)dx~+𝒪(1k).\begin{split}&\quad\int_{\widetilde{B}_{R}}V\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}(d+d_{1})}{\rm d}\tilde{x}\\ &=\int_{\partial\widetilde{B}_{R}}\!\!\left(\partial_{\nu_{\tilde{x}}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}-{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}d_{1}\cdot\nu_{\tilde{x}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\!\right)\!{\rm d}\tilde{x}\\ &\quad-\int_{C_{R}}Vu^{s}\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\sin\alpha_{1}x_{3}{\rm d}x\\ &=\int_{\partial\widetilde{B}_{R}}\!\!\left(\partial_{\nu_{\tilde{x}}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}-{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}d_{1}\cdot\nu_{\tilde{x}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\!\right)\!{\rm d}\tilde{x}\\ &\quad+\mathcal{O}\left(\frac{1}{k}\right).\end{split} (24)

where u1u_{1} is the first Fourier mode of uu. As the inhomogeneous term Vuinc-Vu^{\rm inc} on the right-hand side of the equation (23) has a single Fourier mode in the x3x_{3} variable, in the last equality, we can use the resolvent estimate in Theorem 2.1 to derive

CRVuseik2α12x~d1sinα1x3dx=𝒪(1k).\int_{C_{R}}Vu^{s}\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\sin\alpha_{1}x_{3}{\rm d}x=\mathcal{O}\Big{(}\frac{1}{k}\Big{)}.

Notice that {k2α12(d+d1):d,d1𝕊}={ξ:|ξ|2k2α12}.\left\{\sqrt{k^{2}-\alpha_{1}^{2}}(d+d_{1}):d,d_{1}\in\mathbb{S}\right\}=\left\{\xi:|\xi|\leq 2\sqrt{k^{2}-\alpha_{1}^{2}}\right\}. We next show that the boundary measurements {u(x,k,d):xΓR,kI,d𝕊}\{u(x,k,d):x\in\Gamma_{R},k\in I,d\in\mathbb{S}\} uniquely determine VV. Here I=[K0,K1]I=[K_{0},K_{1}] with K1>K0>max{M,α1}K_{1}>K_{0}>\max\{M,\alpha_{1}\} where MM is specified in Theorem 2.1.

Let V1V_{1} and V2V_{2} be two potential functions. Assume that u(1)u^{(1)} and u(2)u^{(2)} are solutions to (22) corresponding to V1V_{1} and V2V_{2}, respectively. Denote W=V1V2W=V_{1}-V_{2} and v=u(1)u(2)v=u^{(1)}-u^{(2)}. Substituting uu and VV in (24) by u(1),V1u^{(1)},V_{1} and u(2),V2u^{(2)},V_{2}, respectively, and taking subtraction yields

B~RWeik2α12(d+d1)dx~\displaystyle\int_{\widetilde{B}_{R}}W\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}(d+d_{1})}{\rm d}\tilde{x}
=B~R(νx~v1(x~,k)eik2α12x~d1ik2α12d1νx~v1(x~,k)eik2α12x~d1)dx~\displaystyle=\int_{\partial\widetilde{B}_{R}}\left(\partial_{\nu_{\tilde{x}}}v_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}-{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}d_{1}\cdot\nu_{\tilde{x}}v_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\right){\rm d}\tilde{x}
+𝒪(1k).\displaystyle\quad+\mathcal{O}\Big{(}\frac{1}{k}\Big{)}.

Now it suffices to show W=0W=0 if v(x,k,d)=0v(x,k,d)=0 for all d𝕊d\in\mathbb{S} and kIk\in I. As v=v(x,k,d)v=v(x,k,d) is analytic for kIk\in I, we immediately have v(x,k,d)=0v(x,k,d)=0 for all kMk\geq M. Moreover, from the Dirichlet-to-Neumann map the normal derivative νx~v1\partial_{\nu_{\tilde{x}}}v_{1} can be computed from

νx~v1=Tv1=mβ1am1Hm(1)(β1R)Hm(1)(β1R)eimθsinα1x3.\partial_{\nu_{\tilde{x}}}v_{1}=Tv_{1}=\sum_{m\in\mathbb{Z}}\beta_{1}a_{m}^{1}\frac{{H_{m}^{(1)}}^{\prime}(\beta_{1}R)}{H_{m}^{(1)}(\beta_{1}R)}\mathrm{e}^{{\rm i}m\theta}\sin\alpha_{1}x_{3}.

where am1a_{m}^{1} are the Fourier coefficients

am1=πLRCReimθsin(α1x3)vdx,x=(rcosθ,rsinθ,x3).a_{m}^{1}=\sqrt{\frac{\pi}{LR}}\int_{C_{R}}\mathrm{e}^{-{\rm i}m\theta}\sin(\alpha_{1}x_{3})\,v{\rm d}x,\quad x=(r\cos\theta,r\sin\theta,x_{3}).

Thus, v(x,k,d)=0v(x,k,d)=0 gives νx~v(x,k,d)=0\partial_{\nu_{\tilde{x}}}v(x,k,d)=0. Consequently, from (24) we have

W^(ξ)𝒪(1k)for all|ξ|2k2α12.\widehat{W}(\xi)\leq\mathcal{O}\Big{(}\frac{1}{k}\Big{)}\quad\text{for all}\,|\xi|\leq 2\sqrt{k^{2}-\alpha_{1}^{2}}. (25)

As v(x,k,d)=0v(x,k,d)=0 on ΓR\Gamma_{R} holds for all kMk\geq M, by letting kk\to\infty in (25) we arrive at

W^(ξ)=0,ξ2,\widehat{W}(\xi)=0,\quad\xi\in\mathbb{R}^{2},

which yields W=0W=0 by the inverse Fourier transform. This implies the uniqueness of the inverse problem. In summary, we have the following theorem.

Theorem 4.1.

The multi-frequency measurement {u(x,k,d):xΓR,kI,d𝕊}\{u(x,k,d):x\in\Gamma_{R},k\in I,d\in\mathbb{S}\} uniquely determines VV.

Now we discuss the stability. Assume that u1s(x,k,d)u_{1}^{s}(x,k,d) and u2s(x,k,d)u_{2}^{s}(x,k,d) are the scattered field corresponding to the incident wave uinc=eik2α12x~dsinα1x3u^{\rm inc}=\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d}\sin\alpha_{1}x_{3} and potentials V1V_{1} and V2V_{2}, respectively. Let s>0s>0 be an arbitrary positive constant. Define a real-valued function space

Q={VHs(D)L(D):\displaystyle\mathcal{E}_{Q}=\{V\in H^{s}(D)\cap L^{\infty}(D):\ VHs(D)Q,VL(D)Q,\displaystyle\|V\|_{H^{s}(D)}\leq Q,\ \|V\|_{L^{\infty}(D)}\leq Q,
suppVCR,V:D}.\displaystyle\mathrm{supp}V\subset C_{R},~{}V:D\rightarrow\mathbb{R}\}.

Utilizing the resolvent estimates and the estimate (24), we have the following stability estimate (the proof follows [27] in a straightforward way by applying the quantitative analytic continuation. Thus we omit it for brevity).

Theorem 4.2.

Let V1,V2QV_{1},V_{2}\in\mathcal{E}_{Q}. The following increasing stability estimate holds

V1V2L2(D)2Kαϵ2+1Kβ(ln|lnϵ|)β,\displaystyle\|V_{1}-V_{2}\|_{L^{2}(D)}^{2}\lesssim K^{\alpha}\epsilon^{2}+\frac{1}{K^{\beta}(\ln|\ln\epsilon|)^{\beta}}, (26)

where

ϵ2=2supkI,d𝕊(k2u1s(x,k,d)u2s(x,k,d)L2(ΓR)2+T(u1s(x,k,d)u2s(x,k,d))L2(ΓR)2)\epsilon^{2}=2\sup_{k\in I,\,d\in\mathbb{S}}\Big{(}k^{2}\|u^{s}_{1}(x,k,d)-u^{s}_{2}(x,k,d)\|_{L^{2}(\Gamma_{R})}^{2}+\|T(u^{s}_{1}(x,k,d)-u^{s}_{2}(x,k,d))\|_{L^{2}(\Gamma_{R})}^{2}\Big{)}

and I=[K0,K]I=[K_{0},K] with K>MK>M, α=32(3+2s)\alpha=\frac{3}{2(3+2s)} and β=s2(3+2s)\beta=\frac{s}{2(3+2s)}.

The stability estimate (26) implies the uniqueness. It consists of two parts: the data discrepancy and the high-frequency tail. The former is of the Lipschitz type. The latter decreases as KK increases which makes the problem have an almost Lipschitz stability. Overall, the result reveals that the problem becomes more stable when higher-frequency data is used.

5 Inverse problem III: simultaneous recovery of source and potential

This section is devoted to the co-inversion model of simultaneously reconstructing the source and potential from active measurements. In this model, given the incident wave uinc(x~,x3)=eik2α12x~dsinα1x3u^{\rm inc}(\tilde{x},x_{3})=\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d}\sin\alpha_{1}x_{3} with incident direction d𝕊d\in\mathbb{S}, the total field u=uinc+usu=u^{\rm inc}+u^{s} satisfies the wave equation eq. 1 and the boundary conditions (2). We also assume that ff is real-valued and V0V\geq 0 in this section.

We are interested in the inverse problem of determining both ff and VV from u|ΓRu|_{\Gamma_{R}}. To that end, we apply the method developed in [25] to the current geometry of a waveguide. We first present a preliminary result for the subsequent analysis.

Lemma 5.1.

Let d𝕊d\in\mathbb{S} and gH1(B~R)g\in H^{1}(\widetilde{B}_{R}) with suppgB~R\text{supp}g\subset\widetilde{B}_{R} and gH1(B~R)Q\|g\|_{H^{1}(\widetilde{B}_{R})}\leq Q. Then the following estimate holds:

|B~Rg(x)eik2α12x~ddx~|C(Q)k,\left|\int_{\widetilde{B}_{R}}g(x)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d}{\rm d}\tilde{x}\right|\leq\frac{C(Q)}{k},

where C(Q)C(Q) is a generic constant depending on QQ.

Proof.

Since d=(d1,d2)𝕊d=(d_{1},d_{2})\in\mathbb{S}, without loss of generality we assume that the |d1|2/2|d_{1}|\geq\sqrt{2}/2. Using integration by parts yields

B~Rg(x~)eik2α12x~ddx~\displaystyle\int_{\widetilde{B}_{R}}g(\tilde{x})\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d}\,{\rm d}\tilde{x} =1ik2α12d1B~Rx1(eik2α12x~d)g(x~)dx~\displaystyle=\frac{1}{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}d_{1}}\int_{\widetilde{B}_{R}}\frac{\partial}{\partial x_{1}}\left(\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d}\right)g(\tilde{x})\,{\rm d}\tilde{x}
=1ik2α12d1B~Reik2α12x~dgx1dx~,\displaystyle=-\frac{1}{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}d_{1}}\int_{\widetilde{B}_{R}}\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d}\frac{\partial g}{\partial x_{1}}{\rm d}\tilde{x},

which gives by Hölder’s inequality

|B~Rg(x~)eik2α12x~ddx~|CgH1(B~R)1k.\left|\int_{\widetilde{B}_{R}}g(\tilde{x})\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d}\,{\rm d}\tilde{x}\right|\leq C\|g\|_{H^{1}(\widetilde{B}_{R})}\frac{1}{k}.

The proof is completed. ∎

In the case of the equation (1) with an inhomogeneous term ff, by multiplying both sides of (23) by eik2α12x~d1sinα1x3\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\sin\alpha_{1}x_{3} with d1𝕊d_{1}\in\mathbb{S} and integrating by parts over CRC_{R}, (24) now becomes

B~RVeik2α12(d+d1)dx~\displaystyle\int_{\widetilde{B}_{R}}V\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}(d+d_{1})}{\rm d}\tilde{x}
=B~R(νx~u1(x~,k)eik2α12x~d1ik2α12d1νx~u1(x~,k)eik2α12x~d1)dx~\displaystyle=\int_{\partial\widetilde{B}_{R}}\left(\partial_{\nu_{\tilde{x}}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}-{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}d_{1}\cdot\nu_{\tilde{x}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\right){\rm d}\tilde{x}
CRVuseik2α12x~d1sinα1x3dx+CRfeik2α12x~d1sinα1x3dx\displaystyle\quad-\int_{C_{R}}Vu^{s}\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\sin\alpha_{1}x_{3}{\rm d}x+\int_{C_{R}}f\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\sin\alpha_{1}x_{3}{\rm d}x
=B~R(νx~u1(x~,k)eik2α12x~d1ik2α12d1νx~u1(x~,k)eik2α12x~d1)dx~\displaystyle=\int_{\partial\widetilde{B}_{R}}\left(\partial_{\nu_{\tilde{x}}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}-{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}d_{1}\cdot\nu_{\tilde{x}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}\right){\rm d}\tilde{x}
+B~Rf1eik2α12x~d1dx~+𝒪(1k).\displaystyle\quad+\int_{\widetilde{B}_{R}}f_{1}\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}{\rm d}\tilde{x}+\mathcal{O}\left(\frac{1}{k}\right). (27)

By applying Lemma 5.1 we have

B~Rf1eik2α12x~d1dx~=𝒪(1k),\int_{\widetilde{B}_{R}}f_{1}\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}{\rm d}\tilde{x}=\mathcal{O}\Big{(}\frac{1}{k}\Big{)},

and then (5) becomes

B~RVeik2α12(d+d1)dx~\displaystyle\int_{\widetilde{B}_{R}}V\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}(d+d_{1})}{\rm d}\tilde{x} =B~Rνx~u1(x~,k)eik2α12x~d1\displaystyle=\int_{\partial\widetilde{B}_{R}}\partial_{\nu_{\tilde{x}}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}
ik2α12d1νx~u1(x~,k)eik2α12x~d1dx~+𝒪(1k).\displaystyle\quad-{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}d_{1}\cdot\nu_{\tilde{x}}u_{1}(\tilde{x},k)\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d_{1}}{\rm d}\tilde{x}+\mathcal{O}\Big{(}\frac{1}{k}\Big{)}. (28)

As (5) is similar to (24), repeating the previous arguments we have that the active boundary data {u(x,k,d):xΓR,kI,d𝕊}\{u(x,k,d):x\in\Gamma_{R},k\in I,d\in\mathbb{S}\} corresponding to the incident wave and source uniquely determine VV. Once VV is known, we can also recover ff. In summary, we have the following uniqueness result:

Theorem 5.1.

The active multi-wavenumber boundary measurements

{u(x,k,d):xΓR,kI,d𝕊}\{u(x,k,d):x\in\Gamma_{R},\ k\in I,\ d\in\mathbb{S}\}

corresponding to the incident wave eik2α12x~dsinα1x3\mathrm{e}^{{\rm i}\sqrt{k^{2}-\alpha_{1}^{2}}\tilde{x}\cdot d}\sin\alpha_{1}x_{3} uniquely determine VV with unknown ff. As a consequence of the recovery of VV, the source ff can be uniquely determined as well by the passive boundary measurements

{u(x,kn,j):xΓR,|kn,j|M}{u(x,k):xΓR,kI}.\{u(x,k_{n,j}):x\in\Gamma_{R},|k_{n,j}|\leq M\}\cup\{u(x,k):x\in\Gamma_{R},k\in I\}.

6 Conclusion

This work presents a resonance-free region and resolvent estimates for the resolvent of the Schrödinger operator in a planar waveguide in three dimensions. As an application, theoretical uniqueness and stability for several inverse scattering problems are established. The analysis only requires the limited aperture Dirichlet data at multiple wavenumbers. Moreover, we develop an effective Fourier-based reconstruction method for the inverse source problem. We believe that the method can be applied to the biharmonic wave equation in a planar waveguide with Navier boundary conditions and the geometry of tubular waveguides. A more challenging analytic problem is the direct and inverse elastic scattering in a waveguide. In this case, we may not have a straightforward Fourier decomposition such as (6) due to the coupled pressure and shear waves. We hope to report the relevant progress elsewhere in the future.

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